NASA

NASA

Scientific and Technical

publications

Special

Reference

Conference

Catalog -:_ -

of

Publications,

Publications,

Publications, and

Technical Papers

1977- 1986

[NASA-SP-7063_NASA SCIENTIFIC AND

TECHNICAL PUBLICATIONS: A CATALOG OF

SPECIAL[NASA) 390 P Avail: NTIS HC £ree as

PR-655_ Z_AZA Scientific and Technical

iaformatzol. _aciiit¥, P.O. Box 8757, _£

N87-302 18

U n cl as

GI/82 0 |02761

NASA SP-7063 (p_

NASA

ScientificandTechnical

Special

Reference

publications

Conference

A Catalog

of

Publications,

Publications,

Publications, and

Technical Papers

1977- 1986

Scientific and Technical Information Division 1987

National Aeronautics and Space Administration

Washington, DC
This document is available from the National Technical Information Service (NTIS), Springfield,

Virginia 22161 as PR 655B.
PREFACE

The pursuit of human knowledge through scientific research and technical endeavor has vastly

expanded understanding of our world and universe. The contributions of NASA in scientific and technical

research and development affect not only our understanding and use of aeronautics and space but also

touch our daily lives. Geologists, oceanographers, meteorologists, aircraft engineers, aerospace decisionmakers, land-use planners, historians, and rescue teams all make use of the results of NASA_ research.

These findings are published as part of NASA's mandate to disseminate the results of the agency's

far-reaching research and development.

The purpose of this catalog is to provide a listing of NASA publications from four series in the NASA

scientific and technical information database entered during the years 1977 through 1986. An earlier

catalog, Records of Achievement, NASA SP-470, accession number N83-33792, is available for a listing

of earlier NASA publications not covered by this catalog. For non-NASA publications, consult two

semimonthly abstract journals which cover all aspects of aeronautics and space research and development and applications, nationally and worldwide: STAR (Scientific and Technical Aerospace Reports),

which focuses on scientific and technical reports, and IAA (International Aerospace Abstracts), which

covers the open literature. These are available by subscription from, respectively, the U.S. Government

Printing Office and the American Institute of Aeronautics and Astronautics, Inc., 555 West 57th Street,

New York, NY 10019 (212-247-6500).

Specifically, this catalog includes those publicly available reports in four NASA report series: Special

Publications (SPs), Reference Publications (RPs), Conference Publications (CPs), and Technical Papers

(TPs). The type of presentation determines the series.

Special Publications are often concerned with subjects of substantial public

interest. They report scientific and technical information derived from NASA

programs and are for audiences of diverse technical backgrounds.

Research Publications contair_ compilations of scientific and technical data

deemed to be of continuing reference value.

Conference Publications record the proceedings of scientific and technical

symposia and other professional meetings sponsored or cosponsored by

NASA.

Technical Papers present the results of significant research conducted by

NASA scientists and engineers.

Presented here are the citations for each of these publications. An explanation of the elements in typical

citations follows. Please note that these publications are available for purchase either from the U.S.

Government Printing Office for a limited time, depending upon public demand, or indefinitely from the

National Technical Information Service (NTIS). They are also available at any Federal Regional Depository

Library. Availability information follows, including current NTIS price schedules, which are keyed to the

price code in the citation.
TYPICAL CITATION AND ABSTRACT

ACCESSION NUMBER

TITLE

AUTHOR

REPORT NUMBERS

PRICE CODE

COSA_ CODE

NASA SPONSORED

,IRON MICROFICHE

N85-23683"# National Aeronautics and Space Administration, t CORPORATE SOURCE

Washington, D,C.

MODEL RESEARCH: THE NATIONAL ADVISORY COMMITTEE

FOR AERONAUTICS, 1915.1958, VOLUME 1

A. ROLAND 1984 432 p refs 2 Vol,

_" PUBLICATION DATE

(NASA-SP-4103-VOL-1; NAS 121:4103-VOL-1) Avail: NTIS HC

A19/MF A01; also available from SOD HC $26,00 as set of 2

CSCL 01B _ AVAILABILITY SOURCE

The National Advisory Committee for Aeronautics, the

predecessor of NASA, was the premier aeronautical research

organization in the United States. It conducted scientific study of

the problems of flight with a view to their practical solution. This

institutional history traces the birth and evolution of the NACA

and analyzes such recurrent themes as the roles of science and

engineering, the influence of politics on technology, the way in

which the institution shapes technology and technology shapes

the institution, the contributions of key individuals, the nature of

the research process, and the relation between military and civilian

aviation. Author

TYPICAL CITATION AND SUBJECT TERMS

ACCESSION NUMBER

TITLE

AUTHORR

REPORT NUMBERS

PRICE CODE

NASA SPONSORED

F- ON MICROFICHE

=- N82-26217'# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECTS OF WING-LEADING-EDGE MODIFICATIONS ON A

FULL-SCALE, LOW-WING GENERAL AVIATION AIRPLANE:

WIND-TUNNEL INVESTIGATION OF HIGH-ANGLE-OF-ATTACK

AERODYNAMIC CHARACTERISTICS

W. A, NEWSOM, JR., D. R. SATRAN, and J. L. JOHNSON, JR

Jun. 1982 107 p refs

(NASA-TP-2011; L-15101; NAS 1.60:2011) Avail: NTIS HC _-

A06/MF A01 CSCL 01A q

AERODYNAMIC CHARACTERISTICS, AERODYNAMIC

STALLING, ANGLE OF ATTACK, GENERAL AVIATION

AIRCRAFT. LEADING EDGES, WIND TUNNEL TESTS

CORPORATE SOURCE

AVAILABILITY SOURCE

COSATI CODE

iv
SOURCES OF NASA PUBLICATIONS

The source from which a publication is available to the public is given on the last line of the citation.

Addresses for these organizations are given below.

U.S. Government Printing Office

Superintendent of Documents

U.S. Government Printing Office

Washington, DC 20402

(202) 783-3238 Price and order information

Publications are available from GPO in hardcopy for a limited time after publication and initial distribution.

The price and order number are given following the availability line.

National Technical Information Service

National Technical Information Service

5285 Port Royal Rd.

Springfield, VA 22161

(703) 487-4780 Information or document accession number

(703) 487-4650 Sales desk, price information

(703) 487-4630 Subscription information for subscription bibliographies (in the SP-7000 series)

Prices for hardcopy and microfiche are indicated by a price code preceded by the letters HC or MF in

the citation. Current values for the price codes are given in the NTIS Price Schedules. Publications

available on microfiche are identified by a # symbol following the accession number. Note: The # symbol

is used without regard to the source or quality of the microfiche.

Public Collections of NASA Documents

Federal Depository Library Program: In order to provide the general public with greater access to U.S.

Goverment publications, Congress established the Federal Depository Library Program under the Government Printing Office (GPO), with 50 regional depositories responsible for permanent retention of

material, inter-library loan, and reference services. At least one copy of nearly every NASA publication,

either in printed or microfiche format, is received and retained by the 50 regional depositories. A list of

the regional GPO libraries, arranged alphabetically by state, follows. These libraries are notsales outlets.

A local library can contact a Regional Depository to help locate specific reports, or direct contact may

be made by an individual.

Other Domestic: NASA publications are also available to the public for reference purposes at the library

maintained by the American Institute of Aeronautics and Astronautics, Technical Information Service,

555 West 57th Street, 12th Floor, New York, NY 10019.

European: An extensive collection of NASA publications is maintained by the British Library Lending

Division, Boston Spa, Wetherby, Yorkshire, England for public access. European requesters may purchase

facsimile copy or microfiche of NASA documents, those identified by both the symbols # and *, from

ESA, Information Retrieval Service, European Space Agency, 8-10 rue Mario-Nikis, 75738 Paris

CEDEX 15, France.

NASA Scientific and Technical Information Facility

NASA publications are available to NASA personnel, NASA contractors, other Government agencies

and their contractors, and universities through local technical libraries. The NASA Scientific and Technical

Information Facility also makes these publications available to registered users, but not to the general

public.

For registration information contact:

NASA STI Facility

P.O. Box 8757

BWl Airport, MD 21240

(301) 621-0153 Registration information
NTIS PRICE SCHEDULES

(Effective January 1, 1987)

Schedule A

STANDARD PRICE DOCUMENTS

AND MICROFICHE

NORTH

PRICE PAGE AMERICAN FOREIGN

CODE RANGE PRICE PRICE

A01 Microfiche $ 6.50 $13.00

A02 001-025 9.95 19.90

A03 026-050 11.95 23.90

AO4-A05 051-100 13.95 27.90

A06-A09 101-200 18.95 37.90

A10-A13 201-300 24.95 49.90

A14-A17 301-400 30.95 61.90

A18-A21 401-500 36.95 73.90

A22-A25 501-600 42.95 85.90

A99 601 -up

NO1 45.00 80.00

NO2 48.00 80.00

Schedule E

EXCEPTION PRICE DOCUMENTS

AND MICROFICHE

NORTH

PRICE AMERICAN FOREIGN

CODE PRICE PRICE

E01 $ 7.50 15.00

E02 10.00 20.00

E03 11.00 22.00

E04 13.50 27.00

E05 15.50 31.00

E06 18.00 36.00

E07 20.50 41.00

E08 23.00 46.00

E09 25.50 51.00

El0 28.00 56.00

Ell 30.50 61.00

E12 33.00 66.00

E13 35.50 71.00

E14 38.50 77.00

E15 42.00 84.00

E16 46,00 92.00

E17 50.00 100.00

E18 54.00 108.00

E19 60.00 120.00

E20 70.00 140.00

E99 * *

"Contact NTIS for pdce quote.

IMPORTANT NOTICE

NTIS Shipping and Handling Charges

U.S., Canada, Mexico -- ADD $3.00 per TOTAL ORDER

All Other Countries -- ADD $4.00 per TOTAL ORDER

Exceptions -- Does NOT apply to:

ORDERS REQUESTING NTIS RUSH HANDLING

ORDERS FOR SUBSCRIPTION OR STANDING ORDER PRODUCTS ONLY

NOTE: Each additional delivery address on an order

requires a separate shipping and handling charge.
FEDERAL REGIONAL DEPOSITORY LIBRARIES

ALABAMA

AUBURN UNIV. AT MONTGOMERY

LIBRARY

Documents Department

Montgomery, AL 36193

i205) 271-9650

UNIV. OF ALABAMA LIBRARY

Documents Depl -Box S

Un=versnty AL 35486

(205) 348-6046

ARIZONA

DEPT. OF LIBRARY, ARCHIVES

AND PUBLIC RECORDS

Third FlOOr-- State Cap

1700 West Washington

Phoenix, AZ 85007

(602t 255-4121

UNIVERSITY OF ARIZONA LIB.

Government Documents Dept.

Tucson, AZ 85721

(602) 621-6433

ARKANSAS

ARKANSAS STATE LIBRARY

One Capitol Mail

Llffie Rock. AR 72201

(501) 371-2326

CALIFORNIA

CALIFORNIA STATE LIBRARY

Govt Publicafuons Section

PO Box 2037

Sacramento. CA 95809

(916) 324-4863

COLORADO

UNIV OF COLORADO LIB.

Government Pub Division

Campus Box 184

Boulder. CO 80309

(303) 492-8834

DENVER PUBLIC LIBRARY

Govt Pub Department

1357 Broadway

Denver, CO 80203

(303) 571-2131

CONNECTICUT

CONNECTICUT STATE LIBRARY

Government Documents Unit

231 Capitol Avenue

Hartford, CT 06106

(203] 566-7029

FLORIDA

UNIV. OF FLORIDA LIBRARIES

L,0rary West

Documents Department

Galnesvltte, FL 32611

(904) 392-0367

GEORGIA

UNIV. OF GEORGIA LIBRARIES

Government Reference Dept

Athens, GA 30602

(404) 542-8949

HAWAfl

UNIV. OF HAWAII LIBRARY

Gov't Documents Collection

2550 Th_ Mall

Honolulu. HI 96822

i808) 948-8230

IDA HO

UNIV. OF IDAHO LIBRARY

Documents Section

Moscow. ID 83843

[208) 885-6344

ILLINOIS

ILLINOIS STATE LIBRARY

_nformat_on Serwces Branch

Centenmal Budding

Springfield. IL 62756

(217) 782-5185

INDIANA

INDIANA STATE LIBRARY

Serials Documents Section

140 North Senate Avenue

Indianapolis, IN 46204

(317) 232-3686

IOWA

UNIV, OF IOWA LIBRARIES

Govt Documents Depatlment

Iowa Cif'y, IA 52242

(319) 353-3318

KANSAS

UNIVERSITY OF KAN3AS

Doc, Collect-- Spencer Lib.

Lawrence. KS 66045-2800

(913) 864-4662

KENTUCKY

UNIV. OF KENTUCKY LIBRARIES

Govt. Pub Department

Lexington. KY 40506-0039

(606) 257-3139

LOUISIANA

LOUISIANA STATE UNIVERSFFY

Middleton Library

Govt. Docs Dept

Baton Rouge, LA 70803

(504) 388-2570

LOUISIANA TECHNICAL UNIV.

LIBRARY

Documents Department

Ruston, LA 71272-0046

(318) 257-4962

MAINE

UNIVERSITY OF MAINE

Raymond H. Fogler Library

Tri-State Regional Documents

Deposntory

Orono, ME 04469

(207) 58%1680

MARYLAND

UNIVERSITY OF MARYLAND

McKelciin Lib--Doc Div

College Park, MD 20742

(301) 454-3034

MA SSA CHUSETTS

BOSTON PUBLIC LIBRARY

Government Docs, Dept.

Boston, MA 02117

(617) 536-5400 ext.226

MICHIGAN

DETROIT PUBLIC LIBRARY

Sociology Department

5201 Woodward Avenue

Detroit, MI 48202-4093

(313) 833-1409

MICHIGAN STATE LIBRARY

PO Box 30007

Lansing, Mt 48909

I517) 373-1593

MINNESOTA

UNIVERSITY OF MINNESOTA

Government Pubs. Division

409 Wilson Library

309 191h Avenue South

Minneapolis, MN 55455

(6t2) 373-7870

MISSISSIPPI

UNIV. OF MISSISSIPPI LIB.

Documents Department

Un=versity, MS 38677

(601) 232-5857

MONTANA

UNIV. OF MONTANA

Mansfield Library

Documents Division

Missoula, MT 59812

(406) 243-6700

NEBRASKA

UNIVERSITY OF NEBRASKA -

LINCOLN

Love Library

Documents Department

Lincoln, NE 68588-0410

(402) 472-2562

NEVADA

UNIVERSITY OF NEVADA LIB.

Govt Pub Department

RanD, NV 89557-0044

(702) 784-6579

NEW JERSEY

NEWARK PUBLIC LIBRARY

5 Washington Street

Newark, NJ 07101-0630

(201) 733-7812

NEW MEXICO

UNIVERSITY OF NEW MEXICO

Zirnmerman Library

Government Pub. Dept.

Albuquerque, NM 87131

(505) 277-5441

NEW MEXICO STATE LIBRARY

Reference Department

325 Don Gaspar Avenue

Santa Fe, NM 87503

(505) 827-3826

NEW YORK

NEW YORK STATE LIBRARY

Empire State Plaza

Albany. NY 12230

(516) 474-5563

NORTH CAROLINA

UNIVERSITY OF NORTH CAROLINA

AT CHAPEL HILL

Davis Library

BA/SS Documents Diwsion

Chapel Hilt, NC 27515

(919) 962-1151

NORTH DAKOTA

UNIVERSITY OF NORTH DAKOTA

Chester Fritz Library

Documents Department

Grand Forks, NO 58202

(701) 777-4629

In cooperahon w_th Nort_

Dakota State Umv LpOrary

OHIO

STATE LIBRARY OF OHIO

Documents Department

65 South Front Street

Columbus, OH 43266-0334

(614) 462-7051

OKLAHOMA

OKLAHOMA DEPT. OF LIB.

Government Documents

200 NE 181h Street

Oklahoma Cdy. OK 73105

(405) 52t-2502, ext 252

OKLAHOMA STATE UNIV. LIB.

Documents Department

Stlllwater. OK 74078

(405) 624-6546

OREGON

PORTLAND STATE UNIV, LIB.

Documents Department

PO Box 1151

Portland OR 97207

(503) 229-3673

PENNSYLVANIA

STATE LIBRARY OF PENN.

Government Pub Section

PO Box 1601

Harrisburg, PA 17105

(717) 787-3752

TEXAS

TEXAS STATE LIBRARY

Public Services Department

PO Box 12927-Cap Sta

Austin, TX 78711

(512) 475-2996

TEXAS TECH. UNIV. LIBRARY

Govt Documents Department

Lubbock, TX 79409

(806) 742-2268

UTAH

UTAH STATE UNIVERSITY

Merrill Library, UMC 30

Logan, UT 84322

(801) 750-2682

VIRGINIA

UNIVERSITY OF VIRGINIA

Alderman Lib-Pubifc Doc

Charfotlesville, VA 22903-2498

(604) 924-3133

WASHINGTON

WASHINGTON STATE LIBRARY

Documents Section

Olympia, WA 98504

(206) 753-4027

WEST VIRGINIA

WEST VIRGINIA UNIV. LIB.

Documents Departn_ent

Morgantown WV 26506-6069

i304) 293-3640

WISCONSIN

MILWAUKEE PUBLIC LIBRARY

814 West Wisconsin Avenue

Milwaut(ee, WI 53233

/414) 278-3065

ST. HIST LIB. OF WISCONSIN

Government Pub Section

816 State Street

Madison. WI 53706

i606) 262-4347

WYOMING

WYOMING STATE LIBRARY

Supreme Ct & Library Bid

Cheyenne. WY 82002

t307) 777-5919

vii

NASA Scientific and Technical Publications

TABLE OF CONTENTS

AERONAUTICS

Includes aeronautics (general); aerodynamics; air

transportation and safety; aircraft communications and

navigation; aircraft design, testing and performance; aircraft instrumentation; aircraft propulsion and power; aircraft stability and control; and research and support

facilities (air).

For related information see also Astronautics.

01 AERONAUTICS (GENERAL)

02 AERODYNAMICS 5

Includes aerodynamics of bodies, combinations,

wings, rotors, and control surfaces; and internal flow in

ducts and turbomachinery.

For related information see also 34 Fluid Mechanics

and Heat Transfer

03 AIR TRANSPORTATION AND SAFETY 28

Includes passenger and cargo airtransport operations;

and aircraft accidents.

For related information see also 16 Space Transportation and 85 Urban Technology and Transportation.

04 AIRCRAFT COMMUNICATIONS AND

NAVIGATION 30

Includes digital and voice communication with aircraft;

air navigation systems (satellite and ground based); and

air traffic control.

For related information see also 17Space Communications, Spacecraft Communications, Command and Tracking and 32 Communications and Radar.

05 AIRCRAFT DESIGN, TESTING AND

PERFORMANCE 31

Includes aircraft simulation technology.

For related information see also 18Spacecraft Design,

Testing and Performance and 39 Structural Mechanics.

For land transportation vehicles see 85 Urban Technology

and Transportation.

06 AIRCRAFT INSTRUMENTATION 38

Includes cockpit and cabin display devices; and flight

instruments.

For related information see also 19 Spacecraft Instrumentation and 35 Instrumentation and Photography.

07 AIRCRAFT PROPULSION AND POWER 41

Includes prime propulsion systems and systems components, e.g., gas turbine engines and compressors; and

onboard auxiliary power plants for aircraft.

For related information see also 20Spacecraft Propul-

,;ion and Power, 28 Propellants and Fuels, and 44 Energy

Production and Conversion.

08 AIRCRAFT STABILITY AND CONTROL 52

Includes aircraft handling qualities; piloting; flight controls; and autopilots.

For related information see also 05 Aircraft Design,

Testingand Performance.

09 RESEARCH AND SUPPORT

FACILITIES (AIR) 59

Includes airports, hangars and runways; aircraft repair

and overhaul facilities; wind tunnels; shock tubes; and

aircraft engine test stands.

For related information see also 14 Ground Support

Systems and Facilities (Space).

ASTRONAUTICS

Includes astronautics (general); astrodynamics;

ground support systems and facilities (space); launch vehicles and space vehicles; space transportation; space

communications, spacecraft communications, command

and tracking; spacecraft design, testing and performance;

spacecraft instrumentation; and spacecraft propulsion and

power.

For related information see also Aeronautics

12 ASTRONAUTICS (GENERAL) 60

For extraterrestrial exploration see 91 Lunar and Planetary Exploration.

13 ASTRODYNAMICS 64

Includes powered and free-flight trajectories; and orbital and launching dynamics.

14 GROUND SUPPORT SYSTEMS AND

FACILITIES (SPACE) 64

Includes launch complexes, research and production

facilities; ground support equipment, e.g., mobile transporters; and simulators.

For related information see also 09 Research and Support Facilities (Air).

15 LAUNCH VEHICLES AND SPACE

VEHICLES 65

Includes boosters; operating problems of launch/space

vehicle systems; and reusable vehicles.

For related information see also 20 Spacecraft Propulsion and Power.

16 SPACE TRANSPORTATION 68

Includes passenger and cargo space transportation,

e.g., shuttle operations; and space rescue techniques.

For related information see also 03 Air Transportation

and Safety and 18Spacecraft Design, Testing and Performance. For space suits see 54 Man/System Technology

and Life Support.

17 SPACE COMMUNICATIONS,

SPACECRAFT COMMUNICATIONS,

COMMAND AND TRACKING 69

Includes telemetry; space communications networks;

astronavigation and guidance; and radio blackout.

For related information see also 04 Aircraft Communications and Navigation and 32 Communications and

Radar.

PREO-EDING :_ ....,,4 ,.-, ; ....,. ._.. ,. i. ,._,L_.,.._,.,L,,,,..;4,_;. x,,--,r_,..:. _' [f..._w('_
18 SPACECRAFT DESIGN, TESTING AND

PERFORMANCE 70

Includes satellites; space platforms; space stations;

spacecraft systems and components such as thermal and

environmental controls; and attitude controls.

For life support systems see 54 Man/System Technology and Life Support. For related information see also 05

Aircraft Design, Testing and Performance, 39 Structural

Mechanics, and 16 Space Transportation.

19 SPACECRAFT INSTRUMENTATION 75

For related information see also 06Aircraft Instrumentation and 35 Instrumentation and Photography

20 SPACECRAFT PROPULSION AND

POWER 76

Includes main propulsion systems and components,

e.g. rocket engines; and spacecraft auxiliary power

sources.

For related information see also 07Aircraft Propulsion

and Power, 28 Propellants and Fuels, 44 Energy Production and Conversion, and 15 Launch Vehicles and Space

Vehicles.

CHEMISTRY AND MATERIALS

Includes chemistry and materials (general); composite

materials; inorganic and physical chemistry; metallic materials; nonmetallic materials; propellants and fuels; and

materials processing.

23 CHEMISTRY AND MATERIALS

(GENERAL) 78

24 COMPOSITE MATERIALS 79

Includes physical, chemical, and mechanical properties of laminates and other composite materials.

For ceramic materials see 27 Nonmetallic Materials.

25 INORGANIC AND PHYSICAL

CHEMISTRY 84

Includes chemical analysis, e.g., chromatography;

combustion theory; electrochemistry; and photochemistry.

For related information see also 77 Thermodynamics

and Statistical Physics.

26 METALLIC MATERIALS 85

Includes physical, chemical, and mechanical properties of metals, e.g., corrosion; and metallurgy.

27 NONMETALLIC MATERIALS 91

Includes physical, chemical, and mechanical properties of plastics, etastomers, lubricants, polymers, textiles,

adhesives, and ceramic materials.

For composite materials see 24 Composite Materials.

28 PROPELLANTS AND FUELS 96

Includes rocket propellants, igniters and oxidizers; their

storage and handling procedures; and aircraft fuels.

For related information see also 07Aircraft Propulsion

and Power, 20 Spacecraft Propulsion and Power, and 44

Energy Production and Conversion.

29 MATERIALS PROCESSING N.A.

Includes space-based development of products and

processes for commercial application.

For biological materials see 55 Space Biology

ENGINEERING

Includes engineering (general)', communications and

radar; electronics and electrical engineering; fluid

mechanics and heat transfer; instrumentation and photography; lasers and masers; mechanical engineering; quality

assurance and reliability; and structural mechanics.

For related information see also Physics.

31 ENGINEERING (GENERAL) 98

Includes vacuum technology; control engineering; display engineering; cryogenics; and fire prevention.

32 COMMUNICATIONS AND RADAR 100

Includes radar; land and global communications; communications theory; and optical communications.

For related information see also 04 Aircraft Communications and Navigation and 17 Space Communications,

Spacecraft Communications, Command and Tracking. For

search and rescue see 03 Air Transportation and Safe_

and 16 Space Transportation.

33 ELECTRONICS AND ELECTRICAL

ENGINEERING 100

Includes test equipment and maintainability; components, e.g., tunnel diodes and transistors; microminiaturization; and integrated circuitry.

For related information see also 60 Computer Operations and Hardware and 76 Solid-State Physics.

34 FLUID MECHANICS AND HEAT

TRANSFER 104

Includes boundary layers; hydrodynamics; fluidics;

mass transfer and ablation cooling.

For related information see also 02Aerodynamics and

77 Thermodynamics and Statistical Physics.

35 INSTRUMENTATION AND

PHOTOGRAPHY 113

Includes remote sensors; measuring instruments and

gages; detectors; cameras and photographic supplies; and

holography.

For aerial photography see 43 Earth Resources and

Remote Sensing. For related information see also 06 Aircraft Instrumentation and 19 Spacecraft Instrumentation.

36 LASERS AND MASERS 117

Includes parametric amplifiers.

For related information see also 76 Solid-State

Physics.

37 MECHANICAL ENGINEERING 118

Includes auxiliary systems (nonpower); machine elements and processes; and mechanical equipment.

38 QUALITY ASSURANCE AND

RELIABILITY 126

Includes product sampling procedures and techniques;

and quality control.

39 STRUCTURAL MECHANICS 127

Includes structural element design and weight

analysis; fatigue; and thermal stress.

For applications see 05 Aircraft Design, Testing and

Performance and 18 Spacecraft Design, Testing and Performance.
GEOSClENCES

Includes geosciences (general); earth resources and

remote sensing; energy production and conversion; environment pollution; geophysics; meteorology and climatology; and oceanography.

For related information see also Space Sciences.

42 GEOSCIENCES (GENERAL) 136

43 EARTH RESOURCES AND

REMOTE SENSING 137

Includes remote sensing of earth resources by aircraft

and spacecraft; photogrammetry; and aerial photography.

For instrumentation see 35 Instrumentation and Photography.

44 ENERGY PRODUCTION AND

CONVERSION 144

Includes specific energy conversion systems, e.g., fuel

cells; global sources of energy; geophysical conversion;

and windpower.

For related information see also 07Aircraft Propulsion

and Power, 20 Spacecraft Propulsion and Power, and 28

Propellants and Fuels.

45 ENVIRONMENT POLLUTION 147

Includes atmospheric, noise, thermal, and water pollution.

46 GEOPHYSICS 151

Includes aeronomy; upper and lower atmosphere

studies; ionospheric and magnetospheric physics; and

geomagnetism.

For space radiation see 93 Space Radiation.

47 METEOROLOGY AND CLIMATOLOGY

Includes weather forecasting and modification.

157

48 OCEANOGRAPHY 167

Includes biological, dynamic, and physical oceanography; and marine resources.

For related information see also 43 Earth Resources

and Remote Sensing.

LIFE SCIENCES

Includes life sciences (general); aerospace medicine;

behavioral sciences; man/system technology and life support; and space biology.

51 LIFE SCIENCES (GENERAL) 169

52 AEROSPACE MEDICINE 170

Includes physiological factors; biological effects ofradiation; and effects ofweightlessness on man and animals.

53 BEHAVIORAL SCIENCES 171

Includes psychological factors; individual and group

behavior; crew training and evaluation; and psychiatric research.

54 MAN/SYSTEM TECHNOLOGY AND

LIFE SUPPORT 172

Includes human engineering; biotechnology; and

space suits and protective clothing.

For related information see also 16Space Transportation.

xi

55 SPACE BIOLOGY 175

Includes exobiology; planetary biology; and extraterrestrial life,

MATHEMATICAL AND COMPUTER

SCIENCES

Includes mathematical and computer sciences (general); computer operations and hardware; computer programming and software; computer systems; cybernetics;

numerical analysis; statistics and probability; systems

analysis; and theoretical mathematics.

59 MATHEMATICAL AND COMPUTER

SCIENCES (GENERAL) 175

60 COMPUTER OPERATIONS AND

HARDWARE 177

Includes hardware for computer graphics, firmware,

and data processing.

For components see 33 E/ectronics and Electrical En.

gineering.

61 COMPUTER PROGRAMMING AND

SOFTWARE 178

Includes computer programs, routines, algorithms, and

specific applications, e.g., CAD/CAM.

62 COMPUTER SYSTEMS 180

Includes computer networks and special application

computer systems.

63 CYBERNETICS 180

Includes feedback and control theory, artificial intelligence, robotics and expert systems.

For related information see also 54 Man/System

Techno/ogy and Life Support.

64 NUMERICAL ANALYSIS 182

Includes iteration, difference equations, and numerical

approximation.

65 STATISTICS AND PROBABILITY 183

Includes data sampling and smoothing; Monte Carlo

method; and stochastic processes.

66 SYSTEMS ANALYSIS 184

Includes mathematical modeling; network analysis;

and operations research.

67 THEORETICAL MATHEMATICS

Includes topology and number theory.

185

PHYSICS

Includes physics (general); acoustics; atomic and

molecular physics; nuclear and high-energy physics; optics; plasma physics; solid-state physics; and thermodynamics and statistical physics.

For related information see also Engineering.

70 PHYSICS (GENERAL) 185

For precision time and time interval (PTrl) see 35

Instrumentation and Photography; for geophysics, astrophysics or solar physics see 46 Geophysics, 90 Astrophysics, or 92 Solar Physics.
71 ACOUSTICS 185

Includes sound generation, transmission, and attenuation.

For noise pollution see 45 Environment Pollution.

72 ATOMIC AND MOLECULAR PHYSICS 191

Includes atomic structure, electron properties, and

molecular spectra,

73 NUCLEAR AND HIGH-ENERGY

PHYSICS 192

Includes elementary and nuclear particles; and reactor

theory.

For space radiation see 93 Space Radiation.

74 OPTICS

Includes light phenomena and optical devices.

For lasers see 36 Lasers and Masers.

193

75 PLASMA PHYSICS 194

Includes magnetohydrodynamics and plasma fusion.

For ionospheric plasmas see 46 Geophysics. For

space plasmas see 90 Astrophysics,

76 SOLID-STATE PHYSICS 195

Includes superconductivity,

For related information see also 33 Electronics and

Electrical Engineering and 36 Lasers and Masers.

77 THERMODYNAMICS AND

STATISTICAL PHYSICS 195

Includes quantum mechanics; theoretical physics; and

Bose and Fermi statistics.

Forrelated informationsee also25 Inorganicand Physical Chemistry and 34 Fluid Mechanics and Heat Transfer.

SOCIAL SCIENCES

Includes social sciences (general); administration and

management; documentation and information science;

economics and cost analysis; law, political science, and

space policy; and urban technology and transportation.

80 SOCIAL SCIENCES (GENERAL) 196

Includes educational matters.

81 ADMINISTRATION AND

MANAGEMENT

Includes management planning and research.

196

82 DOCUMENTATION AND

INFORMATION SCIENCE 197

Includes information management; information storage and retrieval technology; technical writing; graphic

arts; and micrography.

For computer documentation see 61 Computer Programming and Software.

83 ECONOMICS AND COST ANALYSIS

Includes cost effectiveness studies.

N,A.

84 LAW, POLITICAL SCIENCE

AND SPACE POLICY N.A.

Includes NASA appropriation hearings; aviation law;

space law and policy;international law; international cooperation; and patent policy.

85 URBAN TECHNOLOGY AND

TRANSPORTATION 198

Includes applications of space technology to urban

problems; technology transfer; technology assessment;

and surface and mass transportation.

For related information see 03 Air Transportation and

Safe_ 16Space Transportation,and 44 Energy Production

and Conversion.

SPACE SCIENCES

Includes space sciences (general); astronomy; astrophysics; lunar and planetary exploration; solar physics;

and space radiation,

For related information see also Geosciences,

88 SPACE SCIENCES (GENERAL) 199

89 ASTRONOMY 201

Includes radio, gamma-ray, and infrared astronomy;

and astrometry.

90 ASTROPHYSICS 203

Includes cosmology; celestial mechanics; space plasmas; and interstellar and interplanetary gases and dust,

For related information see also 75 Plasma Physics,

91 LUNAR AND PLANETARY

EXPLORATION 204

Includes planetology; and manned and unmanned

flights,

For spacecraft design or space stations see 18Spacecraft Design, Testingand Performance.

92 SOLAR PHYSICS 209

Includes solar activity, solar flares, solar radiation and

sunspots.

For related information see 93 Space Radiation.

93 SPACE RADIATION 210

Includes cosmic radiation; and inner and outer earth's

radiation belts.

For biological effects of radiation see 52 Aerospace

Medicine. For theory see 73 Nuclear and High-Energy

Physics.

GENERAL

Includes aeronautical, astronautical, and space science related histories, biographies, and pertinent reports

too broad for categorization; histories or broad overviews

of NASA programs.

99 GENERAL 211

Note: N.A. means that no abstracts were assigned to this category for this Issue.

SUBJECT INDEX .................................................................................. A-1

PERSONAL AUTHOR INDEX .............................................................. B-1

REPORT NUMBER INDEX ................................................................... C-1

xii
01

AERONAUTICS (GENERAL)

N77-17996"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

PROCEEDINGS OF THE SCAR CONFERENCE, PART 1

1976 478 p refs Conf. Proceedings held at Hampton, Va.,

9-12 Nov. 1976 2 Vol.

(NASA-CP-001-PT-1) Avail: NTIS HC A21/MF A01 CSCL 01C

AERODYNAMIC CONFIGURATIONS, CONFERENCES,

SUPERSONIC AIRCRAFT, SUPERSONIC SPEED

N77-18019"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

PROCEEDINGS OF THE SCAR CONFERENCE, PART 2

1976 547 p Conf. held at Hampton, Va., 9-12 Nov. 1976

(NASA-CP-001-PT-2) Avail: NTIS HC A23/MF A01 CSCL 01C

CONFERENCES, SUPERSONIC AIRCRAFT, TECHNOLOGY

ASSESSMENT

N77-21022"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

FLUTTER TESTING TECHNIQUES

1976 483 p Conf. Proc. held at Dryden Flight Res. Center in

Edwards, Calif., 9-10 Oct. 1975

(NASA-SP-415) Avail: NTIS HC A21/MF A01 CSCL 01C

Developments in methodology and data analysis techniques

for flutter testing in flight and on the ground are discussed.

N77-32072"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

A STUDY OF THE SONIC-BOOM CHARACTERISTICS OF A

BLUNT BODY AT A MACH NUMBER OF 4.14

H. W. CARLSON and R. J. MACK Sep. 1977 31 p refs

(NASA-TP-1015; L-11456) Avail: NTIS HC A03/MF A01

CSCL 20A

BLUNT BODIES, PRESSURE DISTRIBUTION, SONIC BOOMS

N78-12999"# Texas A&M Univ., College Station. Flight

Mechanics Lab.

AGRICULTURAL AVIATION RESEARCH

H. L. CHEVALIER, comp. and L. F. BOUSE, comp. (Agricultural

Research Service, College Station, Tex.) 1977 151 p Proc.

of Workshop held at College Station, Tex., 19-21 Oct. 1976

(NASA ORDER L-49862-A)

(NASA-CP-2025) Avail: NTIS HC A08/MF A01 CSCL 01C

AERONAUTICS, AGRICULTURE, AIRCRAFT PERFORMANCE

N78-25048"# National Aeronautics and Space Administration.

Wallops Flight Center, Wallops Island, Va.

PRECISION POSITIONAL DATA OF GENERAL AVIATION AIR

TRAFFIC IN TERMINAL AIR SPACE

W. E. MELSON, JR., L. C. PARKER, A. M. NORTHAM (Computer

Sciences Corp., Wallops Island, Va.), and R. P. SINGH (Computer

Sciences Corp., Wallops Island, Va.) May 1978 13 p

(NASA-RP-1020) Avail: NTIS HC A02/MF A01 CSCL 02A

Three dimensional radar tracks of general aviation air traffic at

three uncontrolled airports are considered. Contained are data

which describe the position-time histories, other derived

parameters, and reference data for the approximately 1200 tracks.

All information was correlated such that the date, time, flight

number, and runway number match the pattern type, aircraft type,

wind, visibility, and cloud conditions. Author

N78-25049"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

INTERACTION OF A TURBULENT-JET NOISE SOURCE WITH

TRANSVERSE MODES IN A RECTANGULAR DUCT

G P. SUCCI (MIT, Cambridge, Mass.), K. J. BAUMEISTER, and

K. U. INGARD (MIT, Cambridge, Mass.) Jun. 1978 42 p refs

(NASA-TP-1248; E-9462) Avail: NTIS HC A03/MF A01 CSCL

20A

ACOUSTIC DUCTS, MODES (STANDING WAVES), NOISE

(SOUND), SINGULARITY (MATHEMATICS), TURBULENT JETS

N78-27046"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

CTOL TRANSPORT TECHNOLOGY, 1978

Jun. 1978 5t6 p refs Conf. held at Hampton, Va., 28 Feb. -

3 Mar. 1978

(NASA-CP-2036-PT-1; L-12178) Avail: NTIS HC A22/MF A01

CSCL 02A

AIRCRAFT DESIGN, COMMERCIAL AIRCRAFT, CONFERENCES, TECHNOLOGY ASSESSMENT, TRANSPORT AIRCRAFT

N78-29046"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

CTOL TRANSPORT TECHNOLOGY, 1978

1978 405 p refs Conf. held at Hampton, Va., 28 Feb. - 3

Mar. 1978

(NASA-CP-2036-PT-2; L-t2178) Avail: NTIS HC A18/MF A01

CSCL 02A

AIR TRANSPORTATION, AIRCRAFT DESIGN, CONFERENCES, TRANSPORT AIRCRAFT

N79-15898"# National Aeronautics and Space Administration,

Washington, D.C.

AVIONICS AND CONTROLS RESEARCH AND TECHNOLOGY

H. A. REDIESS, ed. and D. E. MCIVER, ed. 1979 84 p

Workshop held at Hampton, Va., 27-28 Jun. 1978

(NASA-CP-2061; L-12498) Avail: NTIS HC A05/MF A01

CSCL 02A

AVIONICS, CONFERENCES, FLIGHT CONTROL
01 AERONAUTICS (GENERAL)

N79-16796"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

GENERATION OF LINEAR DYNAMIC MODELS FROM A DIGITAL

NONLINEAR SIMULATION

C. J. DANIELE and S. M. KROSEL Feb. 1979 95 p refs

(NASA-TP-1388; E-9490) Avail: NTIS HC A05/MF A01 CSCL

02A

AIRCRAFT ENGINES, CONTROL THEORY, DIGITAL

SIMULATION, DYNAMIC MODELS, ENGINE CONTROL, OPTIMAL

CONTROL

N79-19989"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ADVANCED TECHNOLOGY AIRFOIL RESEARCH, VOLUME 1,

PART 2

1978 303 p refs Proceedings of Conf. held at Hampton, Va.,

7-9 Mar. 1978

(NASA-CP-2045-PT-2; L-12232-VOL-1-PT-2) Avail: NTIS HC

A14/MF A01 CSCL 02A

AIRFOILS, WIND TUNNEL TESTS

N79-23008"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

COMPUTER FORMULATIONS OF AIRCRAFT MODELS FOR

SIMULATION STUDIES

J. C. HOWARD May 1979 73 p refs

(NASA-TP-1470; A-7477) Avail: NTIS HC A04/MF A01 CSCL

02A

AIRCRAFT MODELS, COMPUTERIZED SIMULATION,

MATHEMATICAL MODELS, SYMBOLIC PROGRAMMING

N79-23889"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

THE SCIENCE AND TECHNOLOGY OF LOW SPEED AND

MOTORLESS FLIGHT, PART 1

P. W. HANSON, comp. 1979 299 p refs Conf. held at

Hampton, Va., 29-30 Mar. 1979; cosponsored by NASA and the

Soaring Soc. of America

(NASA-CP-2085-PT-1; L-12973) Avail: NTIS HC A13/MF A01

CSCL 02A

CONFERENCES, FREE FLIGHT, GLIDING, LOW SPEED,

SOARING, TECHNOLOGY ASSESSMENT

N79-27070"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SCIENCE AND TECHNOLOGY OF LOW SPEED AND

MOTORLESS FLIGHT. THIRD INTERNATIONAL SYMPOSIUM

P. W. HANSON, comp. Jun. 1979 297 p refs Syrup. held in

Hampton, Va., 29-30 Mar. 1979; sponsored by NASA-Langley and

Soaring Soc. of Am.

(L-12973; NASA-CP-2085-PT-2) Avail: NTIS HC A13/MF A01

CSCL 02A

AERODYNAMICS, AIRSPEED, CONFERENCES, FLIGHT

CONTROL, GLIDERS, LOW SPEED

N79-30139"# National Aeronautics and Space Administration.

Dryden (Hugh L.) Flight Research Center, Edwards, Calif.

PERFORMANCE EVALUATION METHOD FOR DISSIMILAR

AIRCRAFT DESIGNS

H. J. WALKER Sep. 1979 72 p refs

(NASA-RP-1042; H-1064) Avail: NTIS HC A04/MF A0f CSCL

02A

A rationale is presented for using the square of the wingspan

rather than the wing reference area as a basis for nondimensional

comparisons of the aerodynamic and performance characteristics

of aircraft that differ substantially in planform and loading. Working

relationships are developed and illustrated through application to

several categories of aircraft covering a range of Mach numbers

from 0.60 to 2.00. For each application, direct comparisons of

drag polars, lift-to-drag ratios, and maneuverability are shown for

both nondimensional systems. The inaccuracies that may arise in

the determination of aerodynamic efficiency based on reference

area are noted. Span loading is introduced independently in

comparing the combined effects of loading and aerodynamic

efficiency on overall performance. Performance comparisons are

made for the NACA research aircraft, lifting bodies, century-series

fighter aircraft, F-111A aircraft with conventional and supercritical

wings, and a group of supersonic aircraft including the B-58 and

XB-70 bomber aircraft. An idealized configuration is included in

each category to serve as a standard for comparing overall

efficiency. Author

N80-11028"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EVALUATION OF A WIND-TUNNEL GUST RESPONSE

TECHNIQUE INCLUDING CORRELATIONS WITH ANALYTICAL

AND FLIGHT TEST RESULTS

L. T. REDD, P. W. HANSON, and E. C. WYNNE Nov. 1979 55

p refs

(NASA-TP-1501; L-13137) Avail: NTIS HC A04/MF A01

CSCL 01A

ATMOSPHERIC TURBULENCE, FLIGHT TESTS, GUST

LOADS, WIND TUNNEL TESTS

N80-15028"# National Aeronautics and Space Administration.

Dryden (Hugh L.) Flight Research Center, Edwards, Calif.

LANDING APPROACH AIRFRAME NOISE MEASUREMENTS

AND ANALYSIS

P. L. LASAGNA, K. G. MACKALL, F. W. BURCHAM, JR., and T.

W. PUTNAM Jan. 1980 36 p refs

(NASA-TP-1602) Avail: NTIS HC A03/MF A01 CSCL 20A

AIRCRAFT LANDING, AIRCRAFT NOISE, AIRFRAMES, NOISE

MEASUREMENT

N80-19022"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

ANALYSIS OF FUEL-CONSERVATIVE CURVED DECELERATING

APPROACH TRAJECTORIES FOR POWERED-LIFT ANO CTOL

JET AIRCRAFT

F. NEUMAN Apr. 1980 38 p refs

(NASA-TP-1650; A-7986) Avail: NTIS HC A03/MF A01 CSCL 02A

APPROACH, DESCENT TRAJECTORIES, FUEL CONSUMPTION, POWERED LIFT AIRCRAFT, TRAJECTORY ANALYSIS

N80-29244"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

CONTROL-SYSTEM TECHNIQUES FOR IMPROVED

DEPARTURE/SPIN RESISTANCE FOR FIGHTER AIRCRAFT

L. T. NGUYEN, W. P. GILBERT, and M. E. OGBURN Aug. 1980

69 p refs

(NASA-TP-1689; L-13453) Avail: NTIS HC A04/MF A01

CSCL 01C

AIRCRAFT CONTROL, CONTROL THEORY, FIGHTER

AIRCRAFT, SYSTEMS ENGINEERING

N80-29245"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SUBSONIC AIRCRAFT: EVOLUTION AND THE MATCHING OF

SIZE TO PERFORMANCE

L. K. LOFTIN, JR. Aug. 1980 445 p refs

(NASA-RP-1060; L-13367) Avail: NTIS HC A19/MF A01

CSCL 01B

Methods for estimating the approximate size, weight, and power

of aircraft intended to meet specified performance requirements

are presented for both let-powered and propeller-driven aircraft.

The methods are simple and require only the use of a pocket

computer for rapid application to specific sizing problems.

Application of the methods is illustrated by means of sizing studies

of a series of jet-powered and propeller-driven aircraft with varying

design constraints. Some aspects of the technical evolution of

the airplane from 1918 to the present are also briefly discussed.

Author
N81-13915"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

A STUDY OF THE SONIC-BOOM CHARACTERISTICS OF A

BLUNT BODY AT A MACH NUMBER OF 6

G. C. ASHBY, JR. Dec. 1980 34 p refs

(NASA-TP-1787; L-14017) Avail: NTIS HC A03/MF A01

CSCL 01B

BLUNT BODIES, FINITE DIFFERENCE THEORY, MACH

NUMBER, SIGNATURE ANALYSIS, SONIC BOOMS, STATIC

PRESSURE

N81-14961"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

DETERMINATION OF THE HYPERSONIC-CONTINUUMIRAREFIED-FLOW DRAG COEFFICIENT OF THE VIKING LANDER

CAPSULE 1 AEROSHELL FROM FLIGHT DATA

R. C. BLANCHARD and G. D. WALBERG Dec. 1980 60 p

refs

(NASA-TP-1793; L-14042) Avail: NTIS HC A04/MF A01

CSCL 01B

AERODYNAMIC COEFFICIENTS, AERODYNAMIC DRAG,

ATMOSPHERIC ENTRY, CONTINUUM FLOW, HYPERSONIC

FLOW, SPACECRAFT INSTRUMENTS, TEMPERATURE

PROFILES, VIKING LANDER 1

N81-15969"# National Aeronautics and Space Administration,

Washington, D.C.

THE HIGH-SPEED FRONTIER. CASE HISTORIES OF FOUR

NACA PROGRAMS, 1920 - 1950

J. V. BECKER 1980 196 p refs

(NASA-SP-445; LC-80-607935) Avail: NTIS MF A01; SOD HC

$6.50 CSCL 01B

The case histories focus on the fields of supersonic flow and

aircraft design. The development of supersonic airfoils is described

along with the development of test facilities such as transonic

wind tunnels and slotted wind tunnels. Emphasis is placed on

propeller blade design and configurations. The history of supersonic

flow theory is presented. For individual titles, see N81-15970

through N81-15973.

N81-17981"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SUPERSONIC CRUISE RESEARCH 1979, PART 1

Mar. 1980 542 p refs Conf. held at Hampton, Va., 13-16

Nov. 2 Vol.

(NASA-CP-2108-PT-1; L-13385-PT-1) Avail: NTIS HC A23/MF

A01 CSCL 01A

AERODYNAMICS, AIRCRAFT DESIGN, CONFERENCES,

SUPERSONIC CRUISE AIRCRAFT RESEARCH

N81-18005"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SUPERSONIC CRUISE RESEARCH 1979, PART 2

Mar. 1980 407 p refs Conf. held at Hampton, Va,, 13-16

Nov. 1979

(NASA-CP-2108-PT-2; L-13385-PT-2) Avail: NTIS HC A18/MF

A01 CSCL 01A

AIRCRAFT STRUCTURES, AIRFRAME MATERIALS,

CONFERENCES, ECONOMIC ANALYSIS, SUPERSONIC CRUISE

AIRCRAFT RESEARCH, SYSTEMS INTEGRATION

N81-19001"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ADVANCED AERODYNAMICS AND ACTtVE CONTROLS.

SELECTED NASA RESEARCH

Feb. 1981 180 p refs Presented at the 4th Ann. Status Rev.

of the NASA Aircraft Energy Efficiency (ACEE) Energy Efficient

Transport Program, Mountain View, Calif. 7.9 Oct. 1980

(NASA-CP-2172; L-14278) Avail: NTIS HC A09/MF A01

CSCL 01B

ACTIVE CONTROL, AIRCRAFT DESIGN, CONFERENCES,

DRONE AIRCRAFT, FLIGHT CHARACTERISTICS, FLIGHT TESTS,

01 AERONAUTICS (GENERAL)

FLY BY WIRE CONTROL, LIGHTNING, SUPERCRITICAL WINGS,

TRANSPORT AIRCRAFT, WlNGLETS

N81-21999"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

JOINT UNIVERSITY PROGRAM FOR AIR TRANSPORTATION

RESEARCH, 1980

Mar. 1981 139 p refs Proceedings of Conf. held at Hampton,

Va., 11-12 Dec. 1980

(NASA-CP-2176) Avail: NTIS HC A07/MF A01 CSCL 01B

AIR TRANSPORTATION, CONFERENCES, LORAN C,

NAVIGATION AIDS

N82-11013"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECTS OF VORTEX FLAPS ON THE LOW-SPEED

AERODYNAMIC CHARACTERISTICS OF AN ARROW WING

L. P. YIP and D. G. MURRI Nov. 1981 64 p refs

(NASA-TP-1914; L-14575) Avail: NTIS HC A04/MF A01

CSCL 01B

AERODYNAMIC CHARACTERISTICS, ARROW WINGS, FLOW

VISUALIZATION, LOW SPEED STABILITY, VORTEX FLAPS, WIND

TUNNEL TESTS

N82-14049"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

OPTIMIZATION AND PERFORMANCE CALCULATION OF

DUAL-ROTATION PROPELLERS

R. E. DAVIDSON Dec. 1981 48 p refs

(NASA-TP-1948; L-14678) Avail: NTIS HC A03/MF A01

CSCL 01A

AERODYNAMIC DRAG, AIRFOIL PROFILES, DUAL WING

CONFIGURATIONS, PROPELLER BLADES, THEODORSEN

TRANSFORMATION, WING TIPS

N82-19134"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ELECTRIC FLIGHT SYSTEMS

N. J. GROOM, ed. and R. V. HOOD, ed. Feb. 1982 269 p

Proceedings of workshop held in Hampton, Va., 9-10 Jun. 1981

(NASA-CP-2209; L-14965) Avail: NTIS HC A12/MF A01

CSCL 01C

AIRCRAFT DESIGN, AIRCRAFT ENGINES, AUXILIARY

POWER SOURCES, ELECTRIC GENERATORS, ELECTRIC

MOTORS, ENVIRONMENTAL CONTROL, FLIGHT CONTROL,

SPACECRAFT PROPULSION

N82-21139"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

PROCEEDINGS: FIFTH ANNUAL WORKSHOP ON

METEOROLOGICAL AND ENVIRONMENTAL INPUTS TO

AVIATION SYSTEMS

D. W. CAMP, ed., W. FROST, ed. ('Tennessee Univ. Space Inst.),

and P. D. PARSLEY, ed. Dec. 1981 149 p refs Workshop

held at Tullahoma, Tenn., 30 Mar. - 1 Apr. 1981; sponsored by

NASA, NOAA and FAA

(NAS8-32692)

(NASA-CP-2192; NAS 1.55:2192; FAA-RD-81-67) Avail: NTIS

HCA07/MFA01 CSCL0tB

AERONAUTICS, AIR TRAFFIC CONTROL, ATMOSPHERIC

EFFECTS, FLIGHT SAFETY, METEOROLOGICAL SERVICES,

METEOROLOGY, WEATHER

N82-26199"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

JOINT UNIVERSITY PROGRAM FOR AIR TRANSPORTATION

RESEARCH, 1981

Jun. 1982 235 p refs Proc. of a Conf. held at Washington,

D.C., 11 Dec. 1981

(NGL-22-009-640; NGR-36-O09-017; NGL-31-001-252)

(NASA-CP-2224; L-15346; NAS 1.55:2224) Avail: NTIS HC

A11/MF A01 CSCL01B

AIR NAVIGATION, AUTOMATIC GAIN CONTROL, DEICERS,
01 AERONAUTICS (GENERAL)

INTERPROCESSOR COMMUNICATION,

MICROPROCESSORS

LORAN C,

N82-26217"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECTS OF WING-LEADING-EDGE MODIFICATIONS ON A

FULL-SCALE, LOW-WING GENERAL AVIATION AIRPLANE:

WlNO-TUNNEL INVESTIGATION OF HIGH-ANGLE-OF-ATTACK

AERODYNAMIC CHARACTERISTICS

W. A. NEWSOM, JR., D. R. SATRAN, and J. L. JOHNSON, JR.

Jun. 1982 107p refs

(NASA-TP-2011; L-15101; NAS 1.60:2011) Avail: NTIS HC

A06/MF A01 CSCL 01A

AERODYNAMIC CHARACTERISTICS, AERODYNAMIC

STALLING, ANGLE OF ATTACK, GENERAL AVIATION

AIRCRAFT, LEADING EDGES, WIND TUNNEL TESTS

N82-31294"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

NOISE AND ECONOMIC CHARACTERISTICS OF AN

ADVANCED BLENDED SUPERSONIC TRANSPORT CONCEPT

J. K. MOLLOY, W. D. GRANTHAM, and M. J. NEUBAUER, JR.

Sep. 1982 32 p refs

(NASA-TP-2073; L.15297; NAS 1.60:2073) Avail: NTIS HC

A03/MF A01 CSCL 01B

ECONOMIC FACTORS, NOISE PREDICTION (AIRCRAFT),

SUPERSONIC AIRCRAFT

N83-33827"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

PROCEEDINGS: SIXTH ANNUAL WORKSHOP ON

METEOROLOGICAL AND ENVIRONMENTAL INPUTS TO

AVIATION SYSTEMS

W. FROST, ed., D. W. CAMP, ed., and L. W. HERSHMAN, ed.

Apr. 1983 140 p refs Workshop held in Tullahoma, Tenn.,

26-28 Oct. 1982; sponsored in cooperation with NOAA and FAA

Prepared in cooperation with Tennessee Univ. Space Inst.,

Tullahoma Original contains color illustrations

(NAS8-34627)

(NASA-CP-2274; NAS 1.55:2274; FAA-RD-82-72; AD-A133965)

Avail: NTIS HC A07/MF A01 CSCL 01A

AIR TRAFFIC CONTROL, FLIGHT SAFETY,

METEOROLOGICAL PARAMETERS, SAFETY FACTORS

N84-11099"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

JOINT UNIVERSITY PROGRAM FOR AIR TRANSPORTATION

RESEARCH, 1982

Washington Oct. 1983 147 p refs Conf. held in Hampton,

Va., 10 Dec. 1982

(NASA-CP-2285; L-15688; NAS 1.55:2285) Avail: NTIS HC

A07/MF A01 CSCL 01B

CONFERENCES, DISTRIBUTED PROCESSING, LORAN C,

MICROCOMPUTERS, RESEARCH AND DEVELOPMENT

N84-12029"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va. -

CONTROLS, DISPLAYS, AND INFORMATION TRANSFER FOR

GENERAL AVIATION IFR OPERATIONS

H. P. BERGERON, ed. and J. D. SHAUGHNESSY, ed.

Washington Oct. 1983 272 p refs Workshop held in

Hampton, Va., 30-31 Aug. 1982

(NASA-CP-2279; L-15649; NAS 1.55:2279) Avail: NTIS HC

A12/MFA01 CSCL01B

ACCIDENT INVESTIGATION, AIRCRAFT ACCIDENTS,

CONFERENCES, CONTROL THEORY, DISPLAY DEVICES,

FLIGHT CONTROL, INSTRUMENT FLIGHT RULES, PILOT

TRAINING, PILOTLESS AIRCRAFT, SAFETY

4

N84-27660"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ADVANCED AERODYNAMICS. SELECTED NASA RESEARCH

Washington Dec. 1981 97 p refs Presented at the 5th Ann.

Status Rev. of the NASA Aircraft Energy Efficiency (ACEE) Energy

Efficient Transport Prog., Edwards, Calif., 14-15 Sep. 1981

(NASA-CP-2208; L-14949; NAS 1.55:2208) Avail: NTIS HC

A05/MF A01 CSCL 01B

ACEE PROGRAM, AERODYNAMICS, AIRFOILS,

CONFERENCES, DESIGN ANALYSIS, PROPELLERS

N85-17934"# National Aeronautics and Space Administration.

Dryden (Hugh L.) Flight Research Center, Edwards, Calif.

ON THE FRONTIER: FLIGHT RESEARCH AT DRYDEN

1946-1981

R. P. HALLION 1984 394 p refs

(NASA-SP-4303; NAS 1.21:4303; LC-83-14136) Avail: NTIS MF

A01; SOD HC $15.00 as SN-033-000-00893-7 CSCL 01B

The history of flight research at the NASA Hugh L. Dryden

Flight Research Center is recounted. The period of emerging

supersonic flight technology (1944 to 1959) is reviewed along with

the era of flight outside the Earth's atmosphere (1959 to 1981).

Specific projects such as the X-15, Gemini, Apollo, and the space

shuttle are addressed. The flight chronologies of various aircraft

and spacecraft are given. R.S.F.

N85-23683"# National Aeronautics and Space Administration,

Washington, D.C.

MODEL RESEARCH: THE NATIONAL ADVISORY COMMITTEE

FOR AERONAUTICS, 1915-1958, VOLUME I

A. ROLAND 1984 432 p refs 2 Vol.

(NASA-SP-4103-VOL-1; NAS 1.21:4103-VOL-1) Avail: NTIS HC

A19/MF A01; also available from SOD HC $26.00 as set of 2

CSCL 01B

The National Advisory Committee for Aeronautics, the

predecessor of NASA, was the premier aeronautical research

organization in the United States. It conducted scientific study of

the problems of flight with a view to their practical solution. This

institutional history traces the birth and evolution of the NACA

and analyzes such recurrent themes as the roles of science and

engineering, the influence of politics on technology, the way in

which the institution shapes technology and technology shapes

the institution, the contributions of key individuals, the nature of

the research process, and the relation between military and civilian

aviation. Author

N85-23684"# National Aeronautics and Space Administration,

Washington, D.C.

MODEL RESEARCH, THE NATIONAL ADVISORY COMMITTEE

FOR AERONAUTICS, 1915-1958, VOLUME 2

A. ROLAND 1985 414 p refs 2 Vol.

(NASA-SP-4103-VOL-2; NAS 1.21:4103-VOL-2) Avail: NTIS HC

A18/MF A01; also available from SOD HC $26.00 as set of 2

CSCL 01B

Appendices providing comprehensive data on personnel,

organization, funding, research programs, and publications of the

National Advisory Committee for Aeronautics (NACA) are

presented. Information concerning NACA-related legislation and

research facilities is also included. M.G.

N85-28912"# McLean (F. Edward), Yorktown, Va.

SUPERSONIC CRUISE TECHNOLOGY

F. E. MCLEAN Feb. 1985 194 p refs Original contains

color illustrations

(NASW-3531)

(NASA-SP-472; NAS 1.21:472; LC-83-26912) Avail: NTIS HC

A09/MF A01; SOD HC $6.50 as 033-000-00944-5 CSCL 01B

The history and status of supersonic cruise research is covered.

The early research efforts of the National Advisory Committee for

Aeronautics and efforts during the B-70 and SST phase are

included. Technological progress made during the NASA

Supersonic Cruise Research and Variable Cycle Engine programs

are presented. While emphasis is on NASA's contributions to
supersoniccruiseresearchin the U.S,,alsonotedare

developments in England,France,and Russia.Writtenin

nontechnical language, thisbookpresentsthemostcritical

technology issuesandresearchfindings. Author

N85-32089"# Loftin (Laurence K., Jr.), Newport News, Va.

QUEST FOR PERFORMANCE: THE EVOLUTION OF MODERN

AIRCRAFT

L. K. LOFTIN, JR. 1985 548 p refs Original contains color

illustrations

(NASW-3490)

(NASA-SP-468; NAS 1.21:468) Avail: NTIS HC A23/MF A01;

SOD HC $26.00 as 033-000-00902-0 CSCL 01B

The technical evolution of the subsonic airplane is traced from

a curiosity at the beginning of World War I to the highly useful

machine of today. Included are descriptions of significant aircraft

which incorporated important technical innovations and served to

shape the future course of aeronautical development, as well as

aircraft which represented the state-of-art in a particular time frame

or were much used or liked. The discussion is related primarily to

aircraft configuration evolution and associated aerodynamic

characteristics and, to a lesser extent, to developments in aircraft

construction and propulsion. The material is presented in a manner

designed to appeal to the nontechnical reader who is interested

in the evolution of the airplane, as well as to students of

aeronautical engineering and others with an aeronautical

background. Author

N86-16187"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

VORTEX WAKE ALLEVIATION STUDIES WITH A VARIABLE

TWIST WING

G. T. HOLBROOK, D. M. DUNHAM, and G. C. GREENE Nov.

1985 117 p refs

(NASA-TP-2442; L-15870; NAS 1.60:2442) Avail: NTIS HC

A06/MF A01 CSCL 01B

AIRCRAFT WAKES, AIRFOILS, CONTROL SURFACES,

SLIPSTREAMS, SPOILERS, TRAILING EDGES, TWISTED WINGS,

VARIABLE GEOMETRY STRUCTURES, VORTEX ALLEVIATION,

VORTICES, WIND TUNNEL TESTS, WING FLAPS, WING SPAN

N86-23552" National Aeronautics and Space Administration,

Washington, D.C.

A CUMULATIVE INDEX TO A CONTINUING BIBLIOGRAPHY

ON AERONAUTICAL ENGINEERING

1986 521 p

(NASA-SP-7037(196); NAS 1.21:7037(196)) Avail: NTIS HC

A22 CSCL 01A

This bibliography is a cumulative index to the abstracts

contained in NASA-SP-7037(184) through NASA-SP-7037(195) of

Aeronautical Engineering: A Continuing Bibliography. NASA

SP-7037 and its supplements have been compiled through the

cooperative efforts of the American Institute of Aeronautics and

Astronautics (AIAA) and the National Aeronautics and Space

Administration (NASA). This cumulative index includes subject,

personal author, corporate source, foreign technology, contract,

report number, and accession number indexes. Author

N86-29762"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

MOTION AND INTERACTION OF DECAYING TRAILING

VORTICES IN SPANWISE SHEAR WIND

C. H. LIU and T. LU (New York Univ., New York.) Sep. 1986

26 p

(NASA-TP-2599; L-16040; NAS 1.60:2599) Avail: NTIS HC

A03/MF A01 CSCL 01B

SHEAR FLOW, TRAILING EDGES, VORTICES, WAKES

02 AERODYNAMICS

N86-32389" National Aeronautics and Space Administration,

Washinoton. D.C.

AERONAUTICAL ENGINEERING: A CONTINUING BIBLIOGRAPHY WITH INDEXES (SUPPLEMENT 204)

Sep. 1986 122p

(NASA-SP-7037(204); NAS 1.21:7037(204)) Avail: NTIS HC A06

CSCL 01A

This bibliography lists 419 reports, articles, and other documents

introduced into the NASA scientific and technical information

system in August 1986. Author

02

AERODYNAMICS

Includes aerodynamics of bodies, combinations, wings, rotors, and

control surfaces; and internal flow in ducts and turbomachinery.

N77-30089"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

COLD AIR PERFORMANCE OF A 12.766-CENTIMETER-TIPDIAMETER AXIAL-FLOW COOLED TURBINE. 2: EFFECT OF AIR

EJECTION ON TURBINE PERFORMANCE

J. E. HAAS and M. G. KOFSKEY Aug. 1977 37 p refs

Prepared in cooperation with Army Air Mobility Res. and Develop.

Lab., Cleveland

(NASA-TP-1018) Avail: NTIS HC A03/MF A01 CSCL 21E

AIR COOLING, AXIAL FLOW TURBINES, PERFORMANCE

N77-32082"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

COLD-AIR PERFORMANCE OF A 12.766-CENTIMETER-TIPDIAMETER AXIAL-FLOW COOLED TURBINE. 3: EFFECT OF

ROTOR TIP CLEARANCE ON OVERALL PERFORMANCE OF A

SOLID BLADE CONFIGURATION

J. E. HAAS (Army Air Mobility Research and Development Lab.,

Cleveland, Ohio) and M. G. KOFSKEY Sep. 1977 24 p refs

(NASA-TP-1032; E-9181) Avail: NTIS HC A02/MF A01 CSCL

01A

AXIAL FLOW TURBINES, BLADE TIPS, CLEARANCES,

COMPRESSOR EFFICIENCY

N77-33111"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va,

SPIN-TUNNEL INVESTIGATION OF THE SPINNING

CHARACTERISTICS OF TYPICAL SINGLE-ENGINE GENERAL

AVIATION AIRPLANE DESIGNS. 1. LOW-WING MODEL A:

EFFECTS OF TAIL CONFIGURATIONS

S, M. BURK, JR., J. S. BOWMAN, JR., and W. L. WHITE Sep.

1977 92 p refs

(NASA-TP-1009; L-11227) Avail: NTIS HC A05/MF A01

CSCL 01A

AERODYNAMIC CONFIGURATIONS, AIRCRAFT DESIGN,

LOW WING AIRCRAFT, SPIN TESTS, TAIL ASSEMBLIES

N77-33112"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

THEORETICAL PARAMETRIC STUDY OF THE RELATIVE

ADVANTAGES OF WlNGLETS AND WING-TIP EXTENSIONS

H. H. HEYSON, G. D. RIEBE, and C. L. FULTON Sep. 1977

75 p refs

(NASA-TP-1020; L-11679) Avail: NTIS HC A04/MF A01

CSCL 01A

AERODYNAMIC CHARACTERISTICS, EXTENSIONS, WING

TIPS, WINGLETS
02 AERODYNAMICS

N77-85474" National Aeronautics and Space Administration.

Dryden (Hugh L.) Flight Research Center, Edwards, Calif.

SUPERCRITICAL WING TECHNOLOGY: A REPORT ON FLIGHT

EVALUATIONS

1972 133 p

(NASA-SP-301; C72-71337)

N78-10030"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECT OF A SIMULATED ENGINE JET BLOWING ABOVE

AN ARROW WING AT MACH 2.0

B. L. SHROUT and C. HAYES 1977 56 p refs

(NASA-TP-1050; L-11751) Avail: NTIS HC A04/MEA01

CSCL 01A

ARROW WINGS, EXHAUST FLOW SIMULATION, JET

EXHAUST

N78-11002"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EXPERIMENTAL PERFORMANCE OF A 13.65-CENTIMETER-TIPDIAMETER TANDEM-BLAOED SWEPTBACK CENTRIFUGAL

COMPRESSOR DESIGNED FOR A PRESSURE RATIO OF 6

H. A. KLASSEN, J. R WOOD (Army Air Mobility Res. and Develop.

Lab., Cleveland), and L. F. SCHUMANN (Army Air Mobility Res.

and Develop. Lab., Cleveland) Nov. 1977 27 p refs

(NASA-TP-1091) Avail: NTIS HC A03/MF A01 CSCL 01A

CENTRIFUGAL COMPRESSORS, GAS TURBINE ENGINES,

PERFORMANCE TESTS, PRESSURE MEASUREMENT

N78-11007"# National Aeronautics and Space Administration,

Washington, D.C.

A SURVEY OF COMPUTATIONAL AERODYNAMICS IN THE

UNITED STATES

A. GESSOW and D. J. MORRIS 1977 49 p refs

(NASA-SP-394) Avail: NTIS HC A03/MF A01 CSCL 01A

Programs in theoretical and computational aerodynamics in the

United States are described. Those aspects of programs that relate

to aeronautics are detailed. The role of analysis at various levels

of sophistication is discussed as well as the inverse solution

techniques that are of primary importance in design methodology.

The research is divided into the broad categories of application

for boundary layer flow, Navier-Stokes turbulence modeling, internal

flows, two-dimensional configurations, subsonic and supersonic

aircraft, transonic aircraft, and the space shuttle. A survey of

representative work in each area is presented. Author

N78-11008"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EFFECT OF COOLANT FLOW EJECTION ON AERODYNAMIC

PERFORMANCE OF LOW-ASPECT-RATIO VANES. 2:

PERFORMANCE WITH COOLANT FLOW EJECTION AT

TEMPERATURE RATIOS UP TO 2

J. E. HASS (Army Air Mobility Res. and Develop. Lab., Cleveland

and M. G. KOESKEY Oct. 1977 34 p refs

(NASA-TP-1057; E-9213) Avail: NTIS HC A03/MF A01 CSCL

21E

AERODYNAMIC CHARACTERISTICS, CASCADE FLOW,

LIQUID COOLING, TEMPERATURE DISTRIBUTION, VANES

N78-12017"# National Aeronautics and Space Administration,

Washington, D.C.

WAKE VORTEX MINIMIZATION

1977 403 p Symp. held at Washington, 25-26 Feb. 1976

(NASA-SP-409) Avail: NTIS HC A18/MF A01 CSCL 01A

A status report is presented on research directed at reducing

the vortex disturbances of aircraft wakes. The objective of such a

reduction is to minimize the hazard to smaller aircraft that might

encounter these wakes. Inviscid modeling was used to study trailing

vortices and viscous effects were investigated. Laser velocimeters

were utilized in the measurement of aircraft wakes. Flight and

wind tunnel tests were performed on scale and full model scale

aircraft of various design. Parameters investigated included the

6

effect of wing span, wing flaps, spoilers, splines and engine thrust

on vortex attenuation. Results indicate that vortives may be

alleviated through aerodynamic means. For individual titles, see

N78-12018 through N78-12028.

N78-12038"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AERODYNAMIC CHARACTERISTICS AT MACH NUMBERS

FROM 0.33 TO 1.20 OF A WING-BODY DESIGN CONCEPT FOR

A HYPERSONIC RESEARCH AIRPLANE

J. L. DILLON and J. L. PITTMAN Dec. 1977 76 p refs

(NASA-TP-1044; L-11723) Avail: NTIS HC A05/MF A01

CSCL 01A

AERODYNAMIC CHARACTERISTICS, HYPERSONIC

AIRCRAFT, MACH NUMBER, STRUCTURAL DESIGN,

TRANSONIC WIND TUNNELS

N78-12039"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AN EXPERIMENTAL AND ANALYTICAL INVESTIGATION OF

PROPROTOR WHIRL FLUTTER

R. G. KVATERNIK and J. S. KOHN (Grumman Aerospace Corp.,

Bethpage, N.Y.) Dec. 1977 76 p refs

(NASA-TP-1047; L-11656) Avail: NTIS HC A05/MF A01

CSCL 01A

FLUTTER, PROPELLER BLADES, ROTATION

N78-12040"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SPIN-TUNNEL INVESTIGATION OF THE SPINNING

CHARACTERISTICS OF TYPICAL SINGLE-ENGINE GENERAL

AVIATION AIRPLANE DESIGNS. 2: LOW-WING MODEL A;

TAIL PARACHUTE DIAMETER AND CANOPY DISTANCE FOR

EMERGENCY SPIN RECOVERY

S. M. BURK, JR., J. S. BOWMAN, JR., and W. L. WHITE

Washington Nov. 1977 30 p refs

(NASA-TP-1076; L-11804) Avail: NTIS HC A03/MF A01

CSCL 01A

LIGHT AIRCRAFT, RECOVERY PARACHUTES, SPIN

STABILIZATION, TAIL ASSEMBLIES

N78-12041"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SUPERSONIC AERODYNAMIC CHARACTERISTICS OF A

SPARROW 3 TYPE MISSILE MODEL WITH WING CONTROLS

AND COMPARISON WITH EXISTING TAIL-CONTROL

RESULTS

W. J. MONTA Nov. 1977 84 p refs

(NASA-TP-1078; L-t1715) Avail: NTIS HCA05/MF A0t

CSCL 01A

AERODYNAMIC CHARACTERISTICS, SPARROW 3 MISSILE,

SUPERSONIC FLIGHT, TAIL ASSEMBLIES, WINGS

N78-13014"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECTS OF DEFLECTED THRUST ON THE LONGITUDINAL

AERODYNAMIC CHARACTERISTICS OF A CLOSE-COUPLED

WING-CANARD CONFIGURATION

L. P. YIP and J. W. PAULSON, JR Dec. 1977 88 p refs

(NASA-TP-1090; L-11886) Avail: NTIS HC A05/MF A01

CSCL 01A

CANARD CONFIGURATIONS, DEFLECTION, LONGITUDINAL

STABILITY, THRUST, WIND TUNNEL TESTS
N78-13016"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECTS OF ROUGHNESS SIZE ON THE POSITION OF

BOUNDARY-LAYER TRANSITION AND ON THE AERODYNAMIC

CHARACTERISTICS OF A 65 DEG. SWEPT DELTA WING AT

SUPERSONIC SPEEDS

R. L. STALLINGS, JR. and M. LAMB Dec. 1977 49 p refs

(NASA-TP-1027; L-11496) Avail: NTIS HC A03/MF A01

CSCL 01A

AERODYNAMIC CHARACTERISTICS, BOUNDARY LAYER

TRANSITION, DELTA WINGS, ROUGHNESS, SUPERSONIC

SPEED

N78-13017"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

COMPUTATION OF TRANSONIC BOATTAIL FLOW WITH

SEPARATION

R. G. WlLMOTH Dec. 1977 65 p refs

(NASA-TP-1070; L-11669) Avail: NTIS HC A04/MF A01

CSCL 01A

BOATTAILS, COMPUTATION, ITERATION, SEPARATED

FLOW, TRANSONIC FLOW

N76-14997"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

IMPROVEMENT OF MANEUVER AERODYNAMICS BY

SPANWlSE BLOWING

G. E. ERICKSON (George Washington Univ.) and J. F.

CAMPBELL Dec. 1977 68 p refs

(NASA-Tpo1065; L-11642) Avail: NTIS HC A04/MF A01

CSCL 01A

AERODYNAMIC STABILITY, AIRCRAFT MANEUVERS,

FIGHTER AIRCRAFT, SPANWlSE BLOWING, WIND TUNNEL

MODELS

N78-14998"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

COLD-AIR PERFORMANCE OF A TIP TURBINE DESIGNED TO

DRIVE A LIFT FAN

J. E. HAAS, M. G. KOFSKEY, and G. M. HOTZ Jan. 1978 23

p refs

(NASA-TP-1126; E-9293) Avail: NTIS HC A02/MF A01 CSCL

20E

LIFT FANS, TURBINES, V/STOL AIRCRAFT

N78-16000"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

LONGITUDINAL AERODYNAMIC CHARACTERISTICS AT MACH

0.60 TO 2.86 OF A FIGHTER CONFIGURATION WITH STRUT

BRACED WING

S. M. DOLLYHIGH, W. J. MONTA, and G. SANGIORGIO Dec.

1977 149p refs

(NASA-TP-1102; L-11801) Avail: NTIS HC A07/MF A01

CSCL 01A

AERODYNAMIC CHARACTERISTICS, FIGHTER AIRCRAFT,

LONGITUDINAL STABILITY, STRUTS, WINGS

N78-16001"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

COLD-AIR PERFORMANCE OF A TIP TURBINE DESIGNED TO

DRIVE A LIFT FAN. 3: EFFECT OF SIMULATED FAN LEAKAGE

ON TURBINE PERFORMANCE

J. E. HAAS (Army R and T Labs.), M. G. KOFSKEY, G. M. HOTZ,

and S. M FUTRAL, JR. Jan. 1978 28 p refs

(NASA-TP-1109; E-9331) Avail: NTIS HC A03/MF A01 CSCL

01A

ENGINE DESIGN, LIFT FANS, PERFORMANCE TESTS, TIP

DRIVEN ROTORS, TURBINE ENGINES

02 AERODYNAMICS

N78-17000"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

DYNAMIC STALL EXPERIMENTS ON THE NACA 0012

AIRFOIL

K. W. MCALISTER, L. W. CARR, and W. J. MCCROSKEY Jan.

1978 166 p refs

(NASA-TP-1100; A-7096) Avail: NTIS HC A08/MF A01 CSCL

01A

AERODYNAMIC LOADS, AERODYNAMIC STALLING,

AIRFOILS, DYNAMIC RESPONSE

N78-17997"# National Aeronautics and Space Administration.

Dryden (Hugh L.) Flight Research Center, Edwards, Calif.

EFFECT OF WlNGLETS ON A FIRST-GENERATION JET

TRANSPORT WING. 4: STABILITY CHARACTERISTICS FOR

A FULL-SPAN MODEL AT MACH 0.30

R. R. MEYER, JR. Feb. 1978 74 p refs

(NASA-TP-1119; L-11705) Avail: NTIS HC A04/MF A01

CSCL 01A

AIRCRAFT LANDING, AIRCRAFT STABILITY, SCALE

MODELS, TRANSPORT AIRCRAFT, WINGLETS, WINGS

N78-17998"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EFFECT OF DESIGN CHANGES ON AERODYNAMIC AND

ACOUSTIC PERFORMANCE OF TRANSLATING-CENTERBODY

SONIC INLETS

B. A. MILLER Feb. 1978 49 p refs

(NASA-TP-1132; E-9283) Avail: NTIS HC A03/MF A01 CSCL

01A

ACOUSTIC PROPERTIES, AERODYNAMIC CONFIGURATIONS, INLET FLOW, SCALE MODELS

N78-17999"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

TWO-DIMENSIONAL TRANSONIC TESTING WITH SPLITTER

PLATES

S. DAVIS and B. SATYANARAYANA Feb. 1978 24 p refs

(NASA-TP-1153; A-7221) Avail: NTIS HC A02/MF A01 CSCL

01A

FLAT PLATES, STATIC PRESSURE, TRANSONIC FLOW,

TRANSONIC WIND TUNNELS, WIND TUNNEL TESTS

N78-20078"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SIMPLIFIED SONIC-BOOM PREDICTION

H. W. CARLSON Mar. 1978 50 p refs

(NASA-TP-1122; L-11794) Avail: NTIS HC A03/MF A01

CSCL 20A

AERODYNAMIC CONFIGURATIONS, CALCULATORS,

CHARTS, PREDICTION ANALYSIS TECHNIQUES, SONIC

BOOMS

N78-20079"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

WIND-TUNNEL INVESTIGATION AT MACH NUMBERS FROM

1.90 TO 2.86 OF A CANARD-CONTROLLED MISSILE WITH

RAM-AIR-JET SPOILER ROLL CONTROL

A. B. BLAIR, JR. Mar. 1978 104 p refs

(NASA-TP-1124; L-11873) Avail: NTIS HC A06/MF A01

CSCL 01A

CANARD CONFIGURATIONS, LATERAL CONTROL, MISSILE

CONFIGURATIONS, SPOILERS, SUPERSONIC FLOW, WIND

TUNNEL TESTS
02 AERODYNAMICS

N78-20080"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EFFECT OF COOLING-HOLE GEOMETRY ON AERODYNAMIC

PERFORMANCE OF A FILM-COOLED TURBINE VANE TESTED

WITH COLD AIR IN A TWO-DIMENSIONAL CASCADE

J. F. KLINE, R. G. STABE, and T. P. MOFFITT Mar. 1978 49

p refs

(NASA-TP.1136; E-9174) Avail: NTIS HC A03/MF A01 CSCL

01A

AERODYNAMIC CHARACTERISTICS, CASCADE WIND

TUNNELS, COOLING SYSTEMS, FILM COOLING, HOLE

DISTRIBUTION (MECHANICS), TURBINE BLADES, VANES

N78-20081"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECT OF WINGLETS ON A FIRST-GENERATION JET

TRANSPORT WING. 5: STABILITY CHARACTERISTICS OF A

FULL-SPAN WING WITH A GENERALIZED FUSELAGE AT HIGH

SUBSONIC SPEEDS

P. F. JACOBS Mar. 1978 71 p refs

(NASA-TP-1163; L-11982) Avail: NTIS HC A04/MF A01

CSCL 01A

AERODYNAMIC CHARACTERISTICS, AERODYNAMIC

STABILITY, JET AIRCRAFT, SUBSONIC SPEED, WING SPAN,

WINGLETS

N78-21055"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

NUMERICAL STUDY OF TRANSONIC FLOW OVER

OSCILLATING AIRFOILS USING THE FULL POTENTIAL

EQUATION

K ISOGAI Apr. 1978 41 p refs

(NASA-TP-1120; L-11984) Avail: NTIS HC A03/MF A01

CSCL 01A

AERODYNAMICS, AIRFOILS, FINITE DIFFERENCE THEORY,

TRANSONIC FLOW

N78-22028"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECTS OF STORES ON LONGITUDINAL AERODYNAMIC

CHARACTERISTICS OF A FIGHTER AT SUPERSONIC SPEEDS

S. M. DOLLYHIGH, G. SANGIORGIO, and W. J. MONTA Apr.

1978 46p refs

(NASA.TP-1175; L-11874) Avail: NTIS HC A03/MF A01

CSCL 10C

AERODYNAMIC CHARACTERISTICS, EXTERNAL STORES,

F-16 AIRCRAFT, LONGITUDINAL STABILITY, SUPERSONIC

SPEED

N78-23058"# National Aeronautics and Space Administration.

Dryden (Hugh L.) Flight Research Center, Edwards, Calif.

FLIGHT-MEASURED BUFFET CHARACTERISTICS OF A

SUPERCRITICAL WING AND A CONVENTIONAL WING ON A

VARIABLE-SWEEP AIRPLANE

R. C. MONAGHAN May 1978 39 p refs

(NASA-TP-1244; H-991) Avail: NTIS HC A03/MF A01 CSCL

01A

BUFFETING, F-111 AIRCRAFT, SUPERCRITtCAL WINGS,

VARIABLE SWEEP WINGS

N78-24046"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

POWERED-LIFT AERODYNAMICS AND ACOUSTICS

Washington 1976 502 p refs Conf. held at Hampton, Va.,

24-26, May 1976

(NASA-SP-406) Avail: NTIS HC A22/MF A01 CSCL 01A

Powered lift technology is reviewed. Topics covered include:

(1) high lift aerodynamics; (2) high speed and cruise aerodynamics;

(3) acoustics; (4) propulsion aerodynamics and acoustics; (5)

aerodynamic and acoustic loads; and (6) full-scale and flight

research. For individual titles, see N78-24047 through N78-24076.

N78-25058"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

A DISTRIBUTED VORTEX METHOD FOR COMPUTING THE

VORTEX FIELD OF A MISSILE

R. L. BARGER Jun. 1978 19 p refs

(NASA.TP-1183; L-11963) Avail: NTIS HC A02/MF A01

CSCL 01A

APPROXIMATION, FLOW DISTRIBUTION, MISSILE BODIES,

VORTEX SHEETS

N78-25059"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AERODYNAMIC CHARACTERISTICS AT MACH NUMBER 0,2

OF A WING-BODY CONCEPT FOR A HYPERSONIC RESEARCH

AIRPLANE

J. L. DILLON and T. R. CREEL, JR. Jun. 1978 48 p refs

(NASA-TP-1189: L-12063) Avail: NTIS HC A03/MF A01

CSCL 01A

AERODYNAMIC CHARACTERISTICS, BODY-WING

CONFIGURATIONS, HYPERSONIC AIRCRAFT, SUBSONIC

SPEED

N78-25060"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECTS OF SPANWISE NOZZLE GEOMETRY AND LOCATION

ON THE LONGITUDINAL AERODYNAMIC CHARACTERISTICS

OF A VECTORED-ENGINE-OVER-WING CONFIGURATION AT

SUBSONIC SPEEDS

L. D. LEAVITT and L. P. YIP May 1978 78 p refs

(NASA-TP-1215; L-12015) Avail: NTIS HC A05/MFA01

CSCL 01A

AERODYNAMIC CHARACTERISTICS, SPANWISE BLOWING,

THRUST VECTOR CONTROL, WIND TUNNEL MODELS

N78-25061"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

A WIND-TUNNEL STUDY OF THE APPLICABILITY OF

FAR-FIELD SONIC-BOOM THEORY TO THE SPACE SHUTTLE

ORBITER

H. W. CARLSON and R. J. MACK Jun. 1978 48 p refs

(NASA-TP-1186; L-12051) Avail: NTIS HC A03/MF A01

CSCL 01A

SCALE MODELS, SONIC BOOMS, SPACE SHUTTLE

ORBITERS, WIND TUNNEL TESTS

N78-26109"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EXPERIMENTAL AND ANALYTICAL INVESTIGATION OF A

NONAXlSYMMETRIC WEDGE NOZZLE AT STATIC

CONDITIONS

G. T. CARSON, JR. and M L. MASON Jul. 1978 45 p refs

"(NASA-TP-1188; L-12065) Avail: NTIS HC A03/MF A01

CSCL 01A

EXHAUST NOZZLES, PRESSURE MEASUREMENT, STATIC

TESTS, WEDGE FLOW

N78-28056"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AN ANALYSIS OF THE GUST-INDUCED OVERSPEED TRENDS

OF HELICOPTER ROTORS

J. L. JENKINS, JR. and W. T. YEAGER, JR. (AVRADCOM Res.

and Technol. Labs.) Jul. 1978 23 p refs

(NASA-TP-1213; AVRADCOM-TR-78-24; L-12159) Avail: NTIS

HCA02/MFA01 CSCL01A

GUST LOADS, HELICOPTERS, HIGH SPEED, ROTARY

WINGS
N78-28057"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

STATIC PERFORMANCE OF FIVE TWIN-ENGINE

NONAXlSYMMETRIC NOZZLES WITH VECTORING AND

REVERSING CAPABILITY

F. J. CAPONE Jul. 1978 66 p refs

(NASA-TP-1224; L-12067) Avail: NTIS HC A04/MF A01

CSCL 01A

NOZZLE GEOMETRY, STATIC AERODYNAMIC

CHARACTERISTICS, THRUST REVERSAL, THRUST VECTOR

CONTROL

N78-30052"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

BOUNDARY-LAYER SEPARATION ON ISOLATED BOATTAIL

NOZZLES M.S. Thesla - George Washington Unlv.

W. K. ABEYOUNIS Aug. 1978 63 p refs

(NASA-TP-1226; L-12104) Avail: NTIS HC A04/MF A01

CSCL 10A

BOATTAILS, BOUNDARY LAYER SEPARATION, TRANSONIC

NOZZLES

N78-30053"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

STATIC AERODYNAMIC CHARACTERISTICS OF A WINGED

SINGLE-STAGE-TO-ORBIT VEHICLE AT MACH NUMBERS

FROM 0.3 TO 4.63

D. C. FREEMAN, JR. and R. H. FOURNIER Aug. 1978 119 p

refs

(NASA-TP-1233; L-12200) Avail: NTIS HC A06/MF A01

CSCL 01A

SINGLE STAGE TO ORBIT VEHICLES, STATIC

AERODYNAMIC CHARACTERISTICS

N76-30054*# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

APPROXIMATE INDICIAL LIFT FUNCTION FOR TAPERED,

SWEPT WINGS IN INCOMPRESSIBLE FLOW

M. J. QUEIJO, W. R. WELLS (Wright State Univ., Dayton, Ohio),

and D. A. KESKAR (Cincinnati Univ., Ohio) Aug. 1978 32 p

refs

(NASA-TP-1241; L-12110) Avail: NTIS HC A03/MF A01

CSCL 01A

INCOMPRESSIBLE FLOW, LIFT, SWEPT WINGS

N78-30055"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AERODYNAMIC CHARACTERISTICS AT MACH 6 OF A

WING-BODY CONCEPT FOR A HYPERSONIC RESEARCH

AIRPLANE

J. L. DILLON and J. L. PITTMAN Aug. 1978 59 p refs

(NASA-TP-1249; L-12183) Avail: NTIS HC A04/MF A01

CSCL 0tA

AERODYNAMIC CHARACTERISTICS, BODY-WING AND TAIL

CONFIGURATIONS, HYPERSONIC AIRCRAFT, HYPERSONIC

WIND TUNNELS, WIND TUNNEL MODELS

N78-30056"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

THEORETICAL ESTIMATION OF THE TRANSONIC

AERODYNAMIC CHARACTERISTICS OF A SUPERCRITICALWING TRANSPORT MODEL WITH TRAILING-EDGE CONTROLS

J. M. LUCKRING and M. J. MANN Aug. 1978 34 p refs

(NASA-TP-1253; L-11257) Avail: NTIS HC A03/MF A01

CSCL 01A

AERODYNAMIC CHARACTERISTICS, SUPERCRITICAL

WINGS, SUPERSONIC AIRCRAFT, TRAILING EDGES

02 AERODYNAMICS

N78-30057"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

PERFORMANCE WITH AND WITHOUT INLET RADIAL

DISTORTION OF A TRANSONIC FAN STAGE DESIGNED FOR

REDUCED LOADING IN THE TIP REGION

J. F. SCHMIDT and R. S. RUGGERI Aug. 1978 84 p refs

(NASA-TP-1294; E-9246) Avail: NTIS HC A05/MF A01 CSCL

01A

INTAKE SYSTEMS, ROTOR BLADES (TURBOMACHINERY),

TRANSONIC COMPRESSORS

N78-31045"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AERODYNAMIC CHARACTERISTICS OF A HYPERSONIC

RESEARCH AIRPLANE CONCEPT HAVING A 70 DEC SWEPT

DOUBLE-DELTA WING AT MACH NUMBER 0.2

J. A. PENLAND, T. R. CREEL, JR., and J. L. DILLON Sap. 1978

83 p refs

(NASA-TP-1252; L-12215) Avail: NTIS HC A05/MF A01

CSCL 01A

AERODYNAMIC CHARACTERISTICS, DELTA WINGS,

HYPERSONIC AIRCRAFT, RESEARCH AIRCRAFT, SWEPT

WINGS

N78-32055"# National Aeronautics and Space Administration.

Flight Research Center, Edwards, Calif.

YF-12 EXPERIMENTS SYMPOSIUM, VOLUME 1

Aug. 1978 286 p refs Symp. held at Edwards, Calif., 13-15

Sep. 1978 Prepared by James and Associates, Lancaster, Calif.

(NASA-CP-2054-VOL-1; H-1059) Avail: NTIS HC A13/MF A01

CSCL 01A

CONFERENCES, NASA PROGRAMS, RESEARCH AIRCRAFT,

SUPERSONIC CRUISE AIRCRAFT RESEARCH, YF-12

AIRCRAFT

N78-32067"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

WIND-TUNNEL INVESTIGATION AT SUPERSONIC SPEEDS OF

A CANARD-CONTROLLED MISSILE WITH FIXED AND

FREE-ROLLING TAIL FINS

A. B. BLAIR, JR. Sep. 1978 79 p refs

(NASA-TP-1316; L-12297) Avail: NTIS HC A05/MF A01

CSCL 01A

CANARD CONFIGURATIONS, FREE FLOW, SUPERSONIC

SPEED, WIND TUNNEL TESTS

N78-33050"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SUBSONIC DYNAMIC STABILITY CHARACTERISTICS OF TWO

CLOSE-COUPLED CANARD-WING CONFIGURATIONS

R. P. BOYDEN Oct. 1978 80 p refs

(NASA-TP-1291; L-12057) Avail: NTIS HC A05/MF A01

CSCL 01A

CANARD CONFIGURATIONS, DYNAMIC STABILITY,

SUBSONIC SPEED

N78-33051"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ESTIMATION OF LEADING-EDGE THRUST FOR SUPERSONIC

WINGS OF ARBITRARY PLANFORM

H, W. CARLSON and R. J. MACK Oct, 1978 51 p refs

(NASA-TP-1270; L-12283) Avail: NTIS HC A04/MF A01

CSCL 01A

DELTA WINGS, LEADING EDGES, SUPERSONIC SPEED

9
02 AERODYNAMICS

N78-33053"# National Aeronautics and Space Administration.

Dryden (Hugh L.) Flight Research Center, Edwards, Calif.

COMPARISON OF CONCURRENT STRAIN GAGE- AND

PRESSURE TRANSDUCER-MEASURED FLIGHT LOADS ON A

LIFTING REENTRY VEHICLE AND CORRELATION WITH WIND

TUNNEL PREDICTIONS

M H TANG, W. J. SEFIC, and R. G. SHELDON Oct. 1978 42

p refs

(NASA-TP-1331; H-1035) Avail: NTIS HC A03/MF A01 CSCL

01A

AERODYNAMIC LOADS, FLIGHT LOAD RECORDERS,

LIFTING REENTRY VEHICLES, PRESSURE SENSORS, STRAIN

GAGES

N78-33054"# National Aeronautics and Space Administration.

Dryden (Hugh L.) Flight Research Center, Edwards, Calif.

AERODYNAMIC DERIVATIVES FOR AN OBLIQUE WING

AIRCRAFT ESTIMATED FROM FLIGHT DATA BY USING A

MAXIMUM LIKELIHOOD TECHNIQUE

R E. MAINE Oct. t978 73 p refs

(NASA-TP-1336; H-1003) Avail: NTIS HC A04/MF A01 CSCL

01A

AERODYNAMIC CHARACTERISTICS, AIRCRAFT CONFIGURATIONS, DEGREES OF FREEDOM, STABILITY DERIVATIVES,

WINGS

N79-10022"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

AERODYNAMIC PERFORMANCE OF A 1.35-PRESSURE-RATIO

AXIAL-FLOW FAN STAGE

W. M OSBORN, R. D. MOORE, and R. J. STEINKE Oct. 1978

108 p refs

(NASA-TP-1299; E-9025) Avail: NTIS HC A06/MF A01 CSCL

01A

AERODYNAMIC CHARACTERISTICS, AXIAL FLOW,

PRESSURE DISTRIBUTION, TURBOFANS

N79-12013"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

APPLICATION OF SHOCK TUBES TO TRANSONIC AIRFOIL

TESTING AT HIGH REYNOLDS NUMBERS

W. J. COOK (Iowa State Univ.), M. J. CHANEY (Iowa State Univ.),

L. L. PRESLEY, and G. T. CHAPMAN Nov. 1978 69 p refs

(NASA-TP-1268; A-6855) Avail: NTIS HC A04/MF A01 CSCL

01A

AIRFOILS, REYNOLDS NUMBER, SHOCK TUBES,

TRANSONIC FLOW

N79-13002"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECTS OF WING LEADING-EDGE FLAP DEFLECTIONS ON

SUBSONIC LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF A WING-FUSELAGE CONFIGURATION WITH A 44 DEG

SWEPT WING

W. P. HENDERSON Nov. 1978 38 p refs

(NASA-TP-1351; L-12481) Avail: NTIS HCA03/MF A01

CSCL 01A

AERODYNAMIC CHARACTERISTICS, BODY-WING CONFIGURATIONS, FLAPS (CONTROL SURFACES), LEADING EDGES,

SUBSONIC FLUTTER

N79-13003"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

ANALYSIS OF SUPERSONIC STALL BENDING FLUTTER IN

AXIAL-FLOW COMPRESSOR BY ACTUATOR DISK THEORY

J. J. ADAMCZYK Nov. 1978 58 p refs

(NASA-TP-1345; E-9186) Avail: NTIS HC A04/MF A01 CSCL

01A

ACTUATOR DISKS. SUPERSONIC FLUTTER, TURBOCOMPRESSORS

10

N79-14018"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va,

LOW-SPEED AERODYNAMIC CHARACTERISTICS OF A

16-PERCENT-THICK VARIABLE-GEOMETRY AIRFOIL

DESIGNED FOR GENERAL AVIATION APPLICATIONS

R. W. BARNWELL, K. W. NOONAN, and R. J. MCGHEE Dec.

1978 77 p refs Prepared in cooperation with Army Aviation

Research and Development Command, St. Louis, Mo.

(DA PROJ. 1L1-61102-AH-45)

(NASA-TP-1324; AVRADCOM-TR-78-45) Avail: NTIS HC

A05/MF A01 CSCL01A

AERODYNAMIC CHARACTERISTICS, AIRFOIL PROFILES,

GENERAL AVIATION AIRCRAFT, LOW SPEED

N79-14019"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

A LASER VELOCIMETER FLOW SURVEY ABOVE A STALLED

WING

W. H. YOUNG, JR., J. F. MEYERS, and D. R. HOAD Dec. 1978

138 p refs Prepared in cooperation with Army Aviation Research

and Development Command, St. Louis, Mo.

(DA PROJ. 1 L1-61102-AH-45)

(NASA-TP-1266; AVRADCOM-TR-78-50) Avail: NTIS HC

A07/MF A01 CSCL0tA

AERODYNAMIC STALLING, FLOW MEASUREMENT, LASER

DOPPLER VELOCIMETERS, WINGS

N79-14023"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

THEORETICAL EVALUATION OF HIGH-SPEED AERODYNAMICS

FOR ARROW-WING CONFIGURATIONS

S. M. D©LLYHIGH Jan. 1979 67 p refs

(NASA-TP-1358; L-12485) Avail: NTIS HC A04/MF A01

CSCL 01A

AERODYNAMIC CHARACTERISTICS, ARROW WINGS,

SUPERSONIC CRUISE AIRCRAFT RESEARCH

N79-14996"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

THEORETICAL STUDY OF VTOL TILT-NACELLE

AXlSYMMETRIC INLET GEOMETRIES

J. D. HAWK and N O. STOCKMAN Jan. 1979 29 p refs

(NASA-TP-1380; E-9756) Avail: NTIS HC AO3/MF A01 CSCL

01A

ENGINE INLETS, INLET FLOW, NACELLES, VERTICAL

TAKEOFF AIRCRAFT

N79-15000"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SONIC-BOOM MINIMIZATION WITH NOSE-BLUNTNESS

RELAXATION

C. M. DARDEN Jan. 1979 53 p refs

(NASA-TP-1348; L-12464) Avail: NTIS HC A04/MF A01

CSCL 20A

BLUNT BODIES, NOISE REDUCTION, NOSE CONES, SONIC

BOOMS, SURFACE GEOMETRY

N79-15902"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

A STUDY OF CANARD-WING INTERFERENCE USING

EXPERIMENTAL PRESSURE DATA AT TRANSONIC SPEEDS

B. B. GLOSS and K. E. WASHBURN Jan. 1979 71 p refs

(NASA-TP-1355; L-12491) Avail: NTIS HC A04/MF A01

CSCL 01A

CANARD CONFIGURATIONS, TRANSONIC SPEED, WIND

TUNNEL TESTS
N79-15903"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

A THEORETICAL INVESTIGATION OF FOREBODY SHAPES

DESIGNED FOR NATURAL LAMINAR BOUNDARY-LAYER

FLOW

R. L. BARGER Jan. 1979 18 p refs

(NASA-TP-1375; L-12550) Avail: NTIS HC A02/MF A01

CSCL 01A

FOREBODIES, LAMINAR BOUNDARY LAYER, SHAPES,

STRUCTURAL DESIGN

N79-16803"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECTS OF SPANWISE BLOWING ON THE SURFACE

PRESSURE DISTRIBUTION AND VORTEX-LIFT

CHARACTERISTICS OF A TRAPEZOIDAL WlNG-STRAKE

CONFIGURATION

J. F. CAMPBELL and G. E. ERICKSON (Northrop Corp., Hawthorne,

Calif.) Feb. 1979 72 p refs

(NASA-TP-1290; L-11641) Avail: NTIS HC A04/MF A01

CSCL 01A

NOSE FINS, PRESSURE DISTRIBUTION, WING SPAN

N79-16804"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

THE DESIGN OF SUPERCRITICAL WINGS BY THE USE OF

THREE-DIMENSIONAL TRANSONIC THEORY

M. J. MANN Feb. 1979 33 p refs

(NASA-TP-1400; L-12552) Avail: NTIS HC A03/MF A01

CSCL 01A

SUPERCRITICAL WINGS, THREE DIMENSIONAL FLOW,

TRANSONIC FLOW

N79-17806"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

A MODIFICATION TO LINEARIZED THEORY FOR PREDICTION

OF PRESSURE LOADINGS ON LIFTING SURFACES AT HIGH

SUPERSONIC MACH NUMBERS AND LARGE ANGLES OF

ATTACK

H. W. CARLSON Feb. 1979 39 p refs

(NASA-TP-1406; L-12654) Avail: NTIS HC A03/MF A01

CSCL 01A

AERODYNAMIC LOADS, DELTA WINGS, PRESSURE

DISTRIBUTION

N79-17808"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

STABILITY AND CONTROL CHARACTERISTICS OF A

MONOPLANAR ELLIPTIC MISSILE MODEL AT MACH NUMBERS

FROM 1.60 TO 2.86

W. C. SAWYER and G. SANGIORGIO Feb. 1979 49 p refs

(NASA-TP-1352; L-12268) Avail: NTIS HC A03/MF A01

CSCL 01A

AERODYNAMIC CHARACTERISTICS, MISSILE CONTROL

N79-17809"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AN EXPERIMENTAL WIND-TUNNEL INVESTIGATION OF A

RAM-AIR-SPOILER ROLL-CONTROL DEVICE ON A

FORWARD-CONTROL MISSILE AT SUPERSONIC SPEEDS

A. B. BLAIR, JR. Dec. 1978 191 p refs

(NASA-TP-1353; L-12518) Avail: NTIS HC A09/MF A01

CSCL 01A

CANARD CONFIGURATIONS, CRUCIFORM WINGS, LATERAL

CONTROL, RAMJET MISSILES, SPOILERS, SUPERSONIC

SPEED, WIND TUNNEL TESTS

02 AERODYNAMICS

N79-17810"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

SPACE SHUTTLE AFTERBODY AERODYNAMICS/PLUME

SIMULATION DATA SUMMARY

K. L. BLACKWELL and L. M. HAIR (REMTECH, Inc., Huntsville,

Ala.) Dec. 1978 195 p refs

(NASA-TP-1384; M-276) Avail: NTIS HC A09/MF A01 CSCL

01A

AERODYNAMIC CHARACTERISTICS, PLUMES, SPACE

SHUTTLES, WIND TUNNEL TESTS

N79-18915"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

APPROXIMATION CONCEPTS FOR NUMERICAL AIRFOIL

OPTIMIZATION

G. N. VANDERPLAATS Mar. 1979 38 p refs

(NASA-TP-1370; A-7682) Avail: NTIS HC A03/MF A01 CSCL

01A

AIRFOIL PROFILES, NUMERICAL ANALYSIS, OPTIMAL

CONTROL

N79-20030"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ADVANCED TECHNOLOGY AIRFOIL RESEARCH, VOLUME 1,

PART I

1979 454 p refs Conf. held at Hampton, Va., 7-9 Mar. 1978

(NASA-CP-2045-PT-1; L-12232-VOL-1-PT-1) Avail: NTIS HC

A20/MF A01 CSCL 01A

AERODYNAMICS, AIRFOILS, COMPUTER PROGRAMS,

CONFERENCES, DESIGN ANALYSIS, TEST FACILITIES, WIND

TUNNEL TESTS

N79-20071"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

DETERMINATION OF STABILITY AND CONTROL

PARAMETERS OF A LIGHT AIRPLANE FROM FLIGHT DATA

USING TWO ESTIMATION METHODS

V. KLEIN Mar. 1979 102 p refs

(NASA-TP-1306; L-12291) Avail: NTIS HC A06/MF A01

CSCL 01A

AERODYNAMIC STABILITY, AIRCRAFT CONTROL, IN-FLIGHT

MONITORING, LIGHT AIRCRAFT, MAXIMUM LIKELIHOOD

ESTIMATES, REGRESSION ANALYSIS

N79-22037"# National Aeronautics and Space Administration,

Langley Research Center, Hampton, Va.

EXPERIMENTAL INVESTIGATION OF THREE HELICOPTER

ROTOR AIRFOILS DESIGNED ANALYTICALLY

G. J. BINGHAM and K. W. NOONAN Apr. 1979 95 p refs

Prepared in cooperation with Army Aviation Res. and Develop.

Command, Hampton, Va.

(DA PRO J. 1 L1-61102-AH-45)

(NASA-TP-1396; L-11703; AVRADCOM-TR-79-11) Avail: NTIS

HCA05/MFA01 CSCL01A

AERODYNAMIC CHARACTERISTICS, AIRFOIL PROFILES,

ROTARY WINGS, ROTOR AERODYNAMICS, WIND TUNNEL

TESTS

N79-22038"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

LOW-SPEED WIND-TUNNEL PARAMETRIC INVESTIGATION OF

FLIGHT SPOILERS AS TRAILING-VORTEX-ALLEVIATION

DEVICES ON A TRANSPORT AIRCRAFT MODEL

D. R. CROOM Washington Apr. 1979 46 p refs

(NASA-TP-1419; L-12622) Avail: NTIS HC A03/MF A01

CSCL 01A

AIRCRAFT MODELS, LOW SPEED WIND TUNNELS,

SPOILERS, TRANSPORT AIRCRAFT, VORTICES, WIND TUNNEL

TESTS

11
02 AERODYNAMICS

N79-22043"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ONSET OF CONDENSATION EFFECTS WITH AN NACA 0012-64

AIRFOIL TESTED IN THE LANGLEY 0.3-METER TRANSONIC

CRYOGENIC TUNNEL

R. M. HALL Apr. 1979 72 p refs

(NASA-TP-1385; L-12581) Avail: NTIS HC A04/MF A01

CSCL 01A

AIRFOILS, CRYOGENIC WIND TUNNELS, NASA PROGRAMS,

TRANSONIC WIND TUNNELS

N79-23012"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

FLIGHT INVESTIGATION OF PILOTING TECHNIQUES AND

CROSSWlND LIMITATIONS USING A RESEARCH TYPE

CROSSWIND LANDING GEAR

B. D. FISHER, P. L. DEAL, R. A. CHAMPINE, and J. M. PATTON,

JR. May 1979 55 p refs

(NASA-TP-1423; L-12682) Avail: NTIS HC A04/MF A01

CSCL 01A

AIRCRAFT LANDING, CROSS FLOW, FLIGHT TESTS,

LANDING GEAR, PILOT PERFORMANCE

N79-23013"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AERODYNAMIC CHARACTERISTICS AT MACH NUMBERS OF

1.5, 1.0, AND 2.0 OF A BLENDED WING-BODY CONFIGURATION

WITH AND WITHOUT INTEGRAL CANARDS

A. W. ROBINS, M. LAMB, and D. S. MILLER May 1979 56 p

refs

(NASA-TP-1427; L-12727) Avail: NTIS HC A04/MF A01

CSCL 01A

AERODYNAMIC CHARACTERISTICS, BODY-WING

CONFIGURATIONS, CANARD CONFIGURATIONS

N79-23912"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

AIRCRAFT ICING

B. J. BLAHA, comp. 1979 147 p refs Workshop held at

Cleveland, 19-21 Jul. 1978

(NASA-CP-2086; FAA-RD-78-109; E-027) Avail: NTIS HC

A07/MF A01 CSCL 01C

AIRCRAFT HAZARDS, CONFERENCES, ICE FORMATION

N79-24961"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

LOW-SPEED WIND-TUNNEL INVESTIGATION OF WING FINS

AS TRAILING-VORTEX-ALLEVIATION DEVICES ON A

TRANSPORT AIRPLANE MODEL

D. R. CROOM and G. T. HOLBROOK Jun. 1979 30 p refs

(NASA-TP-1453; L-12776) Avail: NTIS HC A03/MF A01

CSCL 0tA

FINS, TRAILING EDGES, TRANSPORT AIRCRAFT,

VORTICES, WIND TUNNEL TESTS, WINGS

N79-26020"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECTS OF WING LEADING-EDGE DEFLECTION ON

LOW-SPEED AERODYNAMIC CHARACTERISTICS OF A

LOW-ASPECT-RATIO HIGHLY SWEPT ARROW-WING

CONFIGURATION

P. L. COE, JR. and R.P. WESTON 1979 73 p refs

(NASA-TP-1434; L-12784) Avail: NTIS HC A04/MF A01

CSCL 01A

AERODYNAMIC CHARACTERISTICS, ARROW WINGS,

LEADING EDGES, LOW ASPECT RATIO WINGS, LOW SPEED

STABILITY, WIND TUNNEL TESTS

12

N79-26022"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECT OF SEVERAL GEOMETRIC PARAMETERS ON THE

STATIC INTERNAL PERFORMANCE OF THREE

NONAXlSYMMETRIC NOZZLE CONCEPTS

B. L. BERRIER and R. J. RE Jul. 1979 136 p refs

(NASA-TP-1468; L-12810) Avail: NTIS HC A07/MF A01

CSCL 01A

CONVERGENT-DIVERGENT NOZZLES, GIMBALS, STATIC

TESTS

N79-29146"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AN EXPERIMENTAL AND THEORETICAL INVESTIGATION OF

THE EFFECT OF NONMETRIC OVER-THE-WING NACELLES ON

WING-BODY AERODYNAMICS

D. E. REUBUSH Aug. 1979 79 p refs

(NASA-TP-1503; L-13010) Avail: NTIS HC A05/MF A01

CSCL 01A

AERODYNAMIC CONFIGURATIONS, DRAG, TRANSPORT

AIRCRAFT, WIND TUNNEL TESTS, WING NACELLE

CONFIGURATIONS

N79-33164"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF A

VECTORED-ENGINE-OVER-WING CONFIGURATION AT

SUBSONIC SPEEDS

L. D LEAVITT Oct. 1979 136p refs

(NASA-TP-1533; L-13108) Avail: NTIS HC A07/MF A01

CSCL 01A

AERODYNAMIC CHARACTERISTICS, SUBSONIC SPEED,

UPPER SURFACE BLOWN FLAPS, WIND TUNNEL TESTS, WING

NACELLE CONFIGURATIONS

N80-10101"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECT OF WINGLETS ON A FIRST-GENERATION JET

TRANSPORT WING. 6: STABILITY CHARACTERISTICS FOR

A FULL-SPAN MODEL AT SUBSONIC SPEEDS

S. G. FLECHNER Oct. 1979 69 p refs

(NASA-TP-1330; L-12514) Avail: NTIS HC A04/MF A01

CSCL 01A

AIRCRAFT MODELS, DRAG REDUCTION, SUBSONIC SPEED,

TRANSPORT AIRCRAFT, WIND TUNNEL STABILITY TESTS,

WINGLETS, WINGS

N80-10102"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

WIND-TUNNEL INVESTIGATION OF THE VALIDITY OF A

SONIC-BOOM-MINIMIZATION CONCEPT

R.J. MACK andC. M. DARDEN Oct. 1979 47p refs

(NASA-TP-1421; L-12661) Avail: NTIS HC A03/MF A01

CSCL 01A

AIRCRAFT DESIGN, OPTIMIZATION, OVERPRESSURE,

SONIC BOOMS, SUPERSONIC TRANSPORTS, WIND TUNNEL

TESTS

N80-10105"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ESTIMATION OF ATTAINABLE LEADING-EDGE THRUST FOR

WINGS AT SUBSONIC AND SUPERSONIC SPEEDS

H. W. CARLSON, R. J. MACK, and R. L. BARGER 1979 62 p

refs

(NASA-TP-1500; L-13032) Avail: NTIS HC A04/MF A0t

CSCL 01A

ESTIMATES, LEADING EDGES, PREDICTION ANALYSIS

TECHNIQUES, SUBSONIC SPEED, SUPERSONIC SPEED,

THRUST, WINGS
N80-10107"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

WORKSHOP ON THRUST AUGMENTING EJECTORS

A, E, LOPEZ, ed., D. G. KOENIG, ed,, D. S. GREEN, ed, (Naval

Air Development Center, Warminster, Penn,), and K. S, NAGARAJA,

ed. (Air Force Flight Dynamics Lab) Sap. 1979 509 p Conf.

held at Moffett Field, Calif,, 28-29 Jun. 1978; Sponsored by NADC

and AFFDL

(NASA-CP-2093; A-7887) Avail: NTiS HC A22/MF A01 CSCL

01A

CONFERENCES, EJECTORS, NOZZLE FLOW, POWERED

LIFT AIRCRAFT, THRUST AUGMENTATION

N80-11035"# National Aeronautics and Space Administration.

Dryden (Hugh L.) Flight Research Center, Edwards, Calif.

FLIGHT-MEASURED AFTERBODY PRESSURE COEFFICIENTS

FROM AN AIRPLANE HAVING TWIN SIDE-BY-SIDE JET

ENGINES FOR MACH NUMBERS FROM 0.6 TO 1.6

L. L. STEERS Washington Nov. 1979 88 p refs

(NASA-TP-1549; H-1066) Avail: NTIS HC A05/MF A01 CSCL

01A

AFTERBODIES, IN-FLIGHT MONITORING, JET EXHAUST,

MACH NUMBER

N80-11036"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

FUSELAGE AND NOZZLE PRESSURE DISTRIBUTIONS ON A

1/12-SCALE F-15 PROPULSION MODEL AT TRANSONIC

SPEEDS

O. C, PENDERGRAFT, JR. Nov. 1979 140 p refs

(NASA-TP-1521; L-12948) Avail: NTiS HC A07/MF A01

CSCL 01A

AIRCRAFT MODELS, EXHAUST NOZZLES, FUSELAGES,

NOZZLE FLOW, PRESSURE DISTRIBUTION

N80-12064"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AERODYNAMIC CHARACTERISTICS OF A HYPERSONIC

RESEARCH AIRPLANE CONCEPT HAVING A 70 DEG SWEPT

DOUBLE-DELTA WING AT MACH NUMBERS FROM 0.80 TO

1.20, WITH SUMMARY OF DATA FROM 0.20 TO 6.0

J. A. PENLAND, J. B. HALLISSY, and J. L. DILLON Washington

Dec. 1979 147 p refs

(NASA-TP-1552; L-13158) Avail: NTIS HC A07/MF A01

CSCL 01A

AERODYNAMIC CHARACTERISTICS, COMPUTATIONAL

FLUID DYNAMICS, DELTA W_NGS, HYPERSONIC AIRCRAFT,

WIND TUNNEL TESTS

N80-12065"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

APPLICATION OF SUPERSONIC LINEAR THEORY AND

HYPERSONIC IMPACT METHODS TO THREE NONSLENDER

HYPERSONIC AIRPLANE CONCEPTS AT MACH NUMBERS

FROM 1.10 TO 2.86

J. L. PITTMAN Washington Dec. 1979 59 p refs

(NASA-TP-1539; L-13142) Avail: NTIS HC A04/MF A01

CSCL 10A

AERODYNAMIC CHARACTERISTICS, HYPERSONICS, MACH

NUMBER, SUPERSONIC AIRCRAFT, SUPERSONICS

N80-12994"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SUMMARY OF LOW-SPEED LONGITUDINAL AERODYNAMICS

OF TWO POWERED CLOSE-COUPLED WING-CANARD

FIGHTER CONFIGURATIONS

J. W. PAULSON, JR. and J. L. THOMAS Washington Dec.

1979 92 p refs

(NASA-TP-1535; L-13157) Avail: NTIS HC A05/MF A01

CSCL 01A

AERODYNAMIC CHARACTERISTICS, CANARD CONFIGURATIONS, FIGHTER AIRCRAFT, LOW SPEED STABILITY

02 AERODYNAMICS

N80-12995"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

INCLUSION OF UNSTEADY AERODYNAMICS IN

LONGITUDINAL PARAMETER ESTIMATION FROM FLIGHT

DATA

M. J. QUEIJO, W. R. WELLS (Wright State Univ., Dayton, Ohio),

and D. A. KESKAR Washington Dec. 1979 52 p refs

(NASA-TP-1536; L-13009) Avail: NTIS HC A04/MF A01

CSCL 01A

AERODYNAMICS, FLIGHT CHARACTERISTICS, MATHEMATICAL MODELS, PARAMETER_ZATION, VORTICES

N80-13001"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

INVESTIGATION OF FLOW CHARACTERISTICS OVER MISSILE

BODIES AT SUPERSONIC SPEEDS

R. L. BARGER and W. C. SAWYER Dec. 1979 41 p refs

(NASA-TP-1579; L-13224) Avail: NTIS HC A03/MF A01

CSCL 01A

BOUNDARY LAYER SEPARATION, FLOW DISTRIBUTION,

MISSILE BODIES, SEPARATED FLOW, SUPERSONIC SPEED

N80-13002"# National Aeronautics and Space Administration.

Dryden (Hugh L.) Flight Research Center, Edwards, Calif.

EFFECTS OF FUSELAGE FOREBODY GEOMETRY ON

LOW-SPEED LATERAL-DIRECTIONAL CHARACTERISTICS OF

TWIN-TAIL FIGHTER MODEL AT HIGH ANGLES OF ATTACK

P. C. CARR and W. P. GILBERT Dec. 1979 73 p refs

(NASA-TP-1592; L-13270) Avail: NTIS HC A04/MF A01

CSCL 01A

AERODYNAMIC CHARACTERISTICS, AIRCRAFT DESIGN,

ANGLE OF ATTACK, FIGHTER AIRCRAFT, FOREBODIES, LOW

SPEED WIND TUNNELS

N80-14045"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SONIC-BOOM WAVE-FRONT SHAPES AND CURVATURES

ASSOCIATED WITH MANEUVERING FLIGHT

R. L. BARGER Dec. 1979 30 p refs

(NASA-TP-1611; L-13339) Avail: NTIS HC A03/MF A01

CSCL 01A

AIRCRAFT MANEUVERS, CURVATURE, SHOCK WAVE

INTERACTION, SONIC BOOMS. WAVE FRONTS

N80-15033"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

CLASSICAL AERODYNAMIC THEORY

R. T. JONES, comp. Dec. 1979 308 p refs

(NASA-RP-1050; A-7556) Avail: NTIS HC A14/MF A01 CSCL

01A

A collection of papers on modern theoretical aerodynamics is

presented. Included are theories of incompressible potential flow

and research on the aerodynamic forces on win 9 and wing sections

of aircraft and on airship hulls. For individual titles, see N80-15034

through N80-15047.

N80-16032"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

WIND-TUNNEL/FLIGHT CORRELATION STUDY OF

AERODYNAMIC CHARACTERISTICS OF A LARGE FLEXIBLE

SUPERSONIC CRUISE AIRPLANE (XB-701) 2:

EXTRAPOLATION OF WIND-TUNNEL DATA TO FULL-SCALE

CONDITIONS

J. B. PETERSON, JR., M. J. MANN, R. B. SORRELLS, III, W. C.

SAWYER, and D. E. FULLER Feb. 1980 80 p refs

(NASA-TP-1515; L-12688) Avail: NTIS HC A05/MF A01

CSCL 01A

AERODYNAMIC CHARACTERISTICS, B-70 AIRCRAFT,

FLIGHT TESTS, WIND TUNNEL TESTS

13
02 AERODYNAMICS

N80-17030"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

PREDICTION METHOD FOR TWO-DIMENSIONAL

AERODYNAMIC LOSSES OF COOLED VANES USING

INTEGRAL BOUNDARY-LAYER PARAMETERS

L. J. GOLDMAN and R. E. AUGLER Feb. 1980 43 p refs

(NASA-TP-t623; E-076) Avail NTIS HC A03/MF A01 CSCL

01A

AERODYNAMIC CHARACTERISTICS, BOUNDARY LAYERS,

HEAT TRANSFER, PREDICTION ANALYSIS TECHNIQUES,

TURBINE BLADES, TWO DIMENSIONAL FLOW

N80-17984"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

AN EXPERIMENTAL INVESTIGATION OF TWO LARGE

ANNULAR DIFFUSERS WITH SWIRLING AND DISTORTED

INFLOW

W. T. ECKERT, J. P. JOHNSTON (Stanford Univ., Calif.), T. D.

SIMONS (Stanford Univ., Calif.), K. W. MORT, and V. R. PAGE

Feb. 1980 106p refs

(NASA-TP-1628; AVRADCOM-TR-79-40; A-7436) Avail: NTIS

HC A06/MF A01 CSCL 01A

AERODYNAMIC CHARACTERISTICS, EXHAUST DIFFUSERS,

FLOW DISTORTION, SWIRLING

N80-17986"# National Aeronautics and Space Administration.

Dryden (Hugh L.) Flight Research Center, Edwards, Calif.

WIND-TUNNEL/FLIGHT CORRELATION STUDY OF

AERODYNAMIC CHARACTERISTICS OF A LARGE FLEXIBLE

SUPERSONIC CRUISE AIRPLANE (XB-70-1). 3: A

COMPARISON BETWEEN CHARACTERISTICS PREDICTED

FROM WIND-TUNNEL MEASUREMENTS AND THOSE

MEASURED IN FLIGHT

H. H. ARNAIZ, J. B. PETERSON, JR. (NASA. Langley Research

Center), and J. C. DAUGHERTY (NASA. Ames Research Center)

Mar. 1980 59 p refs

(NASA-TP-1516; H-1079) Avail: NTIS HC A04/MF A01 CSCL

01A

AERODYNAMIC CHARACTERISTICS, B-70 AIRCRAFT, DATA

CORRELATION, FLIGHT TESTS, WIND TUNNEL TESTS

N80-19031"# National Aeronautics and Space Administration,

Washington, D.C.

APPLICATION OF A NUMERICALLY GENERATED

ORTHOGONAL COORDINATE SYSTEM TO THE SOLUTION OF

INVlSCID AXISYMMETRIC SUPERSONIC FLOW OVER BLUNT

BODIES

H. H. HAMILTON, II and R. A. GRAVES, JR. Mar. 1980 61 p

(NASA-TP-1619; L-13353) Avail: NTIS HC A04/MF A01

CSCL 01A

BLUNT BODIES, COORDINATES, INVlSCID FLOW,

ORTHOGONALITY, SUPERSONIC FLOW

N80-21279*# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SUPERSONIC WINGS WITH SIGNIFICANT LEADING-EDGE

THRUST AT CRUISE

A. W. ROBINS, H. W. CARLSON, and R. J. MACK Apr. 1980

28 p refs

(NASA-TP-1632; L-13316) Avail: NTIS HCAO3/MF A01 CSCL

01A

AERODYNAMIC CHARACTERISTICS, LEADING EDGE

SWEEP, SUPERSONIC AIRFOILS, THRUST, WING PLANFORMS

14

N80-21280"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

COMPARISON OF PREDICTED AND EXPERIMENTAL

REAL-GAS PRESSURE DISTRIBUTIONS ON SPACE SHUTTLE

ORBITER NOSE FOR SHUTTLE ENTRY AIR OATA SYSTEM

J. L. SHINN Apr. 1980 29 p refs

(NASA-TP-1627; L-13341) Avail: NTIS HC A03/MF A01

CSCL 01A

AIR DATA SYSTEMS, NOSE TIPS, REENTRY EFFECTS,

SPACE SHUTTLE ORBITERS, SPACE TRANSPORTATION

SYSTEM

N80-21283"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ADVANCED TECHNOLOGY AIRFOIL RESEARCH, VOLUME 2

1979 262 p refs Presented at conf., Langley Research

Center, Hampton, Va. 7-9 Mar. 1978

(NASA-CP-2046; L-12232) Avail: NTIS HC A12/MF A0t

CSCL 01A

AIRFOILS, CONFERENCES, TECHNOLOGY ASSESSMENT,

TECHNOLOGY UTILIZATION

N80-22261"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

VISCOUS-INVISClD CALCULATIONS OF JET ENTRAINMENT

EFFECTS ON THE SUBSONIC FLOW OVER NOZZLE

AFTERBODIES

R. G. WILMOTH Apr. 1980 79 p refs

(NASA-TP-1626; L-13362) Avail: NTIS HC A05/MF A01

CSCL 01A

AFTERBODIES, COMPUTER PROGRAMS, ENTRAINMENT,

INVISCID FLOW, JET EXHAUST, SUBSONIC FLOW, VISCOUS

FLOW

N80-22262"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

INVESTIGATION OF THE FLOW FIELD SURROUNDING

CIRCULAR-ARC BOATTAIL NOZZLES AT SUBSONIC SPEEDS

W. K. ABEYOUNIS and L. E. PUTNAM May 1980 51 p refs

(NASA-TP-1633; L-13318) Avail: NTIS HC A04/MF A01

CSCL 01A

BOATTAILS, FLOW DISTRIBUTION, JET EXHAUST, NOZZLE

DESIGN, SUBSONIC SPEED

N80-22265"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

THEORETICAL PREDICTION OF NONLINEAR PROPAGATION

EFFECTS ON NOISE SIGNATURES GENERATED BY SUBSONIC

OR SUPERSONIC PROPELLER OR ROTOR-BLADE TIPS

R. L. BARGER May 1980 18 p refs

(NASA-TP-1660; L-13388) Avail: NTIS HC A02/MF A01

CSCL 01A

AIRCRAFT NOISE, NOISE PROPAGATION, NONLINEAR

EQUATIONS, PROPAGATION MODES, SOUND GENERATORS

N80-22266"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

FULL-SCALE WIND TUNNEL-INVESTIGATION OF THE

ADVANCED TECHNOLOGY LIGHT TWIN-ENGINE AIRPLANE

(ATLIT)

J. L. HASSELL, JR., W. A. NEWSOM, JR., and L. P. YIP May

1980 212 p refs

(NASA-TP-t591; L-13135) Avail: NTIS HC A10/MF A01

CSCL 01A

AERODYNAMIC STABILITY, AIRCRAFT CONTROL,

AIRCRAFT PERFORMANCE, ATLtT PROJECT, FULL SCALE

TESTS, WIND TUNNEL TESTS
N80-24261"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

THEORY FOR COMPUTING THE SIZE AND SHAPE OF A

REGION OF INFLUENCE ASSOCIATED WITH A MANEUVERING

VEHICLE

R. L. BARGER May 1980 22p refs

(NASA-TP-1648; L-13419) Avail: NTIS HC A02/MF A01

CSCL 01A

AIRCRAFT MANEUVERS, AIRCRAFT PERFORMANCE,

MANEUVERABILITY, TRAJECTORY ANALYSIS

N80-24267"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

INVESTIGATION OF AXISYMMETRIC AND NONAXISYMMETRIC

NOZZLES INSTALLED ON A 0.10 SCALE F-18 PROTOTYPE

AIRPLANE MODEL

F. J. CAPONE and B. L. BERRIER Jun. 1980 304 p refs

(NASA-TP-1638; L-13401) Avail: NTIS HC A14/MF A01

CSCL 01A

AERODYNAMIC CHARACTERISTICS, F-18 AIRCRAFT,

NOZZLE FLOW, NOZZLE GEOMETRY, THRUST, WIND TUNNEL

TESTS

N80-25296"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

DEVELOPMENT AND VALIDATION OF A COMBINED ROTOR

FUSELAGE INDUCED FLOW FIELD COMPUTATIONAL

METHOD

C.E. FREEMAN Jun. 1980 61 p refs Prepared incooperation

with Army Aviation Research and Development Command, St.

Louis, Mo.

(NASA-TP-1656; AVRADCOM-TR-80-B-3; L-13363) Avail: NTIS

HC A04/MF A01 CSCL 01A

COMPUTATIONAL FLUID DYNAMICS, DOWNWASH,

HELICOPTER WAKES, PANEL METHOD (FLUID DYNAMICS),

ROTOR AERODYNAMICS, WIND TUNNEL TESTS

N80-27283"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECT OF REYNOLDS NUMBER ON STABILITY

CHARACTERISTICS OF A CRUCIFORM WING-BODY

R. L. STALLINGS, JR., M. LAMB, and C. B. WATSON Jul. 1980

111 p refs

(NASA-TP-t683; L-13530) Avail: NTIS HC A06/MF A01

CSCL 01A

CRUCIFORM WINGS, REYNOLDS NUMBER, SUPERSONIC

FLOW, SUPERSONIC WIND TUNNELS, WIND TUNNEL

STABILITY TESTS

N80-27284"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

CAS2D: FORTRAN PROGRAM FOR NONROTATING

BLADE-TO-BLADE, STEADY, POTENTIAL TRANSONIC

CASCADE FLOWS

D. S. DULIKRAVICH Jul. 1980 36 p refs

(NASA-TP-1705; E-253) Avail: NTIS HC A03/MF A01 CSCL

01A

CASCADE FLOW, COMPUTER PROGRAMS, MATHEMATICAL

MODELS, TRANSONIC FLOW, TURBOMACHINE BLADES

N80-28304"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

WATER-TUNNEL AND ANALYTICAL INVESTIGATION OF THE

EFFECT OF STRAKE DESIGN VARIABLES ON STRAKE

VORTEX BREAKDOWN CHARACTERISTICS

N. T. FRINK and J. E. LAMAR Aug. 1980 92 p refs

(NASA-TP-1676; L-13254) Avail: NTIS HC A05/MF A01

CSCL 01A

CONTROL SURFACES, HYDRAULIC TEST TUNNELS, NOSE

FINS, SCALE MODELS, VORTICES

02 AERODYNAMICS

N80-29250"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

THE EFFECT OF THROAT CONTOURING ON

TWO-DIMENSIONAL CONVERGING-DIVERGING NOZZLES AT

STATIC CONDITIONS

M. L. MASON, L. E. PUTNAM, and R. J. RE Aug. 1980 70 p

refs

(NASA-TP-1704; L-13591) Avail: NTIS HC A04/MF A01

CSCL 01A

CONVERGENT-DIVERGENT NOZZLES, NOZZLE EFFICIENCY, STATIC TESTS, THROATS

N80-32333"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AERODYNAMIC CHARACTERISTICS OF THREE HELICOPTER

ROTOR AIRFOIL SECTIONS AT REYNOLDS NUMBER FROM

MODEL SCALE TO FULL SCALE AT MACH NUMBERS FROM

0.35 TO 0,90

K. W. NOONAN and G. J. BINGHAM Sep. 1980 85 p refs

Prepared in cooperation with Army Aviation Research and

Development Command, St. Louis, Mo.

(DA PROJ. 1L1-61102-AH-45)

(NASA-TP-1701; L-13139; AVRADCOM-TR-80-B-5) Avail: NTIS

HC A05/MF A01 CSCL01A

AERODYNAMIC CHARACTERISTICS, AIRFOILS, HELICOPTERS, REYNOLDS NUMBER, WIND TUNNEL TESTS

N80-32334"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

A NEW THEORY FOR RAPID CALCULATION OF THE GROUND

PATTERN OF THE INCIDENT SOUND INTENSITY PRODUCED

BY A MANEUVERING JET AIRPLANE

R. L. BARGER Washington Sep. 1980 24 p refs

(NASA-TPo1733; L-13629) Avail: NTIS HC A02/MF A01

CSCL 01A

AIRPORT PLANNING, JET AIRCRAFT NOISE, NOISE

MEASUREMENT, NOISE POLLUTION

N80-33356"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

CALCULATION OF THREE-DIMENSIONAL UNSTEADY

TRANSONIC FLOWS PAST HELICOPTER BLADES

J. J. CHATTOT Oct. 1980 32 p refs Prepared in cooperation

with Army Aviation Research and Development Command, Moffett

Field, Calif.

(NASA-TP-1721; A-8024) Avail: NTIS HC A03/MF A01 CSCL

01A

FINITE DIFFERENCE THEORY, HELICOPTER DESIGN,

NUMERICAL ANALYSIS, ROTOR AERODYNAMICS, TRANSONIC

FLOW

N80-33357"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

WIND: COMPUTER PROGRAM FOR CALCULATION OF THREE

DIMENSIONAL POTENTIAL COMPRESSIBLE FLOW ABOUT

WIND TURBINE ROTOR BLADES

D. S. DULIKRAVICH Oct. 1980 20 p refs

(NASA-TP-1729; E-474) Avail: NTIS HC A02/MF A01 CSCL

01A

COMPRESSIBLE FLOW, COMPUTER PROGRAMS,

NUMERICAL FLOW VISUALIZATION, THREE DIMENSIONAL

FLOW, TURBINE BLADES, WINDMILLS (WINDPOWERED

MACHINES)

N81-10004"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ESTIMATION OF WING NONLINEAR AERODYNAMIC

CHARACTERISTICS AT SUPERSONIC SPEEDS

H. W. CARLSON and R. J. MACK Nov. 1980 84 p refs

(NASA-TP-1718; L-13589) Avail: NTIS HC A05/MF A01

CSCL 01A

AERODYNAMIC CHARACTERISTICS, COMPUTER

15
02 AERODYNAMICS

PROGRAMS, NONLINEARITY, SUPERSONIC SPEED, WING

LOADING

N81-I0005"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

A FAN PRESSURE RATIO CORRELATION IN TERMS OF MACH

NUMBER AND REYNOLDS NUMBER FOR THE LANGLEY 0.3

METER TRANSONIC CRYOGENIC TUNNEL

P. L. I.AWING, J. B ADCOCK, and C. L. LADSON Nov. _1980

21 p refs

(NASA-TP-1752; L-13713) Avail: NTIS HC A02/MF A01

CSCL 0tA

CRYOGENIC WIND TUNNELS, MACH NUMBER, REYNOLDS

NUMBER, SCALING LAWS, TRANSONIC WIND TUNNELS, WIND

TUNNEL CALIBRATION

N81-12015"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

LOW-SPEED AERODYNAMIC CHARACTERISTICS OF A 13

PERCENT THICK MEDIUM SPEED AIRFOIL DESIGNED FOR

GENERAL AVIATION APPLICATIONS

R. J. MCGHEE and W. D. BEASLEY Aug. 1979 79 p refs

(NASA-TP-1498; L-12976) Avail: NTIS HC A04/MF A01

CSCL 01A

AIRCRAFT DESIGN, ANGLE OF ATTACK, GENERAL

AVIATION AIRCRAFT, WIND TUNNEL TESTS

N81-12021"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EXPERIMENTAL AND THEORETICAL AERODYNAMIC

CHARACTERISTICS OF TWO HYPERSONIC CRUISE AIRCRAFT

CONCEPTS AT MACH NUMBERS OF 2.96, 3.96, AND 4.63

J. L. PITTMAN and G. D. RIEBE Dec. 1980 116 p refs

(NASA-TP-1767; L-13868) Avail: NTIS HC A06/MF A01

CSCL OtA

ANGLE OF ATTACK, LIFT, NACELLES, SUPERSONIC

AIRCRAFT, SUPERSONIC DRAG

N81-13919"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

NUMERICAL SOLUTIONS OF THE NAVlER-STOKES

EQUATIONS FOR TRANSONIC AFFERBODY FLOWS

R. C. SWANSON, JR. Dec. 1980 60 p refs

(NASA-TP-1784; L-13826) Avail: NTIS HC A04/MF A01

CSCL 01A

BOATTAILS, FINITE DIFFERENCE THEORY, NAVtER-STOKES

EQUATION, PLUMES, TRANSONIC FLOW

N81-14972"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

INVESTIGATION OF CONVERGENT-DIVERGENT NOZZLES

APPLICABLE TO REDUCED-POWER SUPERSONIC CRUISE

AIRCRAFT

B. L. BERRIER and R J. RE Dec. 1980 218 p refs

(NASA-TP-1766; L-13974) Avail: NTIS HC A10/MF A0f

CSCL 01A

CONVERGENT-DIVERGENT NOZZLES, NOZZLE DESIGN,

PERFORMANCE TESTS

N81-14973"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

BIBLIOGRAPHY OF SUPERSONIC CRUISE RESEARCH (SCR)

PROGRAM FROM 1977 TO MID-1980

S. HOFFMAN Dec. 1980 106p

(NASA-RP-t063; L-13764) Avail: NTIS HC A06/MF A01

CSCL 01A

The supersonic cruise research (SCR) program, initiated in July

1972, includes system studies and the following disciplines:

propulsion, stratospheric emission impact, structures and materials,

aerodynamic performance, and stabiJity and control. In a

coordinated effort to provide a sound basis for any future

consideration that may be given by the United States to the

development of an acceptable commercial supersonic transport,

integration of the technical disciplines was undertaken, analytical

16

tools were developed, and wind tunnel, flight, and laboratory

investigations were conducted. The present bibliography covers

the time period from 1977 to mid-1980. It is arranged according

to system studies and the above five SCR disciplines. There are

306 NASA reports and 135 articles, meeting papers, and company

reports cited. E.D.K.

N81-14974"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

LEADING-EDGE DEFLECTION OPTIMIZATION FOR A HIGHLY

SWEPT ARROW WING CONFIGURATION

P. L. COL, JR., J. K. HUFFMAN, and J. W. FENBERT Dec.

1980 59p refs

(NASA-TP.1777; L-13820) Avail: NTIS HC A04/MF A01

CSCL 01A

AERODYNAMIC CONFIGURATIONS, ARROW WINGS,

DEFLECTION, LATERAL STABILITY, LEADING EDGES

N81-14975"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

WIND-TUNNEL MEASUREMENTS AND COMPARISON WITH

FLIGHT OF THE BOUNDARY LAYER AND HEAT TRANSFER

ON A HOLLOW CYLINDER AT MACH 3

R. L. STALLINGS, JR. and M. LAMB Dec. 1980 48 p refs

(NASA-TP-1789; L-14044) Avail: NTIS HC A03/MF A01

CSCL 01A

BOUNDARY LAYER FLOW, CYLINDRICAL SHELLS, DRAG

MEASUREMENT, HEAT TRANSFER, REYNOLDS NUMBER, SKIN

FRICTION, SUPERSONIC BOUNDARY LAYERS, WIND TUNNEL

TESTS

N81-15976"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECTS OF SIDEWALL GEOMETRY ON THE INSTALLED

PERFORMANCE OF NONAXlSYMMETRIC CONVERGENT-DIVERGENT EXHAUST NOZZLES

J. A. YETTER (George Washington Univ., Hampton, Va.) and L.

D. LEAVITT Dec. 1980 119p refs

(NASA-TP-1771; L-13826) Avail: NTIS HC A06/MF A01

CSCL 01A

CONVERGENT-DIVERGENT NOZZLES, EXHAUST FLOW

SIMULATION, EXHAUST NOZZLES, JET EXHAUST, NOZZLE

DESIGN, NOZZLE GEOMETRY, NOZZLE WALLS

N81-16977"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

STEADY AND NONSTEADY SUPERSONIC TURBULENT

AFTERBODY FLOW

K. K. YOSHIKAWA and A. A. WRAY Feb. 1981 23 p refs

(NASA-TP-1769; A-8271) Avail: NTIS HC A02/MF A01 CSCL

01A

AXlSYMMETRIC FLOW, FLOW DISTRIBUTION, NUMERICAL

FLOW VISUALIZATION, STEADY FLOW, SUPERSONIC FLOW,

TURBULENT FLOW, UNSTEADY FLOW

N81-19019"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AEROPROPULSlVE CHARACTERISTICS OF TWIN

NONAXlSYMMETRIC VECTORING NOZZLES INSTALLED WITH

FORWARD-SWEPT AND AFT-SWEPT WINGS

F. J. CAPONE Mar. 1981 260 p

(NASA-TP-1778; L-13902) Avail: NTIS HC A12/MF A01

CSCL 01A

AERODYNAMIC CHARACTERISTICS, CONVERGENT-DIVERGENT NOZZLES, SWEPT FORWARD WINGS, SWEPTBACK

WINGS, WIND TUNNEL TESTS
N81-20026"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

A COMPUTER TECHNIQUE FOR DETAILED ANALYSIS OF

MISSION RADIUS AND MANEUVERABILITY CHARACTERISTICS

OF FIGHTER AIRCRAFT

W. E. FOSS, JR. Mar. 1981 67 p

(NASA-TP-1837; L-14213) Avail: NTIS HC A04/MF A01

CSCL 01A

AERODYNAMICS, AIRCRAFT MANEUVERS, COMPUTER

TECHNIQUES, MANEUVERABILITY, MISSION PLANNING

N81-21016"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

CHARTS FOR DETERMINING POTENTIAL MINIMUM

SONIC-BOOM OVERPRESSURES FOR SUPERSONIC CRUISE

AIRCRAFT

C. M. DARDEN Mar. 1981 49 p refs

(NASA-TP-1820; L-14190) Avail: NTIS HC A03/MF A01

CSCL 01A

ACOUSTIC VELOCITY, GRAPHS (CHARTS), OVERPRESSURE, SONIC BOOMS, SUPERSONIC CRUISE AIRCRAFT RESEARCH

N81-22016"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

PRESSURE AND FORCE DATA FOR A FLAT WING AND A

WARPED CONICAL WING HAVING A SHOCKLESB

RECOMPRESSlON AT MACH 1.62

D. S. MILLER, E. J. LANDRUM, J. C. TOWNSEND, and W. H.

MASON, (Grumman Aerospace Corp., Bethpage, N.Y.) Apr.

1981 333 p refs

(NASA-TP-1759; L-13856) Avail: NTIS HC A15/MF A01

CSCL 10A

CAMBERED WINGS, COMPUTER AIDED DESIGN, CONICAL

FLOW, CROSS FLOW, SUPERCRITICAL FLOW

N61-22017"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

IMPROVED METHOD FOR CALCULATING TRANSONIC

VELOCITIES ON BLADE-TO-BLADE STREAM SURFACES OF

A TURBOMACHINE

J. R. WOOD Apr. 1981 28 p refs

(NASA-TP-1772; E-128) Avail: NTIS HC A03/MF A01 CSCL

01A

AXIAL FLOW TURBINES, TRANSONIC SPEED,

TURBOMACHINE BLADES, VELOCITY DISTRIBUTION

N61-22018"# National Aeronautics and Space Administration_

Ames Research Center, Moffett Field, Calif.

NUMERICAL SIMULATION OF STEADY SUPERSONIC FLOW

L. B. SCHIFF and J. L. STEGER May 1981 42 p refs

(NASA-TP-1749; A-7923) Avail: NTIS HC A03/MF A01 CSCL

01A

FINITE DIFFERENCE THEORY, NAVIER-STOKES EQUATION,

SPATIAL MARCHING, STEADY FLOW, SUPERSONIC FLOW,

VISCOUS FLOW

N81-22019"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SOLUTION OF COMPLEX NONLINEAR PROBLEMS BY A

GENERALIZED APPLICATION OF THE METHOD OF BASE AND

COMPARISON SOLUTIONS WITH APPLICATIONS TO

AERODYNAMICS PROBLEMS

R. L. BARGER May 1981 29 p refs

(NASA-TP-1857; L-14197) Avail: NTIS HC A03/MF A01

CSCL 01A

AERODYNAMIC CONFIGURATIONS, APPROXIMATION,

COMPUTATIONAL FLUID DYNAMICS, NONLINEAR SYSTEMS

02 AERODYNAMICS

N81-24022"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

DESIGN AND EXPERIMENTAL RESULTS FOR A

NATURAL-LAMINAR-FLOW AIRFOIL FOR GENERAL AVIATION

APPLICATIONS

D. M. SOMERS Jun. 1981 104 p refs

(NASA-TP-1861; L-14117) Avail: NTIS HC A06/MF A01

CSCL 01A

DRAG, LAMINAR FLOW AIRFOILS, LEADING EDGES, LIFT

N81-25040"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EXPERIMENTAL AND ANALYTICAL STUDY OF THE

LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF

ANALYTICALLY AND EMPIRICALLY DESIGNED STRAKE-WlNG

CONFIGURATIONS AT SUBCRITICAL SPEEDS

J. E. LAMAR and N. T. FRINK Jun, 1981 226 p refs

(NASA-TP-1803; L-14041) Avail: NTIS HC A11/MF A01

CSCL 01A

AERODYNAMIC CHARACTERISTICS, NOSE FINS,

SUBCRITICAL FLOW, TRAPEZOIDAL WINGS

N81-26078"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

A PROCEDURE FOR DESIGNING FOREBODIES WITH

CONSTRAINTS ON CROSS-SECTION SHAPE AND AXIAL AREA

DISTRIBUTION

R. L. BARGER Jul. 1981 14 p refs

(NASA-TP-1881; L-14516) Avail: NTIS HC A02/MF A01

CSCL 01A

AIRCRAFT DESIGN, FOREBODIES, PRESSURE

DISTRIBUTION, SHAPES, STREAMLINED BODIES

N81-29095"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EXPERIMENTAL AND THEORETICAL SUPERSONIC

LATERAL-DIRECTIONAL STABILITY CHARACTERISTICS OF A

SIMPLIFIED WING-BODY CONFIGURATION WITH A SERIES OF

VERTICAL-TAIL ARRANGEMENTS

M. LAMB, W. C. SAWYER, and J. L, THOMAS Aug. 1981 47

p refs

(NASA-TP-1878; L-14328) Avail: NTIS HC A03/MF A01

CSCL 01A

AERODYNAMIC STABILITY, BODY.WING AND TAIL

CONFIGURATIONS, DIRECTIONAL STABILITY, LATERAL

STABILITY, TAIL ASSEMBLIES

N81-29096"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

A THEORY FOR PREDICTING BOUNDARY IMPEDANCE AND

RESONANCE FREQUENCIES OF SLOTTED-WALL WIND

TUNNELS, INCLUDING PLENUM EFFECTS

R. L. BARGER Jul. 1981 22 p refs

(NASA-TP-1880; L-14480) Avail: NTIS HC A02/MF A01

CSCL 01A

ACOUSTIC IMPEDANCE, PLENUM CHAMBERS, RESONANT

FREQUENCIES, SLOTTED WIND TUNNELS, WIND TUNNEL

WALLS

N81-29098"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AERODYNAMIC TESTS AND ANALYSIS OF A

TURBOJET-BOOSTED LAUNCH VEHICLE CONCEPT

(SPACEJET) OVER A MACH NUMBER RANGE OF 1.50 TO

2.86

G D. RIEBE, W. J. SMALL, and O. A. MORRIS Jul. 1981 55

p refs

(NASA-TP-1888; L-14509) Avail: NTIS HC A04/MF A01

AERODYNAMIC CHARACTERISTICS, SPACE SHUTTLE

BOOSTERS, SPACE TRANSPORTATION SYSTEM, TURBOJET

ENGINES, WIND TUNNEL TESTS

17
02 AERODYNAMICS

N81-30086"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECT OF SIMULATED IN-FLIGHT THRUST REVERSING ON

VERTICAL-TAIL LOADS OF F-18 AND F-15 AIRPLANE

MODELS

E. A. BARE, B L. BERRIER, and F. J. CAPONE Aug. 1981 53

p refs

(NASA-TP-1890; L-14531) Avail: NTIS HC A04/MF A01

CSCL 01A

AERODYNAMIC CONFIGURATIONS, F-15 AIRCRAFT, F-18

AIRCRAFT, THRUST LOADS, THRUST REVERSAL

N81-30087"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

WING-ALONE AERODYNAMIC CHARACTERISTICS FOR HIGH

ANGLES OF ATTACK OF SUPERSONIC SPEEDS

R L. STALLINGS, JR. and M. LAMB Jul. 1981 190 p refs

(NASA-TP-1889; L-14546) Avail: NTIS HC A09/MF A01

CSCL 0tA

AERODYNAMIC CHARACTERISTICS, ANGLE OF ATTACK,

SUPERSONIC SPEED, WINGS

N81-30088'# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

COMPUTER ANALYSIS OF FLOW PERTURBATIONS

GENERATED BY PLACEMENT OF CHOKE BUMPS IN A WIND

TUNNEL

R. L. CAMPBELL Aug. 1981 44 p refs

(NASA-TP-1892; L-14415) Avail: NTIS HC A03/MF A01

CSCL 01A

CHOKES (RESTRICTIONS), COMPUTER PROGRAMS, FLOW

DISTORTION, WIND TUNNELS

N81-31128"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

GRID30: COMPUTER PROGRAM FOR FAST GENERATION OF

MULTILEVEL, THREE-DIMENSIONAL

BOUNDARY-CONFORMING O-TYPE COMPUTATIONAL GRIDS

D. S. DULIKRAVICH Sep. 1981 14 p refs

(NASA-TP-1920; E-590) Avail: NTIS HC A02/MF A01 CSCL

01A

AIRCRAFT, BOUNDARY LAYER FLOW, COMPUTER

PROGRAMS, FLUID FLOW, GEOMETRY, ROTORS, WINGS

N81-31129"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

SURROGATE-EQUATION TECHNIQUE FOR SIMULATION OF

STEADY INVISCID FLOW Final Report

G. M JOHNSON Washington NASA Sep. 1981 40 p refs

(NASA-TP-1866; E-583) Avail: NTIS HC A03/MF A01 CSCL

01A

EULER EQUATIONS OF MOTION, FINITE DIFFERENCE

THEORY, INVISCID FLOW, tTERATIVE SOLUTION,

MATHEMATICAL MODELS

N81-31130" # National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

HIGH REYNOLDS NUMBER RESEARCH - 1980

L. W. MCKtNNEY, ed. and D. D. BAALS, ed. (Joint Inst. for

Advancement of Flight Sciences, Hampton, Va.) Sep. 1981 315

p refs Workshop held at Hampton, Va., 9-11 Dec. 1980

(NASA-CP-2183; L-14416) Avail: NTIS HC A14/MF A01

CSCL 01A

AERODYNAMIC COEFFICIENTS, AERODYNAMIC

CONFIGURATIONS, BOUNDARY LAYER FLOW, CONFERENCES,

REYNOLDS NUMBER

18

N82-11032"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SOME OBSERVATIONS ON A NEW NUMERICAL METHOD FOR

SOLVING NAVIER-STOKES EQUATIONS

A. KUMAR Nov. 1981 19 p refs

(NASA-TP-1934; L-14746) Avail: NTIS HC A02/MF A01

CSCL 01A

COMPUTER PROGRAMS, FINITE DIFFERENCE THEORY,

NAVlER-STOKES EQUATION, TWO DIMENSIONAL FLOW

N82-11033"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

WIND-TUNNEL RESULTS FOR A MODIFIED

17.PERCENT-THICK LOW-SPEED AIRFOIL SECTION

R. J. MCGHEE and W. D. BEASLEY Nov. 1981 87 p refs

(NASA-TP-1919; L-14666) Avail: NTIS HC A05/MF A01

CSCL 01A

AERODYNAMIC COEFFICIENTS, AIRFOIL PROFILES, LOW

SPEED STABILITY, TURBULENT FLOW, WIND TUNNEL TESTS

N82-12035"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

DESCRIPTION AND CALIBRATION OF THE LANGLEY UNITARY

PLAN WIND TUNNEL

C. M. JACKSON, JR., W. A. CORLETT, and W. J. MONTA Nov.

1981 104 p refs

(NASA-TP-1905; L-14024) Avail: NTIS HC A06/MF A01

CSCL 01A

BOUNDARY LAYERS, FLOW CHARACTERISTICS, MACH

NUMBER, SUPERSONIC WIND TUNNELS, TURBULENCE, WIND

TUNNEL CALIBRATION

N82-13106"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

FORCE AND MOMENT, FLOW-VISUALIZATION, AND

BOUNDARY-LAYER TESTS ON A SHUTTLE ORBITER MODEL

AT MACH 6

R L CALLOWAY Dec 1981 28 p refs

(NASA-TP-1952; L-14782) Avail: NTIS HC A02/MF A01

CSCL 01A

AERODYNAMIC CHARACTERISTICS, ANGLE OF ATTACK,

BOUNDARY LAYER FLOW, CONTROL SURFACES, REYNOLDS

NUMBER, SPACE SHUTTLE ORBITERS

N82-13107"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

WIND-TUNNEL INVESTIGATION OF THE EFFECTS OF BLADE

TIP GEOMETRY ON THE INTERACTION OF TORSIONAL LOADS

AND PERFORMANCE FOR AN ARTICULATED HELICOPTER

ROTOR

W. T. YEAGER and W. R. MANTAY Dec. 1981 64 p refs

Prepared in cooperation with Army Aviation Research and

Development Command, Hampton, Va.

(DA PROJ. 1L2-62209-AH-76)

(NASA-TP-1926; AVRADCOM-TR-81-B-5; L-14674) Avail: NTIS

HC A04/MF A01 CSCL 01A

AIRFOIL PROFILES, BLADE TIPS, ROTARY WINGS, ROTOR

AERODYNAMICS, TORSION, WIND TUNNEL TESTS

N82-13108"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

CROSSFLOW EFFECTS ON STEADY AND FLUCTUATING

PRESSURES ON AN OGIVE-CYLINDER CONE-FRUSTUM

MODEL IN SUPERSONIC SEPARATED FLOW

J. B. DODS, JR. (Raman Aeronautics Research and Engineering,

Inc., Palo Alto, Calif.) and C. F. COL Nov. 1981 58 p refs

(NAS2-10139)

(NASA-TP-1951; A-8563) Avail: NTIS HC A04/MF A01 CSCL

01A

CROSS FLOW, CYLINDRICAL BODIES, FLOW THEORY,

FRUSTUMS, OGIVES, PRESSURE GRADIENTS, SEPARATED

FLOW, SUPERSONIC FLOW, WIND TUNNEL TESTS
N82-14051"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

ANALYTIC INVESTIGATION OF EFFECT OF END-WALL

CONTOURING ON STATOR PERFORMANCE

R. J. BOYLE, H. E. RHOLIK, and L. J. GOLDMAN Nov. 1981

12 p refs

(NASA-TP-1943; E-719) Avail: NTIS HC A02/MF A01 CSCL

01A

AERODYNAMIC LOADS, BLADE TIPS, CONTOURS, STATOR

BLADES, STATORS, TURBINES, WALL FLOW

N82-14052"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EXPERIMENTAL AND ANALYTICAL INVESTIGATION OF

AXISYMMETRIC SUPERSONIC CRUISE NOZZLE GEOMETRY

AT MACH NUMBERS FROM 0.60 TO 1.30

G. T. CARSON, JR. and E. E. LEE, JR. Dec. 1981 89 p refs

(NASA-TP-1953; L-14661) Avail: NTIS HC A04/MF A01

CSCL 01A

AXlSYMMETRIC FLOW, BOATTAILS, CONVERGENT-DIVERGENT NOZZLES, MACH NUMBER, NOZZLE DESIGN, NOZZLE

GEOMETRY, SUPERSONIC AIRCRAFT

N82-14055"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

COMPARISON OF EXPERIMENTAL AND THEORETICAL

TURBULENCE REDUCTION CHARACTERISTICS FOR

SCREENS, HONEYCOMB, AND HONEYCOMB-SCREEN

COMBINATIONS

J. SCHEIMAN Dec. 1981 55 p refs

(NASA-TP-1958; L-14628) Avail: NTIS HC A04/MF A01

CSCL 01A

AERODYNAMIC DRAG, DECELERATION, DRAG REDUCTION,

HONEYCOMB STRUCTURES, TURBULENCE EFFECTS

N82-15015"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

LOW-SPEED AERODYNAMIC PERFORMANCE OF A

HIGH-ASPECT-RATIO SUPERCRITICAL-WlNG TRANSPORT

MODEL EQUIPPED WITH FULL-SPAN SLAT AND PART-SPAN

DOUBLE-SLOTTED FLAPS

H. L. MORGAN, JR. and J. W. PAULSON, JR. Dec. 1979 145

p refs

(NASA-TP-1580; L-13201) Avail: NTIS HC A07/MF A01

CSCL 01A

AERODYNAMIC COEFFICIENTS, ASPECT RATIO, LOW

SPEED, SUPERCRITICAL WINGS

N82-20149"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

LAMINAR FLOW CONTROL. THE RESEARCH AND

TECHNOLOGY STUDIES 1981

D, V. MADDALON, ed. Mar. 1982 135 p refs Proceedings

of Conf. held at Dryden Flight Research Center, Edwards, Calif.,

17-18 Sep. 1981

(NASA-Cpo2218; NAS 1.55:2218; L-15084) Avail: NTIS HC

A07/MFA01 CSCL 01A

AIRCRAFT CONSTRUCTION MATERIALS, BOUNDARY

LAYER CONTROL, LAMINAR FLOW AIRFOILS, LEADING EDGE

FLAPS, TRAILING-EDGE FLAPS

N82-20156"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

STATIC INTERNAL PERFORMANCE OF SINGLE

EXPANSION-RAMP NOZZLES WITH THRUST VECTORING AND

REVERSING

R. J. RE and B. L. BERRIER Mar. 1982 143 p refs

(NASA-TP-1962; L-14902; NAS 1.60:1962) Avail: NTIS HC

A07/MF A01 CSCL 01A

EXHAUST NOZZLES, NOZZLE FLOW, NOZZLE GEOMETRY,

STATIC AERODYNAMIC CHARACTERISTICS, STATIC TESTS,

THRUST REVERSAL, THRUST VECTOR CONTROL

02 AERODYNAMICS

N82-222t5"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECTS OF AXISYMMETRIC AND NORMAL AIR JET PLUMES

AND SOLID PLUME ON CYLINDRICAL AFTERBODY PRESSURE

DISTRIBUTIONS AT MACH NUMBERS FROM 1.65 TO 2.50

P. F. COVELL Apr. 1982 35 p refs

(NASA-TP-2005; L-14883; NAS 1.60:2005) Avail: NTIS HC

A03/MFA01 CSCL 01A

AFTERBODIES, AIR JETS, AXISYMMETRIC FLOW, FLOW

DISTRIBUTION, MACH NUMBER, PLUMES, PRESSURE

DISTRIBUTION, WIND TUNNEL TESTS

N82-25193"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AN ANALYTICAL PROCEDURE FOR COMPUTING SMOOTH

TRANSITIONS BETWEEN TWO SPECIFIED CROSS SECTIONS

WITH APPLICATIONS TO BLENDED WING BODY

CONFIGURATION

R. L. BARGER May 1982 20 p refs

(NASA-TP.2012; L-15053; NAS 1.60:20t2) Avail: NTIS HC

A02/MFA01 CSCL 01A

AERODYNAMIC CONFIGURATIONS, BODY-WING

CONFIGURATIONS, COMPUTER SYSTEMS DESIGN, MISSILE

CONFIGURATIONS, MISSILE DESIGN

N82-25196"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

WIND-TUNNEL/FLIGHT CORRELATION, 1981

L. W. MCKINNEY, ed. and D. D. BAALS, ed. Jun. 1982 224 p

refs Workshop held at Hampton, Va., 19-20 Nov. 1981

(NASA-CP-2225; L-15368; NAS 1.55:2225) Avail: NTIS HC

A10/MFA01 CSCL 14B

CONFERENCES, DATA CORRELATION, FLIGHT TESTS,

SPACE SHUTTLE ORBITERS, SUPERSONIC WIND TUNNELS,

TRANSONIC WIND TUNNELS, WIND TUNNEL APPARATUS,

WIND TUNNEL TESTS, WIND TUNNEL WALLS

N82-26227"# National Aeronautics and Space Administration.

Dryden (Hugh L.) Flight Research Center, Edwards, Calif.

IN-FLIGHT TRANSITION MEASUREMENT ON A 10 DEG CONE

AT MACH NUMBERS FROM 0.5 TO 2.0

D. F. FISHER and N S. DOUGHERTY, JR. Jun. 1982 143 p

refs

(NASA-TP-1971; H-1117; NAS 1.60:1971) Avail: NTIS HC

A07/MFA01 CSCL01A

BOUNDARY LAYER TRANSITION, F-15 AIRCRAFT, FLOW

MEASUREMENT, IN-FLIGHT MONITORING, MACH NUMBER,

NOSE CONES, SLENDER CONES

N82-26231"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

PERFORMANCE CHARACTERISTICS OF AXISYMMETRIC

CONVERGENT-DIVERGENT EXHAUST NOZZLES WITH

LONGITUDINAL SLOTS IN THE DIVERGENT

L. D. LEAVITT and L. S. BANGERT Jun. 1962 36 p refs

(NASA-TP-2013; L-15119; NAS 1.60:2013) Avail: NTIS HC

A03/MF A01 CSCL 01A

CONVERGENT-DIVERGENT NOZZLES, FLAPS (CONTROL

SURFACES), NOZZLE GEOMETRY, VENTILATION

N82-26232"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF AN

ELLIPTICAL BODY WITH A HORIZONTAL TAIL AT MACH

NUMBERS FROM 2.3 TO 4.63

B. L. SHROUT and A. W. ROBINS (Kentron International, Inc.)

Jun. 1982 39 p refs

(NASA-TP-2024; NAS 1.60:2024) Avail: NTIS HC A03/MF A01

CSCL 01A

AERODYNAMIC CHARACTERISTICS, HORIZONTAL TAIL

SURFACES, LIFT DRAG RATIO

19
02 AERODYNAMICS

N82-26234"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

LASER ANEMOMETER MEASUREMENTS IN AN ANNULAR

CASCADE OF CORE TURBINE VANES AND COMPARISON

WITH THEORY

L. J. GOLDMAN and R. G. SEASHULTZ Jun, 1982 47 p refs

(NASA-TP-2018; E-876; NAS 1.60:2018) Avail: NTIS HC

A03/MF A01 CSCL 01A

AERODYNAMIC CHARACTERISTICS, ANNULAR FLOW,

LASER ANEMOMETERS, STATOR BLADES, TURBINE BLADES

N82-26235"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

STATIC INTERNAL PERFORMANCE CHARACTERISTICS OF

TWO THRUST REVERSER CONCEPTS FOR AXlSYMMETRIC

NOZZLES

L. D. LEAVITT and R. J. RE Jun. 1982 24 p refs

(NASA-TP-2025; NAS 1.60:2025) Avail: NTIS HC A02/MF A01

CSCL 01A

AXlSYMMETRIC BODIES, EXHAUST NOZZLES, THRUST

REVERSAL, TURBINE BLADES

N82-28247"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

COMPUTER PROGRAM FOR CALCULATING FULL POTENTIAL

TRANSONIC, QUASI-THREE-DIMENSIONAL FLOW THROUGH

A ROTATING TURBOMACHINERY BLADE ROW

C. A. FARRELL Jun. 1982 57 p refs

(NASA-TP-2030; E-1013; NAS 1.60:2030) Avail: NTIS HC

A04/MF A01 CSCL 01A

CASCADE FLOW, COMPUTATIONAL FLUID DYNAMICS,

COMPUTER PROGRAMS, FLOW EQUATIONS, POTENTIAL

FLOW, THREE DIMENSIONAL FLOW, TRANSONIC FLOW,

TURBOMACHINE BLADES

N82-29270"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

VELOCITY GRADIENT METHOD FOR CALULATING

VELOCITIES IN AN AXISYMMETRIC ANNULAR DUCT

T. KATSANIS Jul. 1982 23 p refs

(NASA-Tpo2029; E-1104; NAS 1.60:2029) Avail: NTIS HC

A02/MF A01 CSCL 01A

ANNULAR DUCTS, DUCTED FLOW, FLOW VELOCITY,

VELOCITY DISTRIBUTION, WALL FLOW

N82-30291"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AEROPROPULSIVE CHARACTERISTICS OF MACH NUMBERS

UP TO 2.2 OF AXISYMMETRIC AND NONAXISYMMETRIC

NOZZLES INSTALLED ON AN F-18 MODEL

F. J: CAPONE Aug. 1982 80 p refs

(NASA-TP-2044; L-15208; NAS 1.60:2044) Avail: NTiS HC

A05/MF A01 CSCL 01A

AXISYMMETRIC BODIES, CONVERGENT-DIVERGENT

NOZZLES, F-18 AIRCRAFT, MACH NUMBER, NOZZLE

GEOMETRY

N82-32320"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECT OF NOZZLE AND VERTICAL-TAIL VARIABLES ON THE

PERFORMANCE OF A 3°SURFACE F-15 MODEL AT

TRANSONIC MACH NUMBERS

O. C. PENDERGRAFT, JR. and E. A. BARE Aug. 1982 171 p

(NASA-TP-2043; L-15304; NAS 1.60:2043) Avail: NTIS HC

A08/MF A01 CSCL01A

CONTROL STABILITY, F-15 AIRCRAFT, LONGITUDINAL

STABILITY, NOZZLE GEOMETRY, TAIL ASSEMBLIES, THRUST

REVERSAL, TRANSONIC SPEED

2O

N82-32322"# National Aeronautics and Space Administration.

LanGley Research Center, Hampton, Va.

EXPERIMENTAL INVESTIGATION OF TWO NONAXISYMMETRIC

WEDGE NOZZLES AT FREE STREAM MACH NUMBERS UP TO

1.20

M L. MASON and W. K. ABEYOUNIS Sep. 1982 117 p refs

(NASA-TP-2054; L-15276; NAS 1.60:2054) Avail: NTIS HC

A06/MF A01 CSCL 01A

FREE FLOW, MACH NUMBER, NOZZLE FLOW, NOZZLE

GEOMETRY, WEDGES

N83-10016"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AN EXPERIMENTAL AND THEORETICAL INVESTIGATION OF

THICK WINGS AT VARIOUS SWEEP ANGLES IN AND OUT OF

GROUND EFFECT

J. W. PAULSON, JR_ and S. O. KJELGAARD Oct. 1982 165 p

refs

(NASA-TP-2068; L-15314; NAS 1.60:2068) Avail: NTIS HC

A08/MF A01 CSCL 01A

GROUND EFFECT (AERODYNAMICS), LONGITUDINAL

STABILITY, SPANLOADER AIRCRAFT, SWEEP ANGLE, WIND

TUNNEL TESTS, WING PROFILES

N83-11058"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

PERFORMANCE OF A TANDEM-ROTOR/TANDEM-STATOR

CONICAL-FLOW COMPRESSOR DESIGNED FOR A PRESSURE

RATIO OF 3

J. R. WOOD, A. K. OWEN (Army Aviation Research and

Development Command, Cleveland, Ohio), and L. F. SCHUMANN

(Army Aviation Research and Development Command, Cleveland,

Ohio) Oct. 1982 38 p refs

(NASA-TP-2034; E-369; NAS 1.60:2034; AVRADCOM-TR-81-C-5)

Avail: NTIS HC A03/MF A01 CSCL 01A

COMPRESSORS, CONICAL FLOW, GAS TURBINE ENGINES,

PRESSURE RATIO, ROTORS, STATORS

N83-11059"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

INVESTIGATION OF INSTALLATION EFFECTS OF

SINGLE-ENGINE CONVERGENT-DIVERGENT NOZZLES

J. R. BURLEY, II and B. L. BERRIER Nov. 1982 234 p refs

(NASA-TP-2078; L-15343; NAS 1.60:2078) Avail: NTIS HC

A11/MF A01 CSCL01A

AERODYNAMIC DRAG, CONVERGENT-DIVERGENT

NOZZLES, WIND TUNNEL TESTS

N83-16290"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

LOW-SPEED AERODYNAMIC CHARACTERISTICS OF A

17-PERCENT-THICK MEDIUM SPEED AIRFOIL DESIGNED FOR

GENERAL AVIATION APPLICATIONS

R. J. MCGHEE and W. D. BEASELEY Dec. 1980 87 p refs

(NASA-TP-1786; L-13900; NAS 1.60:1786) Avail: NTIS HC

A05/MFA01 CSCL01A

AERODYNAMIC CHARACTERISTICS, AIRFOIL PROFILES,

AIRFOILS, GENERAL AVIATION AIRCRAFT, LOW SPEED, WIND

TUNNEL TESTS

N83-22161"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AEROPROPULSIVE CHARACTERISTICS OF TWIN

SINGLE-EXPANSION-RAMP VECTORING NOZZLES INSTALLED

WITH FORWARD-SWEPT WINGS AND CANARDS

M. L. MASON and F. J. CAPONE Mar. t983 76 p refs

(NASA-TP-2133; L-15555; NAS 1.60:2133) Avail: NTIS HC

A05/MF A01 CSCL 01A

BODY-WING CONFIGURATIONS, CANARD CONFIGURATIONS, NOZZLE THRUST COEFFICIENTS, SWEPT FORWARD

WINGS, THRUST VECTOR CNTROL, WIND TUNNEL TESTS
N83-22162"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EXPERIMENTAL STUDY OF WING LEADING-EDGE DEVICES

FOR IMPROVED MANEUVER PERFORMANCE OF A

SUPERCRITICAL MANEUVERING FIGHTER CONFIGURATION

M. J. MANN, J. K. HUFFMAN, C. H. FOX, JR., and R. L.

CAMPBELL Mar. 1983 84 p refs

(NASA-TP-2125; L-15539; NAS 1.60:2125) Avail: NTIS HC

A05/MF A01 CSCL 01A

FIGHTER AIRCRAFT, LEADING EDGE FLAPS,

MANEUVERABILITY, SUPERCRITICAL WINGS, VORTEX

GENERATORS, WIND TUNNEL TESTS

N83-22166"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

A COMMON GEOMETRIC DATA-BASE APPROACH FOR

COMPUTER-AIDED MANUFACTURING OF WIND-TUNNEL

MODELS AND THEORETICAL AERODYNAMIC ANALYSIS

, M J. SEE (Kansas Univ., Lawrence) and J. V. COZZOLONGO

Apr. 1983 27p refs

(NASA-TP-2151; A-9169; NAS 1.60:2151) Avail: NTIS HC

A03/MF A01 CSCL 01A

AERODYNAMIC CHARACTERISTICS, AIRCRAFT CONFIGURATIONS, COMPUTER AIDED MANUFACTURING, WIND TUNNEL MODELS

N83-24478"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECTS OF TWIN-VERTICAL-TAIL PARAMETERS ON

TWIN-ENGINE AFTERBODYINOZZLE AERODYNAMIC

CHARACTERISTICS

L. D. LEAVITT and E. A. BARE May 1983 106 p refs

(NASA-TP-2158; L-15570; NAS 1.60:2158) Avail: NTIS HC

A06/MF A01 CSCL 01A

AERODYNAMIC CHARACTERISTICS, AFTERBODIES,

ENGINE AIRFRAME INTEGRATION, NOZZLES, TAIL

ASSEMBLIES, WIND TUNNEL TESTS

N83-25665"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

PRESSURES MEASURED IN FLIGHT ON THE AFT FUSELAGE

AND EXTERNAL NOZZLE OF A TWIN-JET FIGHTER

J. NUGENT, T. J. PLANT, R. A. DAVIS, and N. V. TAILLON May

1983 90 p refs

(NASA-TP-2017; H-1161; NAS 1.60:2017) Avail: NTIS HC

A05/MF A01 CSCL 01A

BOUNDARY LAYERS, FIGHTER AIRCRAFT, FUSELAGES,

NOZZLE FLOW, NOZZLE GEOMETRY, PRESSURE

MEASUREMENT

N83-25666"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECT OF EMPENNAGE LOCATION ON TWIN-ENGINE

AFTERBODY-NOZZLE AERODYNAMIC CHARACTERISTICS AT

MACH NUMBERS FROM 0.6 TO 1.2

L. D. LEAVITT May 1983 223 p refs

(NASA-TP-2116; L-15527; NAS 1.60:2116) Avail: NTIS HC

A10/MFA01 CSCL 01A

AERODYNAMIC CHARACTERISTICS, AFTERBODIES,

AIRCRAFT CONFIGURATIONS, NOZZLE GEOMETRY, TAIL

ASSEMBLIES, WIND TUNNEL TESTS

N83-26821"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECTS OF VARYING PODDED NACELLE-NOZZLE

INSTALLATIONS ON TRANSONIC AEROPROPULSIVE

CHARACTERISTICS OF A SUPERSONIC FIGHTER AIRCRAFT

F. J. CAPONE and D. E. REUBUSH May 1983 337 p refs

(NASA-TP-2120; L-15525; NAS 1.60:2120) Avail: NTIS HC

A15/MF A01 CSCL01A

FIGHTER AIRCRAFT, NACELLES, NOZZLE DESIGN,

PROPULSION SYSTEM PERFORMANCE, SUPERSONIC FLIGHT,

SUPERSONIC NOZZLES

02 AERODYNAMICS

N83-27959"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECT OF TAIL-FIN SPAN ON STABILITY AND CONTROL

CHARACTERISTICS OF A CANARD-CONTROLLED MISSILE AT

SUPERSONIC MACH NUMBERS

A. B. BLAIR, JR., J. M. ALLEN, and G. HERNANDEZ Jun. 1983

86 p refs

(NASA-TP-2157; L-15586; NAS 1.60:2157) Avail: NTIS HC

A05/MF A01 CSCL01A

AERODYNAMIC CONFIGURATIONS, MISSILE CONFIGURATIONS, SUPERSONICS

N83-30386"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

DESIGN AND EXPERIMENTAL RESULTS FOR A FLAPPED

NATURAL-LAMINAR-FLOW AIRFOIL FOR GENERAL AVIATION

APPLICATIONS

D. M. SOMERS Jun. 1981 125 p refs

(NASA-TP-1865; L-14409; NAS 1.60:1865) Avail: NTIS HC

A06/MFA01 CSCL 01A

AIRFOILS, FLAPS (CONTROL SURFACES), LAMINAR FLOW

N83-30389"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EXPERIMENTAL INVESTIGATION OF A 10-PERCENT-THICK

HELICOPTER ROTOR AIRFOIL SECTION DESIGNED WITH A

VISCOUS TRANSONIC ANALYSIS CODE

K. W. NOONAN Jul. 1981 78 p refs

(DA PROJ. 1L1-61102-AH-45)

(NASA-TP-1864; L-14182; NAS 1.60:1864;

AVRADCOM-TR-81-B-3) Avail: NTIS HC A05/MF A01 CSCL

01A

AIRFOIL PROFILES, HELICOPTER DESIGN, ROTARY WINGS,

TRANSONIC SPEED, VISCOUS FLOW

N83-30390"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

LOW-SPEED AERODYNAMIC PERFORMANCE OF AN

ASPECT-RATIO-10 SUPERCRITICAL-WING TRANSPORT

MODEL EQUIPPED WITH A FULL-SPAN SLAT AND PART-SPAN

AND FULL-SPAN DOUBLE-SLOTTED FLAPS

H. L. MORGAN, JR. Apr. 1981 183 p refs

(NASA-TP-1805; L-13825; NAS 1.60:1805) Avail: NTIS HC

A09/MF A01 CSCL 01A

AERODYNAMIC CHARACTERISTICS, LEADING EDGE SLATS,

SUPERCRITICAL WINGS, WING FLAPS

N83-30391"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

WALL-TEMPERATURE EFFECTS ON THE AERODYNAMICS OF

A HYDROGEN-FUELED TRANSPORT CONCEPT IN MACH 8

BLOWDOWN AND SHOCK TUNNELS

J. A. PENLAND, D. C. MARCUM, JR., and S. H. STACK Jul.

1983 61 p refs

(NASA-TP-2159; L-15100; NAS 1.60:2159) Avail: NTIS HC

A04/MF A01 CSCL 01A

AERODYNAMIC CHARACTERISTICS, BOUNDARY LAYER

FLOW, HYPERSONIC AIRCRAFT, WALL TEMPERATURE, WIND

TUNNEL TESTS

N83-31577"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

WIND-TUNNEL INVESTIGATION OF LEADING-EDGE THRUST

ON ARROW WINGS IN SUPERSONIC FLOW

R. J. MACK Aug. 1983 80 p refs

(NASA-TP-2167; L-15535; NAS 1.60:2167) Avail: NTIS HC

A05/MF A01 CSCL 01A

AIRFOILS, BLUNT BODIES, LEADING EDGES, SUPERSONIC

FLOW, WIND TUNNEL TESTS

21
02 AERODYNAMICS

N83-32774"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

COMPARISON OF TWO- AND THREE-DIMENSIONAL FLOW

COMPUTATIONS WITH LASER ANEMOMETER MEASUREMENTS IN A TRANSONIC COMPRESSOR ROTOR

R. V. CHIMA and A. J. STRAZISAR Sep. 1982 21 p refs

Presented at ASME 27th Intern. Gas Turbine Conf., London, 18-22

Apr. 1982 Film supplement C-299 available

(NASA-TP-1931; E-1007; NAS 160:1931) Avail: NTIS HC

A02/MF A01 CSCL 01A

COMPRESSOR ROTORS, EULER EQUATIONS OF MOTION,

FLUID MECHANICS, MACH NUMBER, TURBOMACHtNERY

N83-32776"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

THEORETICAL AND EXPERIMENTAL INVESTIGATION OF

SUPERSONIC AERODYNAMIC CHARACTERISTICS OF A

TWIN-FUSELAGE CONCEPT

R. M. WOOD, D. S. MILLER, and K. S. BRENTNER Aug. 1983

39 p refs

(NASA-TP-2184; L-15607; NAS 1.61:2184) Avail: NTIS HC

A03/MF A01 CSCL01A

AERODYNAMIC CHARACTERISTICS, COMPUTER PROGRAMS, PREDICTIONS, SUPERSONIC TRANSPORTS, WIND

TUNNEL TESTS

N83-34904"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AERODYNAMIC CHARACTERISTICS OF A SERIES OF BODIES

WITH VARIATIONS IN NOSE CAMBER

B. L. SHROUT and P. F. COVELL Sep. 1983 55 p refs

(NASA-TP-2206; L-15647; NAS 1.60:2206) Avail: NTIS HC

A04/MF A01 CSCL 01A

AERODYNAMIC CHARACTERISTICS, AERODYNAMIC

CONFIGURATIONS, CAMBER, FOREBODtES, WIND TUNNEL

TESTS

N83-34905"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EXPERIMENTAL INVESTIGATION OF LEADING-EDGE THRUST

AT SUPERSONIC SPEEDS

R. M. WOOD and D. S. MILLER Sep. 1983 52 p refs

(NASA-TP-2204; L-15620; NAS 1.60:2204) Avail: NTIS HC

A04/MF A01 CSCL 01A

JET THRUST, LEADING EDGES, SUPERSONIC SPEED, WING

PLANFORMS

N83-34906"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

EXPERIMENTS IN A THREE-DIMENSIONAL ADAPTIVE-WALL

WIND TUNNEL

E. T. SCHAIRER Sep. 1983 33 p refs

(NASA-TP-2210; A-9255; NAS 1.60:2210) Avail: NTIS HC

A03/MF A01 CSCL 01A

AERODYNAMIC INTERFERENCE, DATA ACQUISITION, TWO

DIMENSIONAL FLOW, WIND TUNNEL TESTS, WIND TUNNEL

WALLS

N83-36000"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

LOW-SPEED AERODYNAMIC CHARACTERISTICS OF A

HIGHLY SWEPT, UNTWISTED UNCAMBERED ARROW WING

P. L. COL, JR., S. O. KJELGAARD, and G. L. GENTRY, JR.

Oct. 1983 70p refs

(NASA-TP-2176; NAS 1.60:2176) Avail: NTIS HC A04/MF A01

CSCL 01A

AERODYNAMIC CHARACTERISTICS, ARROW WINGS,

SWEPT WINGS, UNCAMBERED WINGS

22

N84-10025" # National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECT OF THRUST VECTORING AND WING MANEUVER

DEVICES ON TRANSONIC AEROPROPULSIVE CHARACTERISTICS OF A SUPERSONIC FIGHTER

F. J. CAPONE and D. E. REUBUSH Feb. 1983 88 p refs

(NASA-TP-2119; L-t5526; NAS 1.60:2119) Avail: NTIS HC

A05/MF A01 CSCL 01A

FIGHTER AIRCRAFT, MANEUVERABILITY, SUPERSONIC

FLOW, THRUST VECTOR CONTROL, TRANSONIC FLOW,

WINGS

N84-13152"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

INVESTIGATION OF INSTALLATION EFFECTS ON

TWIN-ENGINE CONVERGENT-DIVERGENT NOZZLES

E. A. BARE and B. L. BERRIER Nov. 1983 191 p refs

(NASA-TP-2205; L-15609; NAS 1.60:2205) Avail: NTIS HC

A09/MFA01 CSCL01A

CONVERGENT-DIVERGENT NOZZLES, SUPERSONIC

CRUISE AIRCRAFT RESEARCH

N84-13162"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AERODYNAMIC FORCE MEASUREMENTS WITH A

STRAIN-GAGE BALANCE IN A CRYOGENIC WIND TUNNEL

R. P. BOYDEN, W. G. JOHNSON, JR., and A. T. FERRIS Dec.

1983 43 p refs

(NASA-TP-2251; L-15685; NAS 1.60:2251) Avail: NTIS HC

A03/MF A01 CSCL 01A

AERODYNAMIC FORCES, CRYOGENIC WIND TUNNELS,

STRAIN GAGES

N84-13163"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

THRUST-INDUCED EFFECTS ON SUBSONIC LONGITUDINAL

AERODYNAMIC CHARACTERISTICS OF A VECTORED.ENGINEOVER-WING CONFIGURATION

P. F. QUiNTO and J. W. PAULSON, JR. Dec. 1983 56 p rets

(NASA-TP-2228; L-15629; NAS 1.60:2228) Avail: NTIS HC

A04/MF A01 CSCL 01A

JET EXHAUST, PROPULSION SYSTEM CONFIGURATIONS,

SHORT TAKEOFF AIRCRAFT, THRUST VECTOR CONTROL

N84-13164"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AERODYNAMIC CHARACTERISTICS, INCLUDING EFFECT OF

BODY SHAPE, OF A MACH 6 AIRCRAFT CONCEPT

G. D. RIEBE Dec. 1983 32 p refs

(NASA-TP-2235; L-15675; NAS 1.60:2235) Avail: NTIS HC

A03/MF A01 CSCL 01A

AERODYNAMIC CHARACTERISTICS, HYDROGEN FUELS,

HYPERSONIC AIRCRAFT, MACH NUMBER, TRANSPORT

AIRCRAFT

N84-13165"# National Aeronautics and Space Administration.

J_angley Research Center, Hampton, Va.

EFFECT OF THRUST REVERSER OPERATION ON THE

LATERAL-DIRECTIONAL CHARACTERISTICS OF A

THREE-SURFACE F-15 MOOEL AT TRANSONIC SPEEDS

E. A. BARE and O. C. PENDERGRAFT, JR. Dec. 1983 91 p

refs

(NASA-TP-2234; L-15648; NAS 1.60:2234) Avail: NTIS HC

A05/MF A01 CSCL 01A

F-15 AIRCRAFT, NOZZLE DESIGN, PROPULSION SYSTEM

CONFIGURATIONS, RUDDERS, THRUST REVERSAL, WIND

TUNNEL MODELS
N84-17127"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

WAVE DRAG AS THE OBJECTIVE FUNCTION IN TRANSONIC

FIGHTER WING OPTIMIZATION

P. S. PHILLIPS Feb. 1984 23 p refs

(NASA-TP-2265; L-15687; NAS 1.60:2265) Avail: NTIS HC

A02/MF A01 CSCL 01A

AIRCRAFT DESIGN, AIRCRAFT MANEUVERS, DRAG

REDUCTION, FIGHTER AIRCRAFT, TRANSONIC FLIGHT, WAVE

DRAG

N84-17132"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

THEORETICAL AND EXPERIMENTAL ENGINE-INLET FLOW

FIELDS FOR FIGHTER FOREBODIES

S. F. YARDS Feb. 1984 66p refs

(NASA-TP-2270; L-15639; NAS 1.60:2270) Avail: NTIS HC

A04/MF A01 CSCL 01A

ENGINE INLETS, FIGHTER AIRCRAFT, FLOW DISTRIBUTION,

FOREBODIES, INLET FLOW, PREDICTION ANALYSIS

TECHNIQUES

N84-18159"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AIRFOIL INTERACTION WITH IMPINGING VORTEX

K. W. MCALISTER and C. TUNG Feb. 1984 86 p refs

Prepared in cooperation with Army Aviation Systems Command,

St. Louis, Mo.

(NASA-TP-2273; E-1585; NAS 1.60:2273; AVSCOM-TR-83-A-17)

Avail: NTIS HC A05/MF A01 CSCL 01A

AIRFOILS, DRAG, LIFT, PITCHING MOMENTS, VORTICES

N84-18161"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AERODYNAMIC DESIGN FOR IMPROVED MANUEVERABILITY

BY USE OF THREE-DIMENSIONAL TRANSONIC THEORY

M. J. MANN, R. L. CAMPBELL, and J. C. FERRIS Feb. 1984

72 p refs

(NASA-TP-2282; L-15681; NAS 1.60:2282) Avail: NTIS HC

A04/MF A01 CSCL 01A

AERODYNAMIC CONFIGURATIONS, MANEUVERABILITY,

TRANSONIC FLOW

N84-18162*# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AN EXPERIMENTAL INVESTIGATION OF NACELLE-PYLON

INSTALLATION ON AN UNSWEPT WING AT SUBSONIC AND

TRANSONIC SPEEDS

J. R. CARLSON and W. B. COMPTON, III Feb. 1984 203 p

refs

(NASA-TP-2246; L-15589; NAB 1.60:2246) Avail: NTIS HC

A10/MF A01 CSCL01A

AERODYNAMIC INTERFERENCE, NACELLES, SUPERCRITICAL WINGS, TRANSONIC SPEED, UNSWEPT WINGS

N64-18163"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

BODY AND CANARD EFFECTS ON AN ATTACHED-FLOW

MANEUVER WING AT MACH 1.62

J. L. PITTMAN, D. S. MILLER, and W. H. MASON (Grumman

Aerospace Corp., Bethpage, N.Y.) Feb. 1984 149 p refs

(NASA-TP-2249; L-15677; NAS 1.60:2249) Avail: NTIS HC

AO7/MF A01 CSCL 01A

AIRCRAFT MANEUVERS, BODY-WING CONFIGURATIONS,

CAMBERED WINGS, CANARD CONFIGURATIONS, CROSS

FLOW, UNCAMBERED WINGS

02 AERODYNAMICS

N84-18164"# National Aeronautics and Space Administration.

Lanaley Resear_'h Center, Hampton, Va.

INVESTIGATION OF TRAILING-EDGE-FLAP, SPANWISE-BLOWING CONCEPTS ON AN ADVANCED FIGHTER CONFIGURATION

J. W. PAULSON, JR., P. F. QUINTO, and D. W. BANKS Mar.

1984 107p refs

(NASA-TP-2250; L-15627; NAS 1.60:2250) Avail: NTIS HC

A06/MF A01 CSCL 01A

AIRCRAFT CONFIGURATIONS, FIGHTER AIRCRAFT,

SPANWlSE BLOWING, TRAILING EDGES

N84-16165"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

STATIC INTERNAL PERFORMANCE INCLUDING THRUST

VECTORING AND REVERSING OF TWO-DIMENSIONAL

CONVERGENT-DIVERGENT NOZZLES

R. J. RE and L. D. LEAVITT Feb. 1984 111 p refs

(NASA-TP-2253; L-15671; NAS 1.60:2253) Avail: NTIS HC

A06/MF A01 CSCL 01A

CONVERGENT-DIVERGENT NOZZLES, NOZZLE GEOMETRY,

PRESSURE RATIO, THRUST REVERSAL, THRUST VECTOR

CONTROL

N64-20480"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

GENERALIZATION OF THE SUBSONIC KERNEL FUNCTION IN

THE S-PLANE, WITH APPLICATIONS TO FLUTTER ANALYSIS

H. J. CUNNINGHAM and R. N. DESMARAIS Mar. 1984 39 p

refs

(NASA-TP-2292; L-15708; NAS 1.60:2292) Avail: NTIS HC

A03/MF A01 CSCL 01A

AERODYNAMIC FORCES, AEROELASTICITY, CONTROL

THEORY, FLUTTER ANALYSIS, KERNEL FUNCTIONS,

SUBSONIC FLUTTER

N84-20466"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

WING PLANFORM EFFECTS AT SUPERSONIC SPEEDS FOR

AN ADVANCED FIGHTER CONFIGURATION

R. M. WOOD and D. S. MILLER Mar. 1984 117 p refs

(NASA-TP-2269; L-15706; NAS 1.60:2269) Avail: NTIS HC

A06/MF A01 CSCL01A

AERODYNAMIC CHARACTERISTICS, AIRCRAFT CONFIGURATIONS, FIGHTER AIRCRAFT, SUPERSONIC AIRFOILS, WIND

TUNNEL TEST, WING PLANFORMS

N64-20493"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EXPERIMENTAL INVESTIGATION OF TANGENTIAL BLOWING

APPLIED TO A SUBSONIC V/STOL INLET

R. R. BURLEY Apr. 1984 20 p refs

(NASA-TP-2297; E-1907; NAS 1.60:2297) Avail: NTIS HC

A02/MF A01 CSCL 01A

ANGLE OF ATTACK, BOUNDARY LAYER CONTROL, ENGINE

INLETS, SPANWISE BLOWING

N84-24538"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va

AEROPROPULSlVE CHARACTERISTICS OF NONAXlSYMMETRIC-NOZZLE THRUST REVERSERS AT MACH NUMBERS FROM

O TO 1.20

G. T. CARSON, JR., F. J. CAPONE, and M. L. MASON May

1984 126 p refs

(NASA-TP-2306; L-15724; NAS 1.60:2306) Avail: NTIS HC

A07/MF A01 CSCL 01A

AERODYNAMIC CONFIGURATIONS, FIGHTER AIRCRAFT,

NOZZLE FLOW, NOZZLE GEOMETRY, THRUST REVERSAL

23
02 AERODYNAMICS

N84-26660"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

NATURAL LAMINAR FLOW EXPERIMENTS ON MODERN

AIRPLANE SURFACES

B. J. HOLMES, C. J. OBARA (Kentron International, Inc., Hampton,

Va.), and L. P. YIP Jun. 1984 145 p refs

(NASA-TP-2256; L-15552; NAS 1.60:2256) Avail: NTIS HC

A07/MF A01 CSCL 01A

FLOW VISUALIZATION, GENERAL AVIATION AIRCRAFT,

LAMINAR BOUNDARY LAYER, LAMINAR FLOW, VELOCITY

DISTRIBUTION, WIND TUNNEL TESTS

N84-27674"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

BIBLIOGRAPHY OF SUPERSONIC CRUISE RESEARCH (SCR)

PROGRAM FROM 1980 TO 1983

S. HOFFMAN Jul. 1984 56 p

(NASA-RP-1117; L-15740; NAS 1.61:1117) Avail: NTIS HC

A04/MF A01 CSCL 01A

A bibliography for the Supersonic Cruise Research (SCR) and

Variable Cycle Engine (VCE) Programs is presented. An annotated

bibliography for the last 123 formal reports and a listing of titles

for 44 articles and presentations is included. The studies identifies

technologies for producing efficient supersonic commercial jet

transports for cruise Mach numbers from 2.0 to 2.7. MAC.

N84-27675"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

RECENT MODIFICATIONS AND CALIBRATION OF THE

LANGLEY LOW-TURBULENCE PRESSURE TUNNEL

R. J. MCGHEE, W. D. BEASLEY, and J. M. FOSTER 1984 65

p refs

(NASA-TP-2328; L-15728; NAS 1.60:2328) Avail: NTIS HC

A04/MF A01 CSCL 01A

FLOW CHARACTERISTICS, LAMINAR FLOW, LOW SPEED

WIND TUNNELS, LOW TURBULENCE, REVISIONS, WIND

TUNNEL APPARATUS, WIND TUNNEL CALIBRATION

N84-27676"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECT OF FUSELAGE UPWASH ON THE SUPERSONIC

LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF 2

FIGHTER CONFIGURATIONS

R M WOOD and D. S. MILLER Jul. 1984 61 p refs

(NASA-TP-2330; L-15758; NAS 1.60:2330) Avail: NTIS HC

A04/MF A01 CSCL 01A

AERODYNAMIC CHARACTERISTICS, FIGHTER AIRCRAFT,

FUSELAGES, LINEARITY, SUPERSONIC AIRCRAFT, UPWASH

N84-27682"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

VlSCOUS-INVlSCID INTERACTION METHOD INCLUDING WAKE

EFFECTS FOR THREE-DIMENSIONAL WING-BODY

CONFIGURATIONS

C. L. STREETT Sep. 1981 30 p refs Presented at AIAA

14th Fluid and Plasma Dyn. Conf., Palo Alto, Calif., 22-24 Jun.

1981

(NASA-TP-1910; L-14053; NAS 1.60:1910; AIAA-81-1266) Avail:

NTIS HC A03/MF A01 CSCL 01A

FINITE DIFFERENCE THEORY, INVlSCID FLOW, THREE

DIMENSIONAL BOUNDARY LAYER, VISCOUS FLOW

N84-27686"# National Aeronautics and Space Administration.

Dryden (Hugh L.) Flight Research Center, Edwards, Calif.

KC-135 WINGLET PROGRAM REVIEW

Washington Jan. 1982 193 p refs Symp. held in Edwards,

Calif., 16 Sep. t981

(NASA-CP-2211; H-1165; NAS t.55:2211) Avail: NTIS HC

A0g/MF A01 CSCL 01A

AERODYNAMIC CHARACTERISTICS, AERODYNAMIC

LOADS, AIRCRAFT PERFORMANCE, C-135 AIRCRAFT,

CONFERENCES, FLIGHT TESTS, FLUTTER, FUEL

CONSUMPTION, WIND TUNNEL TESTS, WlNGLETS

24

N84-27694"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

TWO-DIMENSIONAL AERODYNAMIC CHARACTERISTICS OF

AN AIRFOIL DESIGNED FOR TWO

G. J. BINGHAM (Army Aviation Research and Development

Command, St. Louis), K. W. NOONAN (Army Aviation Research

and Development Command, St. Louis), and W. G. SEWALL Dec.

1981 79 p refs

(DA PROJ. 1L1-61102-AH-45)

(NASA-TP-1965; L-14825; NAS 1.60:1965;

AVRADCOM-TR-81-B-6) Avail: NTIS HC A05/MF A01 CSCL

01A

AERODYNAMIC CHARACTERISTICS, DESIGN ANALYSIS,

HELICOPTER DESIGN, ROTARY WINGS, TRANSONIC WIND

TUNNELS, WIND TUNNEL TESTS

N84-28743"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

TWO-DIMENSIONAL AERODYNAMIC CHARACTERISTICS OF

THREE ROTORCRAFT AIRFOILS AT MACH NUMBERS FROM

0.35 TO 0.90

G. J. BINGHAM and K. W. NOONAN May 1982 73 p refs

(DA PROJ. 1 L1-61102-AH-45)

(NASA-TP-2000; L-14955; NAS 1.60:2000;

AVRADCOM-TR-82-B-2) Avail: NTIS HC A04/MF A01 CSCL

01A

AERODYNAMIC CHARACTERISTICS, AIRFOILS, HELICOPTER DESIGN, ROTOR BLADES (TURBOMACHINERY)

N84-28750"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

A NUMERICAL SIMULATION OF THREE-DIMENSIONAL FLOW

IN AN ADAPTIVE WALL WIND TUNNEL

J. P. MENDOZA Aug. 1984 36 p refs

(NASA-TP-2351; A-9622; NAS 1.60:2351) Avail: NTIS HC

A03/MF A01 CSCL 01A

ANALYSIS (MATHEMATICS), COMPUTERIZED SIMULATION,

PROTOTYPES, THREE DIMENSIONAL FLOW, WIND TUNNEL

TESTS, WIND TUNNELS

N84-32354"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

FUSELAGE AND NOZZLE PRESSURE DISTRIBUTIONS OF A

1/12-SCALE F-15 PROPULSION MODEL AT TRANSONIC

SPEEDS. EFFECT OF FUSELAGE MODIFICATIONS AND

NOZZLE VARIABLES

O. C_ PENDERGRAFT, JR. and G. T. CARSON, JR. Aug. 1984

469 p

(NASA-TP-2333; L-15755; NAS 1.60:2333) Avail: NTIS HC

A20/MF A01 CSCL01A

BODY-WING AND TAIL CONFIGURATIONS, FLOW

DISTRIBUTION, FUSELAGES, NOZZLE GEOMETRY, PRESSURE

DISTRIBUTION

N84-33377"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AERODYNAMIC DESIGN OF THE CONTOURED WIND-TUNNEL

LINER FOR THE NASA SUPERCRITICAL, LAMINAR-FLOW-CONTROL, SWEPT-WING EXPERIMENT

_-_ A_ NEWMAN, E. C. ANDERSON, and J. B. PE[ERSON, JH.

Sep. 1984 46p refs

(NASA-TP-2335; L-15521; NAS 1.60:2335) Avail: NTIS HC

A03/MF A01 CSCL 01A

BOUNDARY LAYER CONTROL, LAMINAR BOUNDARY

LAYER, SWEPT WINGS, WIND TUNNEL WALLS
N84-33379"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AN EXPERIMENTAL AND THEORETICAL INVESTIGATION OF

DEPOSITION PATTERNS FROM AN AGRICULTURAL

AIRPLANE

D. J. MORRIS, C. C. CROOM, C. P. VANDAM (Kansas Univ.,

Lawrence), and B. J. HOLMES Sep. 1984 157 p refs

(NASA-TP-2348; L-15718; NAS 1.60:2348) Avail: NTIS HC

A08/MF A01 CSCL 01A

AGRICULTURE, AIRSPEED, COMPUTER PROGRAMS,

DEPOSITION, FLIGHT TESTS, VELOCITY MEASUREMENT

N85-10914"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

TRANSONIC FLOW ANALYSIS FOR ROTORS. PART 1:

THREE-DIMENSIONAL QUASI-STEADY, FULL-POTENTIAL

CALCULATION

I.C. CHANG Oct. 1984 87p refs

(NASA-TP-2375-PT-1; A-9721-PT-1; NAS 1.60:2375-PT-1) Avail:

NTIS HC A05/MF A01 CSCL 01A

COMPUTER PROGRAMS, HELICOPTERS, PRESSURE

DISTRIBUTION, ROTARY WINGS, TRANSONIC FLOW

N85-10920"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EXPERIMENTAL TRIM DRAG VALUES AND FLOW-FIELD

MEASUREMENTS FOR A WIDE-BODY TRANSPORT MODEL

WITH CONVENTIONAL AND SUPERCRITICAL WINGS

P. F. JACOBS Oct. 1982 142 p refs

(NASA-TP-2071; L-15315; NAS 1.60:2071) Avail: NTIS HC

A07/MF A01 CSCL 01A

FLOW DISTRIBUTION, HORIZONTAL TAIL SURFACES,

MOMENTS, SUPERCRITICAL WINGS, TRANSPORT AIRCRAFT

N85-12011"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

WIND TUNNEL WALL INTERFERENCE ASSESSMENT AND

CORRECTION, 1983

P. A. NEWMAN, ed. and R. W. BARNWELL, ed. Washington

1984 417 p refs Workshop held in Hampton, Va., 25-26 Jan.

1983

(NASA-CP-2319; L-15812; NAS 1.55:2319) Avail: NTIS HC

A18/MFA01 CSCL 01A

AERODYNAMIC INTERFERENCE, CONFERENCES, FLOW

DISTRIBUTION, TRANSONIC WIND TUNNELS, WIND TUNNEL

WALLS

N85-12862"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

APPLICATION OF THE ONERA MODEL OF DYNAMIC STALL

K. W. MCALISTER, O. LAMBERT (Service Technique des

Programmes Aeronautiques, Paris), and D. PETOT (ONERA,

Chatillon, France) Nov. 1984 65 p refs

(NASA-TP-2399; A-9824; AVSCOM-TR-84-A-3; NAS 1.60:2399;

AD-A159502) Avail: NTIS HC A04/MF A01 CSCL 01A

AERODYNAMIC CHARACTERISTICS, AERODYNAMIC

STALLING, LOADS (FORCES), LOW SPEED STABILITY

N85-12864"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

LOCAL STABILITY ANALYSIS FOR A PLANAR SHOCK WAVE

M, D. SALAS Dec. 1984 14 p refs

(NASA-TP-2387; L-15768; NAS 1.60:2387) Avail: NTIS HC

A02/MF A01 CSCL 01A

FLAT SURFACES, NOZZLE FLOW, RANKINE-HUGONIOT

RELATION, SHOCK WAVES, STABILITY TESTS

02 AERODYNAMICS

N85-15693"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

DOWNWASH IN THE PLANE OF SYMMETRY OF AN

ELLIPTICALLY LOADED WING

J. D. PHILLIPS Jan. 1985 26 p refs

(NASA-TP-2414; A-9871; NAS 1.60:2414) Avail: NTIS HC

A03/MF A01 CSCL 01A

AERODYNAMIC CHARACTERISTICS, DOWNWASH,

ELLIPTICITY, SYMMETRY, WING LOADING

N85-15694"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

A COMPARATIVE STUDY OF THE NONUNIQUENESS PROBLEM

OF THE POTENTIAL EQUATION

M, D. SALAS, A. ,JAMESON (Princeton Univ., N.J.), and R, E.

MELNIK (Grumman Aerospace Corp., Bethpage, N.Y.) Jan.

1985 23 p refs

(NASA-TP-2385; L-15682; NAS 1.60:2385) Avail: NTIS HC

A02/MF A01 CSCL 01A

EULER EQUATIONS OF MOTION, INVISCID FLOW,

POTENTIAL THEORY, SHOCK WAVES, TRANSONIC FLOW

N85-18951"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

STATIC INTERNAL PERFORMANCE OF A TWO-DIMENSIONAL

CONVERGENT NOZZLE WITH THRUST-VECTORING

CAPABILITY UP TO 60 DEG

L. D. LEAVITT Feb. 1985 70 p refs

(NASA-TP-2391; L-15837; NAS 1.60:2391) Avail: NTIS HC

A04/MF A01 CSCL 01A

CONVERGENT NOZZLES, NOZZLE FLOW, NOZZLE THRUST

COEFFICIENTS, THRUST VECTOR CONTROL, WIND TUNNEL

TESTS

N85-19925"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

WIND-TUNNEL INVESTIGATION OF A FULL-SCALE

CANARD-CONFIGURED GENERAL AVIATION AIRPLANE

L. P. YIP Mar. 1985 81 p refs

(NASA-TP-2382; L-15744; NAS 1.60:2382) Avail: NTIS HC

A05/MFA01 CSCL01A

AERODYNAMIC CHARACTERISTICS, CANARD CONFIGURATIONS, CONTROL STABILITY, CONTROL SURFACES, GENERAL

AVIATION AIRCRAFT, WIND TUNNEL TESTS

N85-21118" # National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

FLIGHT-MEASURED LAMINAR BOUNDARY-LAYER

TRANSITION PHENOMENA INCLUDING STABILITY THEORY

ANALYSIS

C. J. OBARA (Kentron International, Inc.) and B. J. HOLMES Apr.

1985 40p refs

(NASA-TP-2417; L-15804; NAS 1.60:2417) Avail: NTIS HC

A03/MFA01 CSCL 01A

AERODYNAMIC COEFFICIENTS, BOUNDARY LAYER

TRANSITION, LAMINAR FLOW, TURBULENT BOUNDARY

LAYER

N85-21120"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SEMIANALYTIC MODELING OF AERODYNAMIC SHAPES

R. L. BARGER and M. S. ADAMS Apr. 1985 20 p refs

(NASA-TP-2413; L-15879; NAS 1.60:2413) Avail: NTIS HC

A02/MF A01 CSCL 01A

AERODYNAMIC CONFIGURATIONS, DIGITAL TECHNIQUES,

GRIDS, LOFTING, SHAPES, SURFACE GEOMETRY

25
02 AERODYNAMICS

N65-23707"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

CALIBRATION OF SONIC VALVES FOR THE LAMINAR FLOW

CONTROL, LEADING-EDGE FLIGHT TEST

D. H. PETLEY, W. ALEXANDER, JR., A. S. WRIGHT, JR., and M.

VALLAS May 1985 53 p refs

(NASA-TP-2423; L-15893; NAS 1.60:2423) Avail: NTIS HC

A04/MF A01 CSCL 01A

FLOW MEASUREMENT, LAMINAR FLOW, MASS FLOW RATE,

PRESSURE RATIO, SUCTION, TRANSONIC FLOW

N65-23706"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

LOW-SPEED STABILITY AND CONTROL WIND-TUNNEL

INVESTIGATIONS OF EFFECTS OF SPANWISE BLOWING ON

FIGHTER FLIGHT CHARACTERISTICS AT HIGH ANGLES OF

ATTACK

D. R SATRAN, W. P. GILBERT, and E. L. ANGLIN May 1985

46 p refs

(NASA-TP-2431; L-15851; NAS 1.60:2431) Avail: NTIS HC

A03/MF A01 CSCL 01A

ANGLE OF ATTACK, FIGHTER AIRCRAFT, FLIGHT

CHARACTERISTICS, LOW SPEED STABILITY, SPANWlSE

BLOWING, WIND TUNNEL TESTS

N85-26667"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EXPLORATORY WIND-TUNNEL INVESTIGATION OF A

WINGTIP-MOUNTED VORTEX TURBINE FOR VORTEX ENERGY

RECOVERY

J. C. PATTERSON, JR. and S. G. FLECHNER Jun. 1985 24 p

(NASA-TP-2468; L-15795; NAS 1.60:2468) Avail: NTIS HC

A02/MF A01 CSCL 01A

DRAG REDUCTION, ENERGY CONVERSION, TURBINES,

VORTICES, WIND TUNNEL TESTS, WING TIPS

N85-27822°# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SUPERSONIC AERODYNAMIC CHARACTERISTICS OF

CANARD, TAILLESS, AND AFT-TAIL CONFIGURATIONS FOR

2 WING PLANFORMS

P. F. COVELL Jun. 1985 69 p refs

(NASA-TP-2434; L-15927; NAS 1.60:2434) Avail: NTIS HC

A04/MF A01 CSCL 01A

AERODYNAMIC CONFIGURATIONS, BODY-WING AND TAIL

CONFIGURATIONS, CANARD CONFIGURATIONS, SUPERSONIC

SPEED, WING PLANFORMS

N85-27823"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

STATIC AND DYNAMIC PRESSURE MEASUREMENTS ON A

NACA 0012 AIRFOIL IN THE AMES HIGH REYNOLDS NUMBER

FACILITY

J. B. MCDEVITT and A. F. OKUNO Jun. 1985 78 p refs

(NASA-TP-2485; A-85100; NAS 1.60:2485) Avail: NTIS HC

A05/MF A01 CSCL 02A

AERODYNAMIC CONFIGURATIONS, AERODYNAMIC

STABILITY, AIRFOILS, FLOW DISTRIBUTION, SUBSONIC FLOW,

SUPERCRITICAL FLOW

N85-28923"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

WIND-TUNNEL EVALUATION OF A 21-PERCENT-SCALE

POWERED MODEL OF A PROTOTYPE ADVANCED SCOUT

HELICOPTER

A. E. PHELPS, III and J. D. BERRY Washington NASA,

Washington Jun. 1985 76 p refs Prepared in cooperation

with Army Aviation Systems Command, St. Louis

(DA PROJ. 1Lt-62209-AH76)

(NASA-TP-2420; L-15895; NAS 1.60:2420; AVSCOM-TR-85-B-2;

AD-A157115) Avail: NTIS HC A04/MF A01 CSCL 01A

AERODYNAMIC CHARACTERISTICS, HELICOPTER

26

PERFORMANCE, P-531 HELICOPTER, SCALE MODELS, WIND

TUNNEL TESTS

N85-26924"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

STATIC INVESTIGATION OF SEVERAL YAW VECTORING

CONCEPTS ON NONAXlSYMMETRIC NOZZLES

M. L. MASON and B. L. BERRIER Jun. 1985 219 p refs

(NASA-TP-2432; L-15890; NAS 1.60:2432) Avail: NTIS HC

A10/MF A01 CSCL01A

CONVERGENT-DIVERGENT NOZZLES, STATIC TESTS,

THRUST VECTOR CONTROL, WIND TUNNEL TESTS, YAW

N85-29921"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

LEE-SIDE FLOW OVER DELTA WINGS AT SUPERSONIC

SPEEDS

D. S. MILLER and R. M WOOD Jun. 1985 154 p refs

(NASA-TP-2430; L-15888; NAS 1.60:2430) Avail: NTIS HC

A08/MF A01 CSCL 01A

DELTA WINGS, FLOW VISUALIZATION, LEADING EDGES,

SUPERSONIC SPEED, VORTICES

N85-29922"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EXPERIMENTAL AND THEORETICAL STUDY OF THE

LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF

DELTA AND DOUBLE-DELTA WINGS AT MACH NUMBERS OF

1.60, 1.90, AND 2.16

R. M. WOOD and P. F. COVELL Jul. 1985 122 p refs

(NASA-TP-2433; L-15899; NAS 1.60:2433) Avail: NTIS HC

A06/MF A01 CSCL 01A

DELTA WINGS, SUPERSONIC AIRFOILS, SUPERSONIC

FLOW, SWEPTBACK WINGS

N85-29923"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECT OF LEADING-EDGE LOAD CONSTRAINTS ON THE

DESIGN AND PERFORMANCE OF SUPERSONIC WINGS

C. M. DARDEN Jul. 1985 78 p refs

(NASA-TP-2446; L-15841; NAS 1.60:2446) Avail: NTIS HC

A05/MF A01 CSCL 01A

BOUNDARY LAYER SEPARATION, SUPERSONIC AIRFOILS,

SUPERSONIC FLOW, SWEPT WINGS, WIND TUNNEL TESTS

N85-29924"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

NACELLE/PYLON/WING INTEGRATION ON A TRANSPORT

MODEL WITH A NATURAL LAMINAR FLOW NACELLE

M LAMB, W. K. AABEYOUNIS, and J. C. PATTERSON, JR. Jul.

1985 61 p refs

(NASA-TP-2439; L-15907; NAS 1.60:2439) Avail: NTIS HC

A04/MF A01 CSCL 01A

LAMINAR FLOW, PYLONS, TRANSPORT AIRCRAFT,

TURBULENT FLOW, WIND TUNNEL TESTS, WING NACELLE

CONFIGURATIONS

N85-31010"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

LOW-SPEED TESTS OF A HIGH-ASPECT-RATIO,

SUPERCRITICAL-WING TRANSPORT MODEL EQUIPPED WITH

A HIGH-LIFT FLAP SYSTEM IN THE LANGLEY 4- BY 7-METER

AND AMES 12-FOOT PRESSURE TUNNELS

H. L. MORGAN, JR. and S. O. KJELGAARD Jul. 1983 277 p

refs

(NASA-TP-2097; L-15484; NAS 1.60:2097) Avail: NTIS HC

A12/MFA01 CSCL 01A

AERODYNAMIC CHARACTERISTICS, HIGH ASPECT RATIO,

LEADING EDGE SLATS, LOW SPEED STABILITY, REYNOLDS

NUMBER, SLENDER WINGS, SUPERCRITICAL WINGS,

TRAILING EDGE FLAPS, TRANSPORT AIRCRAFT, WIND

TUNNEL TESTS, WING PROFILES
N85-33106"#National Aeronautics andSpaceAdministration.

Langley Research Center, Hampton, Va.

AN IMAGE COMPRESSION SURVEY AND ALGORITHM

SWITCHING BASED ON SCENE ACTIVITY

M. M. HART Aug. 1985 20p refs

(NASA-TP-2458; L-15957; NAS 1.60:2458) Avail: NTIS HC

A02/MF A01 CSCL 01A

ALGORITHMS, COMPUTER SYSTEMS PERFORMANCE,

DATA COMPRESSION, DATA TRANSMISSION, IMAGING

TECHNIQUES, SCENE ANALYSIS, SIGNAL DISTORTION

N85-33107"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AERODYNAMIC CHARACTERISTICS OF A DISTINCT

WING-BODY CONFIGURATION AT MACH 6: EXPERIMENT,

THEORY, AND THE HYPERSONIC ISOLATION PRINCIPLE

J. A. PENLAND and J. L. PITTMAN Aug. 1985 34 p refs

(NASA-TP-2467; L-15951; NAS 1.60:2467) Avail: NTIS HC

A03/MF A01 CSCL 01A

AERODYNAMIC CONFIGURATIONS, FUSELAGES,

HYPERSONIC AIRCRAFT, LEADING EDGE FLAPS, LOW

REYNOLDS NUMBER, WINGS

N86-11186"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECT OF AILERON DEFLECTIONS ON THE AERODYNAMIC

CHARACTERISTICS OF A SEMISPAN MODEL OF A SUBSONIC

ENERGY-EFFICIENT TRANSPORT

P. F. JACOBS Oct. 1985 344 p refs

(NASA-TP-2478; L-15934; NAS 1.60:2478) Avail: NTIS HC

A15/MFA01 CSCL01A

AERODYNAMIC CHARACTERISTICS, AILERONS,

SUPERCRITICAL WINGS, TRANSPORT AIRCRAFT, WIND

TUNNEL MODELS

N86-16193"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AERODYNAMIC CHARACTERISTICS OF A HIGH-WING

TRANSPORT CONFIGURATION WITH A OVER-THE-WING

NACELLE-PYLON ARRANGEMENT

W. P. HENDERSON and W. K. ABEYOUNIS Dec. 1985 93 p

refs

(NASA-TP-2497; L-15959; NAS 1.60:2497) Avail: NTIS HC

A05/MF A01 CSCL 01A

AERODYNAMIC CHARACTERISTICS, ENGINE AIRFRAME

INTEGRATION, NACELLES, PYLON MOUNTING, TRANSONIC

WIND TUNNELS, TRANSPORT AIRCRAFT, WIND TUNNEL

TESTS

N86-18289"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

COMPRESSIBLE, UNSTEADY LIFTING-SURFACE THEORY FOR

A HELICOPTER ROTOR IN FORWARD FLIGHT

H. L. RUNYAN and H. TAI Dec. 1985 21 p refs

(NASA-TP-2503; L-15976; NAS 1.60:2503) Avail: NTIS HC

A02/MF A01 CSCL 01A

ACCELERATION (PHYSICS), COMPRESSIBLE FLOW,

HELICOPTERS, LIFT DEVICES, LIFTING ROTORS, UNSTEADY

FLOW

N86-20345"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECT OF UNDERWING AFT-MOUNTED NACELLES ON THE

LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF A

HIGH-WING TRANSPORT AIRPLANE

W. K. ABEYOUNIS and J. C. PATTERSON, JR. Dec. 1985

139 p refs

(NASA-TP-2447; L-15664; NAS 1.60:2447) Avail: NTIS HC

A07/MF A01 CSCL 01A

AERODYNAMIC INTERFERENCE, ENGINE INLETS,

NACELLES, SHOCK ABSORBERS, SUPERSONIC AIRCRAFT,

TRANSPORT AIRCRAFT

02 AERODYNAMICS

N86-20346"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

INSTALLATION EFFECTS OF LONG-DUCT PYLON-MOUNTED

NACELLES ON A TWIN-JET TRANSPORT MODEL WITH SWEPT

SUPERCRITICAL WING

E. E. LEE, JR. and O. C. PENDERGRAFT, JR. Dec. 1985 145

p refs

(NASA-TP-2457; L-15932; NAS 1.60:2457) Avail: NTIS HC

A07/MF A01 CSCL 01A

AERODYNAMIC INTERFERENCE, DUCT GEOMETRY, JET

AIRCRAFT, NACELLES, SUPERCRITICAL WINGS, TRANSPORT

AIRCRAFT

N86-20347"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ORIFICE-INDUCED PRESSURE ERROR STUDIES IN LANGLEY

7- BY 10-FOOT HIGH-SPEED TUNNEL

E. B. PLENTOVICH and B. B. GLOSS Feb. 1986 24 p refs

(NASA-TP-2545; L-16001; NAS 1.60:2545) Avail: NTIS HC

A02/MF A01 CSCL 01A

ERRORS, FLAT PLATES, ORIFICES, PRESSURE

MEASUREMENT, STATIC PRESSURE, WIND TUNNEL TESTS

N86-20348"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

STATIC INTERNAL PERFORMANCE OF A SINGLE-ENGINE

ONAXlSYMMETRIC-NOZZLE VANED-THRUST-REVERSER

DESIGN WITH THRUST MODULATION CAPABILITIES

L. D. LEAVITT and J. R. BURLEY, tl Dec. 1985 109 p refs

(NASA-TP-2519; L-15991; NAS 1.60:2519) Avail: NTIS HC

A06/MF A01 CSCL 01A

NOZZLE GEOMETRY, STATIC TESTS, THRUST REVERSAL,

WIND TUNNEL TESTS

N86-20349"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AERODYNAMIC CHARACTERISTICS OF SEVERAL CURRENT

HELICOPTER TAIL BOOM CROSS SECTIONS INCLUDING THE

EFFECT OF SPOILERS

J. C. WILSON and H. L. KELLEY Jan. 1986 74 p refs

(DA PROJ. 1L1-61102-AH-45)

(NASA-TP-2506; L-15978; NAS 1.60:2506; AVSCOM-TR-85-B-3)

Avail: NTIS HC A04/MF A01 CSCL 01A

AERODYNAMIC CHARACTERISTICS, FUSELAGES,

HELICOPTER TAIL ROTORS, HOVERING, SPOILERS, TAIL

ASSEMBLIES

N86-20350"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

FLIGHT MEASUREMENTS OF SURFACE PRESSURES ON A

FLEXIBLE SUPERCRITICAL RESEARCH WING

C. V. ECKSTROM Dec. 1985 120 p refs

(NASA-TP-2501; L-15877; NAS 1.60:2501) Avail: NTIS HC

A06/MF A01 CSCL 01A

FLEXIBLE WINGS, PRESSURE MEASUREMENT,

SUPERCRITICAL PRESSURES, SUPERCRITICAL WINGS

N86-20351"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

THE APPLICATION TO AIRFOILS OF A TECHNIQUE FOR

REDUCING ORIFICE-INDUCED PRESSURE ERROR AT HIGH

REYNOLDS NUMBERS

E. B. PLENTOVICH Jan. 1986 44 p refs

(NASA-TP-2537; L-16002; NAS 1.60:2537) Avail: NTIS HC

A03/MF A01 CSCL 01A

AIRFOILS, BOUNDARY LAYER STABILITY, ERRORS,

ORIFICES, STATIC PRESSURE, TRANSONIC FLOW

27
02 AERODYNAMICS

N86-20352"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

BREAKDOWN OF THE CONSERVATIVE POTENTIAL

EQUATION

M. D. SALAS and C. R. GUMBERT Feb. 1986 38 p refs

Previously announced in IAA as A85-19700

(NASA-TP-2539; L-15769; NAS 1.60:2539) Avail: NTIS HC

A03/MF A01

FLOW EQUATIONS, POTENTIAL FLOW, TRANSONIC FLOW

N86-21506"# National Aeronautics and Space Administration,

Marshall Space Flight Center, Huntsville, Ata.

ANALYSIS OF JIMSPHERE PAIRS FOR USE IN ASSESSING

SPACE VEHICLE ASCENT CAPABILITY

C.K. HILL Mar. 1986 113p refs

(NASA-TP-2573; NAS 1.60:2573) Avail: NTIS HC A06/MF A01

CSCL 01A

ASCENT PROPULSION SYSTEMS, SPACECRAFT

LAUNCHING, WIND PROFILES, WIND SHEAR, WIND

VARIATIONS

N86-21507"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

INVESTIGATION OF SOLID PLUME SIMULATION CRITERIA TO

PRODUCE FLIGHT PLUME EFFECTS ON MULTIBODY

CONFIGURATION IN WIND TUNNEL TESTS

A. L. FROST and C. C. DILL Mar. 1986 182 p

(NASA-TP-2569; NAS 1.60:2569) Avail: NTIS HC A09/MF A01

CSCL 01A

COMPUTERIZED SIMULATION, PLUMES, SPACE SHUTTLES,

WIND TUNNEL TESTS

N86.23558°# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

MACH 6 FLOW FIELD SURVEYS BENEATH THE FOREBODY

OF AN AIRBREATHING MISSILE

P. J. JOHNSON and J. L. HUNT Mar. 1986 155 p refs

(NASA-TP-2491; L-15973; NAS 1.60:2491) Avail: NTIS HC

A08/MF A01 CSCL 01A

AIR BREATHING BOOSTERS, BOUNDARY LAYERS, FLOW

DISTRIBUTION, HYPERSONIC SPEED, MACH NUMBER,

MISSILES, REYNOLDS NUMBER, WIND TUNNEL TESTS

N86-23559"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

STATIC INVESTIGATION OF TWO STOL NOZZLE CONCEPTS

WITH PITCH THRUST-VECTORING CAPABILITY

M. L. MASON and J. R. BURLEY, tl Apr. 1986 57 p refs

(NASA-TP-2559; L-165052; NAS 1.60:2559) Avail: NTIS HC

A04/MFA01 CSCL01A

AXISYMMETRIC FLOW, NOZZLE GEOMETRY, NOZZLE

THRUST COEFFICIENTS, SHORT TAKEOFF AIRCRAFT, STATIC

TESTS, THRUST VECTOR CONTROL

N86-23560"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

STATIC INTERNAL PERFORMANCE OF A THRUST VECTORING

AND REVERSING TWO-DIMENSIONAL CONVERGENT-DIVERGENT NOZZLE WITH AN AFT FLAP

H. J. RE and L. D. LEAVITT Apr. 1986 113 p refs

(NASA-TP-2549; L-16025; NAS 1.60:2549) Avail: NTIS HC

A06/MF A01 CSCL 01A

NOZZLE GEOMETRY, STATIC TESTS, THRUST REVERSAL,

THRUST VECTOR CONTROL, TRANSONIC WIND TUNNELS,

WIND TUNNEL TESTS

28

N86-23561"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AERODYNAMIC CHARACTERISTICS OF A SUPERSONIC

FIGHTER AIRCRAFT MODEL AT MACH 0.40 TO 2.47

F. J. CAPONE, E. A. BARE, and D. ARBITER (George Washington

Univ., Hampton, Va.) Apr. 1986 105 p refs

(NASA-TP-2580; L-16017; NAS 1.60:2580) Avail: NTIS HC

A06/MF A01 CSCL 01A

AERODYNAMIC CHARACTERISTICS, DATA BASES, FIGHTER

AIRCRAFT, SUPERSONIC AIRCRAFT

N86-23562"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECTS OF UPPER-SURFACE NACELLES ON LONGITUDINAL

AERODYNAMIC CHARACTERISTICS OF HIGH-WING

TRANSPORT CONFIGURATION

L. E. PUTNAM Apr. 1986 70 p refs

(NASA-TP-2579; L-16062; NAS 1.60:2579) Avail: NTIS HC

A04/MF A01 CSCL 01A

AERODYNAMIC CHARACTERISTICS, BODY-WING

CONFIGURATIONS, TRANSONIC SPEED, TRANSPORT

AIRCRAFT, WIND TUNNEL TESTS

N86-24662"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

R4 AIRFOIL DATA CORRECTED FOR SIDEWALL

BOUNDARY-LAYER EFFECTS IN THE LANGLEY 0.3-METER

TRANSONIC CRYOGENIC TUNNEL

R. V. JENKINS May 1986 114 p refs

(NASA-TP-2565; L-16066; NAS 1.60:2565) Avail: NTIS HC

A06/MF A01 CSCL 01A

AIRFOILS, BOUNDARY LAYERS, CRYOGENIC WIND'

TUNNELS, TRANSONIC WIND TUNNELS

N86-27190*# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

VORTEX FLOW AERODYNAMICS, VOLUME 1

J. F. CAMPBELL, ed., R. F. OSBORN, ed. (Air Force Wright

Aeronautical Labs., Wright-Patterson AFB, Ohio), and J. T.

FOUGHNER, JR., ed. Jul. 1986 404 p Conference held in

Hampton, Va., 8-10 Oct. 1985

(NASA-CP-2416-VOL-1; L-16117; NAS 1.55:2416-VOL-1) Avail:

NTIS HC A18/MF A01 CSCL 01A

AERODYNAMICS, AIRCRAFT DESIGN, AIRCRAFT MODELS,

VORTEX FLAPS, VORTICES, WIND TUNNEL TESTS

03

AIR TRANSPORTATION AND SAFETY

Includes passenger and cargo air transport operations; and aircraft

accidents.

N77-18081"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AIRCRAFT SAFETY AND OPERATING PROBLEMS

1976 644 p refs Conf. Proc. held at Hampton, Va., 18-20

Oct. 1976

(NASA-SP-416) Avail: NTIS HC A99/MF A01 CSCL 01C

Results of NASA research in the field of aircraft safety and

operating problems are discussed. Topics include: (1) terminal area

operations, (2) flight dynamics and control; (3) ground operations;

(4) atmospheric environment; (5) structures and materials; (6)

powerplants; (7) noise; and (8) human factors engineering.
N78-10034"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

LIGHT AIRPLANE CRASH TESTS AT IMPACT VELOCITIES OF

13 AND 27 M/SEC

E. ALFARO-BOU and V. L. VAUGHAN, JR. Nov. 1977 52 p

refs

(NASA-TP-1042; L-11426) Avail: NTIS HC A04/MF A01

CSCL 01C

CRASH LANDING, FLIGHT TESTS, IMPACT TOLERANCES

N78-11024"# General Electric Co., Pittsfield, Mass.

LIGHTNING PROTECTION OF AIRCRAFT

F. A. FISHER and J. A. PLUMER Oct. 1977 530 p refs

(NAS3-19080)

(NASA-RP-1008) Avail: NTIS HC A23/MF A01 CSCL 01C

The current knowledge concerning potential lightning effects

on aircraft and the means that are available to designers and

operators to protect against these effects are summarized. The

increased use of nonmetallic materials in the structure of aircraft

and the constant trend toward using electronic equipment to handle

flight-critical control and navigation functions have served as

impetus for this study. For individual titles, see N78-11025 through

N78-11041.

N78-13029"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECTS OF LANDING APPROACH METHODS AND

SEPARATION INTERVALS ON SINGLE RUNWAY LANDING

CAPACITY

E. C. HASTINGS, JR. and R. T. TAYLOR Dec. 1977 40 p

refs

(NASA-TP-1112; L-11834) Avail: NTIS HC A03/MF A01

CSCL 17G

AIRCRAFT LANDING, APPROACH, RUNWAYS, TRANSPORT

AIRCRAFT

N79-21021"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

OZONE CONTAMINATION IN AIRCRAFT CABINS

Washington, D.C. NASA Mar. 1979 81 p refs Workshop

held at Moffett Field, Calif., 27-28 Jul. 1978

(NASA-CP-2066; E-9797) Avail: NTIS HC A05/MF A01 CSCL

06S

AIRCRAFT COMPARTMENTS, CONTAMINATION, NASA

PROGRAMS, OZONE

N79-31166"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

CONFERENCE ON FIRE RESISTANT MATERIALS: A

COMPILATION OF PRESENTATIONS AND PAPERS

D. A: KOURTIDES, ed. and G. A. JOHNSON, ed. (Boeing Com.

Airplane Co., Seattle, Wash.) Jul. 1979 287 p Conf. held in

Seattle, 1-2 Mar. 1979

(NASA-CP-2094; A-7894) Avail: NTIS HC A13/MF A01 CSCL

01C

CONFERENCES, FIREBREAKS, FIREPROOFING, FIRES,

FLAMMABILITY, NONFLAMMABLE MATERIALS

N79-33171"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

PROCEDURES FOR ESTIMATING THE FREQUENCY OF

COMMERCIAL AIRLINE FLIGHTS ENCOUNTERING HIGH

CABIN OZONE LEVELS

J. D. HOLDEMAN Oct. 1979 56 p refs

(NASA-TP-1560; E-9991) Avail: NTIS HC A04/MF A01 CSCL

01C

AIRCRAFT COMPARTMENTS, COMMERCIAL AIRCRAFT,

OZONE

03 AIR TRANSPORTATION AND SAFETY

N80-13013"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

WEAR, FRICTION, AND TEMPERATURE CHARACTERISTICS

OF AN AIRCRAFT TIRE UNDERGOING BRAKING AND

CORNERING

J. L. MCCARTY, T. J. YAGER, and S. R. RICCITIELLO (NASA.

Ames Res. Center) Washington Dec. 1979 40 p refs

(NASA-TP-1569; L-13239) Avail: NTIS HC A03/MF A01

CSCL 01C

AIRCRAFT TIRES, BRAKING, KINETIC FRICTION, WEAR

TESTS

N80-22283"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

RESOURCE MANAGEMENT ON THE FLIGHT DECK

G. E. COOPER, ed., M D. WHITE, ed. (Cooper (George E.),

Saratoga, Calif.), and J. K. LAUBER, ed. Mar, 1980 247 p

refs Proceedings of a NASA/Industry Workshop, San Francisco,

26-28 Jun. 1979

(NASA-CP-2120) Avail: NTIS HC A11/MF A01 CSCL 05J

CONFERENCES, FLIGHT CREWS, FLIGHT TRAINING,

PERSONNEL MANAGEMENT, PILOT PERFORMANCE, PILOT

SELECTION

N80-27302"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

TIRE STIFFNESS AND DAMPING DETERMINED FROM STATIC

AND FREE-VIBRATION TESTS

R. K SLEEPER and R. C. DREHER Jul. 1980 45 p refs

(NASA-TP-1671; L-13500) Avail: NTIS HC A03/MF A01

CSCL 01C

AIRCRAFT TIRES, DAMPING, DYNAMIC TESTS, RESILIENCE,

STATIC TESTS, STIFFNESS, VIBRATION TESTS

N81-12043"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

A SIMULATOR STUDY FOR THE DEVELOPMENT AND

EVALUATION OF OPERATING PROCEDURES ON A

SUPERSONIC CRUISE RESEARCH TRANSPORT TO MINIMIZE

AIRPORT-COMMUNITY NOISE

W. D. GRANTHAM, P. M SMITH (Kentron International, Inc.,

Hampton, Va.), and P. L. DEAL Nov. 1980 79 p refs

(NASA-TP-1742; L-13881) Avail: NTIS HC A05/MF A01

CSCL 01C

FLIGHT SIMULATION, JET AIRCRAFT NOISE, LANDING,

NOISE REDUCTION, SUPERSONIC AIRCRAFT, TAKEOFF

RUNS

N81-19035"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

THE 1980 AIRCRAFT SAFETY AND OPERATING PROBLEMS,

PART 1

J. W. STICKLE, comp. Mar. 1981 380 p refs Conf. held in

Hampton, Va., 5-7 Nov. 1980 2 Vol.

(NASA-CP-2170-PT-1; L-14254) Avail: NTIS HC A17/MF A01

CSCL 01C

AERONAUTICAL ENGINEERING, AIRCRAFT SAFETY,

CONFERENCES, FLIGHT CONTROL, NASA PROGRAMS,

OPERATIONAL PROBLEMS

N81-19056"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

THE 1980 AIRCRAFT SAFETY AND OPERATING PROBLEMS,

PART 2

J. W. STICKLE, comp. Mar. 1981 390 p refs Conf. held at

Hampton, Va., 5-7 Nov. 1980 2 Vol.

(NASA-CP-2170-PT-2; L-14254) Avail: NTIS HC A17/MF A01

CSCL 01C

ACOUSTICS, AVIONICS, CONFERENCES, FLIGHT TESTS,

HUMAN FACTORS ENGINEERING, NOISE REDUCTION,

TERMINAL FACILITIES

29
03 AIR TRANSPORTATION AND SAFETY

N81-_J109*# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECT OF DISPLAY SIZE ON UTILIZATION OF TRAFFIC

SITUATION DISPLAY FOR SELF-SPACING TASK

T. S. ABBOTT and G. C. MOEN (Army Aviation Research and

Development Command, Hampton, Va.) Aug. 1981 30 p refs

(DA PROJ. 1L2-62209-AH-76)

(NASA-TP-1885; L-14418; AVRADCOM-TR-81-B-4) Avail: NTIS

HC A03/MF A01 CSCL 17G

AIR TRAFFIC CONTROL, AIRCRAFT APPROACH SPACING,

DISPLAY DEVICES, SIZE (DIMENSIONS), TRANSPORT

AIRCRAFT

N81-30101"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

GUIDELINES FOR LINE-ORIENTED FLIGHT TRAINING,

VOLUME 1

J. K. LAUBER and H. C. FOUSHEE Aug. 1981 46 p refs

Proceedings of NASA/Industry Workshop, Moffett Field, Calif.,

13-15 Jan. 1981

(NASA-CP-2184; A-8585-VOL-1) Avail: NTIS HC A03/MF A01

CSCL 01C

COMMAND AND CONTROL, FLIGHT SIMULATION, PILOT

TRAINING, RESOURCES MANAGEMENT

N81-31162"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

INFORMATION TRANSFER PROBLEMS IN THE AVIATION

SYSTEM

C. E. BILLINGS, ed. and E. S. CHEANEY, ed. Sep. 1981 95 p

refs

(NASA-TP-1875; A-8567) Avail: NTIS HC A05/MF A01 CSCL

17B

GROUND-AIR-GROUND COMMUNICATION, HUMAN PERFORMANCE, VOICE COMMUNICATION

N82-13123"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

GUIDELINES FOR LINE-ORIENTED FLIGHT TRAINING,

VOLUME 2

J. K. LAUBER and H. C. FOUSHEE 1981 156 p refs

Proceedings of conf. held at NASA Ames Research Center, Calif.,

13-15 Jan. 1981

(NASA-CP-2184-VOL-2) Avail: NTIS HC A08/MF A01 CSCL

051

CIVIL AVIATION, CONFERENCES, FLIGHT CREWS, FLIGHT

TRAINING, TRAINING SIMULATORS

N82-23208"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

HELICOPTER HANDLING QUALITIES

Apr. 1982 243 p refs Proceedings of the special meeting

held at Moffett Field, Calif., 14-15 Apr. 1982; sponsored by the

American Helicopter Society

(NASA-CP-2219; A-8891; NAS 1.55:2219) Avail: NTIS HC

A11/MFA01 CSCL01C

AIRCRAFT SPECIFICATIONS, AVIONICS, COCKPITS,

CONFERENCES, CONTROLLABILITY, HELICOPTER CONTROL,

MANEUVERABILITY, NAP-OF-THE-EARTH NAVIGATION, NIGHT

FLIGHTS (AIRCRAFT)

N83-14077"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

LIGHTNING ATTACHMENT PATTERNS AND FLIGHT

CONDITIONS FOR STORM HAZARDS, 1980

B. D. FISHER, G. L KEYSER, JR. (Air Force Systems Liaison

Office, Langley, Va.), and P. L. DEAL Dec. 1982 71 p refs

Prepared in cooperation with Lightning Technologies, Inc.

(NAS1-15884)

(NASA-TP-2087; L-15438; NAS 1.60:2087) Avail: NTIS HC

A04/MF A01 CSCL 01C

F-106 AIRCRAFT, FLIGHT TESTS, LIGHTNING, STORM

DAMAGE, THUNDERSTORMS

30

N83-34921"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

CRASH TESTS OF THREE IDENTICAL LOW-WING

SINGLE-ENGINE AIRPLANE

C. B. CASTLE and E. ALFARO-BOU Sep. 1983 39 p refs

(NASA-TP-2190; L-1560t; NAS 1.60:2190) Avail: NTIS HC

A03/MF A01 CSCL 01C

AIRCRAFT SAFETY, CONCRETES, CRASHES, GENERAL

AVIATION AIRCRAFT, SOILS

N85-18009"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

FLIGHT TRAINING TECHNOLOGY FOR REGIONAL/COMMUTER

AIRLINE OPERATIONS: REGIONAL AIRLINE ASSOCIATION/

NASA WORKSHOP PROCEEDINGS

A. T. LEE, ed. and J. K. LAUBER, ed. Dec. 1984 253 p refs

Workshop held at Moffett Field, Calif., 28-30 Sep. 1983

(NASA-CP-2348; A-9863; NAS 1.55:2348) Avail: NTIS HC

A12/MF A01 CSCL 051

CIVIL AVIATION, CONFERENCES, FLIGHT SAFETY, FLIGHT

TRAINING, MANAGEMENT, PILOT TRAINING

N85-32101"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

SIMULATION STUDIES OF TIME-CONTROL PROCEDURES FOR

THE ADVANCED AIR TRAFFIC CONTROL SYSTEM

L. TOBIAS, M. ALCABIN, H. ERZBERGER, and P. J. OBRIEN

Jul. 1985 18 p refs

(NASA-TP-2493; T-3309; NAS 1.60:2493) Avail: NTIS HC

A02/MF A01 CSCL 01C

AIR TRAFFIC CONTROL, AIRCRAFT EQUIPMENT, AIRCRAFT

GUIDANCE, COMPUTERIZED SIMULATION, GROUND BASED

CONTROL, SCHEDULING

04

AIRCRAFT COMMUNICATIONS AND NAVIGATION

Includes digital and voice communication with aircraft; air navigation

systems (satellite and ground based); and air traffic control.

N80-13020"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EXPERIMENTAL DETERMINATION OF POSITION-ESTIMATE

ACCURACY USING BACK-AZIMUTH SIGNALS FROM A

MICROWAVE LANDING SYSTEM

C. E. KNOX Dec. 1979 37p

(NASA-TP-1574; L-13074) Avail: NTIS HC A03/MF A01

CSCL 17G

MICROWAVE LANDING SYSTEMS, NAVIGATION AIDS,

POSITION (LOCATION)

N80-28329"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

ALGORITHM FOR FIXED-RANGE OPTIMAL TRAJECTORIES

H. Q. LEE and H. ERZBERGER Jul. 1980 86 p refs

(NASA-TP-1565; A-8003) Avail: NTIS HC A05/MF A01 CSCL

17G

ALGORITHMS, COMPUTER PROGRAMS, COST REDUCTION,

HAMILTONIAN FUNCTIONS, TRAJECTORY OPTIMIZATION
05 AIRCRAFT DESIGN, TESTING AND PERFORMANCE

N81-29111"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EVALUATION OF MICROWAVE LANDING SYSTEM (MLS)

EFFECT ON THE DELIVERY PERFORMANCE OF A FIXED-PATH

METERING AND SPACING SYSTEM

L. CREDEUR, C. M. DAVIS (Research Triangle Inst., Research

Triangle Park, NC.), and W. R. CAPRON (Kentron International,

Inc., Hampton, Va.) Aug. 1981 132 p refs

(NASA-TP-1844; L-14069) Avail: NTIS HC A07/MF A01

CSCL 17G

AIRCRAFT APPROACH SPACING, AREA NAVIGATION,

MICROWAVE LANDING SYSTEMS

N82-22239"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECTS OF CABLE GEOMETRY AND AIRCRAFT ATTITUDE

ON THE ACCURACY OF A MAGNETIC LEADER CABLE SYSTEM

FOR AIRCRAFT GUIDANCE DURING ROLLOUT AND

TURNOFF

W. T. BUNDICK Apr. 1982 32 p refs

(NASA-TP-1978; L-14975; NAS 1.60:1978) Avail: NTIS HC

A03/MF A01 CSCL 17G

AIRCRAFT CONTROL, AIRCRAFT GUIDANCE, MAGNETIC

CONTROL, TAXIING, TECHNOLOGY ASSESSMENT

N84-17165"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

A COMPARISON OF TWO POSITION ESTIMATE ALGORITHMS

THAT USE ILS LOCALIZER AND DME INFORMATION.

SIMULATION AND FLIGHT TEST RESULTS

C. E. KNOX, D. D. VICROY, and C. SCANLON (Arkansas State

Univ.) Feb. 1984 39 p refs

(NASA-TP-2281; L-15711; NAS 1.60:2281) Avail: NTIS HC

A03/MF A01 CSCL 17G

AIRCRAFT GUIDANCE, ALGORITHMS, APPROACH, AREA

NAVIGATION, FLIGHT TESTS, INSTRUMENT LANDING

SYSTEMS

N85-14806"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

TECHNICAL WORKSHOP: ADVANCED HELICOPTER COCKPIT

DESIGN

J. C. HEMINGWAY, ed. and G. P. CALLAS, edo Dec. 1984

346 p refs Workshop held at Moffett Field, Calif., 26-28 Jul.

1983

(NASA-CP-2351; REPT-85057; NAS 1.55:2351) Avail: NTIS HC

A15/MFA01 CSCL01D

COCKPITS, CONFERENCES, HELICOPTERS, HUMAN

FACTORS ENGINEERING, MAN MACHINE SYSTEMS,

SOFTWARE ENGINEERING, STRUCTURAL DESIGN CRITERIA

N82-23233"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ANALYSIS AND MONTE CARLO SIMULATION OF

NEAR-TERMINAL AIRCRAFT FLIGHT PATHS

J. R. SCHIESS and C. G. MATTHEWS (Computer Sciences

Corp.) Apr. 1982 39 p refs

(NASA-TP-1997; L-15062; NAS 1.60:1997) Avail: NTIS HC

A03/MF A01 CSCL 17G

AIR TRAFFIC CONTROL, AIRCRAFT LANDING, AIRPORTS,

FLIGHT PATHS, PARAMETER IDENTIFICATION, TAKEOFF

N83-18704"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

HELICAL AUTOMATIC APPROACHES OF HELICOPTERS WITH

MICROWAVE LANDING SYSTEMS

J. D. FOSTER, L. A. MCGEE, and D. C. DUGAN Dec. 1982

89 p refs

(NASA-TP-2109; A-9034; NAS 1.60:2109) Avail: NTIS HC

A05/MF A01 CSCL 17G

AIR TRAFFIC CONTROL, ALL-WEATHER LANDING

SYSTEMS, APPROACH CONTROL, AUTOMATIC LANDING

CONTROL, FLIGHT TESTS, HELICOPTERS, MICROWAVE

LANDING SYSTEMS

N83-29193"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

DEVELOPMENT AND EVALUATION OF A KALMAN-FILTER

ALGORITHM FOR TERMINAL AREA NAVIGATION USING

SENSORS OF MOOERATE ACCURACY

G. KANNING, L. S. CICOLANI, and S. F. SCHMIDT (Analytical

Mechanics Associates, Inc., Mountain View, Calif.) Jul. 1983

147 p refs

(NASA-TP-2035; A-8955; NAS 1.60:2035) Avail: NTIS HC

A07/MF A01 CSCL 17G

AREA NAVIGATION, AUTOMATIC FLIGHT CONTROL,

DIGITAL NAVIGATION, KALMAN FILTERS, SYSTEMS

SIMULATION, TRAJECTORIES

05

AIRCRAFT DESIGN, TESTING AND

PERFORMANCE

Includes aircraft simulation technology.

N78-10048"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

MEASUREMENT OF MODEL AEROELASTIC DEFORMATIONS

IN THE WIND TUNNEL AT TRANSONIC SPEEDS USING

STEREOPHOTOGRAMMETRY

J. D. BROOKS and J. K. BEAMISH (General Dynamics Corp.,

Fort Worth, Tex.) 1977 43 p refs

(NASA-TP-1010; L-11092) Avail: NTIS HC A03/MF A01

CSCL 01C

AEROELASTICITY, ELASTIC DEFORMATION, STEREOPHOTOGRAPHY

N78-10049"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

VALIDATION OF A FLEXIBLE AIRCRAFT TAKE-OFF AND

LANDING ANALYSIS (FATOLA)

H. D. CARDEN and J. R. MCGEHEE 1977 68 p refs

(NASA-TP-1025; L-lt704) Avail: NTIS HC A04/MF A01

CSCL 01C

AIRCRAFT LANDING, COMPUTER PROGRAMS, TAKEOFF

N78-11053"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

WIND-TUNNEL TESTS OF WIDE-CHORD TEETERING ROTORS

WITH AND WITHOUT OUTBOARD FLAPPING HINGES

W. H. WELLER (Army Aviat. Res. and Develop. Command, St.

Louis, Mo.) and B. L. LEE Washington Nov. 1977 76 p refs

(DA PROJ. 1L2-62209-AH-76)

(NASA-TP-1046; L-11749) Avail: NTIS HC A06/MF A01

CSCL 01C

ROTARY WINGS, ROTOR AERODYNAMICS, TEETERING,

WIND TUNNEL TESTS

31
05 AIRCRAFT DESIGN, TESTING AND PERFORMANCE

N78-13043"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

FRICTION CHARACTERISTICS OF THREE 30 BY 11.5-14.5,

TYPE 8, AIRCRAFT TIRES WITH VARIOUS TREAD GROOVE

PATTERNS AND RUBBER COMPOUNDS

T. J. YAGER and J. L. MCCARTY Dec. 1977 25 p refs

(NASA-TP-1080; L-11808) Avail: NTIS HC A02/MF A01

CSCL 11G

AIRCRAFT TIRES, FRICTION MEASUREMENT, RUBBER,

TREADS

N78-16042"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

GEMPAK: AN ARBITRARY AIRCRAFT GEOMETRY

GENERATOR

S. H STACK, C. L. W. EDWARDS, and W. J. SMALL Dec.

1977 t67 p refs

(NASA-TP-1022; L-11666) Avail: NTIS HC A08/MF A01

CSCL 01C

AIRCRAFT DESIGN, BODY-WING AND TAIL

CONFIGURATIONS, COMPUTER PROGRAMS, REPORT

GENERATORS

N78-18044"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

A FLIGHT EVALUATION OF A TRAILING ANEMOMETER FOR

LOW-SPEED CALIBRATIONS OF AIRSPEED SYSTEMS ON

RESEARCH AIRCRAFT

B. D. FISHER, B. J. HOLMES, and H P. STOUGH, Ill Feb.

1978 62 p refs

(NASA-TP-1135; L-11960) Avail: NTIS HC A04/MF A01

CSCL 01C

AIRSPEED, ANEMOMETERS, CALIBRATING, FLIGHT TESTS,

LOW SPEED, RESEARCH AIRCRAFT

N78-20114"# National Aeronautics and Space Administration.

Dryden (Hugh L.) Flight Research Center, Edwards, Calif.

DEVELOPMENT OF SYSTEMS AND TECHNIQUES FOR

LANDING AN AIRCRAFT USING ONBOARD TELEVISION

S. W. GEE, P. C. CARR, W. R. WINTER, and J. A. MANKE Feb.

1978 24 p refs

(NASA-TP-1171; H-973) Avail: NTIS HC A02/MF A01 CSCL

01C

AIRCRAFT LANDING, F-15 AIRCRAFT, INSTRUMENT

LANDING SYSTEMS, REMOTELY PILOTED VEHICLES,

TELEVISION SYSTEMS

N78-20115°# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

GROUND DISTANCE COVERED DURING AIRBORNE

HORIZONTAL DECELERATION OF AN AIRPLANE

W.H. PHILLIPS Apr. 1978 13 p refs

(NASA-TP-1157; L-12008) Avail: NTIS HC A02/MF A01

CSCL 01C

AIRCRAFT LANDING, DECELERATION, GENERAL AVIATION

AIRCRAFT, LANDING LOADS, LANDING SPEED

N78-25079"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

PRELIMINARY STUDY OF A LARGE SPAN-DISTRIBUTED-LOAD

FLYING-WING CARGO AIRPLANE CONCEPT

L, S. JERNELL May 1978 105 p refs

(NASA-TP-1158; L-11943) Avail: NTIS HC A06/MF A01

CSCL 01C

AERODYNAMIC CHARACTERISTICS, AIRCRAFT DESIGN,

CARGO AIRCRAFT, DESIGN ANALYSIS, SPANLOADER

AIRCRAFT, WING LOADING

N78-27111"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

GROUND-BASED AND IN-FLIGHT SIMULATOR STUDIES OF

LOW-SPEED HANDLING CHARACTERISTICS OF TWO

SUPERSONIC CRUISE TRANSPORT CONCEPTS

W. D. GRANTHAM, L. T. NGUYEN, P. L. DEAL, M. J. NEUBAUER,

P. M. SMITH (Vought Corporation Hampton Technical Center,

Hampton, Va.), and F. D. GREGORY Jul. 1978 101 p refs

(NASA-TP-1240; L-t2t65) Avail: NTIS HC A06/MF A01

CSCL 01C

APPROACH CONTROL, CONTROLLABILITY, LANDING, LOW

SPEED STABILITY, SUPERSONIC TRANSPORTS

N78-27113"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

APPLICATION OF SPECIAL-PURPOSE DIGITAL COMPUTERS

TO ROTORCRAFT REAL-TIME SIMULATION

D. B. MACKIE and S. MICHELSON (Computer Sci. Corp., Mountain

View, Calif.) Jul. 1978 37 p refs

(NASA-TP-1267; A-7343) Avail: NTIS HC A03/MF A01 CSCL

01C

CASCADE CONTROL, COMPUTERIZED SIMULATION,

FORTRAN, ROTORCRAFT AIRCRAFT

N78-30089"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EVALUATION OF SEVERAL SECONDARY TASKS IN THE

DETERMINATION OF PERMISSIBLE TIME DELAYS IN

SIMULATOR VISUAL AND MOTION CUES

G. K. MILLER, JR. and D. R. RILEY Aug. 1978 68 p refs

(NASA-TP-1214; L-12006) Avail: NTIS HC A04/MF A01

CSCL 05H

AUDITORY TASKS, FLIGHT SIMULATORS, TIME LAG,

TRACKING (POSITION), VISUAL TASKS

N78-30090"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SIMULATOR STUDY OF THE EFFECT OF VISUAL-MOTION TIME

DELAYS ON PILOT TRACKING PERFORMANCE WITH AN

AUDIO SIDE TASK

D. R. RILEY and G. K. MILLER, JR. Aug. 1978 74 p refs

(NASA-TP-1216; L-11996) Avail: NTIS HC A04/MF A01

CSCL 05H

AUDITORY TASKS, FLIGHT SIMULATORS, MOTION

PERCEPTION, PILOT PERFORMANCE, TIME LAG, VISUAL

PERCEPTION

N79-14082"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

EFFECTS OF VISUAL AND MOTION SIMULATION CUEING

SYSTEMS ON PILOT PERFORMANCE DURING TAKEOFFS

WITH ENGINE FAILURES

B. L. PARRIS and A. M. COOK Dec. 1978 85 p

(NASA-TP-1365; A-7352) Avail: NTIS HC A05/MF A01 CSCL

05H

CUES, DATA PROCESSING, ENGINE FAILURE, MOTION

SIMULATORS, PILOT PERFORMANCE, VISUAL SIGNALS

N79-14083"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

DEVELOPMENT AND VALIDATION OF A PILOTED SIMULATION

OF A HELICOPTER AND EXTERNAL SLING LOAD

J. D. SHAUGHNESSY, T. N. DEAUX (Sperry Support Services,

Hampton, Va.), and K. R YENNI Jan. 1979 113 p refs

(NASA-TP-1285; L-11925) Avail: NTIS HC A06/MF A01

CSCL 01C

CH-54 HELICOPTER, FLIGHT SIMULATION, MATHEMATICAL

MODELS, PILOT PERFORMANCE, SUSPENSION SYSTEMS

(VEHICLES)

32
05 AIRCRAFTDESIGN,TESTINGANDPERFORMANCE

N79-15938"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EXPERIMENTAL INVESTIGATION OF EFFECTS OF BLADE TIP

GEOMETRY ON LOADS AND PERFORMANCE FOR AN

ARTICULATED ROTOR SYSTEM

W. H. WELLER (Army Aviation Research and Development

Command, St. Louis, Mo.) Jan. 1979 79 p refs

(DA PROJ. 1L2-62209-AH-76)

(NASA-TP-1303; L-12153; AVRADCOM-TR-78-53) Avail: NTIS

HC A05/MF A01 CSCL 01C

BLADE TIPS, ROTARY WINGS, WIND TUNNEL TESTS

N79-29171"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

FRICTION AND WEAR CHARACTERISTICS OF WIRE-BRUSH

SKIDS

R. C. DREHER Aug. 1979 30 p refs

(NASA-TP-1495; L-13095) Avail: NTIS HC A03/MF A01

CSCL 01C

FRICTION, SKIDDING, WEAR

N79-30176"# National Aeronautics and Space Administration.

Dryden (Hugh L.) Flight Research Center, Edwards, Calif.

SIMILITUDE REQUIREMENTS AND SCALING RELATIONSHIPS

AS APPLIED TO MODEL TESTING

C. H. WOLOWICZ, J. S. BROWN, JR., and W. P. GILBERT Aug.

1979 64 p refs Prepared jointly with NASA. Langley Res.

Center

(NASA-TP-1435; H-1022) Avail: NTIS HC A04/MF A01 CSCL

01C

AIRCRAFT MODELS, FLIGHT CHARACTERISTICS,

PARAMETERIZATION, SCALE MODELS, SIMILITUDE LAW, WIND

TUNNEL MODELS, WIND TUNNEL TESTS

N79-33189"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECT OF IMAGE TILT OF A VIRTUAL IMAGE DISPLAY ON

SIMULATED TRANSPORT TOUCHDOWN PERFORMANCE

R. V. PARRISH, W. M. KAHLRAUM, JR., and G. G. STEINMETZ

Washington Oct. 1979 17 p refs

(NASA-TP-1520; L-13087) Avail: NTIS HC A02/MF A01

CSCL 01C

AIRCRAFT LANDING, DISPLAY DEVICES, FLIGHT

SIMULATION, FLIGHT SIMULATORS, IMAGE CONVERTERS,

LANDING SIMULATION, TOUCHDOWN

N79-33191"# National Aeronautics and Space Administration.

Wallops Flight Center, Wallops Island, Va.

PROCESSING OF ON-BOARD RECORDED DATA FOR QUICK

ANALYSIS OF AIRCRAFT PERFORMANCE

N. H. MICHAUD Sep. 1979 326 p

(NASA-RP-1043) Avail: NTIS HC A15/MF A01 CSCL 01C

A system of independent computer programs for the processing

of digitized pulse code modulated (PCM) and frequency modulated

(FM) data is described. Information is stored in a set of random

files and accessed to produce both statistical and graphical output.

The software system is designed primarily to present these reports

within a twenty-four hour period for quick analysis of the helicopter's

performance. A.R.H.

N80-10193"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EXPERIMENTS IN SENSING TRANSIENT ROTATIONAL

ACCELERATION CUES ON A FLIGHT SIMULATOR

R. V. PARRISH Oct. 1979 24 p refs

(NASA-TP-1537; L-13030) Avail: NTIS HC A02/MF A01

CSCL 01C

ANGULAR ACCELERATION, FIGHTER AIRCRAFT, FLIGHT

SIMULATION, MOTION PERCEPTION, ROLL

N80-11068"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

WIND-TUNNEL/FLIGHT CORRELATION STUDY OF

AERODYNAMIC CHARACTERISTICS OF A LARGE FLEXIBLE

SUPERSONIC CRUISE AIRPLANE CXB-70-1). I: WIND-TUNNEL

TESTS OF A 0,03-SCALE MODEL AT MACH NUMBERS FROM

O.6 TO 2.53

J. C. DAUGHERTY Nov. 1979 222 p refs

(NASA-TP-1514; A-7712) Avail: NTIS HC A10/MF A01 CSCL

01C

AERODYNAMIC CHARACTERISTICS, AIRCRAFT MODELS,

B-70 AIRCRAFT, WIND TUNNEL TESTS

N80-11069"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

APPLICATION OF MODIFIED PROFILE ANALYSIS TO

FUNCTION TESTING OF SIMULATED CTOL TRANSPORT

TOUCHDOWN-PERFORMANCE DATA

R. V. PARRISH and B. T. MCKISSICK Nov. 1979 19 p refs

(NASA-TP-1541; L-13091) Avail: NTIS HC A02/MF A0t

CSCL 01C

DISPLAY DEVICES, FLIGHT SIMULATION, PILOT

PERFORMANCE, PROFILE METHOD (FORECASTING),

TOUCHDOWN

N80-12084"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

BEHAVIOR OF AIRCRAFT ANTISKID BRAKING SYSTEMS ON

DRY AND WET RUNWAY SURFACES. A

SLIP-VELOCITY-CONTROLLED,

D SYSTEM

S. M. STUBBS, J. A. TANNER, and E. G. SMITH Washington

Dec. 1979 194 p refs

(NASA-TP-1051; L-11760) Avail: NTIS HC A09/MF A01

CSCL 01C

AIRCRAFT BRAKES, AIRCRAFT TIRES, ANTISKID DEVICES,

RUNWAYS

N80-13024"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

APPLICATION OF MODIFIED PROFILE ANALYSIS TO

FUNCTION TESTING OF THE MOTION/NO-MOTION ISSUE IN

AN AIRCRAFT GROUND-HANDLING SIMULATION

R. V. PARRISH, B. T. MCKISSICK, and G. G. STEINMETZ

Washington Dec. 1979 24 p refs

(NASA-TP-1540; L-13028) Avail: NTIS HC AO2/MF A01

CSCL 01C

FLIGHT SIMULATORS, MAN MACHINE SYSTEMS, MOTION

SIMULATORS, STATISTICAL ANALYSIS

N80-13025"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ANALYTICAL INVESTIGATION OF THE LANDING DYNAMICS

OF A LARGE AIRPLANE WITH A LOAD-CONTROL SYSTEM

IN THE MAIN LANDING GEAR

J. R. MCGEHEE and H. D. CARDEN Dec. 1979 85 p refs

(NASA-TP-1555; L-13250) Avail: NTIS HC AO5/MF A01

CSCL 01C

AIRCRAFT PARTS, COMPUTER PROGRAMMING, DYNAMIC

CONTROL, IMPACT LOADS, LANDING GEAR

N80-13026"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EXPLORATORY STUDY OF THE EFFECTS OF

WING-LEADING-EDGE MODIFICATIONS ON THE STALL/SPIN

BEHAVIOR OF A LIGHT GENERAL AVIATION AIRPLANE

Dec. 1979 98p refs

(NASA-TP-1589; L-13143) Avail: NTIS HC A05/MF A01

CSCL 01C

AERODYNAMIC STALLING, AIRCRAFT SPIN, GENERAL

AVIATION AIRCRAFT, LEADING EDGES, LIGHT AIRCRAFT,

WING PROFILES

33
05 AIRCRAFTDESIGN,TESTINGANDPERFORMANCE

N80-15068"# National Aeronautics and Space Administration.

Dryden (Hugh L) Flight Research Center, Edwards, Calif.

LOADING TESTS OF A WING STRUCTURE FOR A HYPERSONIC

AIRCRAFT

R. A. FIELDS, L. F. REARDON, and W. H. SIEGEL Jan. 1980

72 p refs

(NASA-TP-1596; H-1046) Avail: NTIS HC A04/MF A01 CSCL

01C

HYPERSONIC AIRCRAFT, LOAD TESTS, SPOT WELDS, WING

PANELS

N80-15069"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

THE EFFECTS OF MOTION AND G-SEAT CUES ON PILOT

SIMULATOR PERFORMANCE OF THREE PILOTING TASKS

T. W. SHOWALTER and B. L. PARRIS Jan. 1980 45 p refs

(NASA-TP-1601; A-7875) Avail: NTIS HC A03/MF A01 CSCL

01C

ACCELERATION (PHYSICS), C-135 AIRCRAFT, FLIGHT

SIMULATION, MOTION SIMULATORS, PILOT PERFORMANCE

N80-17060"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

COMPARISON OF ANALYTICAL AND FLIGHT TEST IDENTIFIED

AERODYNAMIC DERIVATIVES FOR A TANDEM-ROTOR

TRANSPORT HELICOPTER

W.F. HODGE Feb. 1980 56p refs

(NASA-TP-1581; L-13228) Avail: NTIS HC A04/MF A01

CSCL 01C

AERODYNAMIC CHARACTERISTICS, CH-47 HELICOPTER,

FLIGHT TESTS, STABILITY DERIVATIVES

N80-18028"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

TERMINAL CONFIGURED VEHICLE PROGRAM: TEST

FACILITIES GUIDE

Washington 1980 67 p refs

(NASA-SP-435) Avail: NTIS HC A04/MF A01 CSCL 01C

The terminal configured vehicle (TCV) program was established

to conduct research and to develop and evaluate aircraft and

flight management system technology concepts that will benefit

conventional take off and landing operations in the terminal area.

Emphasis is placed on the development of operating methods for

the highly automated environment anticipated in the future. The

program involves analyses, simulation, and flight experiments. Flight

experiments are conducted using a modified Boeing 737 airplane

equipped with highly flexible display and control equipment and

an aft flight deck for research purposes. The experimental systems

of the Boeing 737 are described including the flight control

computer systems, the navigation/guidance system, the control

and command panel, and the electronic display system. The ground

based facilities used in the program are described including the

visual motion simulator, the fixed base simulator, the verification

and validation laboratory, and the radio frequency anechoic

facility. A.W.H.

N80-21317"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SIMULATOR STUDY OF THE EFFECT OF CONTROL-SYSTEM

TIME DELAYS ON THE OCCURRENCE OF PILOT-INDUCED

OSCILLATIONS AND ON PILOT TRACKING PERFORMANCE

WITH A SPACE-SHUTTLE-ORBITER CONFIGURATION

D. R. RILEY and G. K. MILLER, JR. Apr. 1980 91 p refs

(NASA-TP-1588; L-13131) Avail: NTIS HC A05/MF A01

CSCL 01C

APPROACH AND LANDING TESTS (STS), HUMAN FACTORS

ENGINEERING, SPACE SHUTTLE ORBITERS, SPACE

TRANSPORTATION SYSTEM, SPACECRAFT CONTROL

N80-21318"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

PARAMETRIC STUDY OF VARIATION IN CARGO-AIRPLANE

PERFORMANCE RELATED TO PROGRESSION FROM

CURRENT TO SPANLOADER DESIGNS

T. A. TOLL Washington Apr. 1980 53 p refs

(NASA-TP-t625; L-13208) Avail: NTIS HC A04/MF A01

CSCL 01C

AIRCRAFT DESIGN, AIRCRAFT PERFORMANCE, CARGO

AIRCRAFT, PAYLOAD MASS RATIO, WING LOADING

N80-24296"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

MEASUREMENT OF AIRCRAFT SPEED AND ALTITUDE

W. GRACEY May 1980 311 p refs

(NASA-RP-1046; L-12610) Avail: NTIS HC A14/MF A01

CSCL 010

Problems involved in measuring speed and altitude with

pressure-actuated instruments (altimeter, airspeed indicator,

true-airspeed indicator, Machmeter, and vertical-speed indicator)

are examined. Equations relating total pressure and static pressure

to the five flight quantities are presented, and criteria for the design

of total and static pressure tubes are given. Calibrations of typical

static pressure installations (fuselage nose, wing tip, vertical fin,

and fuselage vent) are presented, various methods for flight

calibration of these installations are described, and the calibration

of a particular installation by two of the methods is described in

detail. Equations are given for estimating the effects of pressure

lag and leaks. Test procedures for the laboratory calibration of

the five instruments are described, and accuracies of mechanical

and electrical instruments are presented. Operational use of the

altimeter for terrain clearance and vertical separation of aircraft is

discussed, along with flight technical errors and overall altitude

errors of aircraft in cruise operations. Altitude-measuring techniques

based on a variety of properties of the Earth and the atmosphere

are included. Two appendixes present airspeed and altitude tables

and sample calculations for determining the various flight

parameters from measured total and static pressures. R.E.S.

N80-25318"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

LARGE-SCALE WIND-TUNNEL TESTS OF INVERTING FLAPS

ON A STOL UTILITY AIRCRAFT MODEL

T. W. FEISTEL and J. P. MORELLI Jun. t980 56 p refs

(NASA-TP-1696; AVRADCOM-TM-80-A-1; A-7061) Avail: NTIS

HC A04/MF A01 CSCL 01C

FLAPS (CONTROL SURFACES), LIFT AUGMENTATION,

SHORT TAKEOFF AIRCRAFT, WIND TUNNEL TESTS

N80-25321"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EXPERIMENTAL AND ANALYTICAL TRANSONIC FLUTTER

CHARACTERISTICS OF A GEARED-ELEVATOR

CONFIGURATION

C. L. RUHLIN, R. V. DOGGETT, JR., and R. A. GREGORY (Boeing

Commercial Airplane Co., Seattle) Jun. 1980 30 p refs

Revised

(NASA-TP-1666; L-13544) Avail: NTIS HC A03/MF A01

CSCL 01C

ELEVATORS (CONTROL SURFACES), FLUTTER ANALYSIS,

HORIZONTAL TAIL SURFACES, TRANSONIC FLUTTER

N80-29287"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

WIND-TUNNEL EXPERIMENTS ON DIVERGENCE OF

FORWARD-SWEPT WINGS

R. H. RICKETTS and R. V. DOGGEI-I, JR. Aug. 1980 49 p

refs

(NASA-TP-1685; L-13549) Avail: NTIS HC A03/MF A01

CSCL 01C

AEROELASTICITY, FLUTTER, PREDICTION ANALYSIS

TECHNIQUES, SWEPT FORWARD WINGS, WIND TUNNEL

TESTS

34
05 AIRCRAFTDESIGN,TESTINGANDPERFORMANCE

N80-30296"# Nationat Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

CRASH TESTS OF FOUR IDENTICAL HIGH-WING

SINGLE-ENGINE AIRPLANES

V. L. VAUGHAN, JR. and R. J. HAYDUK Aug. 1980 70 p

refs

(NASA-TP-1699; L-13076) Avail: NTIS HC A04/MF A01

CSCL 01C

ATTITUDE (INCLINATION), CRASH LANDING, DAMAGE

ASSESSMENT, FLIGHT PATHS, IMPACT DAMAGE, IMPACT

TESTS

N81o12066"# National Aeronautics and Space Administration.

Dryden (Hugh L.) Flight Research Center, Edwards, Calif.

A MODIFIED T-VALUE METHOD FOR SELECTION OF STRAIN

GAGES FOR MEASURING LOADS ON A LOW ASPECT RATIO

WING

M. H. TANG and R. G. SHELDON Nov. 1980 54 p refs

(NASA-TP-1748; H-1108) Avail: NTIS HC A04/MF A01 CSCL

01C

GRAPHS (CHARTS), LOAD DISTRIBUTION (FORCES),

STRAIN GAGES, TABLES (DATA)

N81-16039"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

USE OF CONSTRAINED OPTIMIZATION IN THE CONCEPTUAL

DESIGN OF A MEDIUM-RANGE SUBSONIC TRANSPORT

S. M. SLIWA Dec. 1980 38 p refs

(NASA-TP-1762; L-13946) Avail: NTIS HC A03/MF A01

CSCL 01C

COST ANALYSIS, DESIGN ANALYSIS, NONLINEAR

PROGRAMMING, OPTIMIZATION, TRANSPORT AIRCRAFT

N81-16040"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

SAMPLE DATA EFFECTS OF HIGH-PASS FILTERS

D. O. CHIN Jan. 1981 32 p refs

(NASA-TP-1797; A-8361) Avail: NTIS HC A03/MF A01 CSCL

01C

DATA PROCESSING EQUIPMENT, HIGH PASS FILTERS,

MATHEMATICAL MODELS, MOTION SIMULATORS

N81-22039"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

KINEMATIC PROPERTIES OF THE HELICOPTER IN

COORDINATED TURNS

R. T. N. CHEN and J. A. JESKE Apr. 1981 41 p refs

(NASA-TP-1773; A-8399) Avail: NTIS HC A03/MF A01 CSCL

01C

ANGLE OF ATTACK, HELICOPTERS, KINEMATIC

EQUATIONS, PITCHING MOMENTS, ROLL, SIDESLIP

N81-24048"# National Aeronautics and Space Administration.

Dryden (Hugh L.) Flight Research Center, Edwards, Calif.

APPLICATION OF A PERFORMANCE MODELING TECHNIQUE

TO AN AIRPLANE WITH VARIABLE SWEEP WINGS

P.C. REDIN May 1981 33 p refs

(NASA-TP-1855; H-1131) Avail: NTtS HC A03/MF A0t CSCL

01C

AIRCRAFT MANEUVERS, AIRCRAFT PERFORMANCE,

COMPUTERIZED SIMULATION, F-111 AIRCRAFT

N81-30112"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

BEHAVIOR OF AIRCRAFT ANTISKID BRAKING SYSTEMS ON

DRY AND WET RUNWAY SURFACES: HYDROMECHANICALLY

CONTROLLED SYSTEM

J. A. TANNER, S. M. STUBBS, and E. G. SMITH Aug. 1981

176 p refs

(NASA-TP-1877; L-14549) Avail: NTIS HC A09/MF A01

CSCL 01C

AIRCRAFT BRAKES, AIRCRAFT TIRES, ANTISKID DEVICES,

RUNWAY CONDITIONS

N8t-31185*# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

VEHICLE CONCEPTS AND TECHNOLOGY REQUIREMENTS

FOR BUOYANT HEAVY-LIFT SYSTEMS

M. D. ARDEMA Sep. 1981 18 p refs

(NASA-TP-1921; A-8022) Avail: NTIS HC AO2/MF A01 CSCL

01C

AIRCRAFT DESIGN, AIRSHIPS, COST ANALYSIS, HEAVY LIFT

HELICOPTERS, TECHNOLOGY ASSESSMENT

N82-11050"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

PARAMETRIC STUDY OF MICROWAVE-POWERED

HIGH-ALTITUDE AIRPLANE PLATFORMS DESIGNED FOR

LINEAR FLIGHT

C. E. K. MORRIS, JR. Nov. 1981 74 p refs

(NASA-TP-1918; L-14606) Avail: NTIS HC A04/MF A01

CSCL 01C

FLYING PLATFORMS, HORIZONTAL FLIGHT, MICROWAVE

TRANSMISSION, PARAMETER IDENTIFICATION, PERFORMANCE PREDICTION, REMOTELY PILOTED VEHICLES

N82-16068"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SPIN TESTS OF A SINGLE-ENGINE, HIGH-WING LIGHT

AIRPLANE

E. C. STEWART, W. T. SUIT, T. M. MOUL, and P. W. BROWN

Jan. 1982 93 p refs

(NASA-TP-1927; Lo14305) Avail: NTIS HC A05/MF A01

CSCL 01C

AERODYNAMIC STALLING, GENERAL AVIATION AIRCRAFT,

SPIN TESTS

N82-18204"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

DYNAMICS OF AIRCRAFT ANTISKID BRAKING SYSTEMS

J. A. TANNER, S. M STUBBS, R. C. DREHER, and E. G. SMITH

Feb. 1982 100 p refs

(NASA-TP-1959; L-14788) Avail: NTIS HC A05/MF A01

CSCL 01C

AIRCRAFT BRAKES, AIRCRAFT TIRES, ANTISKID DEVICES,

BRAKING, DYNAMIC RESPONSE, TORQUE, WHEEL BRAKES

N82-23244"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

PLANAR EQUATIONS OF ROLLOUT MOTION FOR AN

AIRCRAFT WITH FREE OR STEERABLE LANDING GEARS

R. K. SLEEPER and E. G. SMITH May 1982 54 p refs

(NASA-TP-1984; L-11689; NAS 1.60:1984) Avail: NTIS HC

A04/MF A01 CSCL 01C

AIRCRAFT LANDING, EQUATIONS OF MOTION, LANDING

GEAR, ROLL

N82-24193"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

TIRE TREAD TEMPERATURES DURING ANTISKID BRAKING

AND CORNERING ON A DRY RUNWAY

J. A. TANNER, R. C. DREHER, S. M. STUBBS, and E. G. SMITH

May 1982 57p refs

(NASA-TP-2009; L-15110; NAS 1.60:2009) Avail: NTIS HC

04/MF A01 CSCL01C

AIRCRAFT BRAKES, AIRCRAFT TIRES, BRAKING, FRICTION,

SKIDDING, SURFACE TEMPERATURE, TREADS

35
05 AIRCRAFT DESIGN, TESTING AND PERFORMANCE

N82-29311"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

ESTABLISHMENT OF A ROTOR MODEL BASIS

R. E. MCFARLAND Jun. t982 93 p refs Prepared in

cooperation with Army Aviation Research and Development

Command, Moffett Field, Calif.

(NASA-TP-2026; A-8605; NAS 1.60:2026;

AVRADCOM-TR-81-A-14) Avail: NTIS HC A05/MF A01 CSCL

01C

ALGORITHMS, ERROR ANALYSIS, MATHEMATICAL

MODELS, ROTOR AERODYNAMICS, ROTOR BLADES

(TURBOMACHINERY)

N82-31321"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EXPERIMENTAL INVESTIGATION OF ACTIVE LOADS

CONTROL FOR AIRCRAFT LANDING GEAR

J. R. MCGEHEE and R. C. DREHER Aug. 1982 72 p refs

(NASA-TP-2042; L-15224; NAS 1.60:2042) Avail: NTIS HC

A04/MF A01 CSCL01C

DYNAMIC LOADS, HYDRAULIC CONTROL, LANDING GEAR,

VIBRATORY LOADS

N82-32350"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SOME DESIGN CONSIDERATIONS FOR SOLAR-POWERED

AIRCRAFT

W. H. PHILLIPS Jun. 1980 60 p refs

(NASA-TP-1675; L-13562; NAS 1.60:1675) Avail: NTIS HC

A04/MFA01 CSCL01C

AIRCRAFT ENGINES, AIRCRAFT PERFORMANCE, SOLAR

POWERED AIRCRAFT, SOLAR PROPULSION

N83-18714"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

THE VIBRATION CHARACTERISTICS OF A COUPLED

HELICOPTER ROTOR-FUSELAGE BY A FINITE ELEMENT

ANALYSIS

M. J. RUTKOWSKI 1983 76 p refs Prepared in cooperation

with Army Research and Technology Labs.

(NASA-TP-2118; A-9053; NAS 1.60:2118;

AVRADCOM-TR-82-A-15) Avail: NTIS HC A05/MF A01 CSCL

01C

FUSELAGES, HELICOPTERS, HOVERING, ROTARY WINGS,

VIBRATION EFFECTS

N83-18715"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

COMPARISON OF SIMULATOR FIDELITY MODEL

PREDICTIONS WITH IN-SIMULATOR EVALUATION DATA

R. V. PARRISH, B. T. MCKISSICK, and B. R. ASHWORTH Feb.

1983 39p refs

(NASA-TP-2106; L-15519; NAS 1.60:2106) Avail: NTIS HC

AO3/MF A01 CSCL 01C

DIGITAL SYSTEMS, FEEDBACK CONTROL, FLIGHT

SIMULATORS, PILOT TRAINING, REAL TIME OPERATION

N83-20931"# National Aeronautics and Space Administration,

Washington, D.C.

SMALL TRANSPORT AIRCRAFT TECHNOLOGY

L, J. WILLIAMS 1983 118 p refs

(NASA-SP-460; NAS 1.21:460; LC-82-600387) Avail: NTIS MF

A01; SOD HC $5.00 CSCL 01C

Information on commuter airline trends and aircraft

developments is provided to upgrade the preliminary findings of a

NASA-formed small transport aircraft technology (STAT) team,

established to determine whether the agency's research and

development programs could help commuter aircraft manufacturers

solve technical problems related to passenger acceptance and

use of 19- to 50-passenger aircraft. The results and conclusions

of the full set of completed STAT studies are presented. These

studies were performed by five airplane manufacturers, five engine

manufacturers, and two propeller manufacturers. Those portions

of NASA's overall aeronautics research and development programs

which are applicable to commuter aircraft design are summarized.

Areas of technology that might beneficially be expanded or initiated

to aid the US commuter aircraft manufacturers in the evolution of

improved aircraft for the market are suggested. AR.H.

N83-22191"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EVALUATION OF G SEAT AUGMENTATION OF

FIXED-BASE/MOVING BASE SIMULATION FOR TRANSPORT

LANDINGS UNDER TWO VISUALLY IMPOSED RUNWAY WIDTH

CONDITIONS

R. V. PARRISH and G. G. STEINMETZ Apr. 1983 25 p refs

(NASA-TP-2135; L-15540; NAS 1.60:2135) Avail: NTIS HC

AO2/MF A01 CSCL 01C

AIRCRAFT LANDING, LANDING SIMULATION, MOTION

SIMULATORS, RUNWAYS, SEATS, TRANSPORT AIRCRAFT

N83-22192"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

MOTION/VISUAL CUEING REQUIREMENTS FOR VORTEX

ENCOUNTERS DURING SIMULATED TRANSPORT VISUAL

APPROACH AND LANDING

R. V. PARRISH and R. L. BOWLES Apr. 1983 23 p refs

(NASA-TP-2136; L-15544; NAS 1.60:2136) Avail: NTIS HC

A02/MF A01 CSCL 17G

CUES, DISPLAY DEVICES, FLIGHT TESTS, VISUAL

CONTROL, VISUAL PERCEPTION, VORTEX AVOIDANCE,

VORTICES

N83-27977"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

A CONCEPTUAL FRAMEWORK FOR USING DOPPLER RADAR

ACQUIRED ATMOSPHERIC DATA FOR FLIGHT SIMULATION

W. CAMPBELL Jun. 1983 16 p refs

(NASA-TP-2192; NAS 1.60:2192) Avail: NTIS HC A02/MF A01

CSCL 01C

AERODYNAMIC LOADS, ATMOSPHERIC TURBULENCE,

DOPPLER RADAR, FLIGHT SIMULATION, STABILITY

DERIVATIVES, WIND PROFILES

N83-31596"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SERVICE LIFE EVALUATION OF RIGID EXPLOSIVE TRANSFER

LINES

L. J. BEMENT, E. G. KAYSER (NSWC, Silver Spring, Md.), and

M. L. SCHIMMEL (McDonnell Aircraft Co., St. Louis) Aug. 1983

56 p refs Original contains color illustrations

(NASA-TP-2143; L-15558; NAS 1.60:2143) Avail: NTIS HC

A04/MF A01 CSCL01C

ESCAPE SYSTEMS, EXPLOSIVES, FIGHTER AIRCRAFT,

MILITARY OPERATIONS, SERVICE LIFE, TRANSMISSION

LINES

N83-34935"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

BRAKING AND CORNERING STUDIES ON AN AIR CUSHION

LANDING SYSTEM

R. H. DAUGHERTY Sep. 1983 25 p refs

(NASA-TP-2196; L-15640; NAS 1.60:2t96) Avail: NTIS HC

A02/MF A01 CSCL01C

AERODYNAMIC CHARACTERISTICS, AIR CUSHION LANDING

SYSTEMS, BRAKING, STEERING

N84-15144"# National Aeronautics and Space Administration,

Washington, D.C.

FUEL ECONOMY IN AVIATION

J. L. ETHELL 1983 117 p Original contains color illustrations

(NASA-SP-462; NAS 1.21:462) Avail: NTIS MF A01; SOD HC

$15.00 as 033-000-00899-6 CSCL 01C

Engine component improvement, an energy efficient engine,

advanced turboprops, composite structures, energy efficient

transport, and laminar flow control are discussed NW.

36
05 AIRCRAFTDESIGN,TESTINGANDPERFORMANCE

N84-17175"#National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

FRICTION AND WEAR BEHAVIOR OF ALUMINUM AND

COMPOSITE AIRPLANE SKINS

K. E. JACKSON Feb. 1984 28 p refs Prepared in cooperation

with Army Research and Technology Labs., Fort Eustis, Va.

(DA PROJ. 1 L1-61102-AH-45)

(NASA-TP-2262; NAS 1.60:2262; AVSCOM-TR-83-B-7; L-15697)

Avail: NTIS HC A03/MF A01 CSCL 01C

AIRCRAFT CONSTRUCTION MATERIALS, ALUMINUM

ALLOYS, FRICTION, GRAPHITE-EPOXY COMPOSITES, SKIN

(STRUCTURAL MEMBER), WEAR

N84-18189"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECTS OF MOTION BASE AND G-SEAT CUEING OF

SIMULATOR PILOT PERFORMANCE

B. R. ASHWORTH, B. T. MCKISSICK, and R. V. PARRISH Mar.

1984 26p refs

(NASA-TP-2247; L-15559; NAS 1.60:2247) Avail: NTIS HC

AO3/MF A01 CSCL 05t

ACCELERATION (PHYSICS), CUES, FLIGHT SIMULATION,

MOTION SIMULATORS, PILOT PERFORMANCE, SEATS

N85-19979"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

PARAMETRIC STUDY OF A CANARD-CONFIGURED

TRANSPORT USING CONCEPTUAL DESIGN OPTIMIZATION

P. D. ARBUCKLE and S. M. SLIWA Mar. 1985 28 p refs

(NASA-TP-2400; L-15856; NAS 1.60:2400) Avail: NTIS HC

A03/MFA01 CSCL01C

AERODYNAMIC CONFIGURATIONS, AIRCRAFT DESIGN,

CANARD CONFIGURATIONS, TANDEM WING AIRCRAFT

N85-23753"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

RELATIVE CONTROL EFFECTIVENESS TECHNIQUE WITH

APPLICATION TO AIRPLANE CONTROL COORDINATION

F. J. LALLMAN Apr. 1985 18 p refs

(NASA-TP-2416; L-15864; NAS 1.60:2416) Avail: NTIS HC

A02/MFA01 CSCL01C

AIRCRAFT CONTROL, AIRCRAFT STABILITY, DIRECTIONAL

CONTROL, LATERAL CONTROL, OPTIMIZATION, THRUST

VECTOR CONTROL

N84-19333"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

AN ASSESSMENT OF THE CAPABILITY TO CALCULATE

TILTING PROP-ROTOR AIRCRAFT PERFORMANCE, LOADS

AND STABILITY

W. JOHNSON Mar. 1984 25 p refs

(NASA-TP-2291; A-9411; NAS 1.60:2291) Avail: NTIS HC

A02/MF A01 CSCL 01C

AEROELASTICITY, AIRCRAFT STABILITY, LOADS (FORCES),

TILT ROTOR RESEARCH AIRCRAFT PROGRAM, XV-15

AIRCRAFT

N85-25248"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

FLIGHT INVESTIGATION OF STALL, SPIN AND RECOVERY

CHARACTERISTICS OF A LOW-WING, SINGLE-ENGINE, T-TAIL

LIGHT AIRPLANE

H_ P. STOUGH, III, D. J. DICARLO, and J. M PATTON, JR. May

1985 98 p refs

(NASA-TP-2427; L-15868; NAS 1.60:2427) Avail: NTIS HC

A05/MFA01 CSCL01C

AERODYNAMIC STALLING, AERONAUTICS, AIRCRAFT SPIN,

ANGULAR MOMENTUM, SPIN DYNAMICS

N84-31111"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

RESULTS OF THE FIRST COMPLETE STATIC CALIBRATION

OF THE RSRA ROTOR-LOAD-MEASUREMENT SYSTEM

C. W. ACREE, JR. Aug. 1984 57 p refs

(NASA-TP-2327; A-9593; NAS 1.60:2327) Avail: NTIS HC

A04/MF A01 CSCL 01C

CALIBRATING, ERRORS, HYSTERESIS, ROTOR SYSTEMS

RESEARCH AIRCRAFT, STATIC LOADS

N84-32378"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

VALIDATION OF AN ACTIVE GEAR, FLEXIBLE AIRCRAFT

TAKE-OFF AND LANDING ANALYSIS (AGFATL)

J. R. MCGEHEE Sep_ 1984 31 p refs

(NASA-TP-2353; L-15807; NAS 1.60:2353) Avail: NTIS HC

A03/MF A01 CSCL 01C

ACTIVE CONTROL, AIRFRAMES, COMPUTER PROGRAMS,

LANDING GEAR, STRUCTURAL FAILURE, TAKEOFF

N85-12884"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

FLIGHT AND WIND-TUNNEL COMPARISONS OF THE

INLET-AIRFRAME INTERACTION OF THE F-15 AIRPLANE

L. D. WEBB, D. ANDRIYICH-VARDA, and S. A. WHITMORE Nov.

1984 35 p refs

(NASA-TP-2374; H-1175; NAS 1.60:2374) Avail: NTIS HC

A03/MF A01 CSCL 01C

FLIGHT TESTS, FORCE DISTRIBUTION, INLET AIRFRAME

CONFIGURATIONS, PRESSURE DISTRIBUTION, WIND TUNNEL

TESTS

N85-33116"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ENERGY EFFICIENT TRANSPORT TECHNOLOGY: PROGRAM

SUMMARY AND BIBLIOGRAPHY

D. B. MIDDLETON, D. W. BARTLETT, and R. V. HOOD Sep.

1985 54p refs

(NASA-RP-1135; L-15921; NAS 1.61:1135) Avail: NTIS HC

A04/MF A01 CSCL 01C

The Energy Efficient Transport (LET) Program began in 1976

as an element of the NASA Aircraft Energy Efficiency (ACEE)

Program. The LET Program and the results of various applications

of advanced aerodynamics and active controls technology (ACT)

as applicable to future subsonic transport aircraft are discussed.

Advanced aerodynamics research areas included high aspect ratio

supercritical wings, winglets, advanced high lift devices, natural

laminar flow airfoils, hybrid laminar flow control, nacelle

aerodynamic and inertial loads, propulsion/airframe integration

(e.g., long duct nacelles) and wing and empennage surface

coatings. In depth analytical/trade studies, numerous wind tunnel

tests, and several flight tests were conducted. Improved

computational methodology was also developed. The active control

functions considered were maneuver load control, gust load

alleviation, flutter mode control, angle of attack limiting, and pitch

augmented stability. Current and advanced active control laws were

synthesized and alternative control system architectures were

developed and analyzed. Integrated application and fly by wire

implementation of the active control functions were design

requirements in one major subprogram. Additional LET research

included interdisciplinary technology applications, integrated energy

management, handling qualities investigations, reliability

calculations, and economic evaluations related to fuel savings and

cost of ownership of the selected improvements. Author

37
05 AIRCRAFT DESIGN, TESTING AND PERFORMANCE

N86-13316"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ABRASION BEHAVIOR OF ALUMINUM AND COMPOSITE SKIN

COUPONS, STIFFENED SKINS AND STIFFENED PANELS

REPRESENTATIVE OF TRANSPORT AIRPLANE STRUCTURES

K. E. JACKSON Nov. 1985 33 p refs

(DA PROJ. 1 L1-61102-AH-45)

(NASA-TP-2520; L- 18018; NAS 1.60:2520; AVSCOM-TR-85-B-7)

Avail: NTiS HC A03/MF A01 CSCL 01C

ABRASION, ALUMINUM, CRASH LANDING,

GRAPHITE-EPOXY COMPOSITES, PANELS, RUNWAYS, SKID

LANDINGS, SKIN (STRUCTURAL MEMBER), TRANSPORT

AIRCRAFT

N86-15280"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

ROTORCRAFT DYNAMICS 1984

Nov. 1985 497 p refs Proceedings of the 2d Decennial

Specialists' Meeting on Rotorcraft Dynamics, Moffett Field, Calif.,

7-9 Nov. 1984; sponsored by NASA. Ames Research Center and

the American Helicopter Society

(NASA-CP-2400; REPT-85122; NAS 1.55:2400) Avail: NTIS HC

A21/MF A01 CSCL 01C

AERODYNAMIC LOADS, AERODYNAMIC STABILITY,

HELICOPTER DESIGN, HELICOPTER PERFORMANCE, ROTARY

WING AIRCRAFT, VIBRATION

N86-30720"# National Aeronautics and Space Administration,

Washington, D.C.

NASA AND GENERAL AVIATION

J. L. ETHELL 1986 140 p Original contains color illustrations

(NASA-SP-485; NAS 1.21:485) Avail: SOD HC $6.50 as

033-000-00984-4; NTIS MF A01 CSCL 01C

General aviation remains the single most misunderstood sector

of aeronautics in the United States. A detailed look at how general

aviation functions and how NASA helps keep it on the cutting

edge of technology in airfoils, airframes, commuter travel,

environmental concerns, engines, propellers, air traffic control,

agricultural development, electronics, and safety is given. Author

N86-30721"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

IMPACT DATA FROM A TRANSPORT AIRCRAFT DURING A

CONTROLLED IMPACT DEMONSTRATION

E. L. FASANELLA (PRC Kentron, Inc., Hampton, Va.), E.

ALFARO-BOU, and R. J. HAYDUK Sep. 1986 88 p

(NASA-TP-2589; L-16125; NAS 1.60:2589) Avail: NTIS HC

A05/MF A01 CSCL 01B

AIRCRAFT ACCIDENTS, BOEING 720 AIRCRAFT, CRASHES,

CRASHWORTHINESS, IMPACT LOADS, IMPACT TESTS,

STRUCTURAL STABILITY

O6

AIRCRAFT INSTRUMENTATION

Includes cockpit and cabin display devices; and flight instruments.

N78-13054"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

FLIGHT-TEST EVALUATION OF TWO ELECTRONIC DISPLAY

FORMATS FOR APPROACH TO LANDING UNDER

INSTRUMENT CONDITIONS

S. A. MORELLO, C. E. KNOX, and G. G. STEINMETZ Dec.

1977 33 p refs

(NASA-TP-1085; L-11867) Avail: NTIS HC A03/MF A01

CSCL 01D

DISPLAY DEVICES, FLIGHT TESTS, INSTRUMENT LANDING

SYSTEMS

N78-20128"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

A ROTOR-MOUNTED DIGITAL INSTRUMENTATION SYSTEM

FOR HELICOPTER BLADE FLIGHT RESEARCH

MEASUREMENTS

V. H. KNIGHT, JR., W. S. HAYWOOD, JR., and M L. WILLIAMS

Apr. 1978 49 p refs

(NASA-TP-1146; L-11956) Avail: NTIS HC A03/MF A01

CSCL 01D

DIGITAL SYSTEMS, FLIGHT INSTRUMENTS, FLIGHT TESTS,

PRESSURE SENSORS, ROTARY WINGS

N78-31101"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SIMULATION AND FLIGHT EVALUATION OF A HEAD-UP

LANDING AID FOR GENERAL AVIATION

R. L. HARRIS, SR., M W. GOODE, and K. R. YENNI Sep. 1978

38 p refs

(NASA-TP-1276; L-12197) Avail: NTIS HC A03/MF A01

CSCL 01D

FLIGHT SIMULATION, GENERAL AVIATION AIRCRAFT,

HEAD-UP DISPLAYS, LANDING AIDS

N79-23081"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

MINIATURE FLOW-DIRECTION AND AIRSPEED SENSOR FOR

AIRPLANES AND RADIO CONTROLLED MODELS IN SPIN

STUDIES

D. D. KERSHNER May 1979 27 p refs

(NASA-TP-1467; L-12812) Avail: NTIS HC AO3/MF A01

CSCL 01D

AIRCRAFT EQUIPMENT, AIRSPEED, ANGLE OF ATTACK,

FLOW DIRECTION INDICATORS, RADIO CONTROL, REMOTE

SENSORS

N79-33201"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

A REVIEW OF SOME HEAD-UP DISPLAY FORMATS

J. M. NAISH (NAS-NRC) Oct. 1979 51 p refs

(NASA-TP-1499; A-7708; HUD-4) Avail: NTIS HC A04/MF A01

CSCL 01D

FLIGHT INSTRUMENTS, FLIGHT PATHS, FLIGHT TESTS,

HEAD-UP DISPLAYS

N80-23304"# National Aeronautics and Space Administration.

Dryden (Hugh L) Flight Research Center, Edwards, Calif.

WIND TUNNEL INVESTIGATION OF AN ALL FLUSH ORIFICE

AIR DATA SYSTEM FOR A LARGE SUBSONIC AIRCRAFT

T. J. LARSON, S. G. FLECHNER, and P. M. SIEMERS, III May

1980 97 p refs

(NASA-TP-1642; H-1085) Avail: NTIS HC A05/MF A01 CSCL

01D

AIR DATA SYSTEMS, C.135 AIRCRAFT, DATA ACQUISITION,

ORIFICES, PRESSURE MEASUREMENT, SUBSONIC AIRCRAFT

N80-27360"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

FLIGHT INVESTIGATION OF COCKPIT-DISPLAYED TRAFFIC

INFORMATION UTILIZING CODED SYMBOLOGY IN AN

ADVANCED OPERATIONAL ENVIRONMENT

T. S. ABBOTT, G. C. MOEN, L. H. PERSON, JR., G. L. KEYSER,

JR., K. R. YENNI, and J. F. GARREN, JR. Jul. 1980 31 p

refs

(DA PROJ. 1L2-62209-AH-76)

(NASA-TP-1684; AVRADCOM-TR-80-B-4; L-13584) Avail: NTIS

HC A03/MF A01 CSCL 01D

AIR TRAFFIC CONTROL, COLLISION AVOIDANCE, DISPLAY

DEVICES, SYMBOLS

38
N80-28349"#National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

AN EXPERIMENTAL EVALUATION OF HEAD-UP DISPLAY

FORMATS

J. M. NAISH and D. L. MILLER (Informatics, Inc., Palo Alto, Calif.)

Jul. 1980 78p refs

(NASA-TP-1550; A-7970) Avail: NTIS HC A05/MF A01 CSCL

01D

COMPUTERIZED SIMULATION, FLIGHT SIMULATION,

HEAD-UP DISPLAYS, HUMAN FACTORS ENGINEERING

N80-30305"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SIMULATION DEVELOPMENT AND EVALUATION OF AN

IMPROVED LONGITUDINAL VELOCITY VECTOR CONTROL

WHEEL STEERING MODE AND ELECTRONIC DISPLAY

FORMAT

G. G. STEINMETZ Aug. 1980 97 p refs

(NASA-TP-1664; L-13435) Avail: NTIS HC A05/MF A01

CSCL 01D

COMPUTERIZED SIMULATION, DISPLAY DEVICES,

VECTORS (MATHEMATICS), VELOCITY

N80-32389"# National Aeronautics and Space Administration.

Dryden (Hugh L.) Flight Research Center, Edwards, Calif.

USE OF NOSE CAP AND FUSELAGE PRESSURE ORIFICES

FOR DETERMINATION OF AIR DATA FOR SPACE SHUTTLE

ORBITER BELOW SUPERSONIC SPEEDS

T. J. LARSON and P. M. SIEMERS, III (NASA. Langley Research

Center) Sep. 1980 128 p refs

(NASA-TP-1643; H-1096) Avail: NTIS HC A07/MF A01 CSCL

01D

ORIFICE FLOW, PRESSURE GRADIENTS, SPACE SHUTTLE

ORBITERS, SUBSONIC SPEED, TRANSONIC SPEED, WIND

TUNNEL TESTS

N80-33404"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

DEVELOPMENT AND TEST RESULTS OF A FLIGHT

MANAGEMENT ALGORITHM FOR FUEL CONSERVATIVE

DESCENTS IN A TIME-BASED METERED TRAFFIC

ENVIRONMENT

C. E. KNOX and D. G. CANNON (Boeing Commercial Airplane

Co., Seattle) Oct. 1980 50 p refs

(NASA-TP-1717) Avail: NTIS HC A03/MF A01 CSCL 01D

AIR TRAFFIC CONTROL, ALGORITHMS, COMPUTER

PROGRAMS, COMPUTERIZED SIMULATION, FLIGHT TESTS,

FUEL CONSUMPTION

N81-13958"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EVALUATION OF A COMPUTER-GENERATED PERSPECTIVE

TUNNEL DISPLAY FOR FLIGHT PATH FOLLOWING

A. J. GRUNWALD, J. B. ROBERTSON, and J. J. HATFIELD Dec.

1980 100p refs

(NASA-TP-1736; L-13253) Avail: NTIS HC A06/MF A01

CSCL 01D

AIRCRAFT EQUIPMENT, DISPLAY DEVICES, EVALUATION,

FLIGHT CONTROL, PILOT PERFORMANCE, TRAJECTORY

OPTIMIZATION

N81-14997"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SIMULATOR STUDY OF CONVENTIONAL GENERAL AVIATION

INSTRUMENT DISPLAYS IN PATH-FOLLOWING TASKS WITH

EMPHASIS ON PILOT-INDUCED OSCILLATIONS

J.J. ADAMS Dec. 1980 55 p refs

(NASA-TP-1776; L-13785) Avail: NTIS HC A04/MF A01

CSCL 01D

AIRCRAFT INSTRUMENTS, FLIGHT SIMULATION, LATERAL

CONTROL, OSCILLATIONS, PILOT PERFORMANCE, TRACKING

(POSITION)

06 AIRCRAFT INSTRUMENTATION

N81-20074"# National Aeronautics and Space Administration.

Dryden (Hugh L.) Flight Research Center, Edwards, Calif.

DIVERSITY TECHNIQUES FOR OMNIDIRECTIONAL

TELEMETRY COVERAGE OF THE HIMAT RESEARCH

VEHICLE

P. F. HARNEY Mar. 1981 18 p refs

(NASA-TP-1830; H-1133) Avail: NTIS HC A02/MF A01 CSCL

09F

ANTENNA RADIATION PATTERNS, COMMAND AND

CONTROL, OMNIDIRECTIONAL ANTENNAS, RECEPTION

DIVERSITY, REMOTELY PILOTED VEHICLES, TELEMETRY

N81-24058"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

FLIGHT EVALUATION OF A SIMPLE TOTAL ENERGY-RATE

SYSTEM WITH POTENTIAL WIND-SHEAR APPLICATION

A. J. OSTROFF, R. M. HUESCHEN, R. F. HELLBAUM, and J. F.

CREEDON May 1981 52 p refs

(NASA-TP-1854; L-14209) Avail: NTIS HC A04/MF A01

CSCL 01D

AIRCRAFT INSTRUMENTS, KINETIC ENERGY, POTENTIAL

ENERGY, WIND SHEAR

N81-26144"# National Aeronautics and Space Administration.

Dryden (Hugh L.) Flight Research Center, Edwards, Calif.

SUBSONIC TESTS OF AN ALL-FLUSH-PRESSURE-ORIFICE AIR

DATA SYSTEM

T. J. LARSON and P. M SIEMERS, Itl (NASA, Langley Research

Center) Jun. 1981 50 p refs Presented at the 1980 Air

Data Systems Conf.

(NASA-TP-1871; H-t122) Avail: NTIS HC A03/MF A01 CSCL

01D

AIR DATA SYSTEMS, AIRSPEED, FLIGHT TESTS, ORIFICES,

PRESSURE DISTRIBUTION, SUBSONIC SPEED, WIND TUNNEL

TESTS

N81-33203"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SIMULATOR EVALUATION OF SEPARATION OF DISPLAY

PARAMETERS IN PATH-FOLLOWING TASKS

G. R. SARMA and J. J. ADAMS Oct. 1981 44 p refs

(NASA-TP-1915; L-14590) Avail: NTIS HC A03/MF A01

CSCL 01D

AIRCRAFT INSTRUMENTS, DEGREES OF FREEDOM,

INSTRUMENT LANDING SYSTEMS, LATERAL CONTROL

N82-14085"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

A GENERAL AVIATION SIMULATOR EVALUATION OF A

RATE-ENHANCED INSTRUMENT LANDING SYSTEM DISPLAY

D. A. HINTON Dec. 1981 44 p

(NASA-TP-1960; L-13911) Avail: NTIS HC A03/MF A01

CSCL 01D

COCKPIT SIMULATORS, CONTROL SIMULATION, DISPLAY

DEVICES, FLIGHT SIMULATORS, INSTRUMENT LANDING

SYSTEMS, TRACKING (POSITION)

N82-20180"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SIMULATOR STUDY OF A PICTORIAL DISPLAY FOR GENERAL

AVIATION INSTRUMENT FLIGHT

J J ADAMS Mar. 1982 59 p refs

(NASA-TP-1963; L-14675; NAS 1.60:1963) Avail: NTIS HC

A04/MFA01 CSCL01D

COCKPIT SIMULATORS, COMPUTER GRAPHICS, DISPLAY

DEVICES, FLIGHT SIMULATION, GENERAL AVIATION

AIRCRAFT, INSTRUMENT LANDING SYSTEMS

39
06 AIRCRAFTINSTRUMENTATION

N82-33381"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

AN OPERATIONAL EVALUATION OF HEAD UP DISPLAYS FOR

CIVIL TRANSPORT OPERATIONS. NASA/FAA PHASE 3

REPORT Final Report

J. K. LAUBER, R. S, BRAY, R, L+HARRISON, J. C. HEMINGWAY,

and B. C. SCOTT(FAA) Aug. 1982 198p rafs

(NASA-TP-1815; A-8477; NAS t.60:1815; HUD-16) Avail: NTIS

HC A09/MF A01 CSCL 01D

CIVIL AVIATION, COMMERCIAL AIRCRAFT, HEAD-UP

DISPLAYS, TRAINING EVALUATION

N83-16338"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va,

RESULTS FROM TESTS, WITH VAN-MOUNTED SENSOR, OF

MAGNETIC LEADER CABLE FOR AIRCRAFT GUIDANCE

DURING ROLL-OUT AND TURNOFF

J, C+ YOUNG, W. T BUNDICK, and S. H. IRWIN Jan. 1983 38

p refs

(NASA-TP-2092; L-15482; NAS 1.60:2092) Avail: NTIS HC

A03/MF A01 CSCL 01D

AIRCRAFT GUIDANCE, CABLES (ROPES), TOWING

N83-17535"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

PLANNING FUEL-CONSERVATIVE DESCENTS WITH OR WITHOUT TIME CONSTRAINTS USING A SMALL PROGRAMMABLE

CALCULATOR: ALGORITHM DEVELOPMENT AND FLIGHT TEST

RESULTS

C. E. KNOX Mar. 1983 39 p refs

(NASA-TP-2085; L-15389; NAS 1.60:2085) Avail: NTIS HC

A03/MFA01 CSCL01D

CALCULATORS, DESCENT TRAJECTORIES, TRAJECTORY

MEASUREMENT

N83-18723"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SIMULATION STUDY OF TRAFFIC-SENSOR NOISE EFFECTS

ON UTILIZATION OF TRAFFIC SITUATION DISPLAY FOR

SELF-SPACING TASK

D. H. WILLIAMS and G. C. MOEN (Army Research and Technology

Labs., Hampton, Va.) Feb. 1983 36 p refs

(DA PROJ. 1L2-62209-AH-76)

(NASA-TP-2082; L-15403; NAS 1.60:2082;

AVRADCOM-TR-82-B-8) Avail: NTIS HC A03/MF A01 CSCL

05H

AIRCRAFT APPROACH SPACING, AZIMUTH, INSTRUMENT

APPROACH, INSTRUMENT ERRORS, PILOT PERFORMANCE,

RANGE ERRORS

N83-36028"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECT OF LEAD-AIRCRAFT GROUND-SPEED ON

SELF-SPACING PERFORMANCE USING A COCKPIT DISPLAY

OF TRAFFIC INFORMATION

J. R. KELLY Oct. 1983 50 p refs

(NASA-TP-2194; L-15402; NAS 1.60:2194) Avail: NTIS HC

A03/MF A01 CSCL 01D

AIR TRAFFIC, COCKPIT SIMULATORS, COMPUTERIZED

SIMULATION, DISPLAY DEVICES, FACTORIAL DESIGN, FLIGHT

CONTROL

N84-12164"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EVALUATION OF A TOTAL ENERGY-RATE SENSOR ON A

TRANSPORT AIRPLANE

A. J. OSTROFF, R M. HUESCHEN, R. F. HELLBAUM, C. M.

BELCASTRO, and J. F. CREEDON Nov. 1983 48 p refs

(NASA-TP-2212; NAS 1.60:2212; L-15461) Avail: NTIS HC

A03/MF A01 CSCL 01D

ADAPTIVE FILTERS, AIR FLOW, ENERGY REQUIREMENTS,

SENSORS, TRANSPORT AIRCRAFT, WIND SHEAR

40

N84-13182"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SIMULATOR STUDY OF PILOT-AIRCRAFT-DISPLAY SYSTEM

RESPONSE OBTAINED WITH A THREE-DIMENSIONAL-BOX

PICTORIAL DISPLAY

J.J. ADAMS Dec. 1983 52 p refs

(NASA-TP-2122; L-15632; NAS 1.60:2122) Avail: NTIS HC

A04/MF A01 CSCL 01D

AIRCRAFT INSTRUMENTS, DISPLAY DEVICES,

SERVOMECHANISMS

N84-21542"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SIMULATION OF A COCKPIT-DISPLAY CONCEPT FOR

EXECUTING A WAKE-VORTEX AVOIDANCE PROCEDURE

T. S. ABBOTT Apr. 1984 37 p refs

(NASA-TP-2300; L-15736; NAS 1.60:2300) Avail: NTIS HC

A03/MFA0t CSCL01D

AIR TRAFFIC CONTROL, COCKPITS, COMPUTERIZED

SIMULATION, FEASIBILITY ANALYSIS, GLIDE PATHS,

VORTICES, WAKES

N85-10044"# National Aeronautics and Space Administration.

Dryden (Hugh L,) Flight Research Center, Edwards, Calif.

PERIPHERAL VISION HORIZON DISPLAY (PVHD)

Apr. 1984 131 p refs Conf. held at Edwards, Calif., 15-16

Mar. 1983

(NASA-CP-2306; H-1232; NAS 1.55:2306) Avail: NTIS HC

A07/MF A01 CSCL01D

ATTITUDE INDICATORS, CONFERENCES, DISPLAY

DEVICES, PERIPHERAL VISION

N85-16868"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

REFERENCE ENERGY-ALTITUDE DESCENT GUIDANCE:

SIMULATOR EVALUATION

K. H. ABBOTandC. E. KNOX Jan. 1985 39p refs

(NASA-TP-2383; L-15800; NAS 1.60:2383) Avail: NTIS HC

A03/MFA01 CSCL01D

DESCENT, FLIGHT CONTROL, FLIGHT SIMULATORS, FUEL

CONSUMPTION

N85-16869*# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

A COCKPIT-DISPLAY CONCEPT FOR EXECUTING A MULTIPLE

GLIDE-SLOPE APPROACH FOR WAKE-VORTEX AVOIDANCE

T. S. ABBOTT Feb. 1984 44 p refs

(NASA-TP-2386; L-15852; NAS 1.60:2386) Avail: NTIS HC

A03/MF A01 CSCL 01D

AIR TRAFFIC CONTROL, APPROACH, COCKPITS, DISPLAY

DEVICES, GLIDE PATHS

N85-26705"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

PLANNING FUEL-CONSERVATIVE DESCENTS IN AN AIRLINE

ENVIRONMENTAL USING A SMALL PROGRAMMABLE

CALCULATOR: ALGORITHM DEVELOPMENT AND FLIGHT

TEST RESULTS

C. E. KNOX, D. D. VICROY, and D. A. SIMMON (United Airlines,

Inc., Chicago) May 1985 77 p refs

(NASA-TPo2393; L-15844; NAS 1.60:2393) Avail: NTIS HC

A05/MFA01 CSCL01D

COMPUTER TECHNIQUES, DESCENT, ENERGY

CONSERVATION, FLIGHT MANAGEMENT SYSTEMS, FLIGHT

PATHS, FLIGHT TESTS, FUEL CONSUMPTION
07

AIRCRAFT PROPULSION AND POWER

Includes prime propulsion systems and systems components, e.g.,

gas turbine engines and compressors; and onboard auxiliary power

plants for aircraft.

N77-17081"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

AIRCRAFT PISTON ENGINE EXHAUST EMISSION

SYMPOSIUM

Sep. 1976 373 p Symp. held in Cleveland, 14-15 Sep. 1976

(NASA-CP-2005; E-9010) Avail: NTIS HC A16/MF A01 CSCL

21E

AIR POLLUTION, CONFERENCES, EXHAUST GASES, PISTON

ENGINES

N77-31152"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

AERODYNAMIC AND DIRECTIONAL ACOUSTIC PERFORMANCE OF A SCOOP INLET

J. M. ABBOTT and D. A. DIETRICH Sep. 1977 28 p refs

(NASA-TP-1028; E-9134) Avail: NTIS HC A03/MF A01 CSCL

21E

NOISE REDUCTION, SCOOPS, STRUCTURAL DESIGN

CRITERIA, WIND TUNNEL TESTS

N77-31153"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EFFECTS OF TEMPERATURE TRANSIENTS AT FAN INLET OF

A TURBOFAN ENGINE

M. ABDELWAHAB Sep. 1977 40 p refs

(NASA-TP-1031; E-9162) Avail: NTIS HC A03/MF A01 CSCL

21E

INLET FLOW, TEMPERATURE EFFECTS, TEMPERATURE

GRADIENTS, TURBOFAN ENGINES

N77-31154"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

DEVELOPMENT AND VERIFICATION OF REAL-TIME, HYBRID

COMPUTER SIMULATION OF F100-PW-100(3) TURBOFAN

ENGINE

J. R. SZUCH, K. SELDNER, and D. S. CWYNAR Sep. 1977

75 p refs

(NASA-TP-1034; E-9090) Avail: NTIS HC A04/MF A01 CSCL

21E

COMPUTERIZED SIMULATION, HYBRID COMPUTERS, REAL

TIME OPERATION, TURBOFAN ENGINES

N77-32153"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EXPERIMENTAL FLOW COEFFICIENTS OF A FULL-COVERAGE

FILM-COOLEO-VANE CHAMBER

P. L. MEITNER (Army Air Mobility Research and Development

Lab., Cleveland, Ohio) and S. A. HIPPENSTEELE Sep. 1977

31 p refs

(NASA-TP-1036; E-9146) Avail: NTIS HC A03/MF A01 CSCL

21E

FILM COOLING, FLOW COEFFICIENTS, PERFORATI=D

PLATES, TURBINE BLADES

07 AIRCRAFT PROPULSION AND POWER

N77-32154"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EFFECT OF SLOTTED CASING TREATMENT WITH CHANGE

IN REYNOLDS NUMBER INDEX ON PERFORMANCE OF A JET

ENGINE

J. E. MOSS, JR. and W. M. BRAITHWAITE Sep. 1977 19 p

refs

(NASA-TP-1058; E-9185) Avail: NTIS HC A02/MF A01 CSCL

21E

ENGINE TESTS, JET ENGINES, NACELLES, REYNOLDS

NUMBER

N77-33169"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

F100 MULTIVARIABLE CONTROL SYNTHESIS PROGRAM:

EVALUATION OF A MULTIVARIABLE CONTROL USING A

REAL-TIME ENGINE SIMULATION

J. R. SZUCH, J. F. SOLDER, K. SELDNER, and D. S. CWYNAR

Oct. 1977 103 p refs

(NASA-TP-1056; E-9170) Avail: NTIS HC A06/MF A01 CSCL

21E

COMPUTERIZED SIMULATION, ENGINE CONTROL,

TURBOFAN ENGINES

N78-10068"# Massachusetts Inst. of Tech., Cambridge. Dept.

of Aeronautics and Astronautics.

AN ASSESSMENT OF TECHNOLOGY FOR TURBOJET ENGINE

ROTOR FAILURES

E. A. WITMER, ed. Mar. 1977 425 p Workshop held at

Cambridge, Mass., 29-31 Mar. 1977; sponsored by NASA

(NASA-CP-2017; E-8305) Avail: NTIS HC A18/MF A01 CSCL

21E

AIRCRAFT HAZARDS, CONFERENCES, FAILURE ANALYSIS,

ROTORS, TECHNOLOGY ASSESSMENT, TURBOJET ENGINES

N78-11063"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

AIRCRAFT ENGINE EMISSIONS

Oct. 1977 452 p Conf. held in Cleveland, 18-19 May 1977

(NASA-CP-2021; E-9262) Avail: NTIS HC A20/MF A01 CSCL

21E

AIR POLLUTION, AIRCRAFT ENGINES, CONFERENCES,

EXHAUST GASES, POLLUTION CONTROL

N78-11106"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

ALTITUDE TEST OF SEVERAL AFTERBURNER

CONFIGURATIONS ON A TURBOFAN ENGINE WITH A

HYDROGEN HEATER TO SIMULATE AN ELEVATED TURBINE

DISCHARGE TEMPERATURE

R. L JOHNSEN and R. R. CULLOM Nov. 1977 57 p refs

(NASA-TP-1068; E-9207) Avail: NTIS HC A04/MF A01 CSCL

21E

AFTERBURNING, ALTITUDE TESTS, TURBOFAN ENGINES

N78-13064"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

INFLUENCE OF OIL-SQUEEZE-FILM DAMPING ON

STEADY-STATE RESPONSE OF FLEXIBLE ROTOR OPERATING

TO SUPERCRITICAL SPEEDS

R. E. CUNNINGHAM Dec. 1977 44 p refs

(NASA-TP-1094; E-9091) Avail: NTIS HC A03/MF A01 CSCL

21E

FLEXIBLE BODIES, ROTORS, SUPERCRITICAL FLOW,

VISCOUS DAMPING

41
07 AIRCRAFT PROPULSION AND POWER

N78-16053"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

COLD-AIR PERFORMANCE OF FREE-POWER TURBINE

DESIGNED FOR 112-KILOWATT AUTOMOTIVE GAS-TURBINE

ENGINE. 1: DESIGN STATOR-VANE-CHORD SETTING ANGLE

OF 35 DEC

M. G. KOFSKEY and W. J. NUSBAUM Jan. 1978 23 p refs

(NASA-TP-1007; CONS/1011-12; E-8964) Avail: NTIS HC

A02/MF A01 CSCL 21E

AIR COOLING, AUTOMOBILE ENGINES, ENGINE DESIGN,

GAS TURBINE ENGINES, STATOR BLADES

N78-20130"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

TWO-DIMENSIONAL COLD-AIR CASCADE STUDY OF A

FILM-COOLED TURBINE STATOR BLADE. 4: COMPARISON

OF EXPERIMENTAL AND ANALYTICAL AERODYNAMIC

RESULTS FOR BLADE WITH 12 ROWS OF

O.076-CENTIMETER-(O.O30-1NCH-) DIAMETER HOLES HAVING

STREAMWISE EJECTION ANGLES

H. W. PRUST, JR. Mar. 1978 30 p refs

(NASA-TP-1151; E-9187) Avail: NTIS HC A03/MF A01 CSCL

21E

AERODYNAMIC CHARACTERISTICS, CASCADE FLOW, FILM

COOLING, STATOR BLADES, TURBINE BLADES

N78-20131"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

PERFORMANCE OF A SHORT ANNULAR DUMP DIFFUSER

USING SUCTION-STABILIZED VORTICES AT INLET MACH

NUMBERS TO 0.41

J. M. SMITH and A. J. JUHASZ Apr. 1978 40 p refs

(NASA-TP-1194; E-9332) Avail: NTIS HC A03/MF A01 CSCL

21E

ANNULAR NOZZLES, GAS EXPANSION, PERFORMANCE

TESTS, TURBULENT DIFFUSION, VORTICES

N78-20132"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

SIMULATED FLIGHT EFFECTS ON NOISE CHARACTERISTICS

OF A FAN INLET WITH HIGH THROAT MACH NUMBER

H. L. WESOKY, D. A. DIETRICH, and J. M. ABBOTT Apr. t978

45 p refs

(NASA-TP-1199; E-9253) Avail: NTIS HC A03/MF A01 CSCL

21E

AERODYNAMIC NOISE, FLIGHT SIMULATION, INLET FLOW,

MACH NUMBER

N78-20133"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

TWO-DIMENSIONAL COLD-AIR CASCADE STUDY OF A

FILM-COOLED TURBINE STATOR BLADE. 5: COMPARISON

OF EXPERIMENTAL AND ANALYTICAL AERODYNAMIC

RESULTS FOR BLADE WITH 12 ROWS OF

0.038-CENTIMETER-(0.015 INCH) DIAMETER COOLANT HOLES

HAVING STREAMWlSE EJECTION ANGLES

H. W. PRUST, JR. Apr. 1978 23 p refs

(NASA-TP-1204; E-9342) Avail: NTIS HC A02/MF A01 CSCL

21E

AERODYNAMIC CHARACTERISTICS, CASCADE FLOW, FILM

COOLING, STATOR BLADES, TURBINE BLADES

N78-21112'# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

AIRFLOW AND THRUST CALIBRATION OF AN F100 ENGINE,

SIN P680059, AT SELECTED FLIGHT CONDITIONS

T. J. BIESIADNY, D. LEE, and J. R. RODRIGUEZ Apr. 1978

27 p refs

(NASA-TP-1069; E-9257) Avail: NTIS HC AO3/MF A01 CSCL

21E

AIRFRAMES, CALIBRATING, F-100 AIRCRAFT, PROPULSION

SYSTEM PERFORMANCE, THRUST MEASUREMENT

42

N78-21113*# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

FLOW VISUALIZATION OF FILM COOLING WITH SPANWISE

INJECTION FROM A SMALL ARRAY OF HOLES AND

COMPOUND-ANGLE INJECTION FROM A LARGE ARRAY

L. M RUSSELL Apr. 1978 18 p refs

(NASA-TP-1195; Eo9340) Avail: NTIS HC A02/MF A01 CSCL

21E

FILM COOLING, FLOW VISUALIZATION, FLUID INJECTION

N78-21114"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

THEORETICAL FLOW CHARACTERISTICS OF INLETS FOR

TILTING-NACELLE VTOL AIRCRAFT

M A. BOLES, R. W. LUIDENS, and N. O. STOCKMAN Apr.

1978 31 p refs

(NASA-TP-1205; E-9387) Avail: NTIS HC A03/MF A01 CSCL

21E

FLOW CHARACTERISTICS, INLET FLOW, NACELLES,

VERTICAL TAKEOFF AIRCRAFT

N78-22101"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

IN-PLACE RECALIBRATION TECHNIQUE APPLIED TO A

CAPACITANCE-TYPE SYSTEM FOR MEASURING ROTOR

BLADE TIP CLEARANCE

J. P. BARRANGER Apr. 1978 35 p refs

(NASA-TP-1110; E-9395) Avail: NTIS HC A03/MF A01 CSCL

20E

BLADE TIPS, CAPACITANCE, CLEARANCES, ROTOR BLADES

(TURBOMACHINERY)

N78-23093"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

COMBUSTION OF HYDROGEN IN A TWO-DIMENSIONAL DUCT

WITH STEP FUEL INJECTORS

J. M EGGERS, P. G. REAGON, and P. B. GOODERUM May

1978 56p refs

(NASA-TP-1159; L-11981) Avail: NTIS HC AO4/MF A01

CSCL 21E

FUEL INJECTION, HYDROGEN, SUPERSONIC COMBUSTION,

TWO DIMENSIONAL FLOW

N78-23094"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

INTERACTION BETWEEN STEP FUEL INJECTORS ON

OPPOSITE WALLS IN A SUPERSONIC COMBUSTOR MODEL

C. R. MCCLINTON May 1978 61 p refs

(NASA-TP-1174; L-11811) Avail: NTiS HC A04/MF A01

CSCL 21E

FUEL INJECTION, SUPERSONIC COMBUSTION, SUPERSONIC COMBUSTION RAMJET ENGINES

N78-23095"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

ALTITUDE CALIBRATION OF AN FIO0, SIN P680063,

TURBOFAN ENGINE

T. J. BIESIADNY, D. LEE, and J. R. RODRIGUEZ May 1978

23 p refs

(NASA-TP-1228; E-9355) Avail: NTIS HC A02/MF A01 CSCL

21E

ALTITUDE TESTS, ENGINE TESTS, F-100 AIRCRAFT,

THRUST MEASUREMENT, TURBOFAN AIRCRAFT
N78-26148"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EMITTANCE AND ABSORPTANCE OF NASA CERAMIC

THERMAL BARRIER COATING SYSTEM

C. H. LIEBERT Jun. 1978 31 p refs Presented in part at

the Intern. Conf. on Met. Coatings, San Francisco, 3-7 Apr. 1978;

sponsored by the Am. Vacuum Soc.

(NASA-TP-1190; E-9474) Avail: NTIS HC A03/MF A01 CSCL

20E

ABSORPTION SPECTRA, CERAMIC COATINGS, METAL

COMPOUNDS, SPECTRAL EMISSION, THERMAL PROTECTION

N78-27130"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

REVERSE-FLOW COMBUSTOR FOR SMALL GAS TURBINES

WITH PRESSURE-ATOMIZING FUEL INJECTORS

C. T. NORGREN, E. J. MULARZ (AVRADCOM Res. and Technol.

Labs.), and S. M. RIDDLEBAUGH Aug. 1978 30 p refs

(NASA-TP-1260; AVRADCOM-TR-78-22(PL); E-9458) Avail:

NTIS HC A03/MF A01 CSCL 21E

COMBUSTION CHAMBERS, FUEL INJECTION, GAS TURBINE

ENGINES, PRESSURE DISTRIBUTION, REVERSED FLOW

N78-28099"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

FORTRAN PROGRAM FOR CALCULATING COOLANT FLOW

AND METAL TEMPERATURES OF A FULL-COVERAGE-FILMCOOLED VANE OR BLADE

P. L. MEITNER (AVRADCOM R and T Labs., Cleveland) Jul.

1978 92p refs

(NASA-TP-1259; E-9491; AVRADCOM-TR-78-19(PL)) Avail:

NTIS HC A05/MF A01 CSCL 21E

COMPUTER PROGRAMS, FILM COOLING, HEAT TRANSFER,

TURBINE BLADES

N78-31109"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

ANALYSIS OF METAL TEMPERATURE AND COOLANT FLOW

WITH A THERMAL-BARRIER COATING ON A

FULL-COVERAGE-FILM-COOLED TURBINE VANE

P. L. MEITNER (AVRADCOM Res. and Technol. Labs.) Aug.

1978 15p refs

(NASA-TP-1310; AVRADCOM-TR-78-20) Avail: NTIS HC

A02/MF A01 CSCL 21E

FILM COOLING, HEAT TRANSFER, THERMAL CONTROL

COATINGS, TURBINE BLADES

N78-33107"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

PERFORMANCE OF A TRANSONIC FAN STAGE DESIGNED

FOR A LOW MERIDIONAL VELOCITY RATIO

R. D. MOORE, G. W. LEWIS, JR., and W. M. OSBORN Nov.

1978 83 p refs

(NASA-TP-1298; E-8994) Avail: NTIS HC A05/MF A01 CSCL

21E

COMPRESSOR ROTORS, SUPERSONIC TURBINES,

TURBOFANS

N78-33108"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

DESIGN AND OVERALL PERFORMANCE OF FOUR HIGHLY

LOADED, HIGH SPEED INLET STAGES FOR AN ADVANCED

HIGH-PRESSURE-RATIO CORE COMPRESSOR

L. REID and R D. MOORE Oct. 1978 122 p refs

(NASA-TP-1337; E-9302) Avail: NTIS HC A06/MF A01 CSCL

21E

COMPRESSOR EFFICIENCY, COMPRESSOR ROTORS,

ENGINE DESIGN, INTAKE SYSTEMS, PRESSURE

DISTRIBUTION

07 AIRCRAFT PROPULSION AND POWER

N78-33109"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

DESIGN AND PERFORMANCE OF A 427-METER-PER-SECONDTIP-SPEED TWO-STAGE FAN HAVING A 2.40 PRESSURE RATIO

W. S. CUNNAN, W. STEVANS, and D. C. URASEK Oct. 1978

96 p refs

(NASA-TP-1314; E-9005) Avail: NTIS HC A05/MF A01 CSCL

21E

AXIAL FLOW TURBINES, COMPRESSOR ROTORS, TIP

SPEED, TURBOMACHINERY

N78-33110"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

DYGABCD: A PROGRAM FOR CALCULATING LINEAR A, B,

C, AND D MATRICES FROM A NONLINEAR DYNAMIC ENGINE

SIMULATION

L. C. GEYSER Sep. 1978 203 p refs

(NASA-TP-1295; E-9464) Avail: NTIS HC A10/MF A01 CSCL

21E

COMPUTER PROGRAMS, COMPUTERIZED SIMULATION,

MATRICES (MATHEMATICS), TURBOFAN ENGINES, TURBOJET

ENGINES

N79-10060"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

PERFORMANCE OF SINGLE-STAGE AXIAL-FLOW TRANSONIC

COMPRESSOR WITH ROTOR AND STATOR ASPECT RATIOS

OF 1.19 AND 1.26, RESPECTIVELY, AND WITH DESIGN

PRESSURE RATIO OF 1.82

L REID and R. D. MOORE Nov. 1978 103 p refs

(NASA-TP-1338; E-9461) Avail: NTIS HC A06/MF A01 CSCL

21E

TRANSONIC FLOW, TURBOCOMPRESSORS

N79-13044"# National Aeronautics and Space Administration.

Flight Research Center, Edwards, Calif.

COMPARISON OF CALCULATED AND ALTITUDE-FACILITYMEASURED THRUST AND AIRFLOW OF TWO PROTOTYPE F100

TURBOFAN ENGINES

F. J. KURTENBACH Dec. 1978 29 p refs

(NASA-TP-1373; H-1015) Avail: NTIS HC A03/MF A01 CSCL

21E

AIR FLOW, JET THRUST, THRUST MEASUREMENT,

TURBOFAN ENGINES

N79-13045"# National Aeronautics and Space Administration.

Dryden (Hugh L.) Flight Research Center, Edwards, Calif.

MEASUREMENTS AND PREDICTIONS OF FLYOVER AND

STATIC NOISE OF A TF30 AFTERBURNING TURBOFAN

ENGINE

F. W. BURCHAM, JR., P. L. LASAGNA, and S. C. OAS (Boeing

Com. Airplane Co.) Dec. 1978 94 p refs

(NASA-TP-1372; H-1017) Avail: NTIS HC A05/MF A01 CSCL

21E

AFTERBURNING, ENGINE NOISE, F-111 AIRCRAFT, NOISE

MEASUREMENT, TURBOFAN ENGINES

N79-13046"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

LOW-CYCLE FATIGUE OF THERMAL-BARRIER COATINGS AT

982 DEG C

A. KAUFMAN, C. H. LIEBERT, and A. J. NACHTIGALL Dec.

1978 20 p refs

(NASA-TP-1322; E-9688) Avail: NTIS HC A02/MF A01 CSCL

21E

CERAMIC COATINGS, FATIGUE LIFE, THERMAL

RESISTANCE

43
07 AIRCRAFT PROPULSION AND POWER

N79-14098"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

CERAMIC COATING EFFECT ON LINER METAL

TEMPERATURES OF FILM-COOLED ANNULAR COMBUSTOR

R. W. CLAUS, J. D. WEAR, and C. H. LIEBERT Jan. 1979 24

p refs

(NASA-TP-1323; E-9732) Avail: NTIS HC A03/MF A01 CSCL

21E

CERAMICS, COMBUSTION CHAMBERS, FILM COOLING,

PROTECTIVE COATINGS, TEMPERATURE DISTRIBUTION

N79-14099"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EFFECT OF SWIRLER-MOUNTED MIXING VENTURI ON

EMISSIONS OF FLAME-TUBE COMBUSTOR USING JET A

FUEL

D. B. ERCEGOVIC Jan. 1979 23 p refs

(NASA-TP-1393; AVRADCOM-TR-78-41; E-9762) Avail: NTIS

HC A02/MF A01 CSCL 21E

EXHAUST GASES, FUEL COMBUSTION, FUEL INJECTION,

VENTURI TUBES

N79-15961"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

THE ROTARY COMBUSTION ENGINE: A CANDIDATE FOR

GENERAL AVIATION

1978 t90 p refs Symp. held at Cleveland, Ohio, 28 Feb.

1978

(NASA-CP-2067; E-9800) Avail: NTIS HC A09/MF A01 CSCL

21A

AIRCRAFT ENGINES, CONFERENCES, ENGINE DESIGN,

GENERAL AVIATION AIRCRAFT, MECHANICAL DRIVES

N79-16852"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EFFECT OF CASING TREATMENT ON PERFORMANCE OF A

TWO-STAGE HIGH-PRESSURE-RATIO FAN

D. C. URASEK Feb. 1979 68 p refs

(NASA-TP-1409; E-8997) Avail: NTIS HC A04/MF A01 CSCL

21E

COMPRESSOR ROTORS, ROTOR AERODYNAMICS, ROTOR

BLADES (TURBOMACHINERY), STATOR BLADES

N79-22099'# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

PERFORMANCE OF A VORTEX-CONTROLLED DIFFUSER IN

AN ANNULAR SWIRL-CAN COMBUSTOR AT INLET MACH

NUMBERS UP TO 0.53

J. M. SMITH Washington Apr. 1979 17 p refs

(NASA-TP-1452; E-9832) Avail: NTIS HC A02/MF A01 CSCL

21E

ANNULAR NOZZLES, COMBUSTION CHAMBERS,

DIFFUSERS, FLOW STABILITY, SUCTION, VORTICES

N79-23086"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EFFECT OF PRIMARY-ZONE EQUIVALENCE RATIO ON

POLLUTANT FORMATION

R.W. CLAUS May 1979 20p refs

(NASA-TP-1463; E-9896) Avail: NTIS HC A02/MF A01 CSCL

21E

AIR POLLUTION, COMBUSTION CHAMBERS, COMBUSTION

PRODUCTS, EXHAUST GASES, SMOKE

N79-23967°# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

PERFORMANCE OF TWO-STAGE FAN WITH LARGER

DAMPERS ON FIRST-STAGE ROTOR

O. C. URASEK, W. S CUNNAN, and W. STEVANS May 1979

81 p refs

(NASA-TP-1399; E-8958) Avail: NTIS HC A05/MF A01 CSCL

21E

DAMPERS, FANS, HIGH PRESSURE, TURBOMACHINERY

44

N79-24994"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio,

PREMIXED PREVAPORIZED COMBUSTOR TECHNOLOGY

FORUM

1979 262 p refs Conf. held at Cleveland, Ohio, 9-10 Jan.

1979

(NASA-CP-2078; E-9933) Avail: NTIS HC A12/MF A01 CSCL

21E

AIRCRAFT ENGINES, COMBUSTION CHAMBERS,

CONFERENCES, FUEL COMBUSTION, GAS TURBINE ENGINES,

PREMIXED FLAMES, TECHNOLOGY ASSESSMENT,

VAPORIZING

N79-25016"# National Aeronautics and Space Administration,

Lewis Research Center, Cleveland, Ohio.

FUNDAMENTALS OF GAS TURBINE COMBUSTION

M. GERSTEIN (Univ. of Southern Calif., Los Angeles) 1979 52

p Workshop held at Cleveland, 6-7 Feb. 1979

(NASA-CP-2087; E.026) Avail: NTIS HC A04/MF A01 CSCL

21E

AIRCRAFT PARTS, COMBUSTION CHAMBERS, GAS

TURBINES

N79-25022"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

OPERATING CONDITION AND GEOMETRY EFFECTS ON

LOW-FREQUENCY AFTERBURNER COMBUSTION INSTABILITY

IN A TURBOFAN AT ALTITUDE

R. R. CULLOM and R. L JOHNSEN Jun. 1979 31 p refs

(NASA-TP-1475; E-9886) Avail: NTIS HC A03/MF A01 CSCL

21E

AFTERBURNING, COMBUSTION STABILITY, TURBOFAN

ENGINES

N79-25023"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

INDUSTRY TESTS OF NASA CERAMIC THERMAL BARRIER

COATING

C. H. LIEBERT and F. S. STEPKA Jun. 1979 26 p refs

Presented at 6th Intern. Vacuum Metallurgy Conf., San Diego,

Calif., 23-27 Apr. 1979; Sponsored by Am. Vacuum Soc.

(NASA-TP-t425; E-9846) Avail: NTIS HC A03/MF A01 CSCL

2tE

CERAMICS, GAS TURBINE ENGINES, THERMAL CONTROL

COATINGS

N79-26057"# National Aeronautics and Space Administration.

Dryden (Hugh L.) Flight Research Center, Edwards, Calif.

EVALUATION OF A SIMPLIFIED GROSS THRUST

CALCULATION TECHNIQUE USING TWO PROTOTYPE F100

TURBOFAN ENGINES IN AN ALTITUDE FACILITY

F. J. KURTENBACH Jun. 1979 30 p refs

(NASA-TP-1482; H-1061) Avail: NTIS HC A03/MF A01 CSCL

21E

ENGINE TESTS, TEST FACILITIES, THRUST MEASUREMENT,

TURBOFAN ENGINES

N79-27142"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

FLOW VISUALIZATION OF DISCRETE-HOLE FILM COOLING

WITH SPANWlSE INJECTION OVER A CYLINDER

L. M RUSSELL Jul. 1979 15 p refs

(NASA-TP-1491; E-9946) Avail: NTIS HC A02/MF A01 CSCL

21E

FILM COOLING, FLOW VISUALIZATION, TURBINE BLADES
N79-27143"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

PERFORMANCE OF TWO-STAGE FAN HAVING

LOW-ASPECT-RATIO FIRST-STAGE ROTOR BLADING

D. C. URASEK, W. T. GORRELL (Army Aviation Res. and Develop.

Command, Cleveland), and W. S. CUNNAN Aug. 1979 132 p

Prepared in cooperation with US Army Aviation Research and

Development Command, Cleveland

(NASA-TP-1493; AVRADCOM-TR-78-49; E-9237) Avail: NTIS

HC A07/MF A01 CSCL 21E

FANS, LOW ASPECT RATIO, ROTOR BLADES

(TURBOMACHINERY)

N79-28176"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

A THROAT-BYPASS STABILITY-BLEED SYSTEM USING

RELIEF VALVES TO INCREASE THE TRANSIENT STABILITY

OF A MIXED-COMPRESSION INLET

G. H. NEINER, M. O. DUSTIN, and G. L. COLE Jul. 1979 47 p

refs

(NASA-TP-1083; E-8950) Avail: NTIS HC A03/MF A01 CSCL

21E

AIR INTAKES, BYPASSES, FLOW STABILITY, SUPERSONIC

INLETS, WIND TUNNEL TESTS, YF-12 AIRCRAFT

N79-28177"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EFFECT OF ROTOR MERIDIONAL VELOCITY RATIO ON

RESPONSE TO INLET RADIAL AND CIRCUMFERENTIAL

DISTORTION

N. L. SANGER Jul. 1979 73 p refs

(NASA-TP-1278; E-8987) Avail: NTIS HC A04/MF A01 CSCL

21E

COMPRESSOR ROTORS, FLOW DISTORTION, INLET FLOW,

MERIDIONAL FLOW, ROTOR AERODYNAMICS, VELOCITY

DISTRIBUTION

N79-29192"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

CRITERIA FOR SELF-IGNITION OF SUPERSONIC

HYDROGEN-AIR MIXTURES

P. W. HUBER, C. J. SCHEXNAYDER, JR., and C. R.

MCCLINTON Aug. 1979 58 p refs

(NASA-TP-1457; L-12678) Avail: NTIS HC A04/MF A01

CSCL 21A

GAS MIXTURES, HYDROGEN, IGNITION LIMITS,

SUPERSONIC COMBUSTION RAMJET ENGINES

N79-30191"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

PERFORMANCE OF TWO-STAGE FAN WITH A FIRST-STAGE

ROTOR REDESIGNED TO ACCOUNT FOR THE PRESENCE OF

A PART-SPAN DAMPER

W. T. GORRELL and D. C. YRASEK Sep. 1979 72 p refs

(NASA-TP-1483; E-9786; AVRADCOM-TR-79-10) Avail: NTIS

HC A04/MF A01 CSCL 21E

AERODYNAMIC CONFIGURATIONS, COMPRESSOR

ROTORS, ROTOR AERODYNAMICS, ROTOR BLADES

(TURBOMACHINERY), VIBRATION ISOLATORS

N79-31213"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

AERODYNAMIC PERFORMANCE OF 1o38-PRESSURE-RATIO,

VARIABLE-PITCH FAN STAGE

R. D. MOORE and W. M. OSBORN Sep. 1979 71 p

(NASA-TP-1502; E-9700) Avail: NTIS HC A04/MF A01 CSCL

21E

AXIAL FLOW TURBINES, COMPRESSOR BLADES, LIFT

FANS, PRESSURE MEASUREMENT, ROTOR BLADES

(TURBOMACHINERY), TURBOCOMPRESSORS, VARIABLE

PITCH PROPELLERS

07 AIRCRAFT PROPULSION AND POWER

N79-31214"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

AERODYNAMIC PERFORMANCE OF AXIAL-FLOW FAN STAGE

OPERATED AT NINE INLET GUIDE VANE ANGLES

R. D. MOORE and L. REID Sep. 1979 43 p refs

(NASA-TP-1510; E-9714) Avail: NTIS HC A03/MF A01 CSCL

21E

AIR FLOW, AXIAL FLOW TURBINES, ENGINE TESTS, GUIDE

VANES, LIFT FANS, PERFORMANCE TESTS, VERTICAL

TAKEOFF AIRCRAFT

N79-33210"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EFFECTS OF DIFFUSION FACTOR, ASPECT RATIO AND

SOLIDITY ON OVERALL PERFORMANCE OF 14 COMPRESSOR

MIDDLE STAGES

W. R. BRITSCH, W. M. OSBORN, and M. R LAESSIG

Washington Sep. 1979 148 p

(NASA-TP-1523; E-9943) Avail: NTIS HC A07/MF A01 CSCL

21E

ASPECT RATIO, COMPRESSOR BLADES, COMPRESSOR

ROTORS, DIFFUSION, PERFORMANCE TESTS, TURBOCOMPRESSORS

N80-10205"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

AEROPROPULSlON 1979

1979 464 p Proceedings of conf. held at Cleveland, 15-16

May 1979

(NASA-CP-2092; E-079) Avail: NTIS HC A20/MF A01 CSCL

21E

AIRCRAFT ENGINES, CONFERENCES, ENGINE DESIGN,

PROPULSION SYSTEM PERFORMANCE, TURBINE ENGINES

N80-11087"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

INFLUENCE OF COOLANT TUBE CURVATURE ON FILM

COOLING EFFECTIVENESS AS DETECTED BY INFRARED

IMAGERY

S. S. PAPELL, R. W. GRAHAM, and R. P. CAGEAO

Washington Nov. 1979 18 p refs

(NASA-TP-1546; E-066) Avail: NTIS HC A02/MF A01 CSCL

21E

COOLANTS, COOLING, FILM COOLING, HILSCH TUBES,

INFRARED IMAGERY

N80-14121"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

STATIC TEST-STAND PERFORMANCE OF THE YF-102

TURBOFAN ENGINE WITH SEVERAL EXHAUST

CONFIGURATIONS FOR THE QUIET SHORT-HAUL RESEARCH

AIRCRAFT (QSRA)

J. G. MCARDLE, L. HOMYAK, and A. S. MOORE Nov. 1979

62 p

(NASA-TP-1556; E-019) Avail: NTIS HC A04/MF A01 CSCL

21E

EXHAUST SYSTEMS, NOZZLE GEOMETRY, QUIET ENGINE

PROGRAM, SHORT HAUL AIRCRAFT, STATIC FIRING,

TURBOFAN ENGINES

N80-14123"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

DYNAMIC RESPONSE OF A MACH 2.5 AXlSYMMETRIC INLET

AND TURBOJET ENGINE WITH A POPPET-VALUE

CONTROLLED INLET STABILITY BYPASS SYSTEM WHEN

SUBJECTED TO INTERNAL AND EXTERNAL AIRFLOW

TRANSIENTS

B. W. SANDERS Washington Jan. 1980 102 p refs

(NASA-TP-1531; E-9467) Avail: NTIS HC A06/MF A01 CSCL

21E

AERODYNAMIC STABILITY, BYPASSES, PROPULSION

SYSTEM PERFORMANCE, SUPERSONIC INLETS, TURBOJET

ENGINES

45
07 AIRCRAFT PROPULSION AND POWER

N80-14124"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

TURBOJET-EXHAUST-NOZZLE SECONDARY-AIRFLOW

PUMPING AS AN EXIT CONTROL OF AN INLET-STABILITY

BYPASS SYSTEM FOR A MACH 2.5 AXISYMMETRIC

MIXED-COMPRESSION INLET

B. W. SANDERS Jan. 1980 82 p refs

(NASA-TP-1532; E-9468) Avail: NTIS HC A05/MF A01 CSCL

21E

AIR FLOW, EXHAUST NOZZLES, SHOCK WAVE CONTROL,

SUPERSONIC INLETS, TURBOJET ENGINES, WIND TUNNEL

TESTS

N80-14125"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EFFECT OF DEGREE OF FUEL VAPORIZATION UPON

EMISSIONS FOR A PREMIXED PARTIALLY VAPORIZED

COMBUSTION SYSTEM

L. P. COOPER Jan. 1980 25 p refs

(NASA-TP-1582; E-010) Avail: NTIS HC A02/MF A01 CSCL

21E

COMBUSTION CHAMBERS, EXHAUST GASES, FUEL-AIR

RATIO, GAS MIXTURES, GAS TURBINE ENGINES,

VAPORIZING

N80-15127"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

QUIET POWERED-LIFT PROPULSION

1979 426 p refs Conf. held at Cleveland, Ohio, 14-15 Nov.

1978

(NASA-CP-2077; E-9906) Avail: NTIS HC A19/MF A01 CSCL

21E

C-15 AIRCRAFT, CONFERENCES, NASA PROGRAMS,

POWERED LIFT AIRCRAFT, QUIET ENGINE PROGRAM, TILT

ROTOR AIRCRAFT, YC-14 AIRCRAFT

N80-15128"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

DIRECT INTEGRATION OF TRANSIENT ROTOR DYNAMICS

A. F. KASCAK Washington Jan. 1980 23 p refs

(NASA-TP-1597; AVRADCOM-TR-79-42; E-101) Avail: NTIS HC

A02/MF A01 CSCL 21E

NUMERICAL INTEGRATION, ROTATING SHAFTS, ROTORS

N80-15129"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

EVALUATION OF APPROXIMATE METHODS FOR THE

PREDICTION OF NOISE SHIELDING BY AIRFRAME

COMPONENTS

W. F. AHTYE and G. MCCULLEY (Informatics, Inc., Palo Alto,

Calif.) Washington Jan. 1980 105 p refs

(NASA-TP.1004; A-6961) Avail: NTIS HC A06/MF A01 CSCL

21E

ACOUSTIC ATTENUATION, AIRCRAFT STRUCTURES,

ANECHOIC CHAMBERS, APPROXIMATION, NOISE REDUCTION,

SHORT TAKEOFF AIRCRAFT

N80-17071"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

AERODYNAMIC PERFORMANCES OF THREE FAN STATOR

DESIGNS OPERATING WITH ROTOR HAVING TIP SPEED OF

337 METERS PER SECOND AND PRESSURE RATIO OF 1.54.

1: EXPERIMENTAL PERFORMANCE

T. F. GELDER Feb. 1980 108 p refs

(NASA-TP-16t0; E-138) Avail: NTIS HC A06/MF A01 CSCL

21E

ROTOR AERODYNAMICS, STATOR BLADES, TURBOMACHINERY

46

N80-21323"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EXPERIMENTAL EVALUATION OF A SPINNING-MODE

ACOUSTIC-TREATMENT DESIGN CONCEPT FOR AIRCRAFT

INLETS

L. J. HEIDELBERG, E. J. RICE, and L. HOMYAK Apr. 1980 29

p refs

(NASA-TP-1613; E-185) Avail: NTIS HC A03/MF A01 CSCL

21E

ACOUSTIC ATTENUATION, ENGINE INLETS, F-102

AIRCRAFT, JET AIRCRAFT NOISE, NOISE REDUCTION,

TURBOFAN ENGINES

N60-21324"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

AERODYNAMIC PERFORMANCES OF THREE FAN STATOR

DESIGNS OPERATING WITH ROTOR HAVING TIP SPEED OF

337 METERS PER SECOND AND PRESSURE RATIO OF 1.54.

RELATION OF ANALYTICAL CODE CALCULATIONS TO

EXPERIMENTAL PERFORMANCE

T. F. GELDER, J. F. SCHMIDT, and G. M. ESGAR Apr. 1980

53 p refs

(NASA-TP-1614; E-137) Avail: NTIS HC A04/MF A0t CSCL

21E

AERODYNAMIC CHARACTERISTICS, COMPUTER PROGRAMS, FLOW DISTRIBUTION, NUMERICAL FLOW VISUALIZATION, ROTOR AERODYNAMICS, STATOR BLADES

N60-21325"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

PERFORMANCE OF SINGLE-STAGE AXIAL-FLOW TRANSONIC

COMPRESSOR WITH ROTOR AND STATOR ASPECT RATIOS

OF 1.19 AND 1,26 RESPECTIVELY, AND WITH DESIGN

PRESSURE RATIO OF 2.05

R. D. MOORE and L. REID Washington Apr. 1980 103 p

(NASA-TP-1659; E-138) Avail: NTIS HC A06/MF A01 CSCL

21E

LOW ASPECT RATIO, ROTOR AERODYNAMICS, STATOR

BLADES, TRANSONIC COMPRESSORS, TURBOCOMPRESSORS

N60-21326"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

ANALYSIS OF UNCERTAINTIES IN TURBINE METAL

TEMPERATURE PREDICTIONS

F. S. STEPKA Washington Apr. 1980 19 p refs

(NASA-TP-1593; E-228) Avail: NTIS HC A02/MF A01 CSCL

21E

PREDICTION ANALYSIS TECHNIQUES, SURFACE

TEMPERATURE, TURBINE BLADES, TURBOFAN ENGINES

N80-22327"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

GENERAL AVIATION PROPULSION

Mar. 1980 437 p refs Conf. held in Cleveland, 28-29 Nov.

1979

(NASA-CP-2126; E-310) Avail: NTIS HC A19/MF A01 CSCL

21E

AIRCRAFT ENGINES, AIRCRAFT NOISE, CONFERENCES,

ENGINE DESIGN, GENERAL AVIATION AIRCRAFT,

PROPULSION SYSTEM CONFIGURATIONS

N80-25337"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

DESIGN AND COLD-AIR TEST OF SINGLE-STAGE UNCOOLED

TURBINE WITH HIGH WORK OUTPUT

T. P. MOFFITT, E. M. SZANCA, W. J. WHITNEY, and F. P.

BEHNING Jun. 1980 18 p refs

(NASA-TP-1680; E-316) Avail: NTIS HC A02/MF A01 CSCL

21E

COLD FLOW TESTS, ENGINE DESIGN, MASS FLOW,

TURBINES
N80-25338"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

COLD-AIR INVESTIGATION OF A 4 1/2 STAGE TURBINE WITH

STAGE-LOADING FACTOR OF 4.66 AND HIGH SPECIFIC WORK

OUTPUT. 2: STAGE GROUP PERFORMANCE

W. J. WHITNEY, F. P. BEHNING, T. P. MOFFITT, and G. M.

HOTZ Jun. 1980 16p refs

(NASA-TP-1688; E-315) Avail: NTIS HC A02/MF A01 CSCL

21E

AIRCRAFT ENGINES, COLD FLOW TESTS, ENGINE DESIGN,

LOADS (FORCES), TURBINES

N80-25339"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

STATIC AND TRANSIENT PERFORMANCE OF YF-102 ENGINE

WITH UP TO 14 PERCENT CORE AIRBLEED FOR THE QUIET

SHORT-HAUL RESEARCH AIRCRAFT

J. G. MCARDLE, L. HOMYAK, and A. S. MOORE Jun. 1980

26 p refs

(NASA-TP-1692) Avail: NTIS HC A02/MF A01 CSCL 21E

BOUNDARY LAYER CONTROL, ENGINE TESTS, SHORT

HAUL AIRCRAFT, STATIC TESTS, TRANSIENT RESPONSE,

TURBOFAN ENGINES

N80-28352"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

OFF-DESIGN CORRELATION FOR LOSSES DUE TO

PART-SPAN DAMPERS ON TRANSONIC ROTORS

W. B. ROBERTS, J. E. GROUSE, and D. M. SANDERCOCK Jul.

1980 24 p refs

(NASA-TP-1693; E-309) Avail: NTIS HC A02/MF A01 CSCL

21E

COMPRESSOR EFFICIENCY, DAMPERS (VALVES),

OSCILLATION DAMPERS, PREDICTION ANALYSIS

TECHNIQUES, ROTOR BLADES (TURBOMACHINERY),

TURBOFAN ENGINES

N80-29300"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

AIRCRAFT RESEARCH AND TECHNOLOGY FOR FUTURE

FUELS

Jul. 1980 229 p refs Symp. held in Cleveland, Ohio, 16-17Apr.

1980

(NASA-CP-2146; E-398) Avail: NTIS HC A11/MF A01 CSCL

21E

AIRCRAFT FUELS, CONFERENCES, FUEL COMBUSTION,

FUEL PRODUCTION, JET ENGINE FUELS

N80-32396"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

LOW-PRESSURE PERFORMANCE OF ANNULAR, HIGH-PRESSURE (40 ATM) HIGH-TEMPERATURE (2480 K) COMBUSTION

SYSTEM

J. D. WEAR Washington Sep. 1980 20 p refs

(NASA-TP-1713; E-372) Avail: NTIS HC A02/MF A01 CSCL

21E

COMBUSTION CHAMBERS, EXHAUST GASES, FUEL

INJECTION, FUEL-AIR RATIO, GAS PRESSURE, INLET

TEMPERATURE, ISOTHERMAL PROCESSES

N80-33409"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

CONCEPTUAL MODEL OF TURBULENT FLAMEHOLDING FOR

SCRAMJET COMBUSTORS

P. W. HUBER Oct. 1980 36 p refs

(NASA-TP-1543; L-13600) Avail: NTIS HC A03/MF A01

CSCL 21E

COMBUSTION PHYSICS, ENGINE DESIGN, FLAME

HOLDERS, FLAME PROPAGATION, FLAMEOUT, SUPERSONIC

COMBUSTION RAMJET ENGINES

07 AIRCRAFT PROPULSION AND POWER

N80-33410"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EXPERIMENTAL PERFORMANCE AND ANALYSIS OF 15.04-

CENTIMETER-TIP-DIAMETER, RADIAL-INFLOW TURBINE WITH

WORK FACTOR OF 1.126 AND THICK BLADING

K. L. MCLALLIN and J. E. HAAS Oct. 1980 21 p refs

Prepared in cooperation with Army Aviation Research and

Development Command, St. Louis, Mo.

(NASA-TP-1730; E-391; AVRADCOM-TR-80-09) Avail: NTIS HC

A02/MF A01 CSCL 21E

AERODYNAMICS, DESIGN ANALYSIS, PERFORMANCE

PREDICTION, TURBINE BLADES

N81-11037"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

LOW-SPEED AERODYNAMIC PERFORMANCE OF

50.8-CENTIMETER-DIAMETER NOISE-SUPPRESSING INLETS

FOR THE QUIET, CLEAN, SHORT-HAUL EXPERIMENTAL

ENGINE (QCSEE)

J. M ABBOTT, J. H. DIEDRICH, and R C. WILLIAMS Aug.

1978 37 p refs

(NASA-TP-1178; E-9542) Avail: NTIS HC A03/MF A01 CSCL

21E

AERODYNAMIC CHARACTERISTICS, ENGINE INLETS, NOISE

REDUCTION, QUIET ENGINE PROGRAM, SHORT HAUL

AIRCRAFT, WIND TUNNEL TESTS

N81-11038"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio. Propulsion Lab.

OFF-DESIGN PERFORMANCE LOSS MODEL FOR RADIAL

TURBINES WITH PIVOTING, VARIABLE-AREA STATORS

P. L. MEITNER and A. J. GLASSMAN Nov. 1980 15 p refs

(NASA-TP-1708; AVRADCOM-TR-80-C-13; E-455) Avail: NTIS

HC A02/MF A01 CSCL 21E

STATOR BLADES, TURBINE ENGINES, VARIABLE

GEOMETRY STRUCTURES

N81-11039"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

SURFACE PYROMETRY IN PRESENCE OF RADIATION FROM

OTHER SOURCES WITH APPLICATION TO TURBINE BLADE

TEMPERATURE MEASUREMENT

D. R. BUCHELE Nov. 1980 19 p refs

(NASA-TP-1754; E-396) Avail: NTIS HC A02/MF A01 CSCL

21E

RADIATION PYROMETERS, THERMOCOUPLE PYROMETERS, TURBINE BLADES, WAVELENGTHS

N81-12089"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EFFECT OF HOLE GEOMETRY AND ELECTRIC-DISCHARGE

MACHINING (EDM) ON AIRFLOW RATES THROUGH SMALL

DIAMETER HOLES IN TURBINE BLADE MATERIAL

S. A. HIPPENSTEELE and R. P. COCHRAN Nov. 1980 14 p

(NASA-TP-1716; E-417) Avail: NTIS HC AO2/MF A01 CSCL

21E

ELECTRIC DISCHARGES, FLOW VELOCITY, GAS TURBINE

ENGINES, HOLE DISTRIBUTION (ELECTRONICS), MACHINING

N81-12090"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

PROPULSION CONTROLS, 1979

Oct. 1980 147 p refs Proc. of symp. held in Cleveland,

17-19 May 1979

(NASA-CP-2137; E-477) Avail: NTIS HC A07/MF A01 CSCL

21E

ADAPTIVE CONTROL, AIR BREATHING ENGINES, AIRCRAFT

ENGINES, CONFERENCES, CONTROL THEORY, ENGINE

CONTROL, PROPULSION SYSTEM PERFORMANCE

47
07 AIRCRAFTPROPULSIONANDPOWER

N81-13058"#National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EVALUATION OF A BULK CALORIMETER AND HEAT

BALANCE FOR DETERMINATION OF SUPERSONIC

COMBUSTOR EFFICIENCY

C. R. MCCLINTON and G. Y. ANDERSON Dec. 1980 45 p

refs

(NASA-TP-1739; L-13943) Avail: NTIS HC A03/MF A01

CSCL 21E

CALORIMETERS, COMBUSTION EFFICIENCY, HEAT

BALANCE, SUPERSONIC COMBUSTION RAMJET ENGINES

N81-15000"# National Aeronautics and Space Administration.

Dryden (Hugh L.) Flight Research Center, Edwards, Calif.

FLIGHT EVALUATION OF A SIMPLIFIED GROSS THRUST

CALCULATION TECHNIQUE USING AN FIO0 TURBOFAN

ENGINE IN AN F-15 AIRPLANE

F. J. KURTENBACH and F. W. BURCHAM, JR. Jan. 1981 21

p refs

(NASA-TP-1782; H-1118) Avail: NTIS HC A02/MF A0t CSCL

21E

F-15 AIRCRAFT, IN-FLIGHT MONITORING, JET THRUST,

TURBOFAN ENGINES

N81-16050"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

COLD-AIR INVESTIGATION OF FIRST STAGE OF 4-1/2-STAGE,

FAN DRIVE TURBINE WITH AVERAGE STAGE-LOADING

FACTOR OF 4.66

W. J. WHITNEY, T. P. MOFFITT, and F. P. BEHNING Jan. 1981

15 p refs

(NASA-TP-1780; E-461) Avail: NTIS HC A02/MF A01 CSCL

21E

CRITICAL VELOCITY, DESIGN ANALYSIS, FAN BLADES,

LOADS (FORCES)

N81-19121"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

SPECTRAL FLAME RADIANCE FROM A TUBULAR-CAN

COMBUSTOR

R. W. CLAUS Feb. 1981 15 p rets

(NASA.TP-1722; E-509) Avail: NTIS HC A02/MF A01 CSCL

21E

COMBUSTION CHAMBERS, FUEL-AIR RATIO,

HYDROCARBON FUELS, RADIANCE, SPECTRAL EMISSION

N81-20076"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

REASONS FOR LOW AERODYNAMIC PERFORMANCE OF

13.5-CENTIMETER-TIP-DIAMETER AIRCRAFT ENGINE

STARTER TURBINE

J. E. HAAS, R. J. ROELKE, and P. HERMANN (Sundstrand Corp.,

Rockford, II1.) Mar. 1981 18 p Presented at the SAE Aerospace

Meeting, Los Angeles, 13-16 Oct. 1980

(NASA-TP-18t0; E-540; AVRADCOM-TR-80-C-17) Avail: NTIS

HC A02/MF A01 CSCL 21E

AERODYNAMIC CHARACTERISTICS, AIRCRAFT ENGINES,

ENGINE STARTERS, TURBINE ENGINES

N81-21077"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

PERFORMANCE OF SEMI-TRANSPORTATION-COOLED LINER

IN HIGH-TEMPERATURE-RISE COMBUSTORS

J. D. WEAR, A. M. TROUT, and J. M SMITH Mar. 1981 20 p

refs

(NASA-TP-1806; E-494) Avail: NTIS HC A02/MF A01 CSCL

2tE

COMBUSTION CHAMBERS, COMBUSTION EFFICIENCY,

FUEL-AIR RATIO, LININGS

48

N81-24063"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

FUNDAMENTAL HEAT TRANSFER RESEARCH FOR GAS

TURBINE ENGINES

D. E. METZGER, ed. (Arizona State Univ.) 1980 68 p refs

Presented at a Workshop Held at Cleveland, 8-9 Oct. 1980

(NASA-CP-2178; E-666) Avail: NTIS HC A04/MF A01 CSCL

21E

COMPUTATIONAL FLUID DYNAMICS, CONFERENCES, FLUID

FLOW, GAS TURBINE ENGINES, HEAT TRANSFER, RESEARCH

AND DEVELOPMENT

N81-24065"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

ANALYSIS OF EFFECT OF FLAMEHOLDER CHARACTERISTICS

ON LEAN, PREMIXED, PARTIALLY VAPORIZED FUEL-AIR

MIXTURES QUALITY AND NITROGEN OXIDES EMISSIONS

L. P. COOPER May 1981 18 p refs

(NASA-TP-1842; E-563) Avail: NTIS HC A02/MF A01 CSCL

21E

COMBUSTION CHAMBERS, COMBUSTION EFFICIENCY,

EXHAUST EMISSION, FUEL-AIR RATIO, NITROGEN OXIDES

N81-31196"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

AIRCRAFT ENGINE DIAGNOSTICS

Jul. 1981 377 p refs Conf. held at Cleveland, 6-7 May t981

(NASA-CP-2190; E-845) Avail: NTIS HC A17/MF A0t CSCL

21E

AIRCRAFT ENGINES, CONFERENCES, ENGINE

MONITORING INSTRUMENTS, ENGINE TESTS, MAINTENANCE,

RELIABILITY ENGINEERING

N82-13142"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

NUMERICAL ANALYSIS OF THE SCRAMJET-INLET FLOW

FIELD BY USING TWO-DIMENSIONAL NAVIER-STOKES

EQUATIONS

A. KUMAR Dec. 1981 30 p refs

(NASA-TP-1940; L-14776) Avail: NTIS HC A03/MF A01

CSCL 21E

COMPUTER PROGRAMS, ENGINE INLETS, FINITE

DIFFERENCE THEORY, FLOW DISTRIBUTION, INLET FLOW,

NAVlER-STOKES EQUATION, SUPERSONIC COMBUSTION

RAMJET ENGINES

N82-13143"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EFFECT OF FUEL-AIR-RATIO NONUNIFORMITY ON EMISSIONS

OF NITROGEN OXIDES

V. J. LYONS Nov. 1981 14 p refs

(NASA-TP-1798; E-648) Avail: NTIS HC A02/MF A01 CSCL

21E

EXHAUST EMISSION, FUEL COMBUSTION, FUEL-AIR RATIO,

NITROGEN OXIDES, NONUNIFORM FLOW, PREMIXING

N82-14090"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

GAS TURBINE CERAMIC-COATED-VANE CONCEPT WITH

CONVECTION-COOLED POROUS METAL CORE

A. F. KASCAK (AVRADCOM Research and Technology Labs.,

Cleveland), C. H. LIEBERT, R. F. HANDSCHUH, and L. P.

LUDWIG Dec. 1981 14 p refs Sponsored in part by U.S.

Army Aviation Research and Development Command, St. Louis

(NASA-TP-1942; AVRADCOM-TR-81-C-7; E-732) Avail: NTIS

HC A02/MF A01 CSCL 21E

CERAMIC COATINGS, CONVECTION, GAS TURBINES, HEAT

TRANSFER, METAL SURFACES, POROUS MATERIALS,

THICKNESS, VANES
N82-15039"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

COMPUTER PROGRAM FOR AERODYNAMIC AND BLADING

DESIGN OF MULTISTAGE AXIAL-FLOW COMPRESSORS

J. E. CROUSE and W. T. GORRELL Dec. 1981 105 p refs

Prepared in cooperation with Army Aviation Research and

Development Command, St. Louis, Mo.

(NASA-TP-1946; AVRADCOM-TR-80-C-21; E-280) Avail: NTIS

HC A06/MF A01 CSCL 21E

AERODYNAMIC CHARACTERISTICS, AIRFOIL PROFILES,

COMPRESSIBLE FLOW, COMPRESSOR BLADES, COMPUTER

AIDED DESIGN, TURBOCOMPRESSORS

N82-15040°# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EFFECT OF FUEL INJECTOR TYPE ON PERFORMANCE AND

EMISSIONS OF REVERSE-FLOW COMBUSTOR

C. T. NORGREN and S. M RIDDLEBAUGH Dec. 1981 40 p

refs

(NASA-TP-1945; E-556) Avail: NTIS HC A03/MF A01 CSCL

21E

COMBUSTION CHAMBERS, FUEL INJECTION, GAS TURBINE

ENGINES, PERFORMANCE TESTS

N82-19222"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

PERFORMANCE OF SINGLE-STAGE AXIAL-FLOW TRANSONIC

COMPRESSOR WITH ROTOR AND STATOR ASPECT RATIOS

OF 1.63 AND 1.78, RESPECTIVELY, AND WITH DESIGN

PRESSURE RATIO OF 1.62

R. D. MOORE and L. REID Feb. 1982 112 p refs

(NASA-TP-1974; E-259) Avail: NTIS HC A06/MF A01 CSCL

21E

ASPECT RATIO, COMPRESSOR BLADES, COMPRESSOR

ROTORS, INTAKE SYSTEMS, PRESSURE RATIO, STATOR

BLADES, TRANSONIC COMPRESSORS

N82-20183"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

DAMPING SEALS FOR TURBOMACHINERY

G. L. VONPRAGENAU Mar. 1982 28 p refs

(NASA-TP-1987; NAS 1.60:1967; M-373) Avail: NTIS HC

A03/MF A01 CSCL 21E

DAMPERS (VALVES), ROTOR SPEED, SEALS (STOPPERS),

TURBOMACHINERY

N82-22269"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

PERFORMANCE OF SINGLE-STAGE AXIAL-FLOW TRANSONIC

COMPRESSOR WITH ROTOR AND STATOR ASPECT RATIOS

OF 1.63 AND 1.77, RESPECTIVELY, AND WITH DESIGN

PRESSURE RATIO OF 2.05

R. D. MOORE and L. REID Apr. 1982 116 p refs

(NASA-TP-2001; E-334; NAS 1.60:2001) Avail: NTIS HC

AOG/MF A01 CSCL 21E

AERODYNAMIC STALLING, AXIAL FLOW, COMPRESSOR

ROTORS, PRESSURE RATIO, ROTOR BLADES

(TURBOMACHINERY)

N62-25250"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

STGSTK: A COMPUTER CODE FOR PREDICTING MULTISTAGE

AXIAL FLOW COMPRESSOR PERFORMANCE BY A MEANLINE

STAGE STACKING METHOD

R. J. STEINKE May 1982 65 p refs

(NASA-TP-2020; E-551; NAS 1.60:2020) Avail: NTIS HC

A04/MF A01 CSCL 21E

AXIAL FLOW, COMPRESSOR EFFICIENCY, COMPUTER

PROGRAMS, FORTRAN, TURBOCOMPRESSORS

07 AIRCRAFT PROPULSION AND POWER

N82-31329"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

VENTURI NOZZLE EFFECTS ON FUEL DROP SIZE AND

NITROGEN OXIDE EMISSIONS

S. M. JOHNSON Aug. 1982 17 p refs

(NASA-TP-2028; E-1029; NAS 1.60:2028) Avail: NTIS HC

A02/MF A01 CSCL 21E

DROP SIZE, EXHAUST GASES, NITROGEN OXIDES, NOZZLE

FLOW, SPRAY CHARACTERISTICS, VENTURI TUBES

N82-33389"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

ROTOR TIP CLEARANCE EFFECTS ON OVERALL AND

BLADE-ELEMENT PERFORMANCE OF AXIAL-FLOW

TRANSONIC FAN STAGE

R. D. MOORE Sep. 1982 87 p refs

(NASA-TP-2049; E-559; NAS 1.60:2049) Avail: NTIS HC

A05/MF A01 CSCL 21E

AXIAL FLOW TURBINES, BLADE TIPS, CLEARANCES,

ROTOR BLADES

N83-10045"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

FURTHER INDUSTRIAL TESTS OF CERAMIC THERMAL

BARRIER COATINGS

C. H. LIEBERT and S. R. LEVINE Sep. 1982 10 p refs

(NASA-TP-2057; E-lt84; NAS 1.60:2057) Avail: NTIS HC

A02/MF A01 CSCL 21E

CERAMICS, DIESEL ENGINES, METAL BONDING, PLASMA

SPRAYING, THERMAL CONTROL COATINGS, THICKNESS

N83-11125"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

ANALYTICAL AND EXPERIMENTAL INVESTIGATION OF

STATOR ENDWALL CONTOURING IN A SMALL AXIAL-FLOW

TURBINE. 1: STATOR PERFORMANCE

J. E. HAAS Oct. 1982 26 p refs

(NASA-TP-2023; E-1180; NAS 1.60:2023;

AVRADCOM-TR-82-C-4) Avail: NTIS HC A03/MF A01 CSCL

21E

AXIAL FLOW TURBINES, CONTOURS, FLOW DISTRIBUTION,

KINETIC ENERGY, STATORS, WALLS

N63-11126"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

FILM THICKNESS MEASUREMENT FOR SPIRAL GROOVE AND

RAYLEIGH STEP LIFT PAD SELF-ACTING FACE SEALS

E. DIRUSSO Oct. 1982 21 p refs

(NASA-TP-2058; E-1169; NAS 1.60:2058) Avail: NTIS HC

A02/MF A01 CSCL 21E

CLEARANCES, FILM THICKNESS, GAS BEARINGS, SEALS

(STOPPERS), TORQUE

N63-17547"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

AERODYNAMIC EFFECT OF A HONEYCOMB ROTOR TIP

SHROUD ON A 50.8-CENTIMETER-TIP-DIAMETER CORE

TURBINE

T. P. MOFFITT and W. J. WHITNEY Jan. 1983 19 p refs

(NASA-TP-2112; E-1261; NAS 1.60:2112) Avail: NTIS HC

A02/MF A01 CSCL 21E

AERODYNAMIC CHARACTERISTICS, BLADE TIPS, COOLANTS, ROTORS, SHROUDED TURBINES, TURBOMACHINERY

49
07 AIRCRAFT PROPULSION AND POWER

N83-18727" # National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

IGNITION OF SIH4-H2-O2-N2 BEHIND REFLECTED SHOCK

WAVES

A. G. MCLAIN, C. J. JACHIMOWSKI, and R. C. ROGERS Feb.

1983 17 p refs

(NASA-TP-2114; L-15534; NAS 1.60:2114) Avail: NTIS HC

A02/MF A01 CSCL 21E

HYDROGEN, IGNITION, MIXTURES, OXYGEN, REACTION

KINETICS, SHOCK WAVES, SILANES

N83-23309"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EFFECT OF FLAMEHOLDER PRESSURE DROP ON EMISSIONS

AND PERFORMANCE OF PREMIXEO-PREVAPORIZED

COMBUSTORS

R. A. DUERR and V. J. LYONS Apr. 1983 22 p refs

(NASA-TP-2131; E-1358; NAS 1.60:2131) Avail: NTIS HC

A02/MF A01 CSCL 21E

COMBUSTION EFFICIENCY, EXHAUST EMISSION, FLAME

HOLDERS, PREMIXED FLAMES, PRESSURE REDUCTION,

PREVAPORIZATION

N83-24509"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

PARTICLE SIZING BY MEASUREMENT OF

FORWARD-SCATTERED LIGHT AT TWO ANGLES

D. R. BUCHELE May 1983 25 p refs

(NASA-TP-2156; E-1179; NAS 1.60:2156) Avail: NTIS HC

A02/MF A01 CSCL 20F

FORWARD SCATTERING, GAS TURBINE ENGINES, LIGHT

SCATTERING, PARTICLE SIZE DISTRIBUTION, SPRAYERS

N83-25712"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

DESIGN ANALYSIS OF A SELF-ACTING SPIRAL-GROOVE RING

SEAL FOR COUNTER-ROTATING SHAFTS

E. DIRUSSO May 1983 12 p refs

(NASA-TP-2142; E-1253; NAS 1.60:2142) Avail: NTIS HC

A02/MF A01 CSCL ltA

COMPUTER PROGRAMS, GAS BEARINGS, GROOVES, LIFT,

SEALS (STOPPERS), TURBOFAN ENGINES

N83-26839"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

THRUST PERFORMANCE OF A VARIABLE-GEOMETRY,

DIVERGENT EXHAUST NOZZLE ON A TURBOJET ENGINE AT

ALTITUDE

D M. STRAIGHT and R. R. COLLOM Jun. 1983 39 p refs

(NASA-TP-2171; E-1451; NAS 1.60:2171) Avail: NTIS HC

AO3/MF A01 CSCL 21E

EXHAUST NOZZLES, THRUST REVERSAL, THRUST VECTOR

CONTROL, TURBOJET ENGINES

N83-29208"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

COMBUSTION FUNDAMENTALS RESEARCH

Washington Mar. 1983 252 p refs Proc. of conf. held in

Cleveland, 21.22 Oct. 1982

(NASA-CP-2288; E-1525; NAS 1.55:2268) Avail: NTIS HC

A12/MF A01 CSCL 21E

AEROSPACE INDUSTRY, CHEMICAL REACTIONS,

COMBUSTION PHYSICS, CONFERENCES, GAS TURBINES,

HYDRODYNAMICS, PREMIXlNG, REACTION KINETICS

50

N83-30431"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

INCIDENCE LOSS FOR FAN TURBINE ROTOR BLADE IN

TWO-DIMENSIONAL CASCADE

J.F. KLINE, T. P. MOFFITT, and R. G. STABE Jul. 1983 11 p

refs

(NASA-TP-2188; E-1567; NAS 1.60:2188) Avail: NTIS HC

A02/MF A01 CSCL 21E

ENERGY DISSIPATION, FAN BLADES, INCIDENCE, ROTOR

AERODYNAMICS, TURBOFAN ENGINES, TWO DIMENSIONAL

FLOW

N83-32806"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

MODELING INTERFACE MOTION OF COMBUSTION (MINOC).

A COMPUTER CODE FOR TWO-DIMENSIONAL, UNSTEADY

TURBULENT COMBUSTION

A. F. GHONEIM (California Univ., Berkeley), C. J. MAREK, and A.

K. OPPENHEIM (California Univ., Berkeley) Aug. 1983 19 p

refs

(NAG3-313)

(NASA-TP-2132; E-1569; NAS 1.60:2132) Avail: NTIS HC

AO2/MF A01 CSCL 21E

COMBUSTIBLE FLOW, FLAME PROPAGATION, TURBULENT

FLOW, TWO DIMENSIONAL FLOW, VORTICES

N83-32807"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

COMPUTER CODE FOR OFF-DESIGN PERFORMANCE

ANALYSIS OF RADIAL-INFLOW TURBINES WITH ROTOR

BLADE SWEEP

P. L. MEITNER (Army Aviation Research and Development

Command, St. Louis, Mo.) and A. J. GLASSMAN Aug. 1983

26 p refs

(NASA-TP-2199; NAS 1.60:2199; AVRADCOM-TR-83-C-4) Avail:

NTIS HC A03/MF A01 CSCL 21E

RADIAL FLOW, ROTOR BLADES (TURBOMACHINERY),

TURBINES

N83-33893"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

PRELIMINARY TESTS OF AN ADVANCED

HIGH-TEMPERATURE COMBUSTION SYSTEM

J. D. WEAR, A. M. TROUT, J. M. SMITH, and R. E. JACOBS

Sep. 1983 33 p refs

(NASA-TP-2203; E-1633; NAS 1.60:2203) Avail: NTIS HC

A03/MF A01 CSCL 21E

AIR FLOW, COMBUSTION, COMBUSTION CHAMBERS,

COOLING, ENGINE INLETS, IGNITION, STOICHIOMETRY

N83-34941"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EFFECTS OF PERCENTAGE OF BLOCKAGE AND

FLAMEHOLDER DOWNSTREAM COUNTERBORES ON LEAN

COMBUSTION LIMITS OF PREMIXED, PREVAPORIZED

PROPANE-AIR MIXTURE

M. A. B. FERNANDEZ Sep. 1983 11 p refs

(NASA-TP-2227; E-1588; NAS 1.60:2227) Avail: NTIS HC

A02/MF A01 CSCL 21E

COMBUSTION, COMBUSTION CHAMBERS, FLAMES, FUEL

INJECTION, MIXTURES, PROPANE

N84-10055"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

AIRCRAFT ELECTRIC SECONDARY POWER

Washington Jun. 1983 199 p refs Workshop held in

Cleveland, 14-15 Sep. 1982

(NASA-CP-2282; E-1632; NAS 1.55:2282) Avail: NTIS HC

A09/MF A01 CSCL 01C

AUXILIARY POWER SOURCES, CONFERENCES, ELECTRIC

GENERATORS, ELECTRIC POWER SUPPLIES, FIGHTER

AIRCRAFT, JET ENGINES
N84-11171"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

If100 MULTIVARIABLE CONTROL SYNTHESIS PROGRAM.

COMPUTER IMPLEMENTATION OF THE F100 MULTIVARIABLE

CONTROL ALGORITHM

J. F. SOLDER Oct. 1983 46 p

(NASA-TP-2231; E-1496; NAS 1.60:2231) Avail: NTIS HC

A03/MF A01 CSCL 21E

CONTROL THEORY, ENGINE DESIGN, TURBOFAN

ENGINES

N84-16181"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

DYNAMIC BEHAVIOR OF SPIRAL-GROOVE AND

RAYLEIGH-STEP SELF-ACTING FACE SEALS

E. DIRUSSO Jan. 1984 19 p refs

(NASA-TP-2266; NAS 1.60:2266; E-1754) Avail: NTIS HC

A02/MF A01 CSCL 21E

DYNAMIC RESPONSE, FILM THICKNESS, GAS BEARINGS,

HYDRODYNAMICS, SEALS (STOPPERS), VIBRATION

N84-20525"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

COMBUSTION FUNDAMENTALS RESEARCH

Washington Apr. 1984 303 p refs Conf. held in Cleveland,

16-18 Apr. 1984

(NASA-CP-2309; E-2062; NAS 1.55:2309) Avail: NTIS HC

A14/MF A01 CSCL 21E

COMBUSTION PHYSICS, COMPUTATIONAL FLUID

DYNAMICS, CONFERENCES, FLUID FLOW, FUEL SPRAYS, GAS

TURBINE ENGINES

N84-20562"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

FORMULATION OF BLADE-FLUTTER SPECTRAL ANALYSES

IN STATIONARY REFERENCE FRAME

A. P. KURKOV Mar. 1984 32 p refs

(NASA-TP-2296; E-1888; NAS 1.60:2296) Avail: NTIS HC

A03/MF A01 CSCL 21E

AEROELASTICITY, AIRFOILS, FLUTTER, SPECTRUM

ANALYSIS

N84-21549"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

ANALYSIS OF A TOPPING-CYCLE, AIRCRAFT,

GAS-TURBINE-ENGINE SYSTEM WHICH USES CRYOGENIC

FUEL

G. E. TURNEY and L. H. FISHBACH Apr. 1984 23 p refs

Presented at the AIAA Aircraft Systems and Operational Meeting,

Fort Worth, Tex., 17-19 Oct. 1983

(NASA-TP-2294; E-1735; NAS 1.60:2294) Avail: NTIS HC

A02/MFA01 CSCL21E

AIRCRAFT ENGINES, AIRCRAFT FUELS, GAS TURBINE

ENGINES, HYDROGEN FUELS, LIQUID HYDROGEN,

THERMODYNAMIC CYCLES, TOPPING CYCLE ENGINES

N84-23630"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

ASSESSMENT OF ALTERNATIVE AIRCRAFT FUELS

Washington Apr. 1984 188 p refs Conf. held in Cleveland,

2-3 Nov. 1983

(NASA-CP-2307; E-1878; NAS 1.55:2307) Avail: NTIS HC

A09/MF A01 CSCL 21D

COMBUSTION, CONFERENCES, CRUDE OIL, FUEL

PRODUCTION, FUEL SYSTEMS, GAS TURBINE ENGINES, JET

ENGINE FUELS, PETROLEUM PRODUCTS

07 AIRCRAFT PROPULSION AND POWER

N84-24578"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

LEWIS RESEARCH CENTER SPIN RIG AND ITS USE IN

VIBRATION ANALYSIS OF ROTATING SYSTEMS

G. V. BROWN, R. E. KIELB, E. H. MEYN, R. E. MORRIS, and S.

J. POSTA May 1984 19 p refs

(NASA-TP-2304; E-1829; NAS 1.60:2304) Avail: NTIS HC

A02/MFA01 CSCL21E

COMPRESSOR ROTORS, DIGITAL TECHNIQUES, DYNAMIC

STRUCTURAL ANALYSIS, SHAKERS, SPIN TESTS, TURBINE

ENGINES, TURBOMACHINERY, VIBRATION, VIBRATION

SIMULATORS

N84-28795"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

DETAILED FLOW MEASUREMENTS IN CASING BOUNDARY

LAYER OF 429-METER-PER-SECOND-TIP-SPEED TWO-STAGE

FAN

W. T. GORRELL Jan. 1984 33 p refs Prepared in cooperation

with Army Aviation Research and Development Command,

Cleveland

(NASA-TP-2052; E-219; NAS 1.60:2052;

AVRADCOM-TR-81-C-28) Avail: NTIS HC A03/MF A01 CSCL

21E

FAN BLADES, FLOW MEASUREMENT, TURBINE BLADES,

TURBOMACHINERY

N84-32388*# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

ANALYTICAL AND EXPERIMENTAL INVESTIGATION OF

STATOR ENDWALL COUNTOURING IN A SMALL AXIAL-FLOW

TURBINE

J. E. HAAS and R. J. BOYLE Sep, 1984 23 p refs Prepared

in cooperation with Army Research and Technology Labs.,

Cleveland

(NASA-TP-2309; E-2050; NAS 1.60:2309; AVSCOM-TR-84-C-5)

Avail: NTIS HC A02/MF A01 CSCL 21E

AXIAL FLOW TURBINES, COMPUTER PROGRAMS,

CONTOURS, PRESSURE GRADIENTS, STATORS, TIP DRIVEN

ROTORS

N85-10064"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

COMBUSTION GAS PROPERTIES I-ASTM JET A FUEL AND

DRY AIR

R. E. JONES, A. M. TROUT, J. D. WEAR, and B. J. MCBRIDE

Oct. 1984 12 p refs Document incl. microfiche supplement

(NASA-TP-2359; NAS 1.60:2359) Avail: NTIS HC E03/MF A01

CSCL 21E

COMBUSTION PRODUCTS, FUEL COMBUSTION, GAS

COMPOSITION, GASES, JET ENGINE FUELS, THERMODYNAMIC

PROPERTIES

N85-10065"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

COMPARISON OF NUMERICAL TECHNIQUES FOR

INTEGRATION OF STIFF ORDINARY DIFFERENTIAL

EQUATIONS ARISING IN COMBUSTION CHEMISTRY

K. RADHAKRISHNAN Oct. 1984 41 p refs Sponsored in

part by Michigan Univ. and NRC

(NAG3.147; NAG3-294)

(NASA-TP-2372; E-2149; NAS 1.60:2372) Avail: NTIS HC

A03/MF A01 CSCL21E

ALGORITHMS, COMBUSTION CHEMISTRY, COMBUSTION

EFFICIENCY, NUMERICAL ANALYSIS, REACTION KINETICS,

STIFFNESS

51
07 AIRCRAFT PROPULSION AND POWER

N85-21168"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

COMBUSTION GAS PROPERTIES. 2: NATURAL GAS FUEL

AND DRY AIR

J. D. WEAR, R. E JONES, A. M. TROUT, and B. J. MCBRIDE

Apr. 1985 12 p refs

(NASA-TP-2435; E-2435; NAS 1.60:2435) Avail: NTIS HC

A02/MFA01 CSCL 21E

COMBUSTION, COMBUSTION PRODUCTS, FUEL-AIR RATIO,

HYDROCARBON FUELS, NATURAL GAS

N85-22394"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

EFFECTS OF INLET DISTORTION ON A STATIC PRESSURE

PROBE MOUNTED ON THE ENGINE HUB IN AN F-15

AIRPLANE

D. L. HUGHES, L. P. MYERS, and K. G. MACKALL 1985 23 p

refs

(NASA-TP-2411; H-1182; NAS 1.60:2411) Avail: NTIS HC

A02/MF A01 CSCL 21E

AIRCRAFT ENGINES, ENGINE FAILURE, F-15 AIRCRAFT,

INLET FLOW, STATIC PRESSURE, TURBOFAN ENGINES

N85-22395"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

IGNITION OF MIXTURES OF SIH SUB 4, CH SUB 4, O SUB 2,

AND AR OR N SUB 2 BEHIND REFLECTED SHOCK WAVES

A G MCLA1N, C. J. JACHIMOWSKI, and R C. ROGERS Apr.

1985 17 p refs

(NASA-TP-2415; L-15881; NAS 1.60:2415) Avail: NTIS HC

A02/MF A01 CSCL 21E

FUEL COMBUSTION, IGNITION, METHANE, REACTION

KINETICS, SHOCK WAVES, SILANES

N85-25261"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

PERFORMANCE AND SURGE LIMITS OF A TF30-P-3

TURBOFAN ENGINE/AXISYMMETRIC MIXED-COMPRESSION

INLET PROPULSION SYSTEM AT MACH 2.5

J. F. WASSERBAUER, H E. NEUMANN, and R. J. SHAW May

1985 21 p refs

(NASA-TP-2461; E-2412; NAS 1.60:2461) Avail: NTIS HC

A02/MF A01 CSCL21E

ANGLE OF ATTACK, INLET AIRFRAME CONFIGURATIONS,

INTAKE SYSTEMS, PROPULSION SYSTEM PERFORMANCE,

TURBOFAN ENGINES

N85-28944"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

ADVANCED SECONDARY POWER SYSTEM FOR TRANSPORT

AIRCRAFT

A. C. HOFFMAN, t. G. HANSEN, R. F. BEACH, R. M. PLENCNER,

R. P. DENGLER, K S. JEFFERIES, and R. J. FRYE May 1985

38 p refs

(NASA-TP-2463; E-2434; NAS 1.60:2463) Avail: NTIS HC

A03/MFA01 CSCL 21E

AIRCRAFT POWER SUPPLIES, COMPUTER AIDED DESIGN,

FLIGHT CONTROL, TRANSPORT AIRCRAFT

N85-31058"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

COMBUSTION GAS PROPERTIES. PART 3: HYDROGEN GAS

FUEL AND DRY AIR

J. D WEAR, R. E. JONES, B. J. MCBRIDE, and R. A. BEYERLE

(Sverdrup Technology, Inc.) Jun. 1985 12 p refs Doc.

includes microfiche supplement

(NAS3-24105)

(NASA-TP-2477; E-2545; NAS 1.60:2477) Avail: NTIS HC

A02/MF A01 CSCL 07D

CHEMICAL EQUILIBRIUM, COMBUSTION, COMPUTER

PROGRAMS, GAS COMPOSITION. GAS MIXTURES, HYDROGEN

FUELS

N86-15313"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

DYNAMIC RESPONSE OF FILM THICKNESS IN

SPIRAL-GROOVE FACE SEALS

E. DIRUSSO Dec. 1985 22 p refs

(NASA-TP-2544; E-2683; NAS 1.60:2544) Avail: NTIS HC

A02/MF A01 CSCL 21E

DYNAMIC RESPONSE, FILM THICKNESS, GAS BEARINGS,

GROOVES, SEALS (STOPPERS)

N86-22576'# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

STATIC INVESTIGATION OF CIRCULAR-TO-RECTANGULAR

TRANSITION DUCTS FOR HIGH-ASPECT-RATIO

NONAXlSYMMETRIC NOZZLES

J. R. BURLEY, II, L. S. BANGERT, and J. R. CARLSON Mar.

1986 55 p refs

(NASA-TP-2534; L-15874; NAS 1.60:2534) Avail: NTIS HC

A04/MF A01 CSCL 21E

HIGH ASPECT RATIO, STATIC TESTS, WIND TUNNEL

TESTS

N86-24694"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

LOW-SPEED PERFORMANCE OF AN AXISYMMETRIC,

MIXED-COMPRESSION, SUPERSONIC INLET WITH AUXILIARY

INLETS

C. J. TREFNY and J. W. WASSERBAUER Feb. 1986 63 p

refs

(NASA-TP-2557; E-2771; NAS 1.60:2557) Avail: NTIS HC

A04/MF A01 CSCL 21E

INTERNAL COMPRESSION INLETS, LOW SPEED,

SUPERSONIC AIRCRAFT, SUPERSONIC INLETS

N86-25342"# National Aeronautics and Space Administration.

Dryden (Hugh L.) Flight Research Center, Edwards, Calif,

DIGITAL ELECTRONIC ENGINE CONTROL (DEEC) FLIGHT

EVALUATION IN AN F-15 AIRPLANE

Mar. t984 243 p refs Symposium held in Edwards, Calif.,

25-26 May 1983

(NASA-CP-2298; H-1201; NAS 1.55:2298) Avail: NTIS HC

All/MFA01 CSCL 21E

CONFERENCES, DIGITAL TECHNIQUES, ENGINE CONTROL,

F-15 AIRCRAFT, FLIGHT TESTS, NUMERICAL CONTROL,

THRUST CONTROL, TURBOFAN ENGINES

08

AIRCRAFT STABILITY AND CONTROL

includes aircraft handling qualities; piloting; flight controls; and

autopilots.

N78-12100"# National Aeronautics and Space Administration.

Dryden (Hugh L.) Flight Research Center, Edwards, Calif.

PHUGOID CHARACTERISTICS OF A YF-12 AIRPLANE WITH

VARIABLE-GEOMETRY INLETS OBTAINED IN FLIGHT TESTS

AT A MACH NUMBER OF 2.9

B. G. POWERS Dec. 1977 45 p refs

(NASA-TP-1107; H-953) Avail: NTIS HC A03/MF A01 CSCL

01C

FLIGHT TESTS, INTAKE SYSTEMS, LONGITUDINAL

CONTROL, OSCILLATIONS, YF-12 AIRCRAFT

52
N78-13071"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

_.EFFECTS OF CONTROL INPUTS ON THE ESTIMATION OF

STABILITY AND CONTROL PARAMETERS OF A LIGHT

AIRPLANE

R. L. CANNADAY and W. T. SUIT Dec. 1977 72 p refs

(NASA-TP-1043; L-11355) Avail: NTIS HC A04/MF A01

CSCL 01C

AERODYNAMIC STABILITY, CONTROLLABILITY, ESTIMATING, INPUT/OUTPUT ROUTINES, LIGHT AIRCRAFT, PARAMETERIZATtON

N78-16063"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

STUDY OF THE APPLICATION OF AN IMPLICIT

MODEL-FOLLOWING FLIGHT CONTROLLER TO LIFT-FAN

VTOL AIRCRAFT

V. K. MERRICK Nov. 1977 180 p refs

(NASA-TP-1040; A-6712) Avail: NTIS HC A09/MF A01 CSCL

01C

AUTOMATIC FLIGHT CONTROL, CONTROLLABILITY, LIFT

FANS, VERTICAL TAKEOFF AIRCRAFT

N78-18076"# National Aeronautics and Space Administration.

Dryden (Hugh L.) Flight Research Center, Edwards, Calif.

ANALYTICAL STUDY OF RIDE SMOOTHING BENEFITS OF

CONTROL SYSTEM CONFIGURATIONS OPTIMIZED FOR PILOT

HANDLING QUALITIES

B. G. POWERS Feb. 1978 60 p refs

(NASA-TP-1148; H-922) Avail: NTIS HC A04/MF A01 CSCL

01C

AIRCRAFT CONTROL, CONTROL CONFIGURED VEHICLES,

PILOT PERFORMANCE, RIDING QUALITY

N78-20139"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SIMULATOR EVALUATION OF A FLIGHT-PATH-ANGLE

CONTROL SYSTEM FOR A TRANSPORT AIRPLANE WITH

DIRECT LIFT CONTROL

W. W. KELLEY Mar. 1978 33 p refs

(NASA-TP-1116; L-11947) Avail: NTIS HC A03/MF A01

CSCL 01C

AIRCRAFT CONTROL, FLIGHT PATHS, FLIGHT

SIMULATORS, LIFT, TRANSPORT AIRCRAFT

N78-20140"# National Aeronautics and Space Administration.

Dryden (Hugh L.) Flight Research Center, Edwards, Calif.

FLIGHT EVALUATION OF THE TRANSONIC STABILITY AND

CONTROL CHARACTERISTICS OF AN AIRPLANE

INCORPORATING A SUPERCRITICAL WING

N. W. MATHENY and D. H. GATLIN Feb. 1978 61 p refs

(NASA-TP-1167; H-916) Avail: NTIS HC A04/MF A01 CSCL

01C

AERODYNAMIC STABILITY, AIRCRAFT CONTROL, FLIGHT

TESTS, SUPERCRITICAL WINGS, TRANSONIC SPEED

N78-20142"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

STUDY OF THE USE OF A NONLINEAR, RATE-LIMITED FILTER

ON PILOT CONTROL SIGNALS

J. J. ADAMS Apr. 1978 41 p refs

(NASA-TP-1147; L-lt762) Avail: NTIS HC A03/MF A01

CSCL 01C

AIRCRAFT NOISE, AIRCRAFT PERFORMANCE, FEEDBACK

CONTROL, NONLINEAR FILTERS, PILOT PERFORMANCE

08 AIRCRAFT STABILITY AND CONTROL

N78-20143"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

PILOT-MODEL ANALYSIS AND SIMULATION STUDY OF

EFFECT OF CONTROL TASK DESIRED CONTROL RESPONSE

J. J. ADAMS, J. GERA, and J. B. JAUDON Apr. 1978 46 p

refs

(NASA-TP-1140) Avail: NTIS HC A03/MF A01 CSCL 01C

AIRCRAFT CONTROL, ALTITUDE CONTROL, F-8 AIRCRAFT,

FLIGHT SIMULATION, PILOT PERFORMANCE

N78-21160"# National Aeronautics and Space Administration.

Dryden (Hugh L.) Flight Research Center, Edwards, Calif.

RESULTS FROM FLIGHT AND SIMULATOR STUDIES OF A

MACH 3 CRUISE LONGITUDINAL AUTOPILOT

G. B. GILYARD and J. W. SMITH Apr. 1978 85 p refs

(NASA-TP-1180; H-940) Avail: NTIS HC A05/MF A01 CSCL

01D

CONTROL SIMULATION, FLIGHT TESTS, LONGITUDINAL

CONTROL, MACH NUMBER

N78-23100"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

OPTIMAL GUIDANCE AND CONTROL FOR INVESTIGATING

AIRCRAFT NOISE-IMPACT REDUCTION

E. C. STEWART and T. M. CARSON May 1978 58 p refs

(NASA-TP-1237; A-7121) Avail: NTIS HC A04/MF A0t CSCL

01C

AIRCRAFT NOISE, NOISE REDUCTION, THRUST VECTOR

CONTROL

N78-25101"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

MODAL CONTROL THEORY AND APPLICATION TO AIRCRAFT

LATERAL HANDLING QUALITIES DESIGN

S. SRINATHKUMAR Jun. 1978 63 p refs

(NASA-TP-1234; L-12177) Avail: NTIS HC A04/MF A01

CSCL 01C

AIRCRAFT DESIGN, CONTROL THEORY, CONTROLLABILITY,

EIGENVALUES, EIGENVECTORS

N78-26151"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

A FLIGHT INVESTIGATION OF THE STABILITY, CONTROL,

AND HANDLING QUALITIES OF AN AUGMENTED JET FLAP

STOL AIRPLANE

R. F. VOMASKE, R. C. INNIS, B. E. SWAN (Canadian Armed

Forces, Ottawa), and S. W. GROSSMITH (Canadian Dept. of

Transport, Ottawa) Jun. 1978 147 p refs

(NASA-TP-1254; A-7246) Avail: NTIS HC A07/MF A01 CSCL

01C

AIRCRAFT CONTROL, AIRCRAFT STABILITY, SHORT

TAKEOFF AIRCRAFT

N78-27136"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF A

FIGHTER MODEL WITH A CLOSE-COUPLED CANARD AT

MACH NUMBERS FROM 0.40 TO 1.20

R. J. RE and F. J. CAPONE Jul. 1978 80 p refs

(NASA-TP-1206; L-12081) Avail: NTIS HC A05/MF A01

CSCL 01C

AERODYNAMIC CHARACTERISTICS, AIRCRAFT MODELS,

CANARD CONFIGURATIONS

N78-27138"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECTS OF ERRORS ON DECOUPLED CONTROL SYSTEMS

H. A. HAMER and K. G. JOHNSON Jul. 1978 86 p refs

(NASA-TP-1184; L-11959) Avail: NTIS HC AO5/MF A01

CSCL 01C

DECOUPLING, ERROR ANALYSIS, LONGITUDINAL

CONTROL, SHORT TAKEOFF AIRCRAFT

53
08 AIRCRAFTSTABILITYANDCONTROL

N78-30141"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SIMULATION STUDY OF THE OSCILLATORY LONGITUDINAL

MOTION OF AN AIRPLANE AT THE STALL

W. H. PHILLIPS Aug. 1978 43 p refs

(NASA-TP-1242; L-12064) Avail: NTIS HC A03/MF A01

CSCL 01C

AERODYNAMIC STALLING, FLIGHT SIMULATION,

LONGITUDINAL STABILITY

N79-10068"# National Aeronautics and Space Administration.

Dryden (Hugh L.) Flight Research Center, Edwards, Calif.

FLIGHT-DETERMINED STABILITY AND CONTROL

DERIVATIVES FOR THE F-111 TACT RESEARCH AIRCRAFT

A. G. SIM and R. E. CURRY Oct. 1978 78 p refs

(NASA-TP-1350; H-1004) Avail: NTIS HC A05/MF A01 CSCL

01C

AIRCRAFT STABILITY, F-111 AIRCRAFT, STABILITY

DERIVATIVES

N79-13056"# National Aeronautics and Space Administration.

Dryden (Hugh L.) Flight Research Center, Edwards, Calif.

FLIGHT COMPARISON OF THE TRANSONIC AGILITY OF THE

F-111A AIRPLANE AND THE F-111 SUPERCRITICAL WING

AIRPLANE

E. L. FRIEND and G. M. SAKAMOTO Dec. 1978 78 p refs

(NASA-TP-1368; H-985) Avail: NTIS HC A05/MF A01 CSCL

01C

AERODYNAMIC CHARACTERISTICS, ANIONS, F-111

AIRCRAFT, SUPERCRITICAL WINGS, TRANSONIC FLIGHT

N79-13057"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

A NONLINEAR TRAJECTORY COMMAND GENERATOR FOR

A DIGITAL FLIGHT-CONTROL SYSTEM

L. S. CICOLANI and S. WEISSENBERGER Nov. 1978 114 p

refs

(NASA-TP-1221; A-7074) Avail: NTIS HC A06/MF A01 CSCL

01C

AUTOMATIC FLIGHT CONTROL, DIGITAL SYSTEMS,

NONLINEAR SYSTEMS, TRAJECTORY CONTROL, V/STOL

AIRCRAFT

N79-14110"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

THEORETICAL STUDY OF THE EFFECT OF WIND VELOCITY

GRADIENTS ON LONGITUDINAL STABILITY AND CONTROL

IN CLIMBING AND LEVEL FLIGHT

W. L. SHERMAN Dec. 1978 21 p refs

(NASA-TP-1332; L-12273) Avail: NTIS HC A02/MF A01

CSCL 01C

CLIMBING FLIGHT, LONGITUDINAL CONTROL, LONGITUDINAL STABILITY, WIND VELOCITY

N79-.15970"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

DESIGN AND ANALYSIS OF AN ACTIVE JET CONTROL

SYSTEM FOR HELICOPTER SLING LOADS M.S. Thesis - Old

Dominion Univ.

M. D. PARDUE and J. D. SHAUGHNESSY Jan. 1979 35 p

refs

(NASA-TP-1397; L-11836) Avail: NTIS HC A03/MF A01

CSCL 01C

HELICOPTERS, JET CONTROL, MATERIALS HANDLING

54

N79-17872"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

CONFIGURATION MANAGEMENT AND AUTOMATIC CONTROL

OF AN AUGMENTOR WING AIRCRAFT WITH VECTORED

THRUST

L. S. CICOLANI, B. SRIDHAR, and G. MEYER Mar. 1979 138

p refs

(NASA-TP-1222; A-7099) Avail: NTIS HC A07/MF A01 CSCL

01C

FLIGHT CONTROL, POWERED LIFT AIRCRAFT,

TRAJECTORY CONTROL, V/STOL AIRCRAFT

N79-22113"# National Aeronautics and Space Administration.

Dryden (Hugh L.) Flight Research Center, Edwards, Calif.

IMPORTANT FACTORS IN THE MAXIMUM LIKELIHOOD

ANALYSIS OF FLIGHT TEST MANEUVERS

K. W. ILIFF, R. E. MAINE, and T. D. MONTGOMERY Apr. 1979

44 p refs

(NASA-TP-1459; H-1076) Avail: NTIS HC A03/MF A01 CSCL

01C

DYNAMIC TESTS, FLIGHT TESTS, MAXIMUM LIKELIHOOD

ESTIMATES, NASA PROGRAMS

N79-27182"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

A COMPARISON OF THE V/STOL HANDLING QUALITIES OF

THE VAK-191B WITH THE REQUIREMENTS OF AGARD

REPORT 577 AND MIL-F-83300

S. B. ANDERSON Jul. 1979 38 p refs

(NASA-TP-1494; A-7117) Avail: NTIS HC A03/MF A01 CSCL

01C

CONTROLLABILITY, V/STOL AIRCRAFT, VERTICAL

TAKEOFF AIRCRAFT

N79-28186"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

PREDICTING DYNAMIC PERFORMANCE LIMITS FOR

SERVOSYSTEMS WITH SATURATING NONLINEARITIES

J. A. WEBB, JR. and R. A. BLECH Jut. 1979 52 p refs

(NASA-TP-1488; Eo9903) Avail: NTIS HC A04/MF A01 CSCL

01C

DYNAMIC RESPONSE, NONLINEAR SYSTEMS, SERVOMECHANISMS

N79-29195"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

DESCRIPTION OF THE VTOL APPROACH AND LANDING

TECHNOLOGY (VALT) CH-47 RESEARCH SYSTEM

J. R. KELLY, F. R. NIESSEN, J. F. GARREN, JR., and T. S.

ABBOTT Aug. 1979 57 p refs

(NASA-TP-1436; L-t2781) Avail: NTIS HC A04/MF A01

CSCL 01C

AIRBORNE/SPACEBORNE COMPUTERS, CH-47 HELICOPTER, FLIGHT CONTROL, SYSTEMS ENGINEERING, VERTICAL

LANDING, VERTICAL TAKEOFF

N79-31223"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

THEORETICAL AND EXPERIMENTAL INVESTIGATION OF

GROUND-INDUCED EFFECTS FOR A LOW-ASPECT-RATIO

HIGHLY SWEPT ARROW-WING CONFIGURATION

P. L. COL, JR. and J. L. THOMAS Washington Sep. 1979

102 p refs

(NASA-TP-1508; L-13088) Avail: NTIS HC A06/MF A01

CSCL 01C

AERODYNAMIC CHARACTERISTICS, ARROW WINGS,

GROUND EFFECT (AERODYNAMICS), V/STOL AIRCRAFT
N79-33218"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

FIXED-BASE SIMULATION STUDY OF DECOUPLED

LONGITUDINAL CONTROLS DURING APPROACH AND

LANDING OF A MEOIUM JET TRANSPORT IN THE PRESENCE

OF WIND SHEAR

G. K. MILLER, JR. Oct. 1979 69 p

(NASA-TP-1519; L-12842) Avail: NTIS HC AO4/MF A01

CSCL 01C

AIRCRAFT CONTROL, CONTROL SIMULATION, LONGITUDINAL CONTROL, WIND SHEAR

N80-13052"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECTS OF RELAXED STATIC LONGITUDINAL STABILITY

ON A SINGLE-STAGE-TO-ORBIT VEHICLE DESIGN

D. C. FREEMAN, JR. and A. W. WILHITE Washington Dec.

1979 138 p refs

(NASA-TP-1594; L-t3243) Avail: NTIS HC A07/MF A01

CSCL 22B

AERODYNAMIC CHARACTERISTICS, LONGITUDINAL

STABILITY, SPACECRAFT CONFIGURATIONS, SPACECRAFT

DESIGN

N80-14136"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SIMULATOR STUDY OF STALL/POST-STALL

CHARACTERISTICS OF A FIGHTER AIRPLANE WITH RELAXED

LONGITUDINAL STATIC STABILITY

L. T. NGUYEN, M E. OGBURN, W. P. GILBERT, K. S. KIBLER,

P. W. BROWN, and P. L. DEAL Washington Dec. 1979 226

P

(NASA-TP-1538; L-12854) Avail: NTIS HC A11/MF A01

CSCL 01C

AERODYNAMIC STALLING, F-16 AIRCRAFT, FLIGHT

SIMULATION, LONGITUDINAL STABILITY, STATIC STABILITY

N80-15138*# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

EFFECTS OF PRIMARY ROTOR PARAMETERS ON FLAPPING

DYNAMICS

R. T. N. CHEN Jan. 1980 63 p refs

(NASA-TP-1431; A-7777) Avail: NTIS HC A04/MF A01 CSCL

01A

FLAPPING HINGES, HELICOPTER PERFORMANCE, RIGID

ROTORS, ROTARY WINGS, ROTOR AERODYNAMICS

N80-17081"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

FLIGHT TESTS OF THE TOTAL AUTOMATIC FLIGHT CONTROL

SYSTEM (TAFCOS) CONCEPT ON A DHC-6 TWIN OTTER

AIRCRAFT

W. R. WEHREND, JR. and G. MEYER Feb. 1980 73 p refs

(NASA-TP-1513; A-7901) Avail: NTIS HC A04/MF A01 CSCL

01C

AUTOMATIC FLIGHT CONTROL, FLIGHT CHARACTERISTICS,

SHORT TAKEOFF AIRCRAFT, VERTICAL TAKEOFF AIRCRAFT

N80-19126°# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

APPLICATION OF THE CONCEPT OF DYNAMIC TRIM

CONTROL TO AUTOMATIC LANDING OF CARRIER

AIRCRAFT

G. A. SMITH and G. MEYER Apr. 1980 87 p refs

(NASA-TP-1512; A-7801) Avail: NTIS HC A05/MF A01 CSCL

01C

AIRCRAFT LANDING, AUTOMATIC LANDING CONTROL,

DIGITAL TECHNIQUES, DYNAMIC CONTROL, FEEDFORWARD

CONTROL

08 AIRCRAFT STABILITY AND CONTROL

N80-21336"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

DYNAMICS STABILITY DERIVATIVES OF SPACE SHUTTLE

ORBITER OBTAINED FROM WIND-TUNNEL AND APPROACH

AND LANDING FLIGHT TESTS

D. C. FREEMAN, JR. Washington Apr, 1980 20 p refs

(NASA-TP-1634; L-13427) Avail: NTIS HC A02/MF A01

CSCL 01C

APPROACH AND LANDING TESTS (STS), DYNAMIC

STABILITY, SPACE SHUTTLE ORBITERS, STABILITY

DERIVATIVES, WIND TUNNEL TESTS

N80-22358"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

DESCRIPTION OF AN EXPERIMENTAL (HYDROGEN

PEROXIDE) ROCKET SYSTEM AND ITS USE IN MEASURING

AILERON AND RUDDER EFFECTIVENESS OF A LIGHT

AIRPLANE

T. C. OBRYAN, M W. GOODE, F. D. GREGORY, and M. H.

MAYO May 1980 42 p refs

(NASA-TP-1647; L-12494) Avail: NTIS HC A03/MF A01

CSCL 01C

AILERONS, HYDROGEN PEROXIDE, LIGHT AIRCRAFT,

ROCKET ENGINES, RUDDERS, SYSTEM EFFECTIVENESS

N80-23326"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

NAVIGATION, GUIDANCE, AND CONTROL FOR HELICOPTER

AUTOMATIC LANDINGS

J. R. KELLY and F. R. NIESSEN May 1980 58 p refs

(NASA-TP-1649; L-13454) Avail: NTIS HC A04/MF A01

CSCL 01C

AUTOMATIC CONTROL, AUTOMATIC LANDING CONTROL,

HELICOPTER CONTROL, NAVIGATION AIDS

N80-23327"# National Aeronautics and Space Administration.

Dryden (Hugh L.) Flight Research Center, Edwards, Calif.

PRECISION CONTROLLABILITY OF THE YF-17 AIRPLANE

T. R. SISK and N. W. MATAENY May 1980 34 p refs

(NASA-TP-1677; H-1089) Avail: NTIS HC A03/MF A01 CSCL

01C

CONTROLLABILITY, F-17 AIRCRAFT, MANEUVERABILITY,

TRACKING (POSITION)

N80-24323"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

MAXIMUM LIKELIHOOD METHOD FOR ESTIMATING AIRPLANE

STABILITY AND CONTROL PARAMETERS FROM FLIGHT DATA

IN FREQUENCY DOMAIN

V. KLEIN May 1980 60 p refs Prepared in cooperation with

Joint Institutes for Advancement of Flight Sciences, Hampton, Va.

(NASA-TP-1637; L-13383) Avail: NTIS HC A04/MF A01

CSCL 01C

AIRCRAFT CONTROL, AIRCRAFT STABILITY, MAXIMUM

LIKELIHOOD ESTIMATES

N80-24324"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

FLUTTER ANALYSIS OF AN AIRPLANE WITH MULTIPLE

STRUCTURAL NONLINEARITIES IN THE CONTROL SYSTEM

E. J. BREITBACH Mar. 1980 39 p refs

(NASA-TP-1620; L-13356) Avail: NTIS HC A03/MF A01

CSCL 01C

AIRCRAFT CONFIGURATIONS, AIRCRAFT CONTROL,

FLUTTER, NONLINEARITY, NUMERICAL ANALYSIS

55
08 AIRCRAFTSTABILITYANDCONTROL

N80-25345"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va,

MEASUREMENT OF THE HANDLING CHARACTERISTICS OF

TWO LIGHT AIRPLANES

Jun. 1980 80 p refs

(NASA-TP-1636; L-13054) Avail: NTIS HC A05/MF A01

CSCL 01C

CONTROLLABILITY, FLIGHT TESTS, GENERAL AVIATION

AIRCRAFT

N80-26328"# National Aeronautics and Space Administration.

Dryden (Hugh L) Flight Research Center, Edwards, Calif.

DEVELOPMENT AND FLIGHT TEST RESULTS OF AN

AUTOTHROTTLE CONTROL SYSTEM AT MACH 3 CRUISE

G. B. GILYARD and J. J. BURKEN Jul. 1980 40 p refs

(NASA-TP-1621; H-1090) Avail: NTIS HC A03/MF A01 CSCL

01C

AIRSPEED, AUTOMATIC PILOTS, FLIGHT CONTROL, FLIGHT

TESTS, MACH NUMBER, YF-12 AIRCRAFT

N80-29369"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

SINGLE-STAGE ELECTROHYDRAULIC SERVOSYSTEM FOR

ACTUATING ON AIRFLOW VALVE WITH FREQUENCIES TO

500 HERTZ

J. A. WEBB, JR., O. MEHMED, and C. F. LORENZO Aug. 1980

35 p refs

(NASA-TP-1678; E-252) Avail: NTIS HC A03/MF A01 CSCL

01C

ACTUATORS, AIR FLOW, ELECTRIC CONTROL, HYDRAULIC

EQUIPMENT, SERVOMECHANISMS, VALVES

N81-11044"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

FLIGHT EVALUATION OF STABILIZATION AND COMMAND

AUGMENTATION SYSTEM CONCEPTS AND COCKPIT

DISPLAYS DURING APPROACH AND LANDING OF

POWERED-LIFT STOL AIRCRAFT

J. A. FRANKLIN, R. C. INNIS, and G. H. HARDY Nov. 1980

94 p refs

(NASA-TP-1551; A-7968) Avail: NTIS HC A05/MF A01 CSCL

01C

AERODYNAMIC COEFFICIENTS, AERODYNAMIC STABILITY,

APPROACH AND LANDING TESTS (STS), ATTITUDE CONTROL,

SHORT TAKEOFF AIRCRAFT

N81-12109"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SIMULATION COMPARISON OF A DECOUPLED

LONGITUDINAL CONTROL SYSTEM AND A VELOCITY

VECTOR CONTROL WHEEL STEERING SYSTEM DURING

LANDINGS IN WIND SHEAR

G. KIMBALL, JR. Nov. 1980 76 p refs

(NASA-TP-1734; L-13738) Avail: NTIS HC A05/MF A01

AIRCRAFT CONTROL, AIRCRAFT LANDING, PILOT

PERFORMANCE, WIND SHEAR

N81-13065*# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

PSEUDOSTEADY-STATE ANALYSIS OF NONLINEAR

AIRCRAFT MANEUVERS

J. W. YOUNG, A. A. SCHY, and K. G. JOHNSON Dec. 1980

64 p refs

(NASA-TP-1758; L-13743) Avail: NTIS HC A04/MF A01

CSCL 0tC

AERODYNAMIC CHARACTERISTICS, AIRCRAFT MANEUVERS, FLIGHT CHARACTERISTICS, NONLINEAR EQUATIONS

56

N81-13066"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

COMPARISON OF SPACE SHUTTLE ORBITER LOW-SPEED

STATIC STABILITY AND CONTROL DERIVATIVES OBTAINED

FROM WIND-TUNNEL AND APPROACH AND LANDING FLIGHT

TESTS

D. C. FREEMAN, JR. and B. SPENCER, JR. Dec. 1980 36 p

refs

(NASA-TP-1779; L-13945) Avail: NTIS HC A03/MF A01

CSCL 01C

APPROACH AND LANDING TESTS (STS), FLIGHT TESTS,

SPACE SHUTTLE ORBITERS, STATIC STABILITY, WiND TUNNEL

TESTS

N81-13968"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ECONOMIC EVALUATION OF FLYING-QUALITIES DESIGN

CRITERIA FOR A TRANSPORT CONFIGURED WITH RELAXED

STATIC STABILITY

S.M. SLIWA Dec. 1980 30 p refs

(NASA-TP-1760; L-13944) Avail: NTIS HC A03/MF A01

CSCL 01C

AIRCRAFT DESIGN, CONSTRAINTS, DESIGN ANALYSIS,

ECONOMIC ANALYSIS, OPTIMIZATION, PARAMETERIZATION,

STABILITY AUGMENTATION, TRANSPORT AIRCRAFT

N81-19131"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

FLIGHT-TEST EVALUATION OF STOL CONTROL AND FLIGHT

DIRECTOR CONCEPTS IN A POWERED-LIFT AIRCRAFT

FLYING CURVED DECELERATING APPROACHES

W. S. HINDSON (National Research Council of Canada, Ottawa,

Ontario), G. H. HARDY, and R. C. INNIS Mar. 1981 96 p

refs

(NASA-TP-1641; A-8190) Avail: NTIS HC A05/MF A01 CSCL

01C

AIRCRAFT LANDING, APPROACH CONTROL, FLIGHT TESTS,

INSTRUMENT LANDING SYSTEMS, MANUAL CONTROL, SHORT

TAKEOFF AIRCRAFT

N81-20082"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va,

AN ANALYTICAL STUDY OF THE LONGITUDINAL RESPONSE

OF AIRPLANES TO POSITIVE WIND SHEAR

W. L SHERMAN Mar. 1981 51 p refs

(NASA-Tpo1765; L-13623) Avail: NTIS HC A04/MF A01

CSCL 01C

AIRCRAFT CONTROL, AIRCRAFT STABILITY, FLIGHT

CONTROL, FLIGHT HAZARDS, TRANSPORT AIRCRAFT, WIND

SHEAR

N82-10041"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

DETERMINATION OF AIRPLANE MODEL STRUCTURE FROM

FLIGHT DATA BY USING MODIFIED STEPWlSE REGRESSION

V. KLEIN (Joint Inst. for Advancement of Flight Sciences, Hampton,

Va), J. G. BATTERSON, and P C. MURPHY Oct. 1981 48 p

refs

(NASA-TP-1916; L-14613) Avail: NTIS HC A03/MF A01

CSCL 01C

AERODYNAMIC COEFFICIENTS, AIRCRAFT MODELS,

REGRESSION ANALYSIS, STRUCTURAL DESIGN
N82-15075"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

LONGITUDINAL AND LATERAL STATIC STABILITY AND

CONTROL CHARACTERISTICS OF A 1/6-SCALE MODEL OF

A REMOTELY PILOTED RESEARCH VEHICLE WITH A

SUPERCRITICAL WING

T. A. BYRDSONG and J. B. HALLISSY May 1979 118 p refs

(NASA-TP-1360; L-12059) Avail: NTIS HC A06/MF A01

CSCL 01C

FLIGHT SIMULATION, FLUTTER ANALYSIS, SUPERCRITICAL

WINGS, TRANSONIC WIND TUNNELS

N82-19225"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SIMULATOR STUDY OF VORTEX ENCOUNTERS BY A

TWIN-ENGINE, COMMERCIAL, JET TRANSPORT AIRPLANE

E. C. HASTINGS, JR. and G. L. KEYSER, JR. Feb. 1982 65 p

refs

(NASA-TP-1966; L-14187) Avail: NTIS HC A04/MF A01

CSCL 01C

AIRCRAFT HAZARDS, AIRCRAFT WAKES, COMMERCIAL

AIRCRAFT, FLIGHT SIMULATION, FLOW DISTRIBUTION,

TRANSPORT AIRCRAFT, VORTICES

N82-20187"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

DESIGN CRITERIA FOR FLIGHTPATH AND AIRSPEED

CONTROL FOR THE APPROACH AND LANDING OF STOL

AIRCRAFT

J. A. FRANKLIN, R. C. INNIS, G H. HARDY, and J. D.

STEPHENSON Mar. 1982 98 p refs

(NASA-TP-1911; NAS 1.60:1911; A-8645) Avail: NTIS HC

A05/MFA01 CSCL01C

AERODYNAMICS, AIRSPEED, APPROACH CONTROL,

FLIGHT PATHS, SHORT TAKEOFF AIRCRAFT

N82-20188"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

SELF-TUNING REGULATORS FOR MULTICYCLIC CONTROL OF

HELICOPTER VIBRATION

W. JOHNSON Mar. 1982 50 p refs

(NASA-TP-1996; NAS 1.60:1996; A-8719) Avail: NTIS HC

A03/MF A01 CSCL 01C

CONTROLLERS, HELICOPTERS, SELF ADAPTIVE CONTROL

SYSTEMS, VIBRATION DAMPING

N82-24209"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

APPLICATION OF MODAL CONTROL TO WING-FLUTTER

SUPPRESSION

A, J. OSTROFF and S. PINES (Analytical Mechanics Associates,

Inc., Jericho, N,Y.) May 1982 73 p refs

(NASA-TP-1983; L-14976; NAS 1.60:1983) Avail: NTIS HC

A04/MF A01 CSCL 01C

AIRCRAFT DESIGN, CONTROL THEORY, FLUTTER

ANALYSIS, UNSWEPT WINGS, WING OSCILLATIONS

N83-11139"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

GAIN SELECTION METHOD AND MODEL FOR COUPLED

PROPULSION AND AIRFRAME SYSTEMS

P. C. MURPHY 4 Nov. 1982 33 p refs

(NASA-TP-2067; L-15215; NAS 1.60:2067) Avail: NTIS HC

A03/MF A01 CSCL 01C

AIRFRAMES, AUTOMATIC GAIN CONTROL, EIGENVALUES,

FEEDBACK CONTROL, FLIGHT CONTROL, PROPULSION

SYSTEM PERFORMANCE, TURBOFAN ENGINES

08 AIRCRAFT STABILITY AND CONTROL

N83-16350"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

THE APPLICATION OF PARAMETER ESTIMATION TO FLIGHT

MEASUREMENTS TO OBTAIN LATERAL-DIRECTIONAL

STABILITY DERIVATIVES OF AN AUGMENTED JET-FLAP STOL

AIRPLANE

J. D. STEPHENSON Jan. 1983 62 p refs

(NASA-TP-2033; A-8977; NAS 1.60:2033) Avail: NTIS HC

A04/MFA01 CSCL01C

DIRECTIONAL STABILITY, FLIGHT TESTS, JET FLAPS,

LATERAL STABILITY, PARAMETER IDENTIFICATION, SHORT

TAKEOFF AIRCRAFT

N83-19758"# George Washington Univ., Hampton, Va.

DETERMINATION OF AIRPLANE MODEL STRUCTURE FROM

FLIGHT DATA USING SPLINES AND STEPWISE REGRESSION

V. KLEIN (George Washington Univ., Hampton, Va.) and J. G.

BATTERSON Mar. 1983 52 p refs

(NASA-TP-2126; L-15541; NAS 1.60:2126) Avail: NTIS HC

AO4/MFA01 CSCL 01C

AIRCRAFT MODELS, AIRCRAFT STRUCTURES, STRUCTURAL ANALYSIS

N83-33896"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

RESTRUCTURABLE CONTROLS

R. J. MONTOYA, comp. (Research Triangle Inst., Research Triangle

Park, N.C.), W. E. HOWELL, comp., W. T. BUNDICK, comp., A. J.

OSTROFF, comp., R. M. HUESCHEN, comp., and C. M.

BELCASTRO, comp. Aug. 1983 189 p refs Workshop held

in Hampton, Va., 21-22 Sep. 1982

(NASA-CP-2277; L-15638; NAS 1.55:2277) Avail: NTIS HC

A09/MFA01 CSCL01C

AIRCRAFT INSTRUMENTS, AIRCRAFT SURVIVABILITY,

AUTOMATIC FLIGHT CONTROL, CONFERENCES, RELIABILITY

ENGINEERING, SELF REPAIRING DEVICES

N84-12190"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SIMULATOR STUDY OF FLIGHT CHARACTERISTICS OF A

LARGE TWIN-FUSELAGE CARGO TRANSPORT AIRPLANE

DURING APPROACH AND LANDING

W. D. GRANTHAM, P. L. DEAL, G. L. KEYSER, JR., and P. M.

SMITH (Kentron International, Inc.) Nov. 1983 87 p refs

(NASA-TP-2183; L-15505; NAS 1.60:2183) Avail: NTIS HC

A05/MFA01 CSCL01C

AIRCRAFT LANDING, APPROACH, CARGO AIRCRAFT,

FLIGHT CHARACTERISTICS

N84-13198"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

FLIGHT-TEST OF THE GLIDE-SLOPE TRACK AND

FLARE-CONTROL LAWS FOR AN AUTOMATIC LANDING

SYSTEM FOR A POWERED-LIFT STOL AIRPLANE

D. M. WATSON, G. H. HARDY, and D. N. WARNER, JR. Dec.

1983 89p refs

(NASA-TP-2128; A-9199; NAS 1.60:2128) Avail: NTIS HC

A05/MF A01 CSCL 01C

AIRCRAFT LANDING, AUTOMATIC CONTROL, GLIDE

LANDINGS, POWERED LIFT AIRCRAFT, SHORT TAKEOFF

AIRCRAFT

N84-17184"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

WIND-TUNNEL FREE-FLIGHT INVESTIGATION OF A MODEL

OF A FORWARD-SWEPT-WING FIGHTER CONFIGURATION

D. G. MURRI, L. T. NGUYEN, and S. B. GRAFTON Feb. 1984

71 p refs

(NASA-TP-2230; L-15602; NAS 1.60:2230) Avail: NTIS HC

A04/MF A01 CSCL01C

ANGLE OF ATTACK, FIGHTER AIRCRAFT, STABILITY,

SWEPT WINGS, WIND TUNNEL TESTS

57
08 AIRCRAFT STABILITY AND CONTROL

N84-20567"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

NASA AIRCRAFT CONTROLS RESEARCH, 1983

G. P. BEASLEY, comp. Mar. 1984 592 p refs Workshop

held in Hampton, Va., 25-27 Oct. 1983

(NASA-CP-2296; L-t5730; NAS 1.55:2296) Avail: NTIS HC

A25/MF A01 CSCL 01C

AIRCRAFT DESIGN, AIRCRAFT GUIDANCE, AUGMENTATION, COMPUTERIZED SIMULATION, FEEDBACK CONTROL,

FLIGHT CONTROL

N84-23652"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECT OF AERODYNAMIC AND ANGLE-OF-ATTACK

UNCERTAINTIES ON THE BLENDED ENTRY FLIGHT CONTROL

SYSTEM OF THE SPACE SHUTTLE FROM MACH 10 TO 2.5

H. W. STONE and R. W. POWELL Apr. 1984 291 p

(NASA-TP-2283; L-15719; NAS 1.60:2283) Avail: NTIS HC

A13/MFA01 CSCL01C

ANGLE OF ATTACK, COMPUTERIZED SIMULATION,

DEGREES OF FREEDOM

N84-25717"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AN ALGORITHM FOR MAXIMUM LIKELIHOOD ESTIMATION

USING AN EFFICIENT METHOD FOR APPROXIMATING

SENSITIVITIES

P. C. MURPHY Jun. 1984 38 p refs

(NASA-TP-2311; L-15735; NAS 1.60:2311) Avail: NTIS HC

A03/MF A01 CSCL 01C

ALGORITHMS, APPROXIMATION, MAXIMUM LIKELIHOOD

ESTIMATES, OPTIMIZATION, PARAMETER IDENTIFICATION,

SENSITIVITY

N84-28801"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SPACE SHUTTLE SEPARATE-SURFACE CONTROL-SYSTEM

STUDY

L. W. BROWN and R. C. MONTGOMERY Jul. 1984 59 p

refs

(NASA-TP-2340; L-15650; NAS 1.60:2340) Avail: NTIS HC

A04/MF A01 CSCL 01C

AERODYNAMIC STABILITY, CONTROL DATA (COMPUTERS),

CONTROL THEORY, FLIGHT CHARACTERISTICS, SPACECRAFT

CONTROL, YAW

N84-32394"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

MINIMUM-FUEL, 3-DIMENSIONAL FLIGHTPATH GUIDANCE OF

TRANSFER JETS

F. NEUMAN and E. KREINDLER (Technion Israel Inst. of Teoh.,

Haifa) Sap. 1984 90 p refs

(NASA-TP-2326; A-9533; NAS 1.60:2326) Avail: NTIS HC

A05/MF A01 CSCL 01C

COMMERCIAL AIRCRAFT, FLIGHT PATHS, JET AIRCRAFT,

TRANSPORT AIRCRAFT

N85-11002"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SIMULATOR STUDY OF FLIGHT CHARACTERISTICS OF

SEVERAL LARGE, DISSIMILAR, CARGO TRANSPORT

AIRPLANES DURING APPROACH AND LANDING

W. D. GRANTHAM, P. M. SMITH (Kentron International, Inc.), P.

L. DEAL (Air Force Systems Command), and W. R. NEELY, JR.

Nov. 1984 88p refs

(NASA-TP-2357; L-15805; NAS 1.60:2357) Avail: NTIS HC

A05/MF A01 CSCL 01C

AERODYNAMIC CONFIGURATIONS, DATA CORRELATION,

FLIGHT CHARACTERISTICS, FLIGHT SIMULATORS,

TRANSPORT AIRCRAFT

58

N85-23801"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

TOTAL ENERGY-RATE FEEDBACK FOR AUTOMATIC

GMDE-SLOPE TRACKING DURING WIND-SHEAR

PENETRATION

C. M. BELCASTRO and A. J. OSTROFF May 1984 73 p refs

(NASA-TP-2412; L-15845; NAS 1.60:2412) Avail: NTIS HC

A04/MF A01 CSCL 01C

AIRCRAFT LANDING, FEEDBACK, GLIDE PATHS,

LONGITUDINAL CONTROL, OPTIMAL CONTROL, WIND SHEAR

N85-28949"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

PILOTED SIMULATION OF AN ALGORITHM FOR ONBOARD

CONTROL OF TIME-OPTIMAL INTERCEPT

D. B. PRICE, A. J. CALISE (Drexel Univ.), and D. D. MOERDER

(Information and Control Systems, Inc., Hampton, Va.) Jun.

1985 48 p refs

(NASA-TP-2445; L-15896; NAS 1.60:2445) Avail: NTIS HC

A03/MF A01 CSCL 01C

ALGORITHMS, COMPUTERIZED SIMULATION, FLIGHT

CONTROL, ONBOARD DATA PROCESSING, TIME, TRAJECTORY

OPTIMIZATION

N85-34144"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

GROUND-BASED AND IN-FLIGHT SIMULATOR STUDIES OF

FLIGHT CHARACTERISTICS OF A TWIN-FUSELAGE

PASSENGER TRANSPORT AIRPLANE DURING APPROACH

AND LANDING

W. D. GRANTHAM, P. M. SMITH (PRC Kentron, Inc.), W. R. NEELY,

JR. (AFSC Liaison Office, Hampton, Va.), P. L. DEAL, and K. R.

YENNI Sap. 1985 55 p refs

(NASA-TP-2451; L-15941; NAS 1.60:2451) Avail: NTIS HC

A04/MF A01 CSCL 01C

APPROACH, CONTROLLABILITY, DEGREES OF FREEDOM,

FLIGHT CHARACTERISTICS, FUSELAGES, LANDING,

TRANSPORT AIRCRAFT

N86-22579"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

A METHODOLOGY FOR AIRPLANE PARAMETER ESTIMATION

AND CONFIDENCE INTERVAL DETERMINATION IN

NONLINEAR ESTIMATION PROBLEMS Ph.D. Thesis - George

Washington Univ., Apr. 1985

P. C. MURPHY Apr. 1986 56 p refs Revised

(NASA-RP-1153; L-16009; NAS 1.61:1153) Avail: NTIS HC

A04/MF A01 CSCL 01C

An algorithm for maximum likelihood (ML) estimation is

developed with an efficient method for approximating the

sensitivities. The ML algorithm relies on a new optimization method

referred to as a modified Newton-Raphson with estimated

sensitivities (MNRES). MNRES determines sensitivities by using

slope information from local surface approximations of each output

variable in parameter space. With the fitted surface, sensitivity

information can be updated at each iteration with less computational

effort than that required by either a finite-difference method or

integration of the analytically determined sensitivity equations.

MNRES eliminates the need to derive sensitivity equations for

each new model, and thus provides flexibility to use model

equations in any convenient format. A random search technique

for determining the confidence limits of ML parameter estimates

is applied to nonlinear estimation problems for airplanes. The

confidence intervals obtained by the search are compared with

Cramer-Rao (CR) bounds at the same confidence level. The degree

of nonlinearity in the estimation problem is an important factor in

the relationship between CR bounds and the error bounds

determined by the search technique. Beale's measure of

nonlinearity is developed in this study for airplane identification

problems; it is used to empirically correct confidence levels and

to predict the degree of agreement between CR bounds and search

estimates. Author
N86-22580"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

LOW-SPEED STABILITY AND CONTROL CHARACTERISTICS

OF A TRANSPORT MOOEL WITH AFT-FUSELAGE-MOUNTED

ADVANCED TURBOPROPS

Z. T. APPLIN and P. L. COE, JR. Apr. 1986 67 p refs

(NASA-TP-2535; L-16004; NAS 1.60:2535) Avail: NTIS HC

A04/MF A01 CSCL 01C

AERODYNAMIC CHARACTERISTICS, AERODYNAMIC

STABILITY, CONTROL STABILITY, TRANSPORT AIRCRAFT

09

RESEARCH AND SUPPORT FACILITIES (AIR)

Includes airports, hangars and runways; aircraft repair and overhaul

facilities; wind tunnels; shock tubes; and aircraft engine test

stands.

N77-27139"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

HIGH REYNOLDS NUMBER RESEARCH

D. D. BAALS, ed. Washington 1977 185 p Workshop Proc.

held at Hampton, Va., 27-28 Oct. 1976; sponsored in part by

George Washington Univ,

(NASA-CP-2009) Avail: NTIS HC A09/MF A01 CSCL 02A

AERODYNAMICS, AEROELASTICITY, CONFERENCES,

CRYOGENIC WIND TUNNELS, RESEARCH FACILITIES,

REYNOLDS NUMBER, TRANSONIC WIND TUNNELS

N79-16877"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EXPERIMENTAL EVALUATION OF A PILOT MULTINOZZLEDUCT APPARATUS

R. L. PUSTER Feb. 1979 46 p refs

(NASA-TP-1319; L-12282) Avail: NTIS HC A03/MF A01

CSCL 14B

DUCTED BODIES, GASDYNAMIC LASERS, NOZZLE

GEOMETRY

N79-29199"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

A UNIQUE FACILITY FOR V/STOL AIRCRAFT HOVER

TESTING

R. G. CULPEPPER, R. D. MURPHY (Naval Air Systems Command,

Washington, D. C.), E. A. GILLESPIE (Rockwell Intern. Corp.,

Columbus, Ohio), and A. G. LANE Aug. 1979 56 p refs

(NASA-TP-1473; L-12914) Avail: NTIS HC A04/MF A01

CSCL 14B

ANIONS, FLIGHT TESTS, HOVERING, RESEARCH

FACILITIES, TETHERING, V/STOL AIRCRAFT

N80-19131"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

A THEORETICAL ANALYSIS OF SIMULATED TRANSONIC

BOUNDARY LAYERS IN CRYOGENIC-NITROGEN WIND

TUNNELS

J. B. ADCOCK and C. B. JOHNSON Mar. 1980 40 p refs

(NASA*TP-1631; L-13364) Avail: NTIS HC A03/MF A01

CSCL 14B

CRYOGENIC WIND TUNNELS, LAMINAR BOUNDARY LAYER,

NITROGEN, TRANSONIC WIND TUNNELS, TURBULENT

BOUNDARY LAYER

09 RESEARCH AND SUPPORT FACILITIES (AIR)

N80-31413"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

DEVELOPMENT AND VALIDATION OF A HYBRID-COMPUTER

SIMULATOR FOR A TRANSONIC CRYOGENIC WIND TUNNEL

J. J. THIBODEAUX and S. BALAKRISHNA (Old Dominion Univ.)

Sep. 1980 84 p refs

(NASA-TP-1695; L-13691) Avail: NTIS HC A05/MF A01

CSCL t4B

COMPUTERIZED SIMULATION, CRYOGENIC WIND

TUNNELS, TEST FACILITIES

N81-32153"# National Aeronautics and Space Administration,

Washington, D.C.

WIND TUNNELS OF NASA

D. D. BAALS and W. R CORLISS 1981 162 p Original

document contains color illustrations

(NASA-SP-440) Avail: NTIS HC A08/MF A01 CSCL 14B

The contribution of wind tunnels to aerodynamic studies is

described. The development of the wind tunnel and the problems

of calibration, scaling, and instrumentation are discussed. The

NASA wind tunnels form the basis for the book, but Air Force,

university, and industrial facilities are also considered. T.M

N82-11090"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AN ALGORITHM FOR MINIMUM-COST SET-POINT ORDERING

IN A CRYOGENIC WIND TUNNEL

J. S. TRIPP Nov. 1981 32 p refs

(NASA-TP-1923; L-14695) Avail: NTIS HC A03/MF A01

CSCL 14B

ALGORITHMS, COST REDUCTION, CRYOGENIC COOLING,

CRYOGENIC WIND TUNNELS, MATHEMATICAL MODELS,

OPTIMAL CONTROL

N83-17560"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

THE AERODYNAMIC PERFORMANCE OF SEVERAL FLOW

CONTROL DEVICES FOR INTERNAL FLOW SYSTEMS

W. T. ECKERT (Army Aviation Research and Technology Labs.),

B. M. WETTLAUFER (Sverdrup Technology), and K. W. MORT

Dec. 1982 49 p refs Sponsored in part by Army Aviation

Research and Development Command

(NASA-TP-1972; A-8816; NAS 1.60:1972;

AVRADCOM-TR-81-A-2) Avail: NTIS HC A03/MF A01 CSCL

14B

CASCADE FLOW, DUCTS, FLOW DISTRIBUTION, PRESSURE

DISTRIBUTION, THROTTLING, WIND TUNNELS

N83-18748"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

CRYOGENIC WIND TUNNEL MODELS. DESIGN AND

FABRICATION

C. P. YOUNG, JR., comp. and B. B. GLOSS, comp. Mar. 1983

254 p refs Proc. of workshop held in Hampton, Va., 5-9 May

1982

(NASA-CP-2262; L-15567; NAS 1.55:2262) Avail: NTIS HC

A12/MFA01 CSCL 14B

CONFERENCES, CRYOGENIC WIND TUNNELS, TRANSONIC

WIND TUNNELS, WIND TUNNEL MODELS

N83-18770"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

A METHOD FOR MODIFYING TWO-DIMENSIONAL ADAPTIVE

WIND-TUNNEL WALL_ INCLUDING ANALYTICAL AND

EXPERIMENTAL VERIFICATION

J. L. EVERHART Feb. 1983 48 p refs

(NASA-TP-2081; L-15491; NAS 1.60:2081) Avail: NTIS HC

A03/MF A01 CSCL 14B

CAUCHY INTEGRAL FORMULA, CIRCULAR CYLINDERS,

CONVERGENCE, WIND TUNNEL TESTS, WIND TUNNEL

WALLS

59
09 RESEARCH AND SUPPORT FACILITIES (AIR)

N83-36039"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EXPANDED OPERATIONAL CAPABILITIES OF THE LANGLEY

MACH 7 SCRAMJET TEST FACILITY

S. R. THOMAS and R. W. GUY Oct. 1983 74 p refs

(NASA-TP-2186; L-15565; NAS 1.60:2186) Avail: NTIS HC

A04/MF A01 CSCL 14B

AIR FLOW, AIRFRAMES, NITROGEN OXIDES, SUPERSONIC

COMBUSTION RAMJET ENGINES, TEMPERATURE PROFILES,

TEST FACILITIES

N65-18991"# National Aeronautics and Space Administration,

Washington, D.C.

AERONAUTICAL FACILITIES CATALOGUE. VOLUME I: WIND

TUNNELS

F. E. PENARANDA, comp. and M. S. FREDA, comp. Jan. 1985

421 p 2 Vol.

(NASA-RP-1132; NAS 1.61:1132) Avail: NTIS HC A18/MF A01

CSCL 14B

Domestic and foreign wind tunnel facilities are enumerated and

their technical parameters are described. Data pertinent to

managers and engineers are presented. Facilities judged

comparable in testing capability are noted and grouped together.

Several comprehensive cross-indexes and charts are included.

R.S.F.

N86-18326"# National Aeronautics and Space Administration,

Washington, D.C.

AERONAUTICAL FACILITIES CATALOGUE. VOLUME 2:

AIRBREATHING PROPULSION AND FLIGHT SIMULATORS

F. E. PENARANDA and M. S. FREDA Dec. 1985 242 p 2

Vol.

(NASA-RP-1133; NAS 1.61:1133) Avail: NTIS HCA11/MFA01

CSCL 14B

Volume two of the facilities catalogue deals with Airbreathing

Propulsion and Flight Simulation Facilities. Data pertinent to

managers and engineers are presented. Each facility is described

on a data sheet that shows the facility's technical parameters on

a chart and more detailed information in narratives. Facilities judged

comparable in testing capability are noted and grouped together.

Several comprehensive cross-indexes and charts are included.

Author

N86-24709"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

DYNAMIC MEASUREMENT OF TOTAL TEMPERATURE,

PRESSURE AND VELOCITY IN THE LANGLEY 0.3-METER

TRANSONIC CRYOGENIC TUNNEL

C. B. JOHNSON and P. C. STAINBACK May 1986 45 p refs

(NASA-TP-2584; L-16099; NAS 1.60:2584) Avail: NTIS HC

AO3/MF A01 CSCL 14B

CRYOGENIC WIND TUNNELS, LIQUID NITROGEN,

PRESSURE MEASUREMENT, TEMPERATURE MEASUREMENT,

VELOCITY MEASUREMENT

N86-28101"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EXPERIMENTAL EVALUATION OF TWO TURNING VANE

OESIGNS FOR HIGH-SPEED CORNER OF 0.1-SCALE MODEL

OF NASA LEWIS RESEARCH CENTER'S PROPOSED ALTITUDE

WIND TUNNEL

R. D. MOORE. D R BOLDMAN, and R. J. SHYNE Apr. 1986

130 p

(NASA-TP-2570; E-2831; NAS 1.60:2570) Avail: NTIS HC

A07/MF A01 CSCL 14B

AIRFOILS, ALTITUDE TESTS, CASCADE FLOW,

EVALUATION, EXPERIMENTATION, VANES, WIND TUNNEL

TESTS

6O

12

ASTRONAUTICS (GENERAL)

N77-21106" National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

SPACE SETTLEMENTS: A DESIGN STUDY

R. D. JOHNSON, ed. and C. HOLBROW, ed. (Colgate Univ.)

Washington 1977 191 p refs Sponsored in part by Am.

Soc. for Eng. Original contains color illustrations

(NASA-SP-413; LC-76-600068) Avail: SOD HC $5.00 CSCL

22A

Nineteen professors of engineering, physical science, social

science, and architecture, three volunteers, six students, a technical

director, and two co-directors worked for ten weeks to construct

a convincing picture of how people might permanently sustain life

in space on a large scale, and to design a system for the

colonization of space. Because the idea of colonizing space has

awakened strong public interest, the document presented is written

to be understood by the educated public and specialists in other

fields. It also includes considerable background material. A table

of units and conversion factors is included to aid the reader in

interpreting the units of the metric system used in the report.

Author

N77-27155"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

SKYLAB, OUR FIRST SPACE STATION

L. F. BELEW, ed. Washington 1977 176 p

(NASA-SP-400) Avail: NTIS MF A01; SOD HC $7.00 CSCL

22A

The vast accomplishments of Skylab - in solar and stellar

astronomy, in the detailed study of our planet from the incomparable

vantage of orbit, in using the laboratory tool of weightlessness,

and in proving that man can work productively in space for extended

periods - are discussed. The data on solar physics contain valuable

information on the Sun's corona and the solar winds and open up

new concepts to be explored in future solar astronomy programs.

In the area of technology, the data from Skylab's space processing

experiments open a completely new dimension in the field of

materials processing. Author

N78-17088"# National Aeronautics and Space Administration,

Lyndon B. Johnson Space Center, Houston, Tex.

APOLLO-SOYUZ TEST PROJECT. VOLUME 1: ASTRONOMY,

EARTH ATMOSPHERE AND GRAVITY FIELD, LIFE SCIENCES,

AND MATERIALS PROCESSING

1977 570 p refs 2 Vol.

(NASA-SP-412) Avail: NTIS HC A24/MF A01 CSCL 22A

The joint U.S.-USSR experiments and the U.S. conducted

unilateral experiments performed during the Apollo Soyuz Test

Project are described. Scientific concepts and experiment design

and operation are discussed along with scientific results of postflight

analysis. For individual titles, see N78-17089 through N78-17119.

N78-18088"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala

AIAA/MSFC SYMPOSIUM ON SPACE INDUSTRIALIZATION:

PROCEEDINGS

1976 627 p refs Proc. held at Huntsville, Ala., 26-27 May

1976

(NASA-CP-2026) Avail: NTIS HC A99/MF A01 CSCL 22A

CONFERENCES, SATELLITE SOLAR POWER STATIONS,

SPACE MANUFACTURING, SPACE PROCESSING, SPACE

STATIONS, SPACE TRANSPORTATION
12 ASTRONAUTICS (GENERAL)

N78-20151"# National Aeronautics and Space Administration,

Washington, D.C.

ON THE SHOULDERS OF TITANS: A HISTORY OF PROJECT

GEMINI

B. C. HACKER 1977 634 p refs Original contains color

illustrations

(NASA-SP-4203) Avail: NTIS MF A01; SOD HC $8.25 CSCL

22A

Gemini was the intermediate manned space flight program

between America's first steps into space with Mercury and the

manned lunar expeditions of Apollo. Because of its position

between these two other efforts, Gemini is probably less

remembered. Still, it more than had its place in man's progress

into this new frontier. Gemini accomplishments were manyfold.

They included many firsts: first astronaut-controlled maneuvering

in space; first rendezvous in space of one spacecraft with another;

first docking of one spacecraft with a propulsive stage and use of

that stage to transfer man to high altitude; first traverse of man

into the earth's radiation belts; first extended manned flights of a

week or more in duration; first extended stays of man outside his

spacecraft; first controlled reentry and precision landing; and many

more. These achievements were significant in ways one cannot

truly evaluate even today, but two things stand out: (1) it was the

time when America caught up and surpassed the Soviet Union in

manned space flight, and (2) these demonstrations of capability

were an absolute prerequisite to the phenomenal Apollo

accomplishments then yet to come. Author

N78-27146"# Jet Propulsion Lab., California Inst. of Tech.,

Pasadena.

THE VOYAGE OF MARINER 10: MISSIONS TO VENUS AND

MERCURY

J. A. DUNNE and E. BURGESS 1978 233 p refs Original

contains color illustrations

(NASA-SP-424; LC-77-18956) Avail: NTIS MF A01; SOD HC

$12.25 CSCL 22A

The historical details of the Mariner 10 mission are recorded.

Provided is a selection of some of the images obtained by the

spacecraft at both Venus and Mercury. The solar sailing method

greatly reduced the spacecraft's gas usage thus permitting two

returns to Mercury. These revisits provided additional pictures of

the planet's south pole and confirmed the existence of Mercury's

magnetic field. G.G.

N78-76855" National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

FLIGHT MECHANICS/ESTIMATION THEORY SYMPOSIUM

A. FUCHS 1975 265 p refs Syrup. held at Greenbelt, Md.,

29-30 1975

(NASA-CP-2002) Avail: Goddard Space Flight Center, Code

592

CONFERENCES, FLIGHT MECHANICS, ORBIT CALCULATION, ORBITAL POSITION ESTIMATION

N78-21174"# National Aeronautics and Space Administration,

Washington, D.C.

APOLLO OVER THE MOON: A VIEW FROM ORBIT

H. MASURSKY, ed., G. W. COLTON, ed., F. EL-BAZ, ed., F. J.

DOYLE, R. E. EGGLETON, M. J. GROLIER, J. W. HEAD, II1, C.

A. HODGES, K. A. HOWARD, L. J. KOSOFSKY et al. 1978

263 p refs Original contains color illustrations

(NASA-SP-362; LC-77-25922) Avail: NTIS MF A01; SOD HC

$9.25 CSCL 03B

The Apollo metric camera system was flown to acquire

photographic data with accuracy to aid the effort of moon mapping.

The panoramic camera was selected to provide high resolution

photography of lunar surface features for detailed analysis and

photointerpretation. A portion of these photographs is presented.

Various views and subjects include the following: (1) Regional

views;(2) The Terrae; (3) The Maria; (4) Craters; (5) Sinuous and

Straight Rimae; and (6) Unusual features. Author

N79-10074"# National Aeronautics and Space Administration,

Washington, D.C.

THE PARTNERSHIP: A HISTORY OF THE APOLLO-SOYUZ

TEST PROJECT

E. C. EZELL and L. N EZELL 1976 570 p refs Original

contains color illustrations

(NASA-SP-4209) Avail: NTIS SOD HC CSCL 22A

Correspondance, interviews, official documents, and other

published materials were used to trace the evolution of the Apollo

Soyuz Test Project from the initial proposal for international

cooperation in space use and exploration until the successful

completion of the joint Soviet-American mission. Conceptual

drawings of proposed docking modules and mechanisms are

presented and dicussed. Black and white photographs taken during

mission planning and in-flight activities are included with color

photographs of the earth taken during the mission. Joint meetings

are summarized and the scientific experiments and launch vehicles

are discussed in the appendices. A.H.

N78-25115"# National Aeronautics and Space Administration,

Washington, D.C.

SKYLAB: A CHRONOLOGY

R. W. NEWKIRK, I. D. ERTEL, and C. G. BROOKS 1977 476

p refs

(NASA-SP-4011; LC-77-608101) Avail: NTIS MF A01; SOD HC

$7.00 CSCL 22A

The Skylab Program was specifically designed to conduct a

series of experiments from beyond the earth's atmosphere. Since

the number and types of experiments conducted during the

operational phase of Skylab were constantly changing, rather than

encumber the body of the chronology with these changes, a lengthy

appendix on experiments is included in this document. This

appendix identifies the principle investigators and coinvestigators;

gives the types, numbers, and descriptions of the experiments;

explains the purpose of the various experiments; and, where

possible, gives the results or findings of the experiments. The

body of the Skylab chronology is divided into three parts; early

space station activities, Apollo applications, and Skylab

development and operations. Author

N79-13069"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

PROCEEDINGS OF THE WORKSHOP ON AN

ELECTROMAGNETIC POSITIONING SYSTEM IN SPACE

W. A. ORAN, ed. Oct. 1978 25 p refs Workshop held at

Washington, D. C., 1-2 May 1978

(NASA-CP-2069) Avail: NTIS HC A02/MF A01 CSCL 22A

AEROSPACE TECHNOLOGY TRANSFER, CONFERENCES,

ELECTROMAGNETIC PULSES, POSITION (LOCATION)

N79-19013"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

NINTH CONFERENCE ON SPACE SIMULATION

1977 470 p refs Conf. held at Los Angeles, 26-28 Apr. 1977;

sponsored in part by Inst. of Environ. Sci., AIAA, and Am. Soc.

for Testing and Mater.

(NASA-CP-2007) Avail: NTIS HC A20/MF A01 CSCL 22A

CONFERENCES, SPACE ENVIRONMENT SIMULATION,

SPACE SIMULATORS

61
12 ASTRONAUTICS(GENERAL)

N79-20162"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

GOVERNMENT/INDUSTRY WORKSHOP ON PAYLOAD LOADS

TECHNOLOGY

1978 874 p refs Workshop held at Huntsville, Ala., 14-16

Nov. 1978

(NASA-CP-2075) Avail: NTIS HC A99/MF A01 CSCL 22A

CONFERENCES, PAYLOADS, SPACE SHUTTLES,

TECHNOLOGY ASSESSMENT

N79-25048"# Air Force Materials Lab., Wright-Patterson AFB,

Ohio.

PROCEEDINGS OF THE USAF/NASA INTERNATIONAL

SPACECRAFT CONTAMINATION CONFERENCE Scientific

Interim Report, 7-9 Mar. 1978

J. M. JEMIOLA, ed. 1978 1219 p refs Conf. held at AF

Acad., Colo., 7-9 Mar. 1978; cosponsored by NASA and AF

(AF PROJ. 7340)

(NASA-CP-2039; AFML-TR-78-190) Avail: NTIS HC A99/MF

A0t CSCL 22A

CONFERENCES, SPACECRAFT CONTAMINATION, SPACECRAFT ENVIRONMENTS

N79-26076*# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

PROCEEDINGS OF WORKSHOPS TO DEFINE ENGINEERING

REQUIREMENTS FOR A SPACE VACUUM RESEARCH

FACILITY

W. A. ORAN, ed., S. T. WU, ed. (Alabama Univ. in Huntsville),

and R. W. HOFFMAN, ed. (Case Western Reserve Univ., Ohio)

Jun. 1979 152 p refs Workshops held at Huntsville, Ala.,

12-13 Jun. 1978 and 3-4 Apr. 1978

(NASA-CP-2091) Avail: NTIS HC A08/MF A01 CSCL 22A

CONFERENCES, RESEARCH FACILITIES, SPACECRAFT

ENVIRONMENTS, SPACECRAFT SHIELDING, SYSTEMS

ENGINEERING, ULTRAHIGH VACUUM

N79-28203"# National Aeronautics and Space Administration,

Washington, D.C.

CHARIOTS FOR APOLLO: A HISTORY OF MANNED LUNAR

SPACECRAFT

C. G. BROOKS, J. M. GRIMWOOD, and L. S. SWENSON, JR.

1979 553p refs

(NASA-SP-4205) Avail: NTIS MF A01; SOD HC $9.00 CSCL

22B

Beginning with the challenges presented by Sputnik 1 in 1957,

and the formation of NASA, the apollo lunar exploration program

is reviewed through Apollo Flight 11. The focal points are the

spacecraft including the command and service modules, and the

lunar module. F.O.S.

N79-32225"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

SPACE RESOURCES AND SPACE SETTLEMENTS

J. BILLINGHAM, ed., W. P. GILBREATH, ed., B. OLEARY, ed.

(Princeton Univ.), and B. GOSSET, ed. Washington 1979

292 p Derived from 1977 Ames Summer Study, Moffett Field,

Calif. Original contains color illustrations

(NASA-SP-428) Avail: NTIS MF A01; SOD HC CSCL 22B

The technical papers from the five tasks groups that took part

in the 1977 Ames Summer Study on Space Settlements and

Industrialization Using Nonterrestrial Materials are presented. The

papers are presented under the following general topics: (1)

research needs for regenerative life-support systems; (2) habitat

design; (3) dynamics and design of electromagnetic mass drivers;

(4) asteroids as resources for space manufacturing; and (5)

processing of nonterrestrial materials. For individual titles, see

N79o32226 through N79-32241.

62

N81-16075"# National Aeronautics and Space Administration,

Washington, D.C.

MATERIALS PROCESSING IN SPACE: EARLY EXPERIMENTS

R. J. NAUMANN and H. W. HERRING 1980 123 p Original

contains color illustrations

(NASA-SP-443; LC-80-607081) Avail: NTIS MF A01; SOD HC

$10.00 CSCL 22A

The characteristics of the space environment were reviewed.

Potential applications of space processing are discussed and

include metallurgical processing, and processing of semiconductor

materials. The behavior of fluid in low gravity is described. The

evolution of apparatus for materials processing in space was

reviewed, T.M

N81-19144"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

FLOAT ZONE WORKSHOP

R. J. NAUMANN Dec. 1980 175 p refs Workshop held in

Huntsville, Ala., 12 Dec. 1980

(NASA-CP-2179) Avail: NTIS HC A08/MF A01 CSCL 22A

CRYSTAL GROWTH, INTERFACIAL TENSION, LOW GRAVITY

MANUFACTURING, SPACE PROCESSING

N81-26160"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EVA ASSEMBLY OF LARGE SPACE STRUCTURE ELEMENT

L. J. BEMENT, H. G. BUSH, W. L. HEARD, JR., and J. W. STOKES,

JR. (NASA, Marshall Space Flight Center) Jun. 1981 38 p

refs

(NASA-TP-1872; L-14353) Avail: NTIS HC A03/MF A01

CSCL 22A

EXTRAVEHICULAR ACTIVITY, LARGE SPACE STRUCTURES,

ORBITAL ASSEMBLY, SPACE ENVIRONMENT SIMULATION,

SPACE ERECTABLE STRUCTURES

N82-10064"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

SIXTH ANNUAL FLIGHT MECHANICS/ESTIMATION THEORY

SYMPOSIUM

E. LEFFERTS, ed. Oct. 1981 287 p refs Conf. held at

Greenbelt, Md., 27-28 Oct. 1981

(NASA-CP-2205) Avail: NTIS HC A13/MF A01 CSCL 22A

CONFERENCES, FLIGHT MECHANICS, ORBITAL

MECHANICS, ORBITAL POSITION ESTIMATION, SPACECRAFT

ORBITS

N82-26330"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

FLOAT ZONE WORKSHOP

E. L. KERN, ed. and E. K. COTHRAN, ed. Sep. 1981 205 p

refs Workshop held at Huntsville, Ala., 22-23 Sep. 1981

(NASA-CP-2226; NAS 1.55:2226) Avail: NTIS HC A10/MF A01

CSCL 22A

CONFERENCES, CRYSTAL GROWTH, MELTS (CRYSTAL

GROWTH), SPACE PROCESSING, ZONE MELTING

N82-29335"# National Aeronautics and Space Administration,

Washington, D.C.

APPROXIMATE ANALYSIS OF THERMAL CONVECTION IN A

CRYSTAL-GROWTH CELL FOR SPACELAB 3

R. F. DRESSLER Jun. 1982 11 p refs

(NASA-TP-2016; EN-t; NAS 1.60:2016) Avail: NTIS HC

A02/MF A01 CSCL 20B

CRYSTAL GROWTH, FREE CONVECTION, SPACE

PROCESSING, SPACELAB PAYLOADS
N84-25737"#National Aeronautics and Space Administration,

Washington, D.C.

LIVING AND WORKING IN SPACE. A HISTORY OF SKYLAB

W. D. COMPTON and C. D. BENSON 1983 466 p refs

Original document contains color illustrations

(NASA-SP-4208; NAS 1.21:4208; LC-81-22424) Avail: NTIS MF

A01; SOD HC $20.00 as 033-000-00847-3

The history of Skylab is examined with emphasis on program

development from previous Apollo missions, modifications to

spacecraft, onboard experiments, and flight crew training. A listing

of the missions and an evaluation of results are included with a

brief description of the workshop's reentry. MA.C.

N84-27758"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

GET AWAY SPECIAL EXPERIMENTER'S SYMPOSIUM

C. R. PROUTY, ed. Jul. 1984 162 p refs

(NASA-CP-2324; NAS 1.55:2324) Avail: NTIS HC A08/MF A01

CSCL 22A

CONFERENCES, GET AWAY SPECIALS (STS), PAYLOADS,

SPACE SHUTTLES, SPACEBORNE EXPERIMENTS,

STRUCTURAL DESIGN

N85-11011"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

SECOND SYMPOSIUM ON SPACE INDUSTRIALIZATION

C. M. JERNIGAN, ed. Oct. 1984 427 p refs Symp. held in

Huntsville, Ala., 13-15 Feb. 1984 Sponsored in cooperation with

AIAA and Alabama Univ.

(NASA-CP-2313; M-464; NAS 1.55:2313) Avail: NTIS HC

A19/MF A01 CSCL 22A

BIOPROCESSING, COMMUNICATION, CONFERENCES,

ECONOMIC FACTORS, GOVERNMENT/INDUSTRY RELATIONS,

LAUNCH VEHICLES, LAW (JURISPRUDENCE), POLICIES,

REDUCED GRAVITY, REMOTE SENSING, SPACE

COMMERCIALIZATION, SPACE INDUSTRIALIZATION, SPACE

PROCESSING, SPACE STATIONS

N85-16889"# National Aeronautics and Space Administration.

Lyndon B. Johnson Space Center, Houston, Tex.

SPACE SHUTTLE TECHNICAL CONFERENCE, PART 1

N. CHAFFEE, comp. Washington Jan. 1985 598 p refs

Conf. held in Houston, Tex., 28-30 Jun. 1983 2 Vol.

(NASA-CP-2342-PT-1; S-539-PT-1; NAS 1.55:2342-PT-1) Avail:

NTIS HC A25/MF A01 CSCL 22A

SPACE SHUTTLE ORBITERS, SPACE SHUTTLES,

SPACECRAFT DESIGN

N85-16937"# National Aeronautics and Space Administration.

Lyndon B. Johnson Space Center, Houston, Tex.

SPACE SHUTTLE TECHNICAL CONFERENCE, PART 2

N. CHAFFEE, comp. Jan. 1985 530 p refs Conf. held in

Houston, Tex., 28-30 Jun+ 1983 2 Vol.

(NASA-CP-2342-PT-2; S-539; NAS 1.55:2342-PT-2) Avail: NTIS

HC A23/MF A01 CSCL 22A

AVIONICS, COMMUNICATION, CONFERENCES, FLIGHT

CONTROL, NAVIGATION, PROPULSION SYSTEM

PERFORMANCE, SPACE SHUTTLES, SPACECRAFT

STRUCTURES, THERMAL PROTECTION

N85-21188"# National Aeronautics and Space Administration.

Lyndon B. Johnson Space Center, Houston, Tex.

ORBITAL DEBRIS

D. J. KESSLER, comp. and S. Y+ SU, comp. (LockheedoEMSCO,

Houston, Tex.) Mar. 1985 453 p refs Proc. of a Workshop

held in Houston, Tex., 27-29 Jul. 1982

(NASA-CP-2360; S-532; NAS 1.55:2360) Avail: NTIS HC

A20/MF A01 CSCL 22A

COLLISIONS, CONFERENCES, HYPERVELOCITY IMPACT,

IMPACT DAMAGE, ORBIT DECAY, ORBIT TRANSFER VEHICLES,

ORBITAL MECHANICS, ORBITAL SERVICING, SATELLITE

TRACKING, SPACE DEBRIS

12 ASTRONAUTICS (GENERAL)

N85-33126"# Texas A&M Univ., College Station.

FAR TRAVELERS: THE EXPLORING MACHINES

O. W. NICKS Jun. 1985 269 p Original contains color

illustrations

(NASW-3557)

(NASA-SP-480; NAS 1.21:480; LC-85-1794) Avail: NTIS MF

A01; SOD HC $17.00 as 033-000-00957-7 CSCL 22A

During the first two decades of space activities, unmanned

spacecraft played a vital role in the initial exploration of the Moon

and the planets. The spacecraft employed emerging technologies

to provide extensions of man in the close-up viewing and

measurement of the environment and features of Earth's

interplanetary neighbors. An account of early experiences in the

development and use of interplanetary vehicles is presented.

Specific lunar and planetary missions (e.g., Ranger, Mariner, and

Viking) are discussed. In addition, incidents highlighting the

evolution of significant technologies are presented, based on

personal views of people intimately involved in the efforts.

Author

N86-21559"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

GRAPHICAL TECHNIQUES TO ASSIST IN POINTING AND

CONTROL STUDIES OF ORBITING SPACECRAFT

L.W. HOWELL andJ. H. RUF Mar. 1986 20 p

(NASA-TP-2575; NAS 1.60:2575) Avail: NTIS HC A02/MF A01

CSCL 22A

COMPUTER GRAPHICS, CONTROL SYSTEMS DESIGN,

HUBBLE SPACE TELESCOPE, POINTING CONTROL SYSTEMS

N86-27297"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

THE 1985 GET AWAY SPECIAL EXPERIMENTER'S

SYMPOSIUM

L. R. THOMAS, ed. and F. L. MOSIER, ed. May 1986 295 p

Symposium held in Greenbelt, Md., 8-9 Oct. 1985

(NASA-CP-2401; REPT-86B0015; NAS 1.55:2401) Avail: NTIS

HC A13/MF A01 CSCL 22A

EXPLORER SATELLITES, GET AWAY SPECIALS (STS),

REDUCED GRAVITY, SPACE MANUFACTURING, SPACE

SHUTTLE PAYLOADS, SPACE SHUTTLES

N86-28104" National Aeronautics and Space Administration,

Washington, D.C.

TECHNOLOGY FOR LARGE SPACE SYSTEMS: A

BIBLIOGRAPHY WITH INDEXES (SUPPLEMENT 14)

Jul. 1986 172 p

(NASA-SP-7046(14); NAS 1.21:7046(14)) Avail: NTIS HC A07

CSCL 22A

This bibliography lists 645 reports, articles and other documents

introduced into the NASA scientific and technical information

system between July 1, 1985 and December 31, 1985. Its purpose

is to provide helpful information to the researcher, manager, and

designer in technology development and mission design according

to system, interactive analysis and design, structural and thermal

analysis and design, structural concepts and control systems,

electronics, advanced materials, assembly concepts, propulsion,

and solar power satellite systems. Author

N86-28105" National Aeronautics and Space Administration,

Washington, D.C.

SPACE STATION SYSTEMS: A BIBLIOGRAPHY WITH INDEXES

(SUPPLEMENT 2)

Jul. 1986 232 p

(NASA-SP-7056(02); NAS 1.21:7058(02)) Avail: NTIS HC A10

CSCL 22A

This bibliography lists 904 reports, articles and other documents

introduced into the NASA scientific and technical information

system between July 1, 1985 and December 31, 1985. Its purpose

is to provide helpful information to the researcher, manager, and

designer in technology development and mission design according

to system, interactive analysis and design, structural and thermal

analysis and design, structural concepts and control systems,

63
13 ASTRODYNAMICS

electronics, advanced materials, assembly concepts, propulsion,

and solar power satellite systems. The coverage includes

documents that define major systems and subsystems, servicing

and support requirements, procedures and operations, and missions

for the current and future space station. Author

13

ASTRODYNAMICS

Includes powered and free-flight trajectories; and orbital and

launching dynamics.

N78-12113"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AN INTRODUCTION TO ORBIT DYNAMICS AND ITS

APPLICATION TO SATELLITE-BASED EARTH MONITORING

SYSTEMS

D. R. BROOKS Nov. 1977 85 p refs

(NASA-RP-1009; L-11710) Avail: NTIS HC A05/MF A01

CSCL 22A

The long term behavior of satellites is studied at a level of

complexity suitable for the initial planning phases of earth

monitoring missions. First-order perturbation theory is used to

describe in detail the basic orbit dynamics of satellite motion around

the earth and relative to the sun. Surface coverage capabilities of

satellite orbits are examined. Several examples of simulated

observation and monitoring missions are given to illustrate

representative applications of the theory. The examples stress

the need for devising ways of maximizing total mission output in

order to make the best possible use of the resultant data base

as input to those large-scale, long-term earth monitoring activities

which can best justify the use of satellite systems. Author

N79-14121"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

FLIGHT MECHANICS/ESTIMATION THEORY SYMPOSIUM

May 1978 289 p refs Symp. held at Greenbelt, Md., 18-19

Oct. 1977

(NASA-CP-2050) Avail: NTIS HC A13/MF A01 CSCL 22A

CONFERENCES, ORBITAL MECHANICS, ORBITAL POSITION

ESTIMATION, SATELLITE ATTITUDE CONTROL, SATELLITE

ORBITS

N79-26082"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

FLIGHT MECHANICS/ESTIMATION THEORY SYMPOSIUM

A. J. FUCHS, ed Apr. 1979 347 p refs Symp. held at

Greenbelt, Md., 18-19 Oct. 1978

(NASA-CP-2082; G.7813) Avail: NTIS HC A15/MF A01 CSCL

22A

CONFERENCES, FLIGHT MECHANICS, ORBITAL

MECHANICS, ORBITAL POSITION ESTIMATION, SATELLITE

ORBITS, SPACE NAVIGATION

N80-13135"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

TWO-IMPULSE REORIENTATION OF ASYMMETRIC

SPACECRAFT

C. W. MARTZ Washington Dec. 1979 43 p refs

(NASA-TP-1554; L-12921) Avail: NTIS HC A03/MF A01

CSCL 22A

COST ANALYSIS, SATELLITE ATTITUDE CONTROL,

SPACECRAFT MANEUVERS, SPIN STABILIZATION

64

N80-19142"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ORBIT DYNAMICS AND GEOGRAPHICAL COVERAGE

CAPABILITIES OF SATELLITE-BASED SOLAR OCCULTATION

EXPERIMENTS FOR GLOBAL MONITORING OF

STRATOSPHERIC CONSTITUENTS

D. R. BROOKS Mar. 1980 76 p

(NASA-TP-1606; L-12804) Avail: NTIS HC A05/MF A01

CSCL 03B

ATMOSPHERIC COMPOSITION, REMOTE SENSORS,

SATELLITE ORBITS, SOLAR ECLIPSES, STRATOSPHERE

N80-28389"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

FLIGHT MECHANICS/ESTIMATION THEORY SYMPOSIUM

A. J. FUCHS, ed. Washington 1980 260 p refs Symp.

held at Greenbelt, Md., 17-18 Oct. 1979

(NASA-CP-2123) Avail: NTIS HC A12/MF A01 CSCL 22A

CONFERENCES, ORBIT CALCULATION, ORBITAL

MECHANICS, ORBITAL POSITION ESTIMATION, SATELLITE

ORBITS

N81-11070"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

FIFTH ANNUAL FLIGHT MECHANICS/ESTIMATION THEORY

SYMPOSIUM

J. TELES, ed. Oct. 1980 464 p refs Symp. held in

Greenbelt, Md., 21-22 Oct. 1980

(NASA-CP-2152) Avail: NTIS HC A20/MF A01 CSCL 22A

ASTRODYNAMtCS, CONFERENCES, GODDARD TRAJECTORY DETERMINATION SYSTEM, ORBIT CALCULATION, SATELLITE ORBITS

14

GROUND SUPPORT SYSTEMS AND FACILITIES

(SPACE)

Includes launch complexes, research and production facilities;

ground support equipment, e.g., mobile transporters; and

simulators.

N79-12127"# National Aeronautics and Space Administration,

Washington, D.C.

MOONPORT: A HISTORY OF APOLLO LAUNCH FACILITIES

AND OPERATIONS

C. D. BENSON and W. B. FAHERTY 1978 643 p refs

(NASA-SP-4204) Avail: NTIS MF A01; SOD HC CSCL 22D

The development of the Apollo f launch facilities and launch

operations is described from the beginning of design through the

final launch. Management techniques, innovation in automation,

and testing on the ground to avoid failures in space are among

the topics covered. The impact of the Apollo program on the

citrus groves and quiet beaches of Florida's east coast is

included. J.M.S.

N79-20166"# National Aeronautics and Space Administration.

Wallops Flight Center, Wallops Island, Va.

A NEW DIMENSION. WALLOPS ISLAND FLIGHT TEST RANGE:

THE FIRST FIFTEEN YEARS

J. A. SHORTAL Dec. 1978 784 p refs

(NAS6-t 364)

(NASA-RP-1028) Avail: NTIS HC A99/MF A01 CSCL 14B

A record of the first fifteen years (1945-1959) of research and

development tests that were performed at Wallops Island is

presented. It begins with the events that led to the establishment

of the National Advisory Committee for Aeronautics flight test range

on Wallops Island to the first year as a part of the National

Aeronautics and Space Administration. F.O.S.
N82-15095"# Computer Technology Associates, Inc., Arlington,

Va.

OFFICE OF SPACE TERRESTRIAL APPLICATIONS

(OSTA)/APPLICATIONS DATA SERVICE (ADS) DATA SYSTEMS

STANDARDS

B. A. WALTON, ed. Washington Dec. 1981 270 p refs

Proceedings of Workshop held at Greenbelt, Md., 27-29 May

1981

(NASA-CP-2196) Avail: NTIS HC A12/MF A01 CSCL 14B

CONFERENCES, DATA BASES, FILE MAINTENANCE

(COMPUTERS), STANDARDS, USER MANUALS (COMPUTER

PROGRAMS), USER REQUIREMENTS

15

LAUNCH VEHICLES AND SPACE VEHICLES

Includes boosters; operating problems of launch/space vehicle

systems; and reusable vehicles.

N77-29189"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

SKYLAB, CLASSROOM IN SPACE

L. B. SUMMERLIN, ed. Washington 1977 190 p Original

contains color illustrations

(NASA-SP-401; LC-76-30715) Avail: NTIS MF A01; HC SOD

CSCL 22A

Student-designed Skylab experiments are described and the

results reported. Demonstrations performed on Skylab to show

the effect of weightlessness are described. Author

N78-10186"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

PARAMETRIC STUDY OF ASCENT PERFORMANCE OF A

VERTICALLY LAUNCHED HYDROGEN-FUELED SINGLE-STAGE

REUSABLE TRANSPORT

J_ J. REHDER 1977 41 p refs

(NASA-TP-1045) Avail: NTIS HC A03/MF A01 CSCL 22A

CLIMBING FLIGHT, LAUNCH VEHICLES, PROPULSION

SYSTEM PERFORMANCE, ROCKET THRUST

N78-13109"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECT OF PROPULSION SYSTEM CHARACTERISTICS ON

ASCENT PERFORMANCE OF DUAL-FUELED SINGLE-STAGE

EARTH-TO-ORBIT TRANSPORTS

J. J. REHDER Dec. 1977 65 p refs

(NASA-TP-1115; L-11933) Avail: NTIS HC A04/MF A01

CSCL 21H

ASCENT PROPULSION SYSTEMS, LAUNCH VEHICLES,

PROPULSION SYSTEM CONFIGURATIONS, SPACECRAFT

PERFORMANCE

N78-15142"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

SIGNIFICANT INITIAL RESULTS FROM THE ENVIRONMENTAL

MEASUREMENTS EXPERIMENT ON ATS-6

T. A. FRITZ (NOAA, Boulder, Colo.), C. W. ARTHUR (California

Univ., Los Angeles), J. B. BLAKE (Aerospace Corp., Los Angeles),

P. J. COLEMAN, JR. (California Univ., Los Angeles), J. P.

CORRIGAN (NASA. Goddard Space Flight Center), W. D.

CUMMINGS (Grambling State Univ., La.), S. E. DEFOREST

(Alabama Univ., Huntsville), K. N. ERICKSON (Minnesota Univ.,

Minneapolis), A. KONRADI (NASA. Johnson Space Center), W.

LENNARTSSON (NASA. Marshall Space Flight Center) et al. Dec.

1977 34 p refs

(NASA-TP-1101; G-7702-F15) Avail: NTIS HC A03/MF A01

CSCL 22A

ATS 6, ELECTRON DISTRIBUTION, ENVIRONMENTAL

15 LAUNCH VEHICLES AND SPACE VEHICLES

MONITORING, INTERPLANETARY MAGNETIC FIELDS, ION

DISTRIBUTION, RADIATION MEASUREMENT

N78-15143"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

AN ACTIVE NUTATION DAMPER FOR SPACECRAFT

R. A. ABERCROMBIE and T. W. FLATLEY Dec. 1977 24 p

(NASA-TP-1108; G-7702-F23) Avail: NTIS HC A02/MF A01

CSCL 22B

ACCELEROMETERS, NUTATION, NUTATION DAMPERS,

SPACECRAFT CONTROL

N78-15149"# National Aeronautics and Space Administration,

Washington, D.C.

LUNAR IMPACT: A HISTORY OF PROJECT RANGER

R.C. HALL 1977 467 p refs

(NASA-SP-4210) Avail: NTIS MF A01; HC SOD $6.25 CSCL

22A

Complete history of the Ranger project is provided as a tool

for understanding the evolution and operational form of NASA's

continuing progress of unmanned space exploration. Basic

management techniques, flight operating procedures and

technology for NASA's later unmanned lunar and planetary

missions were reviewed. Methods for selecting experiments and

integrating them with the spacecraft were also investigated.

Author

N78-17127"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

PURGING OF A TANK-MOUNTED MULTILAYER INSULATION

SYSTEM BY GAS DIFFUSION

I. E. SUMNER Jan. 1978 59 p refs

(NASA-TP-1127; E-9286) Avail: NTIS HC A04/MF A01 CSCL

22B

CRYOGENIC FLUID STORAGE, GASEOUS DIFFUSION,

HELIUM, MULTILAYER INSULATION, PROPELLANT TANKS,

PURGING

N78-21193"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

THEORETICAL CONTAMINATION OF CRYOGENIC SATELLITE

TELESCOPES

M. MURAKAMI (Tokyo Univ., Japan) Apr. 1978 49 p refs

(NASA-TP-1177; A-7024) Avail: NTIS HC A03/MF A01 CSCL

22A

CRYOGENIC EQUIPMENT, SPACECRAFT CONTAMINATION,

TELESCOPES

N78-28150"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

THERMAL PERFORMANCE OF GASEOUS-HELIUM-PURGED

TANK-MOUNTED MULTILAYER INSULATION SYSTEM DURING

GROUND-HOLD AND SPACE-HOLD THERMAL CYCLING AND

EXPOSURE TO WATER VAPOR

I. E. SUMNER Aug. 1978 74 p

(NASA-TP-1114; E-9443) Avail: NTIS HC A04/MF A01 CSCL

22B

HELIUM, MULTILAYER INSULATION, TANKS (CONTAINERS),

THERMAL CYCLING TESTS

N79-10078"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

LARGE SPACE SYSTEMS TECHNOLOGY, VOLUME 1

E. C. NAUMANN, comp. and A. BUTTERFIELD, comp. (GE Co.)

1978 540 p Seminar held at Hampton, Va., 17-19 Jan. 1978

2 Vol.

(NASA-CP-2035-VOL-1; L-12068) Avail: NTIS HC A23/MF A01

CSCL 22B

CONFERENCES, LARGE SPACE STRUCTURES, MISSION

PLANNING, ORBITAL ASSEMBLY, SPACE ERECTABLE

STRUCTURES, TECHNOLOGY ASSESSMENT

65
15 LAUNCHVEHICLESANDSPACEVEHICLES

N79-10097"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

LARGE SPACE SYSTEMS TECHNOLOGY, VOLUME 2

E. C. NAUMANN, comp. and A. BUTTERFIELD, comp. 1978

505 p Seminar held at Hampton, Va., 17-19 Jan. 1978 2 Vol.

(NASA-CP-2035-VOL-2; L-12068-VOL-2) Avail: NTIS HC

A22/MF A01 CSCL 22B

CONFERENCES, LARGE SPACE STRUCTURES,

TECHNOLOGY ASSESSMENT

N80-19145"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

LARGE SPACE SYSTEMS TECHNOLOGY, 1979

J. C. WARD, JR., comp. Feb. 1980 487 p refs Ann.

Program Tech. Rev. (1st) held at Hampton, Va., 7-8 Nov. 1979

(NASA-CP-2118; L-13488) Avail: NTIS HC A21/MF A01

CSCL 22B

ANTENNA DESIGN, CONFERENCES, LARGE SPACE

STRUCTURES, ORBITAL ASSEMBLY, RETRACTABLE

EQUIPMENT

N81-19164"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

LARGE SPACE SYSTEMS TECHNOLOGY, 1980, VOLUME 1

F. KOPRIVER, III, comp. Feb. 1981 445 p refs Presented

at the 2nd Ann. Tech. Rev., Hampton, Va., 18-20 Nov. 1980

(NASA-CP-2168; L-14219-VOL-1) Avail: NTIS HC A19/MF A01

CSCL 22B

ANTENNA ARRAYS, CONTROL THEORY, LARGE SPACE

STRUCTURES, SPACE PLATFORMS

N81-19196"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

THE 1980 LARGE SPACE SYSTEMS TECHNOLOGY. VOLUME

2: BASE TECHNOLOGY

F. KOPRIVER, III, comp. (Systems Management Associates,

Hampton, Va.) Feb. 1981 188 p refs Second Annual

Technical Review held in Hampton, Va., 18-20 Nov. 1980

(NASA-CP-2168-VOL-2; L-14219) Avail: NTIS HC A09/MF A01

CSCL 22B

CONFERENCES, LARGE SPACE STRUCTURES, ORBITAL

ASSEMBLY, PLATFORMS, SPACE ERECTABLE STRUCTURES,

SPACECRAFT ANTENNAS, STRUCTURAL ANALYSIS

N81-26166"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

STRUCTURAL DYNAMICS AND CONTROL OF LARGE SPACE

STRUCTURES

E. B. LIGHTNER, comp. Jun. 1981 136 p refs Proc. held at

Hampton, Va., 30-3t Oct. 1980

(NASA-CP-2187; L-14609) Avail: NTIS HC A07/MF A01

CSCL 22B

CONFERENCES, DYNAMIC STRUCTURAL ANALYSIS, LARGE

SPACE STRUCTURES, SELF ADAPTIVE CONTROL SYSTEMS,

SYSTEMS ENGINEERING

N82-14202"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

COMPARATIVE ANALYSES OF SPACE-TO-SPACE CENTRAL

POWER STATIONS

P. F. HOLLOWAY and L. B. GARRETT Dec. 1981 49 p refs

(NASA-TP-1955; L-14766) Avail: NTIS HC A03/MF A01

CSCL 22B

COST EFFECTIVENESS, EARTH ORBITS, LASER

APPLICATIONS, POWER EFFICIENCY, SPACE POWER UNIT

REACTORS, TRANSFER ORBITS

66

N82-14203"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

SYSTEM ANALYSIS APPROACH TO DERIVING DESIGN

CRITERIA (LOADS) FOR SPACE SHUTTLE AND ITS

PAYLOADS. VOLUME 1: GENERAL STATEMENT OF

APPROACH

R. S. RYAN, T. BULLOCK, W. B. HOLLAND, D. A. KROSS, and

L. A. KIEFLING Dec. 1981 47 p

(NASA-TP-1949; M-358) Avail: NTIS HC A03/MF A01 CSCL

22B

AERODYNAMIC LOADS, HUDDLE SPACE TELESCOPE,

SPACECRAFT DESIGN, SPACELAB, STRUCTURAL DESIGN

CRITERIA, SYSTEMS ANALYSIS

N82-15106"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

SYSTEM ANALYSIS APPROACH TO DERIVING DESIGN

CRITERIA (LOADS) FOR SPACE SHUTTLE AND ITS

PAYLOADS. VOLUME 2: TYPICAL EXAMPLES

R. S. RYAN, T. BULLOCK, W. B. HOLLAND, D. A. KROSS, and

L. A. KIEFLING Dec. 1981 128 p refs

(NASA-TP-1950; M-359-VOL-2) Avail: NTIS HC A07/MF A01

CSCL 22B

AEROSPACE SYSTEMS, AEROSPACE VEHICLES, DESIGN

ANALYSIS, DYNAMIC LOADS, LOADS (FORCES), STRUCTURAL

DESIGN CRITERIA

N82-18275"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

LARGE SPACE SYSTEMS TECHNOLOGY, 1981

W. J. BOYER, comp. Mar. 1982 430 p refs Presented at

Third Annual Technical Review, Hampton, Va., 16-19 Nov. 1981

(NASA-CP-2215-PT-1; L-15096) Avail: NTIS HC A19/MF A01

CSCL 22B

ATTITUDE CONTROL, CONFERENCES, LARGE SPACE

STRUCTURES, SPACE PLATFORMS, STRUCTURAL DESIGN

CRITERIA

N82-19257"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

I_,_qGE SPACE SYSTEMS TECHNOLOGY, PART 2, 1981

W. J. BOYER, comp. Mar. 1982 479 p refs Conf. held in

Hampton, Va., 16-t9 Nov. 1981

(NASA-CP-2215-PT-2; L-15096-PT-2) Avail: NTIS HC A21/MF

A01 CSCL 22B

ANTENNA DESIGN, ANTENNAS, LARGE SPACE

STRUCTURES, SHAPE CONTROL

N82-20225"# National Aeronautics and Space Administration,

Washington, D.C.

ORBITING QUARANTINE FACILITY. THE ANTAEUS REPORT

D. L. DEVINCENZI, ed. and J. R. BAGBY, ed. (Colorado State

Univ.) 1981 144 p refs

(NASA-SP-454; NAS 1.21:454; LC-81-600179) Avail: NTIS HC

A07/MF A01 CSCL 22B

A mission plan for the Orbiting Quarantine Facility (OQF) is

presented. Coverage includes system overview, quarantine and

protocol, the laboratory, support systems, cost analysis and

possible additional uses of the OQF. For individual titles, see

N82-20226 through N82-20232.

N83-18819"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

MODELING, ANALYSIS, AND OPTIMIZATION ISSUES FOR

LARGE SPACE STRUCTURES

L. D. PINSON, comp., A. K. AMOS, comp.. (AFOSR, Boiling AFB,

Washington, D.C.), and V. B. VENKAYYA, comp. (AFWAL, Wright

Patterson AFB, Ohio) Feb. 1983 222 p refs Proc. of

workshop held in Williamsburg, Va., 13-14 May 1982

(NASA-CP-2258; NAS 1.55:2258; L-15564) Avail: NTIS HC

A10/MF A01

DYNAMIC CONTROL, DYNAMIC RESPONSE, DYNAMIC

STRUCTURAL ANALYSIS, LARGE SPACE STRUCTURES,
MATHEMATICAL MODELS, OPTIMALCONTROL, THERMAL

STRESSES

N83-22256"#National Aeronautics andSpaceAdministration.

LangleyResearchCenter, Hampton, Va.

STRUCTURAL DYNAMICS AND CONTROL OF LARGE SPACE

STRUCTURES, 1982

M. L. BRUMFIELD, comp. Washington Apr. 1983 261 p

refs Workshop held in Hampton, Va., 21-22 Jan. 1982

(NASA-CP-2266; L-15579; NAS 1.55:2266) Avail: NTIS HC

A12/MFA01 CSCL22B

CONFERENCES, CONTROL THEORY, DYNAMIC

STRUCTURAL ANALYSIS, LARGE SPACE STRUCTURES,

SPACECRAFT CONTROL

N83-26853"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

LARGE SPACE ANTENNA SYSTEMS TECHNOLOGY, PART 1

E. B. LIGHTNER, comp. May 1983 596 p refs Conf. held in

Hampton, Va., 30 Nov. - 3 Dec. 1982 2 Vol.

(NASA-CP-2269-PT-1; L-15614-PT-1; NAS 1.55:2269-PT-1)

Avail: NTIS HC A25/MF A01 CSCL 22B

ANTENNA DESIGN, CONFERENCES, LARGE SPACE

STRUCTURES, LONG TERM EFFECTS, PHASED ARRAYS,

STRUCTURAL DESIGN, VERY LONG BASE INTERFEROMETRY

N83-26879"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

LARGE SPACE ANTENNA SYSTEMS TECHNOLOGY, PART 2

E. B. LIGHTNER, comp. May 1983 469 p refs Conf. held in

Hampton, Va., 30 Nov. - 3 Dec. 1982 2 Vol.

(NASA-CP-2269-PT-2; L-15614-PT-2; NAS 1.55:2269-PT-2)

Avail: NTIS HC A20/MF A01 CSCL 22B

CONFERENCES, LARGE SPACE STRUCTURES,

SPACECRAFT ANTENNAS

N83-32826"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

MODAL ANALYSIS OF A NONUNIFORM STRING WITH END

MASS AND VARIABLE TENSION

M. H. RHEINFURTH and Z. J. GALABOFF Aug. 1983 24 p

refs

(NASA-TP-2198; NAS 1.60:2198) Avail: NTIS HC A02/MF A01

CSCL 20K

DISPLACEMENT, LATERAL STABILITY, SHAPES, STRINGS

N83-32828"# National Aeronautics and Space Administration.

Lyndon B. Johnson Space Center, Houston, Tex.

PERFORMANCE REQUIREMENTS ANALYSIS FOR PAYLOAD

DELIVERY FROM A SPACE STATION

A. L. FRIEDLANDER (Science Applications, Inc.), J. K. SOLDNER

(Science Applications, Inc.), J. BELL, ed., G. W. RICKS, R. E.

KINCADE, D. DEATKINS, R. REYNOLDS, B. A. NADER, O. HILL,

G. R. BABB et al. Jul. 1983 228 p refs

(NASA-RP-1110; S-523; NAS 1.61:1110) Avail: NTIS HC

A11/MFA01 CSCL22B

Operations conducted from a space station in low Earth orbit

which have different constraints and opportunities than those

conducted from direct Earth launch were examined. While a space

station relieves many size and performance constraints on the

space shuttle, the space station's inertial orbit has different launch

window constraints from those associated with customary Earth

launches which reflect upon upper stage capability. A performanc_

requirements analysis was developed to provide a reference source

of parametric data, and specific case solutions and upper stage

sizing trade to assist potential space station users and space

station and upper stage developers assess the impacts of a space

station on missions of interest. E.A.K.

15 LAUNCH VEHICLES AND SPACE VEHICLES

N84-17211"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

STEP EXPERIMENT REQUIREMENTS

M. L. BRUMFIELD, comp. Jan. 1984 347 p refs Workshop

held in Hampton, Va., 28 Jun. - 1 Jul. 1983

(NASA-CP-2294; L-15733; NAS 1.55:2294) Avail: NTIS HC

A15/MFA01 CSCL22B

AEROSPACE SCIENCES, AEROSPACE TECHNOLOGY

TRANSFER, CONFERENCES, LARGE SPACE STRUCTURES,

NASA PROGRAMS, PLATFORMS, SPACE STATIONS,

SPACEBORNE EXPERIMENTS

N84-18277"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SPACE STATION TECHNOLOGY, 1983

R. L. WRIGHT, ed. and C. R. MAYS, ed. Feb. 1984 189 p

Workshop held in Williamsburg, Va., 28-31 Mar. 1983

(NASA-CP-2293; L-15732; NAS 1.55:2293) Avail: NTIS HC

A09/MF A01 CSCL 22B

HEAT RADIATORS, LIFE SUPPORT SYSTEMS, MAN

MACHINE SYSTEMS, SOFTWARE ENGINEERING, SPACE

STATIONS, SPACECRAFT COMMUNICATION, SJSER

REQUIREMENTS

N84-24632"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

LONG DURATION EXPOSURE FACILITY (LDEF). MISSION 1

EXPERIMENTS

L. G CLARK, ed., W. H. KINARD, ed., D. L. CARTER, JR., edo,

and J. L. JONES, JR., ed. Washington Feb. 1984 196 p

(NASA-SP-473; L-15230; NAS 1.21:473) Avail: NTIS HC

A09/MF A01; also available SOD HC CSCL 22A

Spaceborne experiments using the space shuttle payload known

as the Long Duration Exposure Facility are described. Experiments

in the fields of materials, coatings, thermal systems, power and

propulsion, electronic, and optics are discussed. For individual titles,

see N84-24633 through N84-24690.

N85-16989"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

OTV PROPULSION ISSUES

Washington Apr. 1984 296 p refs Conf. held in Cleveland,

3-4 Apr. 1984

(NASA-CP-2347; E-2171; NAS 1.55:2347) Avail: NTIS HC

A13/MFA01 CSCL22B

AEROASSIST, CONFERENCES, CRYOGENIC FLUIDS, ORBIT

TRANSFER VEHICLES, PROPULSION SYSTEM CONFIGURATIONS

N85-19003"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SPACE SHUTTLE ORBITER TRIMMED CENTER-OF-GRAVITY

EXTENSION STUDY Summary Report

W. I. SCALLION and W. P. PHILLIPS Mar. 1985 53 p refs

(NASA-TP-2284; L-15701; NAS 1.60:2284) Avail: NTIS HC

A04/MF A01 CSCL 22B

AERODYNAMIC CONFIGURATIONS, CANARD CONFIGURATIONS, CENTER OF GRAVITY, SPACE SHUTTLE ORBITERS

N85-23813"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va,

LARGE SPACE ANTENNA SYSTEMS TECHNOLOGY, 1984

W. J. BOYER, comp. Apr. 1985 466 p rets Conf. held in

Hampton, Va., 4-6 Dec. 1984 2 Vol.

(NASA-CP-2368-PT-1; L- t 5950-PT-1; NAS 1.55:2368-PT-1)

Avail: NTIS HC A20/MF A01 CSCL 22B

ANTENNA DESIGN, CONFERENCES, DYNAMIC

STRUCTURAL ANALYSIS, LARGE SPACE STRUCTURES,

SATELLITE ANTENNAS

67
15 LAUNCH VEHICLES AND SPACE VEHICLES

N85-23840"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

LARGE SPACE ANTENNA SYSTEMS TECHNOLOGY, 1984

W. J. BOYER, comp. Apr. 1985 484 p refs Conf. held in

Hampton, Va., 4-6 Dec. 1984 2 Vol.

(NASA-CP-2368-PT-2; L-15950-PT-2; NAS 1.55:2368-PT-2)

Avail: NTIS HC A21/MF A01 CSCL 22B

ANTENNA DESIGN, CONFERENCES, DYNAMIC

STRUCTURAL ANALYSIS, LARGE SPACE STRUCTURES, SPACE

SHUTTLE PAYLOADS, SPACE STATIONS

N85-34148°# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

SPACE STATION ROTATIONAL EQUATIONS OF MOTION

M H. RHEINFURTH and S. N. CARROLL Aug. 1985 21 p

(NASA-TP-2511; NAS 1.60:2511) Avail: NTIS HC A02/MF A01

CSCL 22B

EQUATIONS OF MOTION, LARGE SPACE STRUCTURES,

SPACE STATIONS, SPACECRAFT CONTROL

N85-34149"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

POTENTIAL SPIN-OFFS OF THE CARBON DIOXIDE

OBSERVATIONAL PLATFORM SYSTEM (CO-OPS) FOR

REMOTE SENSING OPPORTUNITIES

J. B. STEPHENS 1985 36 p refs

(NASA-TP-2510; NAS 1.60:2510) Avail: NTIS HC A03/MF A0t

CSCL 22B

ATMOSPHERIC COMPOSITION, CARBON DIOXIDE, CARBON

DIOXIDE CONCENTRATION, REMOTE SENSING, WATER

VAPOR

N86-11215"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

PROBLEMS EXPERIENCED AND ENVISIONED FOR

DYNAMICAL PHYSICAL SYSTEMS

R. S. RYAN Aug. 1985 148p refs

(NASA-TP-2508; M-494; NAS 1.60:2508) Avail: NTIS HC

A07/MF A01 CSCL 22B

CONTROL SYSTEMS DESIGN, LARGE SPACE STRUCTURES,

SPACECRAFT DESIGN, SYSTEMS ENGINEERING

N86-20460"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

STAR 48 SOLID ROCKET MOTOR NOZZLE ANALYSES AND

INSTRUMENTED FIRINGS

R. L. PORTER Mar. 1986 58 p refs

(NASA-TP-2572; NAS 1.60:2572) Avail: NTIS HC A04/MF A01

CSCL 21H

COMPUTER PROGRAMS, NOZZLE DESIGN, ROCKET

NOZZLES, SOLID PROPELLANT ROCKET ENGINES, STRESS

ANALYSIS

N86-24722"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

PASSIVE EDDY-CURRENT DAMPING AS A MEANS OF

VIBRATION CONTROL IN CRYOGENIC TURBOMACHINERY

R. E. CUNNINGHAM Feb. t986 14 p refs

(NASA-TP-2562; E-2762; NAS 1.60:2562) Avail: NTIS HC

A02/MF A01 CSCL 131

BEARINGS, CRYOGENICS, DAMPING, EDDY CURRENTS,

ROTOR AERODYNAMICS, TURBINE PUMPS

N86-30753"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

A MECHANICAL PROPERTY AND STRESS CORROSION

EVALUATION OF VlM-ESR-VAR WORK STRENGTHENED AND

DIRECT DOUBLE AGED INCONEL 718 BAR MATERIAL

J. W. MONTANO Sep. 1986 37 p

(NASA-TP-2634; NAS 1.60:2634) Avail: NTIS HC A03/MF A01

CSCL 11F

ARC MELTING, ELECTROSLAG REFINING, INCONEL

(TRADEMARK), INDUCTION HEATING, MECHANICAL

PROPERTIES, STRESS CORROSION, VACUUM MELTING

68

16

SPACE TRANSPORTATION

Includes passenger and cargo space transportation, e.g., shuttle

operations; and space rescue techniques.

N78-20176"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

STATIC AND DYNAMIC STABILITY ANALYSIS OF THE SPACE

SHUTTLE VEHICLE-ORBITER

W. J. CHYU, R. K. CAVIN (Texas A and M Univ., College Station),

and L. L. ERICKSON Mar. 1978 62 p refs

(NASA-TP-1179; A-7217) Avail: NTIS HC AO4/MF A01 CSCL

22B

DYNAMIC STABILITY, SPACE SHUTTLE ORBITERS, STATIC

STABILITY

N78-33135"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

NITRIC OXIDE PRODUCTION IN THE STRATOSPHERE WITHIN

THE SPACE SHUTTLE'S SOLID ROCKET MOTOR PLUMES

R. i. GOMBERG, J. R. BRANNAN, and L. R. BONEY Oct. 1978

31 p refs

(NASA-TP-1305; L-12182) Avail: NTIS HC A03/MF A01

CSCL 04A

NITROGEN OXIDES, SOLID PROPELLANT ROCKET

ENGINES, SPACE SHUTTLES, STRATOSPHERE

N79-21119"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

NEAR-FIELD SONIC-BOOM PRESSURE SIGNATURES FOR THE

SPACE SHUTTLE LAUNCH AND ORBITER VEHICLES AT MACH

6

G. C. ASHBY, JR. Apr. 1979 36 p refs

(NASA-TP-1405; Lo12638) Avail: NTIS HC A03/MF A01

CSCL 20A

LAUNCH VEHICLES, SIGNATURES, SONIC BOOMS, SPACE

SHUTTLE ORBITERS

N80-30367"# National Aeronautics and Space Administration,

Washington, D.C.

THE SPACE SHUTTLE AT WORK

H. ALLAWAY 1979 83 p Original contains color illustrations

(NASA-SP-432; NASA-EP-156) Avail: NTIS HC $3.75/MF $3.75

CSCL 22B

The concept of the orbital flight of the space shuttle and the

development of the space transportation system are addressed.

How the system came to be, why it is designed the way it is,

what is expected of it, and how it may grow are among the questions

considered. Emphasis is placed on the effect of the space

transportation system on U.S. space exploration in the next decade,

including plans to make space an extension of life on the Earth's

surface. JM.S.

N81-16111"# National Aeronautics and Space Administration,

Washington, D.C.

SPACE TRANSPORTATION SYSTEM AND ASSOCIATED

PAYLOADS: GLOSSARY, ACRONYMS, AND ABBREVIATIONS

Jan. 1981 265 p

(NASA-RP-1059) Avail: NTIS HC A12/MF A01 CSCL 22A

A collection of acronyms in everyday use concerning shuttle

activities is presented. A glossary of terms pertaining to the Space

Transportation System is included. E.D.K.
17 SPACE COMM., SPACECRAFT COMM., COMMAND AND TRACKING

N82-20236"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

SENSITIVITY ANALYSIS OF THE SPACE SHUTTLE TO ASCENT

WIND PROFILES

O. E. SMITH and L. D. AUSTIN, JR. Mar. 1982 21 p refs

(NASA-TP-1988; M-374; NAS 1.60:1988) Avail: NTIS HC

A02/MF A01 CSCL 22B

CLIMBING FLIGHT, FLIGHT CONDITIONS, FLIGHT

SIMULATION, SPACE SHUTTLES, SPACECRAFT LAUNCHING,

WIND EFFECTS, WIND PROFILES

N85-33169"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

PROCEDURE FOR ESTIMATING ORBITAL DEBRIS RISKS

J. L. CRAFTS and J. P. LINDBERG Aug. 1985 11 p refs

(NASA-TP-2507; M-495; NAS 1.60:2507) Avail: NTIS HC

A02/MF A01 CSCL 22A

EARTH ORBITS, ENVIRONMENT EFFECTS, ESTIMATES,

RISK, SPACE DEBRIS

N82-33417"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

ATMOSPHERIC CONSTRAINT STATISTICS FOR THE SPACE

SHUTTLE MISSION PLANNING

O. E. SMITH, G. W. BATTS (Computer Sciences Corp., Huntsville,

Ala.), and J. A. WlLLETT (Computer Sciences Corp., Huntsville,

Ala.) Aug. 1982 39 p refs

(NASA-TP-2069; NAS 1.60:2069) Avail: NTIS HC A03/MF A01

CSCL 22A

ATMOSPHERIC EFFECTS, MISSION PLANNING, SPACE

SHUTTLES

N84-10115"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SHUTTLE PERFORMANCE: LESSONS LEARNED, PART 1

J. P. ARRINGTON, comp. and J. J. JONES, comp. Washington

Oct. 1983 647 p refs Conf. held in Hampton, Va., 8-10 Mar.

1983 2 Vol.

(NASA-CP-2283-PT-1; L-15673-PT-1; NAS 1.55:2283-PT-1)

Avail: NTIS HC A99/MF A01 CSCL 22B

AEROTHERMODYNAMICS, ASCENT TRAJECTORIES,

CONFERENCES, ENTRY GUIDANCE (STS), SPACE SHUTTLES

N84-10144"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SHUTTLE PERFORMANCE: LESSONS LEARNED, PART 2

J. P. ARRINGTON, comp. and J. J. JONES, comp. Washington

Oct. 1983 746 p refs Conf. held in Hampton, Va., 8-10 Mar.

1983 2 Vol.

(NASA-CP-2283-PT-2; L-15673-PT-2; NAS 1.55:2283-PT-2)

Avail: NTIS HC A99/MF A01 CSCL 22B

AEROTHERMODYNAMICS, ASCENT TRAJECTORIES,

CONFERENCES, ENTRY GUIDANCE (STS), SPACE SHUTTLES

17

SPACE COMM., SPACECRAFT COMM., COMMAND

AND TRACKING

Includes telemetry; space communications

astronavigation and guidance; and radio blackout.

networks;

N78-10200"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

PRELAUNCH TESTING OF THE LASER GEODYNAMIC

SATELLITE (LAGEOS)

M. W. FITZMAURICE, P. O. MINOTT, J. B. ABSHIRE, and H. E.

ROWE 1977 100 p refs

(NASA-TP-1062; G-7702-F16) Avail: NTIS HC A05/MF A01

CSCL 22A

LAGEOS (SATELLITE), LASER RANGE FINDERS,

PRELAUNCH TESTS

N78-28159"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

CARRIER-INTERFERENCE RATIOS FOR FREQUENCY SHARING

BETWEEN FREQUENCY-MODULATED AMPLITUDE-MODULATED-VESTIGIAL-SIDEBAND TELEVISION SYSTEMS

SYSTEMS

S. P. BARNES and E. F. MILLER Aug. 1978 29 p refs

(NASA-TP-1264; E-9478) Avail: NTIS HC A03/MF A01 CSCL

17B

AMPLITUDE MODULATION, ELECTROMAGNETIC INTERFERENCE, FREQUENCY MODULATION, TELEVISION SYSTEMS

N85-15778"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECT OF AERODYNAMIC AND ANGLE-OF-ATTACK

UNCERTAINTIES ON THE MAY 1979 ENTRY FLIGHT CONTROL

SYSTEM OF THE SPACE SHUTTLE FROM MACH 8 TO 1.5

H.W. STONE and R.W. POWELL Jan. 1985 137p refs

(NASA-TP-2365; L-15813; NAS 1.60:2365) Avail: NTIS HC

A07/MF A01 CSCL 22B

AERODYNAMIC CHARACTERISTICS, ANGLE OF ATTACK,

DEGREES OF FREEDOM, FLIGHT CONTROL, SPACE SHUTTLE

ORBITERS, SPACECRAFT REENTRY

N85-19007"# National Aeronautics and Space Administration,

Washington, D.C.

SPACE TRANSPORTATION SYSTEM AND ASSOCIATED

PAYLOADS: GLOSSARY, ACRONYMS, AND ABBREVIATIONS

Feb. 1985 309 p Previously announced as N81-16111

(NASA-RP-1059-REV; NAS 1.61:1059-REV) Avail: NTIS HC

A14/MFA01 CSCL22B

A collection of acronyms now in everyday use in the Shuttle

world are listed. It is a combination of lists that were prepared at

the Kennedy and Johnson Space Centers and by the Air Force.

B.G.

N78-33137"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

THERMAL CHARACTERISTICS OF THE 12-GIGAHERTZ,

200-WATT OUTPUT STAGE TUBE FOR THE COMMUNICATIONS

TECHNOLOGY SATELLITE

A. N. CURREN Oct. 1978 39 p refs

(NASA-TP-1344; E-9560) Avail: NTIS HC AO3/MF A01 CSCL

17B

COMMUNICATIONS TECHNOLOGY SATELLITE, HEAT

TRANSFER, TRAVELING WAVE TUBES

N79-21120"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

THERMAL ANOMALIES OF THE TRANSMITTER EXPERIMENT

PACKAGE ON THE COMMUNICATIONS TECHNOLOGY

SATELLITE

R. E. ALEXOVICH and A. N. CURREN Apr. 1979 113 p refs

(NASA-TP-1410; E-9735) Avail: NTIS HC A06/MF A01 CSCL

17B

ANOMALIES, COMMUNICATIONS TECHNOLOGY SATELLITE,

SATELLITE TRANSMISSION

69
17 SPACE COMM., SPACECRAFT COMM., COMMAND AND TRACKING

N81-18082"# National Aeronautics and Space Administration,

Washington, D.C.

RADIO-WAVE PROPAGATION FOR SPACE COMMUNICATIONS

SYSTEMS

L. J. IPPOLITO Feb. 1981 63 p refs

(NASA-TP-1770; EC-4) Avail: NTIS HC A04/MF A01 CSCL

17B

ATMOSPHERIC ATTENUATION, DEPOLARIZATION, RADIO

TRANSMISSION, SATELLITE TRANSMISSION, SPACE

COMMUNICATION

N81-23182"# National Aeronautics and Space Administration.

Lyndon B Johnson Space Center, Houston, Tex.

EXISTENCE AND UNIQUENESS OF SOLUTIONS TO A CLASS

OF NONLINEAR-OPERATOR-DIFFERENTIAL EQUATIONS

ARISING IN AUTOMATED SPACESHIP NAVIGATION

V. M. BOGDAN (Catholic Univ.) Washington May 1981 23 p

refs

(NASA-TP-18601 S-5061 JSC-16755) Avail: NTIS HC A02/MF

A01 CSCL 17G

DIFFERENTIAL EQUATIONS, EXISTENCE THEOREMS,

NONLINEAR EQUATIONS, SPACE NAVIGATION, SPACECRAFT

CONTROL, UNIQUENESS THEOREM

N85-21246"# National Aeronautics and Space Administration.

Wallops Flight Center, Wallops Island, Va.

WIND-WEIGHTING FOR SOUNDING ROCKETS WITH A

TELEMETRY SYSTEM

F. M. BOYKIN Apr. 1985 12 p

(NASA-TP-2438; NAS 1.60:2438) Avail: NTIS HC A02/MF A01

CSCL 09F

RADIOSONDES, TELEMETRY, TRACKING (POSITION), WIND

MEASUREMENT

N86-23620"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

SPACE STATION WORKSTATION TECHNOLOGY WORKSHOP

REPORT

K. L. MOE, C. M. EMERSON, D. R. EIKE (Carlow Associates,

Fairfax, Va.), and T. B. MALONE (Carlow Associates, Fairfax, Va.)

Mar 1985 135 p

(NAS5-28597)

(NASA-CP-2414; 4033-85-tDRE; NAS 1.55:2414) Avail: NTIS

HC A07/MF A01 CSCL 22B

HUMAN FACTORS ENGINEERING, MAN MACHINE SYSTEMS.

SPACE STATIONS, TECHNOLOGY ASSESSMENT, WORKSTATIONS

18

SPACECRAFT DESIGN, TESTING AND

PERFORMANCE

Includes satellites; space platforms; space stations; spacecraft

systems and components such as thermal and environmental

controls; and attitude controls.

N76-28296"# National Aeronautics and Space Administration,

Washington, D.C.

VIKING 1: EARLY RESULTS

21 Aug. 1976 76 p

(NASA-SP-408) Avail: NTIS HC $2.00 CSCL 22B

A brief outline of the Viking 1 mission to Mars is followed by

descriptions of the Martian landing site and the scientific

instrumentation aboard Viking 1 orbiter and lander. Measurements

of the Martian atmosphere provided data on its molecular

composition, temperature and pressure. The detection of nitrogen

in the Martian atmosphere indicates the existence of life. Panoramic

photographs of the Martian surface were also obtained and are

shown. Preliminary chemical and biological investigations on

samples of Martian soil indicated the presence of the elements

iron, calcium, silicon, titanium and aluminum as major constituents.

Observed biochemical reactions were judged conducive of

biological activity. G.G.

N77-33259"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ENTRY DYNAMICS OF SPACE SHUTTLE ORBITER WITH

LONGITUDINAL STABILITY AND CONTROL UNCERTAINTIES

AT SUPERSONIC AND HYPERSONIC SPEEDS

H W. STONE and R. W. POWELL Oct. 1977 67 p refs

(NASA-TP-1084; L-11288) Avail: NTIS HC A04/MF A01

CSCL 22B

AERODYNAMIC STABILITY, CONTROL STABILITY,

LONGITUDINAL STABILITY, SPACE SHUTTLE ORBITERS

N78-13119"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ENTRY DYNAMICS OF SPACE SHUTTLE ORBITER WITH

LATERAL-DIRECTIONAL STABILITY AND CONTROL

UNCERTAINTIES AT SUPERSONIC AND HYPERSONIC

SPEEDS

H. W. STONE and R. W. POWELL Dec. 1977 103 p refs

(NASA-TP-1011; L-11112) Avail: NTIS HC A06/MF A01

CSCL 22A

ATMOSPHERIC ENTRY, DIRECTIONAL STABILITY, LATERAL

STABILITY, SPACE SHUTTLE ORBITERS

N78-21200"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

THE N-BOD2 USER'S AND PROGRAMMER'S MANUAL

H. P. FRISCH Feb. 1978 307 p refs

(NASA-TP-1145; G-7702-F22) Avail: NTIS HC A14/MF A01

CSCL 22B

ATTITUDE CONTROL, COMPUTER SYSTEMS PROGRAMS,

DIGITAL COMPUTERS, SPACECRAFT CONTROL, USER

MANUALS (COMPUTER PROGRAMS)

N78-25123"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

A DIGITAL COMPUTER PROGRAM FOR THE DYNAMIC

INTERACTION SIMULATION OF CONTROLS AND STRUCTURE

(DISCOS), VOLUME 1

C. S. BODLEY (Martin Marietta Corp., Denver), A. D. DEVERS

(Martin Marietta Corp., Denver), A. C. PARK (Martin Marietta Corp,

Denver), and H. P. FRISCH May 1978 169 p refs

(NASA-TP-1219-VOL-1; G-7702-F26-VOL-1) Avail: NTIS HC

A08/MF A01 CSCL 22B

ATTITUDE CONTROL, COMPUTERIZED SIMULATION,

SPACECRAFT CONTROL

N78-25124"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

A DIGITAL COMPUTER PROGRAM FOR THE DYNAMIC

INTERACTION SIMULATION OF CONTROLS AND STRUCTURE

(DISCOS), VOLUME 2

C. S. BODLEY (Martin Marietta Corp., Denver), A. D. DEVERS

(Martin Marietta Corp., Denver), A. C. PARK (Martin Marietta Corp.,

Denver), and H. P. FRISCH May 1978 368 p

(NASA-TP-1219-VOL-2; G-7702-F26-VOL-2) Avail: NTIS HC

A16/MF A01 CSCL 22B

ATTITUDE CONTROL, COMPUTERIZED SIMULATION,

SPACECRAFT CONTROL

N79-15149"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

JUPITER PROBE CHARGING STUDY

C. K. PURVIS Jan. 1979 38 p refs

(NASA-TP-1263; E-9167) Avail: NTIS HC A03/MF A01 CSCL

22B

ELECTROSTATIC CHARGE, JUPITER PROBES,

SPACECRAFT CHARGING, SPACECRAFT DESIGN

70
18 SPACECRAFTDESIGN,TESTINGANDPERFORMANCE

N79-24001"#National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

SPACECRAFT CHARGING TECHNOLOGY, 1976

1979 908 p refs Conf. held at Colorado Springs, Colo., 31

Oct. - 2 Nov. 1978; sponsored by NASA and AFGL

(NASA-CP-2071; AFGL-TR-79-0082) Avail: NTIS HC A99/MF

A01 CSCL 22B

AEROSPACE ENVIRONMENTS, CONFERENCES, PARTICLE

INTERACTIONS, PLASMA INTERACTIONS, SPACECRAFT

CHARGING, SPACECRAFT ENVIRONMENTS

N79-27237"# Martin Marietta Aerospace, Denver, Colo.

HANDBOOK ON ASTRONAUT CREW MOTION DISTURBANCES

FOR CONTROL SYSTEM DESIGN

M. C. KULLAS May 1979 196 p refs

(NAS2-2982)

(NASA-RP-1025; L-12299) Avail: NTIS HC AO9/MF A01

CSCL 22B

The analyses and results pertinent to the characterization of

the disturbances imparted to the Skylab vehicle by the T-013

crew motion experiments are summarized. Guidelines to help

control system designers assess anticipated crew motion

disturbances during the design cycle of a new manned spacecraft

control system are provided. These guidelines, in conjunction with

the T-013 characterizations outlined, begin with the control system

conceptual design and conclude with preliminary expectations for

pointing performance as affected by crew motions. Block diagrams

to highlight the contents so that the reader can easily identify the

information and data flow are used. These diagrams provide a

handy cross reference of related topics. S.E.S.

N80-16091"# National Aeronautics and Space Administration.

Lyndon B. Johnson Space Center, Houston, Tex.

ORBITER LANDING LOADS MATH MODEL DESCRIPTION AND

CORRELATION WITH ALT FLIGHT DATA

D. A. HAMILTON, J. A. SCHLIESING, and G. A. ZUPP, JR.

Washington Jan. 1980 27 p refs

(NASA-RP-1056; JSC-16202; S-498) Avail: NTIS HC A03/MF

A01 CSCL 22B

Results of the space shuttle approach and landing test are

examined in order to assess landing gear characteristics and

performance and verify landing dynamic analyses. The landing

gears were instrumented with load-calibrated strain gages, a

wheel-speed sensor, and strut stroke measurement devices. The

mathematical procedure used in predicting the shuttle touchdown

loads and dynamics is presented together with the comparisons

between measured flight data and the analytical predictions.

Conclusions from these data are also presented. J.M.S.

N80-29417"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ANALYSIS OF SPACE SHUTTLE ORBITER ENTRY DYNAMICS

FROM MACH 10 TO MACH 2.5 WITH THE NOVEMBER 1976

FLIGHT CONTROL SYSTEM

R. W. POWELL and H. W. STONE Aug. 1980 163 p

(NASA-TP-1667; L-13344) Avail: NTIS HC A08/MF A01

CSCL 22B

ATMOSPHERIC ENTRY SIMULATION, AUTOMATIC PILOTS,

CONTROL SIMULATION, REENTRY GUIDANCE, SPACE

SHUTTLE ORBITERS

N80-32429"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

DEVELOPMENT OF THE REENTRY FLIGHT DYNAMICS

SIMULATOR FOR EVALUATION OF SPACE SHUTTLE ORBITER

ENTRY SYSTEMS

L. F. ROWELL, R. W. POWELL, and H. W. STONE, JR.

Washington Oct. 1980 97 p refs

(NASA-TP-1700; L-t3662) Avail: NTIS HC A05/MF A01

CSCL 14B

COMPUTERIZED SIMULATION, DIGITAL COMPUTERS,

ONBOARD EQUIPMENT, REENTRY GUIDANCE, SPACE

SHUTTLE ORBITERS, SPACECRAFT REENTRY

N81-10100"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

VIKING '75 SPACECRAFT DESIGN AND TEST SUMMARY.

VOLUME 1: LANDER DESIGN

N. A. HOLMBERG, R. P. FAUST, and H. M HOLT Nov. 1980

213 p refs 2 Vol.

(NASA-RP-1027-VOL-1; L-12087-VOL-1) Avail: NTIS HC

A10/MF A01 CSCL 22B

The Viking Mars program is summarized. The design of the

Viking lander spacecraft is described. T.M.

N61-10101"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

VIKING '75 SPACECRAFT DESIGN AND TEST SUMMARY.

VOLUME 2: ORBITER DESIGN

N. A. HOLMBERG, R. P. FAUST, and H. M HOLT Nov. 1980

318 p 2 Vol.

(NASA-RP-1027-VOL-2; L-12087-VOL-2) Avail: NTIS HC

A14/MF A01 CSCL 22B

The design of the Viking orbiter spacecraft is described. System

configuration, telecommunications, and guidance and control

requirements are presented. T.M.

N81-11102"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

VIKING '75 SPACECRAFT DESIGN AND TEST SUMMARY.

VOLUME 3: ENGINEERING TEST SUMMARY

N. A. HOLMBERG, R. P. FAUST, and H. M. HOLT Nov. 1980

107 p refs

(NASA-RP-1027-VOL-3; L-12087-VOL-3) Avail: NTIS HC

A06/MF A01 CSCL 22B

The engineering test program for the lander and the orbiter

are presented. The engineering program was developed to achieve

confidence that the design was adequate to survive the expected

mission environments and to accomplish the mission objective.

T.M.

N81-13082"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

DECOUPLED CONTROL OF A LONG FLEXIBLE BEAM IN

ORBIT

H. A. HAMER and K. G. JOHNSON Dec. 1980 77 p refs

(NASA-TP-1740; L-13726) Avail: NTIS HC A05/MF A01

CSCL 22B

ATTITUDE CONTROL, DECOUPLING, FEEDBACK CONTROL,

LARGE SPACE STRUCTURES, MODAL RESPONSE

N81-19218"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

PRELIMINARY VIBRATION, ACOUSTIC, AND SHOCK DESIGN

AND TEST CRITERIA FOR COMPONENTS ON THE

LIGHTWEIGHT EXTERNAL TANK (LWT)

Feb. 1981 322 p refs

(NASA-RP-1074; M-343) Avail: NTIS HC A14/MF A01 CSCL

22B

The Space Shuttle LWT is divided into zones and subzones.

Zones are designated primarily to assist in determining the

applicable specifications. A subzone (general Specification) is

available for use when the location of the component is known

but component design and weight are not well defined. When the

location, weight, and mounting configuration of the component

are known, specifications for appropriate subzone weight ranges

are available. Along with the specifications are vibration, acoustic,

shock, transportation, handling, and acceptance test requirements

and procedures. A method of selecting applicable vibration,

acoustic, and shock specifications is presented. A.R.H.

71
18 SPACECRAFTDESIGN,TESTINGANDPERFORMANCE

N81-21116"#National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

PERFORMANCE OF A HAYNES 188 METALLIC STANDOFF

THERMAL PROTECTION SYSTEM AT MACH 7

D. E. AVERY Apr. 1981 44 p refs

(NASA-TP-1802; L-13903) Avail: NTIS HC A03/MF A01

CSCL 22B

AEROTHERMODYNAMICS, COBALT ALLOYS, REENTRY

SHIELDING, THERMAL PROTECTION

N81-25138"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

PITFALLS AND GUIDELINES FOR THE NUMERICAL

EVALUATION OF MODERATE-ORDER SYSTEM FREQUENCY

RESPONSE

H. P. FRISCH Jun. 1981 36 p refs

(NASA-TP-1814) Avail: NTIS HC A03/MF 01 CSCL 22C

DYNAMIC RESPONSE, ERROR ANALYSIS, FEEDBACK

CONTROL, NUMERICAL ANALYSIS

N81-25139"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

TIME AND FREQUENCY DOMAIN ANALYSIS OF SAMPLED

DATA CONTROLLERS VIA MIXED OPERATION EQUATIONS

H. P. FRISCH Jun. 1981 25 p refs

(NASA-TP-1817) Avail: NTIS HC A02/MF A01 CSCL 22B

DYNAMIC RESPONSE, FREQUENCY ANALYZERS, NUMERICAL ANALYSIS, SPACECRAFT CONTROL, SPACECRAFT GUIDANCE

N81-25140"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

REDUCED ORDER FEEDBACK CONTROL EQUATIONS FOR

LINEAR TIME AND FREQUENCY DOMAIN ANALYSIS

H. P. FRISCH Jun. 1981 27 p refs

(NASA-TP-1818) Avail: NTIS HC A03/MF A01 CSCL 22B

ALGORITHMS, FEEDBACK CONTROL, FREQUENCY

ANALYZERS, NUMERICAL ANALYSIS, SPACECRAFT CONTROL,

SPACECRAFT GUIDANCE

N81-29154"# National Aeronautics and Space Administration,

Washington, D.C.

STAGES TO SATURN: A TECHNOLOGICAL HISTORY OF THE

APOLLO/SATURN LAUNCH VEHICLES

R E. BILSTEIN 1981 508 p refs

(NASA-SP-4206) Avail: NTIS HC A22/MF A01 CSCL 22B

The origins of the Saturn 1 launch vehicle as a test bed and

the development of the uprated Saturn B as an interim booster

for the orbital testing of the first Apollo capsules are reviewed in

this narrative account of technological advances responsible for

the AS-506 launch vehicle and the success of the Apollo 11 flight.

The evolution of the engine, including the development of high

energy liquid hydrogen engines and of insulation for extended

storage of cryogenic propellants in vehicle tanks are described as

well as advances in computer technology for the guidance and

contro_ systems. Problems encountered in scaling components and

systems for lunar missions are explored as well as political and

administrative aspects ot the Apollo-Saturn project. A.R.H.

N81-29155"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

METEOROID BUMPER EXPERIMENT ON EXPLORER 46

D. H. HUMES Jul. 1981 31 p refs

(NASA-TP-1879; L-14329) Avail: NTIS HC A02/MF A01

CSCL 22B

BUMPERS, EXPLORER SATELLITES, METEOROID

HAZARDS, METEOROID PROTECTION, SPACECRAFT

SHIELDING

N82-12109"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

SPACECRAFT DYNAMICS AS RELATED TO LABORATORY

EXPERIMENTS IN SPACE

G. H, FICHTL, ed., B. N. ANTAR, ed., and F. G. COLLINS, ed.

Nov. 1981 206 p refs Workshop held in Huntsville, Ala., 1-2

May 1979

(NASA-CP-2199; M-362) Avail: NTIS HC At0/MF A01 CSCL

22B

CONFERENCES, EXPERIMENT DESIGN, FLUID MECHANICS,

PHYSICS AND CHEMISTRY EXPERIMENT IN SPACE,

SPACEBORNE EXPERIMENTS, SPACECRAFT MOTION

N82-14213"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

SPACECRAFT CHARGING TECHNOLOGY, 1980

Washington Oct. 1981 1005 p refs Conf. held in Colorado

Springs, 12-14 Nov. 1980; sponsored by AFGL and NASA Lewis

Research Center

(NASA-CP-2182; AFGL-TR-81-0270) Avail: NTIS HC A99/MF

A01 CSCL 22B

CONFERENCES, DIELECTRIC PROPERTIES, ELECTRON

EMISSION, ELECTRON IRRADIATION, PLASMA INTERACTIONS,

SPACE ENVIRONMENT SIMULATION, SPACECRAFT

CHARGING, SPACECRAFT DESIGN

N82-14276"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

INTERACTIVE DESIGN AND ANALYSIS OF FUTURE LARGE

SPACECRAFT CONCEPTS

L. B. GARRETT Dec. 1981 32 p refs Presented at the 16th

AIAA Thermophys. Conf., Palo Alto, Calif., 23-25 Jun. 1981

(NASA.TP-1937; L-14739) Avail: NTIS HC A03/MF A01

CSCL 22B

ARTIFICIAL SATELLITES, COMPUTER AIDED DESIGN,

INTERACTIVE CONTROL, LARGE SPACE STRUCTURES,

ORBITAL SPACE STATIONS, SPACECRAFT DESIGN,

STRUCTURAL MEMBERS

N82-14277"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

THERMAL AND AEROTHERMAL PERFORMANCE OF A

TITANIUM MULTIWALL THERMAL PROTECTION SYSTEM

D. E. AVERY, J. L. SHIDELER, and R. N. STUCKEY (Johnson

Space Center) Dec. 1981 59 p refs

(NASA-TP-1961; L-14719) Avail: NTIS HC A04/MF A01

CSCL 22B

AEROTHERMODYNAMICS, CERAMIC COATINGS,

PROTECTIVE COATINGS, SPACE SHUTTLES, THERMAL

PROTECTION, TILES, TITANIUM

N82-15116"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

THE AERODYNAMICS OF BODIES IN A RAREFIED IONIZED

GAS WITH APPLICATIONS TO SPACECRAFT

ENVIRONMENTAL DYNAMICS

N. H_ STONE Nov. 1981 320 p refs

(NASA-TP-1933; M-361) Avail: NTIS HC A14/MF A01 CSCL

22B

AERODYNAMICS, COLLISIONLESS PLASMAS, MAGNETOHYDRODYNAMIC FLOW, PLASMA INTERACTIONS, RAREFIED

GAS DYNAMICS, SPACECRAFT CHARGING

72
18 SPACECRAFT DESIGN, TESTING AND PERFORMANCE

N82-16147"# National Aeronautics and Space Administration,

Goddard Space Flight Center, Greenbelt, Md.

ATS-6 ENGINEERING PERFORMANCE REPORT.

VOLUME:PROGRAM AND SYSTEMS SUMMARIES:

MECHANICAL AND THERMAL DETAILS Final Report

R. O. WALES, ed. Nov. 1981 272 p refs 6 Vol.

(NAS5-25464)

(NASA-RP-1080-VOL-1; REPT-81F0034-VOL-1) Avail: NTIS HC

A12/MFA01 CSCL22B

The overall mission and spacecraft systems, testing, and

operations are summarized. The mechanical subsystems are

reviewed, encompassing mechanical design requirements;

separation and deployment mechanisms; design and performance

evaluation; and the television camera reflector monitor. Thermal

control and contamination are discussed in terms of thermal control

subsystems, design validation, subsystems performance, the

advanced flight experiment, and the quartz-crystal microbalance

contamination monitor. NW.

N82-16148"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

ATS-6 ENGINEERING PERFORMANCE REPORT. VOLUME 2:

ORBIT AND ATTITUDE CONTROLS Final Report

R. O. WALES, ed. Nov. 1981 289 p refs 6 Vol.

(NAS5-25464)

(NASA-RP-1080-VOL-2; REPT-81F0034-VOL-2) Avail: NTIS HC

A13/MF A01

Attitude control is reviewed, encompassing the attitude control

subsystem, spacecraft attitude precision pointing and slewing

adaptive control experiment, and RF interferometer experiment.

The spacecraft propulsion system (SPS) is discussed, including

subsystem, SPS design description and validation, orbital

operations and performance, in-orbit anomalies and contingency

operations, and the cesium bombardment ion engine experiment.

Thruster failure due to plugging of the propellant feed passages,

a major cause for mission termination, are considered among the

critical generic failures on the satellite. N.W,

N82-16149"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

ATS-6 ENGINEERING PERFORMANCE REPORT. VOLUME 3:

TELECOMMUNICATIONS AND POWER Final Report

R. O. WALES, ed. Nov. 1981 298 p refs 6 Vol.

(NAS5-25464)

(NASA-RP-1080-VOL-3; REPT-81F0034-VOL-3) Avail: NTIS HC

A13/MFA01 CSCL22B

Functional design requirements and in-orbit operations,

performance, and anomalies are discussed for (1) the

communications subsystem, (2) the electrical power system, and

(3) the telemetry and command subsystem. The latter includes a

review of ground support. Tracking and data relay experiments

and the Apollo-Soyuz test program are reviewed. N.W.

N82-16150"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

ATS-6 ENGINEERING PERFORMANCE REPORT. VOLUME 4:

TELEVISION EXPERIMENTS Final Report

R. O. WALES, ed. Nov. 1981 149 p refs 6 Vol.

(NAS5-25464)

(NASA-RP-1080-VOL-4; REPT-81F0034-VOL-4) Avail: NTIS HC

A04/MF A01 CSCL 22B

Experiments sponsored by the US Department of Health

Education and Welfare are discussed, including

telecommunications, Alaskan health service, Appalachian education

satellite project, and the University of the West Indies. The Satellite

Instructional Television Experiment in India is reviewed.

Independent television experiments are addressed, including

AIDSAT and Project Look Up. N.W.

N82-16151"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

ATS-6 ENGINEERING PERFORMANCE REPORT. VOLUME 5:

PROPAGATION EXPERIMENTS Final Report

R. O. WALES, ed. Nov. 1981 302 p refs 6 Vol.

(NAS5-25464)

(NASA-RP-1080-VOL-5; REPT-81F0034-VOL-5) Avail: NTIS HC

A14/MFA01 CSCL22B

Propagation experiments at 1550 MHz to 1650 MHz are

reviewed, including the Integrated L-Band Experiments system and

results, and the Mobile L-Band Terminals for Satellite

Communication system. Experiments at 4 GHz to 6 GHz are

reported, including the Radio Frequency Interferometer

Measurements system and results, and Earth station antenna

evaluations. Experiments above 10 GHz are discussed, including

Comsat and ATS-6 millimeter wave propagation/experiments, and

communication ATS-6 version at 20 and 30 GHz. N.W.

N82-16152"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

ATS-6 ENGINEERING PERFORMANCE REPORT. VOLUME 6:

SCIENTIFIC EXPERIMENTS Final Report

R. O. WALES, ed. Nov. 1981 166 p refs 6 Vol.

(NAS5-25464)

(NASA-RP-1080-VOL-6; REPT-81F0034-VOL-6) Avail: NTIS HC

A08/MF A01 CSCL 22B

Evaluations include a very high resolution radiometer, a radio

beacon experiment, environmental measurement experiments

(EME), EME support hardware, EME anomalies and failures, EME

results, and US/USSR magnetometer experiments. N.W.

N82-16153"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

THE MICROWAVE RADIOMETER SPACECRAFT: A DESIGN

STUDY

R. L. WRIGHT, ed. Dec. 1981 239 p refs

(NASA-RP-1079; L-14258) Avail: NTIS HC All/MF A01

CSCL 22B

A large passive microwave radiometer spacecraft with near all

weather capability of monitoring soil moisture for global crop

forecasting was designed. The design, emphasizing large space

structures technology, characterized the mission hardware at the

conceptual level in sufficient detail to identify enabling and pacing

technologies. Mission and spacecraft requirements, design and

structural concepts, electromagnetic concepts, and control

concepts are addressed. For individual titles, see N82-16154

through N82-t 6167.

N82-20238"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

APPLICATION OF A COMPUTERIZED VIBROACOUSTIC DATA

BANK FOR RANDOM VIBRATION CRITERIA DEVELOPMENT

R. C. FEREBEE Mar. 1982 32 p refs

(NASA-TP-1998; NAS 1.60:1998; M-376) Avail: NTIS HC

A03/MF A01 CSCL 09B

ACOUSTICS, DATA BASES, POWER SPECTRA, RANDOM

VIBRATION, STRUCTURAL DESIGN CRITERIA, USER MANUALS

(COMPUTER PROGRAMS)

N82-25291"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

TWELFTH SPACE SIMULATION CONFERENCE: SHUTTLE

PLUS ONE. A NEW VIEW OF SPACE

R. T. HOLLINGSWORTH, ed. 1982 339 p refs Conf. held

in Pasadena, Calif., 17-19 May 1982; sponsored by JPL, IES, AIAA

and the Am. Soc. for Testing and Mater.

(NASA-CP-2229; NAS 1.55:2229; REPT-82B0455) Avail: NTIS

HC A15/MF A01 CSCL 22B

GALILEO PROBE, REMOTE SENSING, SPACE

ENVIRONMENT SIMULATION, SPACE SHUTTLE PAYLOADS,

SPACE SHUTTLES, SPACE SIMULATORS, SPACECRAFT

CONTAMINATION, SPACECRAFT MOTION, THERMAL

PROTECTION

73
18 SPACECRAFTDESIGN,TESTINGANDPERFORMANCE

N82-33421"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ILLUMINATION FROM SPACE WITH ORBITING

SOLAR-REFLECTOR SPACECRAFT

J. E. CANADY, JR. and J. L. ALLEN, JR. Sep. 1982 90 p

refs

(NASA-TP-2065; L-15127; NAS 1.60:2065) Avail: NTIS HC

A05/MF A01 CSCL 22B

ILLUMINATING, MIRRORS, SOLAR REFLECTORS

N83-19806"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

A MOBILE WORK STATION CONCEPT FOR MECHANICALLY

AIDED ASTRONAUT ASSEMBLY OF LARGE SPACE TRUSSES

W. L. HEARD, JR., H. G. BUSH, R. E. WALLSON (Kentron

International, Inc., Hampton, Va.), and J. K. JENSEN (Kentron

International, Inc., Hampton, Va.) Mar. t983 36 p refs

(NASA-TP-2108; L-15523; NAS 1.60:2108) Avail: NTIS HC

A03/MF A01 CSCL 22B

BUOYANCY, EXTRAVEHICULAR MOBILITY UNITS, LARGE

SPACE STRUCTURES, TRUSSES, WEIGHTLESSNESS

N83-22317"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

PERFORMANCE OF AN ABLATOR FOR SPACE SHUTTLE

INORBIT REPAIR IN AN ARC-PLASMA AIRSTREAM

D. A. STEWART, M. CUELLAR (San Jose State Univ.), and O.

FLOWERS Apr. 1983 18 p refs

(NASA-TP-2150; A-9112; NAS 1.60:2150) Avail: NTIS HC

A02/MF A01 CSCL 22B

AEROSPACE ENVIRONMENTS, ATMOSPHERIC ENTRY,

CAULKING, SPACE SHUTTLES, TECHNOLOGY ASSESSMENT,

THERMAL PROTECTION

N83-31713"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ANALYSIS OF GAP HEATING DUE TO STEPPED TILES IN THE

SHUTTLE THERMAL PROTECTION SYSTEM

D. H. PETLEY, D. M. SMITH, C. L. W. EDWARDS, and A. B.

CARLSON Aug. 1983 100 p refs

(NASA-TP-2209; L-15636; NAS 1.60:2209) Avail: NTIS HC

A05/MF A01 CSCL 22B

CERAMICS, CHANNEL FLOW, CORRELATION, GAPS,

INCOMPRESSIBLE FLOW, SPACE SHUTTLE ORBITERS

N84-16247"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

RADIATING DIPOLE MODEL OF INTERFERENCE INDUCED IN

SPACECRAFT CIRCUITRY BY SURFACE DISCHARGES

R. N. METZ (Colby College) Jan. 1984 7 p refs

(NASA-TP-2240; E-1775; NAS 1.60:2240) Avail: NTIS HC

A02/MF A01 CSCL 22B

COUPLING, ELECTRIC DIPOLES, ELECTRIC FIELDS, HIGH

VOLTAGES, SPACE PLASMAS, SPACECRAFT CHARGING

N84-19393"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

STEADY INTERNAL FLOW AND AERODYNAMIC LOADS

ANALYSIS OF SHUTTLE THERMAL PROTECTION SYSTEM

D. H. PETLEY, W. ALEXANDER, JR., G. W. IVEY, JR., and P. A.

KERR Mar. 1984 68 p refs

(NASA-TP-2255; L-15695; NAS 1.60:2255) Avail: NTIS HC

A04/MF A01 CSCL 22B

SPACE SHUTTLES, STEADY FLOW, THERMAL

PROTECTION

N84-23675"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

DECOUPLED CONTROL ANALYSIS OF A LARGE FLEXIBLE

SPACE ANTENNA WITH LINEAR QUADRATIC REGULATOR

COMPARISONS

J. W. YOUNG, H. A. HAMER, and K. G. JOHNSON May 1984

82 p

(NASA-TP-2293; L-15696; NAS 1.60:2293) Avail: NTIS HC

A05/MF A01 CSCL 22B

DECOUPLING, FEEDBACK CONTROL, FLEXIBILITY, LARGE

SPACE STRUCTURES, OPTIMAL CONTROL, ROTATION,

SPACECRAFT ANTENNAS, THREE AXIS STABILIZATION,

TRANSLATIONAL MOTION

N84-23676"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

SHOCK RESPONSE SPECTRA VARIATIONAL ANALYSIS FOR

PYROTECHNIC QUALIFICATION TESTING OF FLIGHT

HARDWARE

J. L. SMITH May 1984 15 p refs

(NASA-TP-2315; NAS 1.60:2315) Avail: NTIS HC A02/MF A01

CSCL 22B

ELECTRONIC EQUIPMENT, FLIGHT INSTRUMENTS, LOADS

(FORCES), PYROTECHNICS, SHOCK SPECTRA, SHOCK TESTS

N84-23677"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

AUTOMATED RENDEZVOUS AND DOCKING: A PARAMETRIC

STUDY

R. DABNEY May 1984 34 p refs

(NASA-TP-2314; NAS 1.60:2314) Avail: NTIS HC A03/MF A01

CSCL 22B

APPROACH CONTROL, COMPUTERIZED SIMULATION,

GUIDANCE (MOTION), IMAGE PROCESSING, PERFORMANCE

PREDICTION, SPACECRAFT DOCKING, VISUAL CONTROL

N84-33452"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

DESIGN GUIDELINES FOR ASSESSING AND CONTROLLING

SPACECRAFT CHARGING EFFECTS

C. K. PURVIS, H. B. GARRETT (JPL), A. C. WHITTLESEY (JPL),

and N. J. STEVENS (Hughes Aircraft Co., El Segundo, Calif.) Sep.

1984 48p refs

(NASA-TP-2361; E-2073; NAS 1.60:2361) Avail: NTIS HC

A03/MF A01 CSCL 22B

ELECTROMAGNETIC COMPATIBILITY, ELECTROMAGNETIC

PULSES, GEOSYNCHRONOUS ORBITS, SPACECRAFT

CHARGING, SPACECRAFT DESIGN

N84-34468"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

THIRTEENTH SPACE SIMULATION CONFERENCE. THE

PAYLOAD: TESTING FOR SUCCESS

J. STECHER, ed. Washington 1984 283 p refs Conf. held

in Orlando, Fla., 8-11 Oct. 1984 Sponsored in cooperation with

Inst. of Environmental Sciences, AIAA, and the American Society

for Testing and Materials

(NASA-CP-2340; NAS 1.55:2340) Avail: NTIS HC A13/MF A01

CSCL 22A

COMPUTERIZED SIMULATION, CONTAMINATION, DYNAMIC

CONTROL, DYNAMIC TESTS, SPACE SIMULATORS, SYSTEMS

SIMULATION, THERMAL ENVIRONMENTS

N85-11127"# National Aeronautics and Space Administration.

Lyndon B. Johnson Space Center, Houston, Tex.

SPACE SHUTTLE WIND TUNNEL TESTING PROGRAM

A. M. WHITNAH and E. R. HILLJE Nov. 1984 492 p refs

(NASA-RP-1125; S-535; NAS 1.61:1125) Avail: NTIS HC

A21/MF A01 CSCL 22B

A major phase of the Space Shuttle Vehicle (SSV) Development

Program was the acquisition of data through the space shuttle

wind tunnel testing program. It became obvious that the large

number of configuration/environment combinations would

74
necessitate an extremely large wind tunnel testing program. To

make the most efficient use of available test facilities and to assist

the prime contractor for orbiter design and space shuttle vehicle

integration, a unique management plan was devised for the design

and development phase. The space shuttle program is reviewed

together with the evolutional development of the shuttle

configuration. The wind tunnel testing rationale and the associated

test program management plan and its overall results is reviewed.

Information is given for the various facilities and models used

within this program. A unique posttest documentation procedure

and a summary of the types of test per disciplines, per facility,

and per model are presented with detailed listing of the posttest

documentation. E.A.K.

N85-14858"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

CIRCUIT TRANSIENTS DUE TO NEGATIVE BIAS ARCS ON A

HIGH-VOLTAGE SOLAR ARRAY IN LOW EARTH ORBIT

R. N. METZ (Colby Coil., Waterville, Maine) Jan. 1985 12 p

refs

(NASA-TP-2407; E-2239; NAS 1.60:2407) Avail: NTIS HC

A02/MF A01 CSCL 22B

AURORAL ARCS, BIAS, CIRCUIT PROTECTION, HIGH

VOLTAGES, NEGATIVE CONDUCTANCE, SOLAR ARRAYS,

SURGES

N85-19015"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SWING-ARM BEAM ERECTOR (SABER) CONCEPT FOR SINGLE

ASTRONAUT ASSEMBLY OF SPACE STRUCTURE

J. J. WATSON, W. L. HEARD, JR., and J. K. JENSEN (Kentron

International, Inc.) Mar. 1985 32 p refs

(NASA-TP-2379; L-15886; NAS 1.60:2379) Avail: NTIS HC

A03/MF A01 CSCL 22B

BEAMS (SUPPORTS), EXTRAVEHICULAR MOBILITY UNITS,

LARGE SPACE STRUCTURES, MECHANICAL DEVICES,

ORBITAL ASSEMBLY

N85-22470"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

SPACECRAFT ENVIRONMENTAL INTERACTIONS TECHNOLOGY, 1983

Washington Mar. 1985 673 p refs Conf. held in Colorado

Springs, 4-6 Oct. 1983 Prepared in cooperation with AFGL,

Hanscom AFB, Mass.

(NASA-CP-2359; E-2186; NAS 1.55:2359; AFGL-TR-85-0018)

Avail: NTIS HC A99/MF E03 CSCL 22B

CONFERENCES, EARTH ORBITS, ELECTRODYNAMICS,

HIGH VOLTAGES, PLASMA INTERACTIONS, SPACE SHUTTLES,

SPACECRAFT CHARGING

N85-31141"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

RECOVERY OF PYROSHOCK DATA FROM DISTORTED

ACCELERATION RECORDS

J. L. SMITH Washington Jul. 1985 20 p

(NASA-TP-2494; NAS 1.60:2494) Avail: NTIS HC A02/MF A01

CSCL 22B

ACCELERATION (PHYSICS), HIGH FREQUENCIES,

MECHANICAL SHOCK, SHOCK SPECTRA, SIGNAL

DISTORTION

N85-31142"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ADAPTIVE IDENTIFICATION AND CONTROL OF STRUCTURAL

DYNAMICS SYSTEMS USING RECURSIVE LATTICE FILTERS

N. SUNDARARAJAN (Indian Space Research Organization), R. C.

MONTGOMERY, and J. P. WILLIAMS Jan. 1985 51 p refs

(NASA-TP-2371; L-15737; NAS 1.60:2371) Avail: NTIS HC

A04/MF A01 CSCL 22B

ADAPTIVE CONTROL, DYNAMIC STRUCTURAL ANALYSIS,

LATTICES (MATHEMATICS), LEAST SQUARES METHOD,

SIGNAL PROCESSING

19 SPACECRAFT INSTRUMENTATION

N86-16250"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

DECOUPLED AND LINEAR QUADRATIC REGULATOR

CONTROL OF A LARGE, FLEXIBLE SPACE ANTENNA WITH

AN OBSERVER IN THE CONTROL LOOP

H. A. HAMER, K. G. JOHNSON, and J. W. YOUNG Nov. 1985

74 p refs

(NASA-TP-2484; L-15913; NAS 1.60:2484) Avail: NTIS HC

A04/MF A01 CSCL 22B

ANTENNAS, CONTROL MOMENT GYROSCOPES,

DECOUPLING, LARGE SPACE STRUCTURES, LINEARITY,

QUADRATIC EQUATIONS, RIGID STRUCTURES

N86-30800"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

APPLICATION OF THE LQG/LTR TECHNIQUE TO ROBUST

CONTROLLER SYNTHESIS FOR A LARGE FLEXIBLE SPACE

ANTENNA

S. M. JOSHI, E. S. ARMSTRONG, and N. SUNDARARAJAN (Old

Dominion Univ., Norfolk, Va.) Sep. 1986 64 p

(NASA-TP-2560; L-16076; NAS 1.60:2560) Avail: NTIS HC

A04/MF A01 CSCL 22B

ANTENNAS, FLEXIBLE SPACECRAFT, HOOP COLUMN

ANTENNAS, LARGE SPACE STRUCTURES, SPACECRAFT

CONTROL

N86-30801"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECTS OF MODEL ERROR ON CONTROL OF LARGE

FLEXIBLE SPACE ANTENNA WITH COMPARISONS OF

DECOUPLED AND LINEAR QUADRATIC REGULATOR

CONTROL PROCEDURES

H. A. HAMER and K. G. JOHNSON Sep. 1986 52 p

(NASA-TP-2604; L-16114; NAS 1.60:2604) Avail: NTIS HC

A04/MF A01 CSCL 22B

ANTENNAS, CONTROL MOMENT GYROSCOPES, CONTROL

SYSTEMS DESIGN, ERRORS, FLEXIBLE BODIES, HOOP

COLUMN ANTENNAS, LARGE SPACE STRUCTURES,

MATHEMATICAL MODELS, VIBRATION DAMPING

19

SPACECRAFT INSTRUMENTATION

N78-17145"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

DESIGN AND FABRICATION OF A LOW-SPECIFIC-WEIGHT

PARABOLIC DISH SOLAR CONCENTRATOR

C. W. RICHTER, A. G. BIRCHENOUGH, G. A. MARQUIS, and T.

S. MROZ Jan. 1978 18 p refs

(NASA-TP-1152; E-9339) Avail: NTIS HC A02/MF A01 CSCL

10A

CONCENTRATORS, FABRICATION, PARABOLIC REFLECTORS, SOLAR REFLECTORS

N80-13152"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

FLIGHT TECHNOLOGY IMPROVEMENT

Dec. 1979 76 p Proceedings of workshop held at College

Park, Md., 31 Jul. - 2 Aug. 1979

(NASA-CP-2101; L-13259) Avail: NTIS HC A05/MF A01

CSCL 22B

CONFERENCES, ELECTROMECHANtCAL DEVICES,

RADIOMETERS, SATELLITE ATTITUDE CONTROL,

SPACECRAFT INSTRUMENTS, SPACECRAFT POWER

SUPPLIES

75
19 SPACECRAFT INSTRUMENTATION

N80-28424"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

THE TIME-SPACE RELATIONSHIP OF THE DATA POINT

(PIXELS) OF THE THEMATIC MAPPER AND MULTISPECTRAL

SCANNER OR THE MYTH OF SIMULTANEITY

F. GORDON, JR. Jul. 1980 29 p refs

(NASA-TP-1715; REPT-80F5121) Avail: NTIS HC A03/MF A01

CSCL 14B

DATA PROCESSING, IMAGING TECHNIQUES, MULTISPECTRAL BAND SCANNERS, SATELLITE OBSERVATION, SPACETIME FUNCTIONS, THEMATIC MAPPING

N80-33463"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

HIGH SPEED LOOKUP TABLE APPROACH TO RADIOMETRIC

CALIBRATION OF MULTISPECTRAL IMAGE DATA

W. L. KELLY, IV, B D. MEREDITH, and W. M. HOWLE

Washington Oct. 1980 16 p

(NASA-TP-1741; L-13893) Avail: NTIS HC A02/MF A01

CSCL 14B

DATA PROCESSING, IMAGE PROCESSING, MICROPROCESSORS, MULTISPECTRAL PHOTOGRAPHY, ONBOARD DATA

PROCESSING, RADIOMETERS

N81-16119"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

SPACECRAFT TRANSMITTER RELIABILITY

1980 18 p refs Synopsis of Workshop, held in Cleveland,

25-26 Sep. 1979; sponsored by NASA and Air Force

(NASA-CP-2159; E-662) Avail: NTIS HC A06/MF A01 CSCL

t7B

CATHODES, EQUIPMENT SPECIFICATIONS, QUALITY

CONTROL, TRANSMITTERS, TRAVELING WAVE TUBES

N81-31281"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

PROTON-INDUCED NOISE IN DIGICONS

L. C. SMITH (Old Dominion Univ., Norfolk, Va.), J. BECHER (Old

Dominion Univ., Norfolk, Va.), W. B. FOWLER, and K. FLEMMING

Aug. 1981 33 p refs

(NASA-TP-1852; REPT-81F0051) Avail: NTIS HC A03/MF A01

CSCL 09F

NOISE SPECTRA, PROTON IRRADIATION, RADIATION

BELTS, REMOTE SENSING, TELESCOPES

N81-31282"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

DEVELOPMENT AND DESIGN OF THREE MONITORING

INSTRUMENTS FOR SPACECRAFT CHARGING

J. C. STURMAN Sep. 1981 28 p refs

(NASA-TP-1800; E-603) Avail: NTIS HC A03/MF A01 CSCL

22B

ELECTROSTATIC PROBES, MAGNETIC STORMS, POTENTIOMETERS (INSTRUMENTS), SPACECRAFT CHARGING, SYSTEM GENERATED ELECTROMAGNETIC PULSES

N83-15348"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

ADVANCED AUTOMATION FOR SPACE MISSIONS Final

Report

R A. FREITAS, JR., ed. (Santa Clara Univ.) and W. P. GILBREATH,

ed. Nov. 1982 392 p refs Meeting held in Santa Clara,

Calif., 23 Jun. - 29 Aug. 1980; sponsored in cooperation with Am.

Soc. for Eng. Education Original contains color illustrations

(NASA-CP-2255; A-8618; NAS 1.55:2256) Avail: NTIS HC

A17/MF A01 CSCL 22B

ARTIFICIAL INTELLIGENCE, AUTOMATIC CONTROL,

CONFERENCES, ROBOTS, SPACE EXPLORATION, SPACE

MANUFACTURING, SPACE MISSIONS

76

N85-30005"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

SUBMILLIMETER LOCAL OSCILLATORS FOR SPACEBORNE

HETERODYNE APPLICATIONS

S. J. PETUCHOWSKI and J. DURACHTA Washington Jun.

1985 63 p refs Prepared in cooperation with Maryland Univ.,

College Park

(NASA-RP-1147; NAS 1.61:1147; REPT-85B0310) Avail: NTIS

HC A04/MF A01 CSCL 09A

Existing and prospective submillimeter local oscillator

technologies are surveyed and compared with respect to criteria

of suitability for application in spaceborne submillimeter heterodyne

receivers as those proposed for the Large Deployable Reflector

(LDR). Solid-state and plasma devices are considered in terms of

fundamental limitations. Author

N86-19349"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

SOLAR TERRESTRIAL OBSERVATORY SPACE STATION

WORKSHOP REPORT

W. T. ROBERTS, ed. Washington Jan. 1986 41 p refs

Workshop held in Huntsville, Ala., 6 Jun. 1985

(NASA-CP-2411; M-505; NAS 1.55:2411) Avail: NTIS HC

AO3/MF A01 CSCL 14B

CONFERENCES, ORBITAL SERVICING, SOLAR

OBSERVATORIES, SOLAR PHYSICS, SOLAR TERRESTRIAL

INTERACTIONS, SPACE PLATFORMS, SPACE STATIONS,

SPACECRAFT INSTRUMENTS

20

SPACECRAFT PROPULSION AND POWER

Includes main propulsion systems and components, e.g., rocket

engines; and spacecraft auxiliary power sources.

N77-32229*# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

THE ATS-6 POWER SYSTEM: HARDWARE IMPLEMENTATION

AND ORBITAL PERFORMANCE

T. A. LAVIGNA and F. L. HORNBUCKLE Sep. 1977 49 p

refs

(NASA-TP-1023; G-7703-X10) Avail: NTIS HC A03/MF A01

CSCL 100

ATS 6, SPACECRAFT POWER SUPPLIES

N78-13124"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

HYDROGEN FILM COOLING OF A SMALL HYDROGEN-OXYGEN

THRUST CHAMBER AND ITS EFFECT ON EROSION RATES

OF VARIOUS ABLATIVE MATERIALS

N. HANNUM, W. E. ROBERTS, and L. M. RUSSELL Dec. 1977

27 p refs

(NASA-TP-1098; E-8909) Avail: NTIS HC A03/MF A01 CSCL

21H

ABLATIVE MATERIALS, EROSION, FILM COOLING,

HYDROGEN OXYGEN ENGINES, THRUST CHAMBERS

N79-10122"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

FUTURE ORBITAL POWER SYSTEMS TECHNOLOGY

REQUIREMENTS

Sep. 1978 195 p refs Symp. held at Cleveland, 31 May - 1

Jun. 1978

(NASA-CP-2058; E-9713) Avail: NTIS HC A09/MF A01 CSCL

10A

CONFERENCES, ELECTRIC GENERATORS, SPACECRAFT

POWER SUPPLIES, TECHNOLOGY ASSESSMENT
N79-23132"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EFFECT OF LOW-STIFFNESS CLOSEOUT OVERWRAP ON

ROCKET THRUST-CHAMBER LIFE

H. J. KASPER and J. J. NOTA-DONATO May 1979 33 p

refs

(NASA-TP-1456; E-9870) Avail: NTIS HC A03/MF A01 CSCL

21H

COMPOSITE WRAPPING, COPPER, FATIGUE LIFE, ROCKET

LININGS, THRUST CHAMBERS

N80-16095"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

SEALED-CELL NICKEL-CADMIUM BATTERY APPLICATIONS

MANUAL

W. R. SCOTT and D. W. RUSTA Dec. 1979 533 p refs

(NAS5-23514)

(NASA-RP-1052) Avail: NTIS HC A23/MF A01 CSCL 10B

The design, procurement, testing, and application of aerospace

quality, hermetically sealed nickel-cadmium cells and batteries are

presented. Cell technology, cell and battery development, and

spacecraft applications are emphasized. Long term performance

is discussed in terms of the effect of initial design, process, and

application variables. Design guidelines and practices are given.

MG.

N80-31449"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

LARGE SPACE SYSTEMS/LOW-THRUST PROPULSION

TECHNOLOGY

Jul. 1980 347 p refs Meeting held at Cleveland, 20-21 May

1980

(NASA-CP-2144; E-510) Avail: NTIS HC A15/MF A01 CSCL

21H

CONFERENCES, LARGE SPACE STRUCTURES, LOW

THRUST PROPULSION, PROULSION SYSTEM CONFIGURATIONS, SPACE TRANSPORTATION SYSTEM, SPACECRAFT

PROPULSION

N80-33465"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

SYNCHRONOUS ENERGY TECHNOLOGY

Sep. 1980 144 p Symp. held in Cleveland, 29-30 Apr. 1980

(NASA-CP-2154; E-469) Avail: NTIS HC A07/MF A01 CSCL

21H

CONFERENCES, GEOSYNCHRONOUS ORBITS, POWER

EFFICIENCY, SPACECRAFT POWER SUPPLIES

N81-20173"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

ANALYSIS OF COSTS OF GALLIUM ARSENIDE AND SILICON

SOLAR ARRAYS FOR SPACE POWER APPLICATIONS

K. S. JEFFERIES Mar. 1981 16 p refs

(NASA-TP-1811; E-536) Avail: NTIS HC A02/MF A01 CSCL

10A

COST ANALYSIS, EARTH ORBITS, ELECTRIC PROPULSION,

GALLIUM ARSENIDES, SATELLITE SOLAR ENERGY

CONVERSION, SILICON, SOLAR CELLS

N81-20176"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

SOME EFFECTS OF THERMAL-CYCLE-INDUCED DEFORMATION IN ROCKET THRUST CHAMBERS

N. P. HANNUM and R. G. PRICE, JR. Apr. 1981 24 p refs

(NASA-TP-1834; E-553) Avail: NTIS HC A02/MF A01 CSCL

21H

DEFORMATION, FAILURE ANALYSIS, THERMAL FATIGUE,

THRUST CHAMBERS

20 SPACECRAFT PROPULSION AND POWER

N81-24167"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

LIFE TEST OF A NICKEL CADMIUM BATTERY WITH A

PROTECTION/RECONDITIONING CIRCUIT

J. R. LANIER, JR. and J. R. BUSH, JR. May 1981 19 p refs

(NASA-TP-1873; M-350) Avail: NTIS HC A02/MF A01 CSCL

10C

EARTH ORBITS, ELECTRIC DISCHARGES, LIFE CYCLE

COSTS, NICKEL CADMIUM BATTERIES

N81-33231"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala. Structures and

Propulsion Lab.

FEASIBILITY STUDY OF LITVC FOR SHUTTLE SRB

C. L. MARTIN and L. B. POWERS Sep. 1981 19 p refs

(NASA-TP-1912; M-354) Avail: NTIS HC A02/MF A01 CSCL

21H

BOOSTER ROCKET ENGINES, INJECTORS, LIQUID

INJECTION, SPACE SHUTTLE BOOSTERS, THRUST VECTOR

CONTROL

N82-11109"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

CONCEPT FOR A POWER SYSTEM CONTROLLER FOR LARGE

SPACE ELECTRICAL POWER SYSTEMS

L. F. LOLLAR, J. R. LANIER, JR., and J. R. GRAVES Nov.

1981 15p refs

(NASA-TP-1939) Avail: NTIS HC A02/MF A01 CSCL 22B

AUTOMATIC CONTROL, CENTRAL PROCESSING UNITS,

ELECTRIC NETWORKS, NETWORK CONTROL, POWER

MODULES (STS)

N82-21254"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

SPACE POWER SUBSYSTEM AUTOMATION TECHNOLOGY

J. R. GRAVES, comp. Mar. 1982 219 p Proc. of a

Conf./Workshop held at Marshall Space Flight Center, Ala., 28-29

Oct. 1981

(NASA-CP-2213; M-371; NAS 1.55:2213) Avail: NTIS HC

A10/MF A01 CSCL 22B

AUTOMATIC CONTROL, CONFERENCES, ELECTRIC POWER

SUPPLIES, SPACECRAFT POWER SUPPLIES

N83-24549"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

PERFECT BELL NOZZLE PARAMETRIC AND OPTIMIZATION

CURVES

J. L. TUTTLE and D. H. BLOUNT May 1983 32 p refs

(NASA-RP-1104; NAS 1.61:1104) Avail: NTIS HC A03/MF A01

CSCL 21H

Nozzle contour data for untruncated Bell nozzles with expansion

area ratios to 6100 and a specific heat ratio of 1.2 are provided.

Curves for optimization of nozzles for maximum thrust coefficient

within a given length, surface area, or area ratio are included.

The nozzles are two dimensional axisymmetric and calculations

were performed using the method of characteristics. Drag due to

wall friction was included in the final thrust coefficient. Author

N84-12228"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

INTEGRATED FLYWHEEL TECHNOLOGY, 1983

C. R. KECKLER, ed., G. E. RODRIGUEZ, ed. (NASA. Goddard

Space Flight Center), and N. J. GROOM, ed. Washington Dec.

1983 205 p refs Workshop held in Greenbelt, Md, 2-3 Aug.

1983

(NASA-CP-2290; L-t5707; NAS 1.55:2290) Avail: NTIS HC

A10/MF A01 CSCL 10C

ATTITUDE CONTROL, CONFERENCES, FLYWHEELS, SPACE

STATIONS, SYSTEMS INTEGRATION

77
20 SPACECRAFT PROPULSION AND POWER

N85-13850"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AN ASSESSMENT OF INTEGRATED FLYWHEEL SYSTEM

TECHNOLOGY

C. R. KECKLER, ed., R. T. BECHTEL, ed. (NASA. Marshall Space

Flight Center), and N J. GROOM, ed. Washington Nov. 1984

419 p refs Workshop held in Huntsville, Ala., 7-9 Feb. 1984

(NASA-CP-2346; L-15876; NAS 1.55:2346) Avail: NTIS HC

A18/MFA01 CSCL 10B

ATTITUDE CONTROL, CONFERENCES, ENERGY STORAGE,

FLYWHEELS, INTEGRATED ENERGY SYSTEMS, POWER

CONDITIONING

N85-13880"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

SPACE POWER

Washington Apr. 1984 322 p refs Workshop held in

Cleveland, 10-12 Apr. 1984

(NASA-CP-2352; E-2305; NAS 155:2352) Avail: NTIS HC

At4/MFA01 CSCL22B

CONFERENCES, SPACE STATIONS, SPACECRAFT POWER

SUPPLIES

N85-21263"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

HIGH-VOLTAGE, HIGH-POWER, SOLID-STATE REMOTE

POWER CONTROLLERS FOR AEROSPACE APPLICATIONS

J. C. STURMAN Mar. 1985 34 p refs

(NASA-TP-2437; E-2359; NAS 1.60:2437) Avail: NTIS HC

A03/MF A01 CSCL 10B

CIRCUIT BREAKERS, ELECTRIC SWITCHES, FIELD EFFECT

TRANSISTORS, POWER SUPPLY CIRCUITS, SPACECRAFT

EQUIPMENT, THYRISTORS

N85-26862'# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

ADVANCED HIGH PRESSURE O2/H2 TECHNOLOGY

S. F. MOREA, ed. and S. T. WU, ed. (Alabama Univ., Huntsville)

Washington Apr. 1985 753 p refs Conf. held in Huntsville,

Ala., 27-29 Jun. 1984

(NASA-CP-2372; NAS 1.55:2372) Avail: NTIS HC A99/MF E03;

SOD HC CSCL 21H

COMBUSTION CHAMBERS, CONFERENCES, ENGINE

MONITORING INSTRUMENTS, ENGINE PARTS, HYDROGEN

OXYGEN ENGINES, SPACE SHUTTLE MAIN ENGINE, TURBINE

BLADES, TURBINE PUMPS

N85-27941"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

STRUCTURAL INTEGRITY AND DURABILITY OF REUSABLE

SPACE PROPULSION SYSTEMS

Washington May 1985 191 p refs Conf. held in Cleveland,

Ohio, 4-5 Jun. 1985; sponsored by NASA, Washington and NASA.

Lewis Research Center

(NASA-CP-2381; E-2554; NAS 1.55:2381) Avail: NTIS HC

A09/MF A01 CSCL 21H

AEROTHERMODYNAMICS, CONFERENCES, FATIGUE

(MATERIALS), FRACTURING, LOADS (FORCES),

NONDESTRUCTIVE TESTS, REUSABLE ROCKET ENGINES,

SPACE SHUTTLE MAIN ENGINE, SPACECRAFT PROPULSION

N86-21577"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

TECHNOLOGY FOR BAYTON-CYCLE POWERPLANTS USING

SOLAR AND NUCLEAR ENERGY

R. E. ENGLISH Feb. 1986 15 p refs

(NASA-TP-2558; E-2761; NAS 160:2556) Avail: NTIS HC

A02/MF A01 CSCL 10B

BRAYTON CYCLE, ELECTRIC GENERATORS, GAS TURBINE

ENGINES, NUCLEAR PROPULSION, SOLAR ENERGY

78

N86-28123"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

RAIL ACCELERATORS FOR SPACE TRANSPORTATION: AN

EXPERIMENTAL INVESTIGATION

L M. ZANA, W. R. KERSLAKE, and J. L. STURMAN May 1986

37 p

(NASA-TP-2571; E-2754; NAS 1.60:2571) Avail: NTIS HC

A03/MF A01 CSCL 09C

ELECTROMAGNETIC ACCELERATION, HYPERVELOCITY

LAUNCHERS, PLASMA PROPULSION, PROPULSION SYSTEM

CONFIGURATIONS, RAILGUN ACCELERATORS, SPACE

TRANSPORTATION

N86-28124"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

CURRENT EVALUATION OF THE TRIPROPELLANT CONCEPT

R. L. ZURAWSKI Jun. 1986 30 p Presented at the

AIAA/SAI/ASME/ASEE 22nd Joint Propulsion Conference,

Huntsville, Ala., 16-18 Jun. 1986

(NASA-TP-2602; E-2863; NAS 1.60:2602) Avail: NTIS HC

A03/MF A0t CSCL 211

ADDITIVES, HIGH ENERGY PROPELLANTS, LIQUID ROCKET

PROPELLANTS, METAL PROPELLANTS, METALS, SPECIFIC

IMPULSE

23

CHEMISTRY AND MATERIALS (GENERAL)

N78-21216"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

FORMULATION OF ELECTRICALLY CONDUCTIVE

THERMAL-CONTROL COATINGS

M.C. SHAI Apr. 1978 19p refs

(NASA-TP-1218; G-97802-F9) Avail: NTIS HC A02/MF A01

CSCL 11D

ALUMINUM OXIDES, ELECTRIC CONDUCTORS, PIGMENTS,

THERMAL CONTROL COATINGS, ZINC OXIDES

N79-21128"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

THREE METHODS FOR IN SlTU CROSS-LINKING OF

POLYVlNYL ALCOHOL FILMS FOR APPLICATION AS

ION-CONDUCTING MEMBRANES IN POTASSIUM HYDROXIDE

ELECTROLYTE

W. H. PHILIPPand L. C. HSU Apr. 1979 18p refs

(NASA-TP-1407; E-9778) Avail: NTIS HC A02/MF A01 CSCL

07D

CROSSLINKING, ION EXCHANGE MEMBRANE

ELECTROLYTES, POLYMERIC FILMS, POLYVINYL ALCOHOL,

POTASSIUM HYDROXIDES, SEPARATORS

N79-22194"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

IMPROVED ADHERENCE OF SPUTTERED TITANIUM CARBIDE

COATINGS ON NICKEL- AND TITANIUM-BASE ALLOYS

D. R. WHEELER and W. A. BRAINARD Apr. 1979 18 p refs

(NASA-TP-t450; E-9838) Avail: NTIS HC A02/MF A01 CSCL

11F

ADHESION, RENE 41, SPUTTERING, SURFACE FINISHING,

TITANIUM ALLOYS, TITANIUM CARBIDES
N79-31346"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

SURFACE CHEMISTRY OF IRON SLIDING IN AIR AND

NITROGEN LUBRICATED WITH HEXADECANE AND

HEXADECANE CONTAINING DIBENZYL-DILSULFIDE

D. R. WHEELER Sap. 1979 15 p refs

(NASA-TP-1545; E-9956) Avail: NTIS HC A02/MF A01 CSCL

11G

FRICTION REDUCTION, IRON, NITROGEN, OXYGEN,

SLIDING FRICTION, SURFACE REACTIONS, WEAR, WEAR

TESTS

N83-12147"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ADVANCED MATERIALS TECHNOLOGY

C. P. BLANKENSHIP, comp. and L. A. TEICHMAN, comp. Nov.

1982 438 p refs Proc. held at Hampton, Va., 16-17 Nov.

1982 Sponsored in cooperation with AIAA

(NASA-CP-2251; L-15537; NAS 1.55:2251) Avail: NTIS HC

A19/MFA01 CSCL 11G

AIRCRAFT CONSTRUCTION MATERIALS, AIRCRAFT

STRUCTURES, ALUMINUM ALLOYS, CONFERENCES, FATIGUE

LIFE, MATRIX MATERIALS, POWDER METALLURGY

N83-24556"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

THE 1ST SYMPOSIUM ON CHEMICAL EVOLUTION AND THE

ORIGIN AND EVOLUTION OF LIFE

D. L. DEVINCENZI, ed. and L. G. PLEASANT, ed, 1982 119 p

Symp. held at Ames Research Center, Calif., 2-4 Aug. 1982

(NASA-CP-2276; NAS 1.55:2276) Avail: NTIS HC A06/MF A01

CSCL 06C

BIOLOGICAL EVOLUTION, CHEMICAL EVOLUTION,

CONFERENCES, EXOBIOLOGY, EXTRATERRESTRIAL LIFE,

GEOLOGY, PLANETARY ENVIRONMENTS, SPACE

EXPLORATION

N84-20643"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

HOMOGENEOUS REACTIONS OF HYDROCARBONS, SILANE,

AND CHLOROSILANES IN RADIOFREQUENCY PLASMAS AT

LOW PRESSURES

R. AVNI, U. CARMI (Nuclear Research Center Negev, Beer Sheva,

Israel), A. INSPEKTOR (Nuclear Research Center Negev, Beer

Sheva, Israel), and I. ROSENTHAL (Nuclear Research Center

Negev, Beer Sheva, Israel) Apr. 1984 13 p refs Presented

at the 6th Intern. Symp. on Plasma Chem., Montreal, 24-28 Jul.

1983; sponsored by International Union of Pure and Applied

Chemistry

(NASA-TP-2301; E-1919; NAS 1.60:2301) Avail: NTIS HC

A02/MF A01 CSCL 07A

DISSOCIATION, HYDROCARBONS, PLASMA JETS, SILANES

N84-26749"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

MICROSTRUCTURE AND ORIENTATION EFFECTS ON PROPERTIES OF DISCONTINUOUS SILICON CARBIDE/ALUMINUM COMPOSITES

D. L. MCDANELS and C. A. HOFFMAN Jul. 1984 32 p refs

(NASA-TP-2302; E-1977; NAS 1.60:2302) Avail: NTIS HC

A03/MF A01 CSCL 11D

ALUMINUM ALLOYS, MECHANICAL PROPERTIES, METAL

MATRIX COMPOSITES, MICROSTRUCTURE, SILICON

CARBIDES, WHISKER COMPOSITES

24 COMPOSITE MATERIALS

N86-11227"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

WELDING, BONDING AND FASTENING, 1984

J. D. BUCKLEY, ed. and B. A. STEIN, ed. Washington Sep.

1985 484 p refs Conf. held in Hampton, Va., 23-25 Oct.

1984; sponsored by NASA, American Society for Metals, George

Washington Univ., American Welding Society, and Society of Mfg.

Engineers

(NASA-CP-2387; L-16023; NAS 1.55:2387) Avail: NTIS HC

A21/MFA01 CSCL 13H

CONFERENCES, FASTENERS, METAL-METAL BONDING,

SOLDERING, WELDING

24

COMPOSITE MATERIALS

Includes physical, chemical, and mechanical properties of laminates

and other composite materials.

N78-11200"# National Bureau of Standards, Boulder, Colo.

CRYOGENIC FOAM INSULATION: ABSTRACTED

PUBLICATIONS

F.R. WILLIAMSON NASA Sap. 1977 171 p refs Sponsored

by NASA

(NASA-RP-1002) Avail: NTIS HC A08/MF A01 CSCL 11D

A group of documents were chosen and abstracted which

contain information on the properties of foam materials and on

the use of foams as thermal insulation at cryogenic temperatures.

The properties include thermal properties, mechanical properties,

and compatibility properties with oxygen and other cryogenic fluids.

Uses of foams include applications as thermal insulation for

spacecraft propellant tanks, and for liquefied natural gas storage

tanks and pipelines. Author

N78-13138"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

MECHANICAL BEHAVIOR AND FRACTURE CHARACTERISTICS

OF OFF-AXIS FIBER COMPOSITES. 1: EXPERIMENTAL INVESTIGATION

J. H. SINCLAIR and C. C. CHAMIS Dec. 1977 36 p refs

(NASA-TP-1081; E-9085) Avail: NTIS HC A03/MF A01 CSCL

11D

COMPOSITE MATERIALS, FRACTURE MECHANICS,

GRAPHITE-EPOXY COMPOSITES

N78-16098"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

MECHANICAL BEHAVIOR AND FRACTURE CHARACTERISTICS

OF OFF-AXIS FIBER COMPOSITES. 2: THEORY AND COMPARISONS

C. C. CHAMIS and J. H. SINCLAIR Jan. 1978 29 p refs

(NASA-TP-1082; E-9269) Avail: NTIS HC A03/MF A01 CSCL

11D

COMPARISON, FRACTURE STRENGTH, GRAPHITE-EPOXY

COMPOSITES, MECHANICAL PROPERTIES

N78-18135"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

TENSILE STRESS-STRAIN BEHAVIOR OF BORON/ALUMINUM

LAMINATES

J. A. SOVA (Joint inst. for Advan. of Flight Sci., Hampton, Va.,)

and C. C. POE, JR. Feb. 1978 65 p refs

(NASA-TP-1117; L-11864) Avail: NTIS HC A04/MF A01

CSCL 11D

ALUMINUM, BORON, STRESS-STRAIN RELATIONSHIPS,

TENSILE STRESS

79
24 COMPOSITE MATERIALS

N78-20256"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECTS OF FABRICATION AND JOINING PROCESSES ON

COMPRESSIVE STRENGTH OF BORON/ALUMINUM AND

BORSlC/ALUMINUM STRUCTURAL PANELS

D. M ROYSTER, H. R. WIANT (Vought Corp., Hampton, Virginia),

and R R. MCWITHEY Apr. 1978 55 p refs

(NASA-TP-1121; L-11728) Avail: NTIS HC A04/MF A01

CSCL 11 D

ALUMINUM, BORON, COMPRESSIVE STRENGTH,

FABRICATION, PANELS

N79-22196"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

CARBON FIBER RISK ANALYSIS

1979 245 p An Ind./Govt. briefing held at Hampton, Va., 31

Oct. 1978 - 1 Nov. 1978

(NASA-CP-2074; L-12723) Avail: NTIS HC All/MF A01

CSCL 11 D

CARBON FIBERS, CONFERENCES, GRAPHITE-EPOXY

COMPOSITES, RISK

N79-23140"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

STRESS-CONCENTRATION FACTORS FOR FINITE

ORTHOTROPIC LAMINATES WITH A CIRCULAR HOLE AND

UNIAXlAL LOADING

C. S. HONG and J. H. CREWS, JR. May 1979 29 p refs

(NASA-TP-1469; L-12744) Avail: NTIS HC A03/MF A01

CSCL 11 D

AXIAL STRAIN, COMPOSITE MATERIALS, ORTHOTROPIC

PLATES, STRESS RATIO

N79-23141"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EXPLORATORY INVESTIGATION OF TWO RESIN-MATRIX

COMPOSITES SUBJECTED TO ARC-TUNNEL HEATING

C. M. PITTMAN and R. D. BROWN May 1979 30 p refs

(NASA-TP-1429; L-t2665) Avail: NTIS HC A03/MF A01

CSCL 11 D

ARC HEATING, GRAPHITE-EPOXY COMPOSITES, SPACE

SHUTTLES, THERMAL DEGRADATION

N79-28234"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

THERMAL-CONDUCTIVITY MEASUREMENTS OF TUNGSTENFIBER-REINFORCED SUPERALLOY COMPOSITES USING A

THERMAL-CONDUCTIVITY COMPARATOR

L. J, WESTFALL and E. A. WINSA Jul. 1979 23 p refs

(NASA-TP-1445; E-9910) Avail: NTIS HC A02/MF A01 CSCL

11D

COMPARATORS, COMPOSITE MATERIALS, HEAT

RESISTANT ALLOYS, REINFORCING FIBERS, THERMAL

CONDUCTIVITY, TUNGSTEN

N79-29241"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

MOISTURE DIFFUSION PARAMETER CHARACTERISTICS FOR

EPOXY COMPOSITES AND NEAT RESINS

E. R. LONG, JR. Aug. 1979 30 p refs

(NASA-TP-1474; L-12629) Avail: NTIS HC A03/MF A01

CSCL 11D

DIFFUSION COEFFICIENT, EPOXY RESINS, GRAPHITEEPOXY COMPOSITES, HYGROSCOPICITY, MOISTURE CONTENT

80

N79-30297"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

GRAPHITE/POLYIMIDE COMPOSITES

H. B. DEXTER, ed. and J. G. DAVIS, JR., ed. Aug. 1979 449

p refs Proc. held at Hampton, Va., 28 Feb. - 1 Mar. 1979

(NASA-CP-2079; L-12953) Avail: NTIS HC A19/MF A01

CSCL 11D

ADHESIVE BONDING, ADHESlVES, CARBON FIBER

REINFORCED PLASTICS, CONFERENCES, POLYIMIDE RESINS,

POLYIMIDES, POLYMER MATRIX COMPOSITES, SPACE

TRANSPORTATION SYSTEM

N79-32277"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ELEVATED-TEMPERATURE APPLICATION OF THE IITRI

COMPRESSION TEST FIXTURE FOR GRAPHITE/POLYIMIDE

FILAMENTARY COMPOSITES

B. B. RAJU, C. J. CAMARDA, and P. A. COOPER Washington

Sep. 1979 48p refs

(NASA-TP-1496; L-12704) Avail: NTIS HC A03/MF A01

CSCL 11D

CARBON FIBER REINFORCED PLASTICS, COMPRESSION

TESTS, HIGH TEMPERATURE TESTS, POLYIMIDES

N80-19193"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ASSESSMENT OF CARBON FIBER ELECTRICAL EFFECTS

Washington Mar. 1980 278 p refs Conf. held in Hampton,

Va., 4-5 Dec. 1979

(NASA-CP-2119; L-13503) Avail: NTIS HC A13/MF A01

CSCL 11D

AIRCRAFT ACCIDENTS, CARBON FIBERS, COMPOSITE

MATERIALS, ELECTRIC EQUIPMENT, FIRES

N80-27428"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

MOISTURE DETERMINATION IN COMPOSITE MATERIALS

USING POSITRON LIFETIME TECHNIQUES

J. J. SINGH, W. R. HOLT, and W. MOCK, JR. Jut. 1980 23 p

refs

(NASA-TP-1681; L-13651) Avail: NTIS HC A02/MF A01

CSCL 11D

COMPOSITE MATERIALS, MOISTURE CONTENT,

POSITRONS

N80-28436"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SELECTED NASA RESEARCH IN COMPOSITE MATERIALS AND

STRUCTURES

1980 237 p refs Presented at the 2d Ind_ Rev. of the NASA

Aircraft Energy Efficiency (ACEE) Composite Programs, Seattle,

11-13 Aug. 1980

(NASA-CP-2142; L-13915) Avail: NTIS HC A15/MF A01

CSCL 11 D

AIRCRAFT CONSTRUCTION MATERIALS, AIRCRAFT

STRUCTURES, CONFERENCES, FIBER COMPOSITES,

GRAPHITE-EPOXY COMPOSITES, POLYMER MATRIX

COMPOSITES

N80-30441"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

OUTGASSING DATA FOR SPACECRAFT MATERIALS

W. A. CAMPBELL, JR., R. S. MARRIOTT, and J. J. PARK Aug.

1980 259 p refs

(NASA-RP-1061; REPT-80-F-7000) Avail: NTIS HC A12/MF

A01 CSCL 11D

A system for determining the mass loss in vacuum and for

collecting the outgassed compounds was developed. Outgassing

data, derived from tests at 398 K (125 degrees C) for 24 hours in

vacuum as per ASTM E 59577, are compiled for numerous

materials for spacecraft use. The data presented are the total

mass loss (TML) and the collected volatile condensable materials
(CVCM). Thevariousmaterialsarecompiledbylikelyusageand

alphabetically. R.K.G.

N81-11115"#National Aeronautics andSpaceAdministration.

LangleyResearchCenter, Hampton, Va.

FRACTURE TOUGHNESS OF BORON/ALUMINUM LAMINATES

WITH VARIOUS PROPORTIONS OF 0 DEG AND PLUS OR

MINUS 45 DEG

C. C. POE, JR. and J. A. SOVA (Joint Inst. for the Advancement

of Flight Sciences, Hampton, Va.) Nov. 1980 39 p refs

(NASA-TP-1707; L-13880) Avail: NTIS HC A03/MF A01

CSCL 11D

ALUMINUM BORON COMPOSITES, AXIAL LOADS, ELASTIC

PROPERTIES, FRACTURE STRENGTH, LAMINATES, TENSILE

STRESS

N81-14001"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECTS OF TEMPERATURE, THERMAL EXPOSURE, AND

FATIGUE ON AN ALUMINA/ALUMINUM COMPOSITE

G.C. OLSEN Dec. 1980 35p refs

(NASA-TP-1795; L-14074) Avail: NTIS HC A03/MF A01

CSCL 11D

ALUMINUM OXIDES, FIBER REINFORCED COMPOSITES,

METAL MATRIX COMPOSITES

N81-16129"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

TESTS OF GRAPHITEIPOLYIMIDE SANDWICH PANELS IN

UNIAXlAL EDGEWISE COMPRESSION

C. J, CAMARDA Dec. 1980 79 p refs

(NASA-TP-1785; L-13998) Avail: NTIS HC A05/MF A01

CSCL 11 D

COMPRESSION LOADS, GRAPHITE-POLYIMIDE COMPOSITES, SANDWICH STRUCTURES

N81-16130"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

MECHANICAL PROPERTY CHARACTERIZATION OF

BORSICIALUMINUM LAMINATES AT ROOM AND ELEVATED

TEMPERATURES

R. R. MCWITHEY and D. M. ROYSTER Dec. 1980 65 p refs

(NASA-TP-1761; L-13763) Avail: NTIS HC A04/MF A01

CSCL 11D

ALUMINUM, BORSIC (TRADENAME), COMPOSITE

MATERIALS, MECHANICAL PROPERTIES

N81-18096"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

RISK TO THE PUBLIC FROM CARBON FIBERS RELEASED IN

CIVIL AIRCRAFT ACCIDENTS

1980 71 p refs

(NASA-SP-448) Avail: NTIS HC A04/MF A01 CSCL 11D

Because carbon fibers are strong, stiff, and lightweight, they

are attractive for use in composite structures. Because they also

have high electrical conductivity, free carbon fibers settling on

electrical conductors can cause malfunctions. If released from the

composite by burning, the fibers may become a hazard to exposed

electrical and electronic equipment. As part of a Federal study of

the potential hazard associated with the use of carbon fibers,

NASA assessed the public risk associated with crash fire accidents

of civil aircraft. The NASA study projected a dramatic increase in

the use of carbon composites in civil aircraft and developed

technical data to support the risk assessment. Personal injury was

found to be extremely unlikely. In 1993, the year chosen as a

focus for the study, the expected annual cost of damage caused

by released carbon fibers is only $1000. Even the worst-case

carbon fiber incident simulated (costing $178,000 once in 34,000

years) was relatively low-cost compared with the usual air transport

accident cost. On the basis of these observations, the NASA study

concluded that exploitation of composites should continue, that

additional protection of avionics is unnecessary, and that

24 COMPOSITE MATERIALS

development of alternate materials specifically to overcome this

problem is not justified. Author

N81-24178"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

STRESS-CONCENTRATION FACTORS FOR FINITE

ORTHOTROPIC LAMINATES WITH A PIN-LOADED HOLE

J. H. CREWS, JR., C. S. HONG (Korea Inst. of Science, Seoul),

and I. S. RAJU (George Washington Univ., Hampton, Va.) May

1981 43 p refs

(NASA-TP-1862) Avail: NTIS HC AO3/MF A01 CSCL 11D

FINITE ELEMENT METHOD, LAMINATES, ORTHOTROPISM,

STRESS INTENSITY FACTORS

N81-24179"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECTS OF STATIC TENSILE LOAD ON THE THERMAL

EXPANSION OF GR/PI COMPOSITE MATERIAL

G. L. FARLEY Jun. 1981 35 p refs Prepared in cooperation

with Army Aviation Research and Development Command,

Hampton, Va.

(DA PROJ. 1L1-61102-AH-45)

(NASA-TP-1867; AVRADCOM-TR-81-B-2; L-14012) Avail: NTIS

HCA03/MFA01 CSCL 11D

GRAPHITE-POLYIMIDE COMPOSITES, STATIC LOADS,

TENSILE STRESS, THERMAL EXPANSION

N82-22317"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

LONG-TERM THERMAL DEGRADATION AND ALLOYING

CONSTITUENT EFFECTS ON FIVE BORON/ALUMINUM

COMPOSITES

G. C. OLSEN Apr. 1982 107 p refs

(NASA-TP-1977; L14779; NAS 1.60:1977) Avail: NTIS HC

A06/MF A01 CSCL 11D

ALUMINUM BORON COMPOSITES, BORON REINFORCED

MATERIALS, METAL MATRIX COMPOSITES, THERMAL

DEGRADATION, THERMAL FATIGUE, THERMAL STABILITY

N82-25325"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EXPERIMENTAL DATA ON SINGLE-BOLT JOINTS IN QUASI

ISOTROPIC GRAPHITEIPOLYIMIDE LAMINATES

G. R. WICHOREK May 1982 45 p refs

(NASA-TP-2015; L-15103; NAS 1.60:2015) Avail: NTIS HC

A03/MF A01 CSCL 11D

BOLTS, FAILURE MODES, GRAPHITE-POLYtMIDE

COMPOSITES, JOINTS (JUNCTIONS), SHEAR STRENGTH,

TENSILE STRENGTH

N82-31451"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

INTERFACE CONTROL AND MECHANICAL PROPERTY

IMPROVEMENTS IN SILICON CARBIDE/TITANIUM

COMPOSITES

W. D. BREWER and J. UNNAM (Virginia Polytechnic Inst. and

State Univ.) Aug. 1982 22 p refs

(NASA-TP-2066; L-15381; NAS 1.60:2066) Avail: NTIS HC

A02/MF A01 CSCL 11D

DEGRADATION, FIBER REINFORCED COMPOSITES, MATRIX

MATERIALS, SILICON CARBIDES, TITANIUM

N83-16400"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

IDENTIFICATION AND MANAGEMENT OF FILAMENT-WOUND

CASE STIFFNESS PARAMETERS

V. VERDERAIME and M. RHEINFURTH Jan. 1983 17 p refs

(NASA-TP-2117; NAS 1.60:2117) Avail: NTIS HC A02/MF A01

CSCL 11 D

FILAMENT WINDING, HOUSINGS, SOLID PROPELLANT

ROCKET ENGINES, SPACE SHUTTLES

81
24 COMPOSITE MATERIALS

N83-24561"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

BUCKLING AND FAILURE CHARACTERISTICS OF

GRAPHITE-POLYIMIDE SHEAR PANELS

M. J. SHUART and J. A. HAGAMAN May 1983 24 p refs

(NASA-TP-2153; L-15557; NAS 1.60:2153) Avail: NTIS HC

A02/MF A01 CSCL 11D

BUCKLING, FAILURE MODES, GRAPHITE-POLYIMIDE

COMPOSITES, PANELS, STRESS-STRAIN RELATIONSHIPS,

TEMPERATURE EFFECTS, THERMAL EXPANSION

N83-24562"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

FAILURE MECHANICS IN LOW-VELOCITY IMPACTS ON THIN

COMPOSITE PLATES

W. ELBER May 1983 26 p refs

(NASA-TP-2152; L-15588; NAS 1.60:2152) Avail: NTIS HC

A03/MF A01 CSCL 11D

EPOXY RESINS, FAILURE ANALYSIS, IMPACT TESTS, LOW

SPEED, PLATES (STRUCTURAL MEMBERS)

N83-28098'# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

FABRICATION AND EVALUATION OF BRAZED

TITANIUM-CLAD BORSICIALUMINUM SKIN-STRINGER

PANELS

T. T. BALES, D. M. ROYSTER, and R. R. MCWITHEY Jul. 1980

41 p refs

(NASA-TP-1674; L-13413; NAS 1.60:1674) Avail: NTIS HC

A03/MF A01 CSCL 11D

AIRFRAME MATERIALS, BORSIC (TRADENAME), BRAZING,

FABRICATION, HONEYCOMB STRUCTURES, STRINGERS

N83-28099"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

COMPRESSION PANEL STUDIES FOR SUPERSONIC CRUISE

VEHICLES Final Report

R. R. MCWtTHEY, D. M ROYSTER, and W. L. KO Mar. 1980

24 p refs

(NASA-TP-1617; L-13525; NAS 1.60:1617) Avail: NTIS HC

A02/MF A01 CSCL 11D

AIRCRAFT CONSTRUCTION MATERIALS, METAL MATRIX

COMPOSITES, RIGID STRUCTURES, SUPERSONIC CRUISE

AIRCRAFT RESEARCH

N83-28100"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

FABRICATION AND EVALUATION OF BRAZED

TITANIUM-CLAD BORSICIALUMINUM COMPRESSION PANELS

Final Report

D. M. ROYSTER, R. R MCWITHEY, and T. T. BALES Mar.

1980 43 p refs

(NASA-TP-1573; L-13112; NAS 1.60:1573) Avail: NTIS HC

A03/MF A01 CSCL 11D

AIRCRAFT CONSTRUCTION MATERIALS, ALUMINUM

ALLOYS, BORON REINFORCED MATERIALS, METAL MATRIX

COMPOSITES, RIGID STRUCTURES, TITANIUM ALLOYS

N83o31730"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

STANDARD TESTS FOR TOUGHENED RESIN COMPOSITES,

REVISED EDITION

Jul. 1983 38 p refs

(NASA-RP-1092-REV; Lo15317; NAS 1.61:1092-REV) Avail:

NTIS HC A03/MF A01 CSCL 11D

Several toughened resin systems are evaluated to achieve

commonality for certain kinds of tests used to characterize

toughened resin composites. Specifications for five tests were

standardized; these test standards are described. Author

82

N83-33956"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EXPERIMENTAL AND ANALYTICAL INVESTIGATION OF THE

FRACTURE PROCESSES OF BORON/ALUMINUM LAMINATES

CONTAINING NOTCHES

W. S. JOHNSON, C. A. BIGELOW, and Y. A. BAHEI-EL-DIN (Cairo

Univ.) Sep. 1983 44 p refs

(NASA-TP-2187; L-15574; NAS 1.60:2187) Avail: NTIS HC

A03/MF A01 CSCL 11D

ALUMINUM, BORON, FRACTURE MECHANICS, LAMINATES,

METAL MATRIX COMPOSITES

N83-33957"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

FAILURE ANALYSIS AND MECHANISMS OF FAILURE OF

FIBROUS COMPOSITE STRUCTURES

A. K. NOOR, comp. (George Washington Univ.), M. J. SHUART,

comp., J. H. STARNES, JR., comp., and J. G. WILLIAMS, comp.

Aug. 1983 382 p refs Workshop held in Hampton, Va., 23-25

Mar. 1982

(NASA-CP-2278; L-15641; NAS 1.55:2278) Avail: NTIS HC

A17/MF A01 CSCL 11D

AIRCRAFT STRUCTURES, COMPOSITE STRUCTURES,

CONFERENCES, FAILURE ANALYSIS, FIBER COMPOSITES

N84-13224"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

INHYD: COMPUTER CODE FOR INTRAPLY HYBRID

COMPOSITE DESIGN. A USERS MANUAL

C. C. CHAMIS and J. H. SINCLAIR Dec. 1983 41 p refs

(NASA-TP-2239; E-1755; NAS 1.60:2239) Avail: NTIS HC

A03/MFA01 CSCL 11D

COMPOSITE MATERIALS, PLY ORIENTATION, THERMODYNAMICS

N84-23698"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

SOLAR ABSORPTANCE AND THERMAL EMITTANCE OF SOME

COMMON SPACECRAFT THERMAL-CONTROL COATINGS

J. H. HENNINGER Apr. 1984 47 p refs

(NASA-RP-1121; REPT-84F0248; NAS 1.61:1121) Avail: NTIS

HC A03/MF A01 CSCL 11D

Solar absorptance and thermal emittance of spacecraft

materials are critical parameters in determining spacecraft

temperature control. Because thickness, surface preparation,

coatings formulation, manufacturing techniques, etc. affect these

parameters, it is usually necessary to measure the absorptance

and emittance of materials before they are used. Absorptance

and emittance data for many common types of thermal control

coatings, are together with some sample spectral data curves of

absorptance. In some cases for which ultraviolet and particle

radiation data are available, the degraded absorptance and

emittance values are also listed. MA.C.

N84-26751"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

OUTGASSING DATA FOR SELECTING SPACECRAFT

MATERIALS

W. A. CAMPBELL, JR., R. S. MARRIOTT, and J. J. PARK Jun.

1984 280p refs

(NASA-RP-1124; REPT-84B0271; NAS 1.61:1124) Avail: NTIS

HCA13/MF A01 CSCL tld

Outgassing data, derived from tests at 398 K (125 C) for 24

hours in vacuum as per ASTM E 595-77, were compiled for

numerous materials for spacecraft use. The data presented are

the total mass loss (TML) and the collected volatile condensable

materials (CVCM). The various materials are grouped as: adhesives;

cable insulation and shrink tubing; conformat coating; electrical

components; electrical shields; films and sheet materials, foams;

greases and lubricants; lacing tape and cord cable ties; laminates

and circuit boards; marking materials and inks; molding compounds;

paints, lacquers, and varnishes; potting compounds; and rubbers
andelastomers. Thematerials arealsolistedalphabetically. A.R.H.

N84-29969"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ACEE COMPOSITE STRUCTURES TECHNOLOGY: REVIEW OF

SELECTED NASA RESEARCH ON COMPOSITE MATERIALS

AND STRUCTURES

Washington Aug. 1984 181 p refs Conf. held in Seattle,

13-16 Aug. 1984

(NASA-CP-2321; L-15834; NAS 1.55:2321) Avail: NTIS HC

A09/MF A01 CSCL 11D

ACEE PROGRAM, AIRCRAFT CONSTRUCTION MATERIALS,

AIRCRAFT DESIGN, AIRCRAFT STRUCTURES, COMPOSITE

MATERIALS, CONFERENCES, STRUCTURAL DESIGN

N84-33521"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

DEVELOPMENT OF IN SITU STIFFNESS PROPERTIES FOR

SHUTTLE BOOSTER FILAMENT WOUND CASE

V. VERDERAIME Aug. 1984 57 p refs

(NASA-TP-2377; NAS 1.60:2377) Avail: NTIS HC A04/MF A01

CSCL 11 D

ELASTIC PROPERTIES, PRESSURE VESSELS, ROCKET

ENGINE CASES, SPACE SHUTTLES, STIFFNESS

N85-11136"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

FRACTURE TOUGHNESS OF FIBROUS COMPOSITE

MATERIALS

C. C. POE, JR. Nov. 1984 68 p refs

(NASA-TP-2370; L-15848; NAS 1.60:2370) Avail: NTIS HC

A04/MFA01 CSCL 11D

FIBER COMPOSITES, FIBER ORIENTATION, FRACTURE

STRENGTH, GRAPHITE-EPOXY COMPOSITES, LAMINATES,

LAY-UP

N85-12094"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

LONG-TERM THERMAL AGING OF 2 GRAPHITE-POLYIMIDE

COMPOSITE MATERIALS

J. B. NELSON 1984 28 p refs

(NASA-TP-2369; L-t5849; NAS 1.60:2369) Avail: NTIS HC

A03/MF A01 CSCL 11D

AGING (MATERIALS), FLEXING, GRAPHITE-POLYIMIDE

COMPOSITES, LONG TERM EFFECTS, PANELS, TEMPERATURE

EFFECTS

N85-12941"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

TOUGH COMPOSITE MATERIALS

L. F. VOSTEEN, comp., N. J. JOHNSON, comp., and L. A.

TEtCHMAN, comp. Washington Dec. 1984 379 p refs

Workshop held in Hampton, Va., 24-26 May 1983

(NASA-CP-2334; L-15857; NAS 1.55:2334) Avail: NTIS HC

A17/MFA01 CSCL 11D

CONFERENCES, EPOXY MATRIX COMPOSITES, FIBER

COMPOSITES, FRACTURE STRENGTH, IMPACT STRENGTH,

LAMINATES, POLYMER MATRIX COMPOSITES, RESIN MATRIX

COMPOSITES, TOUGHNESS

N85-25435"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SPECTROSCOPIC ANALYSIS OF RADIATION-GENERATED

CHANGES IN TENSILE PROPERTIES OF A POLYETHERIMIDE

FILM

E. R. LONG, JR. and S.A.T. LONG May 1985 38 p refs

(NASA-TP-2429; L-15873; NAS 1.60:2429) Avail: NTIS HC

A03/MF A01 CSCL 11D

EXPOSURE, EXTRATERRESTRIAL RADIATION, POLYIMIDES,

RADIATION EFFECTS, SPECTROSCOPIC ANALYSIS, TENSILE

PROPERTIES

24 COMPOSITE MATERIALS

N85-26923"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

NASA/AIRCRAFT INDUSTRY STANDARD SPECIFICATION FOR

GRAPHITE FIBER TOUGHENED THERMOSET RESIN

COMPOSITE MATERIAL

Washington Jun. 1985 58 p

(NASA-RP-1142; L-15946; NAS 1.61:1142) Avail: NTIS HC

A04/MF A01 CSCL 11D

A standard specification for a selected class of graphite

fiber/toughened thermoset resin matrix material was developed

through joint NASA/Aircraft Industry effort. This specification was

compiled to provide uniform requirements and tests for qualifying

prepreg systems and for acceptance of prepreg batches. The

specification applies specifically to a class of composite prepreg

consisting of unidirectional graphite fibers impregnated with a

toughened thermoset resin that produce laminates with service

temperatures from -65 F to 200 F when cured at temperatures

below or equal to 350 F. The specified prepreg has a fiber areal

weight of 145 g sq m. The specified tests are limited to those

required to set minimum standards for the uncured prepreg and

cured laminates, and are not intended to provide design allowable

properties. Author

N85-26924"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECT OF LOW-VELOCITY OR BALLISTIC IMPACT DAMAGE

ON THE STRENGTH OF THIN COMPOSITE AND ALUMINUM

SHEAR PANELS

G. L. FARLEY (Army Research and Technology Lab., Hampton,

Va.) May 1985 40 p refs

(DA PRO& 1L1-61102-H-4503)

(NASA-TP-2441 ; L-15942; NAS 1.60:2441 ; AVSCOM-TR-85-B-1 )

Avail: NTIS HC A03/MF A01 CSCL 11D

ALUMINUM, BALLISTICS, FIBER REINFORCED

COMPOSITES, GRAPHITE-EPOXY COMPOSITES, IMPACT

STRENGTH, KEVLAR (TRADEMARK)

N86-11260"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

HIGH TEMPERATURE POLYMER MATRIX COMPOSITES

Washington Sep, 1985 409 p refs Conf. held in Cleveland,

Ohio, 16-18 Mar. 1983

(NASA-CP-2385; E-2425; NAS 1.55:2385) Avail: NTIS HC

A18/MFA01 CSCL 11D

ADHESIVES, AIRCRAFT CONSTRUCTION MATERIALS,

CHARACTERIZATION, COMPOSITE MATERIALS, DESIGN

ANALYSIS, ENVIRONMENT EFFECTS, MATRIX MATERIALS,

QUALITY CONTROL

N86-20508'# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

STRENGTH OF GRAPHITE/EPOXY BOLTED WING-SKIN

SPLICE SPECIMENS SUBJECTED TO OUTDOOR EXPOSURE

UNDER CONSTANT LOAD AND YEARLY FATIGUE LOADING

G. R. WICHOREK and J. H. CREWS, JR. 1986 35 p refs

(NASA-TP-2542; L-16065; NAS 1.60:2542) Avail: NTIS HC

A03/MF A01 CSCL 11D

GRAPHITE-EPOXY COMPOSITES, RESIDUAL STRENGTH,

SKIN (STRUCTURAL MEMBER), TRANSPORT AIRCRAFT,

WINGS

N86-21614"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

INTEGRATED COMPOSITE ANALYZER (ICAN): USERS AND

PROGRAMMERS MANUAL

P. L. N MURTHY and C. C. CHAMIS Mar. 1986 77 p refs

(NASA-TP-2515; E-2035; NAS 1.60:2515) Avail: NTIS HC

A05/MF A01 CSCL 11D

COMPUTER PROGRAMS, FIBER COMPOSITES,

STRUCTURAL ANALYSIS, USER MANUALS (COMPUTER

PROGRAMS)

83
25 INORGANIC AND PHYSICAL CHEMISTRY

25

INORGANIC AND PHYSICAL CHEMISTRY

Includes chemical analysis, e.g., chromatography; combustion

theory; electrochemistry; and photochemistry.

N77-33297"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

LEAN PREMIXED/PREVAPORIZED COMBUSTION

A. H. LEFEBVRE, ed. (Purdue Univ., Lafayette, Ind.) 21 Jan.

1977 46 p Presented at Workshop, Cleveland, Ohio, 20-21

Jan. 1977

(NASA-CP-2016; E-9255) Avail: NTIS HC A03/MF A01 CSCL

2tB

GAS TURBINE ENGINES, JET EXHAUST, POLLUTION

CONTROL, PREMIXED FLAMES

N78-12167"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EFFECT OF TRICHLOROFLUOROMETHANE AND MOLECULAR

CHLORINE ON OZONE FORMATION BY SIMULATED SOLAR

RADIATION

D. A. BITTKER and E. L. WONG Nov. 1977 22 p refs

(NASA-TP-1093; E-9078) Avail: NTIS HC A02/MF A01 CSCL

04A

CHLORINE, CHLORINE COMPOUNDS, OZONE, OZONE

FLUORIDE, SOLAR RADIATION

N78-16119"# National Bureau of Standards, Boulder, Colo.

Cryogenics Div.

THERMODYNAMIC AND RELATED PROPERTIES OF OXYGEN

FROM THE TRIPLE POINT TO 300 K AT PRESSURES TO 1000

BAR

L. A. WEBER Dec. 1977 164 p refs

(NASA-RP-1011; NBSIR-77-865) Avail: NTIS HC A08/MF A01

CSCL 07D

The results of an experimental program are presented in the

form of PVT data in the temperature range 58 to 300 K at pressures

up to 800 bar. Tables of the derived thermodynamic properties

on isobars to 1000 bar are given, including density, internal energy,

enthalpy, entropy, specific heats at constant volume and constant

pressure, velocity of sound, and the surface derivatives (delta

P/delta T) sub rho and (delta P/delta Rho) sub T. Auxiliary tables

in engineering units are also given. The accuracy of the data is

discussed and comparisons are made with previous data.

Author

N78-20281"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EFFECT OF NITRIC OXIDE ON PHOTOCHEMICAL OZONE

FORMATION IN MIXTURES OF AIR WITH MOLECULAR

CHLORINE AND WITH TRICHLOROFLUOROMETHANE

D. A. BITTKER and E. L. WONG Apr. 1978 25 p refs

(NASA-TP-1192; E-9297) Avail: NTIS HC A02/MF A01 CSCL

07D

CHLOROCARBONS, NITRIC OXIDE, OZONE PHOTOCHEMICAL REACTIONS

N78-22188"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ADSORPTION AND CHEMICAL REACTION OF GASEOUS

MIXTURES OF HYDROGEN CHLORIDE AND WATER ON

ALUMINUM OXIDE AND APPLICATION TO

SOLID-PROPELLANT ROCKET EXHAUST CLOUDS

W. R. COFER, III and G. L. PELLETT Apr. 1978 39 p refs

(NASA-TP-1105; L-11800) Avail: NTIS HC A03/MF A01

CSCL 07D

ADSORPTION, ALUMINUM OXIDES, CHEMICAL REACTIONS,

HYDROGEN CHLORIDES

84

N78-23172"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EXPERIMENTAL AND ANALYTICAL STUDY OF NITRIC OXIDE

FORMATION DURING COMBUSTION OF PROPANE IN A

JET-STIRRED COMBUSTOR

N. T. WAKELYN, C. J. JACHtMOWSKI, and C. H. WILSON May

1978 23 p refs

(NASA-TP-1181; L-12052) Avail: NTIS HC A02/MF A01

CSCL 07D

COMBUSTION, INJECTORS, NITRIC OXIDE

N79-12178"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ENHANCED HYDROPHILICITY OF CHLORIDED ALUMINUM

OXIDE PARTICULATES

W. R. COFER, III Nov. 1978 28 p refs

(NASA-TP-1312; L-12265) Avail: NTIS HC A02/MF A01

CSCL 07D

ALUMINUM OXIDES, CHEMISORPTION, HYDROCHLORIC

ACID, HYDROGENATION, PARTICULATES

N79-14177"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

A HIGH-PRESSURE PREMIXED FLAT-FLAME BURNER FOR

CHEMICAL PROCESS STUDIES

I. M. MILLER Dec. 1978 31 p refs

(NASA-TP-1318; L-12347) Avail: NTIS HC A03/MF A01

CSCL 21B

AIR POLLUTION, BURNERS, CHEMICAL REACTORS,

METHANE, PREMIXED FLAMES

N79-22246"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

CONTROL OF VOLUME RESISTIVITY IN INORGANIC ORGANIC

SEPARATORS

D. W_ SHEIBLEY and M. A. MANZO Apr. 1979 17 p refs

(NASA-TP-1439; E-9830) Avail: NTIS HC A02/MF A01 CSCL

07D

ALKALINE BATTERIES, ELECTRICAL RESISTIVITY,

INORGANIC COATINGS, ORGANIC COMPOUNDS,

SEPARATORS

N79-28181"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

IMPROVED, LOW COST INORGANIC-ORGANIC SEPARATORS

FOR RECHARGEABLE SILVER-ZINC BATTERIES

D. W. SHEIBLEY Jun. 1979 27 p refs

(NASA-TP-1476; E-9930) Avail: NTIS HC A03/MF A01 CSCL

07D

CURRENT DENSITY, INORGANIC COMPOUNDS, ORGANIC

COMPOUNDS, SEPARATORS, SILVER ZINC BATTERIES

N79-28259"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

CHEMICAL KINETIC MODELING OF BENZENE AND TOLUENE

OXIDATION BEHIND SHOCK WAVES

A. G. MCLAIN, C. J. JACHIMOWSKI, and C. H. WILSON Aug.

1979 26 p refs

(NASA-TP-1472; L-12803) Avail: NTIS HC A03/MF A01

CSCL 07D

BENZENE, OXIDATION, REACTION KINETICS, SHOCK

WAVES, TOLUENE

N80-13191"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECT OF PRESSURE ON STRUCTURE AND NO SUB X

FORMATION IN CO-AIR DIFFUSION FLAMES

H. G. MAAHS and 1. M. MILLER Oct. 1979 58 p refs

(NASA-TP-1448; L-12731) Avail: NTIS HC A04/MF A0t

CSCL 21B

CARBON MONOXIDE, DIFFUSION FLAMES, NITROGEN

OXIDES, PRESSURE EFFECTS
N80-16118"# National Aeronautics and Space Administration.

John F. Kennedy Space Center, Cocoa Beach, Fla.

NITROGEN DIOXIDE VAPOR PENETRATION OF

CHLOROBUTYL RUBBER SCAPE UNDER OPERATIONAL

CONDITIONS

T. A. SCHEHL and T. W. BEALL Feb. 1980 78 p refs

(NASA-TP-1605) Avail: NTIS HC A05/MF A01 CSCL 07D

CONCENTRATION (COMPOSITION), NITROGEN DIOXIDE,

PERMEATING, PROTECTIVE CLOTHING, RUBBER, VAPORS

N80-25392*# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

POLLUTANT EMISSIONS FROM FLAT-FLAME BURNERS AT

HIGH PRESSURES

H. G. MAAHS and I. M. MILLER Jun. 1980 41 p refs

(NASA-TP-1673; L-13550) Avail: NTIS HC A03/MF A01

CSCL 07D

AIR POLLUTION, BURNERS, CONTAMINANTS, EMISSION,

EXHAUST GASES, HIGH PRESSURE

N81-14017"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

CHEMICAL KINETIC MODELS FOR COMBUSTION OF

HYDROCARBONS AND FORMATION OF NITRIC OXIDE

C. J. JACHIMOWSKI and C. H. WILSON Dec. 1980 32 p

refs

(NASA-TP-1794; L-14106) Avail: NTIS HC A03/MF A01

CSCL 21B

CHEMICAL REACTIONS, HYDROCARBONS, NITRIC OXIDE,

REACTION KINETICS

N81-27223*# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

CHEMICAL KINETIC ANALYSIS OF HYDROGEN-AIR IGNITION

AND REACTION TIMES

R. C. ROGERS and C. J. SCHEXNAYDER, JR. Jul. 1981 54 p

refs

(NASA-TP-1856; L-14379) Avail: NTIS HC A04/MF A01

CSCL 07D

AIR, CHEMICAL REACTIONS, HYDROGEN FUELS, IGNITION,

REACTION KINETICS

N82-22330"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

CARBON-CATALYZED OXIDATION OF SO2 BY NO2 AND AIR

R. S. ROGOWSKI, D. R. SCHRYER, W. R. COFER, III, R. A.

EDAHL, JR., and S. MUNAVALLI (Livingstone College) Apr.

1982 10 p refs Submitted for publication

(NASA-TP-2014; L-15214; NAS 1.60:2014) Avail: NTIS HC

A02/MF A0t CSCL07D

ATMOSPHERIC CHEMISTRY, CARBON, CATALYSIS,

CATALYSTS, NITROGEN DIOXIDE, OXIDATION, SULFUR

DIOXIDES

N83-18863"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

MECHANISM OF LUBRICATION BY TRICRESYLPHOSPHATE

(TCP)

O. D. FAUT and D. R. WHEELER Feb. 1983 13 p refs

Presented at the ASLE Lubrication Conf., Washington, D.C., 5-7

Oct. 1982

(NASA-TP-2053; E-1244; NAS 1.60:2053) Avail: NTIS HC

A02/MF A01 CSCL 11H

CHEMICAL REACTIONS, COEFFICIENT OF FRICTION,

LUBRICANTS, METAL SURFACES, PHOSPHATES,

TEMPERATURE MEASUREMENT

26 METALLIC MATERIALS

N83-19825"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

A CHEMICAL KINETIC MIXTURE FOR THE IGNITION OF

SILANEIHYDROGEN MIXTURES

C. J. JACHIMOWSKI and A. G. MCLAIN Feb. 1983 20 p refs

(NASA-TP-2129; L-15542; NAS 1.60:2129) Avail: NTIS HC

A02/MF A01 CSCL21B

IGNITION, REACTION KINETICS, SILANES

N83-24575"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EXPERIMENTAL DESIGN OF AN INTERLABORATORY STUDY

FOR TRACE METAL ANALYSIS OF LIQUID FLUIDS

L. A. GREENBAUER-SENG May 1983 44 p refs

(NASA-TP-2148; E-1311; NAS 1.60:2148) Avail: NTIS HC

A03/MF A01 CSCL 07D

AEROSPACE VEHICLES, CONTAMINANTS, LIQUID FUELS,

TRACE ELEMENTS

N84-11230"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

METALLURGICAL CHARACTERIZATION OF THE FRACTURE

OF SEVERAL HIGH STRENGTH ALUMINUM ALLOYS

M. D. BHANDARKAR and W. B. LISAGOR Dec. 1977 71 p

refs

(NASA-TP-1086; L-11255; NAS 1.60:1086) Avail: NTIS HC

A04/MF A01 CSCL 11F

ALUMINUM ALLOYS, FRACTURE MECHANICS, HEAT TREATMENT, MICROSTRUCTURE, PHASE TRANSFORMATIONS

N84-32446"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

GCKP84-GENERAL CHEMICAL KINETICS CODE FOR

GAS-PHASE FLOW AND BATCH PROCESSES INCLUDING

HEAT TRANSFER EFFECTS

D. A. BITTKER and V. J. SCULLIN Sep. 1984 101 p refs

(NASA-TP-2320; E-1885; NAS 1.60:2320) Avail: NTIS HC

A06/MF A01 CSCL 07D

BATCH PROCESSING, COMPUTER PROGRAMS, GAS FLOW,

HEAT TRANSFER, IDEAL GAS, REACTION KINETICS

N86-31244"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

FUEL-RICH CATALYTIC COMBUSTION: A SOOT-FREE

TECHNIQUE FOR IN SlTU HYDROGEN-LIKE ENRICHMENT

T. A. BRABBS and S. L. OLSON Jul. 1985 12 p refs

Presented at the Fall Meeting of the Eastern Sect. of the Combust.

Inst., Clearwater Beach, Fla., 3-5 Dec. 1984

(NASA-TP-2498; E-2604; NAS 1.60:2498) Avail: NTIS HC

A02/MFA01 CSCL21B

BENZENE, CATALYSIS, COMBUSTION PRODUCTS, FUEL

COMBUSTION, HYDROCARBON FUELS, OXIDATION,

PARTICULATE SAMPLING, PYROLYSIS, SOOT

26

METALLIC MATERIALS

Includes physical, chemical, and mechanical properties of metals,

e.g., corrosion; and metallurgy.

N77-32286"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EFFECT OF CARBON CONTENT ON FRICTION AND WEAR

OF CAST IRONS

D. H. BUCKLEY Sep. 1977 22 p refs

(NASA-TP-1052; E-9110) Avail: NTIS HC AO2/MF A01 CSCL

11F

CARBON, CAST ALLOYS, FRICTION, IRON, WEAR

85
26 METALLIC MATERIALS

N78-11230"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

SECONDARY-ELECTRON-EMISSION PROPERTIES OF

CONDUCTING SURFACES WITH APPLICATION TO

MULTISTAGE DEPRESSED COLLECTORS FOR MICROWAVE

AMPLIFIERS

R. FORMAN Nov. 1977 33 p refs

(NASA-TP-1097; E-9233) Avail: NTIS HC A03/MF A01 CSCL

11F

CONDUCTORS, ELECTRODES, ELECTRON EMISSION,

MICROWAVE AMPLIFIERS

N78-15229"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

FRICTION AND WEAR OF SEVERAL COMPRESSOR GAS-PATH

SEAL MOVEMENTS

R. C. BILL and D. W. WISANDER Jan. 1978 42 p refs

(NASA-TP-1128; E-9276) Avail: NTIS HC A03/MF A01 CSCL

11A

COEFFICIENT OF FRICTION, COMPRESSORS, PLASMA

SPRAYING, SEALS (STOPPERS), WEAR

N78-15230"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

FEASIBILITY STUDY OF TUNGSTEN AS A DIFFUSION BARRIER

BETWEEN NICKEL-CHROMIUM-ALUMINUM AND GAMMA/

GAMMA PRIME - DELTA EUTECTIC ALLOYS

S. G. YOUNG and G. R ZELLARS Jan. 1978 35 p refs

(NASA-TP-1131; E-9271) Avail: NTIS HC A03/MF A01 CSCL

11F

BARRIER LAYERS, DIFFUSION, EUTECTICS, NICKEL

ALLOYS, TUNGSTEN

N78-15236"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

CORRECTION FACTORS FOR ON-LINE MICROPROBE

ANALYSIS OF MULTIELEMENT ALLOY SYSTEMS

J. UNNAM, D. R. TENNEY, and W. D. BREWER Nov. 1977

216 p refs

(NASA-RP-1006) Avail: NTIS HC A10/MF A01 CSCL 11F

An on-line correction technique was developed for the

conversion of electron probe X-ray intensities into concentrations

of emitting elements. This technique consisted of off-line calculation

and representation of binary interaction data which were read into

an on-line minicomputer to calculate variable correction coefficients.

These coefficients were used to correct the X-ray data without

significantly increasing computer core requirements. The binary

interaction data were obtained by running Colby's MAGIC 4 program

in the reverse mode. The data for each binary interaction were

represented by polynomial coefficients obtained by least-squares

fitting a third-order polynomial. Polynomial coefficients were

generated for most of the common binary interactions at different

accelerating potentials and are included. Results are presented

for the analyses of several alloy standards to demonstrate the

applicability of this correction procedure. Author

N78-21269"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

INFLUENCE OF FRETTING ON FLEXURAL FATIGUE OF 304

STAINLESS STEEL AND MILD STEEL

R. C. BILL (Army R and T Labs.) and D. A. ROHN Apr. 1978

19 p refs

(NASA-TP-1193; E-94t4) Avail: NTIS HC A02/MF A01 CSCL

11F

CRACKING (FRACTURING), FATIGUE LIFE, FATIGUE TESTS,

FRETTING, STAINLESS STEELS

86

N78-26198"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

ROLE OF ALLOYING ELEMENTS IN ADHESIVE TRANSFER AND

FRICTION OF COPPER-BASE ALLOYS

D. H. BUCKLEY Jun. 1978 19 p refs

(NASA-TP-1256; E-9471) Avail: NTIS HC A02/MF A01 CSCL

11F

ADHESION, COPPER ALLOYS, SLIDING FRICTION

N78-26199"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

MORPHOLOGY OF GOLD AND COPPER ION-PLATED

COATINGS

T. SPALVINS Jun. 1978 17 p refs

(NASA-TP-1262; E-9528) Avail: NTIS HC A02/MF A01 CSCL

11F

COATINGS, COPPER, GOLD, SURFACE FINISHING

N78-28225"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EROSION/CORROSION OF TURBINE AIRFOIL MATERIALS IN

THE HIGH-VELOCITY EFFLUENT OF A PRESSURIZED

FLUIDIZED COAL COMBUSTOR

G. R. ZELLARS, A. P. ROWE, and C. E. LOWELL Jul. 1978

33 p refs

(NASA-TP-1274; E-9507) Avail: NTIS HC A03/MF A01 CSCL

11F

COAL, COMBUSTION PRODUCTS, CORROSION

RESISTANCE, HEAT RESISTANT ALLOYS, TURBINE BLADES

N78-28226"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

LOW TOXIC CORROSION INHIBITORS FOR ALUMINUM IN

FRESH WATER

T. S. HUMPHRIES Jul. 1978 17 p

(NASA-TP-1279; M-259) Avail: NTIS HC A02/MF A01 CSCL

11F

ALUMINUM, CHEMICAL COMPOUNDS, CORROSION

PREVENTION, WATER

N78-30205"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

SIMULATION MODEL OF A SINGLE-STAGE LITHIUM

BROMIDE-WATER ABSORPTION COOLING UNIT

D. MIAO Aug. 1978 44 p refs

(NASA-TP-1296; E-9547) Avail: NTIS HC A03/MF A01 CSCL

20K

AIR CONDITIONING, COMPUTERIZED SIMULATION,

COOLING SYSTEMS

N78-30206"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EFFECT OF OXYGEN, METHYL MERCAPTAN, AND METHYL

CHLORIDE ON FRICTION BEHAVIOR OF COPPER-IRON

CONTACTS

D. H. BUCKLEY Aug. 1978 19 p refs

(NASA-TP-1309; E-9606) Avail: NTIS HC A02/MF A01 CSCL

11F

FRICTION REDUCTION, METHYL CHLORIDE, OXYGEN,

SLIDING FRICTION, SOLID-SOLID INTERFACES, THIOLS

N78-31213"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EFFECTS OF THERMOMECHANICAL PROCESSING ON

STRENGTH AND TOUGHNESS OF IRON - 12-PERCENT-NICKEL

- REACTIVE METAL ALLOYS AT -196 C

J. R. STEPHENS and W. R. WITZKE Aug. 1978 36 p refs

(NASA-TP-1308; E-9583) Avail: NTIS HC A03/MF A01 CSCL

11F

ALLOYS, IRON, NICKEL, THERMODYNAMIC PROPERTIES,

YIELD STRENGTH
26 METALLIC MATERIALS

N78-33196"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

LONG-TERM HOT-HARDNESS CHARACTERISTICS OF FIVE

THROUGH-HARDENED BEARING STEELS

N. E. ANDERSON Oct. 1978 20 p refs Prepared in

cooperation with US Army Aviation Research and Development

Command, St. Louis, Mo.

(NASA-TP-1341; E-9533) Avail: NTIS HC A02/MF A01 CSCL

11F

BEARING ALLOYS, HARDNESS TESTS, LONG TERM

EFFECTS, STEELS, TEMPERING

N79-13137"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

GEOMETRIC RELATIONSHIPS FOR HOMOGENIZATION IN

SINGLE-PHASE BINARY ALLOY SYSTEMS

J. UNNAM (George Washington Univ,), D. R. TENNEY, and B. A.

STEIN Nov. 1978 15 p refs

(NASA-TP-1349; L-12588) Avail: NTIS HC A02/MF A01

CSCL 11F

BINARY ALLOYS, GEOMETRY, HOMOGENIZING, SURFACE

PROPERTIES, VOLUME

N79-13138"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECT OF CONCENTRATION DEPENDENCE OF THE

DIFFUSION COEFFICIENT ON HOMOGENIZATION KINETICS IN

MULTIPHASE BINARY ALLOY SYSTEMS

D. R, TENNEY and J. UNNAM (George Washington Univ,) Nov,

1978 39 p refs

(NASA-TP-1281; L-12224) Avail: NTIS HC A03/MF A01

CSCL 1t F

BINARY ALLOYS, CONCENTRATION (COMPOSITION),

DIFFUSION COEFFICIENT, HOMOGENIZING, KINETICS

N79-16950"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

CHARACTERIZATION OF LARGE 2219 ALUMINUM ALLOY

HAND FORGINGS FOR THE SPACE SHUTTLE SOLID ROCKET

BOOSTER

M. W. BRENNECKE Dec. 1978 107 p refs

(NASA-TP-1383; M-273) Avail: NTIS HC A06/MF A01 CSCL

11F

ALUMINUM ALLOYS, CHARACTERIZATION, FORGING,

SPACE SHUTTLE BOOSTERS

N79-21184"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

WEAR OF ALUMINUM AND HYPOEUTECTIC ALUMINUM-SILICON ALLOYS IN BOUNDARY-LUBRICATED PIN-ON DISK SLIDING

J. FERRANTE and W. A. BRAINARD Apr. 1979 27 p refs

(NASA-TP-1442; E-9809) Avail: NTIS HC A03/MF A01 CSCL

11F

ALUMINUM, BOUNDARY LUBRICATION, EUTECTIC ALLOYS,

SILICON, WEAR TESTS

N79-28288"# National Aeronautics and Space Administration.

John F. Kennedy Space Center, Cocoa Beach, Fla.

STUDY OF AUSTENITIC STAINLESS STEEL WELDED WITH

LOW ALLOY STEEL FILLER METAL

F. A. BURNS and R. A. DYKE, JR. Jun. 1979 32 p

(NASA-TP-1460) Avail: NTIS HC A03/MF A01 CSCL 11F

ALLOYS, AUSTENITIC STAINLESS STEELS, FILLERS,

IMPACT STRENGTH, TENSILE STRENGTH, WELD TESTS

N80-11188"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

MECHANICAL PROPERTIES AND OXIDATION AND

CORROSION RESISTANCE OF REDUCED-CHROMIUM 304

STAINLESS STEEL ALLOYS

J. R. STEPHENS, C. A. BARRETT, and C. A. GYORGAK

Washington Nov. 1979 22 p refs

(NASA-TP-1557; E-065) Avail: NTIS HC A02/MF A01 CSCL

11F

CHROMIUM ALLOYS, CORROSION RESISTANCE,

STAINLESS STEELS, TENSILE PROPERTIES

N80-15234"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

ADHESION AND FRICTION OF IRON-BASE BINARY ALLOYS

IN CONTACT WITH SILICON CARBIDE IN VACUUM

K. MIYOSHI and D. H. BUCKLEY Jan. 1980 13 p refs

(NASA-TP°1604; E-126) Avail: NTIS HC A02/MF A01 CSCL

11F

ADHESION, BINARY ALLOYS, COEFFICIENT OF FRICTION,

IRON, SILICON CARBIDES

N80-16141"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

SCANNING-ELECTRON-MICROSCOPE STUDY OF NORMAL-IMPINGEMENT EROSION OF DUCTILE METALS

W. A, BRAINARD and J. SALIK Jan. 1980 11 p refs

(NASA-TP-1609; E-085) Avail: NTIS HC A02/MF A01 CSCL

11F

ALUMINUM, COPPER, ELECTRON MICROSCOPY, EROSION,

IMPACT DAMAGE

N80-32489"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

LONG-TIME CREEP BEHAVIOR OF THE TANTALUM ALLOY

ASTAR 811C

W. D. KLOPP, R. H. TITRAN, and K. D. SHEFFLER (Pratt and

Whitney Aircraft, East Hartford, Conn.) Sep. 1980 21 p refs

(NASA-TP-1691; E-041) CSCL 11F

CREEP ANALYSIS, GRAIN BOUNDARIES, STRESS-STRAINTIME RELATIONS, TANTALUM ALLOYS, TEMPERATURE DEPENDENCE

N80-33555"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

LONG-TIME CREEP BEHAVIOR OF THE NIOBIUM ALLOY

C-103

R. H TITRAN and W. D. KLOPP Oct. 1980 12 p refs

(NASA-TP-1727; E-224) Avail: NTIS HC A02/MF A01 CSCL

11F

CREEP PROPERTIES, NIOBIUM ALLOYS, TEMPERATURE

EFFECTS

N81-16210"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EFFECTS OF ERODANT PARTICLE SHAPE AND VARIOUS

HEAT TREATMENTS ON EROSION RESISTANCE OF PLAIN

CARBON STEEL

J. SALIK and D. H. BUCKLEY Jan. 1981 10 p refs

(NASA-TP-1755; E-326) Avail: NTIS HC A02/MF A01 CSCL

11F

CARBON STEELS, EROSION, HEAT TREATMENT, IMPACT

RESISTANCE, METAL SURFACES, SHAPES, TRIBOLOGY

N81-19273"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

CREEP AND RESIDUAL MECHANICAL PROPERTIES OF CAST

SUPERALLOYS AND OXIDE DISPERSION STRENGTHENED

ALLOYS

J. D. WHITTENBERGER Feb. 1981 69 p refs

(NASA-TP-1781; E-472) Avail: NTIS HC A04/MF A01 CSCL

11F

CREEP PROPERTIES, FATIGUE TESTS, HEAT RESISTANT

ALLOYS, MECHANICAL PROPERTIES

87
26 METALLIC MATERIALS

N81-20245"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EFFECTS OF GEOMETRIC VARIABLES ON RUB

CHARACTERISTICS OF TI-6AL-4V

R C. BILL, J. WOLAK (Washington Univ., Seattle), and D. W.

WISANDER Apr. 1981 21 p refs Prepared in cooperation

with Army Aviation Research and Development Command,

Cleveland, Ohio

(NASA-TP-1835; AVRADCOM-TR-80-C-19; E-449) Avail: NTIS

HC A02/MF A01 CSCL 11F

ALUMINUM ALLOYS, BLADE TIPS, TITANIUM ALLOYS,

VANADIUM ALLOYS, WEAR

N82-20291"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

FRICTION AND WEAR OF IRON IN CORROSIVE METAL

G. W. P. RENGSTORFF, K. MIYOSHI, and D. H. BUCKLEY Mar.

1982 18 p refs

(NASA-TP-1985; NAS 1.60:1985; E-638) Avail: NTIS HC

A02/MF A01 CSCL 11F

COEFFICIENT OF FRICTION, CORROSION TESTS, FRICTION,

IRON, METAL SURFACES, SLIDING, WEAR TESTS

N82-21298"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EFFECT OF ALUMINUM PHOSPHATE ADDITIONS ON

COMPOSITION OF THREE-COMPONENT PLASMA-SPRAYED

SOLID LUBRICANT

T. P. JACOBSON and S. G. YOUNG Mar. 1982 19 p refs

(NASA-TP-1990; E-713; NAS 1.60:1990) Avail: NTIS HC

A02/MF A01 CSCL 11F

ADDITIVES, PLASMA SPRAYING, POWDER METALLURGY,

PROTECTIVE COATINGS, SELF LUBRICATION

N82-21300"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

FRICTION WEAR AND AUGER ANALYSIS OF IRON IMPLANTED

WITH 1.5-MEV NITROGEN IONS

J. FERRANTE and W. R. JONES, JR. Mar. 1982 14 p refs

(NASA-TP-1989; E-678; NAS 1.60:1989) Avail: NTIS HC

A02/MF A01 CSCL 11F

ION IMPLANTATI©N, iRON, NITROGEN IONS, SLIDING

FRICTION, WEAR

N82-21301"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

FRICTION AND SURFACE CHEMISTRY OF SOME

FERROUS-BASE METALLIC GLASSES

K. MIYOSHI and D. H BUCKLEY Mar. 1982 14 p refs

(NASA-TP-1991: E-919; NAS 1.60:1991) Avail: NTIS HC

A02/MF A01 CSCL 11F

AMORPHOUS MATERIALS, FERROUS METALS, FRICTION,

METALLIC GLASSES

N82-22349'# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio,

SURFACE CHEMISTRY, MICROSTRUCTURE AND FRICTION

PROPERTIES OF SOME FERROUS-BASE METALLIC GLASSES

AT TEMPERATURES TO 750 C

K. MIYOSHI and D. H. BUCKLEY Apr. 1982 16 p refs

(NASA-TP-2006; E-1001; NAS 1.60:2006) Avail: NTIS HC

A02/MF A01 CSCL 11B

FRICTION FACTOR, METALLIC GLASSES, MICROSTRUCTURE, SLIDING FRICTION

N83-15413"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio,

UNIVERSAL APPROACH TO ANALYSIS OF CAVITATION AND

LIQUID-IMPINGEMENT EROSION DATA

P. V. RAO and S. G. YOUNG Nov. 1982 39 p refs

(NASA-TP-2061; E-1087; NAS 180:2061) Avail: NTIS HC

A03/MF A01 CSCL 20D

CAVITATION CORROSION, EROSION, IMPINGEMENT

88

N83-16491"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

AN ELECTROCHEMICAL METHOD FOR DETERMINING

HYDROGEN CONCENTRATIONS IN METALS AND SOME

APPLICATIONS

M. D. DANFORD Jan. 1983 18 p refs

(NASA-TP-2113; NAS 1.60:2113) Avail: NTIS HC A02/MF A01

CSCL 11F

CORROSION, ELECTROLYSIS, ELECTROPLATING, HYDROGEN EMBRITTLEMENT

N83-16492"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

OPTICAL OBSERVATIONS OF UNIDIRECTIONAL

SOLIDIFICATION IN MICROGRAVITY

M. H. JOHNSTON, R. B. OWEN, and R. E. SHURNEY Jan.

1983 28p refs

(NASA-TP-2110; NAS 1.60:2110) Avail: NTIS HC A03/MF A01

CSCL 11F

AMMONIUM CHLORIDES, REDUCED GRAVITY,

SOLIDIFICATION, TEMPERATURE PROFILES, WATER

N83-18895"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

A POTENTIAL-ENERGY SCALING MODEL TO SIMULATE THE

INITIAL STAGES OF THIN-FILM GROWTH

J. H. HEINBOCKEL (Old Dominion Univ.), R. A. OUTLAW, and G.

H. WALKER Feb. 1983 38 p refs

(NASA-TP-2102; L-15531; NAS 1.60:2102) Avail: NTIS HC

A03/MF A01 CSCL 11F

CRYSTAL GROWTH, POTENTIAL ENERGY, SCALING LAWS,

SOLAR ARRAYS, SOLID-SOLID INTERFACES, THIN FILMS

N83-19889"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va,

ELEVATED TEMPERATURE BEHAVIOR OF SUPERPLASTICALLY FORMED/WELD-BRAZED TITANIUM COMPRESSION

PANELS HAVING ADVANCED SHAPED STIFFENERS

D. M. ROYSTER and T. T. BALES Mar. 1983 29 p rets

(NASA-TP-2123; L-15547; NAS 1.60:2123) Avail: NTIS HC

A03/MF A01 CSCL 11F

SUPERPLASTICITY, TEMPERATURE EFFECTS, TITANIUM

ALLOYS, WELDING

N83-21110"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

SLIDING INDUCED CRYSTALLIZATION OF METALLIC GLASS

K. MIYOSHI and D. H. BUCKLEY Mar, 1983 23 p refs

(NASA-TP-2140; E-1278; NAS 1.60:2140) Avail: NTIS HC

A02/MFA01 CSCL 11F

AMORPHOUS MATERIALS, CRYSTALLIZATION, METALLIC

GLASSES, PHOTOMICROGRAPHY, SLIDING FRICTION, WEAR

TESTS

N83-23419"# National Aeronautics and Space Administration,

Lewis Research Center, Cleveland, Ohio.

X-RAY PHOTOELECTRON SPECTROSCOPY AND FRICTION

STUDIES OF NII_KEL-ZINC AND MANGANESE-ZINC FERRITES

IN CONTACT WITH METALS

K. MIYOSHI and D. H. BUCKLEY Apr. 1983 19 p refs

(NASA-TP-2163; E-1349; NAS 1.60:2163) Avail: NTIS HC

A02/MF A01 CSCL 11F

FERRITES, FRICTION, MANGANESE, NICKEL, SLIDING

FRICTION, SPECTROSCOPIC ANALYSIS, ZINC
N83-24640"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

NITRIDING OF TITANIUM AND TITANIUM: 8 PERCENT

ALUMINUM, 1 PERCENT MOLYBDENUM, 1 PERCENT

VANADIUM ALLOY WITH AN ION-BEAM SOURCE

A. GILL (Ben Gurion Univ. of the Negev) Apr. 1983 11 p refs

(NASA-TP-2149; E-1227; NAS 1.60:2149) Avail: NTIS HC

A02/MFA01 CSCL 11F

ARGON, HARDENING (MATERIALS), ION BEAMS, NITRIDING,

NITROGEN, TITANIUM NITRIDES, WEAR INHIBITORS

N83-24641"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

MORPHOLOGY OF AN ALUMINUM ALLOY ERODED BY A JET

OF ANGULAR PARTICLES IMPINGING AT NORMAL

INCIDENCE

P. V. RAO, S. G. YOUNG (NASA. Kennedy Space Center), and

D. H. BUCKLEY May 1983 15 p refs

(NASA-TP-2139; E-1166; NAS 1.60:2139) Avail: NTIS HC

A02/MFA01 CSCL 11F

ALUMINUM ALLOYS, EROSION, JET IMPINGEMENT,

MORPHOLOGY, PARTICLE LADEN JETS, WEAR

N83-32908"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

TIME DEPENDENCE OF SOLID-PARTICLE IMPINGEMENT

EROSION OF AN ALUMINUM ALLOY

P. VEERABHADRARAO and D. H. BUCKLEY Aug. 1983 24 p

refs Presented at 6th Intern. Conf. on Erosion by Liquid and

Solid Impact, Cambridge, England, 4-8 Sep. 1983

(NASA-TP-2169; E-1381; NAS 1.60:2169) Avail: NTIS HC

A02/MF A01 CSCL 11F

ALUMINUM ALLOYS, BEADS, EROSION, GLASS, JET

IMPINGEMENT, VOLUME

N83-34019"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

FRICTION AND HARDNESS OF GOLD FILMS DEPOSITED BY

ION PLATING AND EVAPORATION

K. MIYOSHI, T. SPALVINS, and D. H. BUCKLEY Aug. 1983

10 p refs

(NASA-TP-2207; E-1528; NAS 1.60:2207) Avail: NTIS HC

A02/MF A01 CSCL 11F

EVAPORATION, GOLD, HARDNESS, ION PLATING, METAL

FILMS, SLIDING FRICTION

N83-35100"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

FABRICATION AND EVALUATION OF COLD/FORMED/WELDBRAZED BETA-TITANIUM SKIN-STIFFENED COMPRESSION

PANELS

D. M. ROYSTER, T. T. BALES, R. C. DAVIS, and H. R. WlANT

(Kentron International, Inc., Hampton, Va.) Sep. 1983 28 p

refs

(NASA-TP-2201; L-15634; NAS 1.60:2201) Avail: NTIS HC

A03/MFA01 CSCL 11F

BETA FACTOR, COLD WORKING, PANELS, STIFFENING,

TEMPERATURE EFFECTS, TITANIUM ALLOYS

N84-13263"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

GALVANIC COUPLING BETWEEN D6AC STEEL, 6061-T6

ALUMINUM, INCONEL 718 AND GRAPHITE-EPOXY

COMPOSITE MATERIAL: CORROSION OCCURRENCE AND

PREVENTION

M. D. DANFORD and R. H. HIGGINS Dec. 1983 18 p refs

(NASA-TP-2236; NAS 1.60:2236) Avail: NTIS HC A02/MF A01

CSCL 11 F

ALUMINUM ALLOYS, CORROSION PREVENTION,

ELECTROCHEMICAL CORROSION, GRAPHITE-EPOXY

COMPOSITES, INCONEL (TRADEMARK), SOLID-SOLID

INTERFACES, STEELS

26 METALLIC MATERIALS

N84-17350"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

PRELIMINARY STUDY OF THERMOMECHANICAL FATIGUE OF

POLYCRYSTALMNE MAR-M 200

R. C. BILL (USAAVSCOM Research and Technology Labs.), M. J.

VERRILLI (Northwestern Univ.), M. A. MCGAW, and G. R.

HALFORD Feb. 1984 17 p refs

(NASA-TP-2280; E-1795; NAS 1.60:2280; AVSCOM-TR-83-C-6)

Avail: NTIS HC A02/MF A01 CSCL 11F

COBALT ALLOYS, FATIGUE TESTS, HEAT RESISTANT

ALLOYS, METAL FATIGUE, THERMAL CYCLING TESTS,

THERMAL FATIGUE

N84-18370"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

ANALYSIS OF THERMOELECTRIC PROPERTIES OF

HIGH-TEMPERATURE COMPLEX ALLOYS OF NICKEL-BASE,

IRON-BASE AND COBALT-BASE GROUPS

R. HOLANDA Jan. 1984 23 p refs

(NASA-TP-2278; E-1854; NAS 1.60:2278) Avail: NTIS HC

A02/MFA01 CSCL 11F

COBALT ALLOYS, HEAT RESISTANT ALLOYS, HIGH

TEMPERATURE RESEARCH, IRON ALLOYS, NICKEL ALLOYS,

THERMOELECTRICITY

N84-21716"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

FRICTION AND WEAR OF IRON IN SULFURIC ACID

G. W. P. RENGSTORFF (Toledo Univ.), K. MIYOSHI, and D_ H.

BUCKLEY Apr. 1983 22 p refs

(NAG3-276)

(NASA-TP-2289; E-1635; NAS 1.60:2289) Avail: NTIS HC

A02/MF A01 CSCL 11F

CORROSION, IRON, SLIDING FRICTION, SULFURIC ACID,

TRtBOLOGY, WEAR TESTS

N84-21721"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

FRICTION AND WEAR OF NICKEL IN SULFURIC ACID

G. W. P. RENGSTORFF (Toledo Univ., Ohio), K. MIYOSHI, and

D. H. BUCKLEY Apr. 1984 17 p refs

(NAG3-276)

(NASA-TP-2290; E-1817; NAS 1.60:2290) Avail: NTIS HC

A02/MF A01 CSCL 11F

CORROSION, METAL SURFACES, NICKEL, SLIDING

FRICTION, SULFURIC ACID, TRIBOLOGY, WEAR TESTS

N84-23750"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

FRACTURE TEMPERATURE AND FLAW GROWTH IN NITRONIC

40 AT CRYOGENIC TEMPERATURES

M. S. DOMACK May 1984 46p refs

(NASA-TP-2312; L-15722; NAS 1.60:2312) Avail: NTIS HC

A03/MF A01 CSCL 11F

AUSTENITIC STAINLESS STEELS, CRACK PROPAGATION,

FRACTURE STRENGTH, LOW TEMPERATURE TESTS, STRESS

ANALYSIS, WIND TUNNEL MODELS

N84-26783"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EFFECTS OF ALLOY COMPOSITION ON CYCLIC FLAME

HOT-CORROSION ATTACK OF CAST NICKEL-BASE

SUPERALLOYS AT 900 DEG C

D. L. DEADMORE Jul. 1984 30 p refs

(NASA-TP-2338; E-2009; NAS 1.60:2338) Avail: NTIS HC

A03/MFA01 CSCL 11F

CHEMICAL COMPOSITION, COBALT ALLOYS, CORROSION

TESTS, HEAT RESISTANT ALLOYS, HOT CORROSION, NICKEL

ALLOYS

89
26 METALLIC MATERIALS

N84-28958"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

CHEMICAL MECHANISMS AND REACTION RATES FOR THE

INITIATION OF HOT CORROSION OF IN-738

G. C. FRYBURG, F. J. KOHL, and C. A. STEARNS Jut. 1984

34 p Submitted for publication

(NASA-TP-2319; E°1847; NAS 1.60:2319) Avail: NTIS HC

A03/MF A01 CSCL 11F

CHEMICAL REACTIONS, HEAT RESISTANT ALLOYS, HOT

CORROSION, NICKEL ALLOYS, REACTION KINETICS

N85-22662"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

AN ELECTROCHEMICAL STUDY OF THE CORROSION

BEHAVIOR OF PRIMER COATED 2219-T87 ALUMINUM

M. D. DANFORD and R. H. HIGGINS Apr. 1985 27 p refs

(NASA-TP-2459; NAS 1.60:2459) Avail: NTIS HC A03/MF A01

CSCL 11F

ALUMINUM, CORROSION TESTS, ELECTROCHEMICAL

CORROSION, PRIMERS (COATINGS)

N84-28965"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EROSION OF IRON-CHROMIUM ALLOYS BY GLASS

PARTICLES

J. SALIKand D. H. BUCKLEY Jul. 1984 10p refs

(NASA-TP-2354; E-1615; NAS 1.60:2354) Avail: NTIS HC

A02/MFA01 CSCL 11F

BEADS, CHEMICAL COMPOSITION, CHROMIUM, EROSION,

FRICTION, HARDNESS, IRON ALLOYS

N84-31349"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EMPIRICAL RELATIONS FOR CAVITATION AND LIQUID

IMPINGEMENT EROSION PROCESSES

P. V. RAO and D. H. BUCKLEY Aug. 1984 27 p refs

Submitted for publication

(NCC3-21)

(NASA-TP-2339; E-1872; NAS 1.60:2339) Avail: NTIS HC

A03/MF A01 CSCL 11F

CAVITATION CORROSION, EROSION, JET IMPINGEMENT,

MATHEMATICAL MODELS, METAL SURFACES

N84-34589"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

FUNDAMENTALS OF ALLOY SOLIDIFICATION APPLIED TO

INDUSTRIAL PROCESSES

Washington Sep. 1984 185 p refs Conf. held in Cleveland,

12-13 Sap. 1984 Sponsored in part by Case Western Reserve

Univ.

(NASA-CP-2337; E-2235; NAS 1.55:2337) Avail: NTIS HC

A09/MF A01 CSCL 11F

CONFERENCES, CRYSTAL GROWTH, LOW GRAVITY

MANUFACTURING, METALS, SOLIDIFICATION, SPACE

SHUTTLE PAYLOADS

N85-13006"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EFFECT OF HUMIDITY ON FRETTING WEAR OF SEVERAL

PURE METALS

H. GOTO (Cleveland State Univ., Ohio) and D. H. BUCKLEY Dec.

1984 12p refs

(NASA-TP-2403; E-2184; NAS 1.60:2403) Avail: NTIS HC

A02/MFA01 CSCL 11F

FRETTING, HUMIDITY, METALS, WEAR

N86-12295"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

AN UPDATE OF THE TOTAL-STRAIN VERSION OF SRP

J. F. SALTSMAN and G. R. HALFORD Oct. 1985 27 p refs

Presented at the Symp. on Low Cycle Fatigue: Direc. for the

Future, Lake George, N.Y., 30 Sep. - 4 Oct. 1985; sponsored by

American Society for Testing and Materials, American Inst. of

Mining, Metallurgical and Petroleum Engineers, and American

Society for Metals

(NASA-TP-2499; E-2575; NAS 1.60:2499) Avail: NTIS HC

A03/MFA01 CSCL 11F

CREEP PROPERTIES, FATIGUE (MATERIALS), NICKEL,

PREDICTION ANALYSIS TECHNIQUES, STRAIN RATE

N86-13406"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

FABRICATION AND EVALUATION OF SUPERPLASTICALLY

FORMED/WELD-BRAZED CORRUGATED COMPRESSION

PANELS WITH BEADED WEBS

D. M ROYSTER, R. C. DAVIS, J. M. SHINN, JR., T. T. BALES,

and H. R. WlANT Nov. 1985 31 p refs

(NASA-TP-2512; L-15988; NAS 1.60:2512) Avail: NTIS HC

A03/MF A01 CSCL 11F

BEADS, BRAZING, COMPRESSION LOADS, CORRUGATED

PLATES, EVALUATION, FABRICATION, FORMING TECHNIQUES,

PANELS, SUPERPLASTICITY, TITANIUM ALLOYS, WEBS

(SUPPORTS), WELDED JOINTS

N86-26412"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

OXIDATION AND EMITTANCE OF SUPERALLOYS IN HEAT

SHIELD APPLICATIONS

K. E. WIEDEMANN (Analytical Services and Materials, Inc.,

Hampton, Va.), R. K. CLARK, and J. UNNAM Jun. 1986 20 p

Presented at the TMS-AIME Fall Meeting, Toronto, Ontario, 13-17

Oct. 1985

(NASA-TP-2578; L-16104; NAS 1.60:2578) Avail: NTIS HC

A02/MF A01 CSCL 11F

ALUMINUM OXIDES, EMITTANCE, HEAT RESISTANT

ALLOYS, HEAT SHIELDING, OXIDATION, OXIDE FILMS,

REENTRY SHIELDING, SPACECRAFT CONSTRUCTION

MATERIALS, WIND TUNNEL TESTS

N85-21323"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EFFECTS OF CHROMIUM AND ALUMINUM ON MECHANICAL

AND OXIDATION PROPERTIES OF IRON-NICKEL-BASE

SUPERALLOYS BASED ON CG-27

S. R. SCHUON Mar. 1985 26 p refs Presented at the

TMS-AIME Fall Meeting, Detroit, 17-20 Sap. 1984

(NASA-TP-2443; E-2320; NAS 1.60:2443) Avail: NTIS HC

A03/MFA01 CSCL 11F

ALUMINUM, CHROMIUM, IRON ALLOYS, MECHANICAL

PROPERTIES, OXIDATION, TENSILE STRENGTH

N86-26413"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ANALYSIS OF THE PHYSICAL ATOMIC FORCES BETWEEN

NOBLE GAS ATOMS, ALKALI IONS AND HALOGEN IONS

J. W. WILSON, J. H. HEtNBOCKEL (Old Dominion Univ., Hampton,

Va.), and R. A. OUTLAW Jun. 1986 37 p

(NASA-TP-2568; L°16093; NAS 1.60:2568) Avail: NTIS HC

A03/MF A01 CSCL 07D

CRYSTAL SURFACES, GAS-SOLID INTERACTIONS, HALITES,

INTERATOMIC FORCES, INTERMOLECULAR FORCES, RARE

GASES

9O
N86-30837"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

THE VARIATION OF CORROSION POTENTIAL WITH TIME FOR

COATED METAL SURFACES

M. D. DANFORD and W. W. KNOCKEMUS (Huntingdon Coll.,

Montgomery, Ala.) Sep. 1986 27 p

(NASA-TP-2636; NAS 1.60:2636) Avail: NTiS HC A03/MF A01

CSCL 11F

CORROSION RESISTANCE, ELECTROCHEMISTRY, PRIMERS

(COATINGS), PROTECTIVE COATINGS

27

NONMETALLIC MATERIALS

Includes physical, chemical, and mechanical properties of plastics,

elastomers, lubricants, polymers, textiles, adhesives, and ceramic

materials.

N77-32312"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

FRICTION AND WEAR BEHAVIOR OF SINGLE-CRYSTAL

SILICON CARBIDE IN CONTACT WITH TITANIUM

K. MIYOSHI and D. H. BUCKLEY Sep. 1977 24 p refs

(NASA-TP-1035; E-9067) Avail: NTIS HC A02/MF A01 CSCL

11G

SILICON CARBIDES, SLIDING FRICTION, TITANIUM, WEAR

N77-33348"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

X-RAY PHOTOELECTRON SPECTROSCOPY STUDY OF

RADIOFREQUENCY-SPUTTERED TITANIUM, CARBIDE,

MOLYBDENUM CARBIDE, AND TITANIUM BORIDE COATINGS

AND THEIR FRICTION PROPERTIES

W. A. BRAINARD and D. R. WHEELER Oct. 1977 21 p refs

(NASA-TP-1033; E-9102) Avail: NTIS HC A02/MF A01 CSCL

11G

FRICTION FACTOR, SPUTTERING, X RAY SPECTROSCOPY

N77-33350"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

FRICTION AND DEFORMATION BEHAVIOR OF

SINGLE-CRYSTAL SILICON CARBIDE

K. MIYOSHI (Kanazawa Univ., Kanazawa, Japan) and D. H.

BUCKLEY Oct. 1977 22 p refs

(NASA-TP-1053; E-9121) Avail: NTIS HC A02/MF A01 CSCL

20B

CRYSTAL SURFACES, ELASTIC DEFORMATION, SILICON

CARBIDES, SLIDING FRICTION

N78-10295"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

FRICTION AND WEAR OF SINGLE-CRYSTAL AND

POLYCRYSTALLINE MAGANESE-ZlNC FERRITE IN CONTACT

WITH VARIOUS METALS

K. MIYOSHI (Kanazawa Univ.) and D. H. BUCKLEY 1977 28 p

refs

(NASA-TP-1059) Avail: NTIS HC A03/MF A01 CSCL 20B

FERRITES, METAL COMPOUNDS, POLYCRYSTALS, SINGLE

CRYSTALS, SLIDING FRICTION, WEAR

N78-12222"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EFFECTIVENESS OF VARIOUS ORGANOMETALLICS AS

ANTIWEAR ADDITIVES IN MINERAL OIL

D. H. BUCKLEY Nov. 1977 20 p refs

(NASA-TP-1096) Avail: NTIS HC A02/MF A01 CSCL 11H

ADDITIVES, COEFFICIENT OF FRICTION, MINERAL OILS,

ORGANOMETALLIC COMPOUNDS

27 NONMETALLIC MATERIALS

N78-12223"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EVALUATION OF A LOW-DENSITY POLYIMIDE FOAM IN A

DYNAMIC, HIGH TEMPERATURE ENVIRONMENT

C. M. PITTMAN and R. D. BROWN Washington Dec. 1977

25 p refs

(NASA-TP-1049; L-11739) Avail: NTIS HC A02/MF A01

CSCL 11G

AEROSPACE VEHICLES, FOAMS, HEAT SHIELDING,

POLYIMIDE RESINS

N78-15277"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EFFECT OF THERMAL EXPOSURE ON LUBRICATING

PROPERTIES OF POLYIMIDE FILMS AND POLYIMIDE-BONDED

GRAPHITE FLUORIDE FILMS

R. L. FUSARO Jan. 1978 26 p refs

(NASA-TP-1125; D-9179) Avail: NTIS HC A03/MF A01 CSCL

11G

FLUORIDES, GRAPHITE, LUBRICANTS, POLYIMIDES,

TEMPERATURE EFFECTS, THIN FILMS

N78-15278"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

FRICTION AND WEAR OF POLYETHYLENE OXIDE POLYMER

HAVING A RANGE OF MOLECULAR WEIGHTS

D. H. BUCKLEY Jan. 1978 17 p refs

(NASA-TP-1129; E-9261) Avail: NTIS HC A02/MF A01 CSCL

11G

COEFFICIENT OF FRICTION, MOLECULAR WEIGHT, OXIDES,

POLYETHYLENES, WEAR

N78-20336"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

X-RAY PHOTOELECTRON SPECTROSCOPY STUDY OF

RADIOFREOUENCY-SPUTTERED REFRACTORY COMPOUND

STEEL INTERFACES

D. R. WHEELER and W. A. BRAINARD Feb. 1978 20 p refs

(NASA-TP-1161; E-9374) Avail: NTIS HC A02/MF A01 CSCL

11G

METAL COATINGS, REFRACTORY MATERIALS,

SPUTTERING, STEELS, X RAY SPECTROSCOPY

N78-20337"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

LUBRICATION AND FAILURE MECHANISMS OF GRAPHITE

FLUORIDE FILMS

R. L. FUSARO Apr. 1978 32 p refs

(NASA-TP-1197; E-9346) Avail: NTIS HC A03/MF A01 CSCL

11H

FAILURE ANALYSIS, LUBRICATION, THIN FILMS, WEAR

N78-20338"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

FRICTION AND WEAR OF RADIOFREQUENCY-SPUTTERED

BORIDES, SlLIClDES, AND CARBIDES

W. A. BRAINARD and D. R. WHEELER Apr. 1978 19 p refs

(NASA-TP-1156; E-9384) Avail: NTIS HC A02/MF A01 CSCL

11G

BORIDES, CARBIDES, FRICTION, SILICIDES, WEAR

N78-21294"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

FRICTION AND METAL TRANSFER FOR SINGLE-CRYSTAL

SILICON CARBIDE IN CONTACT WITH VARIOUS METALS IN

VACUUM

K. MIYOSHI (Kanazawa Univ., Japan) and D. H. BUCKLEY Apr.

1978 27 p refs

(NASA-TP-1191; E-9307) Avail: NTIS HC A03/MF A01 CSCL

11G

CHEMICAL BONDS, COEFFICIENT OF FRICTION,

INTERFACIAL ENERGY, SILICON CARBIDES, SINGLE

CRYSTALS, TRANSITION METALS, VACUUM TESTS

91
27 NONMETALLIC MATERIALS

N18-21295"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

WEAR OF SINGLE-CRYSTAL SILICON CARBIDE IN CONTACT

WITH VARIOUS METALS IN VACUUM

K. MIYOSHI and D. H. BUCKLEY Apr. 1978 24 p refs

(NASA-TP-1198; E-9360) Avail: NTIS HC A02/MF A01 CSCL

11G

ALUMINUM, COPPER, SILICON CARBIDES, SINGLE

CRYSTALS, SLIDING FRICTION, TRANSITION METALS, WEAR

TESTS

N78-22233"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

EVALUATION OF MATERIALS FOR HIGH PERFORMANCE

SOLAR ARRAYS Status Report No. 1

A. F. WHITAKER, C. F. SMITH, JR., C. L. PEACOCK, JR., and S.

A. LITTLE Apr. 1978 41 p

(NASA-TP-1220; M-252) Avail: NTIS HC A03/MF A01 CSCL

11G

IRRADIATION, OUTGASSING, SOLAR ARRAYS, VACUUM

TESTS

N79-13159"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

LUBRICATION AND FAILURE MECHANISMS OF MOLYBDENUM

DISULFIDE FILMS. 2: EFFECT OF SUBSTRATE ROUGHNESS

R. L. FUSARO Dec. 1978 30 p refs

(NASA-TP-1379; E-9715) Avail: NTIS HC A03/MF A01 CSCL

11H

FAILURE ANALYSIS, LUBRICANTS, MOLYBDENUM

DISULFIDES, SURFACE ROUGHNESS

N79-15184"# National Aeronautics and Space Administration.

Lewis Research Canter, Cleveland, Ohio.

EFFECT OF NITROGEN-CONTAINING PLASMA ON ADHERENCE, FRICTION, AND WEAR OF RADIOFREQUENCY-SPUTTERED TITANIUM CARBIDE COATINGS

W. A. BRAINARD and D. R. WHEELER Jan. 1979 21 p refs

(NASA-TP-1377; E-9681) Avail: NTIS HC A02/MF A01 CSCL

11D

ADHESION, COATINGS, FRICTION, NITROGEN,

SPUTTERING, TITANIUM CARBIDES, WEAR TESTS

N78-25215"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

PRESSURELESS SINTERED SIALONS WITH LOW AMOUNTS

OF SINTERING AID

A. ARIAS Jun. 1978 16 p refs

(NASA-TP-1246; E-9522) Avail: NTIS HC A02/MF A01 CSCL

11G

ALUMINUM, CERAMICS, SILICON, SINTERING, YTTRIUM

N79-21204"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EFFECT OF OXYGEN-NITROGEN RATIO ON SINTERABILITY

OF SIALONS

A. ARIAS Apr. 1979 24 p refs

(NASA-TP-1382; E-9814) Avail: NTIS HC A02/MF A01 CSCL

11B

CERAMICS, MASS RATIOS, NITROGEN, OXYGEN, SILICON

COMPOUNDS, SINTERING

N78-28247"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EFFECT OF OXYGEN AND NITROGEN INTERACTIONS ON

FRICTION OF SINGLE-CRYSTAL SILICON CARBIDE

K. MIYOSHI and D. H. BUCKLEY (Kanazawa Univ., Japan) Aug.

1978 22p refs

(NASA-TP-1265; E-9424) Avail: NTIS HC A02/MF A01 CSCL

11G

COEFFICIENT OF FRICTION, FRICTION, NITROGEN,

OXYGEN, SILICON CARBIDES, SINGLE CRYSTALS,

SOLID-SOLID INTERFACES

N79-21205"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio,

THERMAL STRESS ANALYSIS OF CERAMIC GAS-PATH SEAL

COMPONENTS FOR AIRCRAFT TURBINES

F. E. KENNEDY and R. C. BILL Apr. 1979 22 p refs

Prepared in cooperation with Army Aviation Res. and Develop.

Command, Cleveland

(NASA-TP-1437; E-9770; AVRADCOM-TR-78-42) Avail: NTIS

HCA02/MFA01 CSCL 11B

CERAMIC BONDING, GAS FLOW, LEAKAGE, THERMAL

STRESSES, TURBINE BLADES

N78-30238"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

FRICTION AND WEAR OF METALS WITH A SINGLE-CRYSTAL

ABRASIVE GRIT OF SILICON CARBIDE: EFFECT OF SHEAR

STRENGTH OF METAL

K. MIYOSHI (Kanazawa Univ., Japan) and D. H. BUCKLEY Aug.

1978 27 p refs

(NASA-TP-1293; E-9499) Avail: NTIS HC A03/MF A01 CSCL

11G

METAL SURFACES, SHEAR STRENGTH, SILICON CARBIDES,

SLIDING FRICTION

N79-23216*# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EFFECT OF STERILIZATION IRRADIATION ON FRICTION AND

WEAR OF ULTRAHIGH-MOLECULAR-WEIGHT POLYETHYLENE

W. R. JONES, JR., W. F. HADY, and A. CRUGNOLA (Lowell

Univ.) May 1979 22 p refs

(NASA ORDER C-8756)

(NASA-TP-1462; E-9697) Avail: NTIS HC A02/MF A01 CSCL

07C

IRRADIATION, POLYETHYLENES, SLIDING FRICTION,

STERILIZATION, WEAR

N79-13158"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

LUBRICATION AND FAILURE MECHANISMS OF MOLYBDENUM

DISULFIDE FILMS. 1: EFFECT OF ATMOSPHERE

R. L. FUSARO Dec. 1978 29p

(NASA-TP-1343; E-9600) Avail: NTIS HC A03/MF A01 CSCL

11H

ATMOSPHERIC EFFECTS, COEFFICIENT OF FRICTION,

FAILURE ANALYSIS, LUBRICANTS, MOLYBDENUM

DISULFIDES

N79-27308"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

AUGER SPECTROSCOPY ANALYSIS OF LUBRICATION WITH

ZINC DIALKYLDITHIOPHOSPHATE OF SEVERAL METAL

COMBINATIONS IN SLIDING CONTACT

D. H. BUCKLEY Jut. 1979 19 p

(NASA-TP-1489; E-9909) Avail: NTIS HC A02/MF A01 CSCL

11H

AUGER SPECTROSCOPY, LUBRICATION, OIL ADDITIVES,

ZINC COMPOUNDS

92
N79-27309"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

MODULES OF RUPTURE AND OXIDATION RESISTANCE OF

S12.55AL0.6OO.72N3.52 SlALON

A. ARIAS Jul. 1979 15 p refs

(NASA-TP-1490; E-9971) Avail: NTIS HC A02/MF A01 CSCL

11B

CERAMICS, CREEP RUPTURE STRENGTH, OXIDATION

RESISTANCE, SILICON COMPOUNDS

N79-29327"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

PLASMA-SPRAYED COATINGS FOR LUBRICATION OF A

TITANIUM ALLOY IN AIR AT 430 DEG C

H. E. SLINEY and D. H. WISANDER Jul. 1979 14 p

(NASA-TP-1509; E-9876) Avail: NTIS HC A02/MF A01 CSCL

11H

PLASMA SPRAYING, SELF LUBRICATING MATERIALS,

SPRAYED COATINGS, TITANIUM ALLOYS

N79-30380"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

ANISOTROPIC FRICTION, DEFORMATION, AND FRACTURE OF

SINGLE-CRYSTAL SILICON CARBIDE AT ROOM

TEMPERATURE

K. MIYOSHI and D. H. BUCKLEY Aug. 1979 24 p refs

(NASA-TP-1525; E-9988) Avail: NTIS HC A02/MF A01 CSCL

07D

ANISOTROPY, CRYSTAL SURFACES, FRACTURES

(MATERIALS), PLASTIC DEFORMATION, SILICON CARBIDES,

SLIDING FRICTION

N79-30381"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

LUBRICATING AND WEAR MECHANISMS FOR A HEMISPHERE

SLIDING ON POLYIMIDE-BONDED GRAPHITE FLUORIDE

FILM

R. L. FUSARO Aug. 1979 30 p refs

(NASA-TP-1524; E-9965) Avail: NTIS HC A03/MF A01 CSCL

11H

COEFFICIENT OF FRICTION, GRAPHITE, LUBRICATION,

SLIDING FRICTION, SOLID LUBRICANTS, WEAR

N79-32359"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EVALUATION AND AUGER ANALYSIS OF A

ZINC-DIALKYL-DITHIOPHOSPHATE ANTIWEAR ADDITIVE IN

SEVERAL DIESTER LUBRICANTS

W. A. BRAINARD and J. FERRANTE Washington Oct. 1979

16 p refs

(NASA-TP-1544; E-9944) Avail: NTIS HC A02/MF A01 CSCL

11H

ADDITIVES, AUGER SPECTROSCOPY, DIALLYL

COMPOUNDS, LUBRICANT TESTS, SLIDING FRICTION, WEAR

TESTS

N80-11226"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ELECTRON AND PROTON ABSORPTION CALCULATIONS FOR

A GRAPHITE/EPOXY COMPOSITE MODEL

E. R. LONG, JR. Nov. 1979 33 p refs

(NASA-TP-1568; L-13073) Avail: NTIS HC A02/MF A01

CSCL 11G

GRAPHITE-EPOXY COMPOSITES, LARGE SPACE

STRUCTURES, RADIATION ABSORPTION

27 NONMETALLIC MATERIALS

N80-17220"# National Aeronautics and Space Administration,

Lewis Research Center, Cleveland, Ohio.

LUBRICATION AND WEAR MECHANISMS OF

POLYIMIDE-BONDED GRAPHITE FLUORIDE FILMS

SUBJECTED TO LOW CONTACT STRESS

R. L. FUSARO Jan. 1980 27 p refs

(NASA-TP-1584; E-9990) Avail: NTIS HC A03/MF A01 CSCL

11H

GRAPHITE, LUBRICATION, POLYIMIDES, POLYMERIC FILMS,

WEAR

N80-18178"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

WEAR PARTICLES OF SINGLE-CRYSTAL SILICON CARBIDE

IN VACUUM

K. MIYOSHI and D. H. BUCKLEY Feb. 1980 24 p refs

Submitted for publication

(NASA-TP-1624; E-077) Avail: NTIS HC A02/MF A01 CSCL

20B

SILICON CARBIDES, SPALLING, WEAR

N80-21532"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EFFECTS OF OXIDE ADDITIONS AND TEMPERATURE ON

SINTERABILITY OF MILLED SILICON NITRIDE

A. ARIAS Apr. 1980 21 p refs

(NASA-TP-1644; E-243) Avail: NTIS HC A02/MF A0t CSCL

11D

CESIUM OXIDES, MAGNESIUM OXIDES, SILICON NITRIDES,

SINTERING, TEMPERATURE EFFECTS, YTTRIUM OXIDES

N80-22493"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

STEADY-STATE WEAR AND FRICTION IN BOUNDARY

LUBRICATION STUDIES

W. R. LOOMIS and W. R. JONES, JR. May 1980 11 p refs

(NASA-TP-1658; E-129) Avail: NTIS HC A02/MF A01 CSCL

11G

BOUNDARY LUBRICATION, STATIC FRICTION, WEAR

N80-22494"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

FRICTION AND WEAR OF IRON-BASE BINARY ALLOYS IN

SLIDING CONTACT WITH SILICON CARBIDE IN VACUUM

K. MIYOSHI and D. H. BUCKLEY May 1980 11 p refs

(NASA-TP-1612; E-260) Avail: NTIS HC A02/MF A01 CSCL

11F

IRON ALLOYS, SILICON CARBIDES, SLIDING FRICTION,

TRIBOLOGY, WEAR

N80-23453"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

PRELIMINARY STUDY OF METHODS FOR PROVIDING

THERMAL SHOCK RESISTANCE TO PLASMA-SPRAYED

CERAMIC GAS-PATH SEALS

R, C. BILL (AVRADCOM Res. and Technol. Labs.), D. W.

WISANDER, and D. E. BREWE (AVRADCOM Res. and Technol.

Labs.) May 1980 24 p refs

(NASA-TP-1561; E-9941; AVRADCOM-TR-79-28) Avail: NTIS

HC A02/MF A01 CSCL 11G

PLASMA SPRAYING, SHOCK RESISTANCE, THERMAL

SHOCK

N81-11214"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

POLYTETRAFLUOROETHYLENE TRANSFER FILM STUDIED

WITH X-RAY PHOTOELECTRON SPECTROSCOPY

D. R. WHEELER Nov. 1980 11 p refs

(NASA-TP-1728; E-414) Avail: NTIS HC A02/MF A01 CSCL

11G

KNUDSEN FLOW, LOW DENSITY RESEARCH, MEAN FREE

PATH, POLYTETRAFLUOROETHYLENE, THIN FILMS, X RAY

SPECTROSCOPY

93
27 NONMETALLICMATERIALS

N81-14079"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

CHANGES IN SURFACE CHEMISTRY OF SILICON CARBIDE

(0001) SURFACE WITH TEMPERATURE AND THEIR EFFECT

ON FRICTION

K. MIYOSHI and D. H. BUCKLEY Nov. 1980 12 p refs

(NASA-TP-1756; E-475) Avail: NTIS HC A02/MF A01 CSCL

07D

CRYSTAL STRUCTURE, FRICTION, SILICON CARBIDES,

SURFACE REACTIONS

N81-19300"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

SURFACE CHEMISTRY AND FRICTION BEHAVIOR OF THE

SILICON CARBIDE (0001) SURFACE AT TEMPERATURES TO

1500 DEC C

K. MIYOSHI and D. H. BUCKLEY Mar. 1981 14 p refs

(NASA-TP-1813; E-542) Avail: NTIS HC A02/MF A01 CSCL

11C

AUGER SPECTROSCOPY, FRICTION, PHOTOELECTRON

SPECTROSCOPY, SILICON CARBIDES, SURFACE PROPERTIES

N81-21193"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

STEADY-STATE BOUNDARY LUBRICATION WITH

FORMULATED C-ETHERS TO 260 C

W. R. LOOMIS Apr. 1981 16 p refs

(NASA-TP-1812; E-480) Avail: NTIS HC A02/MF A01 CSCL

07C

BOUNDARY LUBRICATION, HIGH TEMPERATURE

LUBRICANTS, POLYPHENYL ETHER

N81-27282"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

CORRELATION OF IDEAL AND ACTUAL SHEAR STRENGTHS

OF METALS WITH THEIR FRICTION PROPERTIES

K. MIYOSHI and D. H BUCKLEY Jul. 1981 12 p refs

(NASA-TP-1891; E-701) Avail: NTIS HC A02/MF A01 CSCL

11F

COEFFICIENT OF FRICTION, METALS, SHEAR STRENGTH,

TRIBOLOGY

N81-31365"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

DEVELOPMENT OF SILANE-HYDROLYSATE BINDER FOR

UV-RESISTANT THERMAL CONTROL COATINGS

W. J. PATTERSON Aug. 1981 23 p refs Original contains

color illustrations

(NASA-TP-1900; M-353) Avail: NTIS HC A02/MF A01 CSCL

11G

HYDROLYSIS, PROTECTIVE COATINGS, SILANES,

TEMPERATURE CONTROL, THERMAL RESISTANCE

N81-31366"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EFFECT OF YTTRIA ADDITIVES ON PROPERTIES OF

PRESSURELESS-SINTERED SILICON NITRIDE

A. ARIAS Sep. 1981 11 p refs

(NASA-TP-1899; E-751) Avail: NTIS HC A02/MF A01 CSCL

1tG

ADDITIVES, CERAMICS, MECHANICAL PROPERTIES,

SILICON NITRIDES, SINTERING, SPALLING, YTTRIUM

N81-33292"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

AVENUES AND INCENTIVES FOR COMMERCIAL USE OF A

LOW-GRAVITY ENVIRONMENT

R. L. BROWN and L. K. ZOLLER Sep. 1981 21 p

(NASA-TP-1925; M-357; LA41/LA01) Avail: NTIS HC A02/MF

A01 CSCL 22A

AEROSPACE ENVIRONMENTS, LOW GRAVITY

MANUFACTURING, SPACE PROCESSING

N81-33293"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

RELATIONSHIP BETWEEN THE IDEAL TENSILE STRENGTH

AND THE FRICTION PROPERTIES OF METALS IN CONTACT

WITH NONMETALS AND THEMSELVES Flnal Report

K. MIYOSHI and D. H. BUCKLEY Washington NASA Sep.

1981 10 p refs

(NASA-TP-1883; E-587) Avail: NTIS HC A02/MF A01 CSCL

11H

COEFFICIENT OF FRICTION, METALS, SLIDING FRICTION,

SURFACE ENERGY, TENSILE STRENGTH, TRIBOLOGY

N82-16239"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

TRIBOLOGICAL CHARACTERISTICS OF A COMPOSITE

TOTAL-SURFACE HIP REPLACEMENT Final Report

W. R JONES, JR., J. C. ROBERTS (Rensselaer Polytechnic Inst.),

and F. F. LING (Rensselaer Polytechnic Inst.) Washington

NASA Jan. 1982 17 p refs Presented at the ASME-ASLE

Joint Lubrication Conf., New Orleans, 5-7 Oct. 1981

(NASA-TP-1853; E-709) Avail: NTIS HC A02/MF A01 CSCL

11H

COMPOSITE MATERIALS, E GLASS, EPOXY RESINS,

TRIBOLOGY

N82-19373"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

TRIBOLOGICAL PROPERTIES AT 25 C OF SEVEN POLYIMIDE

FILMS BONDED TO 440 C HIGH-TEMPERATURE STAINLESS

STEEL

R. L. FUSARO Feb. t982 23 p refs

(NASA-TP-1944; E-758) Avail: NTIS HC A02/MF A01 CSCL

07C

FRICTION, HIGH TEMPERATURE, POLYIMIDES, POLYMERIC

FILMS, SOLID LUBRICANTS, STAINLESS STEELS, TRIBOLOGY,

WEAR

N82-19374"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

SURFACE CHEMISTRY AND WEAR BEHAVIOR OF

SINGLE-CRYSTAL SILICON CARBIDE SLIDING AGAINST IRON

AT TEMPERATURES TO 1500 C IN VACUUM

K. MIYOSHI and D. H. BUCKLEY Feb. 1982 14 p refs

(NASA-TP-1947; E-654) Avail: NTIS HC A02/MF A01 CSCL

07C

CHEMICAL REACTIONS, IRON, SILICON CARBIDES, SINGLE

CRYSTALS, SLIDING FRICTION, SURFACE PROPERTIES,

WEAR

N82-20316"#

Lewis Research Center, Cleveland, Ohio.

INFLUENCE OF MINERAL OIL AND ADDITIVES

MICROHARDNESS AND SURFACE CHEMISTRY

MAGNESIUM OXIDE (001) SURFACE

K. MIYOSHI, H. SHIGAKI, and D. H. BUCKLEY Mar. 1982

p refs

(NASA-TP-1986; E-975; NAS 1,60:1986) Avail: NTIS HC

A02/MF A01 CSCL 11H

CRYSTAL SURFACES, MAGNESIUM OXIDES,

MICROHARDNESS, MINERAL OILS, SURFACE REACTIONS

National Aeronautics and Space Administration.

ON

OF

11

N82-21332"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

THERMAL AND OXIDATIVE DEGRADATION STUDIES OF

FORMULATED C-ETHERS BY GEL-PERMEATION

CHROMATOGRAPHY

W. R. JONES, JR. and W. MORALES Mar. 1982 14 p refs

(NASA-TP-1994; NAS 1.60:1994; E-976) Avail: NTIS HC

A02/MFA01 CSCL07D

ETHERS, LIQUID CHROMATOGRAPHY, LUBRICANTS,

OXIDATION, THERMAL DEGRADATION

94
N82-22366"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EFFECTS OF ENVIRONMENT ON MICROHARDNESS OF

MAGNESIUM OXIDE

H. ISHIGAKI (Osaka Univ.) and D. H. BUCKLEY Apr. 1982 11

p refs

(NASA-TP-2002; E-916; NAS 1.60:2002) Avail: NTIS HC

A02/MF A01 CSCL 11B

ENVIRONMENTAL TESTS, HARDNESS TESTS, HYDROGEN

CHLORIDES, MAGNESIUM OXIDES, MICROHARDNESS

N82-32491"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

OCCURRENCE OF SPHERICAL CERAMIC DEBRIS IN

INDENTATION AND SLIDING CONTACT

K. MIYOSHI and D. H. BUCKLEY Aug. 1982 21 p refs

(NASA-TP-2048; E-1072; NAS 1.60:2048) Avail: NTIS HC

A02/MF A01 CSCL 11G

CERAMICS, DEBRIS, INDENTATION, SILICON CARBIDES,

SLIDING FRICTION, WEAR TESTS

N83-14269"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EFFECT OF SLIDING SPEED AND CONTACT STRESS ON

TRIBOLOGICAL PROPERTIES OF ULTRA-HIGH-MOLECULARWEIGHT POLYETHYLENE

R. L. FUSARO Nov. 1982 22 p refs

(NASA-TP-2059; E-1060; NAS 1.60:2059) Avail: NTIS HC

A02/MF A01 CSCL 11G

DISKS (SHAPES), MOLECULAR WEIGHT, POLYETHYLENES,

SLIDING FRICTION, STAINLESS STEELS, TRIBOLOGY, WEAR

N83-16528"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

ANALYSIS OF A MIL-L-27502 LUBRICANT FROM A

GAS-TURBINE ENGINE TEST BY SIZE-EXCLUSION

CHROMATOGRAPHY

W. R. JONES, JR. and W. MORALES Jan. 1983 15 p refs

(NASA-TP-2063; E-1075; NAS 1.60:2063) Avail: NTIS HC

A02/MF A01 CSCL 11H

DEGRADATION, ESTERS, GAS TURBINE ENGINES, HIGH

TEMPERATURE LUBRICANTS

N83-24695"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

SOLID SPHERICAL GLASS PARTICLE IMPINGEMENT STUDIES

OF PLASTIC MATERIALS

P. V. RAO (National Academy of Sciences - National Research

Council, Washington, D.C.), S. G. YOUNG, and D. H. BUCKLEY

1983 19 p refs

(NASA-TP-2161; E-1122; NAS 1.60:2161) Avail: NTIS HC

A02/MF A01 CSCL 111

BEADS, IMPACT DAMAGE, IMPINGEMENT, POLYCARBONATES, POLYMETHYL METHACRYLATE, POLYTETRAFLUOROETHYLENE

N84-16334"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

FRICTION AND MORPHOLOGY OF MAGNETIC TAPES IN

SLIDING CONTACT WITH NICKEL-ZINC FERRITE

K. MIYOSHI, D. H. BUCKLEY, and B. BHUSHAN (IBM Corp.)

Jan. 1984 18 p refs

(NASA-TP-2267; NAS 1.60:2267; E-1720) Avail: NTIS HC

A02/MF A01 CSCL 131

COEFFICIENT OF FRICTION, DEFORMATION, MAGNETIC

TAPES, NICKEL ALLOYS, SLIDING FRICTION, ZINC ALLOYS

27 NONMETALLIC MATERIALS

N84-18399"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

WATER-VAPOR EFFECTS ON FRICTION OF MAGNETIC TAPE

IN CONTACT WITH NICKEL-ZINC FERRITE

K. MIYOSHI and D. H. BUCKLEY Feb. 1984 10 p refs

(NASA-Tpo2279; E-1768; NAS 1.60:2279) Avail: NTIS HC

A02/MFA01 CSCL 11G

FRICTION, HUMIDITY, MAGNETIC TAPES, NICKEL ALLOYS,

PINS, ZINC ALLOYS

N84-18400"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

BEAM IMPINGEMENT ANGLE EFFECTS ON SECONDARY

ELECTRON EMISSION CHARACTERISTICS OF TEXTURED

PYROLYTIC GRAPHITE

A. N CURREN and K. A. JENSEN Feb. 1984 16 p refs

(NASA-TP-2285; E-1886; NAS 1.60:2285) Avail: NTIS HC

A02/MF A01 CSCL 11G

ELECTRON EMISSION, GRAPHITE, MICROWAVE

AMPLIFIERS, SECONDARY EMISSION, SPACE COMMUNICATION, TRAVELING WAVE TUBES

N84-19564"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

ULTRA-HIGH MOLECULAR WEIGHT SILPHENYLENEoSILOXANE POLYMERS

W. J. PATTERSON, N. H. HUNDLEY, and L. M. LUDWICK Mar.

1984 19p refs

(NASA-TP-2295; NAS 1.60:2295) Avail: NTIS HC A02/MF A01

CSCL 11B

COPOLYMERS, MOLECULAR WEIGHT, POLYMER

CHEMISTRY, POLYMER PHYSICS, POLYMERIZATION

N84-21740"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

OVERVIEW OF ZIRCONIA WITH RESPECT TO GAS TURBINE

APPLICATIONS

J. D. CAWLEY Mar. 1984 29 p refs

(NASA-TP-2286; E-1726; NAS 1.60:2286) Avail: NTIS HC

A03/MF A01 CSCL 11G

CHEMICAL PROPERTIES, GAS TURBINE ENGINES,

MECHANICAL PROPERTIES, PHASE TRANSFORMATIONS,

THERMAL CONDUCTIVITY, ZIRCONIUM OXIDES

N84-23764"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

SIMULATION OF LUBRICATING BEHAVIOR OF A THIOETHER

LIQUID LUBRICANT BY AN ELECTROCHEMICAL METHOD

W. MORALES May 1984 12 p refs

(NASA-TP-2316; E-1808; NAS 1.60:2316) Avail: NTIS HC

A02/MF A01 CSCL 11H

ANIONS, CHEMICAL REACTIONS, ELECTROCHEMICAL

CELLS, LUBRICANTS, SIMULATION

N84-28989"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

SECONDARY ELECTRON EMISSION CHARACTERISTICS OF

ION-TEXTURED COPPER AND HIGH-PURITY ISOTROPIC

GRAPHITE SURFACES

A. N CURREN and K. A. JENSEN Jul. 1984 16 p refs

(NASA-TP-2342; E-2064; NAS 1.60:2342) Avail: NTIS HC

A02/MF A01 CSCL 11G

ACCUMULATORS, COPPER, ELECTRODES, MICROWAVE

AMPLIFIERS, PYROLYTIC GRAPHITE, SECONDARY EMISSION,

SURFACE PROPERTIES, TRAVELING WAVE TUBES

95
27 NONMETALLIC MATERIALS

N84-31379"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

ADHESION BETWEEN POLYMERS AND EVAPORATED GOLD

AND NICKEL FILMS

Y. YAMADA, D. R. WHEELER, and D. H. BUCKLEY Aug. 1984

11 p refs

(NASA-TP.2360; E-2018; NAS 1.60:2360) Avail: NTIS HC

A02/MFA01 CSCL 11B

ADHESION, ADHESION TESTS, GOLD COATINGS, METAL

FILMS, NICKEL COATINGS, POLYETHYLENES

N84-33590"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

FRICTION BEHAVIOR OF SILICON IN CONTACT WITH

TITANIUM, NICKEL, SILVER AND COPPER

H. MISHINA (Institute of Physical and Chemical Research) and D.

H. BUCKLEY Sep. 1984 8 p refs

(NASA-TP-2362; E-2036; NAS 1.60:2362) Avail: NTIS HC

A02/MF A01 CSCL 11G

CHEMICAL REACTIONS, FRICTION MEASUREMENT,

FRICTION REDUCTION, SEMICONDUCTORS (MATERIALS),

SLIDING FRICTION

N85-13044"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EFFECT OF BARRIER HEIGHT ON FRICTION BEHAVIOR OF

THE SEMICONDUCTORS SILICON AND GALLIUM ARSENIDE

IN CONTACT WITH PURE METALS

H. MISHINA (Inst. of Physical and Chemical Research, Saitama,

Japan) and D. H. BUCKLEY Dec. 1984 12 p refs

(NASA-TP-2405; E-2219; NAS 1.60:2405) Avail: NTIS HC

A02/MF A01 CSCL 11B

GALLIUM ARSENIDES, METALS, SCHOTTKY DIODES,

SEMICONDUCTORS (MATERIALS), SILICON, SLIDING

FRICTION

N85-13045"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

HIGH-TEMPERATURE EROSION OF PLASMA-SPRAYED,

YTTRIA-STABILIZED ZlRCONIA IN A SIMULATED TURBINE

ENVIRONMENT

R F. HANSCHUH Dec. 1984 19 p refs Prepared in

cooperation with Army Research and Technology Labs.,

Cleveland

(NASA-TP-2406; E-2271; NAS 1.60:2406; AVSCOM-TR-84-C-17)

Avail: NTIS HC A02/MF A0t CSCL 11B

EROSION, GAS TURBtNE ENGINES, PLASMA SPRAYING,

SEALS (STOPPERS), YTTRIUM, ZIRCONIUM

N85o21359"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

HUMIDITY EFFECTS ON ADHESION OF NICKEL-ZINC FERRITE

IN ELASTIC CONTACT WITH MAGNETIC TAPE AND ITSELF

K. MIYOSHI, D. H. BUCKLEY, T. KUSAKA (Osaka Inst. of

Technology), and C. MAEDA (Osaka Inst, of Technology) Mar.

1985 10p refs

(NASA-TP-2449; E-2361; NAS 1.60:2449) Avail: NTIS HC

A02/MF A01 CSCL 11G

ADHESION, FERR_TES, HUMIDITY, MAGNETIC TAPES,

NICKEL, ZINC

N85-26990*# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ata.

FORMULATION/CURE TECHNOLOGY FOR ULTRAHIGH

MOLECULAR WEIGHT SlLPHENYLENE-SILOXANE POLYMERS

N. H. HUNDLEY and W. J. PATTERSON May 1985 21 p

refs

(NASA-TP-2476; NAS 1.60:2476) Avail: NTIS HC A02/MF A01

CSCL 11G

CURING, ELASTOMERS, MOLECULAR WEIGHT,

POLYMERIZATION, SILOXANES

96

N86-15394"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

TEXTURED CARBON ON COPPER: A NOVEL SURFACE WITH

EXTREMELY LOW SECONDARY ELECTRON EMISSION

CHARACTERISTICS

A. N. CURREN and K. A. JENSEN Dec. 1985 16 p refs

(NASA-TP-2543; E-2674; NAS 1.60:2543) Avail: NTIS HC

A02/MFA01 CSCL 11G

BEAMS (RADIATION), CARBON, COPPER, ELECTRON

EMISSION, IMPINGEMENT, MICROWAVE AMPLIFIERS,

SECONDARY EMISSION, SUBSTRATES, SURFACE

PROPERTIES, TEXTURES, TRAVELING WAVE TUBES

N86-28194"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

MICROGRAVITY POLYMERS

Jun. 1986 22 p Proceedings of a Workshop held in Cleveland,

Ohio, 9 May 1985

(NASA-CP-2392; E-2707; NAS 1.55:2392) Avail: NTIS HC

A02/MF A01 CSCL 11B

CHEMICAL ENGINEERING, GRAVITATIONAL EFFECTS,

POLYMER CHEMISTRY, POLYMER PHYSICS, REDUCED

GRAVITY

N86-29040"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

NUMERICAL MODELING OF PHYSICAL VAPOR TRANSPORT

IN A VERTICAL CYLINDRICAL AMPOULE, WITH AND WITHOUT

GRAVITY

T. L. MILLER Jul. 1986 21 p

(NASA-TP-2620; NAS 1.60:2620) Avail: NTIS HC A02/MF A01

CSCL 20D

COMPUTATIONAL FLUID DYNAMICS, CRYSTAL GROWTH,

MATHEMATICAL MODELS, REDUCED GRAVITY, TRANSPORT

PROPERTIES, VAPOR PHASE EPITAXY

28

PROPELLANTS AND FUELS

Includes rocket propellants, igniters, and oxidizers; their storage

and handling procedures; and aircraft fuels.

N78-13234"# National Aeronautics and Space Administration.

Lyndon B. Johnson Space Center, Houston, Tex.

TRIPLE POINT DETERMINATIONS OF MONOMETHYLHYDRAZlNE AND NITROGEN TETROXlDE, 2.2 PERCENT BY WEIGHT

NITRIC OXIDE

I_ D. SMITH and P. M. DOOGE (Lockheed Electronics Co., Inc.,

Las Cruces, New Mexico) Nov. 1977 16 p refs

(NASA-RP-1013; S-475) Avail: NTIS HC A02/MF A01 CSCL

211

A series of tests was performed to ascertain the triple points

of monomethylhydrazine and nitrogen tetroxide. A laboratory

method indicated a triple point for monomethythydrazine, but tests

in a large vacuum chamber indicated that a triple point does not

occur in spacelike conditions because the mono-methylhydrazine

tends to supercool. Instead, an effective freezing point (with

agitation) was obtained. New experimental values for liquid

monomethylhydrazine vapor pressure were determined for

temperatures from 275.2 to 207.6 K. The values were used to

derive vapor pressure equations. Tentative values were obtained

for the effective freezing point of nitrogen tetroxide spacelike

conditions. Author
N78-19325"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

JET AIRCRAFT HYDROCARBON FUELS TECHNOLOGY

J. P. LONGWELL, ed. 1978 64 p Workshop held at Cleveland,

Ohio, 7-9 Jun. 1977

(NASA-CP-2033; E-9457) Avail: NTIS HC A04/MF A01 CSCL

21D

AIRCRAFT FUELS, HYDROCARBON FUELS, JET AIRCRAFT,

JET ENGINE FUELS

N78-20351"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

COMPUTER PROGRAM FOR OBTAINING THERMODYNAMIC

AND TRANSPORT PROPERTIES OF AIR AND PRODUCTS OF

COMBUSTION OF ASTM-A-1 FUEL AND AIR

S. A. HIPPENSTEELE and R. S. COLLADAY Mar. 1978 56 p

(NASA-TP-1160; E-9371) Avail: NTIS HC A04/MF A01 CSCL

21B

AIR, COMBUSTION PRODUCTS, COMPUTER PROGRAMS,

FUEL COMBUSTION, THERMODYNAMIC PROPERTIES,

TRANSPORT PROPERTIES

N78-25236"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

CATALYTIC DECOMPOSITION OF METHANOL FOR ONBOARD

HYDROGEN GENERATION

T. BRABBS Jun. 1978 47 p refs

(NASA-TP-1247; E-9472) Avail: NTIS HC A03/MF A01 CSCL

21D

CATALYTIC ACTIVITY, DECOMPOSITION, METHYL

ALCOHOL, WATER

N79-16994"# National Aeronautics and Space Administration,

Washington, D.C.

LIQUID HYDROGEN AS A PROPULSION FUEL, 1945-1959

J. L SLOOP 1978 346p refs

(NASA-SP-4404) Avail: NTIS MF A01; HC SOD CSCL 21D

A historical review is presented on the research and

development of liquid hydrogen for use as a propulsion fuel. The

document is divided into three pads: Part 1 (1945-1950); Part 2

(1950-1957); and Part 3 (1957-1958), encompassing eleven topics.

Two appendixes are included. Hydrogen Technology Through World

War 2; and Propulsion Primer, Performance Parameters and Units.

For individual titles, see N79-16995 through N79-17010.

N79-28350'# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

AXIAL JET MIXING OF ETHANOL IN CYLINDRICAL

CONTAINERS DURING WEIGHTLESSNESS

J. C. AYDELOTT Jul. t979 43 p refs

(NASA-TP-1487; E-9937) Avail: NTIS HC A03/MF A01 CSCL

2tD

CYLINDRICAL TANKS, ETHYL ALCOHOL, LIQUID ROCKET

PROPELLANTS, MIXING, WEIGHTLESSNESS

N80-14257"# National Bureau of Standards, Washington, D.C.

Thermophysical Properties Div.

THERMODYNAMIC PROPERTIES OF NITROGEN GAS DERIVED

FROM MEASUREMENTS OF SOUND SPEED

B. YOUNGLOVE and R. D. MCCARTY Washington NASA

Dec. 1979 56p refs

(NASA ORDER L-55450-A; NASA ORDER L-69159-A)

(NASA-RP-1051; NBSIR-79-1611; L-13308) Avail: NTIS HC

A04/MF A01 CSCL 07D

A virial equation of state for nitrogen was determined by use

of newly measured speed-of-sound data and existing

pressure-density-temperature data in a multiproperty-fitting

technique. The experimental data taken were chosen to optimize

the equation of state for a pressure range of 0 to 10 atm and for

a temperature range of 60 to 350 K. Comparisons are made for

thermodynamic properties calculated both from the new equation

and from existing equations of state. Author

28 PROPELLANTS AND FUELS

N80-21551"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

MECHANICAL IMPACT TESTS OF MATERIALS IN OXYGEN

EFFECTS OF CONTAMINATION

P. M. ORDIN Washington Apr. 1980 36 p refs

(NASA-TP-1571; E-047) Avail: NTIS HC A03/MF A01 CSCL

20K

ALUMINUM, CONTAMINATION, HIGH PRESSURE OXYGEN,

IMPACT TESTS, STAINLESS STEELS, TEFLON (TRADEMARK)

N81-24283"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EFFECT OF HYDROPROCESSlNG SEVERITY ON

CHARACTERISTICS OF JET FUEL FROM OSCO 2 AND

PARAHO DISTILLATES

G. M. PROK, F. J. FLORES, and G. T. SENG Jun. 1981 20 p

refs

(NASA-TP-1768; E-617) Avail: NTIS HC A02/MF A01 CSCL

21D

FUEL PRODUCTION, FUEL TESTS, HYDROGENATION, JET

ENGINE FUELS, SHALE OIL

N81-29246"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

PERFORMANCE TESTS OF A GAS BLENDING SYSTEM BASED

ON MASS-FLOW CONTROLLERS

A. EVANS, JR. Aug. 1981 16 p refs

(NASA-TP-1896; E-629) Avail: NTIS HC A02/MF A01 CSCL

21D

CHEMICAL ANALYSIS, EXHAUST GASES, MASS FLOW RATE,

MIXING, PERFORMANCE TESTS

N83-11340"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

RECENT TRENDS IN AVIATION TURBINE FUEL PROPERTIES

R. FRIEDMAN Oct. 1982 33 p refs

(NASA-TP-2056; E-1127; NAS 1.60:2056) Avail: NTIS HC

A03/MF A01 CSCL 21D

CHEMICAL PROPERTIES, HYDROCARBON FUELS, JET

ENGINE FUELS, TURBINE ENGINES

N83-16545"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

MODELING OF SPACE VEHICLE PROPELLANT MIXING

J. C. AYDELOTT Jan. 1983 27 p refs

(NASA-TP-2107; E-1275; NAS 1.60:2107) Avail: NTIS HC

A03/MFA01 CSCL211

CRYOGENIC ROCKET PROPELLANTS, DIMENSIONAL

ANALYSIS, FLUID DYNAMICS, JET MIXING FLOW, SPACECRAFT

PROPULSION

N83-22442"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

AVIATION GASOLINES AND FUTURE ALTERNATIVES

D. J. PATTERSON, ed. Washington May 1983 164 p refs

Workshop held in Cleveland, Ohio, 3-5 Feb. 1981

(NASA-CP-2267; E-1260; NAS 1.55:2267) Avail: NTIS HC

A08/MF A01 CSCL 21D

AIRCRAFT FUELS, CIVIL AVIATION, CONFERENCES, FUEL

SYSTEMS, GASOLINE

N84-23774"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

GROUP-TYPE HYDROCARBON STANDARDS FOR

HIGH-PERFORMANCE LIQUID CHROMATOGRAPHIC

ANALYSIS OF MIDDISTILLATE FUELS

D. A. OTTERSON and G. T. SENG May 1984 18 p refs

(NASA-TP-2317; E-1931; NAS 1.60:2317) Avail: NTIS HC

A02/MF A01 CSCL 21D

FUELS, HYDROCARBONS, LIQUID CHROMATOGRAPHY,

PERFORMANCE TESTS, REFRACTIVITY, STANDARDS

97
28 PROPELLANTS AND FUELS

N85-31307"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

RAPID ESTIMATION OF CONCENTRATION OF AROMATIC

CLASSES IN MIDDISTILLATE FUELS BY HIGH-PERFORMANCE

LIQUID CHROMATOGRAPHY

D. A. OTTERSON and G. T. SENG Washington Jul. 1985 16

p refs

(NASA-TP-2495; E-2376; NAS 1.60:2495) Avail: NTIS HC

A02/MF A01 CSCL 21D

FUEL TESTS, HYDROCARBON FUELS, LIQUID

CHROMATOGRAPHY, QUANTITATIVE ANALYSIS, SULFURIC

ACID

N85-35307"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SOUND SPEED MEASUREMENTS IN LIQUID OXYGEN-LIQUID

NITROGEN MIXTURES

A. J. ZUCKERWAR and D. S. MAZEL (Old Dominion Univ.) Sep.

1985 22p refs

(NASA-TP-2464; L-15965; NAS 1.60:2464) Avail: NTIS HC

AO2/MF A01 CSCL 21D

ACOUSTIC VELOCITY, FUEL CONTAMINATION, LIQUID

NITROGEN, LIQUID OXYGEN, LIQUID PROPELLANT ROCKET

ENGINES, ULTRASONICS

31

ENGINEERING (GENERAL)

Includes vacuum technology; control engineering;

engineenng; cryogenics; and fire prevention.

display

N77-I0230"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ADVANCES IN ENGINEERING SCIENCE, VOLUME 1

1976 360 p refs Presented at the 13th Ann. Meeting of The

Soc. of Eng. Sci. 1-3 Nov. 1976, Hampton, Va.; sponsored by

JIAFS and George Washington Univ. 1 Vol.

(NASA-CP-2001-VOL-1) Avail: NTIS HC A16/MF A01 CSCL

13M

BONDING, CONFERENCES, CRACK PROPAGATION, STRESS

ANALYSIS

N77-10265"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ADVANCES IN ENGINEERING SCIENCE, VOLUME 2

1976 457 p refs Presented at the 13th Ann. Meeting of Soc.

of Eng. Sci., Hampton, Va., 1-3 Nov. 1976, sponsored by JIAFS

and George Washington Univ. 4 VoI.

(NASA-CP-2001-VOL-2) Avail: NTIS HC A20/MF A0t CSCL

13M

COMPUTER PROGRAMMING, CONFERENCES, DYNAMIC

STRUCTURAL ANALYSIS, FRACTURE MECHANICS,

STRUCTURAL ENGINEERING

N77-10305"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ADVANCES IN ENGINEERING SCIENCE, VOLUME 3

1976 464 p refs Presented at the 13th Ann. Meeting of the

Soc. of Eng. Sci., Hampton, Va., 1-3 Nov. 1976; sponsored by

JIAFS and George Washington Univ. 4 Vol.

(NASA-CP-2001-VOL-3) Avail: NTIS HC A20/MF A01 CSCL

13M

ACOUSTICS, CONFERENCES, ENERGY TECHNOLOGY,

ENGINEERING, ENVIRONMENT MODELS

N77-10345"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ADVANCES IN ENGINEERING SCIENCE, VOLUME 4

1976 521 p refs Presented at 13th Ann. Meeting of Soc. of

Eng. Sci., Hampton, Va., 1-3 Nov. 1976; sponsored by JIAFS and

George Washington Univ. 4 Vol.

(NASA-CP-2001-VOL-4) Avail: NTIS HC A22/MF A01 CSCL

13M

FINITE DIFFERENCE THEORY, FINITE ELEMENT METHOD,

HEAT TRANSFER, HUMAN FACTORS ENGINEERING, SWEPT

WINGS, THREE DIMENSIONAL BOUNDARY LAYER, TRANSONIC

FLOW

N77-30273"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

PROCEEDINGS OF THE ASPE/MSFC SYMPOSIUM ON

ENGINEERING AND PRODUCTIVITY GAINS FROM SPACE

TECHNOLOGY

May 1977 279 p Conf. proc. held at Huntsville, Ala., 11-12

May 1977

(NASA-CP-2019) Avail: NTIS HC A13/MF A01 CSCL 05A

AEROSPACE ENGINEERING, CONFERENCES, ENERGY

TECHNOLOGY, TECHNOLOGY TRANSFER

N77-30296"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

TRANSFER OF MOLYBDENUM DISULFIDE TO VARIOUS

METALS

G. C. BARTON (Weber State College, Ogden, Utah) and S. V.

PEPPER Aug. 1977 17p refs

(NASA-TP-1019; E-8965) Avail: NTIS HC A02/MF A01 CSCL

07D

AUGER SPECTROSCOPY, METAL SURFACES,

MOLYBDENUM DISULFIDES, STAINLESS STEELS

N78-18252"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EVALUATION OF A LABORATORY TEST MODEL ANNULAR

MOMENTUM CONTROL DEVICE

N. J. GROOM and D. E. TERRAY Mar. 1978 23 p refs

(NASA-TP-1142; L-11968) Avail: NTIS HC A02/MF A01

CSCL 14B

ANGULAR MOMENTUM, CONTROL EQUIPMENT,

MATHEMATICAL MODELS

N78-22267"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

APPLIED ROUTH APPROXIMATION

W. C. MERRILL Apr. 1978 40 p refs

(NASA-TP-1231; E-9114) Avail: NTIS HC A03/MF A01 CSCL

12B

APPROXIMATION, FREQUENCY MEASUREMENT,

PRESSURE REGULATORS, ROCKET ENGINES, SCALE

MODELS

N80-20437"# National Aeronautics and Space Administration,

Washington, D.C.

THE APOLLO SPACECRAFT: A CHRONOLOGY VOLUME 4,

21 JANUARY 1966 - 13 JULY 1974

I. D. ERTEL, R. W. NEWKIRK, and C. G. BROOKS 1978 476

p refs

(NASA-SP-4009-VOL-4; LC-69-60008) Avail: NTIS MF A01;

SOD HC CSCL 22B

This final volume of the chronology is divided into three parts:

(1) preparation for flight, the accident, and investigation; (2)

recovery, spacecraft redefinition, and the first manned flight; and

(3) man circles the moon, the Eagle lands, and manned space

exploration. Congressional documents, official correspondence,

government and contractor reports, memoranda, working papers,

and minutes of meetings were used as primary sources. A relatively

few entries are based on press releases and newspaper and

magazine articles. A.R.H.

98
N80-23495"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

PROCEEDINGS OF THE 14TH AEROSPACE MECHANISMS

SYMPOSIUM

May 1980 327 p refs Symp. held at Hampton, Va., 1-2 May

1980; sponsored in part by Calif. Inst. of Tech. and Lockheed

Missiles and Space Co.

(NASA-CP-2127; L-13610) Avail: NTIS HC A15/MF A01

CSCL 20K

AEROSPACE ENGINEERING, CONFERENCES, MECHANICAL

ENGINEERING, SPACE TRANSPORTATION SYSTEM

N81-14138"# National Aeronautics and Space Administration.

Lyndon B. Johnson Space Center, Houston, Tex.

THE 11TH SPACE SIMULATION CONFERENCE

A. C. BOND, ed. t980 435 p refs Conf. held at Houston,

Tex., 23-25 Sep. 1980

(NASA-CP-2150; S-508) Avail: NTIS HC A19/MF A01 CSCL

22A

CONFERENCES, DEFENSE COMMUNICATIONS SYSTEM

(DCS), REUSABLE SPACECRAFT, SPACE SHUTTLE ORBITERS,

SPACE SIMULATORS, SPACECRAFT CONTAMINATION

N81-20311"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ANALYSIS AND SIMULATION OF A MAGNETIC BEARING

SUSPENSION SYSTEM FOR A LABORATORY MODEL

ANNULAR MOMENTUM CONTROL DEVICE

N. J. GROOM, C. T. WOOLLEY, and S. M. JOSHI (Vigyan Research

Associates Inc.) Mar. 1981 38 p refs

(NASA-TP-1799; L-t2403) Avail: NTIS HC A03/MF A01

CSCL 14B

ACTUATORS, COMPOSITE MATERIALS, COMPUTERIZED

SIMULATION, MAGNETIC FLUX, MAGNETIC SUSPENSION,

SPACECRAFT CONTROL

N82-19390"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECT OF VACUUM PROCESSING ON OUTGASSlNG WITHIN

AN ORBITING MOLECULAR SHIELD

R. A. OUTLAW Mar. 1982 14 p refs

(NASA-TP-1980; L-14987) Avail: NTIS HC A02/MF A01

CSCL 20H

GAS DENSITY, HYDROGEN, MOLECULAR SHIELDS,

OUTGASSING, VACUUM EFFECTS

N82-20357"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

CRYOGENIC TECHNOLOGY, PART 1

Mar. 1980 273 p refs Conf. held at Hampton, Va., 27-29

Nov. 1979

(NASA-CP-2122-PT-1; L-13547; NAS 1.55:2122-PT-1) Avail:

NTIS HC A12/MF A01 CSCL 20L

CONFERENCES, CRYOGENIC EQUIPMENT, CRYOGENIC

WIND TUNNELS, TRANSONIC WIND TUNNELS, WIND TUNNEL

APPARATUS

N82-20358"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

CRYOGENIC TECHNOLOGY, PART 2

Mar. 1980 !59 p refs Cone held at Hampton, Va., 27-29

Nov. 1979

(NASA-CP-2122-PT-2; L-13547; NAS 1.55:2122-PT-2) Avail:

NTIS HC A08/MF A01 CSCL 20L

CONFERENCES, CRYOGENIC EQUIPMENT, CRYOGENIC

WIND TUNNELS, TRANSONIC WIND TUNNELS, WIND TUNNEL

APPARATUS

31 ENGINEERING (GENERAL)

N82-23344"# National Aeronautics and Space Administration.

John F. Kennedy Space Center, Cocoa Beach, Fla.

THE 16TH AEROSPACE MECHANISMS SYMPOSIUM

May 1982 343 p refs Proceedings of conf. held at Kennedy

Space Center, Fla., 13-14 May 1982; sponsored in part by Calif.

Inst. of Technology and Lockheed Missiles and Space Co., Inc.,

Sunnyvale

(NASA-CP-2221; NAS 1.55:2221) Avail: NTIS HC A15/MF A01

CSCL 12T

ACTUATORS, FASTENERS, LARGE SPACE STRUCTURES,

LATCHES, PAYLOAD DEPLOYMENT & RETRIEVAL SYSTEM,

REMOTE MANIPULATOR SYSTEM, SPACE SHUTTLE ORBITERS,

SPACE TRANSPORTATION SYSTEM

N83-32990"# National Aeronautics and Space Administration.

Lyndon B. Johnson Space Center, Houston, Tex.

DESIGN GUIDE FOR HIGH PRESSURE OXYGEN SYSTEMS

A. C. BOND, H. O. POHL, N. H. CHAFFEE, W. W. GUY, C. S.

ALLTON, R. L. JOHNSTON, W. L. CASTNER, and J. S.

STRADLING (White Sands Missile Range) Aug. 1983 83 p

refs

(NASA-RP-1113; S-526; NAS 1.61:1113) Avail: NTIS HC

A05/MF A01 CSCL 131

A repository for critical and important detailed design data and

information, hitherto unpublished, along with significant data on

oxygen reactivity phenomena with metallic and nonmetallic

materials in moderate to very high pressure environments is

documented. This data and information provide a ready and easy

to use reference for the guidance of designers of propulsion, power,

and life support systems for use in space flight. The document is

also applicable to designs for industrial and civilian uses of high

pressure oxygen systems. The information presented herein are

derived from data and design practices involving oxygen usage at

pressures ranging from about 20 psia to 8000 psia equal with

thermal conditions ranging from room temperatures up to 500 F.

S.L.

N84-15327"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

REFRIGERATION FOR CRYOGENIC SENSORS

M. G. GASSER, ed. Washington Dec. 1983 430 p refs

Conf. held in Greenbelt, Md., 7-8 Dec. 1982

(NASA-CP-2287; REPT-83F5158; NAS 1.55:2287) Avail: NTIS

HC A19/MF A01 CSCL 20L

CONFERENCES, CRYOGENIC COOLING, REFRIGERATORS

N84-33613"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

ENGINEERING AND DESIGN PROPERTIES OF

THALLIUM-DOPED SODIUM IODIDE AND SELECTED

PROPERTIES OF SODIUM-DOPED CESIUM IODIDE

K. FORREST, C. HAEHNER, T. HESLIN, M. MAGIDA, J. UBER,

S. FREIMAN (NBS), G. HICHO (NBS), and R. POLVANI (NBS)

Sep. 1984 74 p refs

(NASA-RP-1131; NAS 1.61:1131; REPT-84F0257) Avail: NTIS

HC A04/MF A01 CSCL 20K

Mechanical and thermal properties, not available in the literature

but necessary to structural design, using thallium doped sodium

iodide and sodium doped cesium iodide were determined to be

coefficient of linear thermal expansion, thermal conductivity, thermal

shock resistance, heat capacity, elastic constants, ultimate

strengths, creep, hardness, susceptibility to subcritical crack growth,

and ingot variation of strength. These properties were measured

for single and polycrystalline materials at room temperature.

Author

99
31 ENGINEERING(ENERAL)

N86-20586"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va

GROWTH OF HIGH-QUALITY THIN-FILM GE SINGLE

CRYSTALS BY PLASMA-ENHANCED CHEMICAL VAPOR

DEPOSITION

R. A OUTLAW and P. HOPSON, JR. Feb. 1986 15 p refs

(NASA-TP-2532; L-16011; NAS 160:2532) Avail: NTIS HC

A02/MF A01 CSCL 20B

GERMANIUM, GROWTH, PLASMAS (PHYSICS), SINGLE

CRYSTALS, THIN FILMS, VAPOR DEPOSITION

32

COMMUNICATIONS AND RADAR

Includes radar; land and global communications; communications

theory; and optical communications.

N79-14275"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

DESIGN OF A VIDEO TELECONFERENCE FACILITY FOR A

SYNCHRONOUS SATELLITE COMMUNICATIONS LINK

M. D. RICHARDSON Jan. 1979 20 p refs

(NASA-TP-1376; E-9202) Avail: NTIS HC A02/MF A01 CSCL

17B

COMMUNICATION SATELLITES, DATA LINKS,

TELECONFERENCING, VIDEO COMMUNICATION

N82-15270"# Operations Research, Inc., Silver Spring, Md.

Space Engineering and Communication Systems Div.

PROPAGATION EFFECTS HANDBOOK FOR SATELLITE

SYSTEMS DESIGN: A SUMMARY OF PROPAGATION

IMPAIRMENTS ON 10 TO 100 GHZ SATELLITE LINKS WITH

TECHNIQUES FOR SYSTEM DESIGN

R. D. KAUL and R. G. WALLACE Dec 1981 423 p refs

(NASW-: 431)

(NASA-RP-1082; ORI-TR-1905) Avail: NTIS HC A18/MF A01

CSCL 14N

The major propagation effects experienced on Earth-space

communications paths in the 10 to 100 GHz frequency range.

Attenuation due to rain is dealt with in detail. For individual titles,

see N82-15271 through N82-15276.

N83-29491"# National Aeronautics and Space Administration,

Washington, D.C.

PROPAGATION EFFECTS HANDBOOK FOR SATELLITE

SYSTEMS DESIGN. A SUMMARY OF PROPAGATION

IMPAIRMENTS ON 10 TO 100 GHZ SATELLITE LINKS WITH

TECHNIQUES FOR SYSTEM DESIGN

L. J. IPPOLITO, R. D. KAUL, and R. G. WALLACE Jun. 1983

468 p refs Prepared in cooperation with Operations Research,

Inc., Silver Spring, Md.

(NASW-3644)

(NASA-RP-1082(03); NAS 1.61:1082(03); ORI-TR-1905) Avail:

NTIS HC A20/MF A01 CSCL 20N

This Propagation Handbook provides satellite system engineers

with a concise summary of the major propagation effects

experienced on Earth-space paths in the 10 to 100 GHz frequency

range. The dominant effect, attenuation due to rain, is dealt with

in some detail, in terms of both experimental data from

measurements made in the U.S. and Canada, and the mathematical

and conceptual models devised to explain the data. In order to

make the Handbook readily usable to many engineers, it has been

arranged in two parts. Chapters 2-5 comprise the descriptive part.

They deal in some detail with rain systems, rain and attenuation

models, depolarization and experimental data. Chapters 6 and 7

make up the design part of the Handbook and may be used

almost independently of the earlier chapters. In Chapter 6, the

design techniques recommended for predicting propagation effects

in Earth-space communications systems are presented. Chapter 7

addresses the questions of where in the system design process

the effects of propagation should be considered, and what

precautions should be taken when applying the propagation

results. Author

N84-13397"# National Aeronautics and Space Administration,

Washington, D.C. Dept. of Electrical Engineering.

PROPAGATION EFFECTS ON SATELLITE SYSTEMS AT

FREQUENCIES BELOW 10 GHZ, A HANDBOOK FOR

SATELLITE SYSTEMS DESIGN, 1ST EDITION

W. L. FLOCK Dec. 1983 433 p refs

(NAS7-100; JPL-956249)

(NASA-RP-1108; NAS 1.61:1108) Avail: NTIS HC A19/MF A01

CSCL 20N

Satellite communications below about 6 GHz may need to

contend with ionospheric effects, including Faraday rotation and

ionospheric scintillation, which become increasingly significant with

decreasing frequency. Scintillation is most serious in equatorial,

auroral, and polar latitudes; even the 4 to 6 GHz frequency range

turns out to be subject to scintillation to a significant degree of

equatorial latitudes. Faraday rotation, excess range or time delay,

phase advance, Doppler frequency fluctuations, and dispersion are

proportional to total electron content (TEC) or its variation along

the path. Tropospheric refraction and fading affects low angle

satellite transmissions as well as terrestrial paths. Attenuation and

depolarization due to rain become tess important with decreasing

frequency but need consideration for frequencies of about 4 GHz

and higher. Empirically derived relations are useful for estimating

the attenuation expected due to rain for particular percentages of

time. Aeronautical, maritime, and land mobile satellite services

are subject to fading due to multipath propagation. Author

N84-20735"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ANALYSIS OF RECTANGULAR MICROSTRIP ANTENNAS

M. C. BAILEY and M D. DESHPANDE (George Washington

Univ.) Mar. 1984 61 p refs

(NASA-TP-2276; L-15698; NAS 1.60:2276) Avail: NTIS HC

A04/MF A01 CSCL 17B

ANTENNA DESIGN, ANTENNA RADIATION PATTERNS,

BANDWIDTH, MICROSTRIP TRANSMISSION LINES, RESONANT

FREQUENCIES

33

ELECTRONICS AND ELECTRICAL ENGINEERING

Includes test equipment and maintainability; components, e.g.,

tunnel diodes and transistors; microminiaturization; and integrated

circuitry.

N77-30367"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

CONCEPT REPORT: MICROPROCESSOR CONTROL OF

ELECTRICAL POWER SYSTEM

E. PERRY Aug. 1977 22 p

(NASA-TP-1016; M-227) Avail: NTIS HC A02/MF A01 CSCL

09C

ELECTRIC POWER SUPPLIES, MICROPROCESSORS, REAL

TIME OPERATION

N78-11301"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

INSTRUMENT TO AVERAGE 100 DATA SETS

G. B. TUMA, A. G. BIRCHENOUGH, and W. J. RICE Oct. 1977

19p

(NASA-TP-1055; E-9159) Avail: NTIS HC A02/MF A01 CSCL

09C

ANALOG DATA, CURVE FITTING, DATA CORRELATION

100
33 ELECTRONICS AND ELECTRICAL ENGINEERING

N78-16266"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

PROCEEDINGS OF THE 1977 NASA/ISHM

MICROELECTRONICS CONFERENCE

S. V. CARUSO, comp. Nov. 1977 170 p refs Conf. held at

Huntsville, Ala., 20-21 Sep. 1977

(NASA-CP-2027) Avail: NTIS HC A08/MF A01 CSCL 09C

CONFERENCES, HYBRID CIRCUITS, MICROELECTRONICS,

TECHNOLOGICAL FORECASTING

N79-14309"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

SPACE SHUTTLE ACTIVE-POGO-SUPPRESSOR CONTROL

DESIGN USING LINEAR QUADRATIC REGULATOR

TECHNIQUES

B. LEHTINEN and C. F. LORENZ Jan. 1979 83 p refs

(NASA-TP-1217; E-9578) Avail: NTIS HC A05/MF A01 CSCL

09C

POGO EFFECTS, SPACE SHUTTLES, STRUCTURAL

VIBRATION, VIBRATION DAMPING

N79-17139"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EFFICIENCY ENHANCEMENT OF OCTAVE-BANDWIDTH

TRAVELING WAVE TUBES BY USE OF MULTISTAGE

DEPRESSED COLLECTORS

P. RAMINS and T. A. FOX Feb. 1979 29 p refs

(NASA-TP-1416; E-9749) Avail: NTIS HC A03/MF A01 CSCL

09A

ACCUMULATORS, ELECTRON BEAMS, POLARIZATION

(WAVES), TRAVELING WAVE TUBES

N79-22375"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

ANALYTICAL PREDICTION WITH MULTIDIMENSIONAL

COMPUTER PROGRAMS AND EXPERIMENTAL VERIFICATION

OF THE PERFORMANCE, AT A VARIETY OF OPERATING

CONDITIONS, OF TWO TRAVELING WAVE TUBES WITH

DEPRESSED COLLECTORS

J. A. DAYTON, JR., H. G. KOSMAHL, P. RAMINS, and N.

STANKIEWICZ May 1979 28 p refs

(NASA-TP-1449; E-9728) Avail: NTIS HC A03/MF A01 CSCL

09A

COMPUTER PROGRAMS, PERFORMANCE PREDICTION,

TRAVELING WAVE TUBES

N79-32467"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

OPTICALLY ISOLATED LOGARITHMIC NANOAMMETER

CAPABLE OF FLOATING TO 5 KILOVOLTS

J. C. STURMAN and J. C. DELAAT Washington Oct. 1979

22 p refs

(NASA-TP-1527; E-9934) Avail: NTIS HC A02/MF A01 CSCL

09C

HIGH VOLTAGES, MICROMILLIAMMETERS, OPTICAL

MEASURING INSTRUMENTS

N80-21669"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

MULTISTAGE DEPRESSED COLLECTOR WITH EFFICIENCY OF

90 TO 94 PERCENT FOR OPERATION OF A DUAL-MODE

TRAVELING WAVE TUBE IN THE LINEAR REGION

P. RAMINS and T. A FOX Washington Apr. 1980 16 p refs

(NASA-TP-1670; E-9975) Avail: NTIS HC A02/MF A01 CSCL

09A

ELECTRON BEAMS, ELECTRON ENERGY, ENERGY

CONVERSION EFFICIENCY, TRAVELING WAVE TUBES

N80-33683"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

COMPARATIVE PERFORMANCE OF HGCDTE PHOTODIODES

FOR HETERODYNE APPLICATION

H. R. KOWITZ Oct. 1980 15 p refs Presented at the

Heterodyne Systems and Technol. Conf., Williamsburg, Va., 25-27

Mar. 1980

(NASA-TP-1745; L-14019) Avail: NTIS HC A02/MF A01

CSCL 09C

HETERODYNING, LASER SPECTROSCOPY, PHOTODtODES,

QUANTUM EFFICIENCY

N81-11315"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

MODULAR INSTRUMENTATION SYSTEM FOR REAL-TIME

MEASUREMENTS AND CONTROL ON RECIPROCATING

ENGINES

W. J. RICE and A. G BIRCHENOUGH Nov. 1980 14 p refs

(NASA-TP-1757; E-455) Avail: NTIS HC A02/MF A01 CSCL

14B

COMBUSTION EFFICIENCY, ENGINE ANALYZERS, ENGINE

MONITORING INSTRUMENTS, PISTON ENGINES

N79-27400"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

DESIGN OF HIGH-PERVEANCE CONFINED-FLOW GUNS FOR

PERIODIC-PERMANENT-MAGNET-FOCUSED TUBES

N. STANKIEWICZ Jun. 1979 17 p refs

(NASA-TP-1485; E-9729) Avail: NTIS HC A02/MF A01 CSCL

09C

ELECTRON GUNS, FLOW CHARACTERISTICS, MAGNETIC

FIELDS

N81-20359"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

THREE-AXIS ELECTRON-BEAM TEST FACILITY

J. A. DAYTON, JR. and B. T. EBIHARA Mar. 1981 8 p

(NASA-TP-1836; E-582) Avail: NTIS HC A02/MF A01 CSCL

09C

AUTOMATIC TEST EQUIPMENT, AXES OF ROTATION,

CURRENT DENSITY, ELECTRON BEAMS, ELECTRONIC

EQUrPMENT TESTS, MICROWAVE TUBES

N79-28420"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EFFICIENCY ENHANCEMENT OF DUAL-MODE TRAVELING

WAVE TUBES AT SATURATION AND IN THE LINEAR RANGE

BY USE OF SPENT-BEAM REFOCUSING AND MULTISTAGE

DEPRESSED COLLECTORS

P. RAMINS andT. A. FOX Jul. 1979 26p refs

(NASA-TP-1486; E-9912) Avail: NTIS HC A03/MF A01 CSCL

09C

ACCUMULATORS, FOCUSING, TRAVELING WAVE TUBES

N81-22281"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

A MICROPROCESSOR-BASED TABLE LOOKUP APPROACH

FOR MAGNETIC BEARING LINEARIZATION

N. J. GROOM and J. B. MILLER May 1981 29 p refs

(NASA-TP-1838; L-13969) Avail: NTIS HC A03/MF A01

CSCL 131

BEARINGS, ENERGY TRANSFER, LINEARIZATION,

MAGNETIC SUSPENSION, MICROPROCESSORS, MOMENTUM

TRANSFER

101
33 ELECTRONICSANDELECTRICALENGINEERING

N81-26372"#National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

CAPACITOR TECHNOLOGIES, APPLICATIONS AND

RELIABILITY

Jun. 1981 158 p refs Proceedings of a Symp. held at

Marshall Space Flight Center, Ala, 24-25 Feb. 1981

(NASA-CP-2186; M-351) Avail: NTIS HC A08/MF A01 CSCL

09A

ACCELERATED LIFE TESTS, CAPACITORS, CONFERENCES,

ELECTRICAL PROPERTIES

N81-28352"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

ANALYTICAL PREDICTION AND EXPERIMENTAL

VERIFICATION OF PERFORMANCE AT VARIOUS OPERATING

CONDITIONS OF A DUAL-MODE TRAVELING WAVE TUBE

WITH MULTISTAGE DEPRESSED COLLECTORS

J. A. DAYTON, JR., H. G. KOSMAHL, P. RAMINS, and N

STANKIEWtCZ Jul. 1981 27 p refs

(NASA-TP-1831; E-577) Avail: NTIS HC A03/MF A01 CSCL

09C

ELECTRON BEAMS, RADIO FREQUENCY DISCHARGE,

TRAVELING WAVE TUBES

N81-30360"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

PERFORMANCE OF COMPUTER-DESIGNED SMALL-SIZED

FOUR-STAGE DEPRESSED COLLECTOR FOR OPERATION OF

DUAL-MODE TRAVELING WAVE TUBE

P. RAMINS and T A FOX Aug. 1981 14 p refs

(NASA-TP.1832; E-643) Avail: NTIS HC A02/MF A01 CSCL

09C

ACCUMULATORS, COMPUTER AIDED DESIGN, CURRENT

DISTRIBUTION, TRAVELING WAVE TUBES

N82-20402"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

THE 1981 GODDARD SPACE FLIGHT CENTER BATTERY

WORKSHOP

G. HALPERT, ed Mar. 1982 544 p Workshop held in Greenbelt,

Md., 17-19 Nov. 1981

(NASA-CP-2217; NAS 1.55:2217) Avail: NTIS HCA23/MF A01

CSCL 10C

CONFERENCES, ELECTRIC BATTERIES, ELECTROLYTES,

LITHIUM SULFUR BATTERIES, NICKEL CADMIUM BATTERIES,

NICKEL HYDROGEN BATTERIES, SPACECRAFT POWER

SUPPLIES

N82-22439"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

THREE-DIMENSIONAL RELATIVISTIC FIELD-ELECTRON

INTERACTION IN A MULTICAVITY HIGH-POWER KLYSTRON.

1: BASIC THEORY

H. G. KOSMAHL Apr. 1982 33 p refs Presented at the

Intern. Electron Devices Meeting, Washington, D.C., 11 Oct. 1971;

sponsored by IEEE; and the Solar Power Space System Workshop,

Houston, Tex., 15-18 Jan. 1979; sponsored by NASA

(NASA-TP-1992; E-1017; NAS 1.60:1992) Avail: NTIS HC

A03/MF A01 CSCL 09A

CAVITY RESONATORS, ELECTROMAGNETIC FIELDS,

ELECTRON TRAJECTORIES, KLYSTRONS, MAGNETIC FIELDS,

PARTICLE MOTION, RELATIVISTIC PARTICLES

N82-23397"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

THREE-DIMENSIONAL RELATIVISTIC FIELD-ELECTRON

INTERACTION IN A MULTICAVITY HIGH-POWER KLYSTRON.

PART 2: WORKING EQUATIONS

H. G. KOSMAHL Apr. 1982 45 p refs Presented at the

Intern. Electrons Devices Meeting, Washington, D.C, 11 Oct. 1971;

sponsored by IEEE Also presented at the Solar Power Space

System Workshop, Houston, Tex., 15-18 Jan. 1979; sponsored by

NASA. Lyndon B. Johnson Space Center

(NASA-TP-2008; E-1018; NAS 1.60:2008) Avail: NTIS HC

A03/MF A01 CSCL 09C

ELECTRON BUNCHING, ELECTRON SCATTERING,

KLYSTRONS, MAGNETIC AMPLIFIERS, RADIO FREQUENCY

DISCHARGE, RELATIVISTIC ELECTRON BEAMS

N82-25441"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

COMPUTER MODELING OF MULTIPLE-CHANNEL INPUT

SIGNALS AND INTERMODULATION LOSSES CAUSED BY

NONLINEAR TRAVELING WAVE TUBE AMPLIFIERS

N. STANKIEWICZ May 1982 26 p

(NASA-TP-1999; E-722; NAS 1.60:1999) Avail: NTIS HC

A03/MF A01 CSCL 09A

INTERMODULATION, MATHEMATICAL MODELS, SIGNAL

DISTORTION, TRAVELING WAVE TUBES

N83-25985"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EXPERIMENTAL VERIFICATION OF THE MULTISTAGE

DEPRESSED COLLECTOR DESIGN PROCEDURE FOR A

HIGH-PERVEANCE, HELIX-TYPE, TRAVELING-WAVE TUBE

J. A. DAYTON, JR., H. G. KOSMAHL, and P. RAMINS May

1983 24p refs

(NASA-TP-2162; E-1362; NAS 1.60:2162) Avail: NTIS HC

A02/MF A01 CSCL 09A

ACCUMULATORS, COMMUNICATION SATELLITES,

ELECTRONIC COUNTERMEASURES, FOCUSING, PERVEANCE,

TRAVELING WAVE TUBES

N83-35230"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

THE 1982 GODDARD SPACE FLIGHT CENTER BATTERY

WORKSHOP

G. HALPERT, ed. Aug. 1983 540 p refs The 15th Ann.

Workshop held in Greenbelt, Md., 16-18 Nov. 1982

(NASA-CP-2263; REPT-83F5181; NAS 1.55:2263) Avail: NTIS

HC A23/MF A01 CSCL 10C

LITHIUM SULFUR BATTERIES, NICKEL HYDROGEN

BATTERIES, SAFETY, SPACECRAFT POWER SUPPLIES,

STORAGE BATTERIES

N84-15394"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

PERFORMANCE OF COMPUTER-DESIGNED SMALL-SIZE

MULTISTAGE DEPRESSED COLLECTORS FOR A

HIGH-PERVEANCE TRAVELING WAVE TUBE

P. RAMINS Jan. t984 24 p refs

(NASA-TP-2248; E-1700; NAS 1.60:2248) Avail: NTIS HC

A02/MF A01 CSCL 09A

ACCUMULATORS, ELECTRODES, TRAVELING WAVE

TUBES

N84-16461"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

DEVELOPMENT OF AN INSTRUMENT FOR REAL-TIME

COMPUTATION OF INDICATED MEAN EFFECTIVE PRESSURE

W. J. RICE Jan. 1984 22 p rets

(NASA-TP-2238; E-1650; NAS 1.60:2238) Avail: NTIS HC

A02/MF A01 CSCL 14B

ELECTRONIC EQUIPMENT, ENGINE MONITORING

INSTRUMENTS, INTERNAL COMBUSTION ENGINES, REAL TIME

OPERATION

102
33 ELECTRONICSANDELECTRICALENGINEERING

N84-20758"#National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

TOPICS IN THE OPTIMIZATION OF MILLIMETER-WAVE

MIXERS

P. H. SIEGEL, A. R. KERR, and W. HWANG Mar. 1984 523 p

refs

(NASA-TP-2287; NAS 1.60:2287) Avail: NTIS HC A22/MF A01

CSCL 09C

COMPUTER PROGRAMS, MILLIMETER WAVES, MIXERS,

MULTIPLIERS, SCHOTTKY DIODES, VARACTOR DIODES

N84-20759"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

PERFORMANCE OF ALKALINE BATTERY CELLS USED IN

EMERGENCY LOCATOR TRANSMITTERS

G. A. HAYNES, S. SOKOL, W. R. MOTLEY, III, and E. L.

MCCLELLAND Mar. 1984 60 p refs

(NASA-TP-2277; L-t5496; NAS 1.60:2277) Avail: NTIS HC

A04/MF A01 CSCL 09C

ALKALINE BATTERIES, EMERGENCY LOCATOR

TRANSMITTERS, MANGANESE COMPOUNDS, ZINC

COMPOUNDS

N84-33668"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

THE 1983 GODDARD SPACE FLIGHT CENTER BATTERY

WORKSHOP

D. BAER, ed. and G. W. MORROW, ed. Washington Sep.

1984 548 p refs Workshop held in Greenbelt, Md., 15-17

Nov. 1983

(NASA-CP-2331; NAS 1.55:2331) Avail: NTIS HC A23/MF A01

CSCL 10C

ENERGY STORAGE, LIFE (DURABILITY), LITHIUM SULFUR

BATTERIES, SPACECRAFT POWER SUPPLIES

N85-13156"# National Aeronautics and Space Administration,

Washington, D.C.

PROCEDURES FOR PRECAP VISUAL INSPECTION

1984 81 p refs

(NASA-RP-1122; NAS 1.61:1122) Avail: NTIS HC A05/MF A01

CSCL 09C

Screening procedures for the final precap visual inspection of

microcircuits used in electronic system components are described

as an aid in training personnel unfamiliar with microcircuits.

Processing techniques used in industry for the manufacture of

monolithic and hybrid components are presented and imperfections

that may be encountered during this inspection are discussed.

Problem areas such as scratches, voids, adhesions, and wire

bonding are illustrated by photomicrographs. This guide can serve

as an effective tool in training personnel to perform precap visual

inspections efficiently and reliably. Author

N86-13643"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

VERIFICATION OF COMPUTER-AIDED DESIGNS OF

TRAVELING-WAVE TUBES UTILIZING NOVEL DYNAMIC

REFOCUSERS AND GRAPHITE ELECTRODES FOR THE

MULTISTAGE DEPRESSED COLLECTOR

P. RAMINS, H. G. KOSMAHL, D. A. FORCE, R. W. PALMER, and

J. A. DAYTON, JR. Oct. 1985 26 p refs

(NASA-TP-2524; E-2566; NAS 1.60:2524) Avail: NTIS HC

A03/MF A01 CSCL 09A

COMPUTER AIDED DESIGN, ELECTRIC POTENTIAL,

ELECTRODES, ELECTRON EMISSION, GRAPHITE, TRAVELING

WAVE TUBES

N86-14498"# National Aeronautics and Space Administration,

Washington, D.C.

HIGH-DENSITY DIGITAL RECORDING

F. KALIL, ed and A. BUSCHMAN, ed. (Naval Intelligence Support

Center, Suitland, Md.) Sep. 1985 319 p refs

(NASA-RP-1111; NAS 1.61:1111) Avail: NTIS HCA14/MFA01

CSCL 01C

The problems associated with high-density digital recording

(HDDR) are discussed. Five independent users of HDDR systems

and their problems, solutions, and insights are provided as guidance

for other users of HDDR systems. Various pulse code modulation

coding techniques are reviewed. An introduction to error detection

and correction head optimization theory and perpendicular

recording are provided. Competitive tape recorder manufacturers

apply all of the above theories and techniques and present their

offerings. The methodology used by the HDDR Users

Subcommittee of THIC to evaluate parallel HDDR systems is

presented. E.A.K.

N86-20678"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

DEVELOPMENT OF UHF RADIOMETER

B. M. KENDALL, H. J. C. BLUME, and A. E. CROSS Dec. 1985

58 p refs

(NASA-TP-2504; L-16006; NAS 1.60:2504) Avail: NTIS HC

A04/MF A01 CSCL 09A

MICROWAVE RADIOMETERS, OCEANS, REMOTE SENSING,

SALINITY, ULTRAHIGH FREQUENCIES

N86-21755"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

PROGRAMMABLE, AUTOMATED TRANSISTOR TEST SYSTEM

L. V. TRUONG and G. R. SUNDBURG 1986 25 p refs

Presented at the 3rd Symposium on Space Nuclear Power Systems,

Albuquerque, N. Mex., 13-16 Jan. 1986

(NASA-TP-2554; E-2768; NAS 1.60:2554) Avail: NTIS HC

A02/MF A01 CSCL 09A

BIPOLAR TRANSISTORS, FIELD EFFECT TRANSISTORS,

PERFORMANCE TESTS, SOF-I'WARE ENGINEERING

N85-31371"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md,

THE 1984 GODDARD SPACE FLIGHT CENTER BATTERY

WORKSHOP

G. W. MORROW, ed. Washington Jul. 1985 592 p refs

Workshop held in Greenbelt, Md., 13-15 Nov, 1984

(NASA ORDER S-14764-D)

(NASA-CP-2382; REPT-85B0328; NAS 1.55:2382) Avail: NTIS

HC A25/MFA01 CSCL 10C

CONFERENCES, NICKEL CADMIUM BATTERIES, NICKEL

HYDROGEN BATTERIES, SPACE STATIONS, SPACECRAFT

POWER SUPPLIES

N86-32629"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

SECONDARY-ELECTRON-EMISSION LOSSES IN MULTISTAGE

DEPRESSED COLLECTORS AND TRAVELING-WAVE-TUBE

EFFICIENCY IMPROVEMENTS WITH CARBON COLLECTOR

ELECTRODE SURFACES

P. RAMINS and B. T. EBIHARA Sep. 1986 23 p

(NASA-TP-2622; E-3062; NAS t.60:2622) Avail: NTIS HC

A02/MF A01 CSCL 09C

ACCUMULATORS, ELECTRODES, ELECTRON EMISSION,

GRAPHITE, SECONDARY EMISSION, TRAVELING WAVE

TUBES

103
34 FLUID MECHANICS AND HEAT TRANSFER

34

FLUID MECHANICS AND HEAT TRANSFER

Includes boundary layers; hydrodynamics; fluidics; mass transfer;

and ablation cooling.

N77-30413"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

LIQUID JET IMPINGEMENT NORMAL TO A DISK IN ZERO

GRAVITY Ph.D. Thesis Toledo Unlv.

T. L. LABUS Aug. 1977 118 p refs

(NASA-TP-1017; E-8668) Avail: NTIS HC A06/MF A01 CSCL

20D

DISKS (SHAPES), FLUID JETS, FREE JETS, JET

IMPINGEMENT, WEIGHTLESSNESS

N77-31441"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

REPRESENTATION OF TURBULENT SHEAR STRESS BY A

PRODUCT OF MEAN VELOCITY DIFFERENCES

W. H. BRAUN Sep. 1977 50 p refs

(NASA-TP-1029; E-9057) Avail: NTIS HC A03/MF A01 CSCL

20D

FLOW VELOCITY, SHEAR STRESS, TURBULENT BOUNDARY

LAYER, TURBULENT FLOW

N77-32431"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

MEAN VELOCITY, TURBULENCE INTENSITY, AND SCALE IN

A SUBSONIC TURBULENT JET IMPINGING NORMAL TO A

LARGE FLAT PLATE

D. R. BOLDMAN and P. F. BRINICH Sep. 1977 35 p refs

(NASA-TP-1037; E-8998) Avail: NTIS HC A03/MF A01 CSCL

20D

AERODYNAMIC NOISE, JET IMPINGEMENT, NOZZLE FLOW,

TURBULENT FLOW

N77-32432"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EFFECT OF FIN PASSAGE LENGTH ON OPTIMZATION OF

CYLINDER HEAD COOLING FINS

R. SIEGEL and R W. GRAHAM Sep. 1977 34 p refs

(NASA-TP-1054; E-9098) Avail: NTIS HC A03/MF A01 CSCL

21A

AIRCRAFT ENGINES, COOLING FINS, ENGINE DESIGN

N77-33444"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

VAPOR INGESTION IN CENTAUR LIQUID-HYDROGEN TANK

E. P. SYMONS Oct. 1977 31 p refs

(NASA-TP-1061; E-9234) Avail: NTIS HC A03/MF A01 CSCL

20D

CENTAUR PROJECT, CRYOGENIC ROCKET PROPELLANTS,

LIQUID HYDROGEN, TANKS (CONTAINERS), VAPOR JETS

N78-13371"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

CALCULATION METHODS FOR COMPRESSIBLE TURBULENT

BOUNDARY LAYERS, 1976

D. M. BUSHNELL, A. M. CARY, JR., and J. E. HARRIS 1977

146 p refs Presented at the 1976 Von Karman Inst. for Fluid

Dyn. Lecture Ser. Compressible Turbulent Boundary Layers,

Rhode-St.-Genese, Belgium, 1-5 Mar. 1976

(NASA-SP-422) Avail: NTIS HC A07/MF A01 CSCL 20D

Equations and closure methods for compressible turbulent

boundary layers are discussed. Flow phenomena peculiar to

calculation of these boundary layers were considered, along with

calculations of three dimensional compressible turbulent boundary

layers. Procedures for ascertaining nonsimilar two and three

dimensional compressible turbulent boundary layers were

appended, including finite difference, finite element, and

104

mass-weighted residual methods. For individual titles, see

N78-13372 through N78-13375.

N78-13379"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EFFECTS OF FILM INJECTION ANGLE ON TURBINE VANE

COOLING

J. W. GAUNTNER Dec. 1977 24 p refs

(NASA-TP-1095; E-9254) Avail: NTIS HC A02/MF A01 CSCL

20D

FILM COOLING, HEAT TRANSFER, TURBINE BLADES

N78-15434"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

A DESIGN HANDBOOK FOR PHASE CHANGE THERMAL

CONTROL AND ENERGY STORAGE DEVICES

W. R. HUMPHRIES and E. I. GRIGGS Nov. 1977 255 p refs

(NASA-TP-1074; M-230) Avail: NTIS HC A12/MF A01 CSCL

20D

ENERGY STORAGE, PARAFFINS, PHASE TRANSFORMATIONS, TEMPERATURE PROBES

N78-16326"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

EFFECTS OF MASS ADDITION ON BLUNT-BODY

BOUNDARY-LAYER TRANSITION AND HEAT TRANSFER

G. E. KAATTARI Jan. 1978 67 p refs

(NASA-TP-1139; A-7169) Avail: NTIS HC A04/MF A01 CSCL

20D

BLUNT BODIES, BOUNDARY LAYER TRANSITION, LAMINAR

HEAT TRANSFER, MASS TRANSFER

N78-17338"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

METHOD FOR CALCULATING CONVECTIVE HEAT-TRANSFER

COEFFICIENTS OVER TURBINE VANE SURFACES

D. J. GAUNTNER and J. SUCEC Jan. 1978 18 p refs

(NASA-TP-1134; E-9324) Avail: NTIS HC A02/MF A01 CSCL

20D

CONVECTIVE HEAT TRANSFER, HEAT TRANSFER

COEFFICIENTS, SURFACE TEMPERATURE, TURBINE BLADES,

VANES

N78-18362"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

FOREBODY AND AFTERBODY SOLUTIONS OF THE

NAVlER-STOKES EQUATIONS FOR SUPERSONIC FLOW OVER

BLUNT BODIES IN A GENERALIZED ORTHOGONAL

COORDINATE SYSTEM

P. A. GNOFFO Feb. 1978 89 p refs

(NASA-TP-1075; L-11770) Avail: NTIS HC A05/MF A01

CSCL 20D

BLUNT BODIES, COORDINATE TRANSFORMATIONS,

NAVIER-STOKES EQUATION, SUPERSONIC FLOW

N78-18363"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

INVISClD, NONADIABATIC FLOW FIELDS OVER BLUNT, SONIC

CORNER BODIES FOR OUTER PLANET ENTRY CONDITIONS

BY A METHOD OF INTEGRAL RELATIONS

P. A. GNOFFO Feb. 1978 52 p refs

(NASA-TP-1133; L-11944) Avail: NTIS HC A04/MF A01

CSCL 20D

ANGLE OF ATTACK, BLUNT BODIES, FLOW DISTRIBUTION,

INVISCID FLOW
N78-18364"# National Aeronautics and Space Administration.

Lyndon B. Johnson Space Center, Houston, Tex.

EFFECTIVE THERMAL CONDUCTIVITY DETERMINATION FOR

LOW-DENSITY INSULATING MATERIALS

S. D. WILLIAMS (Lockheed Electronics Co., Houston, Tex.) and

D. M. CURRY Feb. 1978 25 p refs

(NASA-TP-1155; S-481) Avail: NTIS HC A02/MF A01 CSCL

20D

INSULATION, LOW DENSITY MATERIALS, THERMAL

CONDUCTIVITY

N78-20463"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

APPLICATION OF A TWO-DIMENSIONAL PARABOLIC

COMPUTER PROGRAM TO PREDICTION OF TURBULENT

REACTING FLOWS

J. S. EVANS, C. J. SCHEXNAYDER, JR., and H. L. BEACH, JR.

Mar. 1978 59 p refs

(NASA-TP-1169) Avail: NTIS HC A04/MF A01 CSCL 20D

COMPUTER PROGRAMS, KINETIC ENERGY, PARABOLIC

DIFFERENTIAL EQUATIONS, TURBULENT FLOW, TWO

DIMENSIONAL FLOW

N78-21410"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

CORRELATION OF LASER VELOCIMETER MEASUREMENTS

OVER A WING WITH RESULTS OF TWO PREDICTION

TECHNIQUES

D. R. HOAD, J. F. MEYERS, W. H. YOUNG, JR., and T. P.

HEPNER Apr. 1978 66 p refs

(DA PROJ.1 L1-61102-AH-45)

(NASA-TP-1168; L-11980) Avail: NTIS HC A04/MF A01

CSCL 20D

DATA CORRELATION, LASER DOPPLER VELOCIMETERS,

PREDICTION ANALYSIS TECHNIQUES, UNSWEPT WINGS, WIND

TUNNEL TESTS

N78-22331"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

WAKE-SHOCK INTERACTION AT A MACH NUMBER OF 6

M.J. WALSH Mar. 1978 192p refs

(NASA-TP-1103; L-11904) Avail: NTIS HC A09/MF A01

CSCL 20D

MACH NUMBER, SHOCK WAVE INTERACTION, WAKES

N78-22332"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SOLUTION OF AXISYMMETRIC AND TWO-DIMENSIONAL

INVISCID FLOW OVER BLUNT BODIES BY THE METHOD OF

LINES

H. H. HAMILTON, II Apr. 1978 59 p refs

(NASA-TP-1154; L-11983) Avail: NTIS HC A04/MF A01

CSCL 20D

AXISYMMETRIC FLOW, BLUNT BODIES, INVISCID FLOW,

TWO DIMENSIONAL FLOW

N78-22333"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

COMPARISON OF TWO COMPUTER PROGRAMS BY

PREDICTING TURBULENT MIXING OF HELIUM IN A DUCTED

SUPERSONIC AIRSTREAM

Y. S. PAN, J. P. DRUMMOND, and C. R. MCCLINTON May

1978 69 p refs

(NASA-TP-1166; L-11949) Avail: NTIS HC A04/MF A01

CSCL 20D

COMPUTER PROGRAMS, DUCTED FLOW, HELIUM,

SUPERSONIC FLOW, TURBULENT MIXING

34 FLUID MECHANICS AND HEAT TRANSFER

N78-23389"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

CONFIGURATION HEATING FOR A HYPERSONIC RESEARCH

AIRPLANE CONCEPT HAVING A 70 DEC SWEPT

DOUBLE-DELTA WING

P. L. LAWING May 1978 74 p refs

(NASA-TP-1143; L-11841) Avail: NTIS HC A04/MF A01

CSCL 20D

AIRCRAFT CONFIGURATIONS, DELTA WINGS, HEAT

TRANSFER COEFFICIENTS, HYPERSONIC VEHICLES

N78-23390"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

A NUMERICAL SOLUTION OF THE NAVIER-STOKES

EQUATIONS FOR CHEMICALLY NONEQUILIBRlUM, MERGED

STAGNATION SHOCK LAYERS ON SPHERES AND

TWO-DIMENSIONAL CYLINDERS IN AIR

K. D. JOHNSTON and W. L. HENDRICKS (Lockheed Missiles

and Space Co., Huntsville, Ala.) May 1978 102 p refs

(NASA-TP-1227; M-254) Avail: NTIS HC A06/MF A01 CSCL

20D

NAVIER-STOKES EQUATION, NONEQUILIBRIUM CONDITIONS, SHOCK LAYERS

N78-26392"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

INDUCED VELOCITY FIELD OF A JET IN A CROSSFLOW

R. L. FEARN (Florida Univ., Gainesville) and R. P. WESTON May

1978 148 p refs

(NASA-TP-1087; L-11624) Avail: NTIS HC A07/MF A01

CSCL 20D

CROSS FLOW, JET EXHAUST, SUBSONIC FLOW, VELOCITY

DISTRIBUTION

N78-28373"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AERODYNAMIC HEATING IN GAPS OF THERMAL

PROTECTION SYSTEM TILE ARRAYS IN LAMINAR AND

TURBULENT BOUNDARY LAYERS

D. E. AVERY Jul. 1978 49 p refs

(NASA-TP-1187; L-12009) Avail: NTIS HC A03/MF A01

CSCL 20D

AERODYNAMIC HEAT TRANSFER, GAPS, HEAT SHIELDING,

TILES

N78-28374"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

TACT1, A COMPUTER PROGRAM FOR THE TRANSIENT

THERMAL ANALYSIS OF A COOLED TURBINE BLADE OR

VANE EQUIPPED WITH A COOLANT INSERT. 1. USERS

MANUAL

R. E. GAUGLER Aug. 1978 78 p refs

(NASA-TP-1271; E-9554) Avail: NTIS HC A05/MF A01 CSCL

21E

COMPUTER PROGRAMS, FLOW MEASUREMENT,

PRESSURE MEASUREMENT, TEMPERATURE MEASUREMENT

N78-30554"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

TURBULENT-FLOW SEPARATION CRITERIA FOR

OVEREXPANDED SUPERSONIC NOZZLES

E. L. MORRISETTE and T. J. GOLDBERG Aug. 1978 39 p

refs

(NASA-TP-1207; L-11530) Avail: NTIS HC A03/MF A01

CSCL 20D

SEPARATED FLOW, SUPERSONIC FLOW, SUPERSONIC

NOZZLES, TURBULENT FLOW

105
34 FLUID MECHANICS AND HEAT TRANSFER

N78-30555"# National Aeronautics and Space Administration.

Lyndon B. Johnson Space Center, Houston, Tex.

REINFORCED CARBON-CARBON OXIDATION BEHAVIOR IN

CONVECTIVE AND RADIATIVE ENVIRONMENTS

D. M. CURRY, K. J. JOHANSEN (Vought Corp., Dallas), and E.

W. STEPHENS Aug. 1978 31 p refs

(NASA-TP-1284; S-485) Avail: NTIS HC A03/MF A01 CSCL

20D

CARBON-CARBON COMPOSITES, PLASMA JETS, RADIANT

HEATING, THERMAL PROTECTION

N78-31384"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

DRAINING CHARACTERISTICS OF HEMISPHERICALLY

BOTTOMED CYLINDERS IN A LOW-GRAVITY ENVIRONMENT

E. P. SYMONS Aug. 1978 31 p refs

(NASA-TP-1297; E-9582) Avail: NTIS HC A03/MF A01 CSCL

20D

DRAINAGE, FLUID MECHANICS, GRAVITATIONAL EFFECTS,

WEIGHTLESSNESS

N78-32385"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

INVERSE BOUNDARY-LAYER THEORY AND COMPARISON

WITH EXPERIMENT

J. E. CARTER Sep. 1978 55 p refs

(NASA-TP-1208; L-12190) Avail: NTIS HC A04/MF A01

CSCL 20D

BOUNDARY LAYER FLOW, FINITE DIFFERENCE THEORY,

REATTACHED FLOW, SEPARATED FLOW

N78-33385"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

DIRECT MEASUREMENTS AND ANALYSIS OF SKIN FRICTION

AND COOLING DOWNSTREAM OF MULTIPLE FLUSH-SLOT

INJECTION INTO A TURBULENT MACH 6 BOUNDARY LAYER

F. G. HOWARD and A. J. STROKOWSKI Oct. 1978 112 p

refs

(NASA-TP-1176; L-11950) Avail: NTIS HC A06/MF A01

CSCL 20D

FILM COOLING, FLUID INJECTION, FRICTION

MEASUREMENT, SKIN FRICTION, TURBULENT BOUNDARY

LAYER

N79-10379"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

A SIPHON METHOD OF DETERMINING RESlSTIVITIES OF THIN

HEAT-PIPE WICKS

S. KATZOFF Oct. 1978 16 p refs

(NASA-TP-1304; L-12266) Avail: NTIS HC A02/MF A01

CSCL 20D

FLOW RESISTANCE, HEAT PIPES, SIPHONS, WICKS

N79-13305"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

CRITICAL STUDY OF HIGHER ORDER NUMERICAL METHODS

FOR SOLVING THE BOUNDARY-LAYER EQUATIONS

S. F. WORNOM Nov. 1978 55 p refs

(NASA-TP-1302; L-11860) Avail: NTIS HC AO4/MF A01

CSCL 20D

BOUNDARY LAYER EQUATIONS, FINITE ELEMENT

METHOD, PARABOLIC DIFFERENTIAL EQUATIONS

N79-14327°# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EXPERIMENTAL PERFECT-GAS STUDY OF EXPANSION-TUBE

FLOW CHARACTERISTICS

J. L. SHINN and C. G. MILLER, III Dec. 1978 88 p refs

(NASA-TP-1317; L-12407) Avail: NTIS HC A05/MF A01

CSCL 20D

EXPANSION, FLOW CHARACTERISTICS, HELIUM, TUBES

106

N79-14328"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

CHARACTERISTICS OF MACH 10 TRANSITIONAL AND

TURBULENT BOUNDARY LAYERS

R. D. WATSON Nov. 1978 324 p

(NASA-TP-1243; L-12016) Avail: NTIS HC A14/MF A01

CSCL 20D

BOUNDARY LAYER TRANSITION, FLOW CHARACTERISTICS,

MACH NUMBER, TURBULENT BOUNDARY LAYER

N79-18287"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

TRANSIENT SHUTDOWN ANALYSIS OF LOW-TEMPERATURE

THERMAL DIODES

R. J. WILLIAMS Mar. 1979 21 p refs

(NASA-TP-1369; A-7642) Avail: NTIS HC A02/MF A01 CSCL

20D

CRYOGENIC EQUIPMENT, DIODES, HEAT PIPES,

TEMPERATURE CONTROL

N79-18288"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

TACT 1: A COMPUTER PROGRAM FOR THE TRANSIENT

THERMAL ANALYSIS OF A COOLED TURBINE BLADE OR

VANE EQUIPPED WITH A COOLANT INSERT. 2,

PROGRAMMERS MANUAL

R. E. GAUGLER Jan. 1979 164 p refs

(NASA-TP-1391; E-9767) Avail: NTIS HC A08/MF A01 CSCL

20D

AXIAL FLOW TURBINES, COMPUTER PROGRAMS,

COOLING, IMPINGEMENT, TURBINE BLADES

N79-20344"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

PRESSURE AND THERMAL DISTRIBUTIONS ON WINGS AND

ADJACENT SURFACES INDUCED BY ELEVON DEFLECTIONS

AT MACH 6

L. G. KAUFMAN, II (Grumman Aerospace Corp., Bethpage, N. Y.)

and C. B. JOHNSON Mar. 1979 59 p refs

(NASA-TP-1356; L-12636) Avail: NTIS HC A04/MF A01

CSCL 01A

DEFLECTION, ELEVONS, HEAT TRANSFER, PRESSURE

DISTRIBUTION, TEMPERATURE DISTRIBUTION, WINGS

N79-20345"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

MEASURED AND PREDICTED SHOCK SHAPES AND

AERODYNAMIC COEFFICIENTS FOR BLUNTED CONES AT

INCIDENCE IN HELIUM AT MACH 20.3

R. L. CALLOWAY and N. H. WHITE Mar. 1979 74 p refs

(NASA-TP-1395; L-12058) Avail: NTIS HC A04/MF A01

CSCL 01A

AERODYNAMIC COEFFICIENTS, BLUNT BODIES, HELIUM,

ROCKET NOSE CONES, SHOCK RESISTANCE

N79-22427"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

REVIEW AND STATUS OF LIQUID-COOLING TECHNOLOGY

FOR GAS TURBINES

G. J. VANFOSSEN, JR. and F. S. STEPKA Washington Apr.

1979 31 p refs

(NASA-RP-1038; E-9517; AVRADCOM-TR-78°21) Avail: NTIS

HC A03/MF A01 CSCL 20D

A review was conducted of liquid-cooled turbine technology.

Selected liquid-cooled systems and methods are presented along

with an assessment of the current technology status and

requirements. A comprehensive bibliography is presented.

Author
N79-29467"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

CONTOURED TANK OUTLETS FOR DRAINING OF

CYLINDRICAL TANKS IN LOW-GRAVITY ENVIRONMENT

E. P. SYMONS Jul. 1979 45p

(NASA-TP-1492; E-9969) Avail: NTIS HC A03/MF A01 CSCL

20D

CYLINDRICAL TANKS, DRAINAGE, OUTLET FLOW,

PROPELLANT TANKS, TANK GEOMETRY, WEIGHTLESSNESS

N79-29468"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

TWO-PHASE CHOKED FLOW OF CRYOGENIC FLUIDS IN

CONVERGING-DIVERGING NOZZLES

R. J. SIMONEAU and R. C. HENDRICKS Jul. 1979 83 p refs

(NASA-TP-1484; E-9659) Avail: NTIS HC A05/MF A01 CSCL

20D

CHOKES (RESTRICTIONS), CONVERGENT-DIVERGENT

NOZZLES, CRYOGENIC FLUIDS, TWO PHASE FLOW

N79-30516"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

DESCRIPTION AND ORBIT DATA OF VARIABLE-CONDUCTANCE HEAT-PIPE SYSTEM FOR THE COMMUNICATIONS

TECHNOLOGY SATELLITE

L. GEDEON Aug. 1979 23 p refs

(NASA-TP°1465; E-9880) Avail: NTIS HC A02/MF A01 CSCL

20D

COMMUNICATIONS TECHNOLOGY SATELLITE, HEAT PIPES,

TEMPERATURE CONTROL

N79-30518"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

THE USE OF COMPUTER-GENERATED COLOR GRAPHIC

IMAGES FOR TRANSIENT THERMAL ANALYSIS

C. L. W. EDWARDS, F. T. MEISSNER, and J. B. HALL Jul.

1979 47 p

(NASA-TP-1455; L-12779) Avail: NTIS HC A03/MF A01

CSCL 20D

AERODYNAMIC HEATING, COMPUTER GRAPHICS,

HYPERSONIC AIRCRAFT, IMAGING TECHNIQUES

N79-32500"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

VELOCITY FIELD OF A ROUND JET IN A CROSS FLOW FOR

VARIOUS JET INJECTION ANGLES AND VELOCITY RATIOS

R. L. FEARN (Florida Univ., Gainesville) and R. P. WESTON Oct.

1979 134 p refs

(NASA-TP-1506; L-12775) Avail: NTIS HC A07/MF A01

CSCL 20D

AIR JETS, CROSS FLOW, GAS INJECTION, VELOCITY

DISTRIBUTION, WIND TUNNEL TESTS

N79-33438"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SURVEY AND BIBLIOGRAPHY ON ATTAINMENT OF LAMINAR

FLOW CONTROL IN AIR USING PRESSURE GRADIENT AND

SUCTION, VOLUME I

D. M. BUSHNELL and M. H TUTTLE Sep. 1979 346 p

(NASA-RP-1035; L-12528) Avail: NTIS HC A15/MF A01

CSCL 20D

A survey was conducted and a bibliography compiled on

attainment of laminar flow in air through the use of favorable

pressure gradient and suction. This report contains the survey,

summaries of data for both ground and flight experiments, and

abstracts of referenced reports. Much early information is also

included which may be of some immediate use as background

material for LFC applications. G.Y.

34 FLUID MECHANICS AND HEAT TRANSFER

N79-33441"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

A HYBRIDIZED METHOD FOR COMPUTING

HIGH-REYNOLDS-NUMBER HYPERSONIC FLOW ABOUT

BLUNT BODIES

K. J. WEtLMUENSTER and H. H. HAMILTON, II Washington

Oct. 1979 49 p refs

(NASA-TP-1497; L-12946) Avail: NTIS HC A03/MF A01

CSCL 01A

BLUNT BODIES, FINITE DIFFERENCE THEORY,

HYPERSONIC FLOW, REYNOLDS NUMBER, VISCOUS FLOW

N80-13402"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AEROTHERMAL PERFORMANCE OF RADIATIVELY AND

ACTIVELY COOLED PANEL AT MACH 6.6

C. P. SHORE and I. WEINSTEIN Dec. 1979 42 p refs

(NASA-TP-1595; L-13355) Avail: NTIS HC A03/MF A01

CSCL 20D

AERODYNAMIC HEATING, AEROTHERMODYNAMICS,

AIRFRAMES, COOLING SYSTEMS, HYPERSONIC AIRCRAFT

N80-15361"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio,

COMPUTER PROGRAM FOR GENERATING INPUT FOR

ANALYSIS OF IMPINGEMENT-COOLED, AXIAL-FLOW TURBINE

BLADE

D. ROSENBAUM Jan. 1980 57 p refs Prepared in cooperation

with Army Aviation Research and Development Command,

Cleveland, Ohio

(NASA-TP-1603; AVRADCOM-TR-79-34) Avail: NTIS HC

A04/MF A01 CSCL 20D

AIR COOLING, AXIAL FLOW TURBINES, COMPUTER

PROGRAMS, JET IMPINGEMENT, TURBINE BLADES

N80-17397"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EFFECTS OF A CERAMIC COATING ON METAL

TEMPERATURES OF AN AIR-COOLED TURBINE VANE

H. J. GLADDEN and C. H. LIEBERT Feb. 1980 29 p refs

(NASA-TP-1598; E-167) Avail: NTIS HC A03/MF A01 CSCL

20D

AIR COOLING, CERAMICS, SURFACE TEMPERATURE,

THERMAL CONTROL COATINGS, TURBINE BLADES

N80-17398"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

VOLUME-ENERGY PARAMETERS AND TURBULENT-FLOW

DENSITY FLUCTUATIONS

R. C. HENDRICKS Jan. 1980 28 p refs

(NASA-TP-1585; E-127) Avail: NTIS HC AO3/MF A0t CSCL

20D

DENSITY DISTRIBUTION, GIBBS FREE ENERGY,

TURBULENT FLOW, VOLUME

N80-20527"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

PROGRESS IN TURBULENCE MODELING FOR COMPLEX

FLOW FIELDS INCLUDING EFFECTS OF COMPRESSIBILITY

D. C, WILCOX (DCW Industries, Inc., Studio City, Calif.) and M

W. RUBESIN Washington Apr. 1980 73 p refs

(NASA-TP-1517; A-7916) Avail: NTIS HC A04/MF A01 CSCL

20D

COMPRESSIBLE FLOW, FLOW DISTRIBUTION,

MATHEMATICAL MODEt.S, TURBULENT FLOW

107
34 FLUID MECHANICS AND HEAT TRANSFER

N80-21702"# National Aeronautics and Space _dministration.

Langley Research Center, Hampton, Va.

VELOCITY-SPLIT NAVIER-STOKES SOLUTION PROCEDURE

FOR INCOMPRESSIBLE HIGH REYNOLDS NUMBER EXTERNAL

FLOWS

D. L. DWOYER Washington Apr. 1980 36 p refs

(NASA-TP-1655; L-13343) Avail: NTIS HC A03/MF A01

CSCL 20D

COMPUTATIONAL FLUID DYNAMICS, INCOMPRESSIBLE

FLOW, NAVIER-STOKES EQUATION, VISCOUS FLOW

N80-22633"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

STATUS OF LINEAR BOUNDARY-LAYER STABILITY AND THE

E TO THE NTH METHOD, WITH EMPHASIS ON SWEPT-WING

APPLICATIONS

J. N HEFNER and D. M. BUSHNELL Apr. 1980 50 p refs

(NASA-TP-1645; L-13313) Avail: NTIS HC A03/MF A01

CSCL 20D

BOUNDARY LAYER STABILITY, LAMINAR FLOW,

LOGARITHMS, PERTURBATION THEORY, SWEPT WINGS,

TRANSITION PROBABILITIES

N80-23600"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

MEASURED AND PREDICTED SHOCK SHAPES AND

AERODYNAMIC COEFFICIENTS FOR BLUNTED CONES AT

INCIDENCE IN AIR AT MACH 5.9

R L. CALLOWAY and N. H WHITE May 1980 70 p refs

(NASA-TP-1652; L-13429) Avail: NTIS HC A04/MF A01

CSCL 20D

AERODYNAMIC COEFFICIENTS, BLUNT BODIES,

HYPERSONtCS, NOSE CONES, NUMERICAL ANALYSIS,

PERFORMANCE PREDICTION, SHOCK WAVES, SPACECRAFT

CONFIGURATIONS

N80-24577"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EXTENSION OF SIMILARITY TEST PROCEDURES TO COOLED

ENGINE COMPONENTS WITH INSULATING CERAMIC

COATINGS

H. J. GLADDEN May 1980 16 p refs

(NASA-TP-1615; E-337) Avail: NTIS HC A02/MF A01 CSCL

20D

AIR COOLING, CERAMIC COATINGS, ENGINE PARTS, GAS

TURBINE ENGINES, HEAT TRANSFER, SIMILARITY THEOREM

N80-25588"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

PROCEEDINGS OF THE AERO-OPTICS SYMPOSIUM ON

ELECTROMAGNETIC WAVE PROPAGATION FROM AIRCRAFT

Apr. 1980 666 p refs Symp. held at Moffett Field, Calif.,

14-15 Aug. 1979 Sponsored in part by AFWL

(NASA-CP-2121: A-8090) Avail: NTIS HC A99/MF A01 CSCL

20D

AERODYNAMICS, CONFERENCES, ELECTROMAGNETIC

WAVE TRANSMISSION, TURBULENCE, WAVE PROPAGATION

N80-25615"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECTS OF VARIOUS ASSUMPTIONS ON THE CALCULATED

LIQUID FRACTION IN ISENTROPIC SATURATED EQUILIBRIUM

EXPANSIONS

J. W. BURSIK (Renssalaer Polytechnic Inst., Troy, N.Y.) and R.

M. HALL Jun. 1980 33 p refs

(NASA-TP-1682; L-13437) Avail: NTIS HC A03/MF A01

CSCL 20D

CRYOGENIC WIND TUNNELS, GAS EXPANSION,

NITROGEN

108

N80-26622"# National Aeronautics and Space Administration,

Langley Research Center, Hampton, Va.

NOISE REDUCTION IN A MACH 5 WIND TUNNEL WITH A

RECTANGULAR ROD-WALL SOUND SHIELD

T. R. CREEL, JR., J. W. KEYES, and I. E. BECKWtTH Jun.

1980 82 p refs

(NASA-TP-1672; L-13451) Avail: NTIS HC A05/MF A01

CSCL 20D

BOUNDARY LAYER TRANSITION, NOISE MEASUREMENT,

NOISE REDUCTION, SUPERSONIC WIND TUNNELS, WIND

TUNNEL TESTS

N80-32692"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AEROTHERMAL ANALYSIS OF A WlNG-ELEVON COVE WITH

VARIABLE LEAKAGE

R. L. HUNT Washington Sap. 1980 44 p refs

(NASA-TP-1703; L-13751) Avail: NTIS HC A03/MF A01

CSCL 20D

BOUNDARY LAYER FLOW, CONVECTIVE HEAT TRANSFER,

ELEVONS, MATHEMATICAL MODELS, REENTRY EFFECTS,

SATELLITE CONFIGURATIONS, SPACE SHUTTLE ORBITERS,

WINGS

N80-33719'# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

CALCULATION OF LAMINAR HEATING RATES ON

THREE-DIMENSIONAL CONFIGURATIONS USING THE

AXlSYMMETRIC ANALOGUE

H. H. HAMILTON, II Sep. 1980 80 p refs

(NASA-TP-1698; L-13748) Avail: NTIS HC A05/MF A01

CSCL 20D

AXISYMMETRIC FLOW, BOUNDARY LAYER EQUATIONS,

COMPUTATION, LAMINAR HEAT TRANSFER, THREE

DIMENSIONAL BOUNDARY LAYER

N81-12356"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AN IMPROVED VISCOUS CHARACTERISTICS ANALYSIS

PROGRAM

R. V. JENKINS Nov. 1978 158 p refs

(NASA-TP-1289; L-t2320) Avail: NTIS HC A08/MF A01

CSCL 20D

COMPUTER PROGRAMS, DATA CONVERSION ROUTINES,

FLOW DISTRIBUTION, FORTRAN, SUBROUTINES, SUPERSONIC

COMBUSTION

N81-12361'# National Aeronautics and Space Administration.

Dryden (Hugh L.) Flight Research Center, Edwards, Calif.

IN-FLIGHT BOUNDARY-LAYER MEASUREMENTS ON A

HOLLOW CYLINDER AT A MACH NUMBER OF 3.0

R. D. QUINN and L. GONG Nov. 1980 52 p refs

(NASA-TP-1764; H-1101) Avail: NTIS HC A04/MF A01 CSCL

20D

CYLINDRICAL BODIES, HEAT TRANSFER COEFFICIENTS,

MACH NUMBER, STATIC PRESSURE

N81-13303"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EVALUATION OF FLOW QUALITY IN TWO LARGE NASA WIND

TUNNELS AT TRANSONIC SPEEDS

W. D. HARVEY, P. C. STAINBACK, and F. K. OWEN (COMPLERE

Inc., Palo Alto, Calif.) Dec. 1980 76 p refs

(NASA-TP-1737; L-13448) Avail: NTIS HC A05/MF A01

CSCL 20D

AERODYNAMICS, FLOW VELOCITY, FREE FLOW,

PRESSURE OSCILLATIONS, WIND TUNNELS
N81-15237"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AEROTHERMAL ENVIRONMENT IN CHORDWlSE GAPS

BETWEEN SPLIT ELEVONS AT MACH 8.8

L.R. HUNT Dec. 1980 45p refs

(NASA-TP-t783; L-14076) Avail: NTIS HC A03/MF A01

CSCL 20D

AERODYNAMIC HEATING, AEROTHERMODYNAMICS,

ELEVONS, GAPS, REENTRY PHYSICS, WIND TUNNEL TESTS

N81-16417"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

CAPILLARY AND ACCELERATION WAVE BREAKUP OF LIQUID

JETS IN AXIAL-FLOW AIRSTREAMS

R. D. INGEBO Jan. 1981 13 p refs

(NASA-TP-179t; E-537) Avail: NTIS HC A02/MF A01 CSCL

20D

AXIAL FLOW, CAPILLARY WAVES, FLUID JETS, FUEL

INJECTION, LIQUID ATOMIZATION

N81-23410"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

MEAN-FLOW AND TURBULENCE MEASUREMENTS IN THE

VICINITY OF THE TRAILING EDGE OF AN NACA (63 SUB 1)-012

AIRFOIL

J. C. YU Washington May 1981 45 p refs

(NASA-TP-1845; L-t3959) Avail: NTIS HC A03/MF A01

CSCL 20D

AIRFOILS, INCOMPRESSIBLE FLOW, NEAR WAKES,

REYNOLDS STRESS, TRAILING EDGES, TURBULENT

BOUNDARY LAYER

N81-24387"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

SOME FLOW PHENOMENA ASSOCIATED WITH ALIGNED,

SEQUENTIAL APERTURES WITH BORDA-TYPE INLETS

R. C. HENDERICKS and T. T. STETZ May 1981 63 p refs

(NASA-TP-1792; E-479) Avail: NTIS HC A04/MF A01 CSCL

20D

BOUNDARY LAYER SEPARATION, FLOW VISUALIZATION,

INLET PRESSURE, SEPARATED FLOW

N81-24388"# National Aeronautics and Space Administration,

Lewis Research Center, Cleveland, Ohio.

FORCED AND NATURAL CONVECTION IN LAMINAR-JET

DIFFUSION FLAMES

J. B. HAGGARD, JR. Jun. 1981 24 p refs

(NASA-TP-1841; E-487) Avail: NTIS HC A02/MF A01 CSCL

20D

CONVECTION, DIFFUSION FLAMES, GRAVITATION THEORY,

JET FLOW, LAMINAR FLOW

N81-28389"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

DEPRESSURIZATION AND TWO-PHASE FLOW OF WATER

CONTAINING HIGH LEVELS OF DISSOLVED NITROGEN GAS

R. J. SIMONEAU Jul. 1981 46 p refs

(NASA-TP-1839; E-216) Avail: NTIS HC A03/MF A01 CSCL

20D

CRITICAL FLOW, DISSOLVED GASES, LIQUID NITROGEN,

ORIFICE FLOW, PRESSURE REDUCTION, TWO PHASE FLOW

N81-29384"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

INFLUENCE OF THERMAL BOUNDARY CONDITIONS ON HEAT

TRANSFER FROM A CYLINDER IN CROSS FLOW

S. S. PAPELL Aug. 1981 10 p refs

(NASA-TP-1894; E-627) Avail: NTIS HC A02/MF A01 CSCL

20D

CROSS FLOW, CYLINDRICAL BODIES, HEAT TRANSFER

COEFFICIENTS, STAGNATION POINT, THERMAL BOUNDARY

LAYER

34 FLUID MECHANICS AND HEAT TRANSFER

N81-31509"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

GORTLER VORTICES AND TRANSITION IN WALL BOUNDARY

LAYERS OF TWO MACH 5 NOZZLES

I. E. BECKWITH and B. B. HOLLEY Aug. 1981 72 p refs

(NASA-TP-1869; L-14332) Avail: NTIS HC A04/MF A01

CSCL 20D

BOUNDARY LAYER FLOW, REYNOLDS NUMBER, VORTICES,

WIND TUNNEL NOZZLES

N81-32418"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SIMULATION OF IDEAL-GAS FLOW BY NITROGEN AND OTHER

SELECTED GASES AT CRYOGENIC TEMPERATURES

R. M. HALL and J. B. ADCOCK Sep. 1981 51 p refs

(NASA-TP-1901; L-14587) Avail: NTIS HC A03/MF A01

CSCL 20D

CRYOGENIC WIND TUNNELS, GAS FLOW, IDEAL GAS,

NITROGEN, REAL GASES, TRANSONIC WIND TUNNELS

N82-11391'# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AMPLIFIED CROSSFLOW DISTURBANCES IN THE LAMINAR

BOUNDARY LAYER ON SWEPT WINGS WITH SUCTION

J. R. DAGENHART Nov. 1981 90 p refs

(NASA-TP-1902; L-t4423) Avail: NTIS HC A05/MF A01

CSCL 20D

BOUNDARY LAYER CONTROL, CROSS FLOW, FLOW

DISTORTION, LAMINAR BOUNDARY LAYER, SUCTION, SWEPT

WINGS

N82-13383"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AERODYNAMIC HEATING ON THE CORRUGATED SURFACE

OF A 10,2 DEC HALF-ANGLE BLUNTED CONE AT MACH 6.7

I. WEINSTEIN, D. E. AVERY, and L. R. HUNT Dec. 1981 45 p

refs

(NASA-TP-1928; L-14679) Avail: NTIS HC A03/MF A01

CSCL 20D

AERODYNAMIC HEATING, BLUNT BODIES, CONES,

CORRUGATED PLATES, HEAT RESISTANT ALLOYS, THERMAL

PROTECTION

N82-20467"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

FLOW THROUGH ALIGNED SEQUENTIAL ORIFICE TYPE

INLETS

R. C. HENDRICKS and T. T. STETZ Mar. 1982 53 p refs

(NASA-TP-1967; Eo682; NAS 1.60:1967) Avail: NTIS HC

A04/MF A01 CSCL 20D

CHOKES (FUEL SYSTEMS), FLOW VELOCITY, ORIFICE

FLOW, PRESSURE MEASUREMENT, SEALS (STOPPERS),

SEPARATED FLOW

N82-23473"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

COMPUTATIONAL ASPECTS OF HEAT TRANSFER IN

STRUCTURES

H. M. ADELMAN, Comp. 1982 554 p refs Symp. held at

Hampton, Va., 3-5 Nov. 1981; sponsored by NASA, George

Washington Univ., and Old Dominion Univ.

(NASA-CP-2216; L-15108; NAS 1.55:2216) Avail: NTIS HC

A24/MF A01 CSCL 20D

AERODYNAMIC HEATING, COMPUTATION, HEAT

TRANSFER, LARGE SPACE STRUCTURES, MATHEMATICAL

MODELS, REENTRY EFFECTS, SPACE SHUTTLE ORBITERS,

SPACECRAFT STRUCTURES, STRUCTURAL ANALYSIS,

THERMAL CONDUCTIVITY

109
34 FLUID MECHANICS AND HEAT TRANSFER

N82-30498"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

FLOW VISUALIZATION STUDY OF THE HORSESHOE VORTEX

IN A TURBINE STATOR CASCADE

R. E. GAUGLER and L. M. RUSSELL Jun. 1982 33 p refs

(NASA-TP-1884; E-915; NAS 1.60:1884) Avail: NTIS HC

AO3/MF A01 CSCL 20D

CASCADE FLOW, STATORS, TURBINES, TWO DIMENSIONAL

FLOW, VORTICES

N82-31646"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

STUDIES OF IMPLICIT AND EXPLICIT SOLUTION TECHNIQUES

IN TRANSIENT THERMAL ANALYSIS OF STRUCTURES

H. M. ADELMAN, R. T, HAFTKA, and J. C. ROBINSON Aug.

1982 47 p refs

(NASA-TP-2038; L-15245; NAS 1.60:2038) Avail: NTIS HC

A03/MF A01 CSCL 20D

AEROSPACE VEHICLES, ALGORITHMS, ANALYSIS

(MATHEMATICS), HEAT SHIELDING, HEAT TRANSFER,

STRUCTURAL ANALYSIS

N83-12360"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

FILM-COOLING EFFECTIVENESS WITH DEVELOPING

COOLANT FLOW THROUGH STRAIGHT AND CURVED

TUBULAR PASSAGES

S. S. PAPELL, C. R. WANG, and R. W, GRAHAM Nov. 1982

21 p refs

(NASA-TP.2062; E-1206; NAS 1.60:2062) Avail: NTIS HC

A02/MF A01 CSCL 20D

COOLANTS, FILM COOLING, PASSAGEWAYS, TURBINE

BLADES, WALL TEMPERATURE

N83-16674"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

FLOW IN A TORSIONALLY OSCILLATING FILLED CYLINDER

C. F. SCHAFER Jan. 1983 20 p refs

(NASA-TP-2115; NAS 1.602115) Avail: NTIS HC A02/MF A01

CSCL 20D

CIRCULAR CYLINDERS, CYLINDRICAL SHELLS, FLOW

CHARACTERISTICS, LIQUID FILLED SHELLS, MIXING,

OSCILLATIONS

N83-16675"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

PRESSURES, FORCES, MOMENTS AND SHOCK SHAPES FOR

A GEOMETRICALLY MATCHED SPHERE-CONE AND

HYPERBOLOID AT MACH 20.3 IN HELIUM

R. L. CALLOWAY Jan. 1983 73 p refs

(NASA-TP-2100; L-15499; NAS 1.60:2100) Avail: NTIS HC

A04/MF A01 CSCL 20D

AERODYNAMIC FORCES, ATMOSPHERIC ENTRY, HELIUM,

HYPERBOLAS, PRESSURE DISTRIBUTION, SPHERES,

STABILITY DERIVATIVES

N83-16680"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

MECHANICS OF LIQUID HELIUM IN A PARTIALLY FILLED

ROTATING DEWAR IN LOW GRAVITY WITH APPLICATION TO

GRAVITY PROBE-B

C. F. SCHAFER and S. A. LOWRY Jan. 1983 45 p refs

(NASA-TP-2124; NAS 1.60:2124) Avail: NTIS HC A03/MF A01

CSCL 20D

ASYMMETRY, FLUID MECHANICS, GRAVITY PROBE B,

LIQUID HELIUM, ROTATING FLUIDS

110

N83-20031"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

STUDIES OF SIDEWALL BOUNDARY LAYER IN THE LANGLEY

0.3 METER TRANSONIC CRYOGENIC TUNNEL WITH AND

WITHOUT SUCTION

A. V. MURTHY, C. B. JOHNSON, E. J. RAY, P. L. LAWING, and

J. J. THIBODEAUX Mar. 1983 50 p refs

(NASA-TP-2096; L-15437; NAS 1.60:2096) Avail: NTIS HC

A03/MF A01 CSCL 20D

BOUNDARY LAYER CONTROL, CRYOGENIC WIND

TUNNELS, MACH NUMBER, REYNOLDS NUMBER, THICKNESS

N83-20032"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

REDUCTION METHODS FOR NONLINEAR STEADY-STATE

THERMAL ANALYSIS

A. K, NOOR, C. D, BALCH, and M. A. SHIBUT (George Washington

Univ,, Hampton, Va.) Mar. 1983 48 p refs

(NASA-TP-2098; L-15501; NAS t.60:2098) Avail: NTIS HC

AO3/MF A01 CSCL 20D

FINITE ELEMENT METHOD, GALERKIN METHOD,

NONLINEAR EQUATIONS, TEMPERATURE DISTRIBUTION,

TEMPERATURE EFFECTS

N83-22546"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio,

STOCHASTIC DIFFERENTIAL EQUATIONS AND TURBULENT

DISPERSION

P, A. DURBIN Apr. 1983 72 p refs

(NASA-RP-1103; E-1425; NAS 1.61:1103) Avail: NTIS HC

A04/MF A01 CSCL 20D

Aspects of the theory of continuous stochastic processes that

seem to contribute to an understanding of turbulent dispersion

are introduced and the theory and philosophy of modelling turbulent

transport is emphasized. Examples of eddy diffusion examined

include shear dispersion, the surface layer, and channel flow.

Modeling dispersion with finite-time scale is considered including

the Langevin model for homogeneous turbulence, dispersion in

nonhomogeneous turbulence, and the asymptotic behavior of the

Langevin model for nonhomogeneous turbulence. A.R.H.

N83-24800"# National Bureau of Standards, Boulder, Colo.

Thermophysical Properties Div.

TRANSPORT PROPERTIES OF OXYGEN

H. M RODER Apr. 1983 86p refs

(NASA ORDER C-32369-C)

(NASA-RP-1102; NAS 1.61:1102; NBSIR-82-1672) Avail: NTIS

HC A05/MF A01 CSCL 20D

Tables of viscosity, thermal conductivity, and thermal diffusivity

of oxygen as a function of temperature and pressure from the

triple point to 320 K and at pressures to 100 MPa are presented.

Auxiliary tables in engineering units are also given. Viscosity and

thermal conductivity are calculated from published correlations.

Density and specific heat at constant pressure, required to calculate

thermal diffusivity, are obtained from an equation of state. The

Prandtl number can be obtained quite easily from the values

tabulated. S.L.

N83-24808"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

CALCULATION OF INVISCID FLOW OVER SHUTTLE-LIKE

VEHICLES AT HIGH ANGLES OF ATTACK AND COMPARISONS

WITH EXPERIMENTAL DATA

K. J. WEILMUENSTER and H. H. HAMILTON, II May 1983 90

p refs

(NASA-TP-2103; L-15518; NAS 1.60:2103) Avail: NTIS HC

A05/MF A01 CSCL 20D

ANGLE OF ATTACK, INVISCID FLOW, SPACE SHUTTLES,

SPACECRAFT CONFIGURATIONS, THREE DIMENSIONAL

FLOW
N83-28378"# National Aeronautics and Space Administration,

Langley Research Center, Hampton, Va.

EFFECTS OF FLOW SEPARATION AND COVE LEAKAGE ON

PRESSURE AND HEAT-TRANSFER DISTRIBUTIONS ALONG A

WlNG-COVE-ELEVON CONFIGURATION AT MACH 6.9

W. D. DEVEIKIS Jun. 1963 96 p refs

(NASA-TP-2127; L-15513; NAS 1.60:2127) Avail: NTIS HC

A05/MF A01 CSCL 20D

CHANNEL FLOW, HEAT TRANSFER, PRESSURE

DISTRIBUTION, SEPARATED FLOW, WIND TUNNEL TESTS,

WINGS

N83-34229"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

FREE-STREAM NOISE AND TRANSITION MEASUREMENTS ON

A CONE IN A MACH 3.5 PILOT LOW-DISTURBANCE TUNNEL

I. E. BECKWITH, T. R. CREEL, JR., F. J. CHEN (Systems and

Applied Sciences Corp.), and J. M. KENDALL (JPL) Sep. 1983

70 p refs

(NASA-TP-2180; L-15610; NAS 1.60:2180) Avail: NTIS HC

AO4/MF A01 CSCL 20D

BOUNDARY LAYER TRANSITION, MACH NUMBER, NOISE

(SOUND), SUPERSONIC WIND TUNNELS

N83-34232"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

THREE-DIMENSIONAL TURBULENT-MIXING-LENGTH MODELING FOR DISCRETE-HOLE COOLANT INJECTION INTO A

CROSSFLOW

C. R. WANG andS. S. PAPELL Sep. 1983 16p refs

(NASA-TP-2200; E-1497; NAS 1.60:2200) Avail: NTIS HC

A02/MF A01 CSCL 20D

ENGINE COOLANTS, FILM COOLING, MIXING LENGTH FLOW

THEORY, TEMPERATURE EFFECTS, THREE DIMENSIONAL

FLOW, TURBULENCE

N84-10504"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

PRESSURE AND HEATING-RATE DISTRIBUTIONS ON A

CORRUGATED SURFACE IN A SUPERSONIC TURBULENT

BOUNDARY LAYER

J. W. SAWYER Nov. 1977 84 p refs

(NASA-TP-1024; L-11732; NAS 1.60:1024) Avail: NTIS HC

A05/MF A01 CSCL 20D

CORRUGATED PLATES, HEATING, PRESSURE

DISTRIBUTION, SUPERSONIC BOUNDARY LAYERS,

TURBULENT BOUNDARY LAYER

N84-13500"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

THE DISTURBANCE FLOW FIELD PRODUCED BY AN

EVOLVING VORTEX

T. B. GATSKI Dec. 1983 35 p refs

(NASA-TP-2245; L-15670; NAS t.60:2245) Avail: NTIS HC

A03/MF A01 CSCL 20D

SHEAR FLOW, VISCOUS FLOW, VORTICES

N84-15427"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

LIQUID MANAGEMENT IN LOW GRAVITY USING BAFFLED

ROTATING CONTAINERS

R. F. GANS Jan. 1984 24 p refs

(NASA-TP-2263; NAS 1.60:2263) Avail: NTIS HC A02/MF A01

CSCL 20D

BAFFLES, CYLINDRICAL SHELLS, FLUID MANAGEMENT,

LIQUID FILLED SHELLS, REDUCED GRAVITY, ROTATING

CYLINDERS

34 FLUID MECHANICS AND HEAT TRANSFER

N84-17525"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

HOT-FLOW TESTS OF A SERIES OF 10-PERCENT-SCALE

TURBOFAN FORCED MIXING NOZZLES

V. L. HEAD, L. A. POVINELLI, and W. H. GERSTENMAIER Jan.

1984 95p refs

(NASA-TP-2268; E-1746; NAS 1.60:2268) Avail: NTIS HC

A05/MF A01 CSCL 20D

MIXING LENGTH FLOW THEORY, PRESSURE

MEASUREMENT, STATIC PRESSURE, TURBOFAN ENGINES

N84-17534"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

CORRELATIONS OF SUPERSONIC BOUNDARY-LAYER

TRANSITION ON CONES INCLUDING EFFECTS OF LARGE

AXIAL VARIATIONS IN WIND-TUNNEL NOISE

F, J. CHEN (Systems and Applied Sciences Corp.), I. E. BECKWITH,

and T. R. CREEL, JR. Jan. 1984 56 p refs

(NASA-TP-2229; NAS 1.60:2229; L-15669) Avail: NTIS HC

A04/MF A01 CSCL 20D

AERODYNAMIC NOISE, BOUNDARY LAYER TRANSITION,

CONES, MACH NUMBER, WIND TUNNELS

N84-19741"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EXPERIMENTAL AND THEORETICAL DEPOSITION RATES

FROM SALT-SEEDED COMBUSTION GASES OF A MACH 0.3

BURNER RIG

G. J. SANTORO, F. J. KOHL, C. A. STEARNS, S. A. GOEKOGLU

(Analex Corp.), and D, E. ROSNER (Yale Univ.) Mar. 1984 46

p refs

(NAS3-23293; NAG3-201 )

(NASA-TP-2225; E-1752; NAS 1.60:2225) Avail: NTIS HC

A03/MF A01 CSCL 20D

DEPOSITION, HEAT TRANSFER, MASS TRANSFER

N84-21828"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

REVIEW AND STATUS OF HEAT-TRANSFER TECHNOLOGY

FOR INTERNAL PASSAGES OF AIR-COOLED TURBINE

BLADES

F. C. YEH and F. S. STEPKA Apr. 1984 36 p refs

(NASA-TP-2232; E-1373; NAS 1.60:2232) Avail: NTIS HC

A03/MF A01 CSCL 20D

AIR COOLING, AIR FLOW, HEAT TRANSFER,

PASSAGEWAYS, TURBINE BLADES, TURBULENT FLOW

N84-22906"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AN ANALYSIS OF SHOCK COALESCENCE INCLUDING

THREE-DIMENSIONAL EFFECTS WITH APPLICATION TO

SONIC BOOM EXTRAPOLATION Ph.D. Thesis - George

Washington Univ.

C. M. DARDEN Jan. 1984 77 p refs

(NASA-TP-2214; L-15660; NAS 1.60:2214) Avail: NTIS HC

A05/MF A01 CSCL 20D

COALESCING, SHOCK WAVES, SONIC BOOMS,

SUPERSONIC FLOW

N84-22907"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

HYBRID PERTURBATION/BUBNOV-GALERKIN TECHNIQUE

FOR NONLINEAR THERMAL ANALYSIS

A. K. NOOR (George Washington Univ.) and C. D. BALCH (George

Washington Univ.) Jun. 1983 28 p refs

(NASA°TP-2145; L-15584; NAS 1.60:2145) Avail: NTIS HC

A03/MF A01 CSCL 20D

CONDUCTION, CONVECTION, HEAT TRANSFER,

NONLINEAR SYSTEMS, PERTURBATION, THERMAL ANALYSIS

111
34 FLUIDMECHANICSANDHEATTRANSFER

N84-23852"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

FINITE-DIFFERENCE FLUID DYNAMICS COMPUTER

MATHEMATICAL MODELS FOR THE DESIGN AND

INTERPRETATION OF EXPERIMENTS FOR SPACE FLIGHT

G. O. ROBERTS (Roberts Associates, Inc.), W. W. FOWLIS, and

T. L. MILLER May 1984 16 p refs

(NASA-TP-2323; NAS 1.60:2323) Avail: NTIS HC A02/MF A01

CSCL 05H

EXPERIMENT DESIGN, FINITE DIFFERENCE THEORY, FLUID

DYNAMICS, MATHEMATICAL MODELS, SPACEBORNE

EXPERIMENTS, SPACELAB PAYLOADS

N84-25944"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

DRAG OF TWO-DIMENSIONAL SMALL-AMPLITUDE

SYMMETRIC AND ASYMMETRIC WAVY WALLS IN TURBULENT

BOUNDARY LAYERS

J. C. LIN, M. J. WALSH, and R. BALASUBRAMANIAN (Cambridge

Hydrodynamics, Inc., Lexington, Mass.) Jun. 1984 165 p refs

(NASA-TP-2318; L-15761; NAS 1.60:2318) Avail: NTIS HC

A08/MF A01 CSCL 20D

DRAG, LOW SPEED, SINE WAVES, SKIN FRICTION,

TURBULENT BOUNDARY LAYER, TURBULENT FLOW

N84-31561"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ELECTROLESS-PLATING TECHNIQUE FOR FABRICATING

THIN-WALL CONVECTIVE HEAT-TRANSFER MODELS

D. E. AVERY, G. K. BALLARD, and M. L. WILSON Aug. 1984

39 p refs

(NASA-TP-2349; L-15815; NAS 1.60:2349) Avail: NTIS HC

A03/MF A01 CSCL 20D

ELECTROLESS DEPOSITION, HEAT SHIELDING, HEAT

TRANSFER, PLATING, SPACECRAFT DESIGN, THERMAL

INSULATION, THIN WALLED SHELLS, TILES

N85-12313"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EXPERIMENTAL AND PREDICTED HEATING DISTRIBUTIONS

FOR BICONICS AT INCIDENCE IN AIR AT MACH 10

C. G. MILLER, 111 Nov. 1984 118 p refs

(NASA-TP-2334; L-15785; NAS 1.60:2334) Avail: NTIS HC

A06/MF A01 CSCL 20D

AERODYNAMIC HEATING, AEROTHERMODYNAMICS,

CONICAL BODIES, HEAT TRANSFER, HYPERSONIC FLOW,

WIND TUNNEL TESTS

N85-12314"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

VORTEX-GENERATING COOLANT-FLOW-PASSAGE DESIGN

FOR INCREASED FILM-COOLING EFFECTIVENESS AND

SURFACE COVERAGE

S. S. PAPELL Nov. 1984 24 p refs

(NASA-TP-2388; E-2147; NAS 1.60:2388) Avail: NTIS HC

A02/MF A01 CSCL 20D

DUCTS, ENGINE COOLANTS, FILM COOLING, FLOW

CHARACTERISTICS, PASSAGEWAYS, VORTICES

N85-13175"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

A PRELIMINARY STUDY OF NUMERICAL SIMULATION OF

THERMOSOLUTAL CONVECTION OF INTEREST TO CRYSTAL

GROWTH

T, L. MILLER Nov. 1984 33 p refs

(NASA-TP-2394; NAS 1,60:2394) Avail: NTIS HC A03/MF A01

CSCL 20D

CONVECTION, CRYSTAL GROWTH, FLUID FLOW,

MATHEMATICAL MODELS

112

N85-14078"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

FLOW RATES AND PRESSURE PROFILES FOR ONE TO FOUR

AXIALLY ALINED BORDA INLETS

R. C. HENDRICKS and T. T. STETZ Dec. 1984 32 p refs

(NASA-TP-2390; E-1979; NAS 1.60:2390) Avail: NTiS HC

A03/MF A01 CSCL 20A

FLOW VELOCITY, INLET FLOW, INLET PRESSURE, INTAKE

SYSTEMS

N85-16065"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va

LAMINAR HEAT-TRANSFER DISTRIBUTIONS ON BICONICS AT

INCIDENCE IN HYPERSONIC-HYPERVELOCITY FLOWS

C. G. MILLER, III, J. R. MICOL, and P. A. GNOFFO Jan. 1984

145 p refs

(NASA-TP-2213; L-15645; NAS 1.60:2213) Avail: NTIS HC

A07/MF A01 CSCL 20D

HYPERSONIC FLOW, HYPERVELOCITY FLOW, LAMINAR

HEAT TRANSFER, NOSE CONES, THERMOCHEMISTRY

N85-16066"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

REDUCTION METHOD FOR THERMAL ANALYSIS OF COMPLEX

AEROSPACE STRUCTURES

C. P. SHORE Jan. 1985 31 p refs

(NASA-TP-2373; L-15777; NAS 1.60:2373) Avail: NTIS HC

A03/MF A01 CSCL 20D

AEROSPACE ENGINEERING, ANTENNAS, OPTIMIZATION,

SPACE SHUTTLES, STRUCTURAL ANALYSIS, THERMAL

ANALYSIS, WINGS

N85-17322"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AEROTHERMAL TESTS OF A 12.5 PERCENT CONE AT MACH

6.7 FOR VARIOUS REYNOLDS NUMBERS, ANGLES OF ATTACK

AND NOSE SHAPES

R J. NOWAK, C. W_ ALBERTSON, and L. R. HUNT Jan. 1984

90 p refs

(NASA-TP-2345; L-15729; NAS 1.60:2345) Avail: NTIS HC

A05/MF A01 CSCL 20D

AERODYNAMIC HEATING, BOUNDARY LAYER TRANSITION,

CONES, FLOW DISTRIBUTION, LAMINAR BOUNDARY LAYER,

SHOCK LAYERS, TURBULENT BOUNDARY LAYER

N85-20270*# North American Aviation, Inc., Torrance, Calif.

FLOW THROUGH VERY POROUS SCREENS

P. A. DURBIN and K. K. MURAMOTO Mar. 1985 13 p refs

(NASA-TP-2436; E-2360; NAS 1.60:2436) Avail: NTIS HC

A02/MF A01 CSCL 20D

DRAG MEASUREMENT, FLOW CHARACTERISTICS, FLOW

DISTRIBUTION, PROTECTORS, RESISTANCE, WIRE CLOTH

N85-25757"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

A CRITICAL EVALUATION OF VARIOUS TURBULENCE

MODELS AS APPLIED TO INTERNAL FLUID FLOWS

M. NALLASAMY May 1985 72 p refs

(NASA-TP-2474; NAS 1.60:2474) Avail: NTIS HC A04/MF A01

CSCL 20D

COMPUTATIONAL FLUID DYNAMICS, MATHEMATICAL

MODELS, TURBULENT FLOW

N85-27165"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

FLOW RATE AND PRESSURE PROFILES FOR 1 TO 4 AXIALLY

ALINED ORIFICE INLETS

R, C, HENDRICKS and T, T. STETZ May 1985 44 p refs

(NASA-TP-2460; E-1980; NAS 1.60:2460) Avail: NTIS HC

A03/MFA01 CSCL20D

FLOW VELOCITY, INLET FLOW, ORIFICE FLOW, ORIFICES,

PRESSURE DISTRIBUTION
N85-28260"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

FLUID SURFACE BEHAVIOR IN LOW GRAVITY. CENTER

DISCRETIONARY FUND NO. 83-21 Final Report

F. LESLIE, R. F. GANS, and C. SCHAFER Jun. 1985 28 p

refs

(NASA-TP-2486; NAS 1.60:2486) Avail: NTIS HC A03/MF A01

CSCL 20D

BUBBLES, FLUID MECHANICS, GRAVITATION, REDUCED

GRAVITY, SHAPES, STABILITY

N85-31433"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

TRANSITION IN TURBINES

Washington Jul. 1985 224 p refs Symp. held in Cleveland,

15-16 May 1984

(NASA-CP-2386; E-2456; NAS 1.55:2386) Avail: NTIS HC

A10/MFA01 CSCL20D

BOUNDARY LAYER TRANSITION, EQUATIONS OF MOTION,

FLOW CHARACTERISTICS, FLUID MECHANICS, HEAT

TRANSFER, TURBULENCE, TURBULENT BOUNDARY LAYER

N85-34351"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EXPERIMENTAL AERODYNAMIC HEATING TO SIMULATED

SPACE SHUTTLE TILES IN LAMINAR AND TURBULENT

BOUNDARY LAYERS WITH VARIABLE FLOW ANGLES AT A

NOMINAL MACH NUMBER OF 7 M.S. Thesis - George

Washington Univ., Nov. 1983

D. E. AVERY Aug. 1985 50 p refs Original contains color

illustrations

(NASA-TP-2307; L-15781; NAS 1.60:2307) Avail: NTIS HC

A03/MF A01 CSCL 20D

COLD SURFACES, HEAT SHIELDING, HYPERSONIC FLOW,

IMPINGEMENT, REUSABLE HEAT SHIELDING, THERMAL

PROTECTION, TILES, TURBULENT BOUNDARY LAYER,

TURBULENT FLOW

N86-14530"# National Aeronautics and Space Administration.

Lyndon B. Johnson Space Center, Houston, Tex.

SUP-BOUNDARY EQUATIONS FOR MULTICOMPONENT

NONEQUILIBRIUM AIRFLOW

R. N. GUPTA, C. D. SCOTT, and J. N. MOSS Nov. 1985 58 p

refs

(NASA-TP-2452; L-15952; NAS 1.60:2452) Avail: NTIS HC

A04/MF A01 CSCL 20D

AIR FLOW, BOUNDARY LAYER EQUATIONS, FLIGHT PATHS,

HIGH ALTITUDE ENVIRONMENTS, LOW DENSITY RESEARCH,

LOW REYNOLDS NUMBER, NONEQUILIBRIUM FLOW, SLIP

FLOW, SPACECRAFT TRAJECTORIES, VELOCITY DISTRIBUTION

N86-20720"# National Aeronautics and Space Administration,

Langley Research Center, Hampton, Va.

STUDIES OF CONDENSATION EFFECTS ON AIRFOIL TESTING

IN THE LANGLEY 0.3-METER TRANSONIC CRYOGENIC

TUNNEL

R. M HALL Jan. 1986 34 p refs Previously announced in

IAA as A85-19603

(NASA-TP-2509; L-16021; NAS 1.60:2509) Avail: NTIS HC

A03/MF A01 CSCL 20D

AIRFOILS, CONDENSATION NUCLEI, CRYOGENIC WIND

TUNNELS, TRANSONIC WIND TUNNELS, WIND TUNNEL

TESTS

35 INSTRUMENTATION AND PHOTOGRAPHY

N86-23851"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

ANALYTICAL AND NUMERICAL STUDIES OF THE

THERMOCAPILLARY FLOW IN A UNIFORMLY FLOATING

ZONE

W. W. FOWLIS and G. O. ROBERTS (Roberts Associates, Inc.,

Vienna, Va.) 1986 42 p refs

(NASA-TP-2576; NAS 1.60:2576) Avail: NTIS HC A03/MF A01

CSCL 20D

CAPILLARY FLOW, CRYSTAL GROWTH, FLOAT ZONES,

SPACE MANUFACTURING, WEIGHTLESSNESS

35

INSTRUMENTATION AND PHOTOGRAPHY

Includes remote sensors; measuring instruments and gages;

detectors; cameras and photographic supplies; and holography.

N77-32458"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AN OPTICAL PROFILOMETER FOR SPATIAL

CHARACTERIZATION OF THREE-DIMENSIONAL SURFACES

W. L. KELLY, IV, E. E. BURGHER, and M. W. SKOLAUT, JR.

Sep. 1977 22p refs

(NASA-TP-1012; L-11706) Avail: NTIS HC A02/MF A01

CSCL 14B

EQUIPMENT SPECIFICATIONS, OPTICAL MEASURING

INSTRUMENTS, PHOTOELASTIC ANALYSIS, PROFILOMETERS

N78-13408"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

A GAS FILTER CORRELATION MONITOR FOR CO, CH4, AND

HCL

D. I. SEBACHER Dec. 1977 30 p refs

(NASA-TP-1113; L-11868) Avail: NTIS HC A03/MF A01

CSCL 14B

AIR POLLUTION, CARBON MONOXIDE, HYDROGEN

CHLORIDES, INFRARED FILTERS, METHANE, POLLUTION

MONITORING

N78-15463"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

RECOVERY AND RADIATION CORRECTIONS AND TIME

CONSTANTS OF SEVERAL SIZES OF SHIELDED AND

UNSHIELDED THERMOCOUPLE PROBES FOR MEASURING

GAS TEMPERATURE

G. E. GLAWE, R. HOLANDA, and L. N. KRAUSE Jan, 1978

30 p refs

(NASA-TP-1099; E-9289) Avail: NTIS HC A03/MF A01 CSCL

t4B

GAS TEMPERATURE, HEAT SHIELDING, THERMOCOUPLES

N78-17360"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

NASA GROUND-BASED AND SPACE-BASED LASER RANGING

SYSTEMS

M W. FITZMAURICE Jan. 1978 28 p refs

(NASA-TP-1149; G-7802-F03) Avail: NTIS HC A03/MF A01

CSCL 20E

GROUND BASED CONTROL, LASER RANGER/TRACKER,

SATELLITE-BORNE PHOTOGRAPHY

113
35 INSTRUMENTATION AND PHOTOGRAPHY

N78-21430"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va,

A SMALL GAS INLET SYSTEM FOR ORBITAL

MASS-SPECTROMETER CALIBRATIONS

A. SMITH and R. E. STELL Apr. 1978 33 p refs

(NASA-TP-1170; L-11988) Avail: NTIS HC A03/MF A01

CSCL 14B

CALIBRATING, DUAL AIR DENSITY EXPLORER, INTAKE

SYSTEMS, MASS SPECTROMETERS

N78-21431"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

A FEASIBILITY STUDY OF ION IMPLANTATION TECHNIQUES

FOR MASS SPECTROMETER CALIBRATION

M. E. KOSLIN (Rensselaer Polytech. Inst.), G, A, KRYCUK

(Rensselaer Polytech. inst.), J. G. SCHATZ, JR. (Rensselaer

Polytech. Inst.), F. A. WHITE (Rensselaer Polytech. Inst.), and G.

M. WOOD Apt. 1978 21 p refs

(NASA-TP-1185; L-11920) Avail: NTIS HC A02/MF A01

CSCL 14B

CALIBRATING, FEASIBILITY ANALYSIS, iON IMPLANTATION,

MASS SPECTROMETERS

N78-28412"# National Aeronautics and Space Administration.

Wallops Flight Center, Wallops Island, Va.

TOTAL OZONE MEASUREMENT: INTERCOMPARISON OF

PROTOTYPE NEW ZEALAND FILTER INSTRUMENT AND

DOBSON SPECTROPHOTOMETER

R. E. BASHER Jul. 1978 17 p refs

(NASA-TP-1277) Avail: NTIS HC A02/MF A01 CSCL 14B

CALIBRATING, INSTRUMENT ERRORS, MEASURING

INSTRUMENTS, OZONOMETRY

N79-17195"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

HOLOGRAPHY THROUGH OPTICALLY ACTIVE WINDOWS

A. J. DECKER Feb. 1979 18 p refs

(NASA-TP-1414; E-9808) Avail: NTIS HC A02/MF A01 CSCL

14E

FLOW VISUALIZATION, HOLOGRAPHY, IMAGING

TECHNIQUES, OPTICAL ACTIVITY, WINDOWS (APERTURES)

N79-21329°# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

SIMULATED ELECTRONIC HETERODYNE RECORDING AND

PROCESSING OF PULSED-LASER HOLOGRAMS

A. J. DECKER Apr. 1979 40 p refs

(NASA-TP-1444; E-9813) Avail: NTIS HC A03/MF A01 CSCL

14E

ELECTRONIC RECORDING SYSTEMS, HOLOGRAPHY,

MATHEMATICAL MODELS, OPTICAL HETERODYNING, PULSED

LASERS, SPATIAL FILTERING

N80-12384"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

PRELIMINARY APPLICATIONS AND EVALUATION RESULTS.

LIXISCOPE: PROCEEDINGS OF THE LlXlSCOPE

CONFERENCE

Jul. 1978 89 p refs Conf. held at Greenbelt, Md., 27-28 Jul.

1978

(NASA-CP-2112) Avail: NTIS HC A05/MF A01 CSCL 14E

CONFERENCES, FLUOROSCOPY, OPTICAL MEASURING

INSTRUMENTS, PORTABLE EQUIPMENT, X RAY IMAGERY

114

N80-12399"# National Aeronautics and Space Administration.

Lyndon B. Johnson Space Center, Houston, Tex.

DETERMINATION OF NOISE EQUIVALENT REFLECTANCE FOR

A MULTISPECTRAL SCANNER: A SCANNER SENSITIVITY

STUDY

D. E. GIBBONS (Fort Lewis Coll., Durango, Colo.) and R. R.

RICHARD Dec. 1979 31 p refs

(NASA-TP-1575; S-497) Avail: NTIS HC A03/MF A01 CSCL

14E

MULTISPECTRAL BAND SCANNERS, PHOTOSENSITIVITY,

WHITE NOISE

N80-13430"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

INSTRUMENT ERROR ANALYSIS AS IT APPLIES TO

WIND-TUNNEL TESTING

E. RIND Dec. 1979 61 p

(NASA-TP-1572; L-13222) Avail: NTIS HC A04/MF A01

CSCL 14B

ERROR ANALYSIS, INSTRUMENT ERRORS, WIND TUNNEL

MODELS, WIND TUNNEL TESTS

N80-22660"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ALIASED NOISE IN RADIOMETRIC MEASUREMENTS

F, O, HUCK, S, K. PARK, N. HALYO, and S. T, STALLMAN May

1980 26 p refs

(NASA-TP-1639; L-13410) Avail: NTIS HC A03/MF A01

CSCL 14B

BACKGROUND NOISE, ERROR ANALYSIS, IMAGE

RECONSTRUCTION, IMAGE RESOLUTION, NOISE

MEASUREMENT, RADIOMETERS

N80-24594"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

A SCANNING LASER-VELOCIMETER TECHNIQUE FOR

MEASURING TWO-DIMENSIONAL WAKE-VORTEX VELOCITY

DISTRIBUTIONS

L. R. GARTRELL and D. B. RHODES 23 May 1980 43 p

refs

(NASA-TP-1661; L-13426) Avail: NTIS HC A03/MF A01

CSCL 14B

AIRCRAFT WAKES, LASER DOPPLER VELOCIMETERS,

SCANNERS, VELOCITY MEASUREMENT, VORTICES, WIND

TUNNEL TESTS

N80-24595"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

DYNAMIC BEHAVIOR OF A BEAM DRAG-FORCE

ANEMOMETER

G, C, FRALICK Washington May 1980 16 p refs

(NASA-TP-1687; E-340) Avail: NTIS HC A02/MF A01 CSCL

14B

AERODYNAMIC DRAG, ANEMOMETERS, CANTILEVER

BEAMS, DYNAMIC RESPONSE, LOADS (FORCES), VELOCITY

MEASUREMENT

N80-25635"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

COMPUTERIZED VIDEO DENSITOMETRY METHOD FOR RAPID

ANALYSIS OF INFRARED PHOTOGRAPHIC IMAGES

E, ROBERTS, JR., F, D, CALFO, and F, G, POLLACK Jun.

1980 13 p refs

(NASA TP-1686; E-354) Avail: NTIS HC A05/MF A01

CSCL t4E

DENSITY MEASUREMENT, IMAGE PROCESSING, INFRARED

PHOTOGRAPHY, MICRODENSITOMETERS, TEMPERATURE

DISTRIBUTION, TURBINE BLADES
N80-30716"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

MARS 1414 RECORDER ENVIRONMENTAL TESTS

D. LANGJAHR Aug. 1980 31 p

(NASA-TP-1709; REPT-80F5124) Avail: NTIS HC A03/MF A01

CSCL 14E

AIRBORNE EQUIPMENT, ALTITUDE, AMBIENT TEMPERATURE, ENVIRONMENTAL TESTS, GRAPHS (CHARTS)

N80-30717"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

DIAL WITH HETERODYNE DETECTION INCLUDING SPECKLE

NOISE: AIRCRAFT/SHUTTLE MEASUREMENTS OF 03, H20,

AND NH3 WITH PULSED TUNABLE CO2 LASERS

P. BROCKMAN, R. V. HESS, L. D. STATON, and C. H. BAIR

Aug. 1980 14 p refs Presented at Intern. Conf. on Heterodyne

Systems and Technol., Williamsburg, Va. 25-27 Mar. 1980

Submitted for publication

(NASA-TP-1725; L-13876) Avail: NTIS HC A02/MF A01

CSCL 20E

AMMONIA, CARBON DIOXIDE LASERS, ELECTROMAGNETIC

NOISE, HETERODYNING, OPTICAL RADAR, OZONE, SPECKLE

PATTERNS, WATER VAPOR

N81-23432"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

NASA METROLOGY AND CALIBRATION, 1980 Final Report

Washington NASA 10 Apr. 1981 153 p refs Proceedings

of the 4th Ann. Workshop, Hampton, Va., 21-23 Oct. 1980

(NASA-CP-2174; L-14380) Avail: NTIS HC A08/MF A01

CSCL 13B

CALIBRATING, CONFERENCES, METROLOGY, QUALITY

CONTROL, STANDARDIZATION

N81-25352"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

DESIGN AND ANALYSIS OF A TORSION BRAID PENDULUM

DISPLACEMENT TRANSDUCER

E. RIND and E. L. BRYANT Jun. 1981 63 p refs

(NASA-TP-1840; L-14183) Avail: NTIS HC A04/MF A01

CSCL 14B

ERROR ANALYSIS, MECHANICAL PROPERTIES, OPTICAL

EQUIPMENT, PENDULUMS, TECHNOLOGY ASSESSMENT,

TRANSDUCERS

N81-33452"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

APPLICATION OF INFORMATION THEORY TO THE DESIGN

OF LINE-SCAN IMAGING SYSTEMS

F. O. HUCK, S. K. PARK, N. HALYO, and S. STALLMAN Sep.

1981 40 p refs Prepared in cooperation with Information and

Control Systems, Hampton, Va.

(NASA-TP-1897; L-14542) Avail: NTIS HC A03/MF A01

CSCL 14B

IMAGING TECHNIQUES, INFORMATION THEORY,

MODULATION TRANSFER FUNCTION

N82-15383"# Desert Research Inst., Reno, Nev.

THE THIRD INTERNATIONAL CLOUD CONDENSATION NUCLEI

WORKSHOP Final Report

W. C. KOCMOND, C. R. ROGERS, ed., and S. W. REA, ed. Nov.

1981 287 p refs Workshop held in Reno, Nev., 6-17 Oct.

1980; sponsored in part by NSF

(NAS8-33820)

(NASA-CP-2212) Avail: NTIS HC A13/MF A01 CSCL 14B

AEROSOLS, CLOUD PHYSICS, CONDENSING,

CONFERENCES, ICE NUCLEI, NUCLEATION, PARTICLE SIZE

DISTRIBUTION

35 INSTRUMENTATION AND PHOTOGRAPHY

N82-19521"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

HIGH-SPEED LASER ANEMOMETER SYSTEM FOR

INTRAROTOR FLOW MAPPING IN TURBOMACHINERY

J. A. POWELL, A. J. STRAZISAR, and R. G. SEASHOLTZ Feb.

1982 22 p refs

(NASA-TP-1663; E-276) Avail: NTIS HC A02/MF A01 CSCL

14B

COMPRESSOR ROTORS, FLOW VELOCITY, LASER

ANEMOMETERS, TRANSONIC FLOW, TURBOMACHINERY

N82-22481"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

FRINGE LOCALIZATION REQUIREMENTS FOR

THREE-DIMENSIONAL FLOW VISUALIZATION OF SHOCK

WAVES IN DIFFUSE-ILLUMINATION DOUBLE-PULSE

HOLOGRAPHIC INTERFEROMETRY

A. J. DECKER Apr. 1982 45 p refs

(NASA-TP-1868; NAS 1.60:1868; E-757) Avail: NTIS HC

A03/MF A01 CSCL 14E

FLOW VISUALIZATION, HOLOGRAPHIC INTERFEROMETRY,

SHOCK WAVES, THREE DIMENSIONAL FLOW

N82-23515"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

POCKELS-EFFECT CELL FOR GAS-FLOW SIMULATION

D. WEIMER May 1982 t9 p refs

(NASA-TP-2007; E-1028; NAS 1.60:2007) Avail: NTIS HC

A02/MFA01 CSCL 14B

BIREFRINGENCE, CRYSTAL OPTICS, ELECTRIC FIELDS,

ELECTRO-OPTiCS, GAS FLOW, REFRACTIVITY

N82-26637"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

TROPOSPHERIC PASSIVE REMOTE SENSING

L. S. KEAFER, JR., ed. Jun. 1982 95 p refs Proc. of a

Workshop held in Virginia Beach, Va., 20-23 Jut. 1981

(NASA-CP-2237; L-15390; NAS 1.55:2237) Avail: NTIS HC

A05/MF A01 CSCL 14B

ATMOSPHERIC COMPOSITION, PRODUCT DEVELOPMENT,

REMOTE SENSORS, TECHNOLOGY ASSESSMENT, TRACE

CONTAMINANTS, TROPOSPHERE

N82-27706"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ABSTRACTS OF PAPERS PRESENTED AT THE ELEVENTH

INTERNATIONAL LASER RADAR CONFERENCE

Jun. 1982 267 p refs Conf. held at Madison, Wisc., 21-25

Jun. 1982; sponsored in part by Wisconsin Univ., Am. Meteorol.

Soc., AFOSR, and Air Force Geophys. Lab.

(NASA-CP-2228; L-15380; NAS 1.55:2228) Avail: NTIS HC

A12/MF A01 CSCL 14B

CONFERENCES, MESOSPHERE, METEOROLOGICAL

PARAMETERS, OPTICAL RADAR, REMOTE SENSING

N82-29577"# Systematics General Corp., McLean, Va.

HANDBOOK OF SENSOR TECHNICAL CHARACTERISTICS

S, TANNER Jul. 1982 333 p refs

(NASW-3398)

(NASA-RP-1087; NAS 1.61:1087) Avail: NTIS HC A15/MF A01

CSCL 14B

Space and terrestria_ applications remote sensor systems are

described. Each sensor is presented separately. Information is

included on its objectives, description, technical characteristics,

data products obtained, data archives location, period of operation,

and measurement and potential derived parameters. Each sensor

is cross indexed. Author

115
35 INSTRUMENTATION AND PHOTOGRAPHY

N82-29579'# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

MAGNETIC TAPE RECORDING FOR THE EIGHTIES

F. KALIL, ed Apr. 1982 176 p rafs

(NASA-RP-1075; NAS 1.61:1075) CSCL 14E

The practical and theoretical aspects of state-of-the-art

magnetic tape recording technology are reviewed. Topics covered

include the following: (1) analog and digital magnetic tape

recording, (2) tape and head wear, (3) wear testing, (4) magnetic

tape certification, (5) care, handling, and management of magnetic

tape, (6) cleaning, packing, and winding of magnetic tape, (7)

tape reels, bands, and packaging, (8) coding techniques for

high-density digital recording, and (9) tradeoffs of coding

techniques. Author

N82-32663"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

FLOW VISUALIZATION AND LASER VELOCIMETRY FOR WIND

TUNNELS

W. W. HUNTER, JR., ed. and J. T. FOUGHNER, JR., ed. Sep.

t982 354 p refs Workshop held in Hampton, Va., 25-26 Mar.

1982

(NASA-CP-2243; L-15498; NAS 1.55:2243) Avail: NTIS HC

A16/MFA01 CSCL 148

CRYOGENIC WIND TUNNELS, FLOW DISTRIBUTION, FLOW

VISUALIZATION, LASER DOPPLER VELOCIMETERS,

TRANSONIC WiND TUNNELS, WIND TUNNEL MODELS

N83-28410"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

RADIOMETER REQUIREMENTS FOR EARTH-OBSERVATION

SYSTEMS USING LARGE SPACE ANTENNAS

L. S. KEAFER, JR. and R. F. HARRINGTON Jun. 1983 44 p

refs

(NASA-RP-1101; L-15429; NAS 1.61:1101) Avail: NTIS HC

A03/MF A01 CSCL 14B

Requirements are defined for Earth observation microwave

radiometry for the decade of the 1990's by using large space

antenna (LSA) systems with apertures in the range from 50 to

200 m. General Earth observation needs, specific measurement

requirements, orbit mission guidelines and constraints, and general

radiometer requirements are defined. General Earth observation

needs are derived from NASA's basic space science program.

Specific measurands include soil moisture, sea surface

temperature, salinity, water roughness, ice boundaries, and water

pollutants. Measurements are required with spatial resolution from

10 to 1 km and with temporal resolution from 3 days to 1 day.

The primary orbit altitude and inclination ranges are 450 to 2200

km and 60 to 96 deg, respectively. Contiguous large scale coverage

of several land and ocean areas over the globe dictates large

(several hundred kilometers) swaths, Radiometer measurements

are made in the bandwidth range from 1 to 37 GHz, preferably

with dual polarization radiometers with a minimum of 90 percent

beam efficiency. Reflector surface, root mean square deviation

tolerances are in the wavelength range from 1/30 to 1/100.

Author

N84-11460"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va,

PROPOSED FAST-RESPONSE OXYGEN MONITORING AND

CONTROL SYSTEM FOR THE LANGLEY 8-FOOT

HIGH-TEMPERATURE TUNNEL

J. J. SINGH, W. T. DAVIS, and R. L. PUSTER Nov. 1983 30 p

refs

(NASA-TP-2218; L-15666; NAS 1.60:2218) Avail: NTIS HC

A03/MF A01 CSCL 14B

AIR BREATHING ENGINES, AUTOMATIC CONTROL, HIGH

TEMPERATURE, MONITORS, OXYGEN, WIND TUNNELS

N84-28020"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

ASTRONOMICAL MICRODENSlTOMETRY CONFERENCE

D. A. KLINGLESMITH, ed, Jul. 1984 415 p refs

(NASA-CP-2317; GFSC-84F5182; NAS 1.55:2317) Avail: NTIS

HC A18/MF A01 CSCL 14E

ASTRONOMICAL PHOTOMETRY, DATA RETRIEVAL, DATA

STORAGE, DESIGN ANALYSIS, MICRODENSITOMETERS,

OPTICAL MEASUREMENT, OPTICAL SCANNERS, PERFORMANCE TESTS, TECHNOLOGICAL FORECASTING

N85-16099*# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EFFECT OF FIVE LUBRICANTS ON LIFE OF AlSl 9310 SPUR

GEARS

D. P. TOWNSEND and E. V. ZARETSKY Jan. 1985 15 p

refs

(NASA-TP-2419; E-2183; NAS 1.60:2419) Avail: NTIS HC

A02/MFA01 CSCL 131

ADDITIVES, FATIGUE TESTS, GEARS, LUBRICANTS,

SURFACE PROPERTIES, WEAR

N85-16100"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

INTEGRATED EXHAUST GAS ANALYSIS SYSTEM FOR

AIRCRAFT TURBINE ENGINE COMPONENT TESTING

R. L. SUMMERS and R, C. ANDERSON Jan. 1985 28 p refs

(NASA-TP-2424; E-2302; NAS 1.60:2424) Avail: NTIS HC

A03/MF A01 CSCL 14B

ENGINE TESTS, EXHAUST GASES, GAS ANALYSIS, GAS

TURBINE ENGINES

N86-11437*# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

WIND TUNNEL SEEDING SYSTEMS FOR LASER

VELOCIMETERS

W. W. HUNTER, JR, comp. and C. E. NICHOLS, JR., comp.

Washington Oct. 1985 264 p refs Workshop held in

Hampton, Va., 19-20 Mar. 1985

(NASA-CP-2393; L-16013; NAS 1.55:2393) Avail: NTIS HC

A12/MF A01 CSCL 14B

FLOW DISTRIBUTION, LASER DOPPLER VELOCIMETERS,

PARTICLE DENSITY (CONCENTRATION), PARTICLE SIZE

DISTRIBUTION, SCATTERING, WIND TUNNELS

N83-33126"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

R_!NBOW SCHLIEREN

W. L. HOWE_ c May 1983 21 p refs Original contains color

illustrations

(NASA-TP-2166; E-1173; NAS 1.60:2166) Avail: NTIS HC

A02/MF A01 CSCL 14B

NONUNIFORMITY, RAINBOWS, REFRACTIVITY, SCHLIEREN

PHOTOGRAPHY

N86-12579"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

RAPID ESTIMATION OF FREQUEI'_CY RESPONSE FUNCTIONS

BY CLOSE-RANGE PHOTOGRAMMETRY

J. S. TRIPP Nov. 1985 30 p refs

(NASA-TP-2471; L-t5955; NAS 1.60:2471) Avail: NTIS HC

A03/MF A01 CSCL 14E

DYNAMIC RESPONSE, PERTURBATION THEORY, PHOTOGRAMMETRY, RAMP FUNCTIONS, STEREOPHOTOGRAPHY

116
N86-20753"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

NEW METHOD FOR DETERMINING HEATS OF COMBUSTION

OF GASEOUS HYDROCARBONS

J. J. SINGH, D. R. SPRINKLE, and R. L. PUSTER Dec. 1985

13 p refs

(NASA-TP-2531; L-16054; NAS 1.60:2531) Avail: NTIS HC

A02/MF A01 CSCL 14B

CALORIMETERS, HEAT OF COMBUSTION, NATURAL GAS,

ON-LINE SYSTEMS

N86-24962"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

MEASUREMENT OF VISCOSITY OF GASEOUS MIXTURES AT

ATMOSPHERIC PRESSURE

J. J. SINGH, G. H. MALL (Computer Sciences Corp., Hampton,

Va), and H. CHEGINI (Old Dominion Univ.) May 1986 19 p

refs

(NASA-TP-2582; L-16103; NAS 1.60:2582) Avail: NTIS HC

A02/MF A01 CSCL 14B

CAPILLARY FLOW, CHAPMAN-ENSKOG THEORY,

COEFFICIENTS, GAS MIXTURES, LAMINAR FLOW, NATURAL

GAS, VISCOSITY

36

LASERS AND MASERS

Includes parametric amplifiers.

N78-16354"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

PRELAUNCH TESTING OF THE GEOS-3 LASER REFLECTOR

ARRAY

P. O. MINOTT, M. W. FITZMAURICE, J. B. ABSHIRE, and H. E.

ROWE Jan. 1978 53 p refs

(NASA-TP-1138; G-7702-F19) Avail: NTIS HC A04/MF A01

CSCL 20E

GEOS 3 SATELLITE, PULSED LASERS, REFLECTORS

N78-31413"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

A COMPARATIVE STUDY OF OPTIMUM AND SUBOPTIMUM

DIRECT-DETECTION LASER RANGING RECEIVERS

J. B. ABSHIRE Sep. 1978 43 p refs

(NASA-TP-1315; G-7802-F15) Avail: NTIS HC A03/MF A01

CSCL 20E

LASER RANGE FINDERS, OPTICAL RADAR, RECEIVERS

N79-22455"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

LASER DOPPLER VELOCIMETRY WORKSHOP

R. B. OWEN Mar. 1979 12 p Workshop held at Huntsville,

Ala., 12 Feb. 1979

(NASA-CP-2084) Avail: NTIS HC A02/MF A01 CSCL 20E

DOPPLER EFFECT, LASER APPLICATIONS, LASER DOPPLER

VELOCIMETERS, VELOCITY MEASUREMENT

N80-11414"# National Aeronautics and Space Administration,

Washington, D.C.

SHUTTLE ATMOSPHERIC LIDAR RESEARCH PROGRAM Final

Report

1979 231 p

(NASA-SP-433) Avail: NTIS HC A11/MF A01 CSCL 20E

The Shuttle atmospheric lidar program is discussed in relation

to an understanding of the processes governing the Earth's

atmosphere and in the capacity to evaluate the atmospheric

susceptibility to manmade and natural perturbations. Applications

of the lidar which are discussed are the determination of the

global flow of water vapor and pollutants in the troposphere,

36 LASERS AND MASERS

improvement of chemical and transport models of the stratosphere

and mesosphere, evaluation of radiative models of the atmosphere,

investigation of chemistry and transport of thermospheric atomic

species, and investigation of magnetospheric aspects of

sun/weather relationships. The features of the lidar measurements

discussed are the high spatial resolution, control of the source

wavelength and intensity, and high measurement specificity. For

individual titles, see N80-11415 through N80-11428.

N80-13438"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

NUCLEAR-PUMPED LASERS

Dec, 1979 140 p refs Proc. of Workshop held at Hampton,

Va., 25-26 Jul. 1979

(NASA-CP-2107; L-13366) Avail: NTIS HC A07/MF A01

CSCL 20E

COHERENT RADIATION, CONFERENCES, ENERGY

CONVERSION EFFICIENCY, NUCLEAR PUMPED LASERS,

NUCLEAR REACTIONS

N80-29652"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

HETERODYNE SYSTEMS AND TECHNOLOGY, PART 1

Aug. 1980 266 p refs Intern. Conf. held at Williamsburg, Va.,

25-27 Mar. 1980 2 Vol.

(NASA-CP-2138-PT-1) Avail: NTIS HC A12/MF A01 CSCL

20E

CONFERENCES, DIODES, INFRARED DETECTORS, OPTICAL

HETERODYNING, TUNABLE LASERS

N80-29672"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

HETERODYNE SYSTEMS AND TECHNOLOGY, PART 2

Aug. 1980 321 p refs Conf. held in Williamsburg, Va.,

25-27Mar. 1980

(NASA-CP-2138-PT-2) Avail: NTIS HC A14/MF A01 CSCL

20E

INFRARED SPECTROSCOPY, OPTICAL HETERODYNING,

SEMICONDUCTOR DEVICES

N81-27467"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

PROCEEDINGS OF THE 12TH ANNUAL PRECISE TIME AND

TIME INTERVAL (PTTI) APPLICATIONS AND PLANNING

MEETING

S. C. WARDRIP, ed. Mar. 1981 871 p refs Meeting held at

Greenbelt, Md., 2-4 Dec. 1980 Sponsored in cooperation with

Navy, NBS and Defense Communications Agency

(NASA-CP-2175; REPT-814.2) Avail: NTIS HC A99/MF A01

CSCL 14D

CONFERENCES, FREQUENCY STANDARDS, HYDROGEN

MASERS, RELIABILITY ENGINEERING, SYNCHRONISM, TIME

MEASUREMENT

N82-12431"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EXCESS NOISE IN TUNABLE DIODE LASERS

C. W. ROWLAND Nov. 1981 16 p refs

(NASA-TP-1935; L-14453) Avail: NTIS HC A02/MF A01

CSCL 20E

OPTICAL HETERODYNING, PHOTODIODES, SEMICONDUCTOR LASERS, SIGNAL TO NOISE RATIOS, TUNABLE LASERS

N82-18578"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SPACE LASER POWER TRANSMISSION SYSTEM STUDIES

M. D. WILLIAMS, ed. and E. J. CONWAY, ed. Feb. 1982 210

p refs Syrup. held in Hampton, Va., 14-15 Oct. 1981

(NASA-CP-2214; L-15030) Avail: NTIS HC A10/MF A01

CSCL 20E

CONFERENCES, LASER APPLICATIONS, POWER

TRANSMISSION (LASERS), SATELLITE POWER TRANSMISSION

(TO EARTH), SPACE PLATFORMS

117
36 LASERS AND MASERS

N82-20494"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

PROCEEDINGS OF THE THIRTEENTH ANNUAL PRECISE TIME

AND TIME INTERVAL (P"n'l) APPLICATIONS AND PLANNING

MEETING

S. C. WARDRIP Mar. t982 864 p refs Meeting held at

Washington, D.C., 1-3 Dec. 1981; sponsored by the Naval

Observatory, NASA. Goddard Space Flight Center, Naval

Electronic Systems Command, NRL, Defense Communications

Agency, Chief of Naval Operations, NBS, Army Electronics

Technology and Devices Lab., RADC

(NASA-CP-2220; NAS 1.55.2220) Avail: NTIS HC A99/MF A01

CSCL 20E

ATOMIC CLOCKS, COMPONENT RELIABILITY, GLOBAL

POSITIONING SYSTEM, HYDROGEN MASERS, NAVIGATION

SATELLITES, TIME MEASUREMENT

N83-16738"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

DIRECT NUCLEAR-POWERED LASERS

N. W. JALUFKA Jan. 1983 53 p refs

(NASA-TP-2091; L-15168; NAS 1.60:2091) Avail: NTIS HC

A04/MF A01 CSCL 20E

FISSIONABLE MATERIALS, HELIUM ISOTOPES, LASER

PUMPING, NEUTRON SOURCES, NUCLEAR FISSION

N83-27200"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

A NASA HIGH-POWER SPACE-BASED LASER RESEARCH AND

APPLICATIONS PROGRAM

R. J. DEYOUNG, G. D. WALBERG, E. J. CONWAY, and L. W.

JONES May 1983 46 p refs

(NASA-SP-464; NAS 1.21:464; LC-83-600161) Avail: NTIS HC

A03/MF A01 CSCL 20E

Applications of high power lasers are discussed which might

fulfill the needs of NASA missions, and the technology

characteristics of laser research programs are outlined. The status

of the NASA programs or lasers, laser receivers, and laser

propulsion is discussed, and recommendations are presented for

a proposed expanded NASA program in these areas. Program

elements that are critical are discussed in detail. S.L.

N83-32044"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SOLAR.SIMULATOR-PUMPED ATOMIC IODINE LASER

KINETICS

H. W. WILSON, S. RAJU, and Y. J. SHIU Aug. 1983 t7 p

refs

(NASA-TP-2182; L-15615; NAS 1.60:2182) Avail: NTIS HC

A02/MF A01 CSCL 20E

ENERGY CONVERSION, IODINE LASERS, KINETICS, LASER

PUMPING, PHOTOCHEMICAL REACTIONS, SOLAR

SIMULATORS

N83-35351"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

PROCEEDINGS OF THE 14TH ANNUAL PRECISE TIME AND

TIME INTERVAL (PTTI) APPLICATIONS PLANNING MEETING

S. C. WARDRIP, ed. Feb. 1983 622 p refs Meeting held in

Greenbelt, Md., 30 Nov. - 2 Dec. 1982; sponsored in cooperation

with Naval Observatory, Naval Electronic Systems Command, NRL,

Defense Communications Agency, Chief of Naval Operations, NBS,

Army Electronics Technology and Devices Lab., and RADC

(NASA-CP-2265; NAS 1.55:2265) Avail: NTIS HC A99/MF A01

CSCL 20E

ATOMIC CLOCKS, FREQUENCY STANDARDS, HYDROGEN

MASERS, RESONATORS, SYNCHRONISM, TIME MEASUREMENT, TIME SIGNALS

118

N84-17575"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

THRESHOLD KINETICS OF A SOLAR-SIMULATOR-PUMPED

IODINE LASER

J. W. WILSON, Y. LEE (Hampton Inst.), W. R. WEAVER, D. H.

HUMES, and J. H. LEE (Vanderbilt Univ.) Feb. 1984 43 p

refs

(NGT-47-020-801; NCC1-8)

(NASA-TP-2241; L-15684; NAS 1.60:2241) Avail: NTIS HC

A03/MF A01 CSCL 20E

IODINE LASERS, LASER OUTPUTS, LASER PUMPING,

REACTION KINETICS, SOLAR SIMULATORS

N84-23878"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

INTENSITY AND ABSORBED-POWER DISTRIBUTION IN A

CYLINDRICAL SOLAR-PUMPED DYE LASER

M. D. WILLIAMS 1984 18 p refs

(NASA-TP-2321; L-15694; NAS t.60:2321) Avail: NTIS HC

A02/MF A01 CSCL 20E

ABSORPTIVITY, DYE LASERS, ENERGY ABSORPTION,

LASER PUMPING, SOLAR ENERGY, SUNLIGHT

N84-31617"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

A BLACKBODY-PUMPED CO2-N2 TRANSFER LASER

R. J. DEYOUNG and N. S. HIGDON Aug. 1984 12 p refs

(NASA-TP-2347; L-15753; NAS 1.60:2347) Avail: NTIS HC

A02/MF A01 CSCL 20E

BLACK BODY RADIATION, CARBON DIOXIDE LASERS,

LASER OUTPUTS, LASER PUMPING, NITROGEN LASERS,

SOLAR-PUMPED LASERS

N86-16563"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

PERFORMANCE TEST OF LASER VELOClMETER SYSTEM FOR

THE LANGLEY 16-FOOT TRANSONIC TUNNEL

J. F. MEYERS, W. W. HUNTER, JR., D. E. REUBUSH, C. E.

NICHOLS, JR., T. E. HEPNER (Army Aviation Systems Command,

Hampton, Va.), and J. W. LEE Dec. 1985 38 p refs

(DA PROJ. 1 L1-61102-AH-45)

(NASA-TP-2502; L-15940; NAS 1.60:2502; AVSCOM-TR-85-B-4)

Avail: NTIS HC A03/MF A01 CSCL 20E

FREE FLOW, LASER DOPPLER VELOCIMETERS, PARTICLE

SIZE DISTRIBUTION, TRANSONIC FLOW

37

MECHANICAL ENGINEERING

Includes auxiliary systems (nonpower); machine elements and

processes; and mechanical equipment.

N77-31502"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EXPERIMENTAL EVALUATION OF FOIL-SUPPORTED

RESILIENT-PAD GAS-LUBRICATED THRUST BEARING

Z. N NEMETH Sep. 1977 20 p refs

(NASA-TP-1030; E-9061) Avail: NTIS HC A02/MF A01 CSCL

131

FOIL BEARINGS, GAS LUBRICANTS, PERFORMANCE TESTS,

THRUST BEARINGS
N77-33520"#National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EFFECT OF DOUBLE VACUUM MELTING AND RETAINED

AUSTENITE ON ROLLING-ELEMENT FATIGUE LIFE OF AMS

5749 BEARING STEEL

R. J. PARKER and R. S. HODDER (Latrobe Steel Co., Latrobe,

Pa.) Oct. 1977 16p refs

(NASA-TP-1060; E-9101) Avail: NTIS HC A02/MF A01 CSCL

11F

AUSTENITE, BEARING ALLOYS, STEELS, VACUUM

MELTING

N78-10474"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

STABILITY OF NUMERICAL INTEGRATION TECHNIQUES FOR

TRANSIENT ROTOR DYNAMICS

A. F. KASCAK 1977 22 p refs

(NASA-TP-1092; E-9252) Avail: NTIS HC A02/MF A01 CSCL

21E

NUMERICAL INTEGRATION, NUMERICAL STABILITY,

ROTATING SHAFTS, ROTORS, TRANSIENT RESPONSE

N78o18429"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

STATISTICAL MODEL FOR ASPERITY-CONTACT TIME

FRACTION IN ELASTOHYDRODYNAMIC LUBRICATION

S. M SIDIK and J. J, COY (US Army R and T Labs., Cleveland)

Feb. 1978 41 p refs

(NASA-TP-1130; E-9265) Avail: NTIS HC AO3/MF A01 CSCL

131

BALL BEARINGS, ELASTOHYDRODYNAMICS, LUBRICATION,

STATISTICAL ANALYSIS

N78-20512"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

FRICTION AND WEAR OF SELECTED METALS AND ALLOYS

IN SLIDING CONTACT WITH AISI 440 C STAINLESS STEEL IN

LIQUID METHANE AND IN LIQUID NATURAL GAS

D. W. WlSANDER Feb. 1978 18 p refs

(NASA-TP-1150; E-9195) Avail: NTIS HC A02/MF A01 CSCL

20K

ALUMINUM, BERYLLIUM, COPPER, COPPER ALLOYS, iRON,

NICKEL, SLIDING FRICTION, TITANIUM, WEAR

N78-20513"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

PREDICTED AND EXPERIMENTAL PERFORMANCE OF

JET-LUBRICATED 12g-MILLIMETER-BORE BALL BEARINGS

OPERATING TO 2.5 MILLION DN

H. H. COE and E. V. ZARETSKY Apr. 1978 28 p refs

(NASA-TP-1196; E-9288) Avail: NTIS HC A03/MF A01 CSCL

131

BALL BEARINGS, COMPUTER PROGRAMS, LUBRICATION

SYSTEMS, PREDICTION ANALYSIS TECHNIQUES

N78-21470"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

CHARACTERIZATION OF WEAR DEBRIS GENERATED IN

ACCELERATED ROLLING-ELEMENT FATIGUE TESTS

W. R. JONES, JR. and R. J. PARKER Apr. 1978 28 p refs

(NASA-TP-1203; E-9260) Avail: NTIS HC A03/MF A01 CSCL

131

BALLS, CORROSION RESISTANCE, FATIGUE TESTS,

FERROMAGNETISM, MINERAL OILS

N78-21473"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

ROLLING-ELEMENT FATIGUE LIFE OF AISI M-50 AND 18-4-I

BALLS

R. J. PARKER and E. V. ZARETSKY Apr. 1978 19 p refs

(NASA-TP-1202; E-9350) Avail: NTIS HC A02/MF A01 CSCL

131

BALL BEARINGS, FATIGUE LIFE, FATIGUE TESTS, SHAFTS

(MACHINE ELEMENTS)

37 MECHANICAL ENGINEERING

N78-22377"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

FERROGRAPHIC ANALYSIS OF WEAR PARTICLES FROM

SLIDING ELASTOHYDRODYNAMIC EXPERIMENTS

W. R. JONES, JR., H. S. NAGARAJ (Mechanical Technology, Inc.,

Latham, N. Y.), and W. O. WlNER (Georgia Inst. of Tech.,

Atlanta) Apr. 1978 31 p refs

(NASA-TP-1230; E-9300) Avail: NTIS HC A03/MF A01 CSCL

20K

ELASTOHYDRODYNAMICS, FERROMAGNETISM, GRANULAR MATERIALS, STRUCTURAL ANALYSIS, WEAR

N78-25433"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

SOME EFFECTS OF COMPOSITION ON FRICTION AND WEAR

OF GRAPHITE-FIBER-REINFORCED POLYIMIDE LINERS IN

PLAIN SPHERICAL BEARINGS

H. E. SLINEY and T. P. JACOBSON May 1978 23 p refs

(NASA-TP-1229; E-9296) Avail: NTIS HC A02/MF A01 CSCL

131

BALL BEARINGS, COMPOSITE MATERIALS, FRICTION

MEASUREMENT, GRAPHITE, POLYIMIDES, REINFORCING

FIBERS, WEAR TESTS

N78-28457"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EFFECT OF FILTRATION ON ROLLING-ELEMENT-BEARING

LIFE IN CONTAMINATED LUBRICANT ENVIRONMENT

S. H. LOEWENTHAL, D. W. MOYER (Tribon Bearing Co.,

Cleveland), and J. J. SHERLOCK (Tribon Bearing Co., Cleveland)

Jul. 1978 34 p refs

(NASA-TP-1272; E-9418) Avail: NTIS HC A03/MF A01 CSCL

131

FATIGUE LIFE, FILTRATION, ROLLER BEARINGS

N78-28458"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

ELASTOHYDRODYNAMIC LUBRICATION OF ELLIPTICAL

CONTACTS FOR MATERIALS OF LOW ELASTIC MODULUS.

2: STARVED CONJUNCTION

B. J. HAMROCK and D. DOWSON (Leeds Univ., England) Jul.

1978 26 p refs Proposed for presentation at the Joint

Lubrication Conf., Minneapolis, 24-26 Oct. 1978; sponsored by

the Am. Soc. of Lubrication Engr. and the Am. Soc. of Mech.

Engr.

(NASA-TP-1273; E-9558) Avail: NTIS HC A03/MF A01 CSCL

11H

CONTACT RESISTANCE, FILM THICKNESS, LUBRICANTS,

PRESSURE DISTRIBUTION

N78-30585"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio,

EFFECT OF GEOMETRY ON HYDRODYNAMIC FILM

THICKNESS

D. E. BREWE (AVRADCOM Res. and Technol. Labs.), B. J.

HAMROCK, and C. M TAYLOR (Leeds Univ., England) Aug.

1978 36 p refs Proposed for presentation at ASLE-ASME

Joint Lubrication Conf., Minneapolis, 24-26 Oct. 1978

(NASA-TP-1287; E-9347; AVRADCOM-TR-78-18) Avail: NTIS

HC A03/MF A01 CSCL 20K

BEARINGS, FILM THICKNESS, HYDRODYNAMICS,

ISOTHERMAL PROCESSES

N78-33447"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

MINIMUM FILM THICKNESS IN ELLIPTICAL CONTACTS FOR

DIFFERENT REGIMES OF FLUID-FILM LUBRICATION

B. J. HAMROCK and D. DOWSON (Leeds Univ., Engl.) Oct.

1978 25 p refs

(NASA-TP-1342; E-9687) Avail: NTIS HC A02/MF A01 CSCL

11H

ELASTOHYDRODYNAMICS, FILM THICKNESS, FLUID FILMS,

LUBRICATION

119
37 MECHANICAL ENGINEERING

N79-10424"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

COMPRESSIBLE FLOW ACROSS NARROW PASSAGES:

COMPARISON OF THEORY ANO EXPERIMENT FOR FACE

SEALS

G. P. ALLEN, D. W. WISANDER, and W. F. HADY Nov. 1978

19 p refs

(NASA-TP-1346; E-9120) Avail: NTIS HC A02/MF A01 CSCL

11A

COMPRESSIBLE FLOW, FLUID FLOW, LEAKAGE, SEALS

(STOPPERS)

N79-10425"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

ANISOTROPIC FRICTION AND WEAR OF SINGLE-CRYSTAL

MANGANESE-ZINC FERRITE IN CONTACT WITH ITSELF

K. MIYOSHI (Kanazawa Univ,, Japan) and D. H. BUCKLEY Oct.

1978 23p refs

(NASA-TP-1339; E-9673) Avail: NTIS HC A02/MF A01 CSCL

20L

ANISOTROPY, COEFFICIENT OF FRICTION, FERRITES,

MANGANESE ALLOYS, SINGLE CRYSTALS, ZINC ALLOYS

N79-13369"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

PERFORMANCE OF A NASVYTIS MULTIROLLER TRACTION

DRIVE

S. H. LOEWENTHAL, N. E. ANDERSON (AVRADCOM Res. and

Technol. Labs.), and A. L. NASVYTIS (Transmission Res., Inc.)

Nov. 1978 36 p refs

(NASA-TP-1378; E-9632; AVRADCOM-TR-78-36) Avail: NTIS

HC A03/MF A01 CSCL 131

MECHANICAL DRIVES, TRACTION

N79-14386"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

FRICTION AND TRANSFER OF COPPER, SILVER, AND GOLD

TO IRON IN THE PRESENCE OF VARIOUS ADSORBED

SURFACE FILMS

D. H. BUCKLEY Jan. 1979 19 p refs

(NASA-TP-1392; E-9684) Avail: NTIS HC A02/MF A01 CSCL

20K

ELECTRON TRANSITIONS, IRON, METAL SURFACES,

NOBLE METALS, SLIDING FRICTION

N79-14387"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

FRICTION AND WEAR CHARACTERISTICS OF

IRON-CHROMIUM ALLOYS IN CONTACT WITH THEMSELVES

AND SILICON CARBIDE

K. MIYOSHt and D. H. BUCKLEY Jan. 1979 23 p refs

(NASA-TP-1387; E-9670) Avail: NTIS HC A02/MF A01 CSCL

20K

CHROMIUM ALLOYS, IRON ALLOYS, SLIDING FRICTION,

WEAR

N79-14389"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EVALUATION OF CBS 600 CARBURIZED STEEL AS A GEAR

MATERIAL

D. P. TOWNSEND, R. J. PARKER, and E. V. ZARETSKY Jan.

1979 27 p refs

(NASA-TP-1390; E-9651) Avail: NTIS HC A03/MF A01 CSCL

131

CARBURIZING, FATIGUE (MATERIALS), GEARS, STEELS

120

N79-17227"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

FRICTION AND WEAR WITH A SINGLE-CRYSTAL ABRASIVE

GRIT OF SILICON CARBIDE IN CONTACT WITH IRON BASE

BINARY ALLOYS IN OIL: EFFECTS OF ALLOYING ELEMENT

AND ITS CONTENT

K. MIYOSHI (Kanazawa Univ., Japan) and D. H. BUCKLEY Feb.

1979 19 p

(NASA-TP-1394; E-9765) Avail: NTIS HC A02/MF A01 CSCL

20K

ABRASION, IRON ALLOYS, SILICON CARBIDES, SLIDING

FRICTION, SURFACE PROPERTIES, WEAR TESTS

N79-18323"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

OPERATING CHARACTERISTICS OF A LARGE-BORE ROLLER

BEARING TO SPEEDS OF 3 TIMES 10 TO THE 6TH POWER

DN

F. T. SCHULLER Feb. 1979 32 p refs

(NASA-TP-1413; E-9657) Avail: NTIS HC A03/MF A01 CSCL

131

ROLLER BEARINGS, ROLLING CONTACT LOADS

N79-21352"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

THE 12TH AEROSPACE MECHANISMS SYMPOSIUM

Apr. 1979 241 p refs Syrup. held at Moffett Field, Calif.,

27-28 Apr. 1978; sponsored in part by NASA, Calif. Inst. of Tech.

and Lockheed

(NASA-CP-2080; A-7737) Avail: NTIS HC A11/MF A01 CSCL

20K

AEROSPACE ENGINEERING, CONFERENCES, MECHANICAL

DEVICES, MECHANICAL ENGINEERING

N79-21374"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

THE 11TH AEROSPACE MECHANISMS SYMPOSIUM

28 Apr. 1977 243 p refs Syrup. held at Greenbelt, Md.,

28-29 Apr. 1977; Sponsored by NASA, LMSC, and Calif. Inst. of

Technol.

(NASA-CP-2038) Avail: NTIS HC All/MF A01 CSCL 20K

AEROSPACE ENGINEERING, CONFERENCES

N79-22518*# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

OPERATING CHARACTERISTICS OF A CANTILEVER-MOUNTED

RESILIENT-PAD GAS-LUBRICATED THRUST BEARING

Z. N. NEMETH Washington Apr. 1979 30 p refs

(NASA-TP-1438; E-9815) Avait: NTIS HC A03/MF A01 CSCL

131

CANTILEVER BEAMS, GAS BEARINGS, THRUST BEARINGS

N79-22519"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

COMPARISON OF ANALYSIS AND EXPERIMENT FOR

SELF-ACTING SEALS FOR LIQUID-OXYGEN TURBOPUMPS

G. P. ALLEN Apr. 1979 15 p refs

(NASA-TP-1443; E-9806) Avail: NTIS HC A02/MF A01 CSCL

13t

LIQUID OXYGEN, SEALS (STOPPERS), TURBINE PUMPS

N79-31604"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EVALUATION OF HIGH-CONTACT-RATIO SPUR GEARS WITH

PROFILE MODIFICATION

D. P. TOWSEND, B. B. BABER (Southwest Research Inst., San

Antonio, Tex.), and A. NAGY (Southwest Research Inst., San

Antonio, Tex.) Sep. 1979 24 p refs

(NASA-TP-1458; E-9949) Avail: NTIS HC A02/MF A01 CSCL

131

CONTACT POTENTIALS, FATIGUE TESTS, GEAR TEETH,

GEARS, SURFACE PROPERTIES
37 MECHANICAL ENGINEERING

N79-31605"# National Aeronautics and Space Administration. N80-19495"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio. Lewis Research Center, Cleveland, Ohio.

FERROGRAPHIC ANALYSIS OF WEAR DEBRIS FROM DAMPING IN TAPERED ANNULAR SEALS FOR AN

FULL-SCALE BEARING FATIGUE TESTS INCOMPRESSIBLE FLUID

W. R. JONES, JR. and S. H. LOEWENTHAL Sep. 1979 19 p D.P. FLEMING Apr. 1980 22 p refs

refs (NASA-TP-1646; E-124) Avail: NTIS HC A02/MF A01 CSCL

(NASA-TP-1511; E-9827) Avail: NTIS HC A02/MF A01 CSCL 11A

131 DAMPING, DYNAMIC RESPONSE, INCOMPRESSIBLE

BALL BEARINGS, FATIGUE TESTS, WEAR FLUIDS, O RING SEALS

N79-32552"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

COMPARISON OF PREDICTED AND MEASURED

ELASTOHYDRODYNAMIC FILM THICKNESS IN A

20-MILLIMETER-BORE BALL BEARING

J. J. COY, R. S. R. GORLA (Cleveland State Univ., Ohio), and D.

P. TOWNSEND Oct. 1979 29 p refs

(NASA-TP-1542; AVRADCOM-TR-79-20; E-9992) Avail: NTIS

HC A03/MF A01 CSCL 131

BALL BEARINGS, ELASTOHYDRODYNAMICS, FILM

THICKNESS, LUBRICATION

N79-33475"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

TRACTION DRIVE PERFORMANCE PREDICTION FOR THE

JOHNSON AND TEVAARWERK TRACTION MODEL

J. L. TEVAARWERK Washington Oct. 1979 41 p refs

(NASA-TP-1530; E-033) Avail: NTIS HC A03/MF A01 CSCL

131

MECHANICAL DRIVES, PERFORMANCE PREDICTION,

RHEOLOGY, TRACTION

N79-33476"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

CORRELATION OF ASPERITY CONTACT-TIME FRACTION

WITH ELASTOHYDRODYNAMIC FILM THICKNESS IN A

20-MILLIMETER-BORE BALL BEARING

J. J. COY Washington Oct. 1979 21 p refs

(NASA-TP-1547; AVRADCOM-TR-79-26) Avail: NTIS HC

A02/MF A01 CSCL 131

BALL BEARINGS, ELASTOHYDRODYNAMICS, FILM

THICKNESS, LUBRICATION

N80-14403"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

SELF-ACTING LIFT-PAD GEOMETRY FOR CIRCUMFERENTIAL

SEALS: A NONCONTACTING CONCEPT

G. P. ALLEN Jan. 1980 11 p refs

(NASA-TP-1583; E-154) Avail: NTIS HC A02/MF A01 CSCL

11A

HYDRODYNAMICS, PERFORMANCE TESTS, SEALS

(STOPPERS)

N80-15410"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

COMPARISON OF PREDICTED AND EXPERIMENTAL

PERFORMANCE OF LARGE-BORE ROLLER BEARING

OPERATING TO 3.0 MILLION DN

H. H. COE and F. T. HULLER Jan. 1980 20 p refs

(NASA-TP-1599; E-063) Avail: NTIS HC A02/MF A01 CSCL

131

HEAT TRANSFER, HIGH SPEED, LUBRICATION SYSTEMS,

PERFORMANCE PREDICTION, ROLLER BEARINGS

N80-17466"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

SPUR-GEAR-SYSTEM EFFICIENCY AT PART AND FULL LOAD

N. E. ANDERSON and S. H. LOEWENTHAL Feb. 1980 42 p

refs Prepared in cooperation with Army Aviation Res. and Develop.

Command, Cleveland

(NASA-TP-1622; AVRADCOM-TR-79-46; E-061) Avail: NTIS HC

A03/MF A01 CSCL 131

GEAR TEETH, GEARS, ROLLING CONTACT LOADS

N80-21753"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

OPERATING CHARACTERISTICS OF HIGH-SPEED,

JET-LUBRICATED 35-MILLIMETER-BORE BALL BEARING

WITH A SINGLE-OUTER-LAND-GUIDED CAGE

F. T. SCHULLER, S. I. PINEL (Industrial Tectonics, Inc.), and H.

R. SIGNER (Industrial Tectonics, Inc.) Washington Apr. 1980

16 p refs

(NASA-TP-1657; E-220) Avail: NTIS HC A02/MF A01 CSCL

13t

BALL BEARINGS, GAS TURBINE ENGINES, LUBRICATION,

SHAFTS (MACHINE ELEMENTS)

N80-27694"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

RELEASE MECHANISM FOR RELEASING AND REATTACHING

EXPERIMENTS ON THE SPACE SHUTTLE

A. V. CLARK Jul. 1980 21 p

(NASA-TP-1702; M-301) Avail: NTIS HC A02/MF A01 CSCL

22B

LATCHES, MECHANICAL DRIVES, POSITIONING DEVICES

(MACHINERY), RELEASING, REMOTE CONTROL, SPACE

SHUTTLE PAYLOADS

N80-29706"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

ROTORDYNAMIC INSTABILITY PROBLEMS IN

HIGH-PERFORMANCE TURBOMACHINERY

1980 463 p refs Conf. held at College Station, 12-14 May

1980; sponsored by Texas A and M Univ., Louisville Univ., and

AROD

(NASA-CP-2133; E-413) Avail: NTIS HC A20/MF A01 CSCL

131

CONFERENCES, ROTARY STABILITY, TURBOMACHINERY

N80-29734"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

LUBRICATION OF OPTIMIZED-DESIGN TAPERED-ROLLER

BEARINGS TO 2.4 MILLION DN

R. J. PARKER, S. I. PINEL, and HANS R. SIGNER Aug. 1980

18 p refs Sponsored in part by Industrial Tectonics, Inc.,

Compton, Calif.

(NASA-TP-1714; E-270) Avail: NTIS HC A02/MF A01 CSCL

131

COMPUTER AIDED DESIGN, FLOW VELOCITY, HIGH SPEED,

LUBRICATION, ROLLER BEARINGS, TAPERING

N80-33749"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EFFECT OF CAGE DESIGN ON CHARACTERISTICS OF

HIGH-SPEED-JET-LUBRICATED 35-MILLIMETER-BORE BALL

BEARING

F. T. SCHULLER, S. I. PINEL (Industrial Tectonics, Compton, Calif.),

and H. R. SIGNER (Industrial Tectonics, Compton, Calif.) Oct.

1980 13 p refs

(NASA-TP-1732; E-289) Avail: NTIS HC A02/MF A01 CSCL

131

BALL BEARINGS, HIGH SPEED, LUBRICATION, ROLLER

BEARINGS, SHAFTS (MACHINE ELEMENTS), TURBOJET

ENGINES

121
37 MECHANICAL ENGINEERING

N81-14322"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

COMPARISONS OF MODIFIED VASCO X-2 AND AISI 9310 GEAR

STEELS

D. P. TOWNSEND and E. V. ZARETSKY Nov. 1980 19 p

refs

(NASA-TP-1731; E-070) Avail: NTIS HC A02/MF A01 CSCL

131

FATIGUE (MATERIALS), GEARS, HARDNESS TESTS,

TRANSMISSIONS (MACHINE ELEMENTS), VACUUM MELTING

N81-19458"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

PERFORMANCE OF JET- AND INNER-RING-LUBRICATED 35

MILLIMETER BORE BALL BEARINGS OPERATING TO 2.5

MILLION DN

F. SCHULLER, T. and H. R. SIGNER Feb. 1981 15 p refs

(NASA-TP-1808; E-515) Avail: NTIS HC A02/MF A01 CSCL

131

BALL BEARINGS, COOLING, LUBRICATION, PERFORMANCE

TESTS

N81-20423"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

LIFE ANALYSIS OF MULTIROLLER PLANETARY TRACTION

DRIVE

J. J. COY (Army Aviation Research and Development Command,

Cleveland, Ohio), D. A. ROHN, and S. H. LOEWENTHAL Apr.

1981 16 p refs Prepared in cooperation with Army Aviation

Research and Development Command, Cleveland

(NASA-TP-1710; AVRADCOM-TR-80-C-16; E-484) Avail: NTIS

HC A02/MF A01 CSCL 131

BALL BEARINGS, FATIGUE LIFE, MECHANICAL DRIVES,

ROLLER BEARINGS, TRACTION

N82-25514"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

FRICTIONAL HEATING DUE TO ASPERITY INTERACTION OF

ELASTOHYDRODYNAMIC LINE-CONTACT SURFACES

B. C. MAJUMDAR and B. J. HAMROCK May 1982 23 p refs

Presented at the ASME-ASLE Joint Lubrication Conf., New Orleans,

5-7 Oct. 1981

(NASA-TP-1882; E-897; NAS 1.60:1882) Avail: NTIS HC

A02/MF A01 CSCL 20K

ELASTOHYDRODYNAMICS, ENERGY DISSIPATION, FRICTION, LUBRICATION, SURFACE ROUGHNESS, TEMPERATURE

GRADIENTS

N82-26678"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

MULTIROLLER TRACTION DRIVE SPEED REDUCER:

EVALUATION FOR AUTOMOTIVE GAS TURBINE ENGINE

D. A. ROHN, N. E. ANDERSON, and S. H. LOEWENTHAL Jun.

1982 24 p refs Prepared in cooperation with Army Aviation

Research and Development Command, Cleveland, Ohio

(NASA-TP-2027; E-1002; NAS 1.60:2027;

AVRADCOM-TR-81-C-11) Avail: NTIS HC A02/MF A01 CSCL

20A

AUTOMOBILE ENGINES, GAS TURBINE ENGINES, SPEED

CONTROL, TRACTION, TRANSMISSIONS (MACHINE

ELEMENTS)

N82-31691"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

INFLUENCE OF CORROSIVE SOLUTIONS ON

MICROHARDNESS AND CHEMISTRY OF MAGNESIUM OXIDE

/0011 SURFACES

H. ISHIGAKI (Osaka Univ.), K. MIYOSHI, and D. H. BUCKLEY

Aug. 1982 11 p refs

(NASA-TP-2040; E-1035; NAS 1.60:2040) Avail: NTIS HC

A02/MF A01 CSCL 20K

CORROSION, MAGNESIUM OXIDES, MICROHARDNESS,

SURFACE PROPERTIES

122

N82-32736"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EFFECT OF SHOT PEENING ON SURFACE FATIGUE LIFE OF

CARBURIZED AND HARDENED AISI 9310 SPUR GEARS

D. P. TOWNSEND and E. V. ZARETSKY Aug. 1982 14 p

refs

(NASA-TP-2047; E-936; NAS 160:2047) Avail: NTIS HC

A02/MF A01 CSCL 131

FATIGUE LIFE, GEAR TEETH, RESIDUAL STRESS, SHOT

PEENING

N82-32737"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

WEAR MECHANISM BASED ON ADHESION

T. YAMAMOTO and D. H. BUCKLEY Aug. 1982 13 p refs

(NASA-TP-2037; E-1118; NAS 1.60:2037) Avail: NTIS HC

A02/MF A01 CSCL 11A

ADHESION, SLIDING FRICTION, WEAR

N83-11496"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

PLASTIC DEFORMATION AT SURFACE DURING

UNLUBRICATED SLIDING

T. YAMAMOTO (Tokyo Univ.) and D. H. BUCKLEY Oct. 1982

20 p refs

(NASA-TP-2036; E-1036; NAS 1.60:2036) Avail: NTIS HC

A02/MF A01 CSCL 20K

ALUMINUM OXIDES, PLASTIC DEFORMATION, SLIDING,

STAINLESS STEELS, WEAR

N83-13457"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

ROLLING-ELEMENT FATIGUE LIFE WITH TRACTION FLUIDS

AND AUTOMATIC TRANSMISSION FLUID IN A HIGH-SPEED

ROLLING-CONTACT RIG

R. J. PARKER, A. H. NAHM (General Electric Co., Cincinnati),

and S. H. LOEWENTHAL Nov. 1982 16 p refs

(NAS3-20832)

(NASA-TP-2050; E-1091; NAS 1.60:2050) Avail: NTIS HC

A02/MF A01 CSCL 131

BEARINGS, FATIGUE LIFE, LUBRICANTS, ROLLING

CONTACT LOADS, TRACTION, TRANSMISSION FLUIDS

N83-15629"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

ROTORDYNAMIC INSTABILITY PROBLEMS IN

HIGH-PERFORMANCE TURBOMACHINERY

Washington Dec. 1982 460 p refs Workshop held in

College Station, Tex., 10-12 May t982; sponsored by Texas A

and M Univ. and the Army Research Office

(NASA-CP-2250; E-1287; NAS 1.55:2250) Avail: NTIS HC

A20/MF A01 CSCL 131

CONTROL THEORY, CRACKS, DYNAMIC CHARACTERISTICS, MECHANICAL PROPERTIES, ROTORS, STABILITY, TURBOMACHINERY, VIBRATION TESTS

N83-16758"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

ROLLING-ELEMENT FATIGUE LIFE OF AMS 5900 BALLS

R. J. PARKER Jan. 1983 13 p refs

(NASA-TP-2080; E-1190; NAS 1.60:2080) Avail: NTIS HC

A02/MF A01 CSCL 131

BALL BEARINGS, FATIGUE LIFE, FATIGUE TESTS,

STAINLESS STEELS
37 MECHANICAL ENGINEERING

N83-16759"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EL&STOHYDRODYNAMIC LUBRICATION OF RECTANGULAR

CONTACTS

B. J. HAMROCK and B. O. JACOBSON (Lulea Univ.) Jan. 1983

30 p refs

(NASA-TP-2111; E-1277; NAS 1.60:2111) Avail: NTIS HC

A03/MF A01 CSCL 11H

ELASTOHYDRODYNAMICS, ISOTHERMAL PROCESSES,

LUBRICATION, RECTANGLES, SLIDING FRICTION

N83-33166"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EFFECT OF CARBIDE DISTRIBUTION ON ROLLING-ELEMENT

FATIGUE LIFE OF AMS 5749

R J. PARKER and E. N. BAMBERGER (GE, Cincinnati) Aug.

1983 14 p refs

(NASA-TP-2189; E-1243; NAS 1.60:2189) Avail: NTIS HC

A02/MF A01 CSCL 131

BEARING ALLOYS, CARBIDES, CORROSION RESISTANCE,

FATIGUE LIFE, ROLLER BEARINGS

N83-20119"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

ADVANCED POWER TRANSMISSION TECHNOLOGY

G. K. FISCHER, ed. Jan. 1983 541 p refs Proc. of syrup.

held in Cleveland, Ohio, 9-11 Jun. 1981 Sponsored in cooperation

with Army Aviation Research and Development Command

(NASA-CP-2210; E-817; NAS 1.55:2210;

AVRADCOM-TR-82-C-16) Avail: NTIS HC A23/MF A01 CSCL

131

CONFERENCES, ROLLER BEARINGS, TRACTION,

TRANSMISSIONS (MACHINE ELEMENTS)

N83-24862"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

REGRESSION ANALYSIS OF TRACTION CHARACTERISTICS

OF TRACTION FLUIDS

S. H. LOEWENTHAL and D. A. ROHN May 1983 17 p refs

(NASA-TP-2154; E-1300; NAS 1.60:2154) Avail: NTIS HC

A02/MF A01 CSCL 11H

CORRELATION COEFFICIENTS, ELASTOHYDRODYNAMICS,

LUBRICANTS, REGRESSION ANALYSIS, SLIDING, TRACTION

N83-27214"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

ROLLING-ELEMENT BEARINGS

B. J. HAMROCK and W. J. ANDERSON (Bearings and Lubrication,

North Olmsted, Ohio) Jun. 1983 61 p refs Submitted for

publication

(NASA-RP-1105; E-1440; NAS 1.61:1105) Avail: NTIS HC

A04/MF A01 CSCL 13t

Rolling element bearings are a precision, yet simple, machine

element of great utility. A brief history of rolling element bearings

is reviewed and the type of rolling element bearings, their geometry

and kinematics, as well as the materials they are made from and

the manufacturing processes they involve are described. Unloaded

and unlubricated rolling element bearings, loaded but unlubricated

rolling element bearings and loaded and lubricated rolling element

bearings are considered. The recognition and understanding of

elastohydrodynamic lubrication covered, represents one of the

major development in rolling element bearings. S.L.

N83-28453"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

ELASTOHYDRODYNAMIC CONTACTS. EFFECTS OF DENTS

ANO GROOVES ON TRACTION AND LOCAL FILM

THICKNESS

L. D. WEDEVEN and C_ CUSANO (Illinois Univ., Urbana) Jun.

1983 19p refs

(NASA-TP-2175; E-1333; NAS 1.60:2175) Avail: NTIS HC

A02/MF A01 CSCL 11H

ELASTOHYDRODYNAMICS, FILM THICKNESS, GROOVES,

SLIDING FRICTION, SURFACE DEFECTS, TRACTION

N83-35400"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

CAVITATION PITTING AND EROSION OF ALUMINUM 6061-1"6

IN MINERAL OIL WATER

B. C. S. RAO (Indian Inst. of Science) and D. H. BUCKLEY Aug.

1983 9 p refs Presented at ASME Cavitation and Polyphase

Flow Forum, Houston, Tex., 20-22 Jun. 1983

(NASA-TP-2146; E-1516; NAS 1.60:2146) Avail: NTIS HC

A02/MF A01 CSCL 11F

ALUMINUM, CAVITATION CORROSION, EROSION,

METAL-WATER REACTIONS, MINERAL OILS, PITTING

N84-13577"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

MEASUREMENT OF ROLLING FRICTION BY A DAMPED

OSCILLATOR

M. DAYAN and D. H. BUCKLEY Dec. 1983 8 p refs

(NASA-TP-2257; E-1583; NAS 1.60:2257) Avail: NTIS HC

A02/MF A01 CSCL 20K

FRICTION MEASUREMENT, OSCILLATION DAMPERS,

ROLLING CONTACT LOADS

N84-17590"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EFFECTS OF DIFFERENT RUB MODELS ON SIMULATED

ROTOR DYNAMICS

A. F. KASCAK and J. J. TOMKO Feb. 1984 12 p refs

Presented at the ASME Appl. Mech., Bioeng., and Fluids Eng.

Conf., Houston, Tex., 20-22 Jun. 1983 Prepared in cooperation

with Army Research and Technology Labs., Cleveland

(NASA-TP-2220; E-1801; NAS 1.60:2220; AFSCOM-TR-83-C-8;

AD-A138495) Avail: NTIS HC A02/MF A01 CSCL 131

ROTARY STABILITY, ROTOR AERODYNAMICS, ROTOR

BLADES (TURBOMACHINERY), TRANSIENT RESPONSE

N84-18653"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

MECHANISM OF LUBRICATION BY TRICRESYLPHOSPHATE

(TCP)

O. D. FAUT (Wilkes Coll., Wilkes-Barre, Pa.) and D. H. BUCKLEY

Feb. 1984 13 p refs

(NASA-TP-2274; E-1846; NAS 1.60:2274) Avail: NTIS HC

A02/MF A01 CSCL 11H

COEFFICIENT OF FRICTION, LUBRICATION, PHOSPHATES,

STEELS, TEMPERATURE DEPENDENCE

N84-18654"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

COMPARISON OF PREDICTED AND EXPERIMENTAL THERMAL

PERFORMANCE OF ANGULAR-CONTACT BALL BEARINGS

R. J. PARKER Feb. 1984 19 p refs

(NASA-TP-2275; E-1751; NAS 1.60:2275) Avail: NTIS HC

A02/MF A01 CSCL 131

BALL BEARINGS, LUBRICANTS, THERMAL STRESSES

123
37 MECHANICAL ENGINEERING

N84-23891"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

TRIBOLOGY IN THE 80'S. VOLUME 1: SESSIONS 1 TO 4

Apr. 1984 508 p refs Conf. held at NASA. Lewis Research

Center, 18-21 Apr. 1983 2 Vol.

(NASA-CP-2300-VOL-I; E-1559; NAS 1.55:2300-VOL-1) Avail:

NTIS HC A22/MF A01 CSCL 11H

ADHESIVE BONDING, FRICTION, METAL-METAL BONDING,

PREDICTION ANALYSIS TECHNIQUES, RHEOLOGY, SURFACE

PROPERTIES, TRIBOLOGY, WEAR

N84-25047"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

TRIBOLOGY IN THE 80'S. VOLUME 2: SESSIONS 5 - 8

Aug. 1984 377 p refs Conf. held in Cleveland, 18-21 Apr.

1983 2 Vol.

(NASA-CP-2300-VOL-2; E-1559; NAS 1.55:2300-VOL-2) Avail:

NTIS HC A17/MF A01 CSCL 131

ADHESION, CONFERENCES, FRICTION, LUBRICATING OILS,

MATERIALS SCIENCE, SOLID LUBRICANTS, TRIBOLOGY, WEAR

TESTS

N84-27041"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

DESIGN OF POWER-TRANSMI'n'ING SHIFTS

S. H. LOEWENTHAL Jul. 1984 26 p refs Submitted for

publication

(NASA-RP-1123; E-1899; NAS 1.6t:1123) Avail: NTIS HC

A03/MF A01 CSCL 131

Power transmission shafting which is a vital element of all

rotating machinery is discussed. Design methods, based on

strength considerations for sizing shafts and axles to withstand

both steady and fluctuating loads are summarized. The effects of

combined bending, torsional, and axial loads are considered along

with many application factors that are known to influence the

fatigue strength of shafting materials. Methods are presented to

account for variable amplitude loading histories and their influence

on limited life designs. The influences of shaft rigidity, materials,

and vibration on the design are discussed E.A.K.

N84-29226"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

OPERATING CHARACTERISTICS OF A THREE-PIECE-INNERRING LARGE-BORE ROLLER BEARING TO SPEEDS OF 3 MILLION DN

F. T. SCHULLER Aug. 1984 21 p refs

(NASA-TP-2355; E-1806; NAS 1.60:2355) Avail: NTIS HC

A02/MF A01 CSCL 131

LUBRICANTS, PERFORMANCE PREDICTION, ROLLER

BEARINGS, TEMPERATURE EFFECTS

N84-31640"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

LUBRICATION OF MACHINE ELEMENTS

B. J. HAMROCK Aug. 1984 92 p refs Submitted for

publication

(NASA-RP-1126; E-1949; NAS 1.61:1126) Avail: NTIS HC

A05/MF A01 CSCL 131

The understanding of hydrodynamic lubrication began with the

classical experiments of Tower and Petrov. Reynolds used a

reduced form of the Navier-Stokes equations and the continuity

equation to generate a second order differential equation for the

pressure in the narrow, converging gap of a bearing contact. Such

a pressure enables a load to be transmitted between the surfaces

with very low friction since the surfaces are completely separated

by a film of fluid. In such a situation it is the physical properties

of the lubricant, notably the dynamic viscosity, that dictate the

behavior of the contact. The understanding of boundary lubrication

is normally attributed to Hardy and Doubleday. In boundary

lubrication it is the physical and chemical properties of thin films

of molecular proportions and the surfaces to which they are

attached that determine contact behavior. The lubricant viscosity

is not an influential parameter. Research is devoted to a better

124

understanding and more precise definition of other lubrication

regimes between these extremes. One such regime,

elastohydrodynamic lubrication, occurs in nonconformal contacts,

where the pressures are high and the bearing surfaces deform

elastically, In this situation the viscosity of the lubricant may raise

considerably, and this further assists the formation of an effective

fluid film. The science of these three lubrication regimes

(hydrodynamic, etastohydrodynamic, and boundary) are described

and the manner in which this science is used in the design of

machine elements is examined. M.A.C.

N84-32824"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

THERMAL ANALYSIS OF A PLANETARY TRANSMISSION WITH

SPHERICAL ROLLER BEARINGS OPERATING AFTER

COMPLETE LOSS OF OIL

H.H. COE Sep. 1984 14p refs

(NASA-TP-2367; E-2008; NAS 1.60:2367) Avail: NTIS HC

A02/MF A01 CSCL 131

LOSSES, OILS, ROLLER BEARINGS, THERMAL ANALYSIS,

TRANSMISSIONS (MACHINE ELEMENTS)

N84-32825"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

CHARACTERIZATION OF EROSION OF METALLIC MATERIALS

UNDER CAVITATION ATTACK IN A MINERAL OIL

B. C. S. RAO (Indian Inst. of Science, Bangalore, India) and D. H.

BUCKLEY Sep. 1984 14 p refs

(NASA-TP-2368; E-2049; NAS 1.60:2368) Avail: NTIS HC

A02/MF A01 CSCL 11F

CAVITATION CORROSION, CRYSTAL STRUCTURE,

EROSION, METAL CRYSTALS, MINERAL OILS

N85-13233"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EFFECT OF TWO INNER-RING OIL-FLOW DISTRIBUTION

SCHEMES ON THE OPERATING CHARACTERISTICS OF A 35

MILLIMETER BORE BALL BEARING TO 2.5 MILLION DN

F. T. SCHULLER, S. I. PINEL (Industrial Tectonics, Inc., Rancho

Dominquez, Calif.), and H. R SIGNER (Industrial Tectonics, Inc.,

Rancho Dominquez, Calif.) Jan. 1985 14 p refs

(NAS3-19779)

(NASA-TP-2404; E-2127; NAS 1.60:2404) Avail: NTIS HC

A02/MF A01 CSCL 13t

BALL BEARINGS, FLOW DISTRIBUTION, HIGH SPEED,

LUBRICATING OILS, ROLLER BEARINGS

N85-13234"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EFFECT OF LUBRICANT EXTREME-PRESSURE ADDITIVES ON

SURFACE FATIGUE LIFE OF AlSl 9310 SPUR GEARS

H. W. SCtBBE, D. P. TOWNSEND, and P. R ARON Dec. 1984

14 p refs

(NASA-TP-2408; E-2042; NAS 1.60:2408) Avail: NTIS HC

A02/MF A01 CSCL 13t

ADDITIVES, FATIGUE LIFE, GEARS, LUBRICANTS, STEELS

N85-14116"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

ROTORDYNAMIC INSTABILITY PROBLEMS IN

HIGH-PERFORMANCE TURBOMACHINERY

Washington Dec. 1984 507 p refs Workshop held in

College Station, Tex., 28-30 May 1984; sponsored by Texas A&M

Univ., Army Research Office, and the Air Force Aeroproputsion

Lab.

(NASA-CP-2338; E-2214; NAS 1.55:2338) Avail: NTIS HC

A22/MF A01 CSCL 131

CONFERENCES, FLUID POWER, HYDRODYNAMICS, ROTOR

AERODYNAMICS, STABILITY, TURBOMACHINERY
N85-20339"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

APPLICATIONS OF TETHERS IN SPACE, VOLUME 1

A. C. CRON, comp. (General Research Corp., McLean, Va.)

Washington Mar. 1985 283 p refs Workshop held in

Williamsburg, Va., 15-17 Jun. 1983 2 Vol.

(NAS8-35403)

(NASA-CP-2364; M-475; NAS 1.55:2364) Avail: NTIS HC

A13/MFA01 CSCL 131

CONFERENCES, ORBITAL SERVICING, SPACE STATIONS,

SPACE TRANSPORTATION, TETHERED SATELLITES,

TETHERING

N85-20361"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

APPLICATIONS OF TETHERS IN SPACE, VOLUME 2

A. C. CRON, comp. (General Research Corp., McLean, Va.)

Washington Mar. 1985 319 p refs Workshop held in

Williamsburg, Va., 15-17 Jun. 1983 2 Vol.

(NAS8-35403)

(NASA-CP-2365; M-476; NAS 1.55:2365) Avail: NTIS HC

AI,I/MI: A(31 _SCL 131

CONFERENECES, ELECTRODYNAMICS, ELECTROMAGNETIC INTERACTIONS, PLASMA DIAGNOSTICS, SPACE TRANSPORTATION SYSTEM, TETHERED SATELLITES

N85-21659"# General Research Corp., McLean, Va.

APPLICATIONS OF TETHERS IN SPACE Executive Summary

A. C. CRON 1985 69 p Workshop held in Williamsburg, Va.,

15-17 Jun. 1983

(NAS8-35408)

(NASA-CP-2366; NAS 1.55:2366) Avail: NTIS HC A04/MF A01

CSCL 22A

TECHNOLOGY UTILIZATION, TETHERED SATELLITES,

TETHERLINES

N85-31511"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EFFECT OF SPEED AND PRESS FIT ON FATIGUE LIFE OF

ROLLER-BEARING INNER-RACE CONTACT

H. H. COE and E. V. ZARETSKY Jul. 1985 13 p refs

(NASA-TP-2496; E-2476; NAS 1.60:2496) Avail: NTIS HC

A02/MF A01 CSCL 131

FATIGUE LIFE, ROLLER BEARINGS, ROLLING CONTACT

LOADS, STRESS ANALYSIS

N85-32329"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

SURFACE ROUGHNESS EFFECTS IN ELASTOHYDRODYNAMIC

CONTACTS

J. H. TRIPP (Case Western Reserve Univ.) and B. J. HAMROCK

Jul. 1985 14 p refs Presented at the 11th Leeds-Lyon Symp.

on Mixed Lubrication and Lubricated Wear, Leeds, Engl., 4-7 Sep.

1984

(NASA-TP-2488; E-2524; NAS 1.60:2488) Avail: NTIS HC

A02/MF A01 CSCL 20K

ELASTOHYDRODYNAMICS, FRICTION, LUBRICATION,

SURFACE ROUGHNESS

N85-32330"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

MECHANICS OF A GASEOUS FILM BARRIER TO LUBRICANT

WETTING OF ELASTOHYDRODYNAMICALLY LUBRICATED

CONJUNCTIONS

J. M. PRAHL (Case Western Reserve Univ.) and B. J. HAMROCK

Aug. 1985 17 p refs Presented at the 11th Leeds-Lyon

Symp. on Mixed Lubrication and Lubricated Wear, Leeds, Engl.,

4-7 Sep. 1984

(NCC3-30)

(NASA-TP-2500; E-2523; NAS 1.60:2500) Avail: NTIS HC

A02/MF A01 CSCL 20K

BALL BEARINGS, DYNAMIC MODELS, ELASTOHYDRODY37 MECHANICAL ENGINEERING

NAMICS, GAS DYNAMICS, GAS-LIQUID INTERACTIONS, HYDRODYNAMICS, LUBRICATION, WETTING

N85-32331"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

HERTZIAN CONTACT IN TWO AND THREE DIMENSIONS

J. H. TRIPP (Case Western Reserve Univ.) Jul. 1985 27 p

refs

(NASA-TP-2473; E-2256; NAS 1.60:2473) Avail: NTIS HC

A03/MF A01 CSCL 20K

ELASTIC DEFORMATION, INTERRACIAL TENSION,

STRESS-STRAIN RELATIONSHIPS, TRIBOLOGY

N86-12609"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

SURFACE FATIGUE LIFE AND FAILURE CHARACTERISTICS

OF EX-53, CBS 1000M, AND AISI 9310 GEAR MATERIALS

D. P. TOWNSEND Oct. 1985 14 p refs

(NASA-TP-2513; E-2578; NAS 1.60:2513) Avail: NTIS HC

A02/MF A01 CSCL 131

AMBIENT TEMPERATURE, FAILURE ANALYSIS, FATIGUE

LIFE, FRACTURING, GEAR TEETH, GEARS, LOADS (FORCES),

ROLLING CONTACT LOADS, STEELS, SURFACE REACTIONS

N86-13734"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

DESIGN OF TRACTION DRIVES

S. H. LOEWENTHAL and E. V. ZARETSKY Oct. 1985 49 p

refs Submitted for publication

(NASA-RP-1154; E-2143; NAS 1.61:1154) Avail: NTIS HC

A03/MF A01 CSCL 131

Traction drives are among the simplest of all speed-changing

mechanisms. Because of their simplicity and their ability to smoothly

and continuously adjust speed, they are excellent choices for many

drive system applications. They have been used in industrial service

for more than 100 years. Today's traction drives have power

capacities which rival the best gear and belt drives due to modern

traction fluids and highly fatigue-resistant bearing steels. This report

summarizes methods to analyze and size traction drives. Lubrication

principles, contact kinematics, stress, fatigue life, and performance

prediction methods are presented. The effects of the lubricant's

traction characteristics on life and power loss are discussed. An

example problem is given which illustrates the effects of spin on

power loss. Loading mechanism design and the design of

nonlubricated friction wheels and rings are also treated. Author

N86-14612"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

GEARING

J. J. COY (Army Aviation Research and Technology Activity,

Cleveland, Ohio), D. P. TOWNSEND, and E. V. ZARETSKY Dec.

1985 70p refs

(NASA-RP-1152; E-2003; NAS 1.61:1152; AVSCOM-TR-84-C-15)

Avail: NTIS HC A04/MF A01 CSCL 131

Gearing technology in its modern form has a history of only

100 years. However, the earliest form of gearing can probably be

traced back to fourth century B.C. Greece. Current gear practice

and recent advances in the technology are drawn together. The

history of gearing is reviewed briefly in the Introduction. Subsequent

sections describe types of gearing and their geometry, processing,

and manufacture. Both conventional and more recent methods of

determining gear stress and deflections are considered. The

subjects of life prediction and lubrication are additions to the

literature. New and more complete methods of power loss

predictions as well as an optimum design of spur gear meshes

are described. Conventional and new types of power transmission

systems are presented. Author

125
37 MECHANICAL ENGINEERING

N86-24992"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

TESTING OF YUH-61A HELICOPTER TRANSMISSION IN NASA

LEWIS 2240-KW (3000-HP FACILITY

A. M. MITCHELL, F. B. OSWALD, and F. T. SCHULLER Mar.

1986 28 p refs

(NASA-TP-2538; E-2801; NAS 1.60:2538) Avail: NTIS HC

A03/MF A01 CSCL 01C

GEARS, HELICOPTERS, TRANSMISSIONS (MACHINE

ELEMENTS), VIBRATION

N86-25794"# National Aeronautics and Space Administration,

Washington, D.C.

PROCEEDINGS OF A WORKSHOP ON APPLICATIONS OF

TETHERS IN SPACE: EXECUTIVE SUMMARY

W. A. BARACAT, Compiler 1986 43 p Proc. held in Venice,

Italy, 15-17 Oct. 1985

(NASW-3921)

(NASA-CP-2422; NAS 1.55:2422) Avail: NTIS HC A03/MF A01

CSCL 131

SPACE STATIONS, TETHERED SATELLITES, TETHERLINES

N86-27644"# National Aeronautics and Space Administration,

Washington, D.C.

APPLICATIONS OF TETHERS IN SPACE: WORKSHOP

PROCEEDINGS, VOLUME 2

W. A. BARACAT, comp. (General Research Corp., McLean, Va.)

Jun. 1986 502 p Workshop held in Venice, Italy, 15-17 Oct.

1985; sponsored by NASA, the Italian National Space Plan and

CNR

(NASW-3921)

(NASA-CP-2422-VOL-2; NAS 1.55:2422-VOL-2) Avail: NTIS HC

A23/MF A01 CSCL 131

REDUCED GRAVITY, SPACE PROCESSING, SPACE SHUTTLE

PAYLOADS, SPACE STATIONS, TETHERED SATELLITES,

TETHERLINES

N88-28407"# National Aeronautics and Space Administration,

Washington, D.C.

APPLICATIONS OF TETHERS IN SPACE: WORKSHOP

PROCEEDINGS, VOLUME 1

W. A. BARACAT, comp. (General Research Corp., McLean, Va.)

Jun. 1986 585 p Workshop held in Venice, Italy, 15-17 Oct.

1985; sponsored by NASA, the Italian National Space Plan and

CNR

(NASW-3921)

(NASA-CP-2422-VOL-1; NAS 1.55:2422-VOL-1) Avail: NTIS HC

A25/MF A01 CSCL 131

ELECTRODYNAMICS, TECHNOLOGY UTILIZATION, TETHERED SATELLITES, TETHERLINES

N88-30160"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

INSTABILITY IN ROTATING MACHINERY

Dec. 1985 458 p Symposium held in Carson City, Nev., 10-14

Jun. 1985; sponsored by Bently Rotor Dynamics Research Corp.

(NASA-CP-2409; E-2652; NAS 1.55:2409) Avail: NTIS HC

A21/MF A01 CSCL 131

ANTIFRICTION BEARINGS, INTERNAL FRICTION, LOAD

TESTS, ROTARY STABILITY, TURBOMACHINERY, VIBRATION

MEASUREMENT

126

38

QUALITY ASSURANCE AND RELIABILITY

Includes product sampling procedures and techniques; and quality

control.

N85-23090"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

RELIABILITY BOUNDS FOR FAULT-TOLERANT SYSTEMS

WITH COMPETING RESPONSES TO COMPONENT FAILURES

L. D. LEE Apr. t985 16 p refs

(NASA-TP-2409; L-15853; NAS 1.60:2409) Avail: NTIS HC

A02/MF A01 CSCL 14D

COMPONENT RELIABILITY, FAILURE, FAULT TOLERANCE,

MARKOV CHAINS

N86-22962"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

ANALYTICAL ULTRASONICS IN MATERIALS RESEARCH AND

TESTING

A. VARY Jan. 1986 357 p refs Conference held in

Cleveland, Ohio, 13-14 Nov. 1984

(NASA-CP-2383; E-2486; NAS 1.55:2383) Avail: NTIS HC

A16/MF A01 CSCL 20A

ACOUSTIC EMISSION, COMPOSITE MATERIALS,

CONFERENCES, NONDESTRUCTIVE TESTS, ULTRASONIC

RADIATION, ULTRASONICS, WAVE PROPAGATION

N86-26639"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

EVALUATION OF MULTILAYER PRINTED WIRING BOARDS BY

METALLOGRAPHIC TECHNIQUES: AN ILLUSTRATED GUIDE

TO THE PREPARATION AND INSPECTION OF

PLATED-THROUGH HOLE TEST COUPONS BASED ON THE

REQUIREMENTS OF MIL-P-55110D

J. JELLISON May 1986 72 p refs

(NASA-RP-1161; REPT-86B0088; NAS 1.61:1161) Avail: NTIS

HC A04/MF A01 CSCL 14D

This work is an illustrated handbook containing the rationale

and procedure for the evaluation of multilayer printed wiring board

construction integrity with respect to plated-through holes in

accordance with the requirements of MIL-P-55110D, Printed Wiring

Boards. It is intended as a practical aid for those concerned with

determining the construction integrity of multilayer boards for high

reliability applications. Photomicrographs of cross sectioned holes

illustrate defect types, acceptable and unacceptable conditions,

and methods of measurement. A procedure for specimen

preparation is given, and appropriate paragraphs of the military

specification are included and explained. Author

N86-32763"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

A METHOD FOR DEVELOPING DESIGN DIAGRAMS FOR

CERAMIC AND GLASS MATERIALS USING FATIGUE DATA

T. M. HESLIN, M. B. MAGIDA, and K. A. FORREST Sep. 1986

55 p

(NASA-RP-1174; NAS 1.61:1174) Avail: NTIS HC A04/MF A01

CSCL 14D

The service lifetime of glass and ceramic materials can be

expressed as a plot of time-to-failure versus applied stress whose

plot is parametric in percent probability of failure. This type of plot

is called a design diagram. Confidence interval estimates for such

plots depend on the type of test that is used to generate the

data, on assumptions made concerning the statistical distribution

of the test results, and on the type of analysis used. This report

outlines the development of design diagrams for glass and ceramic

materials in engineering terms using static or dynamic fatigue tests,

assuming either no particular statistical distribution of test results

or a Weibull distribution and using either median value or

homologous ratio analysis of the test results. Author
39

STRUCTURAL MECHANICS

Includes structural element design and weight analysis; fatigue;

and thermal stress.

N78-12443"# National Aeronautics and Space Administration,

Washington, D.C.

SIXTH NASTRAN USERS' COLLOQUIUM

Oct. 1977 473 p refs Colloq. held at Cleveland, 4-6 Oct.

1977

(NASA-CP-2018; E-9303) Avail: NTIS HC A20/MF A01 CSCL

20K

COMPUTER PROGRAMS, CONFERENCES, FINITE ELEMENT

METHOD, NASTRAN, STRUCTURAL ANALYSIS, USER

MANUALS (COMPUTER PROGRAMS)

N78-12475"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECT OF END-RING STIFFNESS ON BUCKLING OF

PRESSURE-LOADED STIFFENED CONICAL SHELLS

R. C. DAVIS and J. G. WILLIAMS Washington Dec. 1977 33

p refs

(NASA-TP-1079; L-11915) Avail: NTIS HC A03/MF A01

CSCL 20K

BUCKLING, COMPRESSION LOADS, CONICAL SHELLS,

STIFFENING

N78-18459"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

DEVELOPMENT AND APPLICATION OF AN OPTIMIZATION

PROCEDURE FOR FLUTTER SUPPRESSION USING THE

AERODYNAMIC ENERGY CONCEPT

E. NISSIM (Technion - Israel Inst, of Tech,) and I. ABEL Feb.

1978 39 p refs

(NASA-TP-1137; L-11909) Avail: NTIS HC A03/MF A01

CSCL 20K

FLUTTER ANALYSIS, GUSTS, TRANSFER FUNCTIONS, WING

OSCILLATIONS

N78-20536"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

GAUSSIAN STEP-PRESSURE LOADING OF RIGID

VlSCOPLASTIC PLATES Ph.D. Thesis

R. J. HAYDUK and B. J. DURLING Mar. 1978 28 p refs

(NASA-TP-1123; L-11885) Avail: NTIS HC A03/MF A01

CSCL 20K

CIRCULAR PLATES, LOADS (FORCES), NORMAL DENSITY

FUNCTIONS, PRESSURE DISTRIBUTION, VISCOELASTICITY

N78-26494"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

LIGHT AIRPLANE CRASH TESTS AT THREE FLIGHT-PATH

ANGLES

C. B. CASTLE and E. ALFARO-BOU Jun. 1978 69 p refs

Films supplement number L-1247 to this report is available on

request

(NASA-TP-1210; L-12060) Avail: NTIS HC A04/MF A01

CSCL 01C

AIRCRAFT ACCIDENTS, CRASH LANDING, FLIGHT PATHS,

IMPACT TESTS

39 STRUCTURAL MECHANICS

N78-28480"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EXPERIMENTAL STUDIES OF EFFECTS OF TILT AND

STRUCTURAL ASYMMETRY ON VIBRATION CHARACTERISTICS OF THIN-WALL CIRCULAR CYLINDERS PARTLY FILLED

WITH LIQUID

R. W. HERR Jul. 1978 41 p refs

(NASA-TP-1211; L-12049) Avail: NTIS HC A03/MF A01

CSCL 20K

ATTITUDE (INCLINATION), CIRCULAR CYLINDERS, LIQUID

FILLED SHELLS, THIN WALLS, VIBRATION

N78-28481"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ANALYSIS OF PREFLUTTER AND POSTFLUTTER

CHARACTERISTICS WITH MOTION-MATCHED AERODYNAMIC

FORCES

H, J. CUNNINGHAM JuL 1978 33 p refs

(NASA-TP-1232; L-12109) Avail: NTIS HC AO3/MF A01

CSCL 01C

AERODYNAMIC FORCES, AEROELASTICITY, FLUTTER

ANALYSIS, LIFT DEVICES, PREDICTION ANALYSIS

TECHNIQUES

N78-28482"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EVALUATION OF A HYBRID, ANISOTROPIC, MULTILAYERED,

QUADRILATERAL FINITE ELEMENT

J. C. ROBINSON and C. L. BLACKBURN (Tenn. Univ. at

Nashville) Aug. 1978 31 p refs

(NASA-TP-1236; L-12113) Avail: NTIS HC A03/MF A01

CSCL 02K

BEAMS (SUPPORTS), DYNAMIC STRUCTURAL ANALYSIS,

FINITE ELEMENT METHOD, LAMINATES, PLATES

(STRUCTURAL MEMBERS)

N78-30610"# National Aeronautics and Space Administration.

Lyndon B. Johnson Space Center, Houston, Tax.

MICROSTRUCTURE AND MECHANICAL PROPERTIES OF

QUENCHED AND TEMPERED 300M STEEL

J. L. YOUNGBLOOD and M. RAGHAVAN Aug. 1978 40 p

refs

(NASA-TP-1288; JSC-13854; S-483) Avail: NTIS HC A03/MF

A01 CSCL 11F

HIGH STRENGTH STEELS, LANDING GEAR, MECHANICAL

PROPERTIES, MICROSTRUCTURE, QUENCHING (COOLING),

SPACE SHUTTLE ORBITERS

N78-32466"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

SEVENTH NASTRAN USER'S COLLOQUIUM

Oct. 1978 499 p refs Colloquium held at Huntsville, Ala., 4-6

Oct. 1978

(NASA-CP-2062) Avail: NTIS HC A21/MF A01 CSCL 20K

CONFERENCES, NASTRAN, STRUCTURAL ANALYSIS

N78-32492"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

BUCKLING AND STRUCTURAL EFFICIENCY OF

SANDWICH-BLADE STIFFENED COMPOSITE COMPRESSION

PANELS

M. STEIN and J. G. WILLIAMS Sep. 1978 40 p refs

(NASA-TP-1269; L-12242) Avail: NTIS HC A03/MF A01

CSCL 20K

BLADES, COMPOSITE STRUCTURES, CREEP BUCKLING,

SANDWICH STRUCTURES, STRUCTURAL FAILURE

127
39 STRUCTURAL MECHANICS

N79-10448"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

RESEARCH IN COMPUTERIZED STRUCTURAL ANALYSIS AND

SYNTHESIS

H. G. MCCOMB, JR., comp. Oct. 1978 224 p refs Presented

at a Symp. on Future Trends in Computerized Structural Analysis

and Syn., Washington, D. C., 30 Oct. - 1 Nov. 1978; sponsored

by George Washington Univ. and NSF and the Am. Soc. of Civil

Engrs.

(NASA-CP-2059; L-12507) Avail: NTIS HC A10/MF A01

CSCL 20K

COMPUTER AIDED DESIGN, COMPUTERIZED SIMULATION,

DYNAMIC STRUCTURAL ANALYSIS

N79-17264"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AN ANALYTICAL TECHNIQUE FOR PREDICTING THE

CHARACTERISTICS OF A FLEXIBLE WING EQUIPPED WITH

AN ACTIVE FLUTTER-SUPPRESSION SYSTEM AND

COMPARISON WITH WIND-TUNNEL DATA

I. ABEL Feb. 1979 45 p refs

(NASA-TP-1367; L-12567) Avail: NTIS HC A03/MF A01

CSCL 20K

FLEXIBLE WINGS, FLUTTER ANALYSIS, PERFORMANCE

PREDICTION, VIBRATION DAMPING, WIND TUNNEL TESTS

N79-21422"# National Aeronautics and Space Administration.

Langley Research Cen_er, Hampton, Va.

RECENT ADVANCES IN STRUCTURES FOR HYPERSONIC

FLIGHT, PART 1

1978 533 p refs Symp. held at Hampton, Va., 6-8 Sep. 1978

(NASA-CP-2065-PT-1; L-12653-PT-1) Avail: NTIS HC A23/MF

A01 CSCL 20K

AIRCRAFT DESIGN, AIRCRAFT STRUCTURES,

CONFERENCES, HYPERSONIC AIRCRAFT, STRUCTURAL

DESIGN

N79-21435"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

RECENT ADVANCES IN STRUCTURES FOR HYPERSONIC

FLIGHT, PART 2

1978 408 p refs Symp. held at Hampton, Va., 6-8 Sep. 1978

(NASA-CP-2065-PT-2; L-12653-PT-2) Avail: NTIS HC A18/MF

A01 CSCL 20K

ANIONS, CONFERENCES, HYPERSONIC FLIGHT

N79-22539"# National Aeronautics and Space Administration.

Lyndon B. Johnson Space Center, Houston, Tex.

THE 13TH AEROSPACE MECHANISMS SYMPOSIUM

A. C. BOND 1979 300 p refs Proc. of Symp. held at

Houston, Tex., 26-27 Apr. 1979

(NASA-CP-2081; S-496) Avail: NTIS HC A13/MF A01 CSCL

13t

AERONAUTICAL ENGINEERING, CONFERENCES, ELECTROMECHANICAL DEVICES, EXPERIMENT DESIGN, MECHANICAL

DEVICES

N79-24372"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

VIBRATION CHARACTERISTICS OF WALLS AND A PLATE

GLASS WINDOW REPRESENTATIVE OF THOSE OF A

WOOD-FRAME HOUSE

H. D. CARDEN May 1979 53 p refs

(NASA-TP-1447; L-12729) Avail: NTIS HC A04/MF A0t

CSCL 20K

CONSTRUCTION MATERIALS, VIBRATION EFFECTS,

WOODEN STRUCTURES

128

N79-25427"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

APPROXIMATION METHODS FOR COMBINED THERMAL/

STRUCTURAL DESIGN

R. T. HAFTKA (Illinois Inst. of Tech.) and C. P. SHORE Jun.

1979 35p refs

(NASA-TP-1428; L-t2674) Avail: NTIS HC A03/MF A01

CSCL 20K

APPROXIMATION, INSULATED STRUCTURES, STRUCTURAL

DESIGN CRITERIA, THERMAL STRESSES

N79-28614"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

A METHOD FOR OBTAINING PRACTICAL

FLUTTER-SUPPRESSION CONTROL LAWS USING RESULTS

OF OPTIMAL CONTROL THEORY

J. R. NEWSON Aug. 1979 34 p refs

(NASA-TP-1471; L-12728) Avail: NTIS HC A03/MF A01

CSCL 20K

AEROELASTICITY, CONTROL THEORY, FLUTTER, OPTIMAL

CONTROL, VIBRATION DAMPING

N79-31626"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

A CRITICAL EXAMINATION OF STRESSES IN AN ELASTIC

SINGLE LAP JOINT

P. A. COOPER and J. W. SAWYER Sep. 1979 61 p refs

(NASA-TP-1507; L-12802) Avail: NTIS HC AO4/MF A01

CSCL 20K

FINITE ELEMENT METHOD, LAP JOINTS, NUMERICAL

ANALYSIS, STRESS ANALYSIS

N79-33500"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

LOAD CONCENTRATION DUE TO MISSING MEMBERS IN

PLANAR FACES OF A LARGE SPACE TRUSS

J. E. WALTZ Washington Oct. 1979 39 p refs

(NASA-TP-1522; L-12872) Avail: NTIS HC A03/MF A01

CSCL 20K

LARGE SPACE STRUCTURES, LOADS (FORCES), STRESS

CONCENTRATION, TRUSSES

N80-10512"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

LIGHT AIRPLANE CRASH TESTS AT THREE ROLL ANGLES

C. B. CASTLE and E. ALFARO-BOU Washington Oct. 1979

77 p refs

(NASA-TP-1477; L-12778) Avail: NTIS HC A05/MF A01

CSCL 01C

CRASHES, GENERAL AVIATION AIRCRAFT, IMPACT TESTS,

ROLL

N80-11505"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

LIGHT AIRPLANE CRASH TESTS AT THREE PITCH ANGLES

V. L. VAUGHAN, JR. and E. ALFARO-BOU Nov. 1979 62 p

refs

(NASA-TP-1481) Avail: NTIS HC A04/MF A01 CSCL 01C

CRASH LANDING, GENERAL AVIATION AIRCRAFT, IMPACT

TESTS, LIGHT AIRCRAFT

N80-12438"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

PRELIMINARY DESIGN PROCEDURE FOR INSULATED

STRUCTURES SUBJECTED TO TRANSIENT HEATING

H. M. ADELMAN Washington Dec. 1979 53 p refs

(NASA-TP-1534; L-13144) Avail: NTIS HC A04/MF A01

CSCL 20L

AIRFRAME MATERIALS, REENTRY SHIELDING, THERMAL

INSULATION, TRANSIENT HEATING
N80-13512"#National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ANALYSIS OF SURFACE CRACKS IN FINITE PLATES UNDER

TENSION OR BENDING LOADS

J. C. NEWMAN, JR. and I. S. RAJU (Joint Inst. for the Advancemer_t

of Flight Sciences, Hampton, Va.) Dec. 1979 46 p refs

(NASA-TP-1578; L-13053) Avail: NTIS HC A03/MF A01

CSCL 20K

BENDING FATIGUE, ELASTIC PLATES, FINITE ELEMENT

METHOD, STRESS ANALYSIS, SURFACE CRACKS, TENSILE

STRESS

N80-15428"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

A RELATION BETWEEN SEMIEMPIRICAL FRACTURE

ANALYSES AND R-CURVES

T. W. ORANGE Jan. 1980 45 p refs

(NASA-TP-1600; E-9963) Avail: NTIS HC A03/MF A01 CSCL

20K

FAILURE ANALYSIS, FRACTURE MECHANICS, FRACTURE

STRENGTH

N80-18427"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

STRESS ANALYSIS AND BUCKLING OF J-STIFFENED

GRAPHITE-EPOXY PANEL

R. C. DAVIS Washington Feb. 1980 23 p refs

(NASA-TP-1607; L-13256) Avail: NTIS HC A02/MF A01

CSCL 20K

BUCKLING, GRAPHITE-EPOXY COMPOSITES, RIGID

STRUCTURES, STRESS ANALYSIS

N80-19563"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

HYDROELASTIC VIBRATION ANALYSIS OF PARTIALLY

LIQUID-FILLED SHELLS USING A SERIES REPRESENTATION

OF THE LIQUID

J. M. HOUSNER, R. W. HERR, and J. L. SEWALL Mar. 1980

68 p rafs

(NASA-TP-1558; L-13279) Avail: NTIS HC A04/MF A01

CSCL 20K

HYDROELASTICITY, LIQUID FILLED SHELLS, PROPELLANT

TANKS, SERIES (MATHEMATICS), STRUCTURAL VIBRATION

N80-20619"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

ON THE NONLINEAR DEFORMATION GEOMETRY OF

EULER-BERNOULLI BEAMS

D. H. HODGES, R. A. ORMISTON, and D. A. PETERS Apr.

1980 57p refs

(NASA-TP-1566; A-7985; AVRADCOM-TR-80-A-1) Avail: NTIS

HC A04/MF A01 CSCL 20K

DEFORMATION, NONLINEAR SYSTEMS, ROTARY WINGS,

ROTATING BODIES

N80-22734"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

NONLINEAR, THREE-DIMENSIONAL FINITE-ELEMENT

ANALYSIS OF AIR-COOLED GAS TURBINE BLADES

A. KAUFMAN and R. E. GAUGLER Apr. 1980 22 p refs

(NASA-TP-1669; E-074) Avail: NTIS HC A02/MF A01 CSCL

21E

AIR COOLING, FINITE ELEMENT METHOD, GAS TURBINES,

TURBINE BLADES

39 STRUCTURAL MECHANICS

N80-22737"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

APPLICATION OF TWO DESIGN METHODS FOR ACTIVE

FLUTTER SUPPRESSION AND WIND-TUNNEL TEST RESULTS

J. R. NEWSOM, I. ABEL, and H. J. DUNN May 1980 84 p

refs

(NASA-TP-1653; L-13177) Avail: NTIS HC A05/MF A01

CSCL 20L

AERODYNAMICS, CONTROL THEORY, ENERGY METHODS,

FLUTTER, OPTIMAL CONTROL, WIND TUNNEL TESTS

N80-23677"# National Aeronautics and Space Administration.

Dryden (Hugh L.) Flight Research Center, Edwards, Calif.

ELASTIC CONSTANTS FOR SUPERPLASTICALLY

FORMED/DIFFUSION-BONDED CORRUGATED SANDWICH

CORE

W. L. KO May 1980 82p refs

(NASA-TP-1562; H-1094) Avail: NTIS HC A05/MF A01 CSCL

20K

DIFFUSION WELDING, ELASTIC PROPERTIES, SANDWICH

STRUCTURES, STRUCTURAL STABILITY, SUPERPLASTICITY

N80-24648"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

EIGHTH NASTRAN USER'S COLLOQUIUM

May 1980 242 p refs Colloq. held at Greenbelt, Md, 30-31

Oct. 1979

(NASA-CP-2131) Avail: NTIS HC A11/MF A01 CSCL 20K

CONFERENCES, FINITE ELEMENT METHOD, NASTRAN

N80-27719"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

COMPARISON OF ELASTIC AND ELASTIC-PLASTIC

STRUCTURAL ANALYSES FOR COOLED TURBINE BLADE

AIRFOILS

A. KAUFMAN Jul. 1980 15 p refs

(NASA-TP-1679; E-241) Avail: NTIS HC A02/MF A01 CSCL

20K

AIRFOILS, ELASTOPLASTICITY, STRESS-STRAIN RELATIONSHIPS, STRUCTURAL ANALYSIS, TURBINE BLADES

N80-32756"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

RESEARCH IN NONLINEAR STRUCTURAL AND SOLID

MECHANICS

H. G. MCCOMB, JR., comp. and A. K. NOOR, comp. (Joint Inst.

for Advancement of Flight Sciences, Hampton, Va.) 1980 287

p refs Symp. on Computational Methods in Nonlinear Struct.

and Solid Mech. held in Washington, D.C., 6-8 Oct. 1980; sponsored

by NASA, George Washington Univ., NSF, ASCE and ASME

(NASA-CP-2147; L-13950) Avail: NTIS HC A13/MF A01

CSCL 20K

DEFORMATION, MATHEMATICAL MODELS, NEWTON

THEORY, NONLINEAR SYSTEMS, SOLID MECHANICS,

STRUCTURAL ANALYSIS

N80-33782"# National Aeronautics and Space Administration.

John F. Kennedy Space Center, Cocoa Beach, Fla.

NINTH NASTRAN USERS' COLLOQUIUM

Oct. 1980 248 p refs Colloq. held in Cocoa Beach, Fla.,

22-23 Oct. 1980

(NASA-CP-2151) Avail: NTIS HC All/MF A01 CSCL 20K

CONFERENCES, FINITE ELEMENT METHOD, NASTRAN,

STRUCTURAL ANALYSIS

N81-11417"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

METHOD FOR ESTIMATING CRACK-EXTENSION RESISTANCE

CURVE FROM RESIDUAL STRENGTH DATA

T. W. ORANGE Nov. 1980 15 p refs

(NASA-TP-1753; E-439) Avail: NTIS HC A02/MF A01 CSCL

20K

CRACKING (FRACTURING), FAILURE ANALYSIS, FRACTURE

STRENGTH, LOADS (FORCES)

129
39 STRUCTURAL MECHANICS

N81-11422"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AN ANALYTICAL TECHNIQUE FOR APPROXIMATING

UNSTEADY AERODYNAMICS IN THE TIME DOMAIN

H. J. DUNN Nov. 1980 31 p refs

(NASA-TP-1738; L-13255) Avail: NTIS HC A03/MF A01

CSCL 20K

AERODYNAMIC FORCES, AEROELASTICITY, LEAST

SQUARES METHOD, MATHEMATICAL MODELS, PADE

APPROXIMATION, WING LOADING

N81-13373"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

A NEW LOOK AT NUMERICAL ANALYSES OF FREE-EDGE

STRESSES IN COMPOSITE LAMINATES

I. S. RAJU, J. D. WHITCOMB, and J. G. GOREE (Clemson Univ.)

Dec. 1980 37 p refs

(NASA-TP-1751; L-13777) Avail: NTIS HC A03/MF A01

CSCL 20K

GRAPHITE-EPOXY COMPOSITES, NUMERICAL ANALYSIS,

STRESSES

N81-14343"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

VIBRATION CHARACTERISTICS OF A STEADILY ROTATING

SLENDER RING

F. J. LALLMAN Dec. 1980 100 p refs

(NASA-TP-t775; L-t3386) Avail: NTIS HC A05/MF A01

CSCL 20K

DYNAMIC RESPONSE, SPACECRAFT DESIGN, VIBRATION

MODE

N81-22388"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

THE 15TH AEROSPACE MECHANISMS SYMPOSIUM

1981 433 p refs Symp. held in Huntsville, Ala., 14-15 May

198t; sponsored in part by California Inst. of Technology and

Lockheed Missiles and Space Co., Inc.

(NASA-CP-2181) Avail: NTIS HC A19/MF A01 CSCL 20K

ACTUATORS, ANTENNAS, CONFERENCES, DEPLOYMENT

EGRESS, ESCAPE SYSTEMS, EXTRAVEHICULAR ACTIVITY

LARGE SPACE STRUCTURES, MECHANICAL DRIVES

REFLECTORS, SPACE ERECTABLE STRUCTURES

SPACECRAFT CONTROL, SPACECRAFT PROPULSION

SPACECREWS

N81-23486"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

MEGA16 - COMPUTER PROGRAM FOR ANALYSIS AND

EXTRAPOLATION OF STRESS-RUPTURE DATA

C. R. ENSIGN May 1981 46 p refs

(NASA-TP-1809; E-495) Avail: NTIS HC A03/MF A01 CSCL

20K

COMPUTER PROGRAMS, CREEP RUPTURE STRENGTH,

EXTRAPOLATION, FAILURE ANALYSIS, RELIABILITY ANALYSIS,

STRESS ANALYSIS

N81-24471"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

STATIC AND YAWED-ROLLING MECHANICAL PROPERTIES OF

TWO TYPE 7 AIRCRAFT TIRES

J. A. TANNER, S. M STUBBS, and J. L. MCCARTY May 1981

80 p refs

(NASA-TP-1863; L-14125) Avail: NTIS HC A05/MF A01

CSCL 20K

AIRCRAFT TIRES, MECHANICAL PROPERTIES, ROLLING

MOMENTS, STATIC LOADS, YAWING MOMENTS

N81-71592" National Aeronautics and Space Administration,

Washington, D.C.

THE NASTRAN DEMONSTRATION PROBLEM MANUAL, LEVEL

17.5

Dec. 1978 185p refs

(NASA-SP-224(05))

130

N81-71594" National Aeronautics and Space Administration,

Washington, D.C.

THE NASTRAN PROGRAMMERS MANUAL, LEVEL 17.5

Dec. 1978 845 p refs

(NASA-SP-223(05))

N82-10430"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

CORNERING CHARACTERISTICS OF THE NOSE-GEAR TIRE

OF THE SPACE SHUTTLE ORBITER

W. A. VOGLER (Kentron International, Inc., Hampton, Va.) and J.

A. TANNER Oct. 1981 29 p refs

(NASA-TP-1917; L-14681) Avail: NTIS HC A03/MF A01

CSCL 20K

AERODYNAMIC CHARACTERISTICS, LANDING GEAR, NOSE

TIPS, SPACE SHUTTLE ORBITERS

N82-11488"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AN IMPROVED TRANSVERSE SHEAR DEFORMATION THEORY

FOR LAMINATED ANTISOTROPIC PLATES

M. V. V. MURTHY Nov. 1981 39 p refs

(NASA-TP-1903; L-14533) Avail: NTIS HC A03/MF A01

CSCL 20K

ANISOTROPIC PLATES, ELASTIC BENDING, LAMINATES,

SHEAR STRESS

N82-11489"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

RESEARCH IN NONLINEAR STRUCTURAL AND SOLID

MECHANICS

H. G. MCCOMB, JR., comp. and A. K. NOOR, comp. (Joint Inst.

for Advancement of Flight Sciences) Jun. 1981 44 p refs

Presented at Symp. held at Washington, D.C., 6-8 Oct. 1980;

Sponsored by George Washington Univ., NSF, American Society

of Civil Engineers and ASME

(NASA-CP-2147°SUPPL; L-13950) Avail: NTIS HC A03/MF A01

CSCL 20K

COMPUTER AIDED DESIGN, MECHANICAL ENGINEERING,

SOLID MECHANICS, STRUCTURAL ENGINEERING

N82-20565"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

ELASTIC-PLASTIC FINITE-ELEMENT ANALYSES OF

THERMALLY CYCLED SINGLE-EDGE WEDGE SPECIMENS

A. KAUFMAN Mar. 1982 27 p refs

(NASA-TP-1982; E-687; NAS 1.60:1982) Avail: NTIS HC

A03/MF A01 CSCL 20K

ELASTOPLASTICITY, FLUIDIZED BED PROCESSORS,

STAINLESS STEELS, STRESS-STRAIN RELATIONSHIPS,

THERMAL CYCLING TESTS, WEDGES

N82-20566"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

ELASTIC-PLASTIC FINITE-ELEMENT ANALYSES OF

THERMALLY CYCLED DOUBLE-EDGE WEDGE SPECIMENS

A. KAUFMAN and L. E. HUNT Mar. 1982 31 p refs

(NASA-TP-1973; E-626; NAS 1.60:1973) Avail: NTIS HC

A03/MF A01 CSCL 20K

ALLOYS, ELASTIC PROPERTIES, ENGINE PARTS, FINITE

ELEMENT METHOD, PLASTIC PROPERTIES, STRESS

ANALYSIS, STRESS-STRAIN RELATIONSHIPS, THERMAL

CYCLING TESTS, WEDGES

N82-20567"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

DESIGN DETAIL VERIFICATION TESTS FOR A LIGHTLY

LOAOED OPEN-CORRUGATION GRAPHITE-EPOXY CYLINDER

R. C. DAVIS and J. H. STARNES, JR. Mar. 1982 26 p refs

(NASA-TP-1981; L-14795; NAS 1.60:1981) Avail: NTIS HC

A03/MF A01 CSCL 20K

CORRUGATED SHELLS, CYLINDRICAL SHELLS,

GRAPHITE-EPOXY COMPOSITES, LOAD TESTS
N82-28703"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

COMPARISON OF ANALYTICAL AND WIND-TUNNEL RESULTS

FOR FLUTTER AND GUST RESPONSE OF A TRANSPORT WING

WITH ACTIVE CONTROLS

I. ABEL, B. PERRY, III, and J. R. NEWSOM Jun. 1982 47 p

refs

(NASA-TP-2010; L-15099; NAS 1.60:2010) Avail: NTIS HC

A03/MF A0t CSCL 01C

ACTIVE CONTROL, AEROELASTICITY, DAMPING, DYNAMIC

RESPONSE, FLUTTER, GUST LOADS, WING LOADING

N82-28665"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

BUCKLING TEST OF A 3-METER-DIAMETER CORRUGATED

GRAPHITE-EPOXY RING-STIFFENED CYLINDER

R.C. DAVIS Jul. 1982 28p refs

(NASA-TP-2032; L-14659; NAS 1.60:2032) Avail: NTIS HC

A03/MF A01 CSCL 20K

BUCKLING, CORRUGATED SHELLS, CYLINDRICAL SHELLS,

GRAPHITE-EPOXY COMPOSITES, REINFORCEMENT RINGS

N82-33739"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

RESEARCH IN STRUCTURAL AND SOLID MECHANICS, 1982

Research-in-Progress Reports

J. M. HOUSNER, comp. and A. K. NOOR, comp. (George

Washington Univ., Washington, D.C.) Oct. 1982 427 p refs

Proc. of Symp. on Advan. and Trends in Struct. and Solid Mech.,

Washington, D.C., 4-7 Oct. 1982; sponsored in cooperation with

NSF, AFOSR, ONR, American Society of Civil Engineers and

American Society of Mechanical Engineers

(NASA-CP-2245; L-15506; NAS 1.55:2245) Avail: NTIS HC

A19/MF A01 CSCL 20K

BOUNDARY ELEMENT METHOD, DEGREES OF FREEDOM,

DYNAMIC RESPONSE, ELASTOPLASTICITY, IMPACT

STRENGTH, NONLINEAR EQUATIONS, RELAXATION

(MECHANICS), SOLID MECHANICS, STRUCTURAL ANALYSIS

N83-10442"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

CRASH TESTS OF FOUR LOW-WING TWIN-ENGINE

AIRPLANES WITH TRUSS-REINFORCED FUSELAGE

STRUCTURE

M. S. WILLIAMS and E. L. FASANELLA (Kentron International,

Inc.) Sep. 1982 120p refs

(NASA-TP-2070; L-15379; NAS 1.60:2070) Avail: NTIS HC

A06/MF A01 CSCL 20K

AIRCRAFT SAFETY, CRASHES, CRASHWORTHINESS,

FUSELAGES, GENERAL AVIATION AIRCRAFT, IMPACT TESTS,

REINFORCEMENT (STRUCTURES), TRUSSES

N83-11513"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

FLIGHTWEIGHT RADIANTLY AND ACTIVELY COOLED PANEL:

THERMAL AND STRUCTURAL PERFORMANCE

C. P. SHORE, R. J. NOWAK, and H. N. KELLY Jan. 1982 53

p refs

(NASA-TP-2074; L-15292; NAS 1.60:2074) Avail: NTIS HC

A04/MF A01 CSCL 20K

AIRCRAFT STRUCTURES, COOLANTS, HEAT SHIELDING,

HYPERSONIC AIRCRAFT, PANELS, RADIANT COOLING

39 STRUCTURAL MECHANICS

N83-12449"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

MATERIALS CONSTITUTIVE MODELS FOR NONLINEAR

ANALYSIS OF THERMALLY CYCLED STRUCTURES

A. KAUFMAN and L. E. HUNT (Arizona Univ., Tucson) Oct.

1982 26 p refs

(NAG3-45)

(NASA-TP-2055; E-1125; NAS 1.60:2055) Avail: NTIS HC

A03/MF A01 CSCL 20K

CONSTITUTIVE EQUATIONS, INELASTIC STRESS, SERVICE

LIFE, STRUCTURAL ANALYSIS

N83-12452"# Georgia Univ., Athens. Computer Software

Management and Information Center.

TENTH NASTRAN USER'S COLLOQUIUM

Nov. 1982 273 p refs Colloq. held at New Orleans, 13-14

May 1982 Sponsored by NASA

(NASA-CP-2249; NAS 1.55:2249) Avail: NTIS HC A12/MF A01

CSCL 20K

AXISYMMETRIC FLOW, ELASTOPLASTICITY, FINITE

ELEMENT METHOD, HARMONIC FUNCTIONS, NASTRAN,

STRUCTURAL ANALYSIS

N83-14521"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

CORRELATION AND ASSESSMENT OF STRUCTURAL

AIRPLANE CRASH DATA WITH FLIGHT PARAMETERS AT

IMPACT

H. D. CARDEN Nov. 1982 44 p refs

(NASA-TP-2083; L-15431; NAS 1.60:2083) Avail: NTIS HC

A03/MF A01 CSCL 20K

AIRCRAFT ACCIDENTS, CRASH INJURIES, CRASHES,

IMPACT RESISTANCE, IMPACT TESTS

N83-16785"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

VIBRATION STUDIES OF A LIGHTWEIGHT THREE-SIDED

MEMBRANE SUITABLE FOR SPACE APPLICATION

J. L. SEWELL, R. MISERENTINO, and R. S. PAPPA Jan. 1983

49 p refs

(NASA-TP-2095; L-15247; NAS 1.60:2095) Avail: NTIS HC

A03/MF A01 CSCL 20K

DYNAMIC RESPONSE, LARGE SPACE STRUCTURES,

MEMBRANES, REFLECTORS, SPACECRAFT ANTENNAS,

STRUCTURAL VIBRATION

N83-21391"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

TIRE MODELING

J. A. TANNER, comp. Washington Mar. 1983 245 p refs

Workshop held in Hampton, Va., 7-9 Sep. 1982

(NASA-CP-2264; L-15578; NAS 1.55:2264) Avail: NTIS HC

Alt/MFA01 CSCL20K

CONFERENCES, DYNAMIC TESTS, FINITE ELEMENT

METHOD, TIRES

N83-24881"# Jet Propulsion Lab., California Inst. of Tech.,

Pasadena.

THE 17TH AEROSPACE MECHANISMS SYMPOSIUM

May 1983 390 p refs Symp. held in Pasadena, Calif., 5-6

May 1983; sponsored by NASA, California Inst. of Tech., and

LMSC

(NASA-CP-2273; NAS 1.55:2273) Avail: NTIS HC A17/MF A01

CSCL 20K

ACTUATORS, CONFERENCES, CONTROL EQUIPMENT,

DEPLOYMENT, ELECTROMECHANICAL DEVICES, SOLAR

ARRAYS, SPACECRAFT LUBRICATION, TETHERED

SATELLITES

131
39 STRUCTURALMECHANICS

N83-28491"#National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

VIBRATION CHARACTERISTICS OF A DEPLOYABLE

CONTROLLABLE-GEOMETRY TRUSS BOOM

J. T. DORSEY Jun. 1983 30 p refs

(NASA-TP-2160; L-15580; NAS 1.60:2160) Avail: NTIS HC

A03/MF A01 CSCL 20K

BOOMS (EQUIPMENT), CANTILEVER BEAMS, DEPLOYMENT,

LARGE SPACE STRUCTURES, TRUSSES, VIBRATION

N83-33216"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECT OF STRAIN ISOLATOR PAD MODULUS ON INPLANE

STRAIN IN SHUTTLE ORBITER THERMAL PROTECTION

SYSTEM TILES

J. W. SAWYER Aug. 1983 48 p refs

(NASA-TP-2141; L-15575; NAS 1.60:2141) Avail: NTIS HC

A03/MF A01 CSCL 20K

CERAMICS, CUSHIONS, HEAT SHIELDING, PAD, SPACE

SHUTTLE ORBITERS, STRAIN RATE, THERMAL PROTECTION,

TILES

N83-33217"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

TEMPERATURE DISTRIBUTION IN AN AIRCRAFT TIRE AT LOW

GROUND SPEEDS

J. L. MCCARTY and J. A. TANNER Aug. 1983 36 p refs

(NASA-TP-2195; L-15605; NAS 1.60:2195) Avail: NTIS HC

A03/MF A01 CSCL 20K

AIRCRAFT TIRES, GROUND SPEED, LOW SPEED, TAXIING,

TEMPERATURE DISTRIBUTION

N83-34351"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

NONLINEAR CONSTITUTIVE RELATIONS FOR HIGH

TEMPERATURE APPLICATIONS

Mar. 1983 360 p refs Symp. held in Akron, Ohio, 19-20 May

1982; sponsored by Akron Univ.

(NASA-CP-2271; E-1541; NAS 1.55:2271) Avail: NTIS HC

A16/MF A01 CSCL 20K

CONFERENCES, DESIGN ANALYSIS, FRACTURE

MECHANICS, REACTION KINETICS, STRUCTURAL DESIGN

CRITERIA

N83-34372"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

SIMPLIFIED METHOD FOR NONLINEAR STRUCTURAL

ANALYSIS

A. KAUFMAN Sep. 1983 15 p refs

(NASA-TP-2208; E-1646; NAS 1.60:2208) Avail: NTIS HC

A02/MF A01 CSCL 20K

CYCLIC LOADS, ELASTIC DEFORMATION, GAS TURBINE

ENGINES, STRESS-STRAIN RELATIONSHIPS, STRUCTURAL

ANALYSIS, THERMOMECHANICAL TREATMENT

N83-34373"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

A SOLUTION PROCEDURE FOR BEHAVIOR OF THICK PLATES

ON A NONLINEAR FOUNDATION AND POSTBUCKLING

BEHAVIOR OF LONG PLATES

M. STEIN and P. A. STEIN Sep. 1978 40 p refs

(NCC1-15)

(NASA-TP-2174; L-15587; NAS 1.60:2174) Avail: NTIS HC

A03/MF A01 CSCL 20K

BUCKLING, NONLINEARITY, PLATES (STRUCTURAL

MEMBERS), STRUCTURAL STRAIN

132

N84-13614"# National Aeronautics and Space Administration,

Langley Research Center, Hampton, Va.

THEORETICAL BASIS FOR DESIGN OF THERMAL-STRESSFREE FASTENERS

M. L. BLOSSER and R. R. MCWITHEY Dec. 1983 24 p refs

(NASA-TP-2226; L-15658; NAS 1.60:2226) Avail: NTIS HC

A02/MF A01 CSCL 20K

CARBON-CARBON COMPOSITES, CONES, FASTENERS,

JOINTS (JUNCTIONS), THERMAL EXPANSION, THERMAL

STRESSES

N84-15590"# Computer Software Management and Information

Center, Athens, Ga.

ELEVENTH NASTRAN USER'S COLLOQUIUM

Washington Nov, 1983 310 p refs Colloq, held in San

Francisco, 2-6 May 1983 Sponsored by NASA, Washington

(NASA-CP-2284; NAS 1.55:2284) Avail: NTIS HC A14/MF A01

CSCL 20K

COMPUTER PROGRAMS, CONFERENCES, DYNAMIC

RESPONSE, FINITE ELEMENT METHOD, STRUCTURAL

ANALYSIS, STRUCTURAL DESIGN CRITERIA, STRUCTURAL

MEMBERS

N84-16585"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

BUCKLING LOADS OF STIFFENED PANELS SUBJECTED TO

COMBINED LONGITUDINAL COMPRESSION AND SHEAR:

RESULTS OBTAINED WITH PASCO, EAL, AND STAGS

COMPUTER PROGRAMS

W. J. STROUD, W. H. GREENE, and M. S. ANDERSON Jan.

1984 79 p refs

(NASA-TP-2215; NAS 1.60:2215; L-15630) Avail: NTIS HC

A05/MF A01 CSCL 20K

BUCKLING, COMPOSITE MATERIALS, COMPRESSION

LOADS, COMPUTER PROGRAMS, PANELS, SHEAR STRESS,

STIFFENING

N84-18675"# National Aeronautics and Space Administration,

Langley Research Center, Hampton, Va.

STRUCTURAL EFFICIENCY STUDIES OF CORRUGATED

COMPRESSION PANELS WITH CURVED CAPS AND BEADED

WEBS

R. C. DAVIS, C. T. MILLS (Old Dominion Univ.), R. PRABHAKARAN

(Old Dominion Univ.), and L. R. JACKSON Feb. 1984 26 p

refs

(NASA-TP-2272; L-15703; NAS 1.60:2272) Avail: NTIS HC

A03/MF A01 CSCL 20K

COMPOSITE MATERIALS, COMPRESSIVE STRENGTH,

CORRUGATING, CURVATURE, MEMBRANES, PANELS,

STRUCTURAL ANALYSIS

N84-18677"# National Aeronautics and Space Administration,

Washington, D.C.

THE NASTRAN THEORETICAL MANUAL

Jan. 1981 944 p

(NASA-SP-221(06); NAS 1.21:221(06)) Avail: NTIS HC A99/MF

A01 CSCL 20K

Designed to accomodate additions and modifications, this

commentary on NASTRAN describes the problem solving

capabilities of the program in a narrative fashion and presents

developments of the analytical and numerical procedures that

underlie the program. Seventeen major sections and numerous

subsections cover; the organizational aspects of the program, utility

matrix routines, static structural analysis, heat transfer, dynamic

structural analysis, computer graphics, special structural modeling

techniques, error analysis, interaction between structures and fluids,

and aeroelastic analysis. A.R.H.
N84-20878"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

DEVELOPMENT OF A SIMPLIFIED PROCEDURE FOR CYCLIC

STRUCTURAL ANALYSIS

A. KAUFMAN Mar. 1984 20 p refs Proposed for presentation

at the 29th ASME Intern. Gas Turbine Conf., Amsterdam, 3-7

Jun. 1984

(NASA-TP-2243; E-1855; NAS 1.60:2243) Avail: NTIS HC

A02/MF A01 CSCL 20K

COMPUTER PROGRAMS, CYCLIC LOADS, INELASTIC

STRESS, NONLINEARITY, STRESS-STRAIN RELATIONSHIPS,

STRUCTURAL ANALYSIS

N84-21899"# National Aeronautics and Space Administration,

Washington, D.C.

THE NASTRAN USER'S MANUAL

Sep. 1983 1572p

(NASA-SP-222(06); NAS 1.12/6:222(06)) Avail: NTIS HC

A99/MF A01 CSCL 20K

All information directly associated with problem solving using

the NASTRAN program is presented. This structural analysis

program uses the finite element approach to structural modeling

wherein the distributed finite properties of a structure are

represented by a finite element of structural elements which are

interconnected at a finite number of grid points, to which loads

are applied and for which displacements are calculated. Procedures

are described for defining and loading a structural model. Functional

references for every card used for structural modeling, the

NASTRAN data deck and control cards, problem solution

sequences (rigid formats), using the plotting capability, writing a

direct matrix abstraction program, and diagnostic messages are

explained. A dictionary of mnemonics, acronyms, phrases, and

other commonly used NASTRAN terms is included. A.R.H.

N84-21901"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SURVEY OF NASA RESEARCH ON CRASH DYNAMICS

R. G. THOMSON, H. D. CARDEN, and R. J. HAYDUK Apr.

1984 46p refs

(NASA-TP-2298; L-15757; NAS 1.60:2298) Avail: NTIS HC

A03/MF A01 CSCL 20K

AIRCRAFT ACCIDENTS, AIRFRAMES, DYNAMIC

STRUCTURAL ANALYSIS, FLOORS, SEATS

N84-25078"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

THE 18TH AEROSPACE MECHANISMS SYMPOSIUM

Washington May 1984 321 p refs Symp. held in Greenbelt,

Md., 2-4 May 1984; sponsored by NASA, the California Inst. of

Tech., and LMSC

(NASA-CP-2311; REPT-84FO235; NAS 1.55:2311) Avail: NTIS

HC A14/MF A01 CSCL 20K

AEROSPACE ENGINEERING, DESIGN ANALYSIS, FOLDING

STRUCTURES, LARGE SPACE STRUCTURES, PAYLOAD

TRANSFER, PERFORMANCE TESTS, SPACEBORNE

EXPERIMENTS

N84-26053"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECT OF PREFORMING ADHERENDS ON STATIC AND

FATIGUE STRENGTH OF BONDED COMPOSITE SINGLE-LAP

JOINTS

J. W. SAWYER Jun. 1984 17 p refs

(NASA-TP-2324; L-15780; NAS 1.60:2324) Avail: NTIS HC

AO2/MF A01 CSCL 20K

ADHESIVE BONDING, COMPOSITE MATERIALS, FATIGUE

LIFE, LAP JOINTS, PREFORMS

39 STRUCTURAL MECHANICS

N84-31688"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

NONLINEAR STRUCTURAL ANALYSIS

Washington Jun. 1984 168 p Workshop held in Cleveland,

19-20 Apr. 1983

(NASA-CP-2297; E-1903; NAS 1.55:2297) Avail: NTIS HC

A08/MF A01 CSCL 20K

BOUNDARY ELEMENT METHOD, CONFERENCES, FINITE

ELEMENT METHOD, FRACTURES (MATERIALS), GAS TURBINE

ENGINES, INELASTIC STRESS, LAMINATES, NONLINEAR

SYSTEMS, SHELLS (STRUCTURAL FORMS), STRESS

ANALYSIS, STRUCTURAL ANALYSIS

N84-32864"# Computer Software Management and Information

Center, Athens, Ga.

TWELFTH NASTRAN USERS' COLLOQUIUM

Washington Aug. 1984 261 p refs Colloq. held in Orlando,

Fla., 7-11 May 1984 Prepared in cooperation with Georgia Univ.,

Athens

(NASA-CP-2328; NAS 1.55:2328) Avail: NTIS HC A12/MF A01

CSCL 20K

COMPUTER TECHNIQUES, CONFERENCES, FINITE

ELEMENT METHOD, NASTRAN, STRUCTURAL ANALYSIS

N84-33832"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

A FORMULATION OF ROTOR-AIRFRAME COUPLING FOR

DESIGN ANALYSIS OF VIBRATIONS OF HELICOPTER

AIRFRAMES

R. G. KVATERNIK and W. C. WALTON, JR. Jun. 1982 135 p

refs

(NASA-RP-1089; L-14243; NAS 1.61:1089) Avail: NTIS HC

A07/MFA01 CSCL01C

A linear formulation of rotor airframe coupling intended for

vibration analysis in airframe structural design is presented. The

airframe is represented by a finite element analysis model; the

rotor is represented by a general set of linear differential equations

with periodic coefficients; and the connections between the rotor

and airframe are specified through general linear equations of

constraint. Coupling equations are applied to the rotor and airframe

equations to produce one set of linear differential equations

governing vibrations of the combined rotor airframe system. These

equations are solved by the harmonic balance method for the

system steady state vibrations. A feature of the solution process

is the representation of the airframe in terms of forced responses

calculated at the rotor harmonics of interest. A method based on

matrix partitioning is worked out for quick recalculations of vibrations

in design studies when only relatively few airframe members are

varied. All relations are presented in forms suitable for direct

computer implementation. E.A.K.

N84-34773"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

MIXED MODELS AND RECUGION TECHNIQUES FOR

LARGE-ROTATION, NONLINEAR ANALYSIS OF SHELLS OF

REVOLUTION WITH APPLICATION TO TIRES

A. K. NOOR (George Washington Univ.), C. M. ANDERSEN (Coll.

of William and Mary), and J. A. TANNER Oct. 1984 57 p

refs

(NCC1-40)

(NASA-TP-2343; L-15802; NAS 1.60:2343) Avail: NTIS HC

A04/MF A01 CSCL 20K

DEFORMATION, ROTATION, SERIES EXPANSION, SHELLS

(STRUCTURAL FORMS), STRESS ANALYSIS, TIRES

133
39 STRUCTURAL MECHANICS

N85-10377"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

RESEARCH IN STRUCTURES AND DYNAMICS, 1984

R. J. HAYDUK, comp. and A. K_ NOOR, comp. (George Washington

Univ.) Washington Oct. 1984 416 p refs Conf. held in

Washington, D.C., 22-25 Oct. 1984 Sponsored in cooperation

with NSF, AFOSR, AIAA, the American Society of Mechanical

Engineers, and the American Society of Civil Engineers

(NASA-CP-2335; L-15866; NAS 1.55:2335) Avail: NTIS HC

At8/MF A01 CSCL 20K

COMPUTATION, COMPUTER PROGRAMMING, COMPUTER

TECHNIQUES, CONTROL THEORY, DYNAMIC STRUCTURAL

ANALYSIS, PROBLEM SOLVING

N85-10405"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala

VIBRATION, ACOUSTIC, AND SHOCK DESIGN AND TEST

CRITERIA FOR COMPONENTS ON THE SOLID ROCKET

BOOSTERS (SRB), LIGHTWEIGHT EXTERNAL TANK (LWT),

AND SPACE SHUTTLE MAIN ENGINES (SSME)

Sep. 1984 812 p

(NASA-RP-1127; NAS 161:1127) Avail: NTIS HC A99/MFA01

CSCL 20K

The vibration, acoustics, and shock design and test criteria for

components and subassemblies on the space shuttle solid rocket

booster (SRB), lightweight tank (LWT), and main engines (SSME)

are presented. Specifications for transportation, handling, and

acceptance testing are also provided. R.S.F.

N85-11378"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

STARS: A GENERAL-PURPOSE FINITE ELEMENT COMPUTER

PROGRAM FOR ANALYSIS OF ENGINEERING STRUCTURES

K. K. GUPTA Oct. 1984 68 p refs

(NASA-RP-1129; H-1224; NAS 1.61:1129) Avail: NTIS HC

A04/MF A01 CSCL 20K

STARS (Structural Analysis Routines) is primarily an interactive,

graphics-oriented, finite-element computer program for analyzing

the static, stability, free vibration, and dynamic responses of

damped and undamped structures, including rotating systems. The

element library consists of one-dimensional (l-D) line elements,

two-dimensional (2-D) triangular and quadrilateral shell elements,

and three-dimensional (3-D) tetrahedral and hexahedral solid

elements. These elements enable the solution of structural

problems that include truss, beam, space frame, plane, plate, shell,

and solid structures, or any combination thereof. Zero, finite, and

interdependent deflection boundary conditions can be implemented

by the program. The associated dynamic response analysis

capability provides for initial deformation and velocity inputs,

whereas the transient excitation may be either forces or

accelerations. An effective in-core or out-of-core solution strategy

is automatically employed by the program, depending on the size

of the problem. Data input may be at random within a data set,

and the program offers certain automatic data-generation features.

Input data are formatted as an optimal combination of free and

fixed formats. Interactive graphics capabilities enable convenient

display of nodal deformations, mode shapes, and element

stresses. R.J.F.

N85-13267"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

FULL-SCALE CRASH-TEST EVALUATION OF TWO

LOAD-LIMITING SUBFLOORS FOR GENERAL AVIATION

AIRFRAMES

H. D. CARDEN Dec. 1984 60 p refs

(NASA-TP-2380; L-15764; NAS 1.60:2380) Avail: NTIS HC

AO4/MF A01 CSCL 20K

AIRFRAME MATERIALS, CRASHWORTHINESS, FLOORS,

GENERAL AVIATION AIRCRAFT, IMPACT TESTS,

SUBSTRUCTURES

134

N85-20396"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

LOCAL STRAIN REDISTRIBUTION CORRECTIONS FOR A

SIMPLIFIED INELASTIC ANALYSIS PROCEDURE BASED ON

AN ELASTIC FINITE-ELEMENT ANALYSIS

A. KAUFMAN and S. Y. HWANG (South Carolina State Coll.,

Orangeburg) Mar. 1985 14 p refs To be presented at the

21st AIAA/SAE/ASME Joint Propulsion Conf., Monterey, Calif.,

8-11 Jul. 1985

(NASA-TP-2421; E-2373; NAS 1.60:2421) Avail: NTIS HC

A02/MF A01 CSCL 20K

CYCLIC LOADS, FINITE ELEMENT METHOD, INELASTIC

STRESS, NONLINEAR EQUATIONS, STRESS CONCENTRATION,

STRESS-STRAIN RELATIONSHIPS

N85-25863"# Computer Software Management and Information

Center, Athens, Ga.

THIRTEENTH NASTRAN USERS' COLLOQUIUM

May 1985 469 p refs Colloq. held in Boston, 6-10 May 1985

Original contains color illustrations

(NASA-CP-2373; NAS 1.55:2373) Avail: NTIS HC A20/MF A01;

also available from COSMIC, Athens, Ga. CSCL 20K

CONFERENCES, FINITE ELEMENT METHOD, NASTRAN,

STRUCTURAL ANALYSIS

N85-27258"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

NONLINEAR EQUATIONS FOR DYNAMICS OF PRETWlSTED

BEAMS UNDERGOING SMALL STRAINS AND LARGE

ROTATIONS

D. H. HODGES May 1985 35 p refs Prepared in cooperation

with Army Research and Technology Labs.

(NASA-TP-2470; A-9833; NAS 1.60:2470; AVSCOM-TR-84-A-5)

Avail: NTIS HC A03/MF A01 CSCL 20K

BEAMS (SUPPORTS), DEFORMATION, DYNAMIC

STRUCTURAL ANALYSIS, KINEMATICS, ROTATING BODIES

N85-31530"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

NONLINEAR CONSTITUTIVE RELATIONS FOR HIGH

TEMPERATURE APPLICATION, 1984

Jun. 1985 368 p refs Symp. held in Cleveland, 15-17 Jun.

1984

(NASA-CP-2369; E-2368; NAS 1.55:2369) Avail: NTIS HC

A16/MF A01 CSCL 20K

CONFERENCES, CONSTITUTIVE EQUATIONS, HIGH

TEMPERATURE TESTS, NONLINEARITY, TEMPERATURE

EFFECTS, VISCOPLASTICITY

N85-32339"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va,

A CRACKED ORTHOTROPIC SHEET STIFFENED BY A

SEMI-INFINITE ORTHOTROPIC SHEET

C. A. BIGELOW Washington Jul. 1985 26 p refs

(NASA-TP-2455; L-15972; NAS 1.60:2455) Avail: NTIS HC

A02/MF A01 CSCL 20K

ADHESIVE BONDING, ALGEBRA, COMPOSITE MATERIALS,

CRACK INITIATION, CRACK PROPAGATION, CRACK TIPS,

GREEN'S FUNCTIONS, HOMOGENEITY, INTEGRAL

EQUATIONS, ORTHOTROPIC PLATES, PLANE STRAIN, SHEAR

STRESS, SPECIMEN GEOMETRY, STRESS INTENSITY

FACTORS, STRINGERS

N85-33512"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

NINTEENTH AEROSPACE MECHANISMS SYMPOSIUM

Aug. 1985 389 p refs Symp. held at Moffett Field, Calif., 1-3

May 1985; sponsored by NASA, Washington, D.C., California Inst,

of Tech., Pasadena, and LMSC, Sunnyvale, Calif.

(NASA-CP-2371; REPT-85181; NAS 1.55:2371) Avail: NTIS HC

A17/MFA01 CSCL20K

AERODYNAMICS, AEROSPACE SYSTEMS, CONFERENCES,

MECHANICAL DRIVES
N85-33537"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

JOINT DESIGN FOR IMPROVED FATIGUE LIFE OF

DIFFUSION-BONDED BOX-STIFFENED PANELS

R. C. DAVIS, P. L. MOSES (PRC Kentron, Inc.), and R. S.

KANENKO (Lockheed California Co., Burbank) Washington Sep.

1985 18 p refs

(NASA-TP-2480; L-15967; NAS 1.60:2480) Avail: NTIS HC

A02/MF A01 CSCL 20K

DIFFUSION WELDING, FATIGUE LIFE, PANELS, RIGID

STRUCTURES, TITANIUM

N86-10579"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

JOINT RESEARCH EFFORT ON VIBRATIONS OF TWISTED

PLATES, PHASE I: FINAL RESULTS

R. E. KIELB, A. W. LEISSA, J. C. MACBAIN, and K. S. CARNEY

Washington Sep. 1985 100 p refs

(NASA-RP-1150; E-2576; NAS 1.61:1150) Avail: NTIS HC

A05/MF A01 CSCL 20K

The complete theoretical and experimental results of the first

phase of a joint government/industry/university research study on

the vibration characteristics of twisted cantilever plates are given.

The study is conducted to generate an experimental data base

and to compare many different theoretical methods with each

other and with the experimental results. Plates with aspect ratios,

thickness ratios, and twist angles representative of current gas

turbine engine blading are investigated. The theoretical results are

generated by numerous finite element, shell, and beam analysis

methods. The experimental results are obtained by precision

matching a set of twisted plates and testing them at two

laboratories. The second and final phase of the study will concern

the effects of rotation. Author

N86-11495"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

TURBINE ENGINE HOT SECTION TECHNOLOGY (HOST)

Oct. 1983 250 p refs Workshop held in Cleveland, Ohio,

25-26 Oct. 1983

(NASA-CP-2289; E-1816; NAS 1.55:2289) Avail: NTIS HC

A11/MFA01 CSCL21E

COMBUSTION, ENGINE PARTS, FAILURE ANALYSIS,

FATIGUE (MATERIALS), GAS TURBINE ENGINES, HEAT

TRANSMISSION, HIGH TEMPERATURE, OPERATING

TEMPERATURE, PROTECTIVE COATINGS, STRUCTURAL

ANALYSIS

N86-11522'# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

A STUDY OF THE CORNERING FORCES GENERATED BY

AIRCRAFT TIRES ON A TILTED, FREE-SWIVELING NOSE

GEAR

R. H. DAUGHERTY and S. M STUBBS Oct. 1985 30 p refs

(NASA-TP-2481; L-15954; NAS 1.60:2481) Avail: NTIS HC

A03/MF A01 CSCL 20K

AIRCRAFT TIRES, ATTITUDE (INCLINATION), FORCE

DISTRIBUTION, GEARS, NOSE WHEELS, SLOPES

N86-20856"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AN APPROXIMATE BUCKLING ANALYSIS FOR RECTANGULAR

ORTHOTROPIC PLATES WITH CENTRALLY LOCATED

CUTOUTS

M. P. NEMETH, M. STEIN, and E. R. JOHNSON (Virginia

Polytechnic Inst. and State Univ., Blacksburg, Va.) Feb. 1986

21 p refs

(NASA-TP-2528; L-16032; NAS 1.60:2528) Avail: NTIS HC

A02/MF A01 CSCL 20K

BUCKLING, DISPLACEMENT, OPENINGS, ORTHOTROPIC

PLATES, PREDICTION ANALYSIS TECHNIQUES

42 GEOSClENCES (GENERAL)

N86-20857"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SOLUTION OF THE SYMMETRIC EIGENPROBLEM

AX=LAMBDA BX BY DELAYED DIVISION

G. A. THURSTON and N. J. C. BAINS Mar. 1986 40 p refs

(NASA-TP-2514; L-15984; NAS 1.60:2514) Avail: NTIS HC

A03/MF A01 CSCL 20K

DIVIDING (MATHEMATICS), EIGENVALUES, ITERATIVE

SOLUTION, SYMMETRY

N86-21933"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

FULL-SCALE TRANSPORT CONTROLLED IMPACT

DEMONSTRATION

R. J. HAYDUK, comp. Jan. 1986 356 p refs Workshop held

in Hampton, Va., 10 Apr. 1985; sponsored by NASA. Langley

Research Center and FAA

(NASA-CP-2395; L-16048; NAS 1.55:2395) Avail: NTIS HC

A16/MF A01 CSCL 20K

AIRCRAFT ACCIDENTS, AIRCRAFT FUELS, AIRCRAFT

STRUCTURES, ANTIMISTING FUELS, CONFERENCES,

CRASHES, CRASHWORTHINESS, DATA ACQUISITION, IMPACT

TESTS, KEROSENE, REMOTELY PILOTED VEHICLES

N86-23974"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

POCKETING MECHANICS OF SRM NOZZLE LINER

V. S. VERDERAIME 1986 27 p refs

(NASA-TP-2577; NAS 1.60:2577) Avail: NTIS HC A03/MF A01

CSCL 20K

COMPOSITE MATERIALS, HOT CORROSION, NOZZLE

INSERTS, SOLID PROPELLANT ROCKET ENGINES

N86-25823"# Computer Software Management and Information

Center, Athens, Ga.

FOURTEENTH NASTRAN USERS' COLLOQUIUM

May 1986 337 p refs Colloquium held in San Diego, Calif.

5-9 May 1986

(NASW-3247)

(NASA-CP-2419; NAS 1.55:2419) Avail: NTIS HC A15/MF A01;

also available from COSMIC, Athens, Ga. CSCL 20K

DESIGN ANALYSIS, DYNAMIC STRUCTURAL ANALYSIS,

FINITE ELEMENT METHOD, NASTRAN, STRUCTURAL

STABILITY

N86-28464"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

THERMAL-FATIGUE AND OXIDATION RESISTANCE OF

COBALT-MODIFIED UDIMET 700 ALLOY

P. T. BIZON and B. J. BARROW Apr. 1986 15 p

(NASA-TP-2591; E-2704; NAS 1.60:2591) Avail: NTIS HC

A02/MF A01 CSCL 20K

COBALT, FATIGUE LIFE, HEAT RESISTANT ALLOYS, NICKEL

ALLOYS, OXIDATION, PROTECTIVE COATINGS, THERMAL

FATIGUE, UDIMET ALLOYS

135
42 GEOSClENCES (GENERAL)

42

GEOSCIENCES (GENERAL)

N77-30521"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

TERRESTRIAL PHOTOVOLTAIC MEASUREMENTS, 2

1976 393 p refs Workshop held at Baton Rouge, La., I0-12

Nov 1976; sponsored by NASA and ERDA

(NASA-CP-2010; ERDA/NASA-1022/76/10) Avail: NTIS HC

A17/MF A01 CSCL 10A

PHOTOVOLTAIC CELLS, SCHOTTKY DIODES, SOLAR

RADIATION, SOLAR SIMULATION, SPECTRAL ENERGY

DISTRIBUTION

N77-32549°# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

NASA WORKSHOP ON SOLAR-TERRESTRIAL STUDIES FROM

A MANNED SPACE STATION

1977 42 p refs Workshop held at Logan, Utah, 14-16 Feb.

1977

(NASA-CP-2024) Avail: NTIS HC A03/MF A01 CSCL 04A

ATMOSPHERIC PHYSICS, MEASURING INSTRUMENTS,

RADIATION EFFECTS, SOLAR RADIATION

N78-33499"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

DISCRIMINATION OF ROCK CLASSES AND ALTERATION

PRODUCTS IN SOUTHWESTERN SAUDI ARABIA WITH

COMPUTER-ENHANCED LANDSAT DATA

H W. BLODGET, F. J. GUNTHER (Computer Sciences Corp.,

Silver Spring, Md.), and M H. PODWYSOCKI Oct. 1978 40 p

refs

(NASA-TP-1327; G7802-F16) Avail: NTIS HC A03/MF A01

CSCL 08G

GEOLOGICAL SURVEYS, LANDSAT SATELLITES, ROCKS,

SAUDI ARABIA

N79-17279"# National Aeronautics and Space Administration.

Lyndon B. Johnson Space Center, Houston, Tex.

SKYLAB EREP INVESTIGATIONS SUMMARY

W. J. PIERSON, ed. (City Univ. of New York) Washington

1978 387 p refs Original contains color illustrations

(NASA-SP-399) Avail: NTIS MF A0t; SOD HC CSCL 05B

The problems in the areas of agriculture, range and forestry;

land use and cartography; geology and hydrology; oceans

atmosphere, and data analysis techniques were investigated and

summarized using Earth Resources Experiment Package (EREP)

data. For individual titles, see N79-17280 through N79-17287.

N79-20424"# National Aeronautics and Space Administration.

John F. Kennedy Space Center, Cocoa Beach, Fla.

PROCEEDINGS OF THE NASA/FLORIDA INSTITUTE OF

TECHNOLOGY ENVIRONMENTAL ENGINEERING CONFERENCE ON NITROGEN TETROXlDE

E. L. RHODES Jun. 1978 203 p refs Conf. held at

Melbourne, Fla., 30-31 Mar. 1978

(NASA-CP-2049) Avail: NTIS HC A10/MF A01 CSCL 13B

CONFERENCES, HYPERGOLIC ROCKET PROPELLANTS,

NITROGEN TETROXIDE, ROCKET OXIDIZERS, SPACE

SHUTTLES

136

N79-22580"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

A COUPLED RADIATIVE-CONVECTIVE-PHOTOCHEMICAL

MODEL OF THE STRATOSPHERE

R E. BOUGHNER and J. E. NEALY Apr. 1979 48 p refs

(NASA-TP-1418; L-12659) Avail: NTIS HC A03/MF A01

CSCL 04A

ATMOSPHERIC CHEMISTRY, GEOPHYSICS, STRATOSPHERE

N79-23461*# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

STRATCOM 8 DATA WORKSHOP AND SUPPLEMENT

E. L. REED, comp. Apr. 1978 137 p refs Workshop held at

Greenbelt, Md., 13-14 Apr. 1978 and presented at the Spring

Meeting of the Am. Geophys. Union, Miami Beach, Fla., 17-21

Apr. 1978

(NASA-CP-2043) Avail: NTIS HC A07/MF A01 CSCL 04A

ATMOSPHERIC COMPOSITION, METEOROLOGICAL

BALLOONS, STRATOSPHERE

N80-15445"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

BAROCLINIC INSTABILITY WITH VARIABLE GRAVITY: A

PERTURBATION ANALYSIS

A. C. GIERE (Univ. Space Res. Assoc.), W. W. FOWLISS, and S.

ARIAS Jan. 1980 30 p refs

(NASA-TP-1586; M-293) Avail: NTIS HC A03/MF A01 CSCL

08G

BAROCLINITY, GRAVITATIONAL EFFECTS, PERTURBATION

THEORY

N81-32564"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

FIELD STUDY FOR REMOTE SENSING: AN INSTRUCTOR'S

MANUAL

W. H. WAKE, ed. (California State Coll., Bakersfield) and G. A.

HULL, ed. 1981 93 p refs Proceedings of the LANDSAT C

Educator's/User's Workshop, Santa Maria, Calif., 2-4 Mar. 1978;

sponsored by the National Council for Geographic Education and

Univ. of Western Illinois, Macomb

(NASA-CP-2155; A-8336; LC-78-61696) Avail: NTIS HC

A05/MF A01 CSCL 051

CONFERENCES, EDUCATION, GROUND TRUTH,

PHOTOINTERPRETATION, REMOTE SENSING, TECHNOLOGY

TRANSFER

N83-11534"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ATMOSPHERIC EFFECTS AND POTENTIAL CLIMATIC IMPACT

OF THE 1980 ERUPTIONS OF MOUNT ST. HELENS

A. DEEPAK, ed. Washington Oct. 1982 296 p refs Symp.

held at Washington, D.C., 18-19 Nov. 1980

(NASA-CP-2240; L-15488; NAS 1.55:2240) Avail: NTIS HC

A13/MF A01 CSCL 04B

AEROSOLS, AIR POLLUTION, ATMOSPHERIC EFFECTS,

CLIMATE, ECOSYSTEMS, ENVIRONMENT EFFECTS,

VOLCANOES, WATER QUALITY

N84-18716"# Science Applications, Inc., McLean, Va.

SPACEBORNE GRAVITY GRADIOMETERS

W. C WELLS, ed. Mar. 1984 82 p refs Workshop held in

Greenbelt, Md., 28 Feb. - 2 Mar. 1983

(NASW-3622)

(NASA-CP-2305; NAS 1,55:2305) Avail: NTIS HC A05/MF A01

CSCL 14B

CONFERENCES, GEOPOTENTIAL, GEOPOTENTIAL

RESEARCH MISSION, GRAVITY GRADtOMETERS, PLANETARY

GRAVITATION, SATELLITE-BORNE INSTRUMENTS
N84-28131"# National Aeronautics and Space Administration,

Washington, D.C.

PROCEEDINGS OF A WORKSHOP ON RESEARCH NEEDS IN

HETEROGENEOUS TROPOSPHERIC CHEMISTRY

1983 83 p refs Workshop held in Sarasota, Fla., 9-13 Jan.

1984

(NASA-CP-2320; L-15801; NAS 1.55:2320) Avail: NTIS HC

A05/MF A01 CSCL 04A

ATMOSPHERIC CHEMISTRY, ATMOSPHERIC CIRCULATION,

ATMOSPHERIC MODELS, CLOUD PHYSICS, RESEARCH

MANAGEMENT, TROPOSPHERE

N84o30359"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

LANDSAT-4 SCIENCE INVESTIGATIONS SUMMARY,

INCLUDING DECEMBER 1983 WORKSHOP RESULTS, VOLUME

1

J. L. BARKER, ed. Jul. 1984 213 p refs Proc. of LANDSAT-4

Early Results Symp., held in Greenbelt, Md., 22-24 Feb. 1983

and LANDSAT Sci. Characterization Workshop, held in Greenbelt,

Md., 6 Dec. 1983 Original contains imagery. Original photography

may be purchased from the EROS Data Center, Sioux Falls, S.D.

57198 ERTS 2 Vol.

(E84-10166; NASA-CP-2326-VOL-1; NAS 1.55:2326-VOL-1)

Avail: NTIS HC A10/MF A01 CSCL 08B

CALIBRATING, DATA CORRELATION, IMAGE PROCESSING,

LANDSAT 4, RADIOMETRIC CORRECTION, SATELLITE

IMAGERY, THEMATIC MAPPING

N84-30380"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

LANDSAT-4 SCIENCE INVESTIGATIONS SUMMARY,

INCLUDING DECEMBER 1983 WORKSHOP RESULTS, VOLUME

2

J. L. BARKER, ed. Jul. 1984 188 p refs Proc. of the

LANDSAT-4 Early Results Symp., held in Greenbelt, Md., 22-24

Feb. 1983 and LANDSAT Sci. Characterization Workshop, held in

Greenbelt, Md., 6 Dec. 1983 ERTS 2 VoI.

(E84-10167; NASA-CP-2326-VOL-2; NAS 1.55:2326-VOL-2)

Avail: NTIS HC A09/MF A01 CSCL 08B

GEOMETRIC ACCURACY, IMAGE PROCESSING, IMAGING

TECHNIQUES, LANDSAT 4, RADIOMETRIC CORRECTION,

RADIOMETRIC RESOLUTION, SPATIAL RESOLUTION,

THEMATIC MAPPING

N84-30475"# National Aeronautics and Space Administration,

Washington, D.C.

GEODYNAMICS

L. S. WALTER Jul. 1984 61 p Workshop held in Airlie, Va.,

15-18 Feb. 1983

(NASA-CP-2325; NAS 1.55:2325) Avail: NTIS HC A04/MF A01

CSCL 08G

CONFERENCES, GEODESY, GEODYNAMICS, GEOMAGNETISM, GEOPOTENTIAL, TECTONICS

N85-23112"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

OZONE CORRELATIVE MEASUREMENTS WORKSHOP

E. HILSENRATH, ed. Washington Mar. 1985 75 p refs

Workshop held in Greenbelt, Md., 16-18 Nov. 1983

(NASA-CP-2362; REPT-85B0183; NAS 1.55:2362) Avail: NTIS

HC A04/MF A01 CSCL 04A

DATA CORRELATION, OZONE, REGRESSION ANALYSIS,

ULTRAVIOLET SPECTROMETERS, VARIABILITY

43 EARTH RESOURCES AND REMOTE SENSING

N85-32357"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

GLOBAL MEGA-GEOMORPHOLOGY

R. S. HAYDEN, ed. (George Mason Univ., Fairfax, Va.) Jul.

1985 130 p refs Workshop held in Oracle, Ariz., 14-16 Jan.

1985; sponsored by NASA and the International Union of Geological

Sciences

(NASA-CP-2312; REPT-85B0472; NAS 1.55:2312) Avail: NTIS

HC A07/MF A01 CSCL 08G

GEOCHEMISTRY, GEOCHRONOLOGY, GEOLOGY,

GEOMORPHOLOGY, GEOPHYSICS, LANDFORMS, OCEANS,

PALEONTOLOGY, STRUCTURAL PROPERTIES (GEOLOGY),

TECTONICS, TOPOLOGY

N86-29282"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

PROCEEDINGS OF THE SECOND PILOT CLIMATE DATA

SYSTEM WORKSHOP

1986 268 p Workshop held in Greenbelt, Md., 29-30 Jan.

1986

(NASA-CP-2430; NAS 1.55:2430) Avail: NTIS HC A12/MF A01

CSCL 04B

CLIMATE, COMPUTER NETWORKS, CONFERENCES, DATA

ACQUISITION, DATA MANAGEMENT, DATA RETRIEVAL, DATA

SYSTEMS, INFORMATION SYSTEMS, ON-LINE SYSTEMS

N86-29301"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

THERMOSPHERE DYNAMICS WORKSHOP, VOLUME 2

H. G. MAYR, ed. and N. J. MILLER, ed. Jun. 1986 461 p

Workshop held in Beltsville and Calverton, Md., 3-5 Oct. 1984

Original contains color illustrations

(NASA-CP-2389; REPT-85B0268; NAS 1.55:2389) Avail: NTIS

HC A20/MF A01 CSCL 04A

ATMOSPHERIC COMPOSITION, AURORAL ZONES,

CONVECTIVE FLOW, ELECTRIC FIELDS, PHOTOIONIZATION,

THERMOSPHERE

43

EARTH RESOURCES AND REMOTE SENSING

Includes remote sensing of earth resources by aircraft and

spacecraft; photogrammetry; and aerial photography.

N78-15549"# National Aeronautics and Space Administration.

Lyndon B. Johnson Space Center, Houston, Tex.

PROCEDURES FOR GATHERING GROUND TRUTH

INFORMATION FOR A SUPERVISED APPROACH TO A

COMPUTER-IMPLEMENTED LAND COVER CLASSIFICATION

OF LANDSAT-ACQUIRED MULTISPECTRAL SCANNER DATA

A. T. JOYCE 1978 48 p refs

(NASA-RP-1015; JSC-12910; S-478) Avail: NTIS HC A03/MF

A01 CSCL 08F

Procedures for gathering ground truth information for a

supervised approach to a computer-implemented land cover

classification of LANDSAT acquired multispectral scanner data are

provided in a step by step manner. Criteria for determining size,

number, uniformity, and predominant land cover of training sample

sites are established. Suggestions are made for the organization

and orientation of field team personnel, the procedures used in

the field, and the format of the forms to be used. Estimates are

made of the probable expenditures in time and costs. Examples

of ground truth forms and definitions and criteria of major land

cover categories are provided in appendixes. Author

137
43 EARTH RESOURCES AND REMOTE SENSING

N78-18497" # National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

ANALYSIS OF DATA SYSTEMS REQUIREMENTS FOR GLOBAL

CROP PRODUCTION FORECASTING IN THE 1985 TIME

FRAME

S. W. DOWNS, P. A. LARSEN, and D. A. GERSTNER Feb.

1978 48 p refs

(NASA-TP-1164; M-248) Avail: NTIS HC A03/MF A01 CSCL

02C

CROP GROWTH, DATA SYSTEMS, TECHNOLOGICAL

FORECASTING, USER REQUIREMENTS

N78-21526"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

APPLICATION OF REMOTE SENSING TO THE CHESAPEAKE

BAY REGION. VOLUME 2: PROCEEDINGS

W. T. CHEN, ed., G. W. FREAS, JR., ed., G. D. HICKMAN, ed.

(Maryland Univ., College Park), D. A. PEMBERTON, ed. (Maryland

Univ., College Park), T. D. WlLKERSON, ed. (Maryland Univ.,

College Park), t. ADLER, ed. (Maryland Univ., College Park), and

V. J. LAURIE, ed. (EPA, Washington, D.C.) Feb. 1978 388 p

refs Conf. held at Berkeley Springs, W. Va., 12-15 Apr. 1977;

sponsored by NASA, EPA, and Maryland Univ., College Park

(NASA-CP-006-PT-2; G-7719-2) Avail: NTIS HC A17/MF A01

CSCL 08J

CHESAPEAKE BAY (US), CONFERENCES, ENVIRONMENTAL

SURVEYS, REMOTE SENSORS

N78-21562"# National Aeronautics and Space Administration.

Lyndon B Johnson Space Center, Houston, Tex.

ACTIVE MICROWAVE USERS WORKSHOP REPORT

R. E. MATTHEWS, ed. 1978 300 p refs Conf. held at

Houston, Tex., Aug. 1976

(NASA-CP-2030; S-476) Avail: NTIS HC A13/MF A01 CSCL

14B

CONFERENCES, EARTH RESOURCES PROGRAM,

MICROWAVE IMAGERY, REMOTE SENSORS,

SATELLITE-BORNE INSTRUMENTS

N78-21568"# National Aeronautics and Space Administration.

Lyndon B. Johnson Space Center, Houston, Tex.

THE USE OF LANDSAT DIGITAL DATA AND

COMPUTER-IMPLEMENTED TECHNIQUES FOR AN

AGRICULTURAL APPLICATION

A. T. JOYCE (NASA. Earth Resources Lab., Slidell, La.) and R.

H. GRIFFIN, II (NASA. Earth Resources Lab., Slidell, La.) Jan.

1978 48 p refs Original contains color illustrations

(NASA-RP-1016; JSC-12897; S-477) Avail: NTIS HC A03/MF

A01 CSCL 02C

Agricultural applications procedures are described for use of

LANDSAT digital data and other digitalized data (e.g., soils). The

results of having followed these procedures are shown in production

estimates for cotton and soybeans in Washington County,

Mississippi. Examples of output products in both line printer and

map formats are included, and a product adequacy assessment is

made. Author

N78-23537"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

APPLICATION OF REMOTE SENSING TO THE CHESAPEAKE

BAY REGION. VOLUME 1: EXECUTIVE SUMMARY

W. T. CHEN, G. W. FREAS, JR., G. D. HICKMAN (Maryland Univ.,

College Park), D. A. PEMBERTON (Maryland Univ., College Park),

T. D. WlLKERSON (Maryland Univ., College Park), I. ADLER

(Maryland Univ., College Park), and V. J. LAURIE (F_PA,

Washington, D.C.) 1978 47 p Conf. held at Berkeley

Springs, W. Va., 12-15 Apr. 1977; sponsored by NASA, EPA, and

Maryland Univ., College Park

(NASA-CP-006-PT-1; G-7719-1) Avail: NTIS HC A03/MF A01

CSCL 08C

CHESAPEAKE BAY (US), CONFERENCES, REMOTE

SENSORS

138

N78-23538"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

DIELECTRIC CONSTANTS OF SOILS AT MICROWAVE

FREQUENCIES-2

J. WANG, T. SCHMUGGE, and D. WILLIAMS May 1978 34 p

refs

(NASA-TP-1238; G-7802-13) Avail: NTIS HC A03/MF A0t

CSCL 20N

MICROWAVE FREQUENCIES, PERMITTIVITY, SOIL

MOISTURE, SOIL SCIENCE

N78-31508"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

HIGH ALTITUDE PERSPECTIVE

1978 33 p Original contains color illustrations

(NASA-SP-427) Avail: NTIS MF A01; SOD HC $1.60 CSCL

14E

The capabilities of the NASA Ames Center U-2 aircraft for

research or experimental programs are described for such areas

as Earth resources inventories; remote sensing data interpretation,

electronic sensor research and development; satellite investigative

support; stratospheric gas studies; and astronomy and astrophysics.

The availability of this aircraft on a cost-reimbursable basis for

use in high-altitude investigations that cannot be performed by

the private sector is discussed. A.R.H.

N79-13475"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

EULUSMAP: AN INTERNATIONAL LAND RESOURCES MAP

UTILIZING SATELLITE IMAGERY

T. PALUDAN and E. CSATI (Inst. of Surveying and Mapping,

Budapest) Dec. 1978 20 p refs

(NASA-TP-1371; M-271) Avail: NTIS HC A02/MF A01 CSCL

08B

IMAGERY, LAND, MAPS, MULTISPECTRAL PHOTOGRAPHY

N79-16329"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

SOIL MOISTURE WORKSHOP

J. L. HEILMAN, ed. (South Dakota State Univ.), D. G. MOORE,

ed. (South Dakota State Univ.), T. J. SCHMUGGE, ed., and D. B.

FRIEDMAN, ed. Nov. 1978 219 p refs Workshop held at

Beltsville, Md., 17-19 Jan. 1978; sponsored in part by NASA and

the US Dept. of Agriculture

(NASA-CP-2073) Avail: NTIS HC AIO/MF A01 CSCL 08M

CONFERENCES, MOISTURE CONTENT, MOISTURE

METERS, SOIL MOISTURE

N80-10537"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

EDUCATOR'S GUIDE FOR MISSION TO EARTH: LANDSAT

VIEWS THE WORLD

M. A. TINDAL 1978 56 p refs Original contains color

illustrations

(NASA-SP-360) Avail: NTIS MF A01, SOD HC CSCL 08B

This teacher's guide is specifically designed to provide

information and suggestions for using LANDSAT imagery to teach

basic concepts in several content areas. Content areas include:

(1) Earth science and geology; (2) environmental studies; (3)

geography; and (4) social and urban studies. R.E.S.

N80-10538"# National Aeronautics and Space Administration.

Lyndon B. Johnson Space Center, Houston, Tex.

APOLLO-SOYUZ TEST PROJECT. VOLUME 2: EARTH

OBSERVATIONS AND PHOTOGRAPHY

F. EL-BAZ, ed. (Smithsionian Institution) and D. M. WARNER, ed.

(Smithsonian Institution) Washington 1979 700 p refs

Original contains color illustrations 2 Vol.

(NASg- t3831 )

(NASA-SP-412-VOL-2) Avail: NTIS HC A99/MF A01 CSCL

05B

Visual observations of the earth are presented along with the
corresponding photographs and maps for specific regions. For

individual titles, see N80-10539 through N80-10581.

N80-15535"# National Aeronautics and Space Administration.

Earth Resources Lab., Bay St. Louis, Miss.

DEMONSTRATION OF WETLAND VEGETATION MAPPING IN

FLORIDA FROM COMPUTER-PROCESSED SATELLITE AND

AIRCRAFT MULTISPECTRAL SCANNER DATA

M. K. BUTERA Oct. 1979 27 p refs

(NASA-TP-1553; S-492) Avail: NTIS HC A03/MF A01 CSCL

08B

MAPPING, MULTISPECTRAL BAND SCANNERS,

VEGETATION, WETLANDS

N80-16405"# National Aeronautics and Space Administration.

Wallops Flight Center, Wallops Island, Va.

SYNTHETIC APERTURE RADAR/LANDSAT MSS IMAGE

REGISTRATION

H. E. MAURER, ed., J. D. OBERHOLTZER, ed., and P. E. ANUTA,

ed. (Purdue Univ.) Jun. 1979 233 p Original contains color

illustrations

(NAS6-2816; NAS6-2827)

(NASA-RP-1039) Avail: NTIS HC A11/MF A01 CSCL 171

Algorithms and procedures necessary to merge aircraft synthetic

aperture radar (SAR) and LANDSAT multispectral scanner (MSS)

imagery were determined. The design of a SAR/LANDSAT data

merging system was developed. Aircraft SAR images were

registered to the corresponding LANDSAT MSS scenes and were

the subject of experimental investigations. Results indicate that

the registration of SAR imagery with LANDSAT MSS imagery is

feasible from a technical viewpoint, and useful from an

information-content viewpoint. J.MS.

N80-25742"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

OPERATIONAL APPLICATIONS OF SATELLITE SNOWCOVER

OBSERVATIONS

A. RANGO, ed. and R. PETERSON, ed. (GE, Beltsville, Md.) May

1980 294 p refs Workshop held at Sparks, Nev., 16-17 Apr.

1979; sponsored in part by Nevada Univ. Original contains

imagery. Original photography may be purchased form the EROS

Data Center, Sioux Falls, S.D. 57198 ERTS

(E80-10167; NASA-CP-2116) Avail: NTIS HC A13/MF A01

CSCL 08L

CONFERENCES, HYDROLOGY, IMAGE PROCESSING,

MOUNTAINS, RESOURCES MANAGEMENT, RIVER BASINS,

SNOW COVER, TECHNOLOGY UTILIZATION, THEMATIC

MAPPING, WATER RUNOFF, WATERSHEDS

N80-28798"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

RADIO INTERFEROMETRY: TECHNIQUES FOR GEODESY

Jul. t980 474 p refs Conf. held in Cambridge and Wesfford,

Mass., 19-21 Jun. 1979

(NASA-CP-2115) Avail: NTIS HC A20/MF A01 CSCL 08E

CONFERENCES, GEODESY, GEOPHYSICS, INTERFEROMETRY

N81-11438"# National Aeronautics and Space Administration.

Wallops Flight Center, Wallops Island, Va.

NASA WALLOPS FLIGHT CENTER GEOS-3 ALTIMETER DATA

PROCESSING REPORT

H. R. STANLEY and R. E. DWYER (Computer Sciences Corp.,

Wallops Island, Va.) Nov. 1980 131 p refs Supersedes

NASA-TM-X-69357

(NASA-RP-1066) Avail: NTIS HC A07/MF A01 CSCL 171

The procedures used to process the GEOS-3 radar altimeter

data from raw telemetry data to a final user data product are

described. In addition, the radar altimeter hardware design and

operating parameters are presented to aid the altimeter user in

understanding the altimeter data. Author

43 EARTH RESOURCES AND REMOTE SENSING

N81-19511"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

MICROWAVE REMOTE SENSING OF SNOWPACK

PROPERTIES

A. RANGO, ed. 1980 272 p refs Conf. held at Fort Collins,

Colo., 20-22 May 1980

(NASA-CP-2153) Avail: NTIS HC A12/MF A01 CSCL 08L

CONFERENCES, HYDROLOGY, MICROWAVE

RADIOMETERS, REMOTE SENSING, SNOW COVER

N81-20489"# National Aeronautics and Space Administration,

Washington, D.C.

DIGITAL PROCESSING OF REMOTELY SENSED IMAGES

J. G. MOIK 1980 338 p refs Original document contains

color illustrations

(NASA-SP-431; LC-79-16727) Avail: NTIS MF A01; SOD HC

$6.50 CSCL 05B

The foundations of image processing were reviewed. Imaging

techniques are discussed and include: image resolution, image

enhancement, image registration, image overlaying and mosaicking,

image analysis and classification, and image data compression.

TM.

N81-20492"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

LABORATORY TANK STUDIES OF A SINGLE SPECIES OF

PHYTOPLANKTON USING A REMOTE SENSING

FLUOROSENSOR

C. A. BROWN, JR., O. JARRETT, JR., and F. H. FARMER Apr.

1981 78 p refs

(NASA-TP-1821; L-14140) Avail: NTIS HC A05/MF A01

CSCL 06C

CHLOROPHYLLS, DYE LASERS, EXCITATION,

FLUORESCENCE, PHYTOPLANKTON, PLANKTON

N81-21437"# National Aeronautics and Space Administration.

John F. Kennedy Space Center, Cocoa Beach, Fla.

AERIAL COLOR INFRARED PHOTOGRAPHY: APPLICATIONS

IN CITRICULTURE

C. H. BLAZQUEZ and F. W. HORN, JR. Nov. 1980 89 p refs

Prepared in cooperation with Florida Univ., Lake Alfred Original

contains color illustrations

(NASA-RP-1067; TR-43-1) Avail: NTIS HC A05/MF A01

CSCL 02C

The photographic specifications and operational parameters in

this handbook were determined in a large aerial color infrared

(ACIR) photographic experiment and in a follow-up demonstration

with the cooperation of Florida citrus growers and aerial

photographers. The ACIR photography in the spring gave the best

separation between healthy and diseased trees. The best scale

for photointerpretation with the use of inexpensive analysis

equipment was 1 in. = 333 ft. Photographs taken with a 12 in.

focal length lens were far superior to those taken with a 6 in.

focal length lens. A cell unit grid system, with window overlays for

rapid photointerpretation and a black and white enlargement for

ground verification, was developed for tree registration. Use of

the enlargement in ground surveys reduced the survey time from

25 hours to 2.5 hours. The cell unit grid system is compatible

with computer processing for rapid recording of photo interpreted

data, storage, retrieval, and analysis. A mapping system with 99

percent accuracy was developed for fast surveillance of tree vigor

and stress. A.R.H.

N81-21440"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

WESTERN REGIONAL REMOTE SENSING CONFERENCE

PROCEEDINGS, 1979

1980 192 p Conf. held at Naval Postgraduate School, Monterey,

Calif., 17 - 19 Oct. 1979

(NASA-CP-2148; REPT-A-8320) Avail: NTIS HC A09/MF A01

CSCL 05A

AGRICULTURE, CONFERENCES, RESOURCES

MANAGEMENT, TECHNOLOGY TRANSFER

139
43 EARTHRESOURCESANDREMOTESENSING

N82-12492"# National Aeronautics and Space Administration.

Lyndon B. Johnson Space Center, Houston, Tex.

SKYLAB EXPLORES THE EARTH

Washington 1977 512 p refs Original contains color

illustrations

(NASA-SP-380; LC-77-829) Avail: NTIS MF A01; SOD HC

$16.50 CSCL 08B

Data from visual observations are integrated with results of

analyses of approxmately 600 of the nearly 2000 photographs

taken of Earth during the 84-day Skylab 4 mission to provide

additional information on (1) Earth features and processes; (2)

operational procedures and constraints in observing and

photographing the planet; and (3) the use of man in real-time

analysis of oceanic and atmospheric phenomena. For individual

titles, see N82-12493 through N82-12509.

N82-13468"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

LABORATORY MEASUREMENTS OF PHYSICAL, CHEMICAL,

AND OPTICAL CHARACTERISTICS OF LAKE CHICOT

SEDIMENT WATERS

W. G. WlTTE, C. H. WHITLOCK, J. W. USRY, W. D. MORRIS,

and E. A. GURGANUS Dec. 1981 30 p refs

(NASA-TP-1941; L-14714) Avail: NTIS HC A03/MF A01

CSCL 08H

LAKES, NEAR INFRARED RADIATION, OPTICAL

PROPERTIES, REMOTE SENSING, SOLIDS FLOW, SPECTRAL

SIGNATURES, TURBIDITY

N82-19647"# Systematics General Corp., Sterling, Va.

GUIDELINES FOR SPACEBORNE MICROWAVE REMOTE

SENSORS

V. LITMAN (Applied Media, Inc., Greenbelt, Md.) and J.

NICHOLAS Mar. 1962 87 p refs

(NASW-3398)

(NASA-RP-1086) Avail: NTIS HC A05/MF A01 CSCL 14B

A handbook was developed to provide information and support

to the spaceborne remote sensing and frequency management

communities: to guide sensor developers in the choice of

frequencies; to advise regulators on sensor technology needs and

sharing potential; to present sharing analysis models and, through

example, methods for determining sensor sharing feasibility; to

introduce developers to the regulatory process; to create

awareness of proper assignment procedures; to present sensor

allocations; and to provide guidelines on the use and limitations

of allocated bands. Controlling physical factors and user

requirements and the regulatory environment are discussed. Sensor

frequency allocation achievable performance and usefulness are

reviewed. Procedures for national and international registration,

the use of non-allocated bands and steps for obtaining new

frequency allocations, and procedures for reporting interference

are also discussed. MD.K.

N82-20617"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

APPLICATIONS SYSTEMS VERIFICATION AND TRANSFER

PROJECT. VOLUME 1: OPERATIONAL APPLICATIONS OF

SATELLITE SNOW COVER OBSERVATIONS: EXECUTIVE

SUMMARY

A. RANGO Dec. 1981 81 p refs 8 Vol.

(NASA-TP-1822; NAS 1.60:1822; REPT-81F0060-VOL-1) Avail:

NTIS HC A05/MF A01 CSCL 05B

ENVIRONMENTAL MONITORING, PHOTOMAPPING,

RESOURCES MANAGEMENT, SNOW COVER, WATER RUNOFF

140

N82-20618"# Geological Survey, Phoenix, Ariz.

APPLICATIONS SYSTEMS VERIFICATION AND TRANSFER

PROJECT. VOLUME 2: OPERATIONAL APPLICATIONS OF

SATELLITE SNOW-COVER OBSERVATIONS AND

DATA-COLLECTION SYSTEMS IN THE ARIZONA TEST SITE

H. H. SCHUMANN Dec. 1981 62 p refs 8 Vot.

(NASA-TP-1823; NAS 1.60:1823; REPT-81F0061-VOL-2) Avail:

NTI_ HC A04/MF A01 CSCL 08L

ARIZONA, ENVIRONMENTAL MONITORING, PHOTOMAPPING, RESOURCES MANAGEMENT, SNOW COVER, WATER

RUNOFF, WATERSHEDS

N82-20619*# California State Dept. of Water Resources,

Sacramento.

APPLICATIONS SYSTEMS VERIFICATION AND TRANSFER

PROJECT. VOLUME 3: OPERATIONAL APPLICATIONS OF

SATELLITE SNOW COVER OBSERVATIONS IN CALIFORNIA

A. J. BROWN and J, F. HANNAFORD (Sierra Hydrotech, Placerville,

Calif.) Dec. 1981 70 p refs 8 Vol.

(NAS5-20831 )

(NASA-TP-1824; NAS 1.60:1824; REPT-81F0062-VOL-3) Avail:

NTIS HC A04/MF A01 CSCL 08L

AERIAL RECONNAISSANCE, FORECASTING, SNOW COVER,

WATER RUNOFF

N82-20620"# Soil Conservation Service, Denver, Colo.

APPLICATIONS SYSTEMS VERIFICATION AND TRANSFER

PROJECT. VOLUME 4: OPERATIONAL APPLICATIONS OF

SATELLITE SNOW COVER OBSERVATIONS. COLORADO

FIELD TEST CENTER

B. A. SHAFER, C. F. LEAF, J. A. DANIELSON (Colorado State

Engineers Office), and G. F. MORAVEC (Colorado State Engineers

Office) Dec. 1981 101 p refs 8 Vol.

(NASA-TP-1825; NAS 1.60:1825; REPT-81F0063-VOL-4) Avail:

NTIS HC A06/MF A01 CSCL 08L

AERIAL RECONNAISSANCE, FORECASTING, SNOW COVER,

WATER RUNOFF, WATERSHEDS

N82-20621"# Bonneville Power Administration, Portland, Oreg.

APPLICATIONS SYSTEMS VERIFICATION AND TRANSFER

PROJECT. VOLUME 5: OPERATIONAL APPLICATIONS OF

SATELLITE SNOW-COVER OBSERVATIONS, NORTHWEST

UNITED STATES

J. P. DILLARD Dec. 1981 84 p refs 8 Vol.

(NASA ORDER S-53877)

(NASA-TP-1826; NAS 1.60:1826; REPT-81F0064-VOL-5) Avail:

NTIS HC A05/MF A01 CSCL 08L

AERIAL RECONNAISSANCE, FORECASTING, SNOW COVER,

WATER RUNOFF

N82-20622"# National Environmental Satellite Service,

Washington, D. C.

APPLICATIONS SYSTEMS VERIFICATION AND TRANSFER

PROJECT. VOLUME 6: OPERATIONAL APPLICATIONS OF

SATELLITE SNOW-COVER OBSERVATIONS NOAA/NESS

SUPPORT STUDY Final Report, 1 Jan. 1975 - 31 Dec. 1978

S. R. SCHNEIDER Dec. 1981 68 p refs 8 Vol.

(NASA ORDER S-53772)

(NASA-TP-1827; NAS 1.60:1827; REPT-81F0065-VOL-6) Avail:

NTIS HC A04/MF A01 CSCL 05B

ENVIRONMENTAL MONITORING, HYDROLOGY MODELS,

PHOTOMAPPING, RESOURCES MANAGEMENT, SNOW COVER,

WATER RUNOFF
N82-20623"# Ecosystems International, Inc., Gambrills, Md.

APPLICATIONS SYSTEMS VERIFICATION AND TRANSFER

PROJECT. VOLUME 7: COST/BENEFIT ANALYSIS FOR THE

ASVT ON OPERATIONAL APPLICATIONS OF SATELLITE

SNOW-COVER OBSERVATIONS

P. CASTRUCCIO, H. LOATS, D. LLOYD, and P. NEWMAN Dec.

1981 245 p refs 8 Vol.

(NAS5-23729)

(NASA-TP-1828; NAS 1.60:1818; REPT-81F0066-VOL-7) Avail:

NTIS HC A11/MF A01 CSCL 08L

AERIAL RECONNAISSANCE, COST ANALYSIS,

FORECASTING, SNOW COVER, WATER RUNOFF

N82-20624"# Environmental Research and Technology, Inc.,

Concord, Mass.

APPLICATIONS SYSTEMS VERIFICATION AND TRANSFER

PROJECT. VOLUME 8: SATELLITE SNOW MAPPING AND

RUNOFF PREDICTION HANDBOOK

C. J, BOWLEY, J. C. BARNES, and A, RANGO (NASA. Goddard

Space Flight Center) Dec. 1981 98 p refs 8 Vol.

(NAS5-24410)

(NASA-TP-1829; NAS 1.60:1829; REPT-81F0067-VOL-8) Avail:

NTIS HC A05/MF A01 CSCL 08L

FORECASTING, HANDBOOKS, PHOTOINTERPRETATION,

SNOW COVER, WATER RUNOFF

N82-22548"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

WESTERN REGIONAL REMOTE SENSING CONFERENCE

PROCEEDINGS, 1981

Sep. 1981 263 p refs Conf. held at Monterey, Calif., 30 Mar.

- 2 Apr. 1981 Original contains imagery. Original photography

may be purchased from the EROS Data Center, Sioux Falls, S.

Dak., 57198 ERTS

(E82-10104; NASA-CP-2195; NAS 1.55:2195; A-8663) Avail:

NTIS HC A12/MF A01 CSCL 05A

CONFERENCES, FEDERAL BUDGETS, IMAGING

TECHNIQUES, INFORMATION SYSTEMS, TECHNOLOGY

TRANSFER, UNITED STATES

N83-10458"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

THE LANDSAT TUTORIAL WORKBOOK: BASICS OF

SATELLITE REMOTE SENSING

N. M. SHORT, Principal Investigator 1982 554 p refs Original

contains color imagery. Original photography may be purchased

from the EROS Data Center, Sioux Falls, S.D. 57198. ERTS

(E83-10001; NASA-RP-1078; NAS 1.61:1078; LC-81-600117)

Avail: NTIS MF A01; SOD HC $55.00 CSCL 05B

Most of the subject matter of a full training course in applying

remote sensing is presented in a self-teaching mode in this how-to

manual which combines a review of basics, a survey of systems,

and a treatment of the principles and mechanics of image analysis

by computers, with a laboratory approach for learning to utilize

the data through practical experiences. All relevant image products

are included. For individual titles, see N83-10459 through

N83-10471.

N83-17942"# Purdue Univ., West Lafayette, Ind. Lab. for

Applications of Remote Sensing.

CORSE-81: THE 1981 CONFERENCE ON REMOTE SENSING

EDUCATION

S. M. DAVIS, comp. 1981 375 p refs Conf. held in

Lafayette, Ind., 18-22 May 1981 Sponsored by NASA and

NOAA Original contains imagery. Original photography may be

purchased from the EROS Data Center, Sioux Falls, S.D. 57198

ERTS

(E83-10179; NASA-CP-2197; NAS 1.55:2197) Avail: NTIS HC

A16/MF A01 CSCL 051

EDUCATION, REMOTE SENSING, UNIVERSITIES

43 EARTH RESOURCES AND REMOTE SENSING

N83-19141"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

SECOND EASTERN REGIONAL REMOTE SENSING

APPLICATIONS CONFERENCE

M. L. IMHOFF, ed., R. G. WITT, ed., and D. KUGELMANN, ed.

1981 398 p refs Conf. held in Danvers, Mass., 9-11 Mar.

1981 Original contains imagery. Original photography may be

purchased from the EROS Data Center, Sioux Falls, S.D. 57198.

ERTS

(E83-10189; NASA-CP-2198; NAS 1.55:2198) Avail: NTIS HC

A17/MF A01 CSCL 05B

DATA PROCESSING, GEOGRAPHIC INFORMATION

SYSTEMS, REMOTE SENSING, RESOURCES MANAGEMENT,

THEMATIC MAPPING, UNITED STATES

N83-21419"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

EASTERN REGIONAL REMOTE SENSING APPLICATIONS

CONFERENCE

N. M. SHORT, ed. Jan. 1981 240 p refs Conf. held in

Easton, Md., 2-5 Oct. 1979 Original contains imagery. Original

phototgraphy may be purchased from the EROS Data Center,

Sioux Falls, S.D. 57198 ERTS

(E83-10201; NASA-CP-2173; NAS 1.55:2173) Avail: NTIS HC

A11/MF A01 CSCL 08B

CONFERENCES, REMOTE SENSING, RESOURCES

MANAGEMENT, TECHNOLOGY TRANSFER, UNITED STATES

N83-23660"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

THE SNOWMELT-RUNOFF MODEL (SRM) USER'S MANUAL

J. MARTINEC (Swiss Federal Inst. for Snow and Avalanche

Research), A. RANGO, and E. MAJOR (Research and Data

Systems, Inc.) Apr. 1983 120 p refs

(NASA-RP-1100; REPT-83B0251; NAS 1.61:1100) Avail: NTIS

HC A06/MF A01 CSCL 08H

A manual to provide a means by which a user may apply the

snowmelt runoff model (SRM) unaided is presented. Model

structure, conditions of application, and data requirements, including

remote sensing, are described. Guidance is given for determining

various model variables and parameters. Possible sources of error

are discussed and conversion of snowmelt runoff model (SRM)

from the simulation mode to the operational forecasting mode is

explained. A computer program is presented for running SRM is

easily adaptable to most systems used by water resources

agencies. E.A.K.

N83-26155"# Marshall Univ., Huntington, W. Va.

PROCEEDINGS OF THE NATIONAL CONFERENCE ON ENERGY

RESOURCE MANAGEMENT. VOLUME 1: TECHNIQUES,

PROCEDURES AND DATA BASES

J. O. BRUMFIELD, ed. and Y. M SCHIFFMAN, ed. 1982 306

p refs Conf. held in Baltimore, 9-12 Sep. 1982; sponsored by

NASA, American Planning Association, Nuclear Regulatory

Commission and US Region of the Remote Sensing Society

Sponsored by NASA Original contains imagery. Original

photography may be purchased from the EROS Data Center, Soiux

Falls, S.D. 57198 ERTS 2 Vol.

(E83-10335; NASA-CP-2261 -VOL-1; NAS 1.55:2261-VOL-1 )

Avail: NTIS HC A14/MF A01 CSCL 05B

CONFERENCES, DATA BASES, DATA INTEGRATION,

ENERGY SOURCES, GEOGRAPHIC INFORMATION SYSTEMS,

IMAGE ANALYSIS, RESOURCES MANAGEMENT

141
43 EARTH RESOURCES AND REMOTE SENSING

N83-26176"# Marshall Univ., Huntington, W. Va.

PROCEEDINGS OF THE NATIONAL CONFERENCE ON ENERGY

RESOURCE MANAGEMENT. VOLUME 2: APPLICATIONS

J. O. BRUMFIELD, ed. and Y. M. SCHIFFMAN, ed. 1982 415

p refs Conf. held in Baltimore, 9-12 Sep. 1982; sponsored by

NASA, American Planning Association, Nuclear Regulatory

Commission and US Region of the Remote Sensing Society

Sponsored by NASA Original contains imagery. Original

photography may be purchased from the EROS Data Center, Sioux

Falls, S.D. 57198 ERTS 2 VoI.

(E83-10336; NASA-CP-2261-VOL-2; NAS 1.55:2261-VOLo2)

Avail: NTIS HC A18/MF A01

BIOMASS, CONFERENCES, ENERGY SOURCES,

ENVIRONMENTAL MONITORING, GEOGRAPHIC INFORMATION

SYSTEMS, LAND USE, MINES (EXCAVATIONS), RESOURCES

MANAGEMENT, SITE SELECTION

N83-26201"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

OCEAN COLOR ALGORITHM FOR REMOTE SENSING OF

CHLOROPHYLL

G.W, GREWand L. S. MAYO May 1983 29p refs

(NASA-TP-2164; L-15573; NAS 1.60:2164) Avail: NTIS HC

A03/MF A01 CSCL 08A

OCEAN COLOR SCANNER, OCEANOGRAPHIC

PARAMETERS, REMOTE SENSING

N83-27293"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

WILDLAND INVENTORY AND RESOURCE MODELING FOR

DOUGLAS AND CARSON CITY COUNTIES, NEVADA, USING

LANDSAT AND DIGITAL TERRAIN DATA

J. A. BRASS, W. C. LIKENS, and R. R. THORNHILL (Nevada Div.

of Forestry, Carson City) Mar. 1983 50 p refs ERTS

(E83-10302; NASA-TP-2137; A-8997; NAS 1.60:2137) Avail:

NTIS HC A03/MF A01 CSCL 08B

CLASSIFICATIONS, DATA REDUCTION, FORESTS,

HABITATS, LAND USE, NEVADA, TIMBER INVENTORY,

WILDERNESS

N83-28506"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

THE MULTISPECTRAL IMAGING SCIENCE WORKING GROUP.

VOLUME 3: APPENOICES Final Report

S. C. COX, ed. 1 Sep. 1982 299 p refs Proc. of working

groups held in Pasadena, Calif. and in Silver Spring, Md., 1982;

sponsored by NASA, Washington Original contains imagery.

Original photography may be purchased from the EROS Data

Center, Sioux Falls, S.D. 57198 ERTS

(E83-10351; NASA-CP-2260-VOL-3; NAS 1.55:2260-VOL-3)

Avail: NTIS HC A13/MF A01 CSCL 20F

CONFERENCES, IMAGE RESOLUTION, IMAGING

TECHNIQUES, MULTISPECTRAL PHOTOGRAPHY, SPECTRAL

BANDS

N83-29750"# National Aeronautics and Space Administration.

Earth Resources Lab., Bay St. Louis, Miss.

LITERATURE REVIEW OF ORGANIC MATTER TRANSPORT

FROM MARSHES

D. D. DOW May 1982 79p refs ERTS

(E83-10352; NASA-TP-2022; NAS 1.60:2022) Avail: NTIS HC

A05/MF A01 CSCL 13B

COASTAL ECOLOGY, ESTUARIES, MARSHLANDS,

MATHEMATICAL MODELS, ORGANIC MATERIALS, SEDIMENT

TRANSPORT, WETLANDS

142

N84-14563" National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

THE HEAT CAPACITY MAPPING MISSION (HCMM)

ANTHOLOGY

N. M. SHORT and L. M. STUART, JR., Principal Investigators

1982 268 p refs Original contains color imagery. Original

imagery may be purchased from NASA. Goddard Space Flight

Center, (code 601), Greenbelt, Md. 20770. Domestic users send

orders to "Attn: National Space Science Data Center";

non-domestic users send orders to "Attn: World Data Center A

for Rockets and Satellites". HCMM

(E84-10051; NASA-SP-465; NAS 1.21:465) Avail: SOD HC

$24.00 CSCL 08B

The analysis and interpretation of thermal imagery is explained

in this tutorial which reviews and evaluates a program that surveyed

reflected solar radiation and thermal emission from the Earth's

surface with a spatial resolution of 600 meters. For individual titles,

see N84-14564 through N84-14570.

N84-27262"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

FRONTIERS OF REMOTE SENSING OF THE OCEANS AND

TROPOSPHERE FROM AIR AND SPACE PLATFORMS

Washington May 1984 615 p refs Symp. held in Shoresh,

Israel, 14-23 May t984; sponsored in cooperation with the Israel

Academy of Sciences and Humanities

(NASA-CP-2303; NAS 1.55:2303) Avail: NTIS HC A99/MF A01

CSCL 08C

AIR WATER INTERACTIONS, OCEAN CURRENTS, OCEANS,

REMOTE SENSING, SATELLITE OBSERVATION, SEA ICE,

TOPOGRAPHY

N85-11404"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

THE MULTISPECTRAL IMAGING SCIENCE WORKING GROUP.

VOLUME 1: EXECUTIVE SUMMARY Final Report

S. C. COX, ed. Washington 1 Sep. 1982 39 p Working

groups held in Pasadena, Calif., San Antonio, and Silver Spring,

Md., 1 Sep. 1982 Original contains imagery. Original photography

may be purchased from the EROS Data Center, Sioux Falls, S.D.

57198 ERTS 3 Vol.

(E85-10001; NASA-CP-2260-VOL-1; NAS 1.55:2260-VOL-1)

Avail: NTIS HC A03/MF A01 CSCL 05B

GEOGRAPHY, GEOLOGY, HYDROLOGY, IMAGE ANALYSIS,

IMAGE RESOLUTION, MULTISPECTRAL PHOTOGRAPHY,

SATELLITE IMAGERY, TECHNOLOGY ASSESSMENT, THEMATIC

MAPPING, VEGETATION

N85-11405"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

THE MULTISPECTRAL IMAGING SCIENCE WORKING GROUP.

VOLUME 2: WORKING GROUP REPORTS Final Report

S. C. COX, ed. Washington 1 Sep. 1982 336 p refs

Meetings held in Pasadena, Calif., San Antonio, and Silver Spring,

Md., 1982 Original contains imagery. Original photography may

be purchased from EROS Data Center, Sioux Falls, S.D. 57198

ERTS 3 Vol.

(E85-10002; NASA-CP-2260-VOL-2; NAS 1.55:2260-VOL-2)

Avail: NTIS HC A15/MF A01 CSCL 05B

CONFERENCES, GEOGRAPHY, GEOLOGY, HYDROLOGY,

IMAGE ANALYSIS, IMAGE RESOLUTION, MULTISPECTRAL

PHOTOGRAPHY, SATELLITE IMAGERY, TECHNOLOGY

ASSESSMENT, THEMATIC MAPPING, VEGETATION
N86-20496"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

LANDSAT-4 SCIENCE CHARACTERIZATION EARLY RESULTS.

VOLUME I: MULTISPECTRAL SCANNER (MSS)

J. L. BARKER, ed. Washington Jan. 1985 206 p refs

Symp. held in Greenbelt, Md., 22-24 Feb. 1983 Original contains

imagery. Original photography may be purchased from the EROS

Data Center, Sioux Falls, S.D. 57198 ERTS 4 VoI.

(E85-10067; NASA-CP-2355-VOL-1 ; REPT-85B0115-VOL-1; NAS

1.55:2355-VOL-1) Avail: NTIS HC A10/MF A01 CSCL 05B

LANDSAT 4, MULTISPECTRAL BAND SCANNERS, SATELLITE

IMAGERY

43 EARTH RESOURCES AND REMOTE SENSING

N85-23237"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

CHARACTERISTIC VECTOR ANALYSIS OF INFLECTION RATIO

SPECTRA: NEW TECHNIQUE FOR ANALYSIS OF OCEAN

COLOR DATA

G. W. GREW Apr. 1985 26 p refs

(NASA-TP-2428; NAS 1.60:2428; L-15885) Avail: NTIS HC

A03/MF A01 CSCL 05B

ALGAE, CHLOROPHYLLS, OCEAN COLOR SCANNER,

OCEAN DYNAMICS, REMOTE SENSING, VECTOR ANALYSIS

N85-20508"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

LANDSATo4 SCIENCE CHARACTERIZATION EARLY RESULTS.

VOLUME 2, PART 1: THEMATIC MAPPER (TM)

J. L. BARKER, ed. Washington Jan. 1985 482 p refs

Symp. held in Greenbelt, Md., 22-24 Feb. 1983 Original contains

imagery. Original photography may be purchased at the EROS

Data Center, Sioux Falls, S.D. 57198 ERTS 4 Vol.

(E85-10068; NASA-CP-2355-VOL-2-PT- 1;

REPT-85B0115-VOL-2-PT-1; HAS 1.55:2355-VOL-2-PT-1) Avail:

NTIS HC A21/MF A01 CSCL 08B

CONFERENCES, LANDSAT 4, REMOTE SENSORS,

SATELLITE IMAGERY, SPECTRAL RESOLUTION, THEMATIC

MAPPING

N86-21724"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

LANDSAT-4 SCIENCE CHARACTERIZATION EARLY RESULTS.

VOLUME 3, PART 2: THEMATIC MAPPER (TM)

J. L. BARKER, ed. Washington Jan. 1985 591 p refs

Symp. held in Greenbelt, Md., 22-24 Feb. 1983 Original contains

imagery. Original photography may be purchased from the EROS

Data Center, Sioux Falls, S.D. 57198 ERTS 4 Vol.

(E85-10069; NASA-CP-2355-VOL-3-PT-2;

REPT-85B0115-VOL-3-PT-2; NAS 1.55:2355-VOL-3-PT-2) Avail:

NTIS HC A25/MF A01 CSCL 08B

GEOMETRIC ACCURACY, IMAGE RESOLUTION, LANDSAT

4, RADIOMETRIC RESOLUTION, SATELLITE IMAGERY,

SPECTRAL RESOLUTION, THEMATIC MAPPING

N85-23186"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

LANDSAT-4 SCIENCE CHARACTERIZATION EARLY RESULTS.

VOLUME 4: APPLICATIONS

J. L. BARKER, ed. Washington Jan. 1985 442 p refs

Symp. held in Greenbelt, Md., 22-24 Feb. 1983 Original contains

imagery. Original photography may be purchased from the EROS

Data Center, Sioux Falls., S. D. 57198 ERTS 4 Vol.

(E85-10070; NASA-CP-2355-VOL-4; REPT-85B0115-VOL-4; NAS

1.55:2355-VOL-4) Avail: NTIS HC A19/MF A01 CSCL 08B

CONFERENCES, DIGITAL DATA, IMAGE PROCESSING,

LANDSAT 4, SATELLITE IMAGERY, SPECTRAL SENSITIVITY,

THEMATIC MAPPING

N85-23223"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

REMOTE SENSING OF SNOW AND EVAPOTRANSPIRATION

T. SCHMUGGE, ed. Washington Feb. 1985 176 p refs

Proc. of 2nd workshop held in Honolulu, Hawaii, 15-19 Nov. 1983

Original contains color illustrations

(NASA-CP-2363; REPT-84B0036; NAS 1.55:2363) Avail: NTIS

HC A09/MF A01 CSCL 08L

CONFERENCES, EVAPOTRANSPIRATION, HYDROLOGY

MODELS, MICROWAVE EMISSION, REMOTE SENSING, SNOW,

WATER RUNOFF

N85-30450"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SPECTRAL REFLECTANCES OF NATURAL TARGETS FOR USE

IN REMOTE SENSING STUDIES

D. E. BOWKER, R. E. DAVIS, D. L. MYRICK, K. STACY, and W.

T. JONES Jun. 1985 185 p refs Prepared in cooperation

with Computer Sciences Corp.

(NASA-RP-1139; L-15920; NAS 1.61:1139) Avail: NTIS HC

A09/MF A01 CSCL 20F

A collection of spectral reflectances of 156 natural targets is

presented in a uniform format. For each target both a graphical

plot and a digital tabulation of reflectance is given. The data were

taken from the literature and include laboratory, field, and aircraft

measurements. A discussion of the different measurements of

reflectance is given, along with the changes in apparent reflectance

when targets are viewed through the atmosphere. The salient

features of the reflectance curves of common target types are

presented and discussed. Author

N86-31940" National Aeronautics and Space Administration,

Washington, D.C.

EARTH RESOURCES: A CONTINUING BIBLIOGRAPHY WITH

INDEXES, ISSUE 50

1986 146 p

(NASA-SP-7041(50); NAS 1.21:7041(50)) Avail: NTIS HC A07

CSCL 05B

This bibliography lists 523 reports, articles and other documents

introduced into the NASA scientific and technical information

system between April 1 and June 30, 1986. Emphasis is placed

on the use of remote sensing and geophysical instrumentation in

spacecraft and aircraft to survey and inventory natural resources

and urban areas. Subject matter is grouped according to agriculture

and forestry, environmental changes and cultural resources,

geodesy and cartography, geology and mineral resources,

hydrology and water management, data processing and distribution

systems, instrumentation and sensors, and economic analysis.

Author

N86-31945"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

LANDSAT-4 AND LANDSAT-5 MULTISPECTRAL SCANNER

COHERENT NOISE CHARACTERIZATION AND REMOVAL

J. C. TILTON and W. L. ALFORD, principal investigators (Defense

Mapping Agency, Washington, D.C.) May 1986 46 p Original

contains color illustrations

(NASA-TP-2595; REPT-86B0040; NAS 1.60:2595) Avail: NTIS

HC A03/MF A01 CSCL 14B

CONTINUOUS NOISE, ELECTRONIC FILTERS, IMAGE

PROCESSING, LANDSAT 4, LANDSAT 5, LOW PASS FILTERS,

MULTISPECTRAL BAND SCANNERS

143
44 ENERGYPRODUCTIONANDCONVERSION

44

ENERGYPRODUCTIONANDCONVERSION

Includes specific energy conversion systems, e.g., fuel cells; global

sources of energy; geophysical conversion; and windpower.

N77-16437" National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

SECONDARY AEROSPACE BATTERIES AND BATTERY

MATERIALS: A BIBLIOGRAPHY, 1969 - 1974

P. MCDERMOTT, G. HALPERT, S. EKPANYASKUN, and P.

NCHE Jul. 1976 161 p

(NASA-SP-7044) Avail: NTIS HC A08 CSCL 09A

This annotated bibliography on the subject of secondary

aerospace battery materials and related physical and

electrochemical processes was compiled from references to journal

articles published between 1969 and 1974. A total of 332 citations

are arranged in chronological order under journal titles. Indices by

system and component, techniques and processes, and author

are included. Author

N77-30617"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

AN ANALYTICAL AND EXPERIMENTAL INVESTIGATION OF A

1.8 BY 3.7 METER FRESNEL LENS SOLAR CONCENTRATOR

L. J. HASTINGS, S. L. ALLUMS, and W. S. JENSEN Aug. 1977

77 p refs

(NASA-TP-1005; M-224) Avail: NTIS HC A05/MF A01 CSCL

10A

ENERGY TRANSFER, FRESNEL LENSES, SOLAR

COLLECTORS

N78-13527"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

SOLAR CELL HIGH EFFICIENCY AND RADIATION DAMAGE

1977 221 p refs Conf. held at Cleveland, 18-19 May 1977

(NASA-CP-2020) Avail: NTIS HC At0/MF A01 CSCL 10A

CONFERENCES, CRYSTAL DEFECTS, ENERGY

CONVERSION EFFICIENCY, ENERGY POLICY, ENERGY

SOURCES, RADIATION DAMAGE, SEMICONDUCTOR

JUNCTIONS, SOLAR CELLS

N78-19600*# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

GUNTERSVILLE WORKSHOP ON SOLAR-TERRESTRIAL

STUDIES

1977 71 p Presented at University of Alabama in Huntsville/NASA

Workshop, 13-17 Oct. 1977, Lake Guntersville State Park

Convention Center, Guntersville, Alabama

(NASA-CP-2037) Avail: NTIS HC A04/MF A01 CSCL 10A

CONFERENCES, EARTH ATMOSPHERE, GEOPHYSICS,

NASA PROGRAMS, SOLAR PHYSICS, SPACECRAFT MODULES

N78-19616"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

WIND TURBINE STRUCTURAL DYNAMICS

D. R. MILLER, ed. 1978 280 p refs Workshop held at

Cleveland. 15-17 Nov. 1977; sponsored by DOE

(NASA-CP-2034; DOE-CONF-771148; E-9518) Avail: NTIS HC

A13/MFA01 CSCL 10A

DYNAMIC LOADS, DYNAMIC STRUCTURAL ANALYSIS,

MECHANICAL DRIVES, TURBINES, WINDPOWERED

GENERATORS

144

N78-23571"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

NUCLEAR WASTE DISPOSAL IN SPACE

R. E. BURNS, W. E. CAUSEY, W. E. GALLOWAY, and R. W.

NELSON May 1978 118p refs

(NASA-TP-1225; M-250) Avail: NTIS HC A06/MF A01 CSCL

18G

AEROSPACE ENVIRONMENTS, RADIOACTIVE WASTES,

WASTE DISPOSAL

N78-28615"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EMERGING ENERGY ALTERNATIVES FOR THE

SOUTHEASTERN STATES

E. K. STEFANAKOS, ed. 1978 149 p refs Proc. of Symp.

held at North Carolina A and T State Univ., Greensboro, 31 Mar.

1978; sponsored by DOE and North Carolina A and T State Univ.

(NASA-CP-2042; L-12251) Avail: NTIS HC A07/MF A01

CSCL 10A

CONFERENCES, ENERGY POLICY, ENERGY SOURCES,

UNITED STATES

N78-28624"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

SOLUBILITY, STABILITY, AND ELECTROCHEMICAL STUDIES

OF SULFUR-SULFIDE SOLUTIONS IN ORGANIC SOLVENTS

W. L. FIELDER and J. SINGER Aug. 1978 43 p refs

(NASA-TP-1245; E-9552) Avail: NTIS HC A03/MF A01 CSCL

10A

ELECTRIC MOTOR VEHICLES, ELECTROCHEMICAL CELLS,

ORGANIC SULFUR COMPOUNDS, SULFIDES

N79-21565"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

THE 1977 GODDARD SPACE FLIGHT CENTER BATTERY

WORKSHOP

t977 579 p Workshop held at Greenbelt, Md., 15-17 Nov.

1977

(NASA-CP-2041) Avail: NTIS HC A25/MF A01 CSCL 10C

CONFERENCES, ELECTRIC BATTERIES, SPACECRAFT

POWER SUPPLIES, STORAGE BATTERIES, TECHNOLOGY

ASSESSMENT

N79-22626"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EFFECT OF STEAM ADDITION ON CYCLE PERFORMANCE OF

SIMPLE AND RECUPERATED GAS TURBINES

R. J. BOYLE Apr. 1979 52 p refs

(NASA-TP-1440; E-9795) Avail: NTIS HC A04/MF A0t CSCL

10B

FLUID INJECTION, GAS TURBINES, STEAM FLOW,

THERMODYNAMIC CYCLES

N79-28669"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

THE 11TH ANNUAL BATTERY WORKSHOP

1978 545 p Workshop held at Goddard Space Flight Center,

Greenbelt, Md., 15-17 Nov. 1978

(NASA-CP-2088) Avail: NTIS HC A23/MF A01 CSCL 10C

CONFERENCES, ELECTROCHEMISTRY, SPACECRAFT

POWER SUPPLIES, STORAGE BATTERIES

N79-32640"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

SOLAR CELL HIGH EFFICIENCY AND RADIATION DAMAGE,

1979

Aug. 1979 290 p refs Conf. held at Cleveland, 13-14 Jun.

1979

(NASA-CP-2097; D-133) Avail: NTIS HC A13/MF A01 CSCL

10A

CONFERENCES, ENERGY CONVERSION EFFICIENCY,

RADIATION TOLERANCE, SOLAR CELLS
N79-33572"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

ANNEALING OF RADIATION DAMAGE IN 0.1- AND

2-OHM-CENTIMETER SILICON SOLAR CELLS

I. WEINBERG and C. K. SWARTZ Oct. 1979 13 p refs

(NASA-TP-1559; E-9997) Avail: NTIS HC A02/MF A01 CSCL

10A

ANNEALING, RADIATION DAMAGE, SOLAR CELLS

N80-11559"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AN EVALUATION OF THE NASA TECH HOUSE, INCLUDING

LIVE-IN TEST RESULTS, VOLUME 1

I. H. A. ABBOTT, K. A. HOPPING, and W. D. HYPES Nov. 1979

72 p refs

(NASA-TP-1564; L-13440) Avail: NTIS HC A04/MF A01

CSCL 10A

BUILDINGS, ENERGY CONSERVATION, NASA PROGRAMS,

SOLAR HOUSES, TECHNOLOGY ASSESSMENT, WASTE

WATER

N80-16453"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

LARGE WIND TURBINE DESIGN CHARACTERISTICS AND R

AND D REQUIREMENTS

S. LIEBLEIN, ed. (Technical Report Services, Rocky River, Ohio)

Dec. 1979 459 p refs Conf. held at Cleveland, 24-26 Apr.

1979; sponsored in part by DOE

(NASA-CP-2106; CONF-7904111) Avail: NTIS HC A20/MF A01

CSCL 10B

ELECTRIC GENERATORS, ENERGY CONVERSION, ENERGY

TECHNOLOGY, WlNDPOWER UTILIZATION, WlNDPOWERED

GENERATORS

N80-20820"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

THE 1979 GODDARD SPACE FLIGHT CENTER BATTERY

WORKSHOP

G. HALPERT, ed. Apr 1980 521 p refs Workshop held in

Greenbelt, Md., 13-15 Nov. 1979

(NASA-CP-2117) Avail: NTIS HC A22/MF A01 CSCL 10C

AEROSPACE ENGINEERING, CONFERENCES, ELECTRIC

BATTERIES, ELECTROCHEMISTRY, SPACECRAFT POWER

SUPPLIES

N80-22788"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

THERMAL ENERGY STORAGE: FOURTH ANNUAL REVIEW

MEETING

Mar. 1980 650 p refs Meeting held at Tysons Corner, Va.,

3-4 Dec. 1979; sponsored by DOE

(NASA-CP-2125; E-428; CONF-791232) Avail: NTIS HC

A99/MF A01 CSCL 10C

CONFERENCES, ENERGY POLICY, ENERGY TECHNOLOGY,

HEAT STORAGE, THERMAL ENERGY

N81-16533"# National Aeronautics and Space Administration.

Lyndon B. Johnson Space Center, Houston, Tex.

SOLAR POWER SATELLITE MICROWAVE TRANSMISSION AND

RECEPTION

R. H. DIETZ Dec. 1980 271 p refs Workshop held in

Houston, Tex., 15-18 Jan. 1980

(NASA-CP-2141; S-503) Avail: NTIS HC A16/MF A01 CSCL

10A

CONFERENCES, MICROWAVE TRANSMISSION,

RECTENNAS, SATELLITE POWER TRANSMISSION (TO EARTH),

SOLAR POWER SATELLITES, SYSTEMS ENGINEERING

44 ENERGY PRODUCTION AND CONVERSION

N81-17531"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

SPACE PHOTOVOLTAIC RESEARCH AND TECHNOLOGY 1980.

HIGH EFFICIENCY, RADIATION DAMAGE AND BLANKET

TECHNOLOGY

1980 395 p refs Conf. held in Cleveland, 15-17 Oct. 1980

(NASA-CP-2169; E-469) Avail: NTIS HC A17/MF A01 CSCL

10A

CONFERENCES, LASER ANNEALING, RADIATION DAMAGE,

SEMICONDUCTORS (MATERIALS), SILICON, SOLAR CELLS

N81-18493"# National Aeronautics and Space Administration.

Lyndon B. Johnson Space Center, Houston, Tex.

SOLAR POWER SATELLITE SYSTEM SIZING TRADEOFFS

G. D ARNDT and L G. MONFORD Feb. 1981 44 p refs

(NASA-TP-1804; S-505) Avail: NTIS HC A03/MF A01 CSCL

10A

ANTENNA DESIGN, COST ANALYSIS, ENERGY

CONVERSION EFFICIENCY, SOLAR POWER SATELLITES,

SYSTEMS ENGINEERING, TRADEOFFS

N81-21493"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

THE 1980 GODDARD SPACE FLIGHT CENTER BATTERY

WORKSHOP

G. HALPERT Mar. 1981 426 p Proceedings of workshop

held at Greenbelt, Md., 18-20 November 1980

(NASA-CP-2177) Avail: NTIS HC A19/MF A01 CSCL 10C

CONFERENCES, ELECTROCHEMICAL CELLS, SAFETY

FACTORS, SYSTEMS ENGINEERING

N81-27622"# National Aeronautics and Space Administration.

Lyndon B. Johnson Space Center, Houston, Tex.

SATELLITE POWER SYSTEM: CONCEPT DEVELOPMENT AND

EVALUATION PROGRAM. VOLUME 3: POWER

TRANSMISSION AND RECEPTION. TECHNICAL SUMMARY

AND ASSESSMENT

R. H. DIETZ, G. D. ARNDT, J. W. SEYL, L. LEOPOLD, and J. S.

KELLEY Jul. 1981 280 p refs

(NASA-RP-1076; S-507) Avail: NTIS HC A13/MF A01 CSCL

10A

Efforts in the DOE/NASA concept development and evaluation

program are discussed for the solar power satellite power

transmission and reception system. A technical summary is

provided together with a summary of system assessment activities.

System options and system definition drivers are described. Major

system assessment activities were in support of the reference

system definition, solid state system studies, critical technology

supporting investigations, and various system and subsystem

tradeoffs. These activities are described together with reference

system updates and alternative concepts for each of the subsystem

areas. Conclusions reached as a result of the numerous analytical

and experimental evaluations are presented. Remaining issues for

a possible follow-on program are identified. A.R.H

N82-16477"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

NEW FEATURES AND APPLICATIONS OF PRESTO, A

COMPUTER CODE FOR THE PERFORMANCE OF

REGENERATIVE, SUPERHEATED STEAM TURBINE CYCLES

Y. K. CHOO and P. J. STAIGER Jan. 1982 39 p refs

(NASA*TP-1954; E-721) Avail: NTIS HC A03/MF A01 CSCL

10B

COMPUTERIZED SIMULATION, REGENERATION

(ENGINEERING), STEAM TURBINES, THERMODYNAMIC

CYCLES, TURBOGENERATORS

145
44 ENERGYPRODUCTIONANDCONVERSION

N82-23684"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

WIND TURBINE DYNAMICS

R. W. THRESHER, ed. (Oregon State Univ., Corvallis) May

1981 422 p refs Workshop held in Cleveland 24-26 Feb.

1981 Sponsored in part by DOE

(NASA-CP-2185; NAS 1.55:2185; CONF-810226;

SERI/CP-635-1238) Avail: NTIS HC A18/MF A01 CSCL 10B

DYNAMIC STRUCTURAL ANALYSIS, ROTOR AERODYNAMICS, WIND TURBINES, WINDMILLS (WINDPOWERED

MACHINES), WINDPOWERED GENERATORS

N82-28783"# National Aeronautics and Space Administration,

Washington, D.C.

CAPTURING ENERGY FROM THE WIND

J. L. SCHEFTER 1982 88 p refs Original contains color

illustrations

(NASA-SP-455; NAS 1.21:455; LC-81-600180) Avail: NTIS MF

A01; SOD HC $6.00 as 033-000-008-50-3 CSCL 10A

The history of windpower is reviewed. Wind turbine technology

is discussed. Examples of small and large turbines are provided.

Electric power generation is considered. Numerous illustrations are

included. N.W.

N82-32859"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

ENERGY SAVING CONCEPTS RELATING TO INDUCTION

GENERATORS

F. J. NOLA Aug. 1980 12 p refs

(NASA-TP-1719; NAS 1.60:1719) Avail: NTIS HC A02/MF A01

CSCL 10B

ELECTRIC GENERATORS, ENERGY POLICY, INDUCTION

MOTORS, WlNDPOWER UTILIZATION, WlNDPOWERED

GENERATORS

N83-14684"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

LITHIUM/SULFUR DIOXIDE CELL AND BATTERY SAFETY

G. HALPERT and A ANDERSON Nov. 1982 19 p refs

(NASA-RP-1099; NAS 1.61:1099) Avail: NTIS HC A02/MF A01

CSCL 10C

The new high-energy lithium/sulfur dioxide primary

electrochemical cell, having a number of advantages, has received

considerable attention as a power source in the past few years.

With greater experience and improved design by the manufacturers,

this system can be used in a safe manner provided the guidelines

for use and safety precautions described herein are followed. In

addition to a description of cell design and appropriate definitions,

there is a safety precautions checklist provided to guide the user.

Specific safety procedures for marking, handling, transportation,

and disposal are also given, as is a suggested series of tests, to

assure manufacturer conformance to requirements. Author

N83-15806"# National Aeronautics and Space Administration_

Lewis Research Center, Cleveland, Ohio.

SPACE PHOTOVOLTAIC RESEARCH AND TECHNOLOGY 1982:

HIGH EFFICIENCY, RADIATION DAMAGE, AND BLANKET

TECHNOLOGY

Washington 1982 263 p refs Conf. held in Cleveland,

20-22 Apr. 1982

(NASA-CP-2256; E-1303; NAS 1.55:2256) Avail: NTIS HC

A12/MF A01 CSCL IOA

CONFERENCES, PHOTOVOLTAIC CELLS, SPACE

PLATFORMS, SPACECRAFT POWER SUPPLIES

146

N83-t8024*# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SEMICONDUCTOR PHOTOELECTROCHEMISTRY

A. M. BUONCRISTIANI (Christopher Newport Coll.) and C. E.

BYVIK Jan. 1983 94 p refs

(NSG-1514)

(NASA-TP-2088; L-15495; NAS 1.60:2088) Avail: NTIS HC

A05/MF A01 CSCL 10A

CHARGE CARRIERS, CHARGE DISTRIBUTION, CHARGE

TRANSFER, ELECTRODES, ENERGY CONVERSION, PHOTOELECTROCHEMISTRY, SEMICONDUCTORS (MATERIALS)

N83-19231"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

LARGE HORIZONTAL-AXIS WIND TURBINES

R. W. THRESHER, ed. (Oregon State Univ., Corvallis) 1982

823 p refs Workshop held in Cleveland, 28-30 Jul. 1981

Sponsored in part by DOE

(NASA-CP-2230; NAS 1.55:2230; CONF-810752;

SERI/CP-635-1273) Avail: NTIS HC A99/MF A01 CSCL 10A

CONFERENCES, DESIGN ANALYSIS, ENERGY POLICY,

ROTOR BLADES (TURBOMACHINERY), SITE SELECTION, WIND

(METEOROLOGY), WIND TURBINES, WINDPOWERED

GENERATORS

N83-36549"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

ANALYSIS OF POTENTIAL BENEFITS OF

INTEGRATED-GASIFIER COMBINED CYCLES FOR A UTILITY

SYSTEM

Y. K. CHOO Oct. 1983 21 p

(NASA-TP-2172; E-1465; NAS 1.60:2172) Avail: NTIS HC

A02/MF A01 CSCL lOB

COAL GASIFICATION, COMBINED CYCLE POWER

GENERATION, STEAM TURBINES

N84-21977" National Aeronautics and Space Administration,

Washington, D.C.

ENERGY: A CONTINUING BIBLIOGRAPHY WITH INDEXES,

ISSUE 40, JANUARY 1984

Jan. 1984 212 p

(NASA-SP-7043(40); NAS 1.21:7043(40)) Avail: NTIS HC

$15.00 CSCL 10A

This bibliography lists 775 reports, articles and other documents

introduced into the NASA scientific and technical information

system from October 1, 1983 through December 31, 1983.

A.RH.

N84-29307"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

SPACE PHOTOVOLTAIC RESEARCH AND TECHNOLOGY 1983.

HIGH EFFICIENCY, RADIATION DAMAGE, AND BLANKET

TECHNOLOGY

Washington, D.C. 1984 266 p refs Conf. held in Cleveland,

18-20 Oct. 1983

(NASA-CP-2314; E-2005; NAS 1.55:2314) Avail: NTIS HC

A12/MF A01 CSCL 10A

CONFERENCES, RADIATION DAMAGE, SOLAR BLANKETS,

SPACECRAFT POWER SUPPLIES

N86-17839"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

SPACE PHOTOVOLTAIC RESEARCH AND TECHNOLOGY 1985:

HIGH EFFICIENCY, SPACE ENVIRONMENT, AND ARRAY

TECHNOLOGY

1985 282 p refs Conference held in Cleveland, Ohio, 30 Apr.

- 2 May 1985

(NASA-CP-2408; E-2706; NAS 1.55:2408) Avail: NTIS HC

A_!MF A0_ CSCL 10A

AEROSPACE ENVIRONMENTS, EFFICIENCY, PHOTOVOLTAlC CELLS, SOLAR ARRAYS, SOLAR CELLS, SPACECRAFT

POWER SUPPLIES
45 ENVIRONMENT POLLUTION

45

ENVIRONMENT POLLUTION

Includes atmospheric, noise, thermal, and water pollution.

N77-32622"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AN ULTRAVIOLET VIDEO TECHNIQUE FOR VISUALIZATION

OF STACK PLUMES AND FOR MEASURING SULFUR DIOXIDE

CONCENTRATION AND EFFLUENT VELOCITY

R.J. EXTON Sep. 1977 38p refs

(NASA-TP-1014; L-11628) Avail: NTIS HC A03/MF A01

CSCL 13B

PLUMES, SULFUR OXIDES, ULTRAVIOLET PHOTOGRAPHY,

VIDEO EQUIPMENT

N78-11517"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

RESEARCH IN THE USE OF ELECTRETS IN MEASURING

EFFLUENTS FROM ROCKET EXHAUST OF THE SPACE

SHUI-I'LE (6.4 PERCENT SCALED MODEL) AND VIKING 1

LAUNCH

M. SUSKO Nov. 1977 122 p refs

(NASA-TP-1073; M-231) Avail: NTIS HC A06/MF A01 CSCL

13B

ELECTRETS, ROCKET EXHAUST, SPACE SHUTTLES, VIKING

1 SPACECRAFT

N76-11520*# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SOME PHYSICAL AND THERMODYNAMIC PROPERTIES OF

ROCKET EXHAUST CLOUDS MEASURED WITH INFRARED

SCANNERS

R. I. GOMBERG, A. G. KANTSIOS, and F. J. ROSENSTEEL Nov.

1977 32p refs

(NASA-TP-1041; L-11742) Avail: NTIS HC A03/MF A01

CSCL 13B

INFRARED SCANNERS, ROCKET EXHAUST,

THERMODYNAMIC PROPERTIES

N78-13628"# National Aeronautics and Space Administration.

Lanalev Research Center, Hampton, Va.

QUANTITATIVE ANALYSIS OF AIRCRAFT MULTISPECTRALSCANNER DATA AND MAPPING OF WATER-QUALITY PARAMETERS IN THE JAMES RIVER IN VIRGINIA

R. W. JOHNSON and G. S. BAHN (Vought Corp., Hampton, Va.)

Dec. 1977 33 p refs

(NASA-TP-1021; L-10968) Avail: NTiS HC A03/MF A01

CSCL 13B

MULTtSPECTRAL BAND SCANNERS, QUANTITATIVE

ANALYSIS, RIVERS, VIRGINIA, WATER QUALITY

N78-15596"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECTS OF ENTRAINED WATER AND STRONG TURBULENCE

ON AFTERBURNING WITHIN SOLID ROCKET MOTOR

PLUMES

R. I. GOMBERG and R. G. WILMOTH Jan. 1978 39 p refs

(NASA-TP-1111; L-11875) Avail: NTIS HC A03/MF A01

CSCL 21H

AFTERBURNING, EXHAUST GASES, ROCKET EXHAUST,

SPACE SHUTTLES

N78-20654"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

WATER-VAPOR PRESSURE CONTROL IN A VOLUME

J. J. SCIALDONE Mar. 1978 20 p refs

(NASA-TP-1172; G-7802-F6) Avail: NTIS HC A02/MF A01

CSCL 13B

PURGING, SPACECRAFT CABIN ATMOSPHERES, WATER

VAPOR

N78-28682"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

THERMODYNAMIC AND CHEMICAL PARAMETERS OF THE

EXHAUST EFFLUENTS FROM THE HARPOON BOOSTER

MOTOR

J. B. STEPHENS and A. I. GOLDFORD (Science Applications,

Inc., Huntsville, Ala.) Jul. 1978 49 p refs

(NASA-TP-1280; M-257) Avail: NTIS HC A03/MF A01 CSCL

13B

BOOSTER ROCKET ENGINES, COMBUSTION PRODUCTS,

EXHAUST GASES, HARPOON MISSILE

N78-12554"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

LABORATORY MEASUREMENTS OF RADIANCE AND

REFLECTANCE SPECTRA OF DILUTE PRIMARY-TREATED

SEWAGE SLUDGE

J. W. USRY, W. G. WITTE, C. H. WHITLOCK, and E. A.

GURGANUS Nov. 1977 27 p refs

(NASA-TP-1038; L-11767) Avail: NTIS HC A03/MF A01

CSCL 13B

RADIANCE, REFLECTANCE, SEWAGE TREATMENT

N78-33616"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

LABORATORY AND FIELD MEASUREMENTS OF UPWELLED

RADIANCE AND REFLECTANCE SPECTRA OF SUSPENDED

JAMES RIVER SEDIMENTS NEAR HOPEWELL, VIRGINIA

C. H. WHILOCK, W. G. WITTE, E. A. GURGANUS, and J. W.

USRY Oct. 1978 30 p refs

(NASA-TP-1292; L-12298) Avail: NTIS HC A03/MF A01

CSCL 13B

SEDIMENTS, SPECTRAL REFLECTANCE, UPWELLING

WATER, VIRGINIA, WATER POLLUTION

N78-12555"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

LABORATORY MEASUREMENTS OF RADIANCE AND

REFLECTANCE SPECTRA OF DILUTE SECONDARY-TREATED

SEWAGE SLUDGE

W. G. WITTE, J. W. USRY, C. H. WHITLOCK, and E. A.

GURGANUS Dec. 1977 23 p refs

(NASA-TP-1089; L-11870) Avail: NTIS HC A02/MF A01

CSCL 13B

OCEANS, REMOTE SENSORS, WASTE DISPOSAL

N78-33617"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

QUANTITATIVE MAPPING BY REMOTE SENSING OF AN

OCEAN ACID-WASTE DUMP

C. W. OHLHORST Oct. 1978 27 p refs

(NASA-TP-1275; L-11927) Avail: NTIS HC A02/MF A01

CSCL 13B

ACIDS, ENVIRONMENTAL SURVEYS, MAPPING, OCEAN

SURFACE, QUANTITATIVE ANALYSIS, REMOTE SENSORS,

WATER POLLUTION

147
45 ENVIRONMENT POLLUTION

N78-33618"# National Aeronautics and Space Administration.

!pwi_ _,_eRreh m.'-ter, Cleveland, Ohio.

OZONE CONCENTRATION IN THE CABIN OF A GATES LEARJET MEASURED SIMULTANEOUSLY WITH ATMOSPHERIC

OZONE CONCENTRATIONS

D. BRtEHL anO P. J. PERKINS Oct. 1978 20 p refs

(NASA-TP-1340; E-9653) Avail: NTIS HC A02/MF A01 CSCL

_3FI

AIRCRAFT COMPARTMENTS, ATMOSPHERIC COMPOSITION, CABIN ATMOSPHERES, CONCENTRATION (COMPOSITION), LEAR JET AIRCRAFT, OZONOMETRY

N79-14591"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

DESCRIPTION AND FIELD TEST OF AN IN SITU COLIFORM

MONITORING SYSTEM

D. C. GRANA and J. R. WILKINS Jan. 1979 37 p refs

(NASA-TP-1334; L-12361) Avail: NTIS HC A03/MF A01

CSCL 13B

BACTERIA, POLLUTION MONITORING, SAMPLING

N79-17360"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

LABORATORY MEASUREMENTS OF RADIANCE AND

REFLECTANCE SPECTRA OF A DILUTE BIOSOLID

INDUSTRIAL WASTE PRODUCT

J. W. USRY, W. G. WITTE, C. H. WHITLOCK, and E. A.

GURGANUS Feb. 1979 23 p refs

(NASA-TP-1401; L-12641) Avail: NTIS HC A02/MF A01

CSCL 13B

INDUSTRIAL WASTES, RADIANCE, REFLECTANCE, SLUDGE,

SPECTRAL SIGNATURES

N79-18479"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

CONDENSATION-NUCLEI (AITKEN PARTICLE) MEASUREMENT

SYSTEM USED IN NASA GLOBAL ATMOSPHERIC SAMPLING

PROGRAM

T. W. NYLAND Feb. 1979 28 p refs

(NASA-TP-1415; E-9816) Avail: NTIS HC A03/MF A01 CSCL

13B

AITKEN NUCLEI, CALIBRATING, CONDENSING, GLOBAL

ATMOSPHERIC RESEARCH PROGRAM, MEASURING

INSTRUMENTS, POLLUTION MONITORING

N79-22654"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

OZONE MEASUREMENT SYSTEM FOR NASA GLOBAL AIR

SAMPLING PROGRAM

M. W. TIEFERMANN May 1979 21 p refs

(NASA-TP-1451; E-9829) Avail: NTIS HC A02/MF A01 CSCL

13B

AIR POLLUTION, CONCENTRATION (COMPOSITION),

GLOBAL AIR SAMPLING PROGRAM, OZONE

N79-28796"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECTS OF ROAD TRAFFIC BACKGROUND NOISE ON

JUDGMENTS OF INDIVIDUAL AIRPLANE NOISES Ph.D. Thesis

C. A. POWELL JuL 1979 44 p refs

(NASA-TP-1433; L-12651) Avail: NTIS HC A03/MF A0t

CSCL 13B

AIRCRAFT NOISE, BACKGROUND NOISE, NOISE

MEASUREMENT, PSYCHOACOUSTICS

148

N79-29679"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SPATIAL-FREQUENCY RESPONSE OF THE LIMB INFRARED

MONITOR OF THE STRATOSPHERE

R. G. WILSON, A. JALINK, JR., and W. M. KAHLBAUM, JR. Aug.

1979 52p refs

(NASA-TP-1504; L-13037) Avail: NTIS HC A04/MF A01

CSCL 13B

FREQUENCY RESPONSE, INFRARED SCANNERS,

STRATOSPHERE

N79-30844"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

PROGRAMS FOR CALCULATING CELL PARAMETERS IN

ELECTRON AND X-RAY DIFFRACTION

G. POLKOWSKI (LFE Corp., Richmond, Calif.), K. G. SNETSINGER,

and N, H. FARLOW Aug, 1979 57 p refs

(NASA-TP-1529; A-7761) Avail: NTIS HC A04/MF A01 CSCL

13B

AEROSOLS, COMPUTER PROGRAMS, DIFFRACTION

PATTERNS, ELECTRON DIFFRACTION, STRATOSPHERE, X RAY

DIFFRACTION

N79-31841"# National Aeronautics and Space Administration,

Lewis Research Center, Cleveland, Ohio.

CARBON MONOXIDE MEASUREMENT IN THE GLOBAL

ATMOSPHERIC SAMPLING PROGRAM

T. J. DUDZINSKI Sep. 1979 26 p refs

(NASA-TP-1526; E-9972) Avail: NTIS HC AO3/MF A01 CSCL

13B

CARBON MONOXIDE, GLOBAL AIR SAMPLING PROGRAM,

MEASURING INSTRUMENTS, POLLUTION MONITORING

N79-32743"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

LABORATORY STUDY OF ANNOYANCE TO COMBINED

AIRPLANE AND ROAD-TRAFFIC NOISE

C. A. POWELL Washington Sep. 1979 40 p refs

(NASA-TP-1478; L-12977) Avail: NTIS HC A03/MF A01

CSCL 13B

ACOUSTIC SIMULATION, AIRCRAFT NOISE, HUMAN

TOLERANCES, NOISE POLLUTION, NOISE TOLERANCE

N79-32744'# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

A SUMMATION AND INHIBITION MODEL OF ANNOYANCE

RESPONSE TO MULTIPLE COMMUNITY NOISE SOURCES

C. A. POWELL Washington Sep. 1979 23 p refs

(NASA-TP-1479; L-12978) Avail: NTIS HC A02/MF A01

CSCL 13B

COMMUNITIES, MATHEMATICAL MODELS, NOISE

POLLUTION, NOISE REDUCTION

N79-33611"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

MEASUREMENT TECHNIQUES FOR TRACE METALS IN

COAL-PLANT EFFLUENTS: A BRIEF REVIEW

J. J. SINGH Washington Oct. 1979 34 p refs

(NASA-RP-1047; L-13164) Avail: NTIS HC A03/MF A01

CSCL 13B

The strong features and limitations of techniques for determining

trace elements in aerosols emitted from coal plants are discussed.

Techniques reviewed include atomic absorption spectroscopy,

charged particle scattering and activation, instrumental neutron

activation analysis, gas/liquid chromatography, gas

chromatographJc./mass spectrometric methods, X-ray fluorescence,

and charged-particle-induced X-ray emission. The latter two

methods are emphasized. They provide simultaneous, sensitive

multielement analyses and lend themselves readily to depth

profiling. It is recommended that whenever feasible, two or more

complementary techniques should be used for analyzing

environmental samples. K.L.
N80-14581"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

SULFATE AND NITRATE COLLECTED BY FILTER SAMPLING

NEAR THE TROPOPAUSE

F. M. HUMENIK, E. A, LEZBERG, and D. A. OTTERSON Jan.

1980 30p refs

(NASA-TP-1567; E-073) Avail: NTIS HC A03/MF A01 CSCL

13B

AIR POLLUTION, AIR SAMPLING, NITRATES, SULFATES,

TROPOPAUSE

N80-15649"# National Aeronautics and Space Administration.

Lyndon B, Johnson Space Center, Houston, Tex.

PROCEEDINGS OF SHUTTLE ENVIRONMENTAL EFFECTS

PROGRAM REVIEW

A. E. POTTER, ed. Washington Jan. 1980 124 p refs

Conf. held at Kennedy Space Center, Fla., 21-22 Mar. 1978

(NASA-CP-2110; S-489) Avail: NTIS HC A06/MF A01 CSCL

13B

CONFERENCES, ECOLOGY, ROCKET EXHAUST, SOLID

PROPELLANT ROCKET ENGINES, SPACE SHUTTLES

N80-27832"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

COORDINATED AIRCRAFT AND SHIP SURVEYS FOR

DETERMINING IMPACT OF RIVER INPUTS ON GREAT LAKES

WATERS. REMOTE SENSING RESULTS

C. A. RAQUET, J. A. SALZMAN, T. A. CONEY, R. A. SVEHLA, D.

F. SHOOK, and R. T. GEDNEY Jul. 1980 105 p refs

(NASA-Tpo1694; E-172) Avail: NTIS HC A06/MF A01 CSCL

13B

EFFLUENTS, LAKE ERIE, LAKE MICHIGAN, LAKE ONTARIO,

LAKE SUPERIOR, POLLUTION MONITORING

N80-28946"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ANNOYANCE DUE TO MULTIPLE AIRPLANE NOISE

EXPOSURE

C. A. POWELL Aug. 1980 42 p refs

(NASA-TP-1706; L-13710) Avail: NTIS HC A03/MF A01

CSCL 13B

AIRCRAFT NOISE, HUMAN FACTORS ENGINEERING,

HUMAN REACTIONS, NOISE POLLUTION

N80-29911"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECTS OF CONVERSATION INTERFERENCE ON

ANNOYANCE DUE TO AIRCRAFT NOISE

K. F. KEY andC. A. POWELL Aug. 1980 38 p refs

(NASA-TP-1712; L-t3709) Avail: NTIS HC A03/MF A01

CSCL 13B

AIRCRAFT NOISE, CONVERSATION, INTERFERENCE, NOISE

TOLERANCE

N81-11565"# National Aeronautics and Space Administration.

Langley Research Center, Hamptor Va.

EXPERIMENTAL STUDY OF CLUSTER FORMATION IN BINARY

MIXTURE OF H20 AND H2SO4 VAPORS IN THE PRESENCE

OF AN IONIZING RADIATION SOURCE

J. J. SINGH, A. C. SMITH, and G. K. YUE (Inst. for Atmospheric

Optics and Remote Sensing, Hampton, Va.) Nov. 1980 30 p

refs

(NASA-TP-1735; L-13878) Avail: NTIS HC A03/MF A01

CSCL 13B

IONIZING RADIATION, MOLECULAR INTERACTIONS,

NITROGEN, SPECTROSCOPIC ANALYSIS, SULFURIC ACID,

WATER

45 ENVIRONMENT POLLUTION

N81-17622"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

TWO-DIMENSIONAL MODEL STUDIES OF THE EFFECT OF

SUPERSONIC AIRCRAFT OPERATIONS ON THE

STRATOSPHERIC OZONE CONTENT

R. C. WHITTEN, W. J. BORUCKI, t. G. POPPOFF (Flick Point

Associates, Carnelian Bay, Calif.), L. LATT (Aerospace Corp., El

Segundo, Calif.), G. F. WlDHOPF (Aerospace Corp., El Segundo,

Calif.), L. A. CAPONE (San Jose State Univ.), and C. A. REIGEL

(San Jose State Univ.) Feb. 1981 72 p refs

(NASA-RP-1064; A-8270) Avail: NTIS HC A04/MF A01 CSCL

13B

For a fleet of 250 aircraft, the change in the ozone column is

predicted to be very close to zero; in fact, the ozone overburden

may actually increase as a result of show that above 25 to 30 km

the ozone abundance decreases via catalytic destruction, but at

lower heights it increases, mainly as a result of coupling with odd

hydrogen species. Water vapor released in the engine exhaust is

predicted to cause ozone decreases; for the hypothetical engines

used in the study, the total column ozone changes due to water

vapor emission largely offset the predicted ozone increases due

to NOx emission. The actual effect of water vapor may be less

than calculated because present models do not include thermal

feedback. Feedback refers to the cooling effect of additional water

vapor that would tend to slow the NOx reactions which destroy

ozone, TM.

N81-22587"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

A DIAGNOSTIC MODEL FOR STUDYING DAYTIME URBAN AIR

QUALITY TRENDS

D. A. BREWER (George Washington Univ., Hampton, Va.), E. E.

REMSBERG, and G. E. WOODBURY May 1981 43 p refs

(NASA-TP-1843; L-14251) Avail: NTIS HC A03/MF A01

CSCL 13B

AIR QUALITY, ATMOSPHERIC MODELS, PHOTOCHEMICAL

REACTIONS, POLLUTION MONITORING, SMOG, URBAN

RESEARCH

N81-24601"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ANALYTIC MODEL FOR WASHOUT OF HCL(G) FROM

DISPERSING ROCKET EXHAUST CLOUDS

G. L. PELLETT May 1981 92 p refs

(NASA-TP-1801; L-14107) Avail: NTIS HC A05/MF A01

CSCL 13B

ACID RAIN, CHEMICAL CLOUDS, ENVIRONMENT

POLLUTION, HYDROGEN CHLORIDES, MATHEMATICAL

MODELS, ROCKET EXHAUST

N82-12654"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECTS OF ACTIVITY INTERFERENCE ON ANNOYANCE DUE

TO AIRCRAFT NOISE

K. F. WILLSHIRE and C. A. POWELL Nov. 1981 29 p refs

(NASA-TP-1938; L-14808) Avail: NTIS HC A03/MF A01

CSCL 13B

AIRCRAFT NOISE, HUMAN REACTIONS, NOISE POLLUTION,

PSYCHOACOUSTICS

N82-14672"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

APPLICATION OF A GAUSSIAN MULTILAYER DIFFUSION

MODEL TO CHARACTERIZE DISPERSION OF VERTICAL HCL

COLUMN DENSITY IN ROCKET EXHAUST CLOUDS

G. L. PELLETT and W. L. STATON Dec. 1981 74 p refs

(NASA-TP-1956; L-14715) Avail: NTIS HCA04/MF A01

CSCL 13B

AIR POLLUTION, ATMOSPHERIC EFFECTS, FLORIDA,

HYDROGEN CHLORIDES, ROCKET EXHAUST, SOLID ROCKET

PROPELLANTS, VERTICAL DISTRIBUTION

149
45 ENVIRONMENT POLLUTION

N82-19707"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECTS OF REPETITION RATE AND IMPULSIVENESS OF

SIMULATED HELICOPTER ROTOR NOISE ON ANNOYANCE

C. A. POWELL and D. A. MCCURDY Feb. 1982 59 p refs

(NASA-TP-1969; L-14936) Avail: NTIS HC A04/MF A01

CSCL 20A

AIRCRAFT NOISE, HELICOPTERS, NOISE TOLERANCE,

PRESSURE PULSES, PULSE RATE, ROTARY WINGS

N82.21TT4*# Nationat Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

LABORATORY UPWELLED RADIANCE AND REFLECTANCE

SPECTRA OF KERR RESERVOIR SEDIMENT WATERS

W. G. WITTE, C. H. WHITLOCK, W. D, MORRIS, and E, A.

GURGANUS Mar. 1982 22 p refs

(NASA-TP-1993; L-14992; NAS 1.60:1993) Avail: NTIS HC

A02/MF A01 CSCL 13B

RADIANCE, RESERVOIRS, SEDIMENTS, SPECTRAL

REFLECTANCE, UPWELLING WATER

N82-27867"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

CALCULATION OF COMPOSITION DISTRIBUTION OF

ULTRAFINE ION-H20-H2S04 CLUSTERS USING A MODIFIED

BINARY ION NUCLEATION THEORY

J. J. SINGH, A. S. SMITH, L. Y. CHAN (Institute for Atmospheric

Optics and Remote Sensing), and G. K. YUE (Institute for

Atmospheric Optics and Remote Sensing) Jun. 1982 24 p

refs

(NASA-TP-2031; L-1533; NAS 1.60:2031) Avail: NTIS HC

A02/MFA01 CSCL 13B

CLUMPS, IONS, NUCLEATION

N82-28839"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SIMPLIFIED FREE-ENERGY CALCULATION FOR ION-INDUCED

HETEROMOLECULAR NUCLEATION

J. J. SINGH. A. C. SMITH, L. Y. CHAN (Inst. for Atmospheric

Optics and Remote Sensing), and G. K. YUE (Inst. for Atmospheric

Optics and Remote Sensing) Jul. 1982 22 p refs

(NASA-TP-2039; L-15392; NAS 1.60:2039) Avail: NTIS HC

A02/MF A01 CSCL 13B

CLUMPS, GIBBS FREE ENERGY, NUCLEATION

N83-12595"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

CHARACTERIZATION OF SOIL AND POSTLAUNCH PAD

DEBRIS FROM CAPE CANAVERAL LAUNCH COMPLEX AND

ANALYSIS OF SOIL INTERACTION WITH AQUEOUS HCL

G. L. PELLETT, L. W. SPANGLER, R. W. STOREY, and R. J.

BENDURA Oct. 1982 26 p refs Presented at an Environ.

Effects Program Review at Cocoa Beach, Fla., Mar. 1978

(NASA-TP-2076; L-t5433; NAS 1.60:2076) Avail: NTIS HC

A03/MF A01 CSCL 13B

DEBRIS, FRACTIONATION, HYDROCHLORIC ACID,

LAUNCHING PADS, QUARTZ, ROCKET EXHAUST, SOIL

MAPPING, SOIL MECHANICS

N83-13643"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

WATER VAPOR MEASUREMENT SYSTEM IN GLOBAL

ATMOSPHERIC SAMPLING PROGRAM, APPENDIX

D. R. ENGLUND and T. J. DUDZINSKI Nov. 1982 18 p refs

(NASA-TP-2051; E-1167; NAS 1.60:2051) Avail: NTIS HC

A02/MF A01 CSCL 13B

DEW, FROST, GLOBAL AIR SAMPLING PROGRAM,

MOISTURE CONTENT, POLLUTION MONITORING, WATER

VAPOR

150

N83-16951"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

MULTIPLE-EVENT AIRPLANE NOISE ANNOYANCE

C. A. POWELL Jan. 1983 34 p refs

(NASA-TP-2101; L-15517; NAS 1.60:2101) Avail: NTIS HC

A03/MFA01 CSCL 13B

AIRCRAFT NOISE, AUDITORY STIMULI, PHYSIOLOGICAL

FACTORS, PSYCHOACOUSTICS, PSYCHOLOGICAL EFFECTS

N83-16952"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AIRBORNE MEASUREMENTS OF LAUNCH VEHICLE

EFFLUENT: LAUNCH OF SPACE SHUTTLE (STS-1) ON 12

APRIL 1981

G. L. GREGORY, D. C. WOODS, and D. I. SEBACHER Jan.

1983 74 p refs

(NASA-TP-2090; L-15494; NAS 1.60:2090) Avail: NTIS HC

A04/MF A01 CSCL 13B

EFFLUENTS, ENVIRONMENT EFFECTS, HYDROGEN

CHLORIDES, ROCKET EXHAUST, SPACE TRANSPORTATION

SYSTEM 1 FLIGHT, SPACECRAFT LAUNCHING

N84-18764"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AIRBORNE MEASUREMENTS OF LAUNCH VEHICLE EFFLUENT

OF STS-2 LAUNCH ON NOVEMBER 12, 1981 AT CAPE

CANAVERAL, FLORIDA

G. L. MADDREA, JR., G. L. GREGORY, D. I. SEBACHER, and D.

C. WOODS Feb. 1984 47 p refs

(NASA-TP-2260; L-15715; NAS 1.60:2260) Avail: NTIS HC

A03/MF A01 CSCL 13B

AIR QUALITY, CORRELATION, EXHAUST EMISSION,

FLORIDA, LIGHT SCATTERING, SAMPLING, SPACE SHUTTLES

N86-16748"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AIRBORNE LIDAR MEASUREMENTS OF AEROSOLS, MIXED

LAYER HEIGHTS, AND OZONE DURING THE 1980

PEPE/NEROS SUMMER FIELD EXPERIMENT

E. V. BROWELL, S. T. SHIPLEY, C. F. BUTLER (Old Dominion

Univ., Norfolk, Va.), and S. ISMAIL (SASC Technologies, Inc.,

Hampton, Va.) Dec. 1985 197 p refs

(NASA-RP-1143; L-15943; NAS 1.61:1143) Avail: NTIS HC

A09/MF A01 CSCL 13B

A detailed summary of the NASA Ultraviolet Differential

Absorption Lidar (UV DIAL) data archive obtained during the EPA

Persistent Elevated Pollution Episode/Northeast Regional Oxidant

Study (PEPE/NEROS) Summer Field Experiment Program (July

through August 1980) is presented. The UV dial data set consists

of remote measurements of mixed layer heights, aerosol

backscatter cross sections, and sequential ozone profiles taken

during 14 long-range flights onboard the NASA Wallops Flight

Center Electra aircraft. These data are presented in graphic and

tabular form, and they have been submitted to the PEPE/NEROS

data archive on digital magnetic tape. The derivation of mixing

heights and ozone profiles from UV Dial signals is discussed, and

detailed intercomparisons with measurements obtained by in situ

sensors are presented. Author
46

GEOPHYSICS

Includes aeronomy; upper and lower atmosphere studies;

ionospheric and magnetospheric physics; and geomagnetism.

N77-15563"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ATMOSPHERIC AEROSOLS: THEIR OPTICAL PROPERTIES

AND EFFECTS

1976 316 p refs Conf. proc. held at Williamsburg, Va., 13-15

Dec. 1976; Sponsored by NASA Langley Research Center and

the Optical Soc. of Am.

(NASA-CP-2004) Avail: NTIS HC At4/MF A01 CSCL 04A

AEROSOLS, HUMIDITY, OPTICAL PROPERTIES

N77-15564"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ATMOSPHERIC AEROSOLS: THEIR OPTICAL PROPERTIES

AND EFFECTS (SUPPLEMENT)

1976 46 p refs Conf. proc. held at Williamsburg, Va., 13-15

Dec. 1976; sponsored by NASA Langley Research Center and

the Optical Soc. of Am.

(NASA-CP-2004-SUPPL) Avail: NTIS HC A03/MF A01 CSCL

04A

AEROSOLS, ATMOSPHERIC EFFECTS, ATMOSPHERIC

REFRACTION, CONFERENCES, OPTICAL PROPERTIES

N77-31694"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

CHLOROFLUOROMETHANES AND THE STRATOSPHERE

R. D. HUDSON, ed. Aug. 1977 268 p refs Workshop held

at Warrenton, Va., 10 Jan. 1977

(NASA-RP-t010; G-7725) Avail: NTIS HC A12/MF A01 CSCL

04A

The conclusions of a workshop held by the National Aeronautics

and Space Administration to assess the current knowledge of the

impact of chlorofluoromethane release in the troposphere on

stratospheric ozone concentrations. The following topics are

discussed; (1) Laboratory measurements; (2) Ozone measurements

and trends; (3) Minor species and aerosol measurements; (4) One

dimensional modeling; and (5) Multidimensional modeling.

N78-11545"# National Aeronautics and Space Administration,

Washington, D.C.

NATIONAL GEODETIC SATELLITE PROGRAM, PART 1 Final

Report

S. W. HENRIKSEN, ed. (Am. Geophys. Union) 1977 523 p

refs 2 Vol.

(NASA-SP-365-PT-1) Avail: NTIS MF A01; SOD HC CSCL

04A

The work performed by individual contributors to the National

Geodetic Satellite Program is presented. The purpose of the

organization, the instruments used in obtaining the data, a

description of the data itself, the theory used in processing the

data, and evaluation of the results are detailed for the participating

organizations. For individual titles, see N78-11548 through

N78-11551.

N78-11552"# National Aeronautics and Space Administration,

Washington, D.C.

NATIONAL GEODETIC SATELLITE PROGRAM, PART 2 Final

Report

1977 509 p refs 2 Vol.

(NASA-SP-365-PT-2) Avail: NTIS MF A01; SOD HC CSCL

04A

The work performed by individual contributors to the National

Geodetic Satellite Program is presented. The purpose of the

specific organization, the instruments used in obtaining the data,

a description of the data itself, the theory used in processing the

data, and evaluation of the results are detailed for each participating

46 GEOPHYSICS

organization. An overall evaluation of the entire program is given.

For individual titles, see N78-11553 through N78-11557.

N78-12586"# National Aeronautics and Space Administration,

Washington, D.C.

INVERSION METHODS IN ATMOSPHERIC REMOTE

SOUNDING

A. DEEPAK, ed. 1977 609 p refs Workshop held at

Hampton, Va., 15-17 Dec. 1976 Sponsored in part by Old Dominion

Univ.

(NASA-CP-004) Avail: NTIS HC A99/MF A01 CSCL 04A

APPLICATIONS OF MATHEMATICS, ATMOSPHERIC

COMPOSITION, CONFERENCES, DATA PROCESSING,

INVERSIONS, REMOTE SENSORS

N78-21690"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

MICROWAVE EMISSION FROM POLAR FIRN

A. T, C. CHANG and B. J. CHOUDHURY (Computer Sciences

Corp., Silver Spring, Md.) Apr. 1978 24 p refs

(NASA-TP-1212) Avail: NTIS HC A02/MF A01 CSCL 04A

MICROWAVE EMISSION, POLAR CAPS, SNOW COVER

N78-21691"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

ON THE TIDAL OSCILLATIONS OF THE LIQUID CORE OF THE

EARTH

P. MUSEN Apr. 1978 71 p refs

(NASA-TP-1223; G-7802-F11) Avail: NTIS HC A04/MF A01

CSCL 08K

EARTH CORE, LIQUIDS, TIDES

N78-26677"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

ESTIMATION OF SNOW TEMPERATURE AND MEAN CRYSTAL

RADIUS FROM REMOTE MULTISPECTRAL PASSIVE

MICROWAVE MEASUREMENTS

A. T. C. CHANG Jun. 1978 15 p refs

(NASA-TP-1251) Avail: NTIS HC A02/MF A01 CSCL 08L

MICROWAVES, RADIOMETERS, RAYLEIGH SCATTERING,

SNOW COVER, TEMPERATURE MEASUREMENT

N78-29669"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

EXPLORATORY MEETING ON ATMOSPHERIC ELECTRICITY

AND SEVERE STORMS

W. W. VAUGHAN, ed. Jul. 1978 30 p refs Meeting held at

Huntsville, Ala., 10-tl Apr. 1978

(NASA-CP-2056) Avail: NTIS HC A03/MF A01 CSCL 04A

ATMOSPHERIC ELECTRICITY, CONFERENCES, STORMS

(METEOROLOGY)

N79-10634"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

MAN'S IMPACT ON THE TROPOSPHERE: LECTURES IN

TROPOSPHERIC CHEMISTRY

J. S. LEVINE, ed. and D. R. SCHRYER, ed. Sep. 1978 371 p

refs Lectures held at Hampton, Va, 1977

(NASA-RP-1022; L-12142) Avail: NTIS HC A16/MF A01

CSCL 04A

Lectures covering a broad spectrum of current research in

tropospheric chemistry with particular emphasis on the interaction

of measurements, modeling, and understanding of fundamental

processes are presented. For individual titles, see N79-10635

through N79-10644.

N79-13601" National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

OGO PROGRAM SUMMARY, SUPPLEMENT 1

J. E. JACKSON Jun. 1978 119 p

(NASA-SP-7601-SUPPL-1) Avail: NTIS HC A06 CSCL 04A

Scientific results from OGO-5 and OGO-6 experiments are

summarized and approximately 200 citations are included to update

the 1975 OGO bibliography. Personal author, subject, and corporate

151
46 GEOPHYSICS

source indexes are included. The supplement follows the same

format as that of the OGO Program Summary; it does not repeat

the finalized information in the original publication, which should

be consulted for indexes of experiments, experimenters, institutions,

and the glossary of abbreviations and acronyms. A.R.H.

N79-13607"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

ATMOSPHERIC EFFECTS ON CO2 LASER PROPAGATION

S. S. R. MURTY (Alabama A and M Univ., Normal) and J. W.

BILBRO Nov. 1978 107 p refs

(NASA-TP-1357; M-269) Avail: NTIS HC A06/MF A01 CSCL

04A

ATMOSPHERIC EFFECTS, CARBON DIOXIDE LASERS,

LASER OUTPUTS, TRANSMISSION, WAVE PROPAGATION

N79-16473"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

PRELIMINARY RESULTS OF SAR SOIL MOISTURE

EXPERIMENT, NOVEMBER 1975

B. J. CHOUDHURY, A. T. C. CHANG, T. J. SCHMUGGE, V. V.

SALOMONSON, and J. R. WANG Jan. 1979 21 p refs

(NASA-TP-1404; G-7802-F21) Avail: NTIS HC A02/MF A01

CSCL 08M

REMOTE SENSORS, SOIL MOISTURE, SYNTHETIC

APERTURE RADAR

N79-17388°# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

LIDAR BACKSCATTERING MEASUREMENTS OF

BACKGROUND STRATOSPHERIC AEROSOLS

E. E. REMSBERG, G. B. NORTHAM, and C. F. BUTLER (Old

Dominion Univ.) Feb. 1979 35 p refs

(NASA-TP-1381; L-12292) Avail: NTIS HC A03/MF A01

CSCL 04A

AEROSOLS, BACKSCATTERING, OPTICAL RADAR,

POLLUTION MONITORING, STRATOSPHERE

N79-19519"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

PRELIMINARY RESULTS OF PASSIVE MICROWAVE SNOW

EXPERIMENT DURING FEBRUARY AND MARCH 1978

A. T. C. CHANG, J. C. SHIUE, H. BOYNE (NBS, Boulder, Colo.),

D. ELLERBRUCH (NBS, Boulder, Colo.), G. COUNAS (NBS,

Boulder, Colo.), R. WITTMANN (NBS, Boulder, Colo.), and R.

JONES (NBS, Boulder, Colo.) Mar. 1979 114 p refs

(NASA-TP-t408; REPT-7802-F22) Avail: NTIS HC A06/MF A01

CSCL 04A

MICROWAVE RADIOMETERS, MULTISPECTRAL BAND

SCANNERS, SNOW COVER

N79-30869"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

PROCEEDINGS: WORKSHOP ON THE NEED FOR LIGHTNING

OBSERVATIONS FROM SPACE

L. S. CHRISTENSEN, ed., W. FROST, ed., and W. W. VAUGHAN,

ed. Jul. 1979 255 p refs Workshop held at Tullahoma,

Tenn., 13-15 Feb. 1979 Supersedes NASA-CP-2083; N79-21697

Prepared in cooperation with Tenn. Univ. Space Inst., Tullahoma

(NASA-CP-2095) Avail: NTIS HC A12/MF A01 CSCL 04A

CONFERENCES, LIGHTNING, REMOTE SENSORS,

SATELLITE OBSERVATION, SATELLITE-BORNE INSTRUMENTS

N79-31864"# National Aeronautics and Space Administration,

Washington, D.C.

APPLICATION OF SPACE TECHNOLOGY TO CRUSTAL

DYNAMICS AND EARTHQUAKE RESEARCH

Aug. 1979 274 p refs

(NASA-TP-1464) Avail: NTIS HC A12/MF A0t CSCL 08K

EARTH CRUST, EARTHQUAKES, GEODESY, GEOPHYSICS,

TECHNOLOGY UTILIZATION

N80-13730"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AN ASYMPTOTIC EXPANSION APPROACH TO THE INVERSE

RADIATIVE TRANSFER PROBLEM

R. I. GOMBERG and J. J. BUGLIA Washington Dec. 1979

32 p refs

(NASA-TP-1587; L-13165) Avail: NTIS HC A03/MF A01

CSCL 04A

ASYMPTOTIC SERIES, ATMOSPHERIC COMPOSITION,

CONCENTRATION (COMPOSITION), RADIATIVE TRANSFER

N80-23912"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

VOLCANIC FEATURES OF HAWAII. A BASIS FOR

COMPARISON WITH MARS

M. H. CARR (U.S. Geological Survey, Menlo Park, Calif.) and R.

GREELEY Washington 1980 216 p refs Original contains

color illustrations

(NASA-SP-403; LC-80-600024) Avail: NTIS MF A01; SOD HC

$14.00 CSCL 08K

Despite the difference in size Martian and Hawaiian volcanoes

have numerous characteristics in common. Specific features such

as lava channels, collapsed lava tubes, levees and flow fronts, all

very common in Hawaii, are also abundant on the flanks of some

of the Martian volcanoes. Striking differences also exist, such as

the apparent lack of radial rift zones on some Martian volcanoes

and the paucity of cinder and spatter cones. Some of the best

photographs of Martian and Hawaiian volcanic features are

presented. Descriptive legends are provided for each picture. An

overview of the geological processes and structures depicted is

included. A.R.H.

N79-25609"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

MIDDLE ATMOSPHERE ELECTRODYNAMICS: REPORT OF

THE WORKSHOP ON THE ROLE OF THE ELECTRODYNAMICS

OF THE MIDDLE ATMOSPHERE ON SOLAR TERRESTRIAL

COUPLING

N. C. MAYNARD, ed. Jun. 1979 268 p refs Workshop held

at Reston, Va., 17-19 Jan. 1979

(NASA-CP-2090) Avail: NTIS HC A12/MF A01 CSCL 04A

ATMOSPHERIC ELECTRICITY, CONFERENCES, COUPLING,

ELECTRIC FIELDS, ELECTRODYNAMICS, MIDLATtTUDE

ATMOSPHERE, TERRESTRIAL RADIATION

N80-27866"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

HIGH RESOLUTION INFRARED SPECTROSCOPY TECHNIQUES

FOR UPPER ATMOSPHERIC MEASUREMENTS

D. G. MURCRAY, ed. (Denver, Univ.) and J. M. ALVAREZ, ed.

May 1980 109 p refs Workshop held in Silverthorne Colo.,

31 Jul. - 2 Aug. 1979

(NASA-CP-2134; L-13780) Avail: NTIS HC A06/MF A01

CSCL 04A

ATMOSPHERIC COMPOSITION, CONFERENCES, HIGH

RESOLUTION, INFRARED SPECTROSCOPY, UPPER

ATMOSPHERE

152
46 GEOPHYSICS

N80-28965"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala. Space Sciences

Lab., Science and Engineering.

NASA/MSFC FY-80 ATMOSPHERIC PROCESSES RESEARCH

REVIEW

R. E. TURNER, comp. Jun. 1980 167 p refs Review held

at Huntsville, Ala., 3-5 Jun. 1980

(NASA-CP-2145) Avail: NTIS HC A08/MF A01 CSCL 04A

ATMOSPHERIC ELECTRICITY, CONFERENCES, NASA

PROGRAMS, OPTICAL RADAR, STORMS (METEOROLOGY),

UPPER ATMOSPHERE

N80-33998"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ATMOSPHERIC SOLAR ABSORPTION MEASUREMENTS IN THE

9 TO 11 MU M REGION USING A DIODE LASER HETERODYNE

SPECTROMETER

C. N. HARWARD and J. M HOELL, JR. Oct. 1980 14 p refs

Presented at Heterodyne Systems and Technol. Conf.,

Williamsburg, Va., 25-27 Mar. 1980

(NASA-TP-1726; L-13877) Avail: NTIS HC A02/MF A01

CSCL 04A

ATMOSPHERIC ATTENUATION, DIODES, HETERODYNING,

INFRARED TRACKING, LASER SPECTROSCOPY,

SPECTRORADIOMETERS, TUNING

N81-23742"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

REPORT OF THE NASA WORKING GROUP ON TROPOSPHERIC

PROGRAM PLANNING Final Report

J. H. SEINFELD, F. ALLARIO, W. R. BANDEEN, W. L. CHAMEIDES,

D. D. DAVIS, E. D. HINKLEY, and R. W. STEWART Apr. 1981

162 p refs

(NASA-RP-1062; L-13855) Avail: NTIS HC A08/MF A01

CSCL 04A

Increased understanding of the chemical phenomena occurring

in the troposphere was the research goal. Emphasis was placed

on tropospheric impact on environmental quality, including public

health, agriculture, climate, and weather. S.F.

N82-10624"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

OZONE TREND DETECTABILITY

J. W. CAMPBELL, ed. Jul. 1981 108 p refs Proc. of Symp.

held at Boulder, Colo., 28-29 Jul. 1977

(NASA-CP-2189; L-14654) Avail: NTIS HC A06/MF A01

CSCL 04A

CLIMATOLOGY, CONFERENCES, ERROR ANALYSIS, ERROR

FUNCTIONS, OZONOSPHERE, PERIODIC VARIATIONS,

TRENDS

N82-13592"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SAM 2 MEASUREMENTS OF THE POLAR STRATOSPHERIC

AEROSOL, VOLUME 1: OCTOBER TO APRIL 1979

M. P. MCCORMICK Dec. 1981 78 p refs

(NASA-RP-1081) Avail: NTIS HC A05/MF A01 CSCL 04A

Weekly averages of Antarctic and Arctic stratospheric aerosol

data as well as corresponding temperature profiles for the time

and place of each stratospheric aerosol measurement (SAM) II

measurement during the first 6 months of satellite flight are

presented. From the aerosol extinction profile data, contours of

aerosol extinction as a function of altitude and longitude or time

are plotted. Aerosol optical depths are calculated for each week.

Polar stratospheric clouds at altitudes of about 22 km were

observed during the Arctic winter at various times and locations.

A representative sample of the first 6 months of data to be used

in atmospheric and climatic studies is outlined. E.A.K.

N82-19734"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SAM 2 MEASUREMENTS OF THE POLAR STRATOSPHERIC

AEROSOL, VOLUME 2. APRIL 1979 TO OCTOBER 1979

M. P. MCCORMICK, H. M. STEELE (Systems and Applied Sciences

Corp., Hampton, Va.), and P. HAMILL (Systems and Applied

Sciences Corp., Hampton, Va.) Mar. 1982 78 p refs

(NASA-RP-1088-VOL-2; L-15120) Avail: NTIS HC A05/MF A01

CSCL 04A

The Stratospheric Aerosol Measurement (SAM) II sensor is

abroad the Earth orbiting Nimbus 7 spacecraft proving extinction

measurements of the Antarctic and Arctic stratospheric aerosol

with a vertical resolution of 1 km. Representative examples and

weekly averages of aerosol data and corresponding temperature

profiles for the time and place of each SAM II measurement (April

29, 1979, to October 27, 1979) is presented. Contours of aerosol

extinction as a function of altitude and longitude or time were

plotted and weekly aerosol optical depths were calculated.

Seasonal variations and variations in space (altitude and longitude)

for both polar regions are easily seen. Typical values of aerosol

extinction at the SAM II wavelength of 1.0 micron for the time

priod were 1 to 3 x 10 to the -4th power km -1 in the main

stratospheric aerosol layer. Optical depths for the stratosphere

were about 0.002. Polar stratospheric clouds at altitudes between

the tropopause and 20 km were observed during the Antarctic

winter at various times and locations. A ready-to-use format

containing a representative sample of the second 6 months of

data to be used in atmospheric and climatic studies is presented.

MD.K.

N82-12687"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SAGE MEASUREMENTS OF THE STRATOSPHERIC AEROSOL

DISPERSION AND LOADING FROM THE SOUFRIERE

VOLCANO

M. P. MCCORMICK, G. S. KENT (Institute for Atmospheric Optics

and Remote Sensing Hampton, Va.), G. K. YUE (Institute for

Atmospheric Optics and Remote Sensing Hampton, Va.), and D.

M CUNNOLD (Georgia Inst. of Techn., Atlanta) Nov. 1981 23

p refs

(NASA-TP-1922; L-14611) Avail: NTIS HC A02/MF A01

CSCL 04A

AEROSOLS, CARIBBEAN SEA, REMOTE SENSING, SAGE

SATELLITE, SHOCK WAVES, STRATOSPHERE, VIRGIN

ISLANDS, VOLCANOES

N82-29796"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

APPLYING MODELING RESULTS IN DESIGNING A GLOBAL

TROPOSPHERIC EXPERIMENT

Jul. 1982 95 p refs Presented at a Working Group Meeting,

Virginia Beach, Va., 15-16 Jul. 1981

(NASA-CP-2235; L-15383; NAS 1.55:2235) Avail: NTIS HC

A05/MF A01 CSCL 04A

AIR QUALITY, ATMOSPHERIC COMPOSITION, EARTH

OBSERVATIONS (FROM SPACE), TROPOSPHERE

153
46 GEOPHYSICS

N82-32915"# Massachusetts Inst. of Tech., Cambridge. Dept.

of Meteorology and Physical Oceanography.

REPORT OF WORKSHOP ON MOUNT SAINT HELENS: ITS

ATMOSPHERIC EFFECTS AND POTENTIAL CLIMATIC

IMPACT

R. E. NEWELL, ed. and A. DEEPAK, ed. (Inst. for Atmospheric

Optics and Remote Sensing) 1982 141 p refs Workshop

held in Washington, D.C., 20-21 Nov. 1980; sponsored by Inst. for

Atmospheric Optics and Remote Sensing Original contains color

illustrations

(NAS1-16454)

(NASA-SP-458; NAS 1.26:458; LC-82-8005) Avail: NTIS MF

A01; SOD HC $6.00 CSCL 08K

The atmospheric and potential climatic aspects of a volcanic

eruption were discussed. Measurements and techniques used in

collecting the data are summarized. SL

N82-33918"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

A TUTORIAL SOLUTION TO SCATTERING OF RADIATION IN

A THIN ATMOSPHERE BOUNDED BELOW BY A DIFFUSELY

REFLECTING, ABSORBING SURFACE

J. J, BUGLIA Sep. 1982 29 p refs

(NASA-TP.2077; L-15432; NAS 1.60:2077) Avail: NTIS HC

A03/MF A01 CSCL 04A

ALBEDO, ATMOSPHERIC SCATTERING, OPTICAL

REFLECTION, RADIATIVE TRANSFER, SURFACE PROPERTIES

N83-16992*# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

OZONE CLIMATOLOGY SERIES. VOLUME 1: ATLAS OF

TOTAL OZONE, APRIL 1970 - DECEMBER 1976

D. F. HEATH, A. J. FLEIG, A. J. MILLER, T. G. ROGERS, R. M.

NAGATANI, H. D. BOWMAN, II, V. G. KAVEESHWAR, K. F. KLENK,

P. K. BHARTIA, and K. D. LEE Dec. 1982 180 p refs

Prepared in cooperation with National Oceanic and Atmospheric

Administration, Washington D. C. and Systems and Applied

Sciences Corp., Riverdale, MD.

(NASA-RP-1098; NAS 1.61:1098; REPT-82F0128-VOL-1) Avail:

NTIS HC A09/MF A01 CSCL 04A

Contours and gridded values are given for seven years of

monthly mean total ozone data derived from observations with

the Backscattered Ultraviolet instrument on Nimbus-4 for the

Northern and Southern Hemispheres. The instrument, algorithm,

uncertainties in derived ozone and systematic changes in the bias

with respect to the international groundbased ozone network of

Dobson instruments, are discussed. Author

N83-27520"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SAM 2 MEASUREMENTS OF THE POLAR STRATOSPHERIC

AEROSOL. VOLUME 3: OCTOBER 1979 TO APRIL 1980

M. P. MCCORMICK and D. BRANDL (Systems and Applied

Sciences Corp., Hampton, Va.) Jun. 1983 77 p refs

(NASA-RP-1106; L-15624; NAS 1.61:1106) Avail: NTIS HC

A05/MF A01 CSCL 04A

The Stratospheric Aerosol Measurement (SAM) II sensor is

aboard the Earth-orbiting Nimbus 7 spacecraft providing extinction

measurements of the Antarctic and Arctic stratospheric aerosol

with a vertical resolution of 1 km. Representative examples and

weekly averages of aerosol data and corresponding temperature

profiles for the time and place of each SAM II measurement (Oct.

1979 through Apr. 1980) are presented. Contours of aerosol

extinction as a function of altitude and longitude or time are plotted

and weekly aerosol optical depths are calculated. Seasonal

variations and variations in space (altitude and longitude) for both

polar regions are easily seen. Typical values of aerosol extinction

at the SAM II wavelength of 1.0 microns for this time period are

2 to 4 times .0001/km in the main stratospheric aerosol layer.

Optical depths for the stratosphere are about 0.002 to 0.003, up

slightly over normal background levels (due to the eruption of

Sierra Negra, Nov. 1979). Polar stratospheric clouds at altitudes

of about 22 km were observed during the Arctic winter. A

154

ready-to-use format containing a representative sample of the third

6 months of data to be used in atmospheric and climatic studies

is presented. Author

N83-28796"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SAM 2 MEASUREMENTS OF THE POLAR STRATOSPHERIC

AEROSOL. VOLUME 4: APRIL 1980 TO OCTOBER 1980

M. P. MCCORMICK and D. BRANDL (Systems and Applied

Sciences Corp., Hampton, Va.) Jun. 1983 78 p refs 4 Vol.

(NASA-RP-1107; L-15625; NAS 1.61:1107) Avail: NTIS HC

AO5/MF A01 CSCL 04A

The Stratospheric Aerosol Measurement (SAM) 2 sensor is

aboard the Nimbus 7 spacecraft providing extinction measurements

of the Antarctic and Arctic stratospheric aerosols with a vertical

resolution of t kin. Representative examples and weekly averages

of these aerosol data and corresponding temperature profiles are

presented. Contours of aerosols extinction as a function of altitude

and longitude or time are plotted and weekly aerosol optical depths

are calculated. Stratospheric optical depths are 0.002 to 0.003 for

the Antarctic and 0.002 to 0.003 at the beginning to 0.005 to

0.006 at the end of the time period for the Arctic. Polar stratospheric

clouds at altitudes between the tropopause and 20 km were

observed during the Antarctic winter. A ready-to-use format

containing a representative sample of the fourth 6 months of data

to be used in atmospheric and climatic studies is reported.

Author

N84-10675"# National Aeronautics and Space Administration,

Washington, D.C.

THE NASA GEODYNAMICS PROGRAM: AN OVERVIEW

Jan 1983 132 p refs

(NASA-TP-2147; NAS 1.60:2147) Avail: NTIS HC A07/MF A01

CSCL 08G

EARTH ROTATION, GEODYNAMICS, NASA PROGRAMS,

TECTONICS

N84-13706"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

PROCEEDINGS OF A WORKSHOP ON ASSESSMENT OF

TECHNIQUES FOR MEASURING TROPOSPHERIC N SUB X O

SUB Y

Dec. 1983 63 p refs Workshop held in Palo Alto, Calif.,

16-20 Aug. 1982

(NASA-CP-2292; L-15720; NAS 1.55:2292) Avail: NTIS HC

A04/MF A01 CSCL 04A

ATMOSPHERIC CHEMISTRY, NITRIC OXIDE,

TROPOSPHERE

N84-14606"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

SPACE SHUTTLE EXHAUST CLOUD PROPERTIES

B. J. ANDERSON and V. W. KELLER Dec. 1983 117 p refs

(NASA-TP-2258; NAS 1.60:2258) Avail: NTIS HC A06/MF A01

CSCL 04A

CLOUDS, ROCKET EXHAUST, SPACE SHUTTLES

N84-32952"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

PROCEEDINGS OF A WORKSHOP ON POLAR

STRATOSPHERIC CLOUDS: THEIR ROLE IN ATMOSPHERIC

PROCESSES

P. HAMILL, ed. (San Jose State Univ., Calif,) and L. R. MCMASTER,

ed. Sep. 1984 80 p refs Proc. held in Virginia Beach, Va.,

20-22 Jun. 1983

(NASA-Cpo2318; L-15809; NAS 1.55:2318) Avail: NTIS HC

A05/MF A01 CSCL 04A

ATMOSPHERIC CHEMISTRY, ATMOSPHERIC RADIATION,

CONFERENCES, POLAR METEOROLOGY, STRATOSPHERE
N85-14336"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ASSESSMENT OF TECHNIQUES FOR MEASURING

TROPOSPHERIC H SUB X O SUB Y

J. M. HOELL, ed. Washington Dec. 1984 139 p refs

Workshop held in Palo Alto, Calif., 16-20 Aug. 1982

(NASA-CP-2332; L-15847; NAS 1.55:2332) Avail: NTIS HC

A07/MF A01 CSCL 04A

ATMOSPHERIC CHEMISTRY, CONFERENCES, MEASURING

INSTRUMENTS, RADIOCHEMISTRY, TROPOSPHERE

N85-19550"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AIRBORNE LIDAR MEASUREMENTS OF EL CHICHON

STRATOSPHERIC AEROSOLS, OCTOBER 1982 TO NOVEMBER

1982

M. P. MCCORMICK and M. T. OSBORN (Systems and Applied

Sciences Corp.) Feb. 1985 120 p refs

(NASA-RP-1136; L-15904; NAS 1.61:1136) Avail: NTIS HC

A06/MF A01 CSCL 04A

A coordinated flight mission to determine the spatial distribution

and aerosol characteristics of the El Chichon produced

stratospheric aerosol was flown in October to November 1982.

The mission covered 46 deg N to 46 deg S and included rendezvous

between balloon-, airplane-, and satellite-borne sensors. The lidar

data from the flight mission are presented. Representative profiles

of lidar backscatter ratio, plots of the integrated backscattering

function versus latitude, and contours of backscatter mixing ratio

versus altitude and latitude are given. In addition, tables containing

numerical values of the backscatter ratio and backscattering

functions versus altitude are supplied for each profile. The bulk of

the material produced by the El Chichon eruptions of late March

10 to early April 1982 resided between latitudes from 5 to 7 deg

S to 35 to 37 deg N and was concentrated above 21 km in a

layer that peaked at 23 to 25 km. In this latitude region, peak

scattering ratios at a wavelength of 0.6943 micron were

approximately 24. The results of this mission are presented in a

ready-to-use format for atmospheric and climatic studies. Author

N85-25970"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SAM 2 MEASUREMENTS OF THE POLAR STRATOSPHERIC

AEROSOL, VOLUME 5 Report, Oct. 1980 - Apr. 1981

M. P. MCCORMICK and D. BRANDL (Systems and Applied

Sciences Corp., Hampton, Va.) May 1985 78 p refs

(NASA-RP-1140; L-15947; NAS 1.61:1140) Avail: NTIS HC

A05/MF A01 CSCL 04A

The Stratospheric Aerosol Measurement (SAM) 2 sensor is

aboard the Earth-orbiting Nimbus 7 spacecraft providing extinction

measurements of the Antarctic and Arctic stratospheric aerosol

with a vertical resolution of 1 km. Representative examples and

weekly averages of aerosol data and corresponding temperature

profiles for the time and place of each SAM 2 mesurement (Oct.

1980 through Apr. 1981) are presented. Contours of aerosol

extinction as a function of altitude and longitude or time are plotted

and weekly aerosol optical depths are calculated. Seasonal

variations and variations in space (altitude and longitude) for both

polar regions are easily seen. Stratospheric optical depths are

0.002 to 0.003 for the Antarctic region and 0.005 to 0.006 at the

beginning to 0.002 to 0.003 at the end of the time period for the

Arctic region. The Northern Hemisphere values are quite large

due mainly to the eruption of Mount St. Helens (46.2 deg N,

122.2 deg W) in May 1980. Polar stratospheric clouds at altitudes

of about 20 km were observed during the Arctic winter. A

ready-to-use format containing a representative sample of the fifth

6 months of data to be used in atmospheric and climatic studies

is presented. B.W.

46 GEOPHYSICS

N85-27422"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SAM II MEASUREMENTS OF THE POLAR STRATOSPHERIC

AEROSOL. VOLUME 6: APRIL TO OCTOBER 1981

M. P. MCCORMICK and D. BRANDL (Systems and Applied

Sciences Corp., Hampton, Va.) May 1985 78 p refs 6 Vol.

(NASA-RP-1141; L-15948; NAS 1.61:1141) Avail: NTIS HC

A05/MF A01 CSCL 04A

The Stratospheric Aerosol Measurement (SAM) II sensor is

aboard the Earth-orbiting Nimbus 7 spacecraft providing extinction

measurements of the Antarctic and Arctic stratospheric aerosols

with a vertical resolution of 1 km. Representative examples and

weekly averages of these aerosol data and corresponding

temperature profiles (Apr. 1981 to Oct. 1981) are presented.

Contours of aerosol extinction as a function of altitude and longitude

or time are plotted and weekly aerosol optical depths are calculated.

Stratospheric optical depths are 0.002 to 0.003 for the Antarctic

region and 0.006 to 0.007 at the beginning to 0.003 to 0.004 at

the end of the time period for the Arctic region. Polar stratospheric

clouds at altitudes between the tropopause and 20 km were

observed during the Antarctic winter. A ready-to-use format

containing a representative sample of the sixth 6 months of data

to be used in atmospheric and climatic studies is reported.

Author

N86-11700"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SAGE AEROSOL MEASUREMENTS. VOLUME 1: FEBRUARY

21, 1979 TO DECEMBER 31, 1979

M. P. MCCORMICK Oct. 1985 371 p refs

(NASA-RP-1144; L-15962; NAS 1.61:1144) Avail: NTIS HC

A16/MF A01 CSCL 04A

The Stratospheric Aerosol and Gas Experiment (SAGE) satellite

system, launched on February 18, 1979, provides profiles of aerosol

extinction, ozone concentration, and nitrogen dioxide concentration

between about 80 N and 80 S. Zonal averages, separated into

sunrise and sunset events, and seasonal averages of the aerosol

extinction at 1.00 microns and 0.45 microns ratios of the aerosol

extinction to the molecular extinction at 1.00 microns, and ratios

of the aerosol extinction at 0.45 microns to the aerosol extinction

at 1.00 microns are given. The averages for 1979 are shown in

tables and in profile and contour plots (as a function of altitude

and latitude). In addition, temperature data provided by the National

Oceanic and Atmospheric Administration (NOAA) for the time and

location of each SAGE measurement are averaged and shown in

a similar format. Typical values of the peak aerosol extinction

were 0.0001 to 0.0002 km at 1.00 microns depth values for the

1.00 microns channel varied between 0.001 and 0.002 over all

latitudes. Author

N86-12852"# National Aeronautics and Space Administration,

Washington, D.C.

GEOPOTENTIAL RESEARCH MISSION (GRM)

Oct. 1985 141 p refs Conf. held in College Park, Md., 29-31

Oct. 1984

(NASA-CP-2390; NAS 1.55:2390) Avail: NTIS HC A07/MF A01

CSCL 08E

ALTIMETERS, CONFERENCES, EARTH CRUST, GEODESY,

GEODYNAMICS, GEOPOTENTIAL, GEOPOTENTIAL RESEARCH

MISSION, GRAVITATIONAL FIELDS, MAGNETIC FIELDS,

TECTONICS

N86-13850"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AIRBORNE LIDAR MEASUREMENTS OF EL CHICHON

STRATOSPHERIC AEROSOLS

M. P. MCCORMICK and M. T. OSBORN (SASC Technologies,

Inc., Hampton, Va.) Oct. 1985 89 p refs

(NASA-RP-1148; L-16007; NAS 1.61:1148) Avail: NTIS HC

A05/MF A01 CSCL 04A

A NASA Electra airplane, outfitted with a lidar system, was

flown in January to February 1983 between the latitudes of 27

deg N and 76 deg N. One of the primary purposes of this mission

155
46 GEOPHYSICS

was to determine the spatial distribution and aerosol characteristics

of the El Chichon-produced stratospheric material. This report

presents the lidar data from that flight mission. Representative

profiles of lidar backscatter ratio, plots of the integrated

backscattering function versus latitude, and contours of backscatter

mixing ratio versus altitude and latitude are given. It addition, tables

containing numerical values of the backscatter ratio and

backscattering function versus altitude are supplied for each profile.

The largest amount of material produced by the El Chichon

eruptions of late March to early April 1982, which was measured

by this flight, resided between 35 deg N and 52 deg N. Peak

backscatter ratios at a wavelength of 0.6943 micro m decreased

from 8 to 10 at the lower latitudes to 3 at the higher latitudes.

Backscatter ratio profiles taken while crossing the polar vortex

show that the high-altitude material from El Chichon arrived at

the north polar region sometime after the winter polar vortex was

established. This report presents the results of this mission in a

ready-to-use format for atmospheric and climatic studies. Author

N86-22022"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

COMPARATIVE ACCURACY OF THE ALBEDO, TRANSMISSION

AND ABSORPTION FOR SELECTED RADIATIVE TRANSFER

APPROXIMATIONS

M. D. KING and HARSHVARDHAN Jan. 1986 47 p refs

(NAG5-309)

(NASA-RP-1160; REPT-86B0034; NAS 1.61:1160) Avail: NTIS

HC A03/MF A01 CSCL 04A

Illustrations of both the relative and absolute accuracy of eight

different radiative transfer approximations as a function of optical

thickness, solar zenith angle and single scattering albedo are given.

Computational results for the plane albedo, total transmission and

fractional absorption were obtained for plane-parallel atmospheres

composed of cloud particles. These computations, which were

obtained using the doubling method, are compared with comparable

results obtained using selected radiative transfer approximations.

Comparisons were made between asymptotic theory for thick layers

and the following widely used two stream approximations:

Coakley-Chylek's models 1 and 2, Meador-Weaver, Eddington,

delta-Eddington, PIFM and delta-discrete ordinates. Author

N86-23088"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SAGE AEROSOL MEASUREMENTS. VOLUME 2:1 JANUARY

- 31 DECEMBER 1980

M. P. MCCORMICK Jan. 1986 310 p refs 2 VoI.

(NASA-RP-1149; L-16028; NAS 1.61:1149) Avail: NTIS HC

A14/MF A01 CSCL 04A

The stratospheric Aerosol and Gas Experiment (SAGE) satellite

system, launched on February 18, 1979, provides profiles of aerosol

extinction at wavelengths of 1.00 and 0.45 micron, ozone

concentration, and nitrogen dioxide concentration. Data taken

during sunset events in the form of zonal averages and seasonal

averages of the aerosol extinction at 1.00 and 0.45 micron, ratios

of the aerosol extinction to the molecular extinction at 1.00 micron,

and ratios of the aerosol extinction at 0.45 micron to the aerosol

extinction at 1.00 micron are presented. The averages for 1980

are shown in tables and in profile and contour plots (as a function

of altitude and latitude). In addition, temperature data provided by

the National Oceanic and Atmospheric Administration (NOAA) for

the time and location of each SAGE measurement are averaged

and shown in a similar format. Author

N86-25900"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

COMPENDIUM OF METEOROLOGY SCIENTIFIC ISSUES OF

1950 STILL OUTSTANDING

W. W. VAUGHAN Apr. 1986 59 p refs

(NASA-RP-1167; NAS 1.61:1167) Avail: NTIS HC A04/MF A01

CSCL 04A

The Compendium of Meteorology was published in 1951 by

the American Meteorological Society. A review was made of the

Compendium of Meteorology to identify the studies and future

156

needs which the authors expressed in their papers. The needs as

seen by the authors are organized into sections and papers

following the format of the Compendium of Meteorology. In some

cases the needs they identified are as valid today as they were in

1951. In other cases one will easily be able to identify examples

where significant progress has been made. It is left to the individual

scientists and scientific program managers to assess whether

significant progress has been made over the past thirty-five years

on these outstanding scientific issues. Author

N86-25911"# National Aeronautics and Space Administration,

Washington, D.C.

PRESENT STATE OF KNOWLEDGE OF THE UPPER

ATMOSPHERE" AN ASSESSMENT REPORT; PROCESSES THAT

CONTROL OZONE AND OTHER CLIMATICALLY IMPORTANT

TRACE GASES

R. T. WATSON, M. A. GELLER (National Aeronautics and Space

Administration. Goddard Space Flight Center, Greenbelt, Md.), R.

S. STOLARSKI, and R. F. HAMPSON May 1986 149 p refs

Original doc. contains color illustrations

(NASA-RP-1162; NAS 1.61:1162) Avail: NTIS HC A07/MF A01

CSCL 04A

The state of knowledge of the upper atmosphere was assessed

as of January 1986. The physical, chemical, and radiative processes

which control the spatial and temporal distribution of ozone in the

atmosphere; the predicted magnitude of ozone perturbations and

climate changes for a variety of trace gas scenarios; and the

ozone and temperature data used to detect the presence or

absence of a long term trend were discussed. This assessment

report was written by a small group of NASA scientists, was peer

reviewed, and is based primarily on the comprehensive international

assessment document entitled Atmospheric Ozone 1985:

Assessment of Our Understanding of the Processes Controlling

Its Present Distribution and Change, to be published as the World

Meteorological Organization Global Ozone Research and

Monitoring Project Report No. 16. Author

N86-27835"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AIRBORNE LIDAR MEASUREMENTS OF EL CHICHON

STRATOSHPERIC AEROSOLS

M. P. MCCORMICK and M. T. OSBORN (SASC Technologies,

Inc., Hampton, Va.) Jul. 1982 49 p Supersedes NASA-RP-1136

NASA-RP-1148

(NASA-RP-1166; L-16107; NAS 1.61:1166) Avail: NTIS HC

A03/MF A01 CSCL 04A

A NASA Electra airplane outfitted with a lidar system was flown

in July 1982 between the latitudes of 42 deg. N and 12 deg. N.

The primary purpose of this mission was to determine the spatial

distribution and aerosol characteristics of the El Chichon-produced

stratospheric material. This report presents the lidar data from

that flight mission. Representative profiles of lidar backscatter ratio,

plots of the integrated backscattering function versus latitude, and

contours of backscatter mixing ratio versus altitude and latitude

are given. In addition, tables containing numerical values of the

backscatter ratio and backscattering functions versus altitude are

supplied for each profile. The largest amount of material produced

by the El Chichon eruptions of late March-early April 1982 which

was measured by this flight resided south of 30 deg. N and was

concentrated above 21 km in a layer that peaked at 24 to 27 kin.

In this latitude region, peak backscatter ratios at a wavelength of

0.6943 microns were approximately 50, and peak optical depths

were calculated to be 0.2. This report presents the results of this

mission in a ready-to-use format for atmospheric and climatic

studies. Author
N86-27839"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

INTRODUCTION TO THE THEORY OF ATMOSPHERIC

RADIATIVE TRANSFER

J. J. BUGLIA Jul. 1986 171 p

(NASA-RP-1156; L16068; NAS 1.61:1156) Avail: NTIS HC

A08/MF A01 CSCL 04A

The fundamental physical and mathematical principles

governing the transmission of radiation through the atmosphere

are presented, with emphasis on the scattering of visible and

near-IR radiation. The classical two-stream, thin-atmosphere, and

Eddington approximations, along with some of their offspring, are

developed in detail, along with the discrete ordinates method of

Chandrasekhar. The adding and doubling methods are discussed

from basic principles, and references for further reading are

suggested. Author

N86-28562"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SAM 2 MEASUREMENTS OF THE POLAR STRATOSPHERIC

AEROSOL, VOLUME 2 Report, Oct. 1981 - Apr. 1982

M P. MCCORMICK and D. BRANDL (SASC Technologies, Inc.,

Hampton, Va.) Aug. 1986 78 p

(NASA-RP-1164; L-16105; NAS 1.61:1164) Avail: NTIS HC

A05/MF A01 CSCL 04A

The Stratospheric Aerosol Measurement (SAM) 2 sensor aboard

Nimbus 7 is providing extinction measurements of Antarctic and

Arctic stratospheric aerosols with a vertical resolution of 1 km

Representative examples and weekly averages including

corresponding temperature profiles provided by NOAA for the time

and place of each SAM 2 measurement (Oct. 1981 - Apr. 1982)

are presented. Contours of aerosol extinction as a function of

altitude and longitude or time are plotted, and aerosol optical

depths are calculated for each week. Typical values of aerosol

extinction at 1.0 micron in the main lower stratospheric aerosol

layer for this time period are 2 to 4 times 10 to the -4 power/km.

for the Antarctic region and 0.5 to 1 times 10 to the -3 power/km.

for the Arctic region. Stratospheric optical depths are about 0.001

to 0.004 for the Antarctic region and 0.003 to 0.004 at the beginning

to about 0.006 at the end of the time period for the Arctic region.

Polar stratospheric clouds (PSC's) were observed during the Arctic

winter, as expected. This report provides, in a ready-to-use format,

a representative sample of the seventh semester of data to be

used in atmospheric and climatic studies. Author

N86-29425"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

EL NINO AND OUTGOING LONGWAVE RADIATION: AN ATLAS

OF NIMBUS-7 EARTH RADIATION BUDGET OBSERVATIONS

H. L. KYLE (Research and Data Systems, Inc., Lanham, Md.), P.

E. ARDANUY, and R. R. HUCEK Apr. 1986 184 p

(NAS5-27728)

(NASA-RP-1163; NAS 1.61:1163; REPT-85B0565) Avail: NTIS

HC A05/MF A01 CSCL 04A

Five years of broadband Earth Radiation Budget (ERB)

measurements taken by the Nimbus-7 ERB experiment have been

archived. This five year period included the 1982 to 1983 El

Nino/Southern Oscillation event, which reached its peak in January

1983 (near the beginning of the fifth data year). An outgoing

Iongwave radiation subset of the data, for the period June 1980

to October 1983, was processed to enhance spatial resolution.

This atlas contains the analyses of the resultant fields. In addition,

a set of anomaly maps, based on a definition of pre-EI Nino

climatology, is included. Together, these two sets of maps provide

the first broadband glimpse of the terrestrial outgoing Iongwave

radiation response to the El Nino event. Author

47 METEOROLOGY AND CLIMATOLOGY

N86-29428"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SAM 2 MEASUREMENTS OF THE POLAR STRATOSPHERIC

AEROSOL, VOLUME 8 Report, Apr. - Oct. 1982

M. P. MCCORMICK and D. BRANDL (Systems and Applied

Sciences Corp., Hampton, Va.) Aug. 1986 80 p

(NASA-RP-1165; L-16106; NAS 1.61:1165) Avail: NTIS HC

A05/MF A01 CSCL 04A

The Stratospheric Aerosol Measurement (SAM) 2 sensor aboard

Nimbus 7 is providing extinction measurements of Antarctic and

Arctic stratospheric aerosols with a vertical resolution of 1 kin.

Representative examples and weekly averages including

corresponding temperature profiles provided by NOAA for the time

and place of each SAM 2 measurement (Apr. 1982 - Oct. 1982)

are presented. Contours of aerosol extinction as a function of

altitude and longitude or time are plotted, and aerosol optical

depths are calculated for each week. Typical values of aerosol

extinction at 1.0 microns in the main stratospheric aerosol layer

are approximately 4 to 6 times .0001/km at the beginning to 1 to

2 times .001/km at the end of the time period for the Antarctic

region and approximately 1 to 3 times .001/km for the Arctic

region throughout the time period. Stratospheric optical depths

are about 0.002 to 0.009 for the Antarctic region and about 0.007

at the beginning to 0.024 at the end of the time period for the

Arctic region. Polar stratospheric clouds were observed during the

Antarctic winter, as expected. This report provides, in a ready-to-use

format, a representative sample of the eighth 6 months of data to

be used in atmospheric and climatic studies.

47

METEOROLOGY AND CLIMATOLOGY

Includes weather forecasting and modification.

N77-10755"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

THE 1976 STANDARD ATMOSPHERE ABOVE 86-KM ALTITUDE:

RECOMMENDATIONS OF TASK GROUP 2 TO COESA

R. A. MINZNER, ed. Washington 1976 77 p refs

(NASA-SP-398) Avail: NTIS HC $4.75 CSCL 04A

The development of an atmospheric model for altitudes above

86 kin. is described. Temperature and composition profiles are

given particular attention. D.M.L.

N77-19709" National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

SATELLITE-DERIVED GLOBAL OCEANIC RAINFALL ATLAS

(1973 AND 1974)

M. S. V. RAO, W. V. ABBOTT, III, and J. S. THEON 1976 336

p refs Original contains color illustrations

(NASA-SP-410; LC-76-600054) Avail: SOD HC as C/N

NAS1.21:410 CSCL04B

Based on the relationship between satellite-borne electrically

scanning microwave radiometer brightness temperatures and rain

rates over oceans, quantitative maps of rainfall were obtained

from Nimbus-5 microwave data. Weekly, monthly, seasonally, and

annually averaged maps were generated from December 1972

through February 1975. From these maps, the patterns of rainfall

in the Pacific, Atlantic, and Indian Oceans were analyzed. It was

shown that the data permit the monitoring of features such as the

movement of the Intertropical Convergence Zone and the advance

of the Indian Monsoon. An interesting rainfall pattern in the Pacific,

associated with the El Nino phenomenon, was interpreted in terms

of a local variation of the Hadley cell circulation. The variations in

oceanic rainfall and in latent heat release (which was also

computed) should provide useful inputs to numerical models and

to studies of planetary energy and water budgets. Author

157
47 METEOROLOGYANDCLIMATOLOGY

N77-30705"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

FRONTS AND FRONTOGENESlS AS REVEALED BY HIGH TIME

RESOLUTION DATA

A. E. FRANK (Oregon State Univ.) and D. A. BARBER (Oregon

State Univ.) Aug. 1977 135 p refs

(NASA-RP-1005; M-226) Avail: NTIS HC A07/MF A01 CSCL

04B

Upper air sounding are used to examine a cold front of average

intensity. Vertical cross sections of potential temperature and wind,

and horizontal analyses were compared and adjusted for

consistency. These analyses were then used to study the evolution

of the front, found to consist of a complex system of fronts occurring

at all levels of the troposphere. Low level fronts were strongest

at the surface and rapidly weakened with height. Fronts in the

midddle troposphere were much more intense. The warm air ahead

of the fronts was nearly barotropic, while the cold air behind was

baroclinic through deep layers. A deep mixed layer was observed

to grow in this cotd air. Author

N77-32688"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

THE NASA AMES RESEARCH CENTER ONE- AND

TWO-DIMENSIONAL STRATOSPHERIC MODELS. PART 1: THE

ONE-DIMENSIONAL MODEL

R. P. TURCO (R and D Assoc., Marina Del Rey, Calif.) and R. C.

WHITTEN Sep. 1977 32 p refs

(NASA-TP-1002; A-6983) Avail: NTIS HC A03/MF A01 CSCL

04B

ATMOSPHERIC CHEMISTRY, ATMOSPHERIC MODELS,

DIFFERENTIAL EQUATIONS, STRATOSPHERE

N77-32689"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

THE NASA AMES RESEARCH CENTER ONE- AND

TWO-DIMENSIONAL STRATOSPHERIC MODELS. PART 2: THE

TWO-DIMENSIONAL MODEL

R. C. WHITTEN, W. J. BORUCKI, V. R. WATSON, T. SHIMAZAKI,

H. T. WOODWARD, C. A. RIEGEL (San Jose State Univ., Calif.),

L. A. CAPONE (San Jose State Univ., Calif.), and T. BECKER

(Informatics, Inc., Palo Alto, Calif.) Sep. 1977 23 p refs

(NASA-TP-1003; A-6982) Avail: NTIS HC A02/MF A01 CSCL

04B

ATMOSPHERIC CHEMISTRY, ATMOSPHERIC MODELS,

DIFFERENTIAL EQUATIONS, STRATOSPHERE, TRACE

ELEMENTS

N78-11642"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

DEVELOPMENT OF A PROCEDURE TO MODEL

HIGH-RESOLUTION WIND PROFILES FROM SMOOTHED OR

LOW-FREQUENCY DATA

D. W. CAMP Washington Nov. 1977 92 p refs

(NASA-TP-1071; M-239) Avail: NTIS HC A05/MF A01 CSCL

04B

HIGH RESOLUTION, MODELS, RAWINSONDES, WIND

PROFILES

N78-15641"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

THE MECHANICS OF ATMOSPHERIC SYSTEMS DERIVED

THROUGH VERTICAL AND HORIZONTAL ANALYSIS OF

PARAMETRIC DATA

R. E. TURNER Nov. 1977 187 p refs Original contains

color illustrations

(NASA-TP-1072; M-237) Avail: NTIS HC E06/MF A01 CSCL

04B

ATMOSPHERICS, INDEPENDENT VARIABLES

158

N78-18630"# National Meteorological Center, Washington, D.C.

STRATOSPHERIC WARMINGS: SYNOPTIC, DYNAMIC AND

GENERAL-CIRCULATION ASPECTS

R. M. MCINTURFF, ed. Jan. 1978 173 p refs Sponsored

by NASA

(NASA-RP-1017) Avail: NTIS HC A08/MF A01 CSCL 04B

Synoptic descriptions consist largely of case studies, which

involve a distinction between major and minor warmings. Results

of energetics studies show the importance of

tropospheric-stratospheric interaction, and the significance of the

pressure-work term near the tropopause. Theoretical studies have

suggested the role of wave-zonal flow interaction as well as

nonlinear interaction between eddies, chemical and photochemical

reactions, boundary forcing, and other factors. Numerical models

have been based on such considerations, and these are discussed

under various categories. Some indication is given as to why some

of the models have been more successful than others in simulating

warnings. The question of ozone and its role in warmings is briefly

discussed. Finally, a broad view is taken of stratospheric warmings

in relation to man's activities. Author

N78-19711"# Tennessee Univ. Space Inst., Tullahoma.

PROCEEDINGS OF THE FIRST ANNUAL METEOROLOGICAL

AND ENVIRONMENTAL INPUTS TO AVIATION SYSTEMS

WORKSHOP

D. W. CAMP, ed. and W. FROST, ed. Mar. 1977 335 p refs

Workshop held at Tullahoma, Tenn., 6-10 Mar. 1977; sponsored

by NASA, NOAA, and FAA

(NAS8-29584)

(NASA-CP-2028; FAA-RD-77-173) Avail: NTIS HC A15/MF A01

CSCL 04B

AERONAUTICS, AIRCRAFT DESIGN, MAN ENVIRONMENT

INTERACTIONS, REPORTS, SERVICES, SIMULATION

N78-23679"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SIMULATION STUDIES OF WIDE AND MEDIUM FIELD OF VIEW

EARTH RADIATION DATA ANALYSIS

R. N. GREEN May 1978 46 p refs

(NASA-TP-1182; L-12003) Avail: NTIS HC A03/MF A01

CSCL 04B

COMPUTERIZED SIMULATION, DATA PROCESSING,

RADIATION DISTRIBUTION, TERRESTRIAL RADIATION

N78-27706"# National Aeronautics and Space Administration.

Wallops Flight Center, Wallops Island, Va.

AN EVALUATION OF IN SlTU OZONE SENSOR PERFORMANCE

DURING A COLD FRONTAL PASSAGE

C. L. PARSONS Jul. 1978 34 p refs

(NASA-TP-1239) Avail: NTIS HC A03/MF A01 CSCL 04B

ATMOSPHERIC COMPOSITION, CLIMATOLOGY, OZONE

N78-28748"# National Weather Service, Camp Springs, Md.

SYNOPTIC ANALYSES, 5-, 2-, AND 0.4-MILLIBAR SURFACES

FOR JULY 1974 THROUGH JUNE 1976

Jun. 1978 330 p refs

(NASA ORDER P-55946-G)

(NASA-RP-1023) Avail: NTIS HC A15/MF A01 CSCL 04B

Meteorological rocketsonde and satellite radiance data were

employed for analyses of a continuing series of high altitude

constant pressure charts. The methods of processing, the various

types of data utilized and the analysis procedure are described.

Broad-scale analyses of temperature and geopotential height for

the Northern Hemisphere 5, 2, and 0.4 mb surfaces are presented

for each week of the period July 1974 through June 1976. Brief

discussions of the variations of the temperature and height fields

throughout the two year period are also given. G.Y.
N78-30774"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

AN ASSESSMENT OF THE EFFECT OF SUPERSONIC

AIRCRAFT OPERATIONS ON THE STRATOSPHERIC OZONE

CONTENT

t. G. POPPOFF, R. C. WHITTEN, R. P. TURCO (R and D Associates,

Marina del Rey, Calif.), and L. A. CAPONE (San Jose State Univ.,

Calif.) Aug. 1978 60 p refs

(NASA-RP-1026; A-7399) Avail: NTIS HC A04/MF A01 CSCL

13B

An assessment of the potential effect on stratospheric ozone

of an advanced supersonic transport operations is presented. This

assessment, which was undertaken because of NASA's desire for

an up-to-date evaluation to guide programs for the development

of supersonic technology and improved aircraft engine designs,

uses the most recent chemical reaction rate data. From the results

of the present assessment it would appear that realistic fleet sizes

should not cause concern with regard to the depletion of the total

ozone overburden. For example, the NOx emission of one type

designed to cruise at 20 km altitude will cause the ozone

overburden to increase by 0.03% to 0.12%, depending upon which

vertical transport is used. These ozone changes can be compared

with the predictions of a 1.74% ozone decrease (for 100 Large

SST's flying at 20 km) made in 1974 by the FAA's Climatic Impact

Assessment Program. Author

N78-32641"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

THE EFFECTS OF CURVATURE AND VISCOSITY ON

BAROCLINIC INSTABILITY: A TWO-LAYER MODEL

W. W. FOWLIS and S. ARIAS Sep. 1978 31 p refs

(NASA-TP-1328; M-264) Avail: NTIS HC A03/MF A01 CSCL

04B

BAROCLINITY, CURVATURE, FLUID FLOW, VISCOUS FLOW

N79-13644"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

PARAMETER ESTIMATION APPLIED TO NIMBUS 6

WIDE-ANGLE LONGWAVE RADIATION MEASUREMENTS

R. N. GREEN and G. L. SMITH Dec. 1978 40 p refs

(NASA-TP-1307; L-12233) Avail: NTIS HC A03/MF A0t

CSCL 04B

LONG WAVE RADIATION, NIMBUS 6 SATELLITE,

PARAMETERIZATION, RADIATION MEASUREMENT, SPHERICAL

HARMONICS

N79-14678"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

SUMMARY OF ATMOSPHERIC WIND DESIGN CRITERIA FOR

WIND ENERGY CONVERSION SYSTEM DEVELOPMENT

W. FROST (Tennessee Univ. Space Inst., Tullahoma) and R. E.

TURNER Jan. 1979 54 p

(NAS8-32118)

(NASA-TP-1389; M-280) Avail: NTIS HC A04/MF A01 CSCL

04B

ENERGY CONVERSION, ENERGY POLICY, WlNDPOWER

UTILIZATION

N79-14679"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

ENGINEERING HANDBOOK ON THE ATMOSPHERIC

ENVIRONMENTAL GUIDELINES FOR USE IN WIND TURBINE

GENERATOR DEVELOPMENT

W. FROST (Tennessee Univ. Space Inst., Tullahoma), B. H. LONG

(Tennessee Univ. Space Inst., Tullahoma), and R. E TURNER

Dec. 1978 379 p refs

(NASA-TP-1359; M-267) Avail: NTIS HC A17/MF A01 CSCL

04B

HANDBOOKS, MECHANICAL ENGINEERING, VALUE

ENGINEERING, WIND (METEOROLOGY), WlNDPOWERED

GENERATORS

47 METEOROLOGY AND CLIMATOLOGY

N79-14680"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

SEQUENTIAL HIGH-RESOLUTION WIND PROFILE

MEASUREMENTS

D. L. JOHNSON and W. W. VAUGHAN Dec. 1978 411 p

refs

(NASA-TP-1354) Avail: NTIS HC A18/MF A01 CSCL 04B

HIGH RESOLUTION, SEQUENTIAL ANALYSIS, WIND

MEASUREMENT, WIND PROFILES

N79-18493"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

A SIMPLIFIED METHOD FOR CALCULATING THE

ATMOSPHERIC HEATING RATE BY ABSORPTION OF SOLAR

RADIATION IN THE STRATOSPHERE AND MESOSPHERE

T. SHIMAZAKI and L. C. HELMLE (Informatics, Inc., Palo Alto,

Calif.) Jan. 1979 34 p refs

(NASA-TP-1398; A-7557) Avail: NTIS HC A04/MF A01 CSCL

04B

ATMOSPHERIC HEATING, NUMERICAL ANALYSIS,

RADIATION ABSORPTION, SOLAR RADIATION

N79-17413"# Tennessee Univ. Space Inst., Tullahoma.

PROCEEDINGS OF THE 2ND ANNUAL WORKSHOP ON

METEOROLOGICAL AND ENVIRONMENTAL INPUTS TO

AVIATION SYSTEMS

W. FROST, ed., D. W. CAMP, ed., and D. E. DURHAM, ed. Mar.

1978 259 p refs Workshop held at Tullahoma, Tenn., 28-30

Mar. 1978; sponsored in part by FAA and NOAA Prepared in

part by NASA. Marshall Space Flight Center

(NAS8-29584)

(NASA-CP-2057; FAA-RD-78-99) Avail: NTIS HC A12/MF A01

CSCL 04B

AIRCRAFT HAZARDS, CONFERENCES, FLIGHT SAFETY,

METEOROLOGY, RESEARCH, STORMS

N79-19569"# National Weather Service, Camp Springs, Md.

SYNOPTIC ANALYSES, 5-, 2-, 1-, AND 0.4-MILLIBAR SURFACES

FOR JULY 1976 THROUGH JUNE 1977

Dec. 1978 226 p refs

(NASA ORDER P-59946-G)

(NASA-RP-1032) Avail: NTIS HC A11/MF A01 CSCL 04B

Meteorological rocketsonde and satellite radiance data are

employed for analyses of a continuing series of high-altitude

constant-pressure charts. The automated methods of data

processing and the objective analysis procedures are described.

Broad-scale analyses of temperature and geopotential height for

the Northern Hemisphere 5-, 2-, 1-, and 0.4-mb surfaces are

presented for each week of the period July 1976 through June

1977. Brief discussions of the variations of the temperature and

height fields throughout the period are also given. Author

N79-20575"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

THIRD NATIONAL AERONAUTICS AND SPACE

ADMINISTRATION WEATHER AND CLIMATE PROGRAM

SCIENCE REVIEW

E. R. KREINS, ed. 1977 304 p refs Proc. held at Greenbelt,

Md., 29-30 Nov. 1977

(NASA-CP-2029) Avail: NTIS HC A14/MF A01 CSCL 04B

CLIMATOLOGY, CONFERENCES, STORMS (METEOROLOGY), WEATHER FORECASTING

N79-20633"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

FOURTH NATIONAL AERONAUTICS AND SPACE

ADMINISTRATION WEATHER AND CLIMATE PROGRAM

SCIENCE REVIEW

E. R. KREINS, ed. 1979 396 p refs Proc. held at Greenbelt,

Md., 24-25 Jan. 1979

(NASA-CP-2076) Avail: NTIS HC A17/MF A01 CSCL 04B

CLIMATE, CONFERENCES, NASA PROGRAMS, WEATHER

159
47 METEOROLOGY AND CLIMATOLOGY

N79-21720"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

THE NASA-AMES RESEARCH CENTER STRATOSPHERIC

AEROSOL MODEL. 2. SENSITIVITY STUDIES AND

COMPARISON WITH OBSERVATORIES

O. B. TOON, R. P. TURCO (R and D Associates, Marina del Rey,

Calif.), P. HAMILL, C. S. KIANG (National Center for Atmospheric

Research), and R. C. WHITTEN Apr. 1979 70 p refs

(NASA-TP-1363; A-7551) Avail: NTIS HC A04/MF A01 CSCL

04A

AEROSOLS, ATMOSPHERIC MODELS, DATA CORRELATION,

STRATOSPHERE

N79-21721"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

THE NASA-AMES RESEARCH CENTER STRATOSPHERIC

AEROSOL MODEL. 1. PHYSICAL PROCESSES AND

COMPUTATIONAL ANALOGS

R. P. TURCO (R and D Associates, Marina del Rey, Calif.), P.

HAMILL, O. B. TOON, R. C. WHITTEN, and C. S. KIANG (National

Center for Atmospheric Research) Apr. 1979 100 p refs

(NASA-TP-1362; A-7532) Avail: NTIS HC A05/MF A01 CSCL

04A

AEROSOLS, ATMOSPHERIC MODELS, MATHEMATICAL

MODELS, STRATOSPHERE

N79-22708"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

RF RADIATION PRODUCED BY INTRACLOUD LIGHTNING

DISCHARGES

D. M. LEVINE, E. P. KRIDER, and C. D. WEIDMAN Apr. 1979

17 p refs

(NASA-TP-1454; G-7951-03) Avail: NTIS HC A02/MF A01

CSCL 04B

ELECTROMAGNETIC RADIATION, LIGHTNING, RADIO

FREQUENCY DISCHARGE

N79-22709"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ANALYSES OF EARTH RADIATION BUDGET DATA FROM

UNRESTRICTED BROADBAND RADIOMETERS ON THE ESSA

7 SATELLITE

W. L. WEAVER and F. B. HOUSE (Drexel Univ.) May 1979 56

p refs

(NASA-TP-1402; L-12587) Avail: NTIS HC A04/MF A01

CSCL 04B

ATMOSPHERIC HEAT BUDGET, EARTH ATMOSPHERE,

EARTH RADIATION BUDGET, ESSA 7 SATELLITE, INFRARED

RADIOMETERS

N79-31885"# Texas A&M Univ., College Station.

CONVECTIVE RAINFALL ESTIMATION FROM DIGITAL GOES-1

INFRARED DATA

G. L. SICKLER and A. H. THOMPSON Washington NASA

Sep. 1979 96 p refs

(NASA-RP-1034) Avail: NTIS HC A05/MF A01 CSCL O4B

An investigation was conducted to determine the feasibility of

developing and objective technique for estimating convective

rainfall from digital GOES-1 infrared data. The study area was a

240 km by 240 km box centered on College Station, Texas (Texas

A and M University). The Scofietd and Oliver (1977) rainfall

estimation scheme was adapted and used with the digital

geostationary satellite data. The concept of enhancement curves

with respect to rainfall approximation is discussed. Raingage rainfall

analyses and satellite-derived rainfall estimation analyses were

compared. The correlation for the station data pairs (observed

versus estimated rainfall amounts) for the convective portion of

the storm was 0.92. It was demonstrated that a fairly accurate

objective rainfall technique using digital geostationary infrared

satellite data is feasible. The rawinsonde and some synoptic data

that were used in this investigation came from NASA's Atmospheric

Variability Experiment, AVE 7. G.Y.

160

N79-32796"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

THE WAVE STRUCTURES OF THE EADY MODEL OF

BAROCLINIC INSTABILITY

J. M. HYUN and W. W. FOWLIS Washington Oct. 1979 26 p

refs

(NASA-TP-1548) Avail: NTIS HC A03/MF A01 CSCL 04B

ATMOSPHERIC MODELS, BAROCLINIC WAVES, FLOW

STABILITY, FLUID DYNAMICS, PROPAGATION MODES, WAVE

PROPAGATION

N79-32797"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EARTH RADIATION BUDGET SCIENCE, 1978

1978 79 p refs Workshop held at Williamsburg, Va., 28-30

Mar. 1978

(NASA-CP-2100) Avail: NTIS HC A05/MF A01 CSCL 04B

CLIMATOLOGY, CLOUD PHYSICS, CONFERENCES,

DYNAMIC MODELS, EARTH RADIATION BUDGET, ENERGY

BUDGETS, RADIATION MEASUREMENT, RADIATIVE HEAT

TRANSFER, SATELLITE OBSERVATION, TERRESTRIAL

RADIATION

N79-33722"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

SUMMARY OF THE NASA/MSFC FY-79 SEVERE STORM AND

LOCAL WEATHER RESEARCH REVIEW

Sep. 1979 92 p Presented at the NASA/MSFC FY-79 Severe

Storm and Local Weather Res. Rev., Huntsville, Ala. 12-13 Sep.

1979

(NASA-CP-2105) Avail: NTIS HC A06/MF A01 CSCL 04B

ATMOSPHERIC ELECTRICITY, CLOUD PHYSICS,

CONFERENCES, EARTH IONOSPHERE, NASA PROGRAMS,

STORMS, WEATHER

N80-12661"# National Aeronautics and Space Administration.

Wallops Flight Center, Wallops Island, Va.

WIND STUDY FOR HIGH ALTITUDE PLATFORM DESIGN

T. W. STRGANAC Washington Dec. 1979 288 p refs

(NASA-RP-1044) Avail: NTIS HC A13/MF A01 CSCL 04B

An analysis of upper air winds was performed to define the

wind environment at potential operating altitudes for high altitude

powered platform concepts. Wind conditions of the continental

United States, Pacific area (Alaska to Sea of Japan), and European

area (Norwegian and Mediterranean Sea) were obtained using a

representative network of sites selected based upon adequate

high altitude sampling, geographic dispersion, and observed upper

wind patterns. A data base of twenty plus years of rawinsonde

gathered wind information was used in the analysis. Annual

variations from surface to 10 mb pressure altitude were investigated

to encompass the practical operating range for the platform

concepts. Parametric analysis for the United States and foreign

areas was performed to provide a basis for vehicle system design

tradeoffs. This analysis of wind magnitudes indicates the feasibility

of annual operation at a majority of sites and more selective

seasonal operation for the extreme conditions between the

pressure altitudes of 100 to 25 mb based upon the assumed

design speeds. R.C.T.

N80-14633"# Tennessee Univ. Space Inst., Tullahoma.

PROCEEDINGS, THIRD ANNUAL WORKSHOP ON

METEOROLOGICAL AND ENVIRONMENTAL INPUTS TO

AVIATION SYSTEMS

D. W. CAMP, ed. and W. FROST, ed. Apr. 1979 190 p refs

Proc. held at Tullahoma, Tenn., 3-5 Apr. 1979; sponsored by NASA,

NOAA, and FAA

(NAS8-32692)

(NASA-CP-2104; FAA-RD-79-49) Avail: NTIS HC A09/MF A01

CSCL 04B

AIR TRAFFIC CONTROL, CONFERENCES, FLIGHT SAFETY,

METEOROLOGY
N80-14641"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

THE STRATOSPHERE: PRESENT AND FUTURE

R. D. HUDSON, ed. and E. I. REED, ed. Dec. 1979 443 p

refs

(NASA-RP-1049) Avail: NTIS HC A19/MF A01 CSCL 04B

The present status of stratospheric science is discussed. The

three basic elements of stratospheric science-laboratory

measurements, atmospheric observations, and theoretical studies

are presented along with an attempt to predict, with reasonable

confidence, the effect on ozone of particular anthropogenic sources

of pollution. For individual titles, see N80-14642 through

N80-14648.

N80-15726"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

STRATOSPHERIC AEROSOL MODIFICATION BY SUPERSONIC

TRANSPORT OPERATIONS WITH CLIMATE IMPLICATIONS

O. B. TOON, R. P. TURCO (R and D Assoc., Marina Del Rey,

Calif.), J. B. POLLACK, R. C. WHITTEN, I. G. POPPOFF, and P.

HAMILL (Systems and Applied Sciences Corp., Hampton, Va.) Jan.

1980 20p refs

(NASA-RP-1058; A-7938) Avail: NTIS HC A02/MF A01 CSCL

04B

The potential effects on stratospheric aerosols of supersonic

transport emissions of sulfur dioxide gas and submicron size soot

granules are estimated. An interactive particle-gas model of the

stratospheric aerosol is used to compute particle changes due to

exhaust emissions, and an accurate radiation transport model is

used to compute the attendant surface temperature changes. It is

shown that a fleet of several hundred supersonic aircraft, operating

daily at 20 km, could produce about a 20% increase in the

concentration of large particles in the stratosphere. Aerosol

increases of this magnitude would reduce the global surface

temperature by less than 0.01 K. Author

N80-16675"# National Aeronautics and Space Administration,

Marshall Space Flight Center, Huntsville, Ala.

THUNDERSTORM-ENVIRONMENT INTERACTIONS DETERMINED WITH THREE-DIMENSIONAL TRAJECTORIES

G. S. WILSON Washington Jan. 1980 163 p refs

(NASA-RP-1054) Avail: NTIS HC A08/MF A01 CSCL 04B

Diagnostically determined three dimensional trajectories were

used to reveal some of the scale interaction processes that occur

between convective storms and their environment. Data from

NASA's fourth Atmospheric Variability Experiment are analyzed.

Two intense squall lines and numerous reports of severe weather

occurred during the period. Convective storm systems with good

temporal and spatial continuity are shown to be related to the

development and movement of short wave circulation systems

aloft that propagate eastward within a zonal mid tropospheric wind

pattern. These short wave systems are found to produce the

potential instability and dynamic triggering needed for thunderstorm

formation. The environmental flow patterns, relative to convective

storm systems, are shown to produce large upward air parcel

movements in excess of 50 mb/3h in the immediate vicinity of

the storms. The air undergoing strong lifting originates as potentially

unstable low level air traveling into the storm environment from

southern and southwestern directions. The thermo and

hydrodynamical processes that lead to changes in atmospheric

structure before, during, and after convective storm formation are

described using total time derivatives of pressure or net vertical

displacement, potential temperature, and vector wind calculated

by following air parcels. R.C.T,

N80-16676"# National Aeronautics and Space Administration.

Wallops Flight Center, Wallops Island, Va.

THE ROLE OF SATELLITE ALTIMETRY IN CLIMATE STUDIES

C. L. PARSONS Washington Jan. 1980 32 p refs

(NASA-TP-1570) Avail: NTIS HC A03/MF A01 CSCL 04B

AIR WATER INTERACTIONS, ALTIMETERS, CLIMATOLOGY,

ICE MAPPING, MARINE METEOROLOGY, OCEANOGRAPHY,

POLAR CAPS, SEA ICE, SEASAT 1, SKYLAB PROGRAM

47 METEOROLOGY AND CLIMATOLOGY

N80-18682"# National Aeronautics and Space Administration.

Wallops Flight Center, Wallops Island, Va.

RESULTS OF THE AUGUST 1977 SOVIET AND AMERICAN

METEROLOGICAL ROCKETSONDE INTERCOMPARISON HELD

AT WALLOPS ISLAND, VIRGINIA

F. J. SCHMIDLIN, J. R. DUKE, A. I. IVANOVSKY, and Y. M

CHERNYSHENKO Feb. 1980 193 p refs Prepared in

cooperation with the Hydrometeorological Service of the USSR

(NASA-RP-1053) Avail: NTIS HC A09/MF A01 CSCL 04B

A coordinated program of rocketsonde investigations along

about 60 deg E and 70 deg W between the United States and

U.S.S.R. is discussed. The rocketsonde instruments used by the

U.S. and U.S.S.R. were compared and the results are presented.

The U.S. Super Loki Datasonde and the U.S.S.R. M100B

rocketsonde are discussed. Results indicate that the U.S/U.S.S.R

rocketsonde measurement agreement improved since the 1973

intercomparisons. It was learned that the mean of the differences

of the temperatures compare to within 6 C at about 60 km and to

within 2 C near 50 km. Wind measurements were also found to

agree. A.W.H.

N80-20986"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SIMULATION STUDY OF A GEOMETRIC SHAPE FACTOR

TECHNIQUE FOR ESTIMATING EARTH-EMITTED RADIANT

FLUX DENSITIES FROM WIDE-FIELD-OF-VIEW RADIATION

MEASUREMENTS

W. L. WEAVER and R. N. GREEN Washington Apr. 1980 29

p refs

(NASA-TP-1629; L-13373) Avail: NTIS HC A02/MF A01

CSCL 04B

EARTH SURFACE, RADIANT FLUX DENSITY, RADIATION

MEASUREMENT, RADIOMETERS

N80-21927"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

LIGHTNING TECHNOLOGY: PROCEEDINGS OF A TECHNICAL

SYMPOSIUM

Apr. 1980 444 p refs Symp. held in Hampton, Va., 22-24

Apr. 1980; sponsored in cooperation with Fla. Inst. of Technol.

and DOT

(NASA-CP-2128; L-13666; FAA-RD-80-30) Avail: NTIS HC

A19/MF A01 CSCL 04B

AIRCRAFT HAZARDS, CONFERENCES, ELECTROMAGNETIC

SHIELDING, LIGHTNING, MATHEMATICAL MODELS,

MEASURING INSTRUMENTS

N80-22924"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

THE STRATCOM 8 EFFORT

E. I. REED, ed. Apr. 1980 221 p refs

(NASA-TP-1640) Avail: NTIS HC A10/MF A01 CSCL 04B

NITROGEN OXIDES, OZONE, PHOTOCHEMICAL REACTIONS,

STRATOSPHERE, ULTRAVIOLET RADIATION

N80-23933"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

RATE STATISTICS FOR RADIO NOISE FROM LIGHTNING

D. M. LEVINE, R. MENEGHINI (Maryland Univ., College Park),

and S. A. TRETTER May 1980 34 p refs

(NASA-TP-1665; G80F5117) Avail: NTIS HC A03/MF A01

CSCL 04B

LIGHTNING, RADIO FREQUENCY INTERFERENCE,

STATISTICAL ANALYSIS

161
47 METEOROLOGY AND CLIMATOLOGY

N80-23934"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala. Space Sciences

Lab.

ICE CRYSTAL GROWTH IN A DYNAMIC THERMAL DIFFUSION

CHAMBER

V. W. KELLER May 1980 216 p refs

(NSF ATM-75-10935; NSF ATM-77-07995)

(NASA-TP-1651) Avail: NTIS HC A10/MF A01 CSCL 04B

CONTROLLED ATMOSPHERES, CRYSTAL GROWTH, ICE

FORMATION, NUCLEATION, TEST CHAMBERS, THERMAL

DIFFUSION

N80-26999"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

EXPLORATORY MEETING ON AIRBORNE DOPPLER LIDAR

WIND VELOCITY MEASUREMENTS

G. H. FICHTEL, ed., J. W. KAUFMAN, ed., and W. W. VAUGHAN,

ed. Apr. 1980 57 p refs Meeting held in Huntsville, Ala., 1

Apr. 1980

(NASA-CP-2140) Avail: NTIS HC A04/MF A01 CSCL 04B

AIRBORNE EQUIPMENT, CONFERENCES, LASER DOPPLER

VELOCIMETERS, OPTICAL RADAR, WIND VELOCITY

MEASUREMENT

N81-10637"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

FIRST SCIENTIFIC WORKING GROUP MEETING OF AIRBORNE

DOPPLER LIDAR WIND VELOCITY MEASUREMENT

PROGRAM

J. W. KAUFMAN, ed. Oct. 1980 135 p refs Meeting held in

Huntsville, Ala., 25-26 Aug. 1980

(NASA-CP-2161) Avail: NTIS HC A07/MF A01 CSCL 04B

CONFERENCES, DOPPLER RADAR, LASER APPLICATIONS,

METEOROLOGICAL FLIGHT, WIND MEASUREMENT

N81-13593"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

DECONVOLUTION AND ANALYSIS OF WIDE-ANGLE

LONGWAVE RADIATION DATA FROM NIMBUS 6 EARTH

RADIATION BUDGET EXPERIMENT FOR THE FIRST YEAR

T. D. BESS, R. N GREEN, and G. L. SMITH Dec. 1980 62 p

refs

(NASA-TP-1746; L-13873) Avail: NTIS HC A04/MF A01

CSCL 04B

DATA REDUCTION, EARTH RADIATION BUDGET, EARTH

RADIATION BUDGET EXPERIMENT, LONG WAVE RADIATION,

RESOLUTION, SPHERICAL HARMONICS

N81-14555"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

PROCEEDINGS: FOURTH ANNUAL WORKSHOP ON

METEOROLOGICAL AND ENVIRONMENTAL INPUTS TO

AVIATION SYSTEMS

W. FROST, ed. and D. W. CAMP, ed. Mar. 1980 287 p refs

Workshop held in Tullahoma, Tenn., 25-27 Mar. 1980; sponsored

in part by FAA and NOAA Prepared in cooperation with Tennessee

Univ. Space Inst.

(NAS8-32692)

(NASA-CP-2139; FAA-RD-80-67) Avail: NTIS HC A13/MF A01

CSCL 04B

AIR TRAFFIC CONTROL, AIRCRAFT SAFETY,

CONFERENCES, METEOROLOGICAL PARAMETERS

162

N81-15639"# Texas A&M Univ., College Station. Dept. of

Meteorology.

DETERMINATION OF WIND FROM NIMBUS 6 SATELLITE

SOUNDING DATA

W. E. CARLE and J. R. SCOGGINS Jan. 198t 83 p refs

Sponsored by NASA

(DAAG29-76-G-0078)

(NASA-RP-1072; M-329) Avail: NTIS HC A05/MF A01 CSCL

04B

Objective methods of computing upper level and surface wind

fields from NIMBUS 6 satellite sounding data are developed. These

methods are evaluated by comparing satellite derived and

rawinsonde wind fields on gridded constant pressure charts in

four geographical regions. Satellite-derived and hourly observed

surface wind fields are compared. Results indicate that the best

satellite-derived wind on constant pressure charts is a geostrophic

wind derived from highly smoothed fields of geopotential height.

Satellite-derived winds computed in this manner and rawinsonde

winds show similar circulation patterns except in areas of small

height gradients. Magnitudes of the standard deviation of the

differences between satellite derived and rawinsonde wind speeds

range from approximately 3 to 12 m/sec on constant pressure

charts and peak at the jet stream level. Fields of satellite-derived

surface wind computed with the logarithmic wind law agree well

with fields of observed surface wind in most regions. Magnitudes

of the standard deviation of the differences in surface wind speed

range from approximately 2 to 4 m/sec, and satellite derived

surface winds are able to depict flow across a cold front and

around a low pressure center. Author

N81-15640"# Texas A&M Univ., College Station. Dept. of

Meteorology.

A COMPARATIVE ANALYSIS OF RAWINSONDE AND NIMBUS

6 AND TIROS N SATELLITE PROFILE DATA

J. R. SCOGGINS, W. E. CARLE, K. KNIGHT, V. MOYER, and N.

M. CHENG Jan. 1981 84 p refs Sponsored by NASA

(DAAG29-76-G-0078)

(NASA-RP-1070; M-327) Avail: NTIS HC A05/MF A01 CSCL

04B

Comparisons are made between rawinsonde and satellite

profiles in seven areas for a wide range of surface and weather

conditions. Variables considered include temperature, dewpoint

temperature, thickness, precipitable water, lapse rate of

temperature, stability, geopotential height, mixing ratio, wind

direction, wind speed, and kinematic parameters, including vorticity

and the advection of vorticity and temperature. In addition,

comparisons are made in the form of cross sections and synoptic

fields for selected variables. Sounding data from the NIMBUS 6

and TIROS N satellites were used. Geostrophic wind computed

from smoothed geopotential heights provided large scale flow

patterns that agreed well with the rawinsonde wind fields. Surface

wind patterns as welt as magnitudes computed by use of the log

law to extrapolate wind to a height of 10 m agreed with

observations. Results of this study demonstrate rather conclusively

that satellite profile data can be used to determine characteristics

of large scale systems but that small scale features, such as

frontal zones, cannot yet be resolved. Author

N81-16678"# Texas A&M Univ., College Station. Dept. of

Meteorology.

ATMOSPHERIC STRUCTURE DETERMINED FROM SATELLITE

DATA

K. S. KNIGHT and J. R. SCOGGINS 1981 107 p refs

Sponsored in part by NASA

(DAAG29-76-G-0078)

(NASA-RP-1071; M-328) Avail: NTIS HC A06/MF A01 CSCL

04B

The capabilities of the Nimbus 6 satellite sounding data for

use in synoptic analysis were considered and interpreted. An

evaluation of the ability of the satellite sounding data to detect

and depict structural features of the atmosphere was made on

the basis of vertical profiles of average difference and standard

deviation of differences between satellite and rawinsonde data at
47 METEOROLOGY AND CLIMATOLOGY

nine pressure levels from 850 to 100 mb; and constant pressure

charts and cross sections of satellite, rawinsonde and difference

values. Results indicate that satellite measurements of temperature

as well as the vertical lapse rate and horizontal gradient of

temperature are accurate enough to show large scale patterns

but not to precisely define fronts or tropopauses; satellite

measurements of dew point temperature are smoothed enough to

severely reduce contrasts between air masses across fronts; the

magnitude of the standard deviation of differences between

rawinsonde and satellite data for most variables increases with

the synoptic activity in the region; and the most reliable variables

to examine from satellite data for depiction of synoptic features

are the temperature equivalent potential temperature and mixing

ratio. T.M.

N81-16679"# Texas A&M Univ., College Station. Dept. of

Meteorology.

COMPARISONS BETWEEN NIMBUS 6 SATELLITE AND

RAWlNSONDE SOUNDINGS FOR SEVERAL GEOGRAPHICAL

AREAS

N.M. CHENGandJ. R. SCOGGINS 1981 76p refs Sponsored

in part by NASA

(DAAG29-76-G-0078)

(NASA-RP-1073; M-330) Avail: NTIS HC A05/MF A01 CSCL

04B

Good agreement between satellite and weighted (linearly

interpolated) rawinsonde temperature and temperature derived

parameters was found in most instances with the poorest

agreement either near the tropopause region or near the ground.

However, satellite moisture data are highly questionable. The

smallest discrepancy between satellite and weighted mean

rawinsonde temperature and parameters derived from temperature

was found over water and the largest discrepancy was found

over mountains. Cumulative frequency distributions show that

discrepancies between satellite and rawinsonde data can be

represented by a normal distribution except for dew point

temperature. T. M

N81-21686"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

GODDARD LABORATORY FOR ATMOSPHERIC SCIENCE,

COLLECTED REPRINTS 1978-1979, VOLUME 1

W. C. SKILLMAN, ed. and E. R. KREINS, ed Mar. 1981 565 p

refs

(NASA-TP-1788-VOL-1) Avail: NTIS HC A24/MF A01 CSCL

04B

ATMOSPHERIC SOUNDING, EARTH ATMOSPHERE,

METEOROLOGY, NASA PROGRAMS, ROCKET SOUNDING,

SATELLITE SOUNDING, WEATHER

N81-21693"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

GODDARD LABORATORY FOR ATMOSPHERIC SCIENCES,

COLLECTED REPRINTS 1978 - 1979, VOLUME 2

W. C. SKILLMAN and E. R. KREINS Mar. 1981 521 p refs

2 VoI.

(NASA-TP-1788-VOL-2) Copyright Avail: NTIS HC A22/MF

A01 CSCL 04B

EARTH HYDROSPHERE, MICROWAVE SENSORS, NASA

PROGRAMS, OCEANOGRAPHY, SATELLITE SOUNDING

N81-22658"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

A COMPARATIVE STATISTICAL STUDY OF LONG-TERM

AGROCLIMATIC CONDITIONS AFFECTING THE GROWTH OF

US WINTER WHEAT: DISTRIBUTIONS OF REGIONAL

MONTHLY AVERAGE PRECIPITATION ON THE GREAT PLAINS

AND THE STATE OF MARYLAND AND THE EFFECT OF

AGROCLIMATIC CONDITIONS ON YIELD IN THE STATE OF

KANSAS

J. WELKER Apr. 1981 189 p refs

(NASA-TP-1724; REPT-80F5125) Avail: NTIS HC A09/MF A01

CSCL 04B

AGRICULTURE, AGROCLIMATOLOGY, ANNUAL VARIATIONS, CROP GROWTH, KANSAS, MARYLAND, PRECIPITATION (METEOROLOGY), WHEAT YIELD

N81-19709"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

VAS DEMONSTRATION SOUNDING WORKSHOP: THE

PROCEEDINGS OF A SATELLITE SOUNDING WORKSHOP

D. L, ENDRES, ed. and L. W. UCCELLINI, ed. 1980 83 p

refs Conf. held at Goddard Space Flight Center, Greenbelt, Md.,

15 Jul. 1980

(NASA-CP-2157) Avail: NTIS HC A05/MF A01 CSCL 04B

ATMOSPHERIC SOUNDING, CONFERENCES, SATELLITE

SOUNDING, SATELLITE-BORNE INSTRUMENTS, TIROS N

SATELLITE

N81-23761"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va,

ENERGETICS OF A SUDDEN STRATOSPHERIC WARMING

SIMULATED WITH A THREE-DIMENSIONAL, SPECTRAL,

QUASI-GEOSTROPHIC MODEL

K. V. HAGGARD and W. L. GROSE May 1981 30 p refs

(NASA-TP-1847; L-t4245) Avail: NTIS HC A03/MF A01

CSCL 04B

ATMOSPHERIC HEATING, ATMOSPHERIC MODELS,

ATMOSPHERIC PHYSICS, ATMOSPHERIC TEMPERATURE,

STRATOSPHERE

N81-21685"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

ANALYSIS OF ATMOSPHERIC OZONE LEVELS AT

COMMERCIAL AIRPLANE CRUISE ALTITUDES IN WINTER AND

SPRING, 1976 - 1977

J. D. HOLDEMAN and G. D. NASTROM (Control Data Corp.,

Minneapolis) Apr. 1981 18 p refs

(DOT-FA78WAI-893)

(NASA-TP-1807; FAA-EE-81-1; E-468) Avail: NTIS HC A02/MF

A01 CSCL 04B

AIR SAMPLING, AIRCRAFT COMPARTMENTS, CABIN

ATMOSPHERES, COMMERCIAL AIRCRAFT, GLOBAL AIR

SAMPLING PROGRAM, OZONOMETRY

N82-12715"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

THE NUMERICAL STUDIES PROGRAM FOR THE

ATMOSPHERIC GENERAL CIRCULATION EXPERIMENT (AGCE)

FOR SPACELAB FLIGHTS

W. W. FOWLIS, ed. and M. H. DAVIS, ed. (Univ. Space Research

Association, Boulder, Colo.) Nov. 1981 65 p refs Proc. of

Meeting held in Boulder, Colo., 14-15 Apr. 1981

(NASA-CP-2200; M-366) Avail: NTIS HC A04/MF A01 CSCL

04B

ATMOSPHERIC CIRCULATION, ATMOSPHERIC PHYSICS,

AXISYMMETRIC FLOW, BAROCLINtC WAVES, EARTH

ATMOSPHERE, FLOW GEOMETRY

163
47 METEOROLOGYANDCLIMATOLOGY

N82.13620°# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

COMPARISON OF DATA INVERSION TECHNIQUES FOR

REMOTELY SENSED WIDE-ANGLE OBSERVATIONS OF EARTH

EMITTED RADIATION

R. N. GREEN Dec. 1981 46 p refs

(NASA-TP-1924; L-14591) Avail: NTIS HC A03/MF A0t

CSCL 04B

CONVOLUTION INTEGRALS, DATA REDUCTION, ENERGY

BUDGETS, FIELD OF VIEW, RADIANT FLUX DENSITY,

TERRESTRIAL RADIATION

N82-15677"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

CLOUD-ENCOUNTER AND PARTICLE-CONCENTRATION

VARIABILITIES FROM GASP DATA

G. D. NASTROM (Control Data Corp., Minneapolis), J. D.

HOLDEMAN (NASA. Lewis Research Center, Cleveland), and R.

E. DAVIS Dec. 1981 245 p refs

(NASA-TP-1886; L-14483) Avail: NTIS HC AI1/MF A01

CSCL 04B

CLOUDS, GLOBAL AIR SAMPLING PROGRAM, ICE,

METEOROLOGICAL PARAMETERS, PARTICLE DENSITY

(CONCENTRATION), STATISTICAL ANALYSIS, VARIABILITY

N82-16660*# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

NASA/MSFC FY-81 ATMOSPHERIC PROCESSES RESEARCH

REVIEW

R. E. TURNER, comp. Dec. 1981 161 p refs Review held

in Huntsville, Ala., 1-3 Sep. 1981

(NASA-CP-2204; M-367) Avail: NTIS HC A08/MF A01 CSCL

04B

EARTH OBSERVATIONS (FROM SPACE), METEOROLOGICAL

PARAMETERS, PROGRAMS, STORMS (METEOROLOGY),

UPPER ATMOSPHERE, WEATHER

N82-24781"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

METEOROLOGICAL SATELLITES: PAST, PRESENT, AND

FUTURE

May 1982 61 p refs Proc. of the Session on Meteorol.

Satellites at the AIAA 20th Aerospace Sci. Meeting, Orlando, Fla.,

11-14 Jan. 1982

(NASA-CP-2227; NAS 1.55:2227) Avail: NTIS HC A04/MF A01

CSCL 04B

CONFERENCES, HISTORIES, METEOROLOGICAL

PARAMETERS, METEOROLOGICAL SATELLITES, SATELLITE

OBSERVATION

N82-24790"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

POWER SPECTRAL MEASUREMENTS OF CLEAR-AIR

TURBULENCE TO LONG WAVELENGTHS FOR ALTITUDES UP

TO 14,000 METERS

H. N. MURROW, W. E. MCCAIN, and R. H. RHYNE Apr. 1982

163 p refs

(NASA-TP-1979; L-14829; NAS 1.60:1979) Avail: NTIS HC

A08/MF A01 CSCL 04B

CLEAR AIR TURBULENCE, DATA ACQUISITION, JET

STREAMS (METEOROLOGY), POWER SPECTRA,

WAVELENGTHS

164

N82-28880"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md,

USER'S GUIDE FOR THE TOTAL-OZONE MAPPING

SPECTROMETER (TOMS) INSTRUMENT FIRST YEAR OZONE

T DATA SET

A. J, FLEIG, K. F. KLENK (Systems and Applied Sciences Corp.,

Bladensburg, Md.), P. K. BHARTIA (Systems and Applied Sciences

Corp., Bladensburg, Md,), and D. GORDON (Systems and Applied

Sciences Corp., Bladensburg, Md.) Jun. 1982 50 p refs

(NASA-RP-1096; NAS 1.61:1096) Avail: NTIS HC A03/MF A01

CSCL 04B

The TOMS experiment and algorithms are described. Detailed

information on the data available on computer tape is provided.

Author

N82-29826"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

USER'S GUIDE FOR THE SOLAR BACKSCATTERED

ULTRAVIOLET (SBUV) INSTRUMENT FIRST YEAR OZONE-S

DATA SET

A. J. FLEIG, K. F. KLENK, P. K. BHARTIA, D. GORDON, and W.

H. SCHNEIDER Jun. 1982 69 p refs Prepared in cooperation

with Systems and Applied Sciences Corp., Bladensburg, Md.

(NAS5-26753)

(NASA-RP-1095; REPT-82FO136; NAS 1.61:1095) Avail: NTIS

HC A04/MF A01 CSCL 04B

Total-ozone and ozone vertical profile results for Solar

Backscattered Ultraviolet/Total Ozone Mapping Spectrometer

(SBUV/TOMS) Nimbus 7 operation from November 1978 to

November 1979 are available. The algorithm used have been

thoroughly tested, the instrument performance has been examined

in details, and the ozone results have been compared with Dobson,

Umkehr, balloon, and rocket observations. The accuracy and

precision of the satellite ozone data are good to at least within

the ability of the ground truth to check and are self-consistent to

within the specifications of the instrument. The 'SBUV User's Guide'

describes the SBUV experiment and algorithms used. Detailed

information on the data available on computer tape is provided

including how to order tapes from the National Space Science

Data Center. J.MS.

N83-14824"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

A STABILITY ANALYSIS OF AVE-4 SEVERE WEATHER

SOUNDINGS

D. L. JOHNSON Nov. 1982 139 p refs

(NASA-TP-2045; NAS 1.60:2045) Avail: NTIS HC A07/MF A01

CSCL 04B

STORMS (METEOROLOGY), THERMODYNAMICS, VERTICAL

DISTRIBUTION, WEATHER FORECASTING, WIND PROFILES

N83-14825"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

THE CONCEPTION, GROWTH, ACCOMPLISHMENTS AND

FUTURE OF METEOROLOGICAL SATELLITES

W. W. VAUGHAN, comp. Washington Nov. 1982 105 p

refs Proc. of the 62d Ann. Meeting held at San Antonio, Tex.,

11-15 Jan. 1982; sponsored by the American Meteorological

Society

(NASA-CP-2257; NAS 1.55:2257) Avail: NTIS HC A06/MF A01

CSCL 04B

METEOROLOGICAL SATELLITES, NIMBUS PROJECT,

SATELLITE OBSERVATION, TIROS N SERIES SATELLITES,

TIROS PROJECT
N83-14835"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

NIMBUS 6 RANDOM ACCESS MEASUREMENT SYSTEM

APPLICATIONS EXPERIMENTS

C, E. COTE, ed., R. TAYLOR, ed., and E. GILBERT, ed. Oct.

1982 103 p

(NASA-SP-457; LC-82-14553; NAS 1.21:457) Avail: NTIS HC

A06/MF A01 CSCL 04B

The advantages of a technique in which data collection

platforms randomly transmit signal to a polar orbiting satellite,

thus eliminating satellite interrogation are demonstrated in

investigations of the atmosphere; oceanographic parameters; Arctic

regions and ice conditions; navigation and position location; and

data buoy development. For individual titles, see N83-14836

through N83-14862.

N83-19391"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

NASAIMSFC FY-82 ATMOSPHERIC PROCESSES RESEARCH

REVIEW Summary Report

R. E. TURNER, comp. 1982 243 p refs Meeting held at

Huntsville, Ala., 19-21 Oct. 1982

(NASA-CP-2259; NAS 1.55:2259) Avail: NTIS HC A11/MF A01

CSCL 04B

AIR CURRENTS, METEOROLOGICAL PARAMETERS,

STORMS (METEOROLOGY), UPPER ATMOSPHERE, WEATHER

N83-24028"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

VISSR ATMOSPHERIC SOUNDER (VAS) RESEARCH REVIEW

J. R. GREAVES, ed. Washington Mar. 1983 54 p refs

Rev. held in Greenbelt, Md., 16-17 Jun. 1982 Original contains

color illustrations

(NASA-CP-2253; REPT-83F0188; NAS 1.55:2253) Avail: NTIS

HC A04/MF A01 CSCL 04B

ATMOSPHERIC MOISTURE, ATMOSPHERIC SOUNDING,

CLOUDS, VISIBLE INFRARED SPIN SCAN RADIOMETER, WATER

VAPOR, WEATHER FORECASTING

N83-25265"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ata.

SUMMARY PROCEEDINGS OF A WIND SHEAR WORKSHOP

J. H. ENDERS (Flight Safety Foundation, Arlington, Va.), W. W.

MELVIN (Air Line Pilots Assoc., Denison, Tax.), W. FROST

(Tennessee Univ. Space Inst., Tullahoma, Tenn.), and D. W.

CAMP Apr. 1983 20 p Workshop Held at Tennessee Univ.

Space Inst., Tullahoma, Tenn., 25 Oct. 1982

(NASA-CP-2270; NAS 1.55:2270) Avail: NTIS HC A02/MF A01

CSCL 04B

AIRCRAFT SAFETY, COMPUTERIZED SIMULATION,

DOPPLER RADAR, FLIGHT CREWS, FLIGHT TRAINING, VORTEX

GENERATORS, WARNING SYSTEMS, WIND SHEAR

N83-28828"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

USER'S GUIDE FOR THE SOLAR BACKSCATTERED

ULTRAVIOLET (SBUV) AND THE TOTAL OZONE MAPPING

SPECTROMETER (TOMS) RUT-S AND RUT-T DATA SETS:

OCTOBER 31, 1978 TO NOVEMBER 1, 1980

A. J. FLEIG, D. F. HEATH, K. F. KLENK (Systems and Applied

Sciences Corp., Bladensburg, Md), N. OSLIK (Systems and Applied

Sciences Corp., Bladensburg, MD.), K. D. LEE (Systems and

Applied Sciences Corp., Bladensburg, Md.), H. PARK (Systems

and Applied Sciences Corp., Bladensburg, Md.), P. K. BHARTIA

(Systems and Applied Sciences Corp., Bladensburg, Md.), and D.

GORDON (Systems and Applied Sciences Corp., Bladensburg,

Md.) Jun. 1983 135 p refs

(NAS5-27393)

(NASA-RP-1112; REPT-910; NAS 1.61:1112) Avail: NTIS HC

A07/MF A01 CSCL 04B

Raw data from the Solar Backscattered Ultrviolet/Total Ozone

Mapping Spectrometer (SBUV/TOMS) Nimbus 7 operation are

available on computer tape. These data are contained on two

47 METEOROLOGY AND CLIMATOLOGY

separate sets of RUTs (Raw Units Tapes) for SBUV and TOMS,

labelled RUT-S and RUT-T respectively. The RUT-S and RUT-T

tapes contain uncalibrated radiance and irradiance data,

housekeeping data, wavelength and electronic calibration data,

instrument field-of-view location and solar ephemeris information.

These tapes also contain colocated cloud, terrain pressure and

snow/ice thickness data, each derived from an independent source.

The 'RUT User's Guide' describes the SBUV and TOMS

experiments, the instrument calibration and performance, operating

schedules, and data coverage, and provides an assessment of

RUT-S and -T data quality. It also provides detailed information

on the data available on the computer tapes. S.L.

N83-33494"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

NASAIMSFC FY-83 ATMOSPHERIC PROCESSES RESEARCH

REVIEW

R. E. TURNER, comp. Aug. 1983 163 p Program review held

at Huntsville, Ala., 24-25 May 1983

(NASA-CP-2281; M-417; NAS 1.55:2281) Avail: NTIS HC

A08/MF A01 CSCL 04B

CONFERENCES, DOPPLER RADAR, LIGHTNING,

MESOSCALE PHENOMENA, STORMS (METEOROLOGY), UPPER

ATMOSPHERE, WEATHER, WIND (METEOROLOGY)

N83-36587"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

NASAIMSFC FY-83 ATMOSPHERIC RESEARCH REVIEW

R. E. TURNER, comp. and D. W. CAMP, comp. Washington

Oct. 1983 34 p refs Rev. held in Huntsville, Ala., 24-25 May

1983

(NASA-CP-2288; NAS 1.55:2288) Avail: NTIS HC A03/MF A01

CSCL 04B

AIRCRAFT HAZARDS, AIRPORTS, GUSTS, METEOROLOGY,

WIND SHEAR

N84-16720"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

USER'S GUIDE FOR SBUV/TOMS OZONE DERIVATIVE

PRODUCTS

A. J. FLEIG, C. WELLEMEYER, N. OSLIK, D. LEE, J. MILLER,

and R. MAGATANI Jan. 1984 91 p refs

(NAS5o27393)

(NASA-RP-1116; NAS 1.61:1116) Avail: NTIS HC A05/MFA01

CSCL 04B

A series of products are available derived from the total-ozone

and ozone vertical profile results for the Solar Backscattered

Ultraviolet/Total-Ozone Mapping Spectrometer (SBUV/TOMS)

Nimbus-7 operation. Products available are (1) orbital height-latitude

cross sections of the SBUV profile data, (2) daily global total

ozone contours in polar coordinates, (3) daily averages of total

ozone in global 5x5 degree latitude-longitude grid, (4) daily, monthly

and quarterly averages of total ozone and profile data in 10 degree

latitude zones, (5) tabular presentation of zonal means, (6) daily

global total ozone and profile contours in polar coordinates. The

"Derivative Products User's Guide" describes each of these

products in detail, including their derivation and presentation format.

Information is provided on how to order the tapes and microfilm

from the National Space Science Data Center. Author

N84-24044"# National Aeronautics and Space Administration,

Washington, D.C.

A SPATIAL MODEL OF WIND SHEAR AND TURBULENCE FOR

FLIGHT SIMULATION Ph.D. Thesis - Colorado State Univ.

C. W. CAMPBELL May 1984 131 p refs

(NASA-TP-2313; NAS 1.60:2313) Avail: NTIS HC A07/MF A01

CSCL 04B

ATMOSPHERIC MODELS, ATMOSPHERIC TURBULENCE,

COMPUTERIZED SIMULATION, FLIGHT SIMULATION,

ISOTROPIC TURBULENCE, THREE DIMENSIONAL FLOW,

TURBULENT FLOW, WIND PROFILES, WIND SHEAR

165
47 METEOROLOGY AND CLIMATOLOGY

N84-31865"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

CLIMATOLOGY OF OZONE AT ALTITUDES FROM 19,000 AT

59,000 FEET BASED ON COMBINED GASP AND OZONESONDE

DATA

W. H. JASPERSON (Control Data Corp.), G. D. NASTROM (Control

Data Corp.), and J. D. HOLDEMAN Aug. 1984 363 p refs

(DOT-FA78WAI-893)

(NASA-Tpo2303; E-1626; NAS 1.60:2303) Avail: NTIS HC

A16/MFA01 CSCL04B

CLIMATOLOGY, DATA ACQUISITION, DATA CORRELATION,

GLOBAL AIR SAMPLING PROGRAM, OZONE

N84-34829"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

NASA/MSFC FY-84 ATMOSPHERIC PROCESSES RESEARCH

REVIEW

W. W. VAUGHAN, comp. and F. PORTER, comp. Washington

Sep. 1984 223 p refs Rev. held in Huntsville, Ala., 30 Apr.

and 2-3 May 1984

(NASA-CP-2329; M-458; NAS 1.55:2329) Avail: NTIS HC

A10/MF A01 CSCL 04B

ATMOSPHERIC CIRCULATION, ATMOSPHERIC MODELS,

ATMOSPHERIC SOUNDING, BACKSCATTERING, BAROCLINIC

INSTABILITY, CLOUDS (METEOROLOGY), CONFERENCES,

CYCLONES, DOPPLER RADAR, EARTH ATMOSPHERE,

LIGHTNING, MESOSCALE PHENOMENA, OPTICAL RADAR,

PRECIPITATION (METEOROLOGY), THUNDERSTORMS, WIND

MEASUREMENT

N85-14360"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

GLOBAL SCALE ATMOSPHERIC PROCESSES RESEARCH

PROGRAM REVIEW

B. A. WORLEY, ed. and C. A. PESLEN, ed. Washington Nov.

1984 233 p refs Rev. held in Greenbelt, Md., 8-10 Aug.

1984

(NASA-CP-2344; NAS 1.55:2344) Avail: NTIS HC A11/MF A01

CSCL 04B

ATMOSPHERIC CIRCULATION, GLOBAL ATMOSPHERIC

RESEARCH PROGRAM, PLANETARY WAVES, REMOTE

SENSING, WEATHER FORECASTING

N85-16343"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

INTERNATIONAL AEROSPACE AND GROUND CONFERENCE

ON LIGHTNING AND STATIC ELECTRICITY. 1984 TECHNICAL

PAPERS. SUPPLEMENT

Washington Dec. 1984 65 p refs Conf. held in Orlando,

Fla., 26-28 Jun. 1984; sponsored in cooperation with NASA, Army,

Navy, AF, DOT, Florida Inst. of Tech., IEEE, Society of Automotive

Engineers, United Kingdom Civil Aviation Authority, United Kingdom

Royal Aircraft Establishment, and Culham Lab.

(NASA-CP-2356; L-15910; NAS 1.55:2356;

NADC-84104-20-SUPPL) Avail: NTIS HC A04/MF A01 CSCL

04B

CONFERENCES, LIGHTNING, STATIC ELECTRICITY

N85-16351"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

AN EVALUATION AND COMPARISON OF VERTICAL PROFILE

DATA FROM THE VISSR ATMOSPHERIC SOUNDER (VAS)

G. J. JEDLOVEC Washington Jan. 1985 40 p refs

(NASA-TP-2425; NAS 1.60:2425) Avail: NTIS HC A03/MF A01

CSCL 04B

ALGORITHMS, EVALUATION, MOISTURE, RAWlNSONDES,

STATISTICAL ANALYSIS, TEMPERATURE PROFILES, VISIBLE

INFRARED SPIN SCAN RADIOMETER

166

N85-20605"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

THREE-DIMENSIONAL BAROCLINIC INSTABILITY OF A

HADLEY CELL FOR SMALL RICHARDSON NUMBER

B. N. ANTAR and W. W. FOWLIS Mar. 1985 33 p refs

(NASA-TP-2450; NAS 1.60:2450) Avail: NTIS HC A03/MF A01

CSCL 04B

BAROCLINIC INSTABILITY, FLUID DYNAMICS,

PERTURBATION, RICHARDSON NUMBER

N85-21878"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

A NEW NASA/MSFC MISSION ANALYSIS GLOBAL CLOUD

COVER DATA BASE

S. C. BROWN and W. R. JEFFRtES, Ill (Computer Sciences Corp.,

Huntsville, Ala.) Mar. 1985 17 p refs

(NASA-TP-2448; NAS 1.60:2448) Avail: NTIS HC A02/MF A01

CSCL 03B

CLIMATOLOGY, CLOUD COVER, DATA BASES,

NEPHANALYSIS, NORTHERN HEMISPHERE, SOUTHERN

HEMISPHERE

N86-11735"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

METEOROLOGICAL AND ENVIRONMENTAL INPUTS TO

AVIATION SYSTEMS

D. W. CAMP, ed. and W. FROST, ed. (Tennessee Univ. Space

Inst.) Sep. 1985 144 p refs Workshop held in Tullahoma,

Tenn., 26-28 Oct. 1983; sponsored by NASA, NOAA, FAA, DOD,

and Office of the Federal Coordinator for Meteorology

(NAS8-36177)

(NASA-CP-2388; NAS t.55:2388) Avail: NTIS HC A07/MF A01

CSCL 04B

AIRCRAFT SAFETY, FLIGHT CHARACTERISTICS, FLIGHT

HAZARDS, METEOROLOGICAL PARAMETERS, METEOROLOGICAL SERVICES, WEATHER FORECASTING

N86-13866"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

UNDERSTANDING CLIMATE: A STRATEGY FOR CLIMATE

MODELING AND PREDICTABILITY RESEARCH, 1985-1995

O. THIELE, ed. and R. A. SCHIFFER, ed. Oct. 1985 38 p

refs

(NASA-RP-1158; REPT-85B0489; NAS 1.61:1158) Avail: NTIS

HC A03/MF A01 CSCL 04B

The emphasis of the NASA strategy for climate modeling and

predictability research is on the utilization of space technology to

understand the processes which control the Earth's climate system

and it's sensitivity to natural and man-induced changes and to

assess the possibilities for climate prediction on time scales of

from about two weeks to several decades. Because the climate

is a complex multi-phenomena system, which interacts on a wide

range of space and time scales, the diversity of scientific problems

addressed requires a hierarchy of models along with the application

of modern empirical and statistical techniques which exploit the

extensive current and potential future global data sets afforded by

space observations. Observing system simulation experiments,

exploiting these models and data, will also provide the foundation

for the future climate space observing system, e.g., Earth observing

system (EOS), 1985; Tropical Rainfall Measuring Mission (TRMM)

North, et al. NASA, 1984. Author

N86-13867"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

VAS DEMONSTRATION: (VISSR ATMOSPHERIC SOUNDER)

DESCRIPTION Final Report

H. E. MONTGOMERY and L. W. UCCELLINI Oct. 1985 193 p

refs

(NASA-Rpo1151; REPT-85F0274; NAS 1.61:1151) Avail: NTIS

HC A09/MF A01 CSCL 04B

The VAS Demonstration (VISSR Atmospheric Sounder) is a

project designed to evaluate the VAS instrument as a remote

sensor of the Earth's atmosphere and surface. This report describes
theinstrument andgroundprocessingsystem, theinstrument

performance, thvaliationasatemperature andmoistureprofiler

comparedwithgroundtruthandothersatellites, andassesses its

performance asa valuablemeteorological tool.Thereportalso

addresses theavailability ofdataforscientificresearch.Author

N86-23160"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SITE SELECTION AND DIRECTIONAL MODELS OF DESERTS

USED FOR ERBE VALIDATION TARGETS

W.F. STAYLOR Apr. 1986 15p refs

(NASA-TP-2540; L-16041; NAS 1.60:2540) Avail: NTIS HC

A02/MF A01 CSCL 04B

ACCURACY, DESERTS, EARTH RADIATION BUDGET

EXPERIMENT, MODELS, RADIANCE, SITE SELECTION

N86-24082"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

CURRENT SCIENTIFIC ISSUES IN LARGE SCALE

ATMOSPHERIC DYNAMICS

T. L. MILLER, comp. Washington Jan. 1986 46 p refs

Workshop held in Huntsville, Ala., 20-21 Jun. 1985

(NASA-CP-2410; M-506; NAS 1.55:2410) Avail: NTIS HC

A03/MF A01

ATMOSPHERIC CIRCULATION, BAROCLINIC WAVES,

BLOCKING, CONFERENCES, CYCLOGENESIS, FRONTS

(METEOROLOGY), GRAVITY WAVES, OROGRAPHY,

PLANETARY WAVES, SYNOPTIC METEOROLOGY

N86-24090"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

STATISTICAL ANALYSIS OF DIRECT-STRIKE LIGHTNING

DATA (1980 TO 1982)

L. D. LEE, G. B. FINELLI, M. E. THOMAS, and F. L. PITTS Jan.

1984 30p refs

(NASA-TP-2252; L-15686; NAS 1.60:2252) Avail: NTIS HC

A03/MF A01 CSCL 04B

AIRCRAFT HAZARDS, ELECTROMAGNETIC MEASUREMENT,

EXTREMUM VALUES, LIGHTNING, QUANTILES, STATISTICAL

ANALYSIS

N86-25924"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

DESCRIPTION OF DATA ON THE NIMBUS 7 LIMS MAP

ARCHIVE TAPE: TEMPERATURE AND GEOPOTENTIAL

HEIGHT

K. V. HAGGARD, E. E. REMSBERG, W. L. GROSE, J. M. RUSSELL,

III, B. T. MARSHALL (SASC Technologies, Inc., Hampton, Va.),

and G. LINGENFELSER (Analytical Mechanics Associates, Inc.,

Hampton, Va.) May 1986 55 p refs

(NASA-TP-2553; L-16071; NAS 1.60:2553) Avail: NTIS HC

A04/MF A01 CSCL 04B

EARTH LIMB, MAPPING, NIMBUS 7 SATELLITE,

STRATOSPHERE, SYNOPTIC METEOROLOGY

N86-28574"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SURFACE RADIATION BUDGET FOR CLIMATE

APPLICATIONS

J. T. SUTTLES, ed. and G. OHRING, ed. (National Oceanic and

Atmospheric Administration, Washington, D.C.) Aug. 1986 123

P

(NASA-RP-1169; L-16133; NAS 1.61:1169) Avail: NTIS HC

A07/MF A01 CSCL 04B

The Surface Radiation Budget (SRB) consists of the upwelling

and downwelling radiation fluxes at the surface, separately

determined for the broadband shortwave (SW) (0 to 5 micron)

and Iongwave (LW) (greater than 5 microns) spectral regions plus

certain key parameters that control these fluxes, specifically, SW

albedo, LW emissivity, and surface temperature. The uses and

requirements for SRB data, critical assessment of current

capabilities for producing these data, and directions for future

research are presented. B.G.

48 OCEANOGRAPHY

48

OCEANOGRAPHY

Includes biological, dynamic, and physical oceanography; and

marine resources.

N77-16675"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

FREE DRIFTING BUOYS

1974 378 p refs Presented at Drift Buoy Symp., Hampton,

Va., 22-23 May 1974; Sponsored by AIAA Tech. Comm. on Marine

Systems and Technol.

(NASA-CP-2003) Avail: NTIS HC A17/MF A01 CSCL 08C

BUOYS, OPTICAL TRACKING, RADIO TRACKING, TRACKING

RADAR

N78-12644"# National Aeronautics and Space Administration.

Lyndon B. Johnson Space Center, Houston, Tex.

REMOTE SENSING OF OCEANIC PARAMETERS DURING THE

SKYLABIGAMEFISH EXPERIMENT

K. H. FALLER Nov. 1977 43 p refs

(NASA-RP-1012; JSC-S-468) Avail: NTIS HC A03/MF A01

CSCL 08J

Effort to demonstrate the feasibility of using remotely acquired

information to assess and monitor the distribution of oceanic

gamefish are described. Data supplied by Skylab and aircraft

surveying an area in the Gulf of Mexico with thermal and optical

radiometers and cameras were used in conjunction with

oceanographic data provided by surface vessels to explore a

relationship between oceanographic parameters and remotely

acquired data. Thermal scanner imagery and precision radiometric

thermometer data obtained by the two aircraft were combined to

provide a composite surface temperature map of the test area.

Spectral radiometer data were studied in conjunction with surface

measurements of chlorophytl-a and turbidity, and several models

were developed which predicted these two oceanic parameters

from the radiance data. Contour maps of the chlorophyll-a content

and turbidity were developed from the best chlorophyll and turbidity

models and from surface measurements. Basic problems

concerning the remote measurement of the Sicchi extinction depth

are discussed, and suggestions are made for improving the remote

measurement turbidity. Author

N78-12645"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

LABORATORY MEASUREMENTS OF UPWELLED RADIANCE

AND REFLECTANCE SPECTRA OF CALVERT, BALL, JORDAN,

AND FELDSPAR SOIL SEDIMENTS

C. H. WHITLOCK, J. W. USRY, W. G. WITTE, and E. A.

GURGANUS Dec. 1977 36 p refs

(NASA-TP-1039; L-11854) Avail: NTIS HC A03/MF A01

CSCL 08J

RADIANCE, REFLECTANCE, SEDIMENTS, SOILS, SPECTRAL

SIGNATURES, UPWELLING WATER

N78-21737"# National Aeronautics and Space Administration.

Wallops Flight Center, Wallops Island, Va.

REMOTE SENSING OF GULF STREAM USING GEOS-3 RADAR

ALTIMETER

C. D. LEITAO, N. E. HUANG (EG and G Washington Anal. Serv.

Center, Inc., Pocomoke City, Md.), and C. G. PARRA Apr. 1978

34 p refs

(NASA-TP-1209) Avail: NTIS HC AO3/MF A01 CSCL 08J

ALTIMETERS, GEOS 3 SATELLITE, GULF STREAM, REMOTE

SENSORS, TOPOGRAPHY

167
48 OCEANOGRAPHY

N79-28863"#National Aeronautics andSpace Administration.

Langley Research Center, Hampton, Va.

SEA-SURFACE TEMPERATURE AND SALINITY MAPPING

FROM REMOTE MICROWAVE RADIOMETRIC MEASUREMENTS

OF BRIGHTNESS TEMPERATURE

C. B. HANS-JUERGEN, B. M KENDALL, and J. C. FEDORS Dec.

1977 29 p refs

(NASA-TP-1077; L-11763) Avail: NTIS HC A03/MF A01

CSCL 08J

BRIGHTNESS TEMPERATURE, MAPPING, MICROWAVE

EQUIPMENT, OCEAN SURFACE, RADIOMETERS, SALINITY

N79-28864"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

INVESTIGATION OF EFFECTS OF BACKGROUND WATER ON

UPWELLED REFLECTANCE SPECTRA AND TECHNIQUES FOR

ANALYSIS OF DILUTE PRIMARY-TREATED SEWAGE SLUDGE

C. H. WHITLOCK, J. W. USRY, W. G. WITTE, F. H. FARMER,

and E. A. GURGANUS Aug. 1979 36 p refs

(NASA-TP-1446; L-12694) Avail: NTIS HC A03/MF A01

CSCL 08J

ENVIRONMENTAL MONITORING, REFLECTANCE, REMOTE

SENSORS, SPECTRAL SIGNATURES, WATER

N79-31890"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SPECTRAL MEASUREMENTS OF OCEAN-DUMPED WASTES

TESTED IN THE MARINE UPWELLED SPECTRAL SIGNATURE

LABORATORY

W. G. WITTE, J. W. USRY, C. H. WHITLOCK, and E. A.

GURGANUS Washington Sep. 1979 34 p refs

(NASA-TP-1480; L-12906) Avail: NTIS HC A03/MF A01

CSCL 08C

INDUSTRIAL WASTES, REMOTE SENSORS, WASTE

DISPOSAL

N60-12718"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

REMOTE SENSING AND PROBLEMS OF THE HYDROSPHERE

E. D. GOLDBERG, ed. (Scripps Institution of Oceanography, La

Jolla, Calif.) Washington Dec. 1979 67 p refs Workshop

held at Warner Springs, Calif., 29-31 Jan. 1979; sponsored by

NASA, Langley Res. Center and NASA, Washington

(NASA-CP-2109; L-t3404) Avail: NTIS HC A04/MF A01

CSCL 08J

EARTH HYDROSPHERE, MARINE ENVIRONMENTS, REMOTE

SENSORS

N80-23956"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

REMOTE SENSING AND PROBLEMS OF THE HYDROSPHERE.

A FOCUS FOR FUTURE RESEARCH

E D. GOLDBERG, ed. (Scripps Inst. of Oceanography, La Jolla,

Calif.) Apr. 1980 35 p refs Meeting held at New Orleans,

9-11 May 1979

(NASA-CP-2132; L-13645) Avail: NTIS HC A03/MF A01

CSCL 08C

CONFERENCES, EARTH HYDROSPHERE, REMOTE

SENSORS

N81-31801"# National Aeronautics and Space Administration,

Washington, D.C.

OCEANIC LIDAR

K. L. CARDER, ed. Aug. 1981 45 p refs Workshop

presented at Greenbelt, MD., 13-14 Nov. 1980

(NASA-CP-2194) Avail: NTIS HC A03/MF A01 CSCL 08C

CHLOROPHYLLS, COASTAL ZONE COLOR SCANNER,

CONFERENCES, FLUORESCENCE, LASER APPLICATIONS,

OCEANOGRAPHIC PARAMETERS, OPTICAL RADAR

168

N82-10661"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

CHESAPEAKE BAY PLUME STUDY: SUPERFLUX 1980

J. W. CAMPBELL, ed. and J. P. THOMAS, ed. (National Marine

Fisheries Service, Highland, N.J.) Oct. 1981 504 p refs

Syrup. held at Williamburg, Va., 21-23 Jan. 1981; sponsored in

part by National Marine Fisheries Service, NOAA, and Dept. of

Commerce

(NASA-CP-2188; L-14680; NOAA-NEMP-t 11-81-ABCDFG-0042)

Avail: NTIS HC A22/MF A01 CSCL 08C

CHESAPEAKE BAY (US), CONFERENCES, ECOSYSTEMS,

ESTUARIES, REMOTE SENSING

N82-16683*# National Aeronautics and Space Administration.

Wallops Flight Center, Wallops Island, Va.

NOSS ALTIMETER ALGORITHM SPECIFICATIONS

D. W. HANCOCK, R. G. FORSYTHE, and J. D. MCMILLAN

(Washington Analytical Services Center, Pocomoke City, Md.) Jan.

1982 112 p refs

(NASA-RP-1083) Avail: NTIS HC A06/MF A01 CSCL 08C

A description of all algorithms required for altimeter processing

is given. Each description includes title, description, inputs/outputs,

general algebraic sequences and data volume. All required

input/output data files are described and the computer resources

required for the entire altimeter processing system were estimated.

The majority of the data processing requirements for any radar

altimeter of the Seasat-1 type are scoped. Additions and deletions

could be made for the specific altimeter products required by

other projects. T.M.

N83-19411"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

VISIBLE ABSORBANCE SPECTRA: A BASIS FOR IN SITU AND

PASSIVE REMOTE SENSING OF PHYTOPLANKTON

CONCENTRATION AND COMMUNITY COMPOSITION

F. H. FARMER, O. JARRETT, JR., and C. A. BROWN, JR. Feb.

1983 35p refs

(NASA-TP-2094; L-15490; NAS 1.60:2094) Avail: NTIS HC

A03/MF A01 CSCL 08A

ABSORPTION SPECTRA, CHEMICAL COMPOSITION,

PHYTOPLANKTON, PLANKTON, POPULATIONS

N83-24133"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

MEASUREMENTS OF SPECTRAL ATTENUATION

COEFFICIENTS IN THE LOWER CHESAPEAKE BAY

W. M. HOUGHTON Apr. 1983 36 p refs

(NASA-TP-2130; L-15406; NAS 1.60:2130) Avail: NTIS HC

A03/MF A01 CSCL 08J

ABSORPTION, ABSORPTIVITY, ATTENUATION, ESTUARIES,

LIGHT TRANSMISSION, OCEANOGRAPHY

N84-10718"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

ANTARTIC SEA ICE, 1973 1976: SATELLITE

PASSIVE-MICROWAVE OBSERVATIONS

H. J. ZWALLY, J. C. COMISO, C. L. PARKINSON, W. J. CAMPBELL

(Geological Survey, Takoma, Wash.), F. D. CARSEY (Jet Propulsion

Lab., California Inst. of Tech., Pasadena), and P. GLOERSEN

Washington 1983 216 p refs Original document contains

color illustrations

(NASA-SP-459; NAS 1.21:459; LC-83-600167) Avail: NTIS HC

A10/MFA01; SOD HC$21.00 CSCL08L

Data from the Electrically Scanning Microwave Radiometer

(ESMR) on the Nimbus 5 satellite are used to determine the extent

and distribution of Antarctic sea ice. The characteristics of the

southern ocean, the mathematical formulas used to obtain

quantitative sea ice concentrations, the general characteristics of

the seasonal sea ice growth/decay cycle and regional differences,

and the observed seasonal growth/decay cycle for individual years

and interannual variations of the ice cover are discussed. The

sea ice data from the ESMR are presented in the form of

color-coded maps of the Antarctic and the southern oceans. The
mapsshow brightness temperatures and concentrations of pack

ice averaged for each month, 4-year monthly averages, and

month-to-month changes. Graphs summarizing the results, such

as areas of sea ice as a function of time in the various sectors of

the southern ocean are included. The images demonstrate that

satellite microwave data provide unique information on large-scale

sea ice conditions for determining climatic conditions in polar

regions and possible global climatic changes. J.M.S.

N85-26028"# National Aeronautics and Space Administration.

Goddard Inst. for Space Studies, New York, N.Y.

NORTH ATLANTIC DEEP WATER FORMATION

T. BENNETT, ed., W. S. BROECKER, ed., and J. HANSEN, ed.

Dec. 1984 74 p refs Symp. held in Palisades, N.Y., Feb.

1985 Sponsored by NASA. Goddard Space Flight Center

(NASA-CP-2367; NAS 1.55:2367) Avail: NTIS HC A04/MF A01

CSCL 08J

AIR WATER INTERACTIONS, ATLANTIC OCEAN,

CONVECTIVE FLOW, DISSOLVED GASES, GREENLAND, ICE,

MIXING, OCEAN TEMPERATURE, PERIODIC VARIATIONS,

SALINITY, WATER CIRCULATION

51

LIFE SCIENCES (GENERAL)

N77-33780"# National Aeronautics and Space Administration.

Lyndon B. Johnson Space Center, Houston, Tex.

BIOMEDICAL RESULTS FROM SKYLAB

R. S. JOHNSTON, ed. and L. F. DIETLEIN, ed. Washington

1977 502 p refs Original contains color illustrations

(NASA-SP-377; LC-76-54287) Avail: NTIS MF A01; SOD HC as

033-000-00648-9 CSCL 06P

Biomedical data from various experiments and observations

reflect the physiological responses of spacecrews to prolonged

space flight stress. For individual titles, see N77-33781 through

N77-33836.

N78-11663"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

THE USE OF NONHUMAN PRIMATES IN SPACE

R. C. SIMMONDS, ed. and G. H. BOURNE, ed. (Emory Univ.)

Sep. 1977 390 p refs Proc. held at Moffett Field, Calif., 2-4

Dec. 1974

(NASA-CP-005; A-6133) Avail: NTIS HC A17/MF A01 CSCL

06C

AEROSPACE MEDICINE, BIODYNAMICS, CONFERENCES,

EXPERIMENT DESIGN, PRIMATES, SPACE FLIGHT STRESS,

WEIGHTLESSNESS

N78-18673"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

DESIGN OF A BLOOD-FREEZING SYSTEM FOR LEUKEMIA

RESEARCH

T. E. WILLIAMS and T. A. CYGNAROWICZ Feb. 1978 43 p

refs

(NASA-TP-1165; G-7702-F9) Avail: NTIS HC A03/MF A01

CSCL 06E

BLOOD, FREEZING, HEMATOLOGY, LEUKEMIAS, MEDICAL

EQUIPMENT, RESEARCH AND DEVELOPMENT

51 LIFE SCIENCES (GENERAL)

N79-19592"# National Aeronautics and Space Administration.

Wallops Flight Center, Wallops Island, Va.

RADAR, INSECT POPULATION ECOLOGY, AND PEST

MANAGEMENT

C. R. VAUGHN, ed., W. WOLF, ed. (Dept. of Agriculture, Beltsville,

Md.), and W. KLASSEN, ed. Mar. 1979 252 p refs Workshop

held at Wallops Island, Va., 2-4 May 1978; sponsored in part by

US Dept. of Agriculture

(NASA-CP-2070) Avail: NTIS HC A12/MF A01 CSCL 06C

ECOLOGY, INSECTS, POPULATIONS, RADAR

N84-11720"# Texas Univ., Austin. Dept. of Botany.

THE REGULATORY FUNCTIONS OF CALCIUM AND THE

POTENTIAL ROLE OF CALCIUM IN MEDIATING

GRAVITATIONAL RESPONSES IN CELLS AND TISSUES

S. J. ROUX, ed. Nov. 1983 295 p refs Workshop held in

Bethesda, Md., 16-18 Sep. 1982

(NSG-7480)

(NASA-CP-2286; NAS 1.55:2286) Avail: NTIS HC A13/MF A01

CSCL 06B

CALCIUM, CELLS (BIOLOGY), CONFERENCES,

GRAVIRECEPTORS, PHYSIOLOGICAL RESPONSES, TISSUES

(BIOLOGY)

N84-18829"# National Aeronautics and Space Administration,

Washington, D.C.

NASA SPACE BIOLOGY PROGRAM. EIGHTH ANNUAL

SYMPOSIUM'S PROGRAM AND ABSTRACTS

T. W. HALSTEAD, ed. Feb. 1984 121 p refs Symp. held in

Arlington, Va., 12-14 Oct. 1983

(NASA-CP-2299; EBT-3; NAS 1.55:2299) Avail: NTIS HC

A06/MF A01 CSCL 06C

ABSTRACTS, ANIMALS, BIOSYNTHESIS, CONFERENCES,

EXOBIOLOGY, GRAVIRECEPTORS, METABOLISM, PLANTS

(BOTANY)

N84-30665"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

GLOBAL BIOLOGY RESEARCH PROGRAM: BIOGEOCHEMICAL

PROCESSES IN WETLANDS

D. S. BARTLErT, ed. Washington Aug. 1984 43 p refs

Workshop held in Arlington, 22-24 Mar. 1983

(NASA-CP-2316; L-15791; NAS 1.55:2316) Avail: NTIS HC

A03/MF A01 CSCL 13B

AIR WATER INTERACTIONS, BIOGEOCHEMISTRY, CYCLES,

DATA BASES, EXCHANGING, GEOGRAPHY, WETLANDS

N85-26054"# National Aeronautics and Space Administration,

Washington, D.C.

NASA SPACE BIOLOGY PROGRAM: 9TH ANNUAL SYMPOSIUM

Abstracts Only

T. W. HALSTEAD Apr. 1985 128 p refs Syrup. held in

Harper's Ferry, W. Va., 6-9 Nov. 1984

(NASA-CP-2336; NAS 1.55:2336) Avail: NTIS HC A07/MF A01

CSCL 06C

ANIMALS, CONFERENCES, GRAVITATIONAL EFFECTS,

METABOLISM, PLANTS (BOTANY), SPACE FLIGHT

N85-32708"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

THE EVOLUTION OF COMPLEX AND HIGHER ORGANISMS

D. Milne, ed. (Evergreen State Coll.), D. RAUP, ed. (Chicago Univ.),

J. BILLINGHAM, ed., K. NIKLAUS, ed. (Cornell Univ., Ithaca, N.Y.),

and K. PADIAN, ed. (California Univ., Berkeley) 1985 113 p

refs Original contains color illustrations

(NASA-SP-478; A-9363; NAS 1.21:478; LC-85-7159) Avail:

NTIS HC A06/MF A01; SOD HC $8.50 as 033-000-00951-8

CSCL 06C

The evolution of Phanerozoic life has probably been influenced

by extraterrestrial events and properties of the Earth-Moon system

that have not, until now, been widely recognized. Tide range,

gravitational strength, the Earth's axial tilt, and other planetary

properties provide background conditions whose effects on

169
51 LIFE SCIENCES (GENERAL)

evolution may be difficult to distinguish. Solar flares, asteroid

impacts, supernovae, and passage of the solar system through

galactic clouds can provide catastrophic changes on the Earth

with consequent characteristic extinctions. Study of the fossil record

and the evolution of complex Phanerozoic life can reveal evidence

of past disturbances in space near the Earth. Conversely, better

understanding of environmental influences caused by

extraterrestrial factors and properties of the solar system can clarify

aspects of evolution, and may aid in visualizing life on other planets

with different properties. Author

N86-21097"# National Aeronautics and Space Administration,

Washington, D.C,

THE HUMAN FACTOR: BIOMEDICINE IN THE MANNED SPACE

PROGRAM TO 1980

J. A. PITTS 1985 402 p refs In its History Series

(NASW-3213)

(NASA-SP-4213; NAS 1.21:4213; LC-85-21526) Avail: SOD HC

$23.00 as 033-000-00977-1; NTIS MF A01 CSCL 05E

The purpose of this publication is to provide NASA personnel,

NASA managers, and the biomedical and historical research

communities a well-documented, historical summary of the content

and organization of NASA's biomedical programs from Project

Mercury up to the Shuttle program. The publication includes not

only a major narrative portion, but appendixes and reference

notes. Author

52

AEROSPACE MEDICINE

Includes physiological factors; biological effects of radiation; and

effects of weightlessness on man and animals.

N77-30735"# National Aeronautics and Space Administration.

Lyndon B. Johnson Space Center, Houston, Tex.

THE APOLLO-SOYUZ TEST PROJECT: MEDICAL REPORT

A. E. NICOGOSSIAN, comp. Washington 1977 129 p refs

Original contains color illustrations

(NASA-SP-411) Avail: NTIS HC A07/MF A01 CSCL 06E

The results of the clinical aspects as well as the preflight and

postflight research studies that were performed on the astronauts

are presented. Because of the compromised postflight crew health

status, not all postflight research procedures could be

accomplished. This compromise was the result of the anomalous

entrance of toxic gas into the spacecraft cabin during the earth

landing sequence. Despite the exposure, the medical data collected

are of sufficient interest to warrant inclusion in this official ASTP

Medical Report. Author

N79-10728"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

HYPERTHERMIA AS AN ANTINEOPLASTIC TREATMENT

MODALITY

S. A. T. LONG, ed., J. SHAEFFER, ed. (Eastern Va. Med. School),

and A. M. EL-MAHDI, ed. (Eastern Va. Med. School) 1978 96

p refs Symp. held at Norfolk, Va, 28 Jan. 1978

(NASA-CP-2051; L-12082) Avail: NTIS HC A05/MF A01

CSCL 06E

CANCER, CONFERENCES, HYPERTHERMIA, RADIATION

THERAPY, RADIO FREQUENCY HEATING

170

N79-13686"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

PHYSIOLOGICAL RESPONSES OF WOMEN TO SIMULATED

WEIGHTLESSNESS: A REVIEW OF THE FIRST FEMALE

BED-REST STUDY

H. SANDLER and D. L. WINTER 1978 92 p refs

(NASA-SP-430) Avail: NTIS HC A05/MF A01 CSCL 06S

Subjects were exposed to centrifugation, to lower body negative

pressure (LBNP), and to exericse stress both before and after

bed rest. Areas studied were centrifugation tolerance, fluid

electrolyte changes and hematology, tolerance to LBNP, physical

working capacity, biochemistries, blood fibrinolytic activity, female

metabolic and hormonal responses, circadian alterations, and

gynecology. Results were compared with the responses observed

in similarly bed-rested male subjects. The bed-rested females

showed deconditioning responses similar to those of the males,

although with some differences. Results indicate that women are

capable of coping with exposure to weightlessness and, moreover,

that they may be more sensitive subjects for evaluating

countermeasures to weightlessness and developing criteria for

assessing applicants for shuttle voyages. G.G.

N80-15788"# National Aeronautics and Space Administration.

Lyndon B. Johnson Space Center, Houston, Tex.

THE PHYSIOLOGICAL BASIS FOR SPACECRAFT

ENVIRONMENTAL LIMITS

J. M. WALIGORA, comp. Washington Nov. 1979 229 p refs

(NASA-RP-1045; S-487) Avail: NTIS HC A11/MF A01 CSCL

06K

Limits for operational environments are discussed in terms of

acceptable physiological changes. The environmental factors

considered are pressure, contaminants, temperature, acceleration,

noise, rf radiation, and weightlessness. For individual titles, see

N80-15789 through N80-15795.

N83-16018"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

SPACE GERONTOLOGY

J. MIQUEL, ed. and A. C. ECONOMOS, ed. (Technology, Inc.,

Mountain View, Calif.) Washington Nov. 1982 t25 p refs

Workshop held at Moffett Field, Calif., 30-31 Jan. 1978

(NASA-CP-2248; A-8627; NAS 1.55:2248) Avail: NTIS HC

A06/MF A01 CSCL 06S

AEROSPACE MEDICINE, AGING (BIOLOGY),

BIOASTRONAUTICS, GERIATRICS, GERONTOLOGY

N83-25349"# National Aeronautics and Space Administration,

Washington, D.C.

SPACE PHYSIOLOGY AND MEDICINE

A. E. NICOGOSSIAN and J. F. PARKER, JR. (BioTechnology,

Inc.) 1982 33t p refs

(NASA-SP-447; NAS 1.2t:447; LC-82-23047) Avail: NTIS HC

$15.00/MF A01 CSCL06P

The state of knowledge in space physiology and medicine are

reviewed. Overviews of manned space flight, the space

environment, spaceflight systems and procedures, physiological

adaptation to space flight, health maintenance of space crew

members, and medical problems of space flight are presented.

S.L.

N86-23265" National Aeronautics and Space Administration,

Washington, D.C.

AEROSPACE MEDICINE AND BIOLOGY: A CUMULATIVE

INDEX TO THE 1985 ISSUES

Jan. 1986 291 p

(NASA-SP-7011(280); NAS 1.21:70011(280)) Avail: NTIS HC

A13 CSCL 06E

This publication is a cumulative index to the abstracts contained

in the Supplements 268 through 279 of Aerospace Medicine and

Biology: A Continuing Bibliography. It includes seven indexes -

subject, personal author, corporate source, foreign technology,

contract number, report number, and accession number. Author
N86-32088" National Aeronautics and Space Administration,

Washington, D.C.

AEROSPACE MEDICINE AND BIOLOGY: A CONTINUING

BIBLIOGRAPHY WITH INDEXES (SUPPLEMENT 288)

1986 69 p

(NASA-SP-7011(288); NAS 1.21:7011(288)) Avail: NTIS HC A05

CSCL 06E

This bibliography lists 190 reports, articles and other documents

introduced into the NASA scientific and technical information

system in August 1986. Author

53

BEHAVIORAL SCIENCES

Includes psychological factors; individual and group behavior; crew

training and evaluation; and psychiatric research.

N78-11696"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AN INVESTIGATION OF RIDE QUALITY RATING SCALES

T. K. DEMPSEY, G. D. COATES (Old Dominion Univ.), and J. D.

LEATHERWOOD Nov. 1977 48 p refs

(NASA-TP-1064) Avail: NTIS HC A03/MF A01 CSCL 05J

COMFORT, RIDING QUALITY, VIBRATION EFFECTS

N78-32717"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECT OF VIBRATION DURATION ON HUMAN

DISCOMFORT

S. A. CLEVENSON, T. K. DEMPSEY, and J_ D. LEATHERWOOD

Sep. 1978 26p refs

(NASA-TP-1283; L-12248) Avail: NTIS HC A03/MF A01

CSCL 05H

COMFORT, HUMAN FACTORS ENGINEERING, HUMAN

TOLERANCES, PASSENGERS, RANDOM VIBRATION,

VIBRATION EFFECTS

N79-19682"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AIRLINE PILOT SCAN PATTERNS DURING SIMULATED ILS

APPROACHES

A. A. SPADY, JR. Oct. 1978 72 p refs

(NASA-TP-1250; L-11989) Avail: NTIS HC A04/MF A01

CSCL 05J

AIRCRAFT PILOTS, FLIGHT SIMULATION, INSTRUMENT

LANDING SYSTEMS, VISUAL OBSERVATION

N79-22761"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

HUMAN DISCOMFORT RESPONSE TO NOISE COMBINED WITH

VERTICAL VIBRATION

J. D. LEATHERWOOD Apr. 1979 49 p refs

(NASA-TP-1374; L-12492) Avail: NTIS HC A03/MF A01

CSCL 05H

HUMAN TOLERANCES, NOISE TOLERANCE, RIDING

QUALITY, VERTICAL MOTION, VIBRATION EFFECTS

N79-23662"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

DISCOMFORT CRITERIA FOR SINGLE-AXIS VIBRATIONS

T. K. DEMPSEY, J. D. LEATHERWOOD, and S. A. CLEVENSON

May 1979 60p refs

(NASA-TP-1422; L-12681) Avail: NTIS HC A04/MF A01

CSCL 05H

HUMAN REACTIONS, HUMAN TOLERANCES, VIBRATION

53 BEHAVIORAL SCIENCES

N79-25753"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

OVERALL LOUDNESS OF STEADY SOUNDS ACCORDING TO

THEORY AND EXPERIMENT

W. L. HOWES Oct. 1979 150 p refs

(NASA-RP-1001; E-8342) Avail: NTIS MF A01; HC SOD

CSCL 05J

A mathematical theory for calculating the loudness of any steady

sound from information on its spectrum is constructed from physical

principles and psychological and physiological information on

mammalian auditory systems. The theory involves filtering,

channeling, squaring, half-wave rectification, and time average of

the signal. The theory accounts for critical bands for loudness,

audibility of sounds consisting of subliminal components, audible

beats, periodicity pitch, and pitch of the residue. These and other

pyschoacoustic phenomena are explained in terms of electrical

activity in the peripheral nervous system. Simple approximations

for loudness are derived from the more exact formulas. Loudness

predictions are compared with a wide variety of published loudness

judgement data with considerable success. Author

N79-33838"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

MODELS OF HUMAN OPERATORS IN VISION DEPENDENT

TASKS

M C. WALLER, ed. Oct. 1979 86 p refs Seminars held at

the Human Factors Soc. 1979 Ann. Meeting, Boston, 29 Oct. - 1

Nov. 1979; sponsored in part by Human Factors Soc. Visual

Performance Tech. Group

(NASA-CP-2103; L-13338) Avail: NTIS HC A05/MF A01

CSCL 05J

COMPUTERIZED SIMULATION, HUMAN FACTORS

ENGINEERING, MAN MACHINE SYSTEMS, OPERATOR

PERFORMANCE

N80-13769"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECT OF NOISE SPECTRA AND A LISTENING TASK UPON

PASSENGER ANNOYANCE IN A HELICOPTER INTERIOR NOISE

ENVIRONMENT

S. A. CLEVENSON and J. D. LEATHERWOOD Dec. 1979 26

p refs

(NASA-TP-1590; L-13233) Avail: NTIS HC A03/MF A01

CSCL 051

AIRCRAFT NOISE, AUDITORY PERCEPTION, HELICOPTERS,

HUMAN REACTIONS, NOISE TOLERANCE

N80-34099"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

EFFECTS OF MAGNIFICATION AND VISUAL

ACCOMMODATION ON AIMPOINT ESTIMATION IN SIMULATED

LANDINGS WITH REAL AND VIRTUAL IMAGE DISPLAYS

R. J. RANDLE, S. N. ROSCOE (New Mexico State Univ., Las

Cruces), and J. C. PETITT (California Univ., San Diego) Oct.

1980 29p refs

(NASA-TP-1635; A-8104) Avail: NTIS HC A03/MF A01 CSCL

051

IMAGING TECHNIQUES, LANDING SIMULATION, TRAINING

SIMULATORS, VIRTUAL PROPERTIES, VISUAL CONTROL,

VISUAL PERCEPTION

N81-23791"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECTS OF CURVED APPROACH PATHS AND ADVANCED

DISPLAYS ON PILOT SCAN PATTERNS

R. L. HARRIS, SR. and R. W. MIXON Washington May 1981

29 p refs

(NASA-TP-1846: L-14229) Avail: NTIS HC A03/MF A01

CSCL 051

COCKPITS, INSTRUMENT ORIENTATION, PILOT PERFORMANCE, SCANNING, SENSORIMOTOR PERFORMANCE, SENSORY PERCEPTION

171
53 BEHAVIORAL SCIENCES

N82-14804"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

INFLUENCE OF DISPLAY AND CONTROL COMPATIBILITY ON

PILOT-INDUCED OSCILLATIONS

M. C. WALLER, R. L. HARRIS, SR., and L. H. PERSON, JR.

Dec. 1981 40 p refs

(NASA-TP-1936; L-14364) Avail: NTIS HC A03/MF A01

CSCL 05t

COCKPIT SIMULATORS, OSCILLATIONS, TERMINAL

CONFIGURED VEHICLE PROGRAM, VERTICAL MOTION

SIMULATORS

Ne3-335311"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

THE WINDOW OF VISIBILITY: A PSYCHOLOGICAL THEORY

OF FIDELITY IN TIME-SAMPLED VISUAL MOTION DISPLAYS

A. B. WATSON, A. J. AHUMADA, JR., and J. E. FARRELL Aug.

1983 22p refs

(NASA-TP-2211; A-9270; NAS 1.60:2211) Avail: NTIS HC

A02/MF A01 CSCL 051

ACCURACY, COMPUTER GRAPHICS, DISPLAY DEVICES,

PSYCHOPHYSIOLOGY

N83-34579"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECT OF LOW-FREQUENCY TONES AND

TURBULENT-BOUNDARY-LAYER NOISE ON ANNOYANCE

K P. SHEPHERD (Bionetics Corp., Hampton, Va.), J. D.

LEATHERWOOD, and S. A. CLEVENSON Sep. 1983 27 p

refs

(NASA-TP-2202; L-15628; NAS 1.21:2202) Avail: NTIS HC

A03/MF A01 CSCL 05t

AERODYNAMIC NOISE, HUMAN FACTORS ENGINEERING,

LOW FREQUENCIES, SPECTRUM ANALYSIS, TURBULENT

BOUNDARY LAYER

N84-20155"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EVALUATION OF RIDE QUALITY PREDICTION METHODS FOR

HELICOPTER INTERIOR NOISE AND VIBRATION

ENVIRONMENTS

J. D. LEATHERWOOD, S. A. CLEVENSON, and D. D.

HOLLENBAUGH (USAAVSCOM Research and Technology Labs.)

Mar. 1984 47 p refs

(DA PROJ. 1L2-62209-AH-76)

(NASA-TP-2261 ; L-15661; NAS 1.60:2261; AVSCOM-TR-84-D-2)

Avail: NTIS HC A03/MF A01 CSCL 05H

AIRCRAFT NOISE, HELICOPTERS, PREDICTION ANALYSIS

TECHNIQUES, RIDING QUALITY

N84-22162"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

A USER-ORIENTED AND COMPUTERIZED MODEL FOR

ESTIMATING VEHICLE RIDE QUALITY

J. D. LEATHERWOOD and L. M. BARKER (System Development

Corp., Hampton, Va.) Apr 1984 45 p refs

(NASA-TPo2299; L-15745; NAS 1.60:2299) Avail: NTIS HC

A03/MF A01 CSCL 05H

COMFORT, COMPUTER PROGRAMS, HUMAN REACTIONS,

PHYSIOLOGICAL RESPONSES, RIDING QUALITY

N86-27920"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ANALYTICAL TECHNIQUES OF PILOT SCANNING BEHAVIOR

AND THEIR APPLICATION

R. L. HARRIS, SR., B. J. GLOVER (PRC Kentron, Inc., Hampton,

Va.), and A. A. SPADY, JR. Jul. 1986 46 p refs

(NASA-TP-2525; L-t5995; NAS 1.60:2525) Avail: NTIS HC

A03/MF A01 CSCL 051

DWELL, HISTOGRAMS, HUMAN FACTORS ENGINEERING,

OCULOMETERS, PILOT PERFORMANCE, PILOT TRAINING,

REAL TIME OPERATION, WORKLOADS (PSYCHOPHYSlOLOGY)

172

54

MAN/SYSTEM TECHNOLOGY AND LIFE

SUPPORT

Includes human engineering; biotechnology; and space suits and

protective clothing.

N77-27710"# Virginia Univ., Charlottesville. Dept. of Engineering

Science and Systems.

PROCEEDINGS AND FINDINGS OF THE 1976 WORKSHOP ON

RIDE QUALITY

A. R. KUHLTHAU, ed. 20 Dec. 1976 86 p refs Proc. held

at Fairlee, Vt., 13-15 Oct. 1976 Sponsored by NASA

(DOT-AS-60060)

(NASA-CP-2006; DOT-TST-77-38) Avail: NTIS HC A05/MF A01

CSCL 05H

HUMAN REACTIONS, RIDING QUALITY, TRANSFER

FUNCTIONS, TRANSPORT VEHICLES

N78-11705"# Transportation Systems Center, Cambridge,

Mass.

SUMMARY REPORT: WORKSHOP ON VEHICLE RIDE QUALITY

Final Report, 11-15 Aug, 1975

A. R. KULTHAU, ed. (Virginia Univ.) and A. W. WICHANSKY, ed.

Jul. 1977 167 p refs Workshop held at Williamsburg, Va.,

13-15 Aug. 1975

(NGR-47-005-181)

(NASA-CP-2013; DOT-TSC-OST-77-44) Avail: NTIS HC

A08/MF A01 CSCL 05H

MOTOR VEHICLES, QUALITY CONTROL, URBAN

TRANSPORTATION

N78-31739"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

A PILOT EVALUATION OF TWO G-SEAT CUEING SCHEMES

T. W. SHOWALTER Aug. 1978 34 p refs

(NASA-TP-1255; A-7390) Avail: NTIS HC A03/MF A01 CSCL

05H

FLIGHT SIMULATION, PERFORMANCE TESTS, TEST

PILOTS

N78-31740"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

DISPOSAL OF RADIOACTIVE IODINE IN SPACE

R. E. BURNS and J. G. DEFIELD Aug. 1978 40 p refs

(NASA-TP-1313; M-260) Avail: NTIS HC A03/MF A01 CSCL

06T

IODINE, RADIOACTIVE WASTES, SPACE TRANSPORTATION

SYSTEM, WASTE DISPOSAL

N79-11734"# Webb Associates, Yellow Springs, Ohio.

ANTHROPOMETRIC SOURCE BOOK. VOLUME 1:

ANTHROPOMETRY FOR DESIGNERS

E. CHURCHILL, comp., L. L. LAUBACH, comp., J. T. MCCONVILLE,

comp, and I. TEBBETTS, comp. Houston, Tex. NASA Jul.

1978 603 p refs

(NASA-RP-1024; S-479-VOL-1) Avail: NTIS HC A99/MF A01

CSCL 05H

All the basic areas of anthropometry and its applications to

the design of clothing, equipment, and workspaces for manned

space flight are presented. For individual titles, see N79-11735

through N79-11743.

N79-13711"# Webb Associates, Yellow Springs, Ohio.

ANTHROPOMETRIC SOURCE BOOK. VOLUME 2: A

HANDBOOK OF ANTHROPOMETRIC DATA

Jut. 1978 428 p refs For Volume 1 see N79-11734

(NASA-RP-1024-VOL-2; S-479-VOL-2) Avail: NTIS HC A19/MF

A01 CSCL 05H

Volume 2 contains data resulting from surveys of 61 military

and civilian populations of both sexes from the U.S., Europe, and
54 MAN/SYSTEM TECHNOLOGY AND LIFE SUPPORT

Asia. Some 295 measured variables are defined and illustrated.

Author

N79-13712"# Webb Associates, Yellow Springs, Ohio.

ANTHROPOMETRIC SOURCE BOOK. VOLUME 3: ANNOTATED

BIBLIOGRAPHY OF ANTHROPOMETRY

Jul. 1978 130p refs For volume 1 see N79-11734

(NASA-RP-1024-VOL-3; S-479-VOL-3) Avail: NTIS HC A07/MF

A01 CSCL 05H

Volume 3 is an annotated bibliography covering a broad

spectrum of topics relevant to applied physical anthropology with

emphasis on anthropometry and its applications in sizing and

design. Author

N79-15588"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

THE 14TH ANNUAL CONFERENCE ON MANUAL CONTROL

Nov. 1978 692 p refs Conf. held at Univ. of Southern Calif.,

Los Angeles, 25-27 Apr. 1978

(NASA-CP-2060; A-7615) Avail: NTIS HC A99/MF A01 CSCL

05H

AEROSPACE MEDICINE, CONFERENCES, HUMAN

REACTIONS, MAN MACHINE SYSTEMS, MANUAL CONTROL,

OPERATOR PERFORMANCE

N80-15821"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

SOME HUMAN FACTORS ISSUES IN THE DEVELOPMENT AND

EVALUATION OF COCKPIT ALERTING AND WARNING

SYSTEMS

R. J. RANDLE, JR., W. E. LARSEN, and D. H. WILLIAMS

Washington Jan. 1980 65 p refs

(NASA-RP-1055; A-7696) Avail: NTIS HC A04/MF A01 CSCL

05H

A set of general guidelines for evaluating a newly developed

cockpit alerting and warning system in terms of human factors

issues are provided. Although the discussion centers around a

general methodology, it is made specifically to the issues involved

in alerting systems. An overall statement of the current operational

problem is presented. Human factors problems with reference to

existing alerting and warning systems are described. The

methodology for proceeding through system development to system

test is discussed. The differences between traditional human factors

laboratory evaluations and those required for evaluation of complex

man-machine systems under development are emphasized.

Performance evaluation in the alerting and warning subsystem using

a hypothetical sample system is explained. R.C.T.

N80-26039"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

HEAD-UP TRANSITION BEHAVIOR OF PILOTS DURING

SIMULATED LOW-VISIBILITY APPROACHES

R. F. HAINES Jun. 1980 35 p refs

(NASA-TP-1618; A-8057) Avail: NTIS HC A03/MF A01 CSCL

05H

APPROACH CONTROL, HUMAN FACTORS ENGINEERING,

LOW VISIBILITY, MAN MACHINE SYSTEMS, PILOT

PERFORMANCE, VISUAL PERCEPTION

N81-13635"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

HEAD-UP TRANSITION BEHAVIOR OF PILOTS WITH AND

WITHOUT HEAD-UP DISPLAY IN SIMULATED LOW-VISIBILITY

APPROACHES

R. F. HAINES, E. FISCHER, and T. A. PRICE Dec. 1980 37 p

refs Prepared in cooperation with San Jose Univ. Foundation,

Calif.

(NASA-TP-1720; A-8296; HUD-10) Avail: NTIS HC A03/MF

A01 CSCL 05H

APPROACH CONTROL, FLIGHT SIMULATION, HEAD-UP

DISPLAYS, HUMAN FACTORS ENGINEERING, PILOT

PERFORMANCE

N81-13636"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

COGNITIVE ISSUES IN HEAD-UP DISPLAYS

E. FISCHER and R. F. HAINES (San Jose State Univ,, Calif.)

Dec, 1980 32p refs

(NASA-TP-1711; A-8246) Avail: NTIS HC A03/MF A0t CSCL

01D

APPROACH CONTROL, COGNITION, FLIGHT INSTRUMENTS,

HEAD-UP DISPLAYS, PILOT PERFORMANCE

N81-17711"#

MAGNITUDE OF VISUAL ACCOMMODATION TO A HEAD-UP

DISPLAY

E. F. LEiTNER and R. F. HAINES Feb. 1981 12 p refs

(NASA-TP-1796; A-8379; HUD-15) Avail: NTIS HC A02/MF

A01 CSCL 01D

ACCOMMODATION, HEAD-UP DISPLAYS, HUMAN FACTORS

ENGINEERING, VISUAL AIDS

N82-24834"# Wisconsin Univ,, Madison. Dept. of Horticulture.

CONTROLLED ECOLOGICAL LIFE SUPPORT SYSTEM: USE

OF HIGHER PLANTS

T, W. TIBBITS and D. K. ALFORD (Metropolitan State Coll.) May

1982 88 p refs Proc. of NASA Workshop held at Chicago,

Nov. 1979 and at Moffett Field, Calif., Mar. 1980

(NSG-2405)

(NASA-CP-2231; NAS 1.55:2231) Avail: NTIS HC A05/MF A01

CSCL 06K

CLOSED ECOLOGICAL SYSTEMS, LIFE SUPPORT SYSTEMS,

PLANTS (BOTANY), SPACE FLIGHT FEEDING

N82-24835"# Metrics, Inc., Atlanta, Ca.

CONTROLLED ECOLOGICAL LIFE SUPPORT SYSTEM:

RESEARCH AND DEVELOPMENT GUIDELINES

R. M. MASON, ed. and J. L. CARDEN, ed. (Georgia Inst. of

Technology) May 1982 99 p refs Proceedings of NASA

Workshop held at Moffett Field, Calif., 9-12, 1979

(NSG-2323)

(NASA-CP-2232; NAS 1.55:2323) Avail: NTIS HC A05/MF A01

CSCL 06K

CLOSED ECOLOGICAL SYSTEMS, LIFE SUPPORT SYSTEMS,

PLANTS (BOTANY), SPACE FLIGHT FEEDING

N82-24836"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

CONTROLLED ECOLOGICAL LIFE SUPPORT SYSTEM

BIOLOGICAL PROBLEMS

B. MOORE, III, ed. (New Hampshire Univ.) and R. D. MACELROY,

ed. 1982 42p refs

(NASA-CP-2233; A-8842; NAS 1.55:2233) Avail: NTIS HC

A03/MF A01 CSCL 06K

BIOLOGICAL EFFECTS, CLOSED ECOLOGICAL SYSTEMS,

PLANTS (BOTANY), WASTE TREATMENT

N83-18238"# National Aeronautics and Space Administration,

Goddard Space Flight Center, Greenbelt, Md.

HUMAN FACTORS CONSIDERATIONS IN SYSTEM DESIGN

C. M. MITCHELL, ed. (George Mason Univ.), P. M. VANBALEN,

ed. (George Mason Univ.), and K. L. MOE, ed. Jan. 1983 381

p refs Symp. held in Greenbelt, Md. and College Park, Md.,

25-26 May 1982

(NAS5-26952)

(NASA-CP-2246; NAS 1.55:2246) Avail: NTIS HC A17/MF A01

CSCL 05H

AUTOMATIC CONTROL, COMMAND AND CONTROL,

COMPUTER SYSTEMS DESIGN, CONFERENCES, DATA

PROCESSING, DESIGN, DISPLAY DEVICES, HUMAN FACTORS

ENGINEERING, INFORMATION MANAGEMENT

173
54 MAN/SYSTEMTECHNOLOGYANDLIFESUPPORT

N83-30016"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

CONTROLLED ECOLOGICAL LIFE SUPPORT SYSTEM. FIRST

PRINCIPAL INVESTIGATORS MEETING

B. MOORE, III, ed. (New Hampshire Univ., Durham), R. A.

WHARTON, JR., ed. (New Hampshire Univ., Durham), and R. D.

MACELROY, ed. Dec. 1982 90 p refs Meeting held in

Durham, N.H., 3-6 May 1981

(NCC2-27)

(NASA-CP-2247; A-9055; NAS t.55:2247; CELSS-19) Avail:

NTIS HC A05/MF A01 CSCL 06C

CLOSED ECOLOGICAL SYSTEMS, CONFERENCES, GRAINS

(FOOD), LIFE SUPPORT SYSTEMS, WASTE TREATMENT

N84-29465"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

PHYSIOLOGICAL, PSYCHOLOGICAL, AND SOCIAL EFFECTS

OF NOISE

K. D. KRYTER (Acousis Co., Bodega Bay, Calif.) Jul. 1984

654 p refs

(NASl-15435)

(NASA-RP-1115; L-15612; NAS 1.61:1115) Avail: NTIS HC

A99/MF A01 CSCL 20A

The physiological, and behavioral effects of noise on man are

investigated. Basic parameters such as definitions of noise,

measuring techniques of noise, and the physiology of the ear are

presented prior to the development of topics on hearing loss,

speech communication in noise, social effects of noise, and the

health effects of noise pollution. Recommendations for the

assessment and subsequent control of noise is included. For

individual titles, see N84-29466 through N84-29477.

N84-29479"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

HUMAN EXPOSURE IN LOW EARTH ORBIT

J. W. WILSON and F. CUCINOTTA (Old Dominion Univ.) Aug.

1984 22p refs

(NASA-TP-2344; L-15803; NAS 1.60:2344) Avail: NTIS HC

A02/MF A01 CSCL 06R

HEALTH PHYSICS, HUMAN PERFORMANCE, RADIATION

DOSAGE, RADIATION EFFECTS, RADIATION SHIELDING,

TOLERANCES (PHYSIOLOGY)

N85-14487"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

TWENTIETH ANNUAL CONFERENCE ON MANUAL CONTROL,

VOLUME 1

S. G. HART, comp. and E. J. HARTZELL, comp. Sep. 1984

653 p refs Conf. held at Moffett Field, Calif., 12-14 Jun. 1984

2 Vol.

(NASA-CP-2341 -VOL-1 ; A-9879-VOL-1; NAS 1.55:2341 -VOL-1 )

Avail: NTIS HC A99/MF A01 CSCL 05H

BIODYNAMICS, CONFERENCES, HUMAN FACTORS

ENGINEERING, MAN MACHINE SYSTEMS, MANUAL CONTROL,

PERCEPTION

N85-24733"# National Aeronautics and Space Administration.

Lyndon B. Johnson Space Center, Houston, Tex.

FOOD SERVICE AND NUTRITION FOR THE SPACE STATION

R. L. SAUER, ed. Apr. 1985 99 p refs Workshop held in

Houston, Tex., 10-11 Apr. 1984

(NASA-CP-2370; S-541; NAS 1.55:2370) Avail: NTIS HC

A05/MF A01 CSCL 06H

CONSUMABLES (SPACECREW SUPPLIES), FOOD

PROCESSING, NUTRITION, SPACE FLIGHT FEEDING

N85-29531"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

CONTROLLED ECOLOGICAL LIFE SUPPORT SYSTEM, LIFE

SUPPORT SYSTEMS IN SPACE TRAVEL

R. D. MACELROY, ed., D. T. SMERNOFF, ed. (New Hampshire

Univ., Durham), and H. P. KLEIN, ed. (Santa Clara Univ., Calif.)

Jun. 1985 74 p refs Proc. of the 25th COSPAR Meeting,

held in Graz, Jul. 1984

(NASA-CP-2378; A-85190; NAS 1.55:2378) Avail: NTIS HC

A04/MF A01 CSCL 06K

CELLS (BIOLOGY), CLOSED ECOLOGICAL SYSTEMS,

CONFERENCES, CONTROLLED ATMOSPHERES, LIFE

SUPPORT SYSTEMS

N85-32772"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

LIVING ALOFT: HUMAN REQUIREMENTS FOR EXTENDED

SPACEFLIGHT

M. M. CONNORS, A. A. HARRISON (California Univ., Davis), and

F. R. AKINS (Santa Clara Univ., Calif.) Washington 1985 426

p refs Original contains color illustrations

(NASA-SP-483; NAS 1.21:483) Avail: NTIS HC A19/MF A01;

SOD HC $14.00 as 033-000-00949-6 CSCL 06K

Human psychological and social adjustment to space is

investigated. Studies and experiences bearing on human

performance capability, psychological well being, and social

organization, as they relate to space, were identified and assessed,

and suggestions offered as to where further research could ease

the Earth/space transition. Special emphasis was given to the

variables of crew size, crew diversity, and mission duration, all of

which can be expected to increase in future spaceflight. By

providing a conceptual framework in which issues and related

information can be integrated, the hope is to aid in discovering

those conditions under which future space travelers can flourish.

Author

N86-26836"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

BASELINE EXPERIMENTS IN TELEOPERATOR CONTROL

W. W. HANKINS, III and R. W. MIXON JuL 1986 65 p

(NASA-TP-2547; L-15963; NAS 1.60:2547) Avail: NTIS HC

A04/MF A01 CSCL 05H

AUTOMATIC CONTROL, HUMAN FACTORS ENGINEERING,

MAN MACHINE SYSTEMS, MANIPULATORS, PROVING,

TELEOPERATORS

N85-14535"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

TWENTIETH ANNUAL CONFERENCE ON MANUAL CONTROL,

VOLUME 2

S. G. HART, comp. and E. J. HARTZELL, comp. Sep. 1984

423 p refs Conf. held at Moffett Field, Calif., 12-14 Jun. 1984

2 VoI.

(NASA-CP-2341-VOL-2; A-9879-VOL-2; NAS 1.55:2341-VOL-2)

Avail: NTIS HC A18/MF A01 CSCL 05H

CONFERENCES, FLIGHT CONTROL, HUMAN FACTORS

ENGINEERING, MAN MACHINE SYSTEMS, MANUAL CONTROL,

PILOT PERFORMANCE, TASKS, WORKLOADS (PSYCHOPHYSIOLOGY)

N86-32976"# National Aeronautics and Space Admini_ration.

Ames Research Center, Moffett Field, Calif.

TWENTY-FIRST ANNUAL CONFERENCE ON MANUAL

CONTROL

R. A. MILLER, comp. (Ohio State Univ., Columbus.) and R. J.

JAGACINSKI, comp. May 1986 504 p Conference held in

Columbus, Ohio, 17-19 Jun. 1985

(NAG2-195)

(NASA-CP-2428; A-86218; NAS 1.55:2428) Avail: NTIS HC

A22/MF A01 CSCL 05H

DECISION MAKING, HUMAN FACTORS ENGINEERING,

HUMAN PERFORMANCE, MAN MACHINE SYSTEMS, MANUAL

CONTROL, WORKLOADS (PSYCHOPHYSIOLOGY)

174
59 MATHEMATICAL AND COMPUTER SCIENCES (GENERAL)

55

SPACE BIOLOGY

Includes exobiology; planetary biology; and extraterrestrial life.

N77-12718"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

ON THE HABITABILITY OF MARS: AN APPROACH TO

PLANETARY ECOSYNTHESIS

M. M. AVERNER, ed. and R. D. MACELROY, ed. Washington

1976 114p refs

(NASA-SP-414) Avail: NTIS HC A06/MF A01 CSCL 06F

The possibility of utilizing Mars as a habitat for terrestrial life,

including man, is examined. Available data, assumptions, and

speculations on the climate, physical state, and chemical inventory

of Mars are reviewed and compared with the known requirements

and environmental limits of terrestrial life. No fundamental,

insuperable limitation of the ability of Mars to support a terrestrial

ecology is identified. The lack of an oxygen-containing atmosphere

would prevent the unaided habitation of Mars by man. The present

strong ultraviolet surface irradiation is an additional major barrier.

The creation of ar_ adequate oxygen and ozone-containing

atmosphere on Mars may be feasible through the use of

photosynthetic organisms. The time needed to generate such an

atmosphere, however, might be several millions of years. This

period might be drastically reduced by the synthesis of novel,

Mars-adapted, oxygen producing photosynthetic strains by

techniques of genetic engineering, and modifying the present

Martian climate by melting of the Martian polar caps and

concomitant advective and greenhouse heating effects. Author

N78-18771"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

THE SEARCH FOR EXTRATERRESTRIAL INTELLIGENCE

(SETI)

P. MORRISON, ed. (MIT, Cambridge), J. BILLINGHAM, ed., and

J. WOLFE, ed. 1977 289 p refs

(NASA-SP-419) Avail: NTIS MF A01; SOD HC $4.50 CSCL

06C

A bibliography of reports concerning the Search for

Extraterrestrial Intelligence is presented. Cosmic evolution, space

communication, and technological advances are discussed along

with search strategies and search systems. J.C.S.

N82-20884"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

LIFE IN THE UNIVERSE

J. BILLINGHAM, ed. Jan. 1982 465 p refs Proc. of conf.

held at Moffett Field, Calif., 19-20 Jun. 1979 Analytic primary

previously announced in IAA as A82-22976; subsidiaries previously

announced as A82-22977 through A82-23004

(NASA-CP-2156; A-8242; NAS 1.55:2156; LC-81-22350) Avail:

NTIS MF A01; SOD HC $8.00 as SN 033-000-0084-4 CSCL

06F

BIOLOGICAL EVOLUTION, CHEMICAL EVOLUTION,

EXOBIOLOGY, EXTRATERRESTRIAL LIFE, UNIVERSE

N85-28562"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

THE COSMIC HISTORY OF THE BIOGENIC ELEMENTS AND

COMPOUNDS

J. A. WOOD (Harvard-Smithsonian Center for Astrophysics) and

S. CHANG 1985 87p

(NASA-SP-476; NAS 1.21:476) Avail: NTIS MF A01; SOD HC

$3.50 as 033-000-00948-8 CSCL 01C

An overview of the cosmic history of biogenic elements is

presented. G.LC.

N85-32777"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

SEARCH FOR THE UNIVERSAL ANCESTORS

H. HARTMAN, ed. (MIT), J. G. LAWLESS, ed., and P. MORRISON,

ed. (MIT) Jul. 1985 145 p refs

(NASA-SP-477; A-8646; NAS 1.21:477) Avail: NTIS MF A01;

SOD HC $3.75 as 033-000-009-3-4 CSCL 06C

By its nature, the study of the origins of life is multidisciplinary,

requiring contributions from astronomers, biologists, chemists,

geologists, physicists, and many others. Partial answers are

provided to many questions about organic chemical evolution and

the origin of life. It is observed that the gaps in our knowledge

concerning the steps from the nonliving to the living are numerous.

Among these gaps are: (1) a solar system formation with its

accumulation of raw materials; (2) the synthesis of the life forming

monomers, such as the amino acids, nucleotides, and lipids; (3)

the condensation of these monomers into useful polymers, such

as proteins and nucleic acids; (4) the sequestering of these

materials into droplets of proteinoid or membrane-like structures;

and (5) the development of a chemical memory (the genetic code)

to pass on to the progeny the information acquired. Author

N86-26844"# National Aeronautics and Space Administration,

Washington, D.C.

SECOND SYMPOSIUM ON CHEMICAL EVOLUTION AND THE

ORIGIN OF LIFE

D. L. DEVINCENZI, ed. and P. A. DUFOUR, ed. (George

Washington Univ., Washington, D.C.) May 1986 128 p refs

Symposium held at Moffett Field, Calif., 23-26 Jul. 1985

(NASW-3165)

(NASA-CP-2425; NAS 1.55:2425) Avail: NTIS HC A07/MF A01

CSCL 06C

BIOLOGICAL EVOLUTION, CHEMICAL EVOLUTION,

EXOBIOLOGY, PLANETARY EVOLUTION, PROJECT SETI

59

MATHEMATICAL AND COMPUTER SCIENCES

(GENERAL)

N84-22178"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

SETI SCIENCE WORKING GROUP REPORT

F. DRAKE (Cornell Univ.), J. H. WOLFE (San Francisco Univ.),

and C. L. SEEGER (San Francisco Univ.) Jan. 1984 119 p

refs

(NASA-TP-2244; A-9326; NAS 1.60:2244) Avail: NTIS HC

A07/MF A01 CSCL 05K

ANTENNAS, BROADBAND, ELECTROMAGNETIC SPECTRA,

PROJECT SETI, RADIO ASTRONOMY, SIGNAL PROCESSING,

SPECTRUM ANALYSIS

N77-22808"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

SYSTEMS RELIABILITY ISSUES FOR FUTURE AIRCRAFT

1975 212 p refs Workshop held at Cambridge, Mass., 18-20

Aug. 1975

(Contract NSG-2076)

iNASA-(.;P-U03) Avail: NTIS HC A10/MF A01 CSCL 12B

AIRCRAFT DESIGN, AIRCRAFT RELIABILITY,

CONFERENCES, RELIABILITY ENGINEERING, SYSTEMS

ENGINEERING

175
59 MATHEMATICAL AND COMPUTER SCIENCES (GENERAL)

N77-28750"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

PROCEEDINGS OF THE 1977 MACSYMA USERS' CONFERENCE

(NASA)

1977 596 p Conf. held at Calif. Univ., Berkeley, 27 - 29 Jul.

1977; sponsored by NASA, MIT and Calif. Univ., Berkeley

(NASA-CP-2012) Avail: NTIS HC A25/MF A01 CSCL 09B

COMPUTER PROGRAMS, CONFERENCES

N78-19778"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

FUTURE COMPUTER REQUIREMENTS FOR COMPUTATIONAL

AERODYNAMICS

Feb. 1978 515 p refs Proceedings held at Moffett Field,

Calif., 4-6 Oct. 1977

(NASA-CP-2032; A-7291) Avail: NTIS HC A22/MF A01 CSCL

09B

AERODYNAMICS, COMPUTER SYSTEMS DESIGN,

CONFERENCES, NUMERICAL ANALYSIS, NUMERICAL FLOW

VISUALIZATION, TECHNOLOGICAL FORECASTING

N81-15702"# Duke Univ., Durham, N. C. Dept. of Computer

Sciences.

VALIDATION METHODS RESEARCH FOR FAULT-TOLERANT

AVIONICS AND CONTROL SYSTEMS SUB-WORKING GROUP

MEETING. CARE 3 PEER REVIEW

K. S. TRIVEDI, ed. and J. B. CLARY, ed (Research Triangle Inst.,

Research Triangle Park, N.C.) Dec. 1980 30 p refs Meeting

held at Research Triangle Park, N.C., 15-16 Sep. 1980

(NAG1-70)

(NASA-CP-2167; L-14215) Avail: NTIS HC A03/MF A01

CSCL 12A

AVIONICS, FAULT TOLERANCE, FLIGHT CONTROL,

RELIABILITY ANALYSIS

N81-21775"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

MARKING PARTS TO AID ROBOT VISION

J. W. BALES (Tuskegee Inst., Ala.) and L. K. BARKER Apr.

1981 36 p

(NASA-TP-1819; L-14055) Avail: NTIS HC AO3/MF A0t

CSCL 12A

ARTIFICIAL INTELLIGENCE, AUTOMATA THEORY, MARKING,

PATTERN RECOGNITION, ROBOTS

N79-33855"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

COMPUTER-AUTOMATED OPPONENT FOR MANNED

AIR-TO-AIR COMBAT SIMULATIONS

W. W. HANKINS, III Sep. 1979 153 p refs

(NASA-TP-1518; L-12768) Avail: NTIS HC A08/MF A01

CSCL 12B

COMBAT, COMPUTERIZED SIMULATION, FIGHTER

AIRCRAFT

NS0-12741"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

VALIDATION METHODS FOR FAULT-TOLERANT AVIONICS

AND CONTROL SYSTEMS, WORKING GROUP MEETING 1

Washington Dec. t979 112 p refs Workshop held at

Hampton, Va., 12-14 Mar. 1979

(NASA-CP-2114; L-13436) Avail: NTIS HC A06/MF A01

CSCL 12A

AVIONICS, COMPUTER SYSTEMS DESIGN, FLIGHT

CONTROL

N80-23008"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

VALIDATION METHODS RESEARCH FOR FAULT-TOLERANT

AVIONICS AND CONTROL SYSTEMS: WORKING GROUP

MEETING, 2

J. W. GAULT, ed , K. S. TRIVEDI, ed., and J. B. CLARY, ed.

1980 105 p Meeting held at Hampton, Va. 3-4 Oct. 1979

(NASA-CP-2130; L-13716) Avail: NTIS HC A06/MF A01

CSCL 12A

AIRBORNE EQUIPMENT, AUTOMATIC CONTROL,

COMPUTER SYSTEMS DESIGN, CONTROL UNITS

(COMPUTERS), ERROR DETECTION CODES, SYSTEM

FAILURES

N81-12744"# National Aeronautics and Space Administration.

Dryden (Hugh L.) Flight Research Center, Edwards, Calif.

USER'S MANUAL FOR MMLE3, A GENERAL FORTRAN

PROGRAM FOR MAXIMUM LIKELIHOOD PARAMETER

ESTIMATION

R. E. MAINE and K. W. ILIFF Nov. 1980 90 p refs

(NASA-TP-1563; H-1084) Avail: NTIS HC A05/MF A01 CSCL

09B

COMPUTER PROGRAMS, FLIGHT TESTS, FORTRAN,

MAXIMUM LIKELIHOOD ESTIMATES, PARAMETER

IDENTIFICATION, USER MANUALS (COMPUTER PROGRAMS)

N81-27813"# National Aeronautics and Space Administration.

Dryden (Hugh L.) Flight Research Center, Edwards, Calif.

PROGRAMMER'S MANUAL FOR MMLE3, A GENERAL

FORTRAN PROGRAM FOR MAXIMUM LIKELIHOOD

PARAMETER ESTIMATION

R. E. MAINE Jun. 1981 118 p refs Document includes a

microfiche supplement

(NASA-TP-1690; H-1105) Avail: NTIS HC A06/MF A01 CSCL

09B

COMPUTER PROGRAMS, FLOW CHARTS, FORTRAN,

MANUALS, MAXIMUM LIKELIHOOD ESTIMATES

N82-21907*# National Aeronautics and Space Administration.

Dryden (Hugh L.) Flight Research Center, Edwards, Calif.

A GENERAL SOLUTION TO THE HIDDEN-LINE PROBLEM

D. R. HEDGLEY, JR. Mar. 1982 17 p refs

(NASA-RP-1085; H-1162; NAS 1.61:1085) Avail: NTIS HC

A02/MF A01 CSCL 12A

The requirements for computer-generated perspective

projections of three dimensional objects has escalated. A general

solution was developed. The theoretical solution to this problem

is presented. The method is very efficient as it minimizes the

selection of points and comparison of line segments and hence

avoids the devastation of square-law growth. Author

N82-26996"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

COMPUTER SCIENCE RESEARCH AT LANGLEY

S. J. VOIGT, ed. Jun. 1982 68 p Workshop held at Hampton,

Va., 2-5 Nov. 1981

(NASA-CP-2236; NAS 1.55:2236; L-15418) Avail: NTIS HC

A04/MF A01 CSCL 09B

COMPUTER GRAPHICS, COMPUTER TECHNIQUES,

CONFERENCES, RESEARCH, USER REQUIREMENTS

N82-29904"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

GLOBAL DIFFERENTIAL GEOMETRY: AN INTRODUCTION FOR

CONTROL ENGINEERS

B. F. DOOLIN (Computer Services Corp.) and C. F. MARTIN (Case

Western Reserve Univ.) Jun. 1982 69 p refs

(NASA-RP-1091; NAS 1.61:1091) Avail: NTIS HC A04/MF A01

CSCL 12A

The basic concepts and terminology of modern global

differential geometry are discussed as an introduction to the Lie

theory of differential equations and to the role of Grassmannians

in control systems analysis. To reach these topics, the fundamental

notions of manifolds, tangent spaces, vector fields, and Lie algebras

are discussed and exemplified. An appendix reviews such concepts

176
needed for vector calculus as open and closed sets, compactness,

continuity, and derivative. Although the content is mathematical,

this is not a mathematical treatise but rather a text for engineers

to understand geometric and nonlinear control. J.M.S.

N84-22179"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

COMPUTER-AIDED GEOMETRY MODELING

J. N. SHOOSMITH, comp. and R. E. FULTON, comp.

Washington Mar. 1984 387 p refs Syrup. held in Hampton,

Va., 20-22 Apr. 1983

(NASA-CP-2272; L-15618; NAS 1.55:2272) Avail: NTIS HC

A17/MF A01 CSCL 12A

COMPUTER AIDED DESIGN, COMPUTER GRAPHICS,

CONFERENCES, COORDINATES, GEOMETRY, MATHEMATICAL

MODELS, SHAPES, SURFACES

N84-24114"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

GEOMETRIC INTERPRETATIONS OF THE DISCRETE FOURIER

TRANSFORM (DFT)

C. W. CAMPBELL May 1984 16 p refs

(NASA-TP-2332; NAS 1.60:2332) Avail: NTIS HC A02/MF A01

CSCL 12A

DIGITAL TECHNIQUES, FAST FOURIER TRANSFORMATIONS, INTEGRAL TRANSFORMATIONS, POWER SPECTRA,

TRANSFORMATIONS (MATHEMATICS)

N85-23305"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

AN INTEGRAL REPRESENTATION OF THE GENERALIZED

EULER-MASCHERONI CONSTANTS

O. R. AINSWORTH (Alabama Univ., Tuscaloosa) and L. W.

HOWELL Apr. 1985 14 p refs

(NASA-TP-2456; NAS 1.80:2456) Avail: NTIS HC AO2/MF A01

CSCL 12A

CONSTANTS, INTEGRALS, SERIES (MATHEMATICS)

N85-28563"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

COMPUTATIONAL GEOMETRY AND COMPUTER-AIDED

DESIGN Extended Abstracts

T. H. FAY, comp. (Univ. of Southern Mississippi, Hattiesburg) and

J. N. SHOOSMITH, comp. Washington 3un. 1985 117 p

refs Conf. held in New Orleans, 5-8 Jun. 1985; sponsored in

cooperation with Univ. of Southern Mississippi

(NASA-CP-2379; L-16003; NAS 1.55:2379) Avail NTIS HC

A06/MF A01 CSCL 12A

COMPUTATIONAL GRIDS, COMPUTER AIDED DESIGN,

GEOMETRY

N85-31839"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

INTERSECTION OF THREE-DIMENSIONAL GEOMETRIC

SURFACES

V. K. CRISP, J. J. REHDER, and J. L. SCHWING (Old Dominion

Univ.) Jul. 1985 33 p refs

(NASA-TP-2454; L-15911; NAS 1.60:2454) Avail: NTIS HC

A03/MF A01 CSCL 12A

COMPUTER AIDED DESIGN, COMPUTER GRAPHICS,

DRAWINGS, INTERSECTIONS

N86-23282"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

INTERACTIVE ALGEBRAIC GRID-GENERATION TECHNIQUE

R. E. SMITH and M. R. WIESE (Computer Sciences Corp.,

Hampton, Va.) Mar. 1986 40 p refs

(NASA-TP-2533; L-16019; NAS 1.60:2533) Avail NTIS HC

A03/MF A01 CSCL 12A

COMPUTATIONAL FLUID DYNAMICS, COMPUTER

GRAPHICS, FINITE DIFFERENCE THEORY, PROBLEM

SOLVING

60 COMPUTER OPERATIONS AND HARDWARE

60

COMPUTER OPERATIONS AND HARDWARE

Includes hardware for computer graphics, firmware, and data

processing.

N77-33868"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

FAULT TOLERANT COMPUTING: A PREAMBLE FOR

ASSURING VIABILITY OF LARGE COMPUTER SYSTEMS

R. S. LIM Oct. 1977 25 p refs

(NASA.TP-1067; A-7072) Avail: NTIS HC A02/MF A01 CSCL

09B

COMPUTER NETWORKS, ERROR CORRECTING CODES,

ERROR DETECTION CODES

N78-74659" National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

THE MSFC/UAH DATA MANAGEMENT SYMPOSIUM

A. CASTELLt, ed. 16 Feb. 1978 423 p refs Syrup. held at

Huntsville, Ala., 18-19 Oct. 1977

(NASA-CP-2040)

ALABAMA, CONFERENCES, DATA MANAGEMENT, NASA

PROGRAMS, UNWERSITIES

N79-30947"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

CONCURRENT ERROR DETECTING CODES FOR ARITHMETIC

PROCESSORS

R. S. ElM Aug. 1979 27 p refs

(NASA-TP-1528; A-7810) Avail: NTIS HC A03/MF A01 CSCL

09B

ARITHMETIC, ERROR DETECTION CODES

N79-33858"# National Aeronautics and Space Administration.

Earth Resources Lab., Bay St. Louis, Miss.

PROCEDURE FOR EXTRACTION OF DISPARATE DATA FROM

MAPS INTO COMPUTERIZED DATA BASES

B. G. JUNKIN Washington Oct. 1979 23 p refs

(NASA-RP-1048) Avail: NTIS HC A02/MF A01 CSCL 09B

A procedure is presented for extracting disparate sources of

data from geographic maps and for the conversion of these data

into a suitable format for processing on a computer-oriented

information system. Several graphic digitizing considerations are

included and related to the NASA Earth Resources Laboratory's

Digitizer System. Current operating procedures for the Digitizer

System are given in a simplified and logical manner. The report

serves as a guide to those organizations interested in converting

map-based data by using a comparable map digitizing system.

Author

N80-16742"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

INFORM: AN INTERACTIVE DATA COLLECTION AND DISPLAY

PROGRAM WITH DEBUGGING CAPABILITY

D. S. CWYNAR Jan. 1980 169 p refs

(NASA-TP-1424; E-9810) Avail: NTIS HC A08/MF A01 CSCL

09B

COMPUTER GRAPHICS, COMPUTER SYSTEMS PROGRAMS,

LANGUAGE PROGRAMMING

N81-11644"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

AEROSPACE APPLICATIONS OF MICROPROCESSORS

1980 269 p refs Workshop held in Greenbelt, Md., 3-4 Nov.

1980; sponsored by NASA. Goddard Space Flight Center and

AIAA

(NASA-CP-2158) Avail: NTIS HC A12/MF A01 CSCL 09B

AEROSPACE ENGINEERING, COMPUTER PROGRAMS,

MICROPROCESSORS, MICROPROGRAMMING, SPACECRAFT

INSTRUMENTS, TECHNOLOGY ASSESSMENT

177
60 COMPUTEROPERATIONSANDHARDWARE

N81-25690"#National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

A DESIGN APPROACH TO REAL-TIME FORMATTING OF HIGH

SPEED MULTISPECTRAL IMAGE DATA

B. D. MEREDITH and W. L. KELLY, IV May 1981 20 p refs

(NASA-TP-1870; L-14454) Avail: NTIS HC A02/MF A01

CSCL 09B

BUFFER STORAGE, IMAGE PROCESSING,

MICROPROCESSORS, ONBOARD DATA PROCESSING, REAL

TtME OPERATION

N82-11784"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala. Data Systems Lab.

SPACE SHUTrLE MAIN ENGINE CONTROLLER

R. M. MATTOX and J. B. WHITE Nov. 1981 40 p refs

(NASA-TP-1932; M-360) Avail: NTIS HC A03/MF A01 CSCL

09B

ENGINE CONTROL, MECHANICAL ENGINEERING, SPACE

SHUTTLE MAIN ENGINE, SYSTEMS ENGINEERING

61

COMPUTER PROGRAMMING AND SOFTWARE

Includes computer programs, routines, and algorithms, and specific

applications, e.g., CAD/CAM

N77-33876*# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

STANDARDIZATION, CERTIFICATION, MAINTENANCE, AND

DISSEMINATION OF LARGE SCALE ENGINEERING SOFTWARE

SYSTEMS

T. G. TORIDIS, ed. (George Washington Univ., Washington, D.C.),

H. G. MCCOMB, JR., ed., and K. KHOZEIMEH, ed. (George

Washington Univ., Washington, D.C.) Sep. 1977 103 p refs

Panel Discussion Held at Washington, D.C., 29-31 Mar. 1976;

sponsored by NASA and NSF

(NASA-CP-2015; L-11771) Avail: NTIS HC A06/MF A01

CSCL 09B

COMPUTER PROGRAMS, CONFERENCES, MAINTENANCE

STANDARDIZATION, STRUCTURAL ANALYSIS

N78-10746"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

USER'S GUIDE FOR SFTRAN/360

T. E. FESSLER and W. F. FORD Oct. 1977 5t p refs

(NASA-TP-1006; E-9264) Avail: NTIS HC A04/MF A01 CSCL

09B

PROGRAMMING LANGUAGES, USER MANUALS

(COMPUTER PROGRAMS)

N78-20806"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

USER'S GUIDE TO SFTRAN/1100

W. F. FORD and T. E. FESSLER Apr. 1978 44 p refs

(NASA-TP-1200; E-9445) Avail: NTIS HC A03/MF A01 CSCL

09B

FORTRAN, UNIVAC 1100 SERIES COMPUTERS, USER

MANUALS (COMPUTER PROGRAMS)

178

N78-33776"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ENGINEERING AND SCIENTIFIC DATA MANAGEMENT

1978 255 p refs Proc. of Conf. held at Hampton, Va., 18-19

May 1978 Sponsored in part by the Inst. for Computer Appl. in

Sci. and Eng., and the George Washington Univ. Joint Inst. for

Advan. of Flight Sci., Hampton, Va.

(NASA-CP-2055; L-12043) Avail: NTIS HC A12/MF A01

CSCL 09B

COMPUTER TECHNIQUES, CONFERENCES, DATA BASES,

DATA MANAGEMENT, SCIENCE, SYSTEMS ENGINEERING

N78-33791"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

GUIDE TO A CONDENSED FORM OF NASTRAN

J. L ROGERS, JR. Sep. 1978 297 p refs

(NASA-RP-1019; L-11900) Avail: NTIS HC A13/MF A01

CSCL 09B

A limited capability form of NASTRAN level 16 is presented to

meet the needs of universities and small consulting firms. The

input cards, the programming language of the direct matrix

abstraction program, the plotting, the problem definition, and the

modules' diagnostic messages are described. Sample problems

relating to the analysis of linear static, vibration, and buckling are

included. This guide can serve as a handbook for instructional

courses in the use of NASTRAN or for users who need only the

capability provided by the condensed form. A.R.H.

N79-13736"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

TOOLS FOR EMBEDDED COMPUTING SYSTEMS SOFTWARE

1978 137 p refs Workshop held at Hampton, Va., 7-8 Nov.

1978; sponsored in part by AIAA

(NASA-CP-2064; L-12640) Avail: NTIS HC A07/MF A01

CSCL 09B

COMPUTER PROGRAMS, COMPUTER SYSTEMS

PROGRAMS, PROGRAMMING LANGUAGES, TOOLS

N79-17580"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AN INTEGRATED COMPUTER PROCEDURE FOR SIZING

COMPOSITE AIRFRAME STRUCTURES

J. SOBIESZCZANSKI-SOBIESKI Feb. 1979 45 p refs

(NASA-TP-1300; L-11817) Avail: NTIS HC A03/MF A01

CSCL 09B

AIRFRAME MATERIALS, COMPOSITE MATERIALS,

COMPUTER PROGRAMS, OPTIMIZATION

N79-21798"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

INTERACTIVE DEBUG PROGRAM FOR EVALUATION AND

MODIFICATION OF ASSEMBLY-LANGUAGE SOFTWARE

D. J. ARPASI Apr. 1979 82 p refs

(NASA-TP-1441; E-9219) Avail: NTIS HC A05/MF A01 CSCL

09B

ASSEMBLY LANGUAGE, COMPUTER PROGRAMS,

HONEYWELL COMPUTERS

N79-23688"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

WETAIR: A COMPUTER CODE FOR CALCULATING

THERMODYNAMIC AND TRANSPORT PROPERTIES OF

AIR-WATER MIXTURES

T. E. FESSLER May 1979 16 p refs

(NASA-TP-1466; E-9801) Avail: NTIS HC A02/MF A01 CSCL

09B

AIR WATER INTERACTIONS, COMPUTER PROGRAMS,

LIQUID-GAS MIXTURES, THERMODYNAMIC PROPERTIES,

TRANSPORT PROPERTIES
N81-12760"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

THE PR2D (PLACE, ROUTE IN 2-DIMENSIONS) AUTOMATIC

LAYOUT COMPUTER PROGRAM HANDBOOK

T, M. EDGE Sep. 1978 256 p refs

(NASA-RP-1029; M-268) Avail: NTIS HC A12/MF A01 CSCL

09B

Place, Route in 2-Dimensions is a standard cell automatic layout

computer program for generating large scale integrated/metal oxide

semiconductor arrays. The program was utilized successfully for a

number of years in both government and private sectors but until

now was undocumented. The compilation, loading, and execution

of the program on a Sigma V CP-V operating system is

described. S.F.

N81-33838"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

COMPUTER PROGRAM FOR PULSED THERMOCOUPLES WITH

CORRECTIONS FOR RADIATION EFFECTS

H. A. WILL Sep. 1981 42 p refs

(NASA-TP-1895; E-615) Avail: NTIS HC A03/MF A01 CSCL

09B

COMPUTER PROGRAMS, RADIATION DAMAGE,

THERMOCOUPLES

N82-24845"# Research Triangle Inst., Research Triangle Park,

N.C. Systems and Measurements Div.

PRODUCTION OF RELIABLE FLIGHT CRUCIAL SOFTWARE:

VALIDATION METHODS RESEARCH FOR FAULT TOLERANT

AVIONICS AND CONTROL SYSTEMS SUB-WORKING GROUP

MEETING

J. R. DUNHAM, ed. and J. C. KNIGHT, ed. (Virginia Univ.) May

1982 27 p refs Meeting held at Research Triangle Park,

N.C., 2-4 Nov. 1981

(NASA-CP-2222; L-15291; NAS 1.55:2222) Avail: NTIS HC

A03/MF A01 CSCL 09B

AUTOMATIC FLIGHT CONTROL, AVIONICS, COMPUTER

SYSTEMS PERFORMANCE, CONFERENCES, FAULT

TOLERANCE, PROGRAM VERIFICATION (COMPUTERS),

RELIABILITY ENGINEERING

N82-33020"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

AUTOMATED PROCEDURE FOR DEVELOPING HYBRID

COMPUTER SIMULATIONS OF TURBOFAN ENGINES. PART

1: GENERAL DESCRIPTION

J. R. SZUCH, S. M. KROSEL, and W. M. BRUTON Aug. 1982

120 p refs

(NASA-TP-1851; E-779; NAS 1.60:1851) Avail: NTIS HC

A06/MF A01 CSCL 09B

COMPUTER AIDED DESIGN, COMPUTER PROGRAMS,

COMPUTERIZED SIMULATION, ENGINE DESIGN, TURBOFAN

ENGINES

N83-17115"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

IPAD: INTEGRATED PROGRAMS FOR AEROSPACE-VEHICLE

DESIGN

Sep. 1980 398 p refs Proc. of Symp. held in Denver, 17-19

Sep. 1980 Sponsored in cooperation with Industry Technical

Advisory Board

(NASA-CP-2143; L-13916; NAS 1.55:2143) Avail: NTIS HC

A17/MF A01 CSCL09B

AEROSPACE VEHICLES, COMPUTER AIDED DESIGN,

COMPUTER AIDED MANUFACTURING, COMPUTER

PROGRAMS, PRODUCTION MANAGEMENT, PROJECT

MANAGEMENT, SPACECRAFT DESIGN

61 COMPUTER PROGRAMMING AND SOFTWARE

N84-20208"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

CYBER 200 APPLICATIONS SEMINAR

J. P. GARY, comp. Mar. 1984 342 p refs Seminar held in

Lanham, Md., 10-12 Oct. 1983; sponsored in cooperation with

Control Data Corp.

(NASA-CP-2295; NAS 1.55:2295; REPT-84F5215) Avail: NTIS

HCA15/MFA01 CSCL09B

COMPUTER PROGRAMMING, COMPUTERIZED SIMULATION,

CONFERENCES, DIGITAL COMPUTERS

N84-27461"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

STABCAR: A PROGRAM FOR FINDING CHARACTERISTIC

ROOT SYSTEMS HAVING TRANSCENDENTAL STABILITY

MATRICES

W. M. ADAMS, JR., S. H. TIFFANY, J. R. NEWSOM, and E. L.

PEELE Jun. t984 144 p refs

(NASA-TP-2165; L-14861; NAS 1.60:2165) Avail: NTIS HC

A07/MF A01 CSCL 09B

AERODYNAMIC CHARACTERISTICS, AIRCRAFT, COMPUTER

PROGRAMS, FLUTTER, MATRICES (MATHEMATICS),

STABILITY

N85-17576"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

MINDS: A MICROCOMPUTER INTERACTIVE DATA SYSTEM

FOR 8086-BASED CONTROLLERS

J. F. SOEDER Jan. 1985 41 p refs

(NASA-TP-2378; E-2172; NAS 1.60:2378) Avail: NTIS HC

A03/MF A01 CSCL 09B

COMPUTER SYSTEMS PROGRAMS, INTERACTIVE

CONTROL, MICROCOMPUTERS

N85-20689"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SPACE STATION SOFTWARE ISSUES

S. VOIGT, ed. and S. BESKENIS, ed. (Kentron International, Inc.,

Hampton, Va.) Washington Feb. 1985 68 p refs Workshop

held in Hampton, Va., 20-21 Aug. 1984

(NASA-CP-2361; L-15945; NAS 1.55:2361) Avail: NTIS HC

A04/MF A01 CSCL 09B

COMPUTER PROGRAMMING, CONFIGURATION

MANAGEMENT, ORBITAL SPACE STATIONS, PROJECT

MANAGEMENT, SOFTWARE ENGINEERING

N85-28609"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

PEER REVIEW OF A FORMAL VERIFICATION/DESIGN PROOF

METHODOLOGY Summary Report

1983 56 p refs Meeting held in Atlanta, 7-8 Jul. 1983

Prepared in cooperation with Research Triangle Inst.

(NASA-CP-2377; L-15992; NAS 1.55:2377) Avail: NTIS HC

A04/MF A01 CSCL 09B

CONFERENCES, DESIGN ANALYSIS, PROVING, SOFTWARE

ENGINEERING

N85-28610"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

REAL-TIME MULTIPROCESSOR PROGRAMMING LANGUAGE

(RTMPL) USER'S MANUAL

D. J. ARPASt Jun. 1985 115 p refs

(NASA-TP-2422; E-1999; NAS 1.60:2422) Avail: NTIS HC

A06/MF A01 CSCL 09B

DISTRIBUTED PROCESSING, MULTIPROCESSING

(COMPUTERS), REAL TIME OPERATION, USER MANUALS

(COMPUTER PROGRAMS)

179
61 COMPUTER PROGRAMMING AND SOFTWARE

N86-23314"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SPACE STATION SOFTWARE RECOMMENDATIONS

S. VOIGT, ed. Dec. 1985 142 p refs Forum held in

Huntsville, Ala., 24-25 Apr. 1985

(NASA-CP-2394; L-16063; NAS 1.55:2394) Avail: NTIS HC

A07/MF A01 CSCL 09B

COMPUTER PROGRAMS, PROJECT MANAGEMENT,

SOFTWARE ENGINEERING, SPACE STATIONS

62

COMPUTER SYSTEMS

Includes computer networks and special application computer

systems.

N78-30862"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

A DECODING PROCEDURE FOR THE REED-SOLOMON

CODES

R. S. LIM Aug. 1978 25p refs

(NASA-TP-1286; A-7372) Avail: NTIS HC AO2/MF A01 CSCL

09B

DECODING, ERROR CORRECTING CODES, MAGNETIC

STORAGE

N79-21822"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

NASF TRANSPOSITION NETWORK: A COMPUTING NETWORK

FOR UNSCRAMBLING P-ORDERED VECTORS

R. SLIM Apr. 1979 37 p refs

(NASA-TP-1426: A-7645) Avail: NTIS HC AOJ/MF A0t CSCL

09B

COMPUTER NETWORKS, NASA PROGRAMS, RANDOM

ACCESS MEMORY, VECTORS (MATHEMATICS)

N82-14829"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

RUGGEDIZED MINICOMPUTER HARDWARE AND SOFTWARE

TOPICS, 1981: PROCEEDINGS OF THE 4TH ROLM MIL-SPEC

COMPUTER USER'S GROUP CONFERENCE

Dec. 1981 214 p refs Con[ held in San Diego, Calif., 22-25

Feb, 1981

(NASA-CP-2206; L-14886) Avail: NTIS HC A11/MF A01

CSCL 09B

AIRBORNE/SPACEBORNE COMPUTERS, COMMERCIAL

AIRCRAFT, COMPUTER STORAGE DEVICES, CONFERENCES,

DISPLAY DEVICES, FLIGHT TESTS, MICROPROCESSORS,

ONBOARD DATA PROCESSING, TECHNOLOGY UTILIZATION,

USER REQUIREMENTS

N83-28921"# National Aeronautics and Space Administration.

L_s Research Center, Cleveland, Ohio.

PARALLEL, ASYNCHRONOUS EXECUTIVE (PAX): SYSTEM

CONCEPTS, FACILITIES, AND ARCHITECTURE

W. H. JONES Jun. 1983 60 p refs

(NASA-TP-2179; E-1584; NAS 1.60:2179) Avail: NTIS HC

A04/MF A01 CSCL 09B

ARCHITECTURE (COMPUTERS), DISTRIBUTED PROCESSING, PARALLEL PROCESSING (COMPUTERS)

180

N84-22299"# National Aeronautics and Space Administration,

Langley Research Center, Hampton, Va.

IPAD 2: ADVANCES IN DISTRIBUTED DATA BASE

MANAGEMENT FOR CAD/CAM

S. W. BOSTIC, comp. Washington Apr. 1984 258 p refs

Symp. held in Denver, 17-19 Apr, 1984; sponsored by NASA,

Naval Material Command and the industrial Technical Advisory

Board

(NASA-CP-2301; L-15765; NAS 1.55:2301) Avail: NTIS HC

A12/MF A01 CSCL 09B

COMPUTER AIDED DESIGN, COMPUTER AIDED

MANUFACTURING, CONFERENCES, DATA BASE

MANAGEMENT SYSTEMS, SYSTEMS iNTEGRATION

N84-34198"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va,

VALIDATION OF A FAULT-TOLERANT CLOCK

SYNCHRONIZATION SYSTEM

R. W, BUTLER and S. C. JOHNSON Sep. 1984 23 p refs

(NASA-TP-2346; L-t5799; NAS 1,60:2346) Avail: NTIS HC

A02/MF A01 CSCL 09B

CLOCKS, COMPUTER SYSTEMS PERFORMANCE, FAULT

TOLERANCE, PROVING, RELIABILITY, SYNCHRONISM

N85-17596"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

OPERATING SYSTEM FOR A REAL-TIME MULTIPROCESSOR

PROPULSION SYSTEM SIMULATOR. USER'S MANUAL

G. L. COLE Jan. 1985 42 p refs

(NASA-TP-2426; D-1998; NAS 1.60:2426) Avail: NTIS HC

A03/MF A01 CSCL 09B

MULTIPROCESSING (COMPUTERS), REAL TIME

OPERATION, SIMULATORS, USER MANUALS (COMPUTER

PROGRAMS)

N86-27947"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

HYBRID ROUTING TECHNIQUE FOR A FAULT-TOLERANT,

INTEGRATED INFORMATION NETWORK

B. D. MEREDITH Jut. 1986 20 p

(NASA-TP-2605; L-16034; NAS 1.60:2605) Avail: NTIS HC

A02/MF A01 CSCL 09B

ALGORITHMS, COMMUNICATION NETWORKS, FAULT

TOLERANCE, INFORMATION SYSTEMS, REAL TIME

OPERATION, SPACE STATIONS, SPACECRAFT

COMMUNICATION, SPACECREWS, TOPOLOGY

63

CYBERNETICS

Includes feedback and control theory, artificial intelligence, robotics

and expert systems.

N78-18823"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EIGENVALUE/EIGENVECTOR ASSIGNMENT USING OUTPUT

FEEDBACK

S. SRINATHKUMAR Feb. 1978 32 p refs

(NASA-TP-1118; L-11869) Avail: NTIS HC A03/MF A01

CSCL 09B

EIGENVALUES, EIGENVECTORS, FEEDBACK CONTROL
N78-22809"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ORACLS: A SYSTEM FOR LINEAR-QUADRATIC-GAUSSIAN

CONTROL LAW DESIGN

E. S. ARMSTRONG Apr. 1978 198 p refs

(NASA-TP-1106; L-11769) Avail: NTIS HC A09/MF A01

CSCL 09B

COMPUTER PROGRAMS, CONTROL THEORY, LINEAR

SYSTEMS, OPTIMAL CONTROL, QUADRATIC EQUATIONS

N80-25039"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

REALIZABLE OPTIMAL CONTROL FOR A REMOTELY PILOTED

RESEARCH VEHICLE

H,J. DUNN May1980 35p refs

(NASA-TP-1654; L-13403) Avail: NTIS HC A03/MF A01

CSCL 01C

CONTROL THEORY, CONTROLLERS, OPTIMAL CONTROL,

REMOTELY PILOTED VEHICLES, STABILITY AUGMENTATION

N81-29840"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AN APPLICATION OF MULTIVARIABLE DESIGN TECHNIQUES

TO THE CONTROL OF THE NATIONAL TRANSONIC FACILITY

E. S. ARMSTRONG and J_ S. TRIPP Aug. 1981 34 p refs

(NASA-TP-1887; L-14491) Avail: NTIS HC A03/MF A01

CSCL 14B

CONTROL SIMULATION, CRYOGENIC WIND TUNNELS,

DIGITAL TECHNIQUES, FEEDBACK CONTROL, OPTIMAL

CONTROL, TRANSONIC WIND TUNNELS

N81-30851"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

A METHOD FOR OBTAINING REDUCED-ORDER CONTROL

LAWS FOR HIGH-ORDER SYSTEMS USING OPTIMIZATION

TECHNIQUES

V. MUKHOPADHYAY, J. R. NEWSOM, and I. ABEL Aug. 1981

66 p refs

(NASA-TP-1876; L-14355) Avail: NTIS HC A04/MF A01

CSCL 12A

CONTROL THEORY, FEEDBACK CONTROL, NONLINEAR

PROGRAMMING, OPTIMIZATION

N84-16843"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

AESOP: AN INTERACTIVE COMPUTER PROGRAM FOR THE

DESIGN OF LINEAR QUADRATIC REGULATORS AND KALMAN

FILTERS

B. LEHTINEN and L. C. GEYSER Jan. 1984 115 p refs

(NASA-TP-2221; E-1686; NAS 1.60:2221) Avail: NTIS HC

A06/MF A01 CSCL09B

COMPUTER AIDED DESIGN, INTERACTIVE CONTROL,

KALMAN FILTERS, REGULATORS

N84-28538"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

REGIONS OF ATTRACTION AND ULTIMATE BOUNDEDNESS

FOR LINEAR QUADRATIC REGULATORS WITH

NONLINEARITIES

S. M. JOSHI Jul. 1984 34 p refs

(NASA-TP-2322; L-15739; NAS 1.60:2322) Avail: NTIS HC

A03/MF A01 CSCL 09C

ATTITUDE CONTROL, ATTRACTION, CONTROLLERS,

FEEDBACK CONTROL, LARGE SPACE STRUCTURES,

NONLINEAR FEEDBACK, NONLINEAR SYSTEMS, OPTIMAL

CONTROL, VIBRATION DAMPING

64 NUMERICAL ANALYSIS

N84-28539"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

KINEMATIC CONTROL OF ROBOT WITH DEGENERATE

WRIST

L. K. BARKER and M. C, MOORE Jul. 1984 37 p refs

(NASA-TP-2341; L-15743; NAS 1.60:2341) Avail: NTIS HC

A03/MF A01 CSCL 09B

ARTIFICIAL INTELLIGENCE, DYNAMIC CHARACTERISTICS,

DYNAMIC CONTROL, KINEMATIC EQUATIONS, ROBOTICS,

WRIST

N85-15446"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

TRANSLATIONAL CONTROL OF A GRAPHICALLY SIMULATED

ROBOT ARM BY KINEMATIC RATE EQUATIONS THAT

OVERCOME ELBOW JOINT SINGULARITY

L. K. BARKER, J. A. HOUCK, and S. W. CARZOO (Sperry Corp.,

Hampton, Va.) Dec. 1984 44 p refs

(NASA-TP-2376; L-15828; NAS 1.60:2376) Avail: NTIS HC

A03/MF A01 CSCL 05H

COMPUTERIZED SIMULATION, JOINTS (JUNCTIONS),

KINEMATIC EQUATIONS, MANEUVERS, MANIPULATORS,

ROBOTS, SINGULARITY (MATHEMATICS), TELEOPERATORS,

TRANSLATIONAL MOTION

N85-27575"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

KINEMATIC RATE CONTROL OF SIMULATED ROBOT HAND

AT OR NEAR WRIST SINGULARITY

K. BARKER, J. A. HOUCK, and S. W. CARZOO (Sperry Corp.,

Hampton, Va.) May 1985 28 p refs

(NASA-TP-2440; L-15889; NAS 1.60:2440) Avail: NTIS HC

A03/MF A01 CSCL 09B

COMPUTERIZED SIMULATION, KINEMATIC EQUATIONS,

MANIPULATORS, ROBOTS, WRIST

N86-13946"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

A METHOD TO STABILIZE LINEAR SYSTEMS USING

EIGENVALUE GRADIENT INFORMATION

C. D. WIESEMAN Nov. 1985 40 p refs

(NASA-TP-2479; L-15964; NAS 1.60:2479) Avail: NTIS HC

AO3/MF A01 CSCL 09B

CONTROL STABILITY, EIGENVALUES, LINEAR SYSTEMS,

OPTIMIZATION, SYSTEMS STABILITY

N86-25168"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

THEORETICAL THREE-AND FOUR-AXIS GIMBAL ROBOT

WRISTS

L. K. BARKER and J. A. HOUCK May 1986 38 p refs

(NASA-TP-2564; L-16042; NAS 1.60:2564) Avail: NTIS HC

A03/MF A01 CSCL 09B

FLIGHT SIMULATION, GIMBALS, HAND (ANATOMY),

MANIPULATORS, REMOTE HANDLING, ROBOTS, WRIST

181
64 NUMERICALANALYSIS

64

NUMERICAL ANALYSIS

Includes iteration, difference equations, and numerical

approximation.

N78-31836"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AN ALTERNATING DIRECTION IMPLICIT METHOD FOR THE

CONTROL DATA STAR-100 VECTOR COMPUTER

J. J. LAMBIOTTE, JR. Sep. 1978 25 p refs

(NASA-TP-1282; L-12287) Avail: NTIS HC A02/MF A01

CSCL 12A

ALGORITHMS, ALTERNATING DIRECTION IMPLICIT

METHODS, CONTROL DATA (COMPUTERS)

N80-13839"# National Aeronautics and Space Administration,

Washington, D.C.

MATHEMATICAL MODELING OF DIVERSE PHENOMENA

J. C. HOWARD 1979 402 p refs

(NASA-SP-437; LC-79-18506) Avail: NTIS HC A18/MF A01

CSCL "12A

Tensor calculus is applied to the formulation of mathematical

models of diverse phenomena. Aeronautics, fluid dynamics, and

cosmology are among the areas of application. The feasibility of

combining tensor methods and computer capability to formulate

problems is demonstrated. The techniques described are an

attempt to simplify the formulation of mathematical models by

reducing the modeling process to a series of routine operations,

which can be performed either manually or by computer. J.M.S.

N81-14690"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

NUMERICAL GRID GENERATION TECHNIQUES

1980 561 p refs Conf. held at NASA Langley Research

Center, Hampton, Va., 6-7 Oct. 1980 Sponsored in part by

Institute for Computer Applications in Science and Engineering,

Hampton, Va.

(NASA-CP-2166) Avail: NTIS HC A24/MF A01 CSCL 12A

BOUNDARY VALUE PROBLEMS, CONFERENCES,

CONFORMAL MAPPING, COORDINATE TRANSFORMATIONS,

FINITE DIFFERENCE THEORY, FLUID FLOW, MESH, PARTIAL

DIFFERENTIAL EQUATIONS, PROBLEM SOLVING, TOPOLOGY

N81-22754"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

TEMPORAL AND SPATIAL INCONSISTENCIES OF TIME-SPLIT

FINITE-DIFFERENCE SCHEMES

D. L. DWOYER and F. C. THAMES Apr. 1981 58 p refs

(NASA-TP-1790; L-13941) Avail: NTIS HC A04/MF A01

CSCL 12A

ALGORITHMS, CONSISTENCY, FINITE DIFFERENCE

THEORY, FLOW EQUATIONS, TIME

N81-33856"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

NUMERICAL BOUNDARY CONDITION PROCEDURES

Oct. 1981 383 p refs Symp. held at Moffett Field, Calif.,

19-20 Oct. 1981

(NASA-CP-2201; A-8736) Avail: NTIS HC A17/MF A01

BOUNDARY VALUE PROBLEMS, COMPUTATIONAL FLUID

DYNAMICS, CONDITIONS, CONFERENCES, GAS DYNAMICS,

NUMERICAL FLOW VISUALIZATION

182

N81-33879"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

MULTIGRID METHODS

Oct. 1981 304 p refs Symp. held at Moffett Field, Calif.,

21-22 Oct. 1981

(NASA-CP-2202; A-8738) Avail: NTIS HC A14/MF A01 CSCL

I?A

CONFERENCES, MATRICES (MATHEMATICS), NAVlERSTOKES EQUATION, NUMERICAL ANALYSIS, PARTIAL DIFFERENTIAL EQUATIONS

N83-25438"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

THEORETICAL METHOD FOR CALCULATING RELATIVE JOINT

GEOMETRY OF ASSEMBLED ROBOT ARMS

L. K. BARKER and M. C. MOORE May 1983 25 p refs

(NASA-TP-2155; L-15562; NAS 1.60:2155) Avail: NTIS HC

A02/MF A01 CSCL 12A

EQUATIONS OF MOTION, GEOMETRY, MATHEMATICAL

MODELS, REMOTE HANDLING, ROBOTS

N83-34661"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

VECTOR-ALGEBRA APPROACH TO EXTRACT

DENAVIT-HARTENBERG PARAMETERS OF ASSEMBLED

ROBOT ARMS

L. K. BARKER Aug. 1983 34 p refs

(NASA-TP-2191; L-15621; NAS 1.60:2191) Avail: NTIS HC

A03/MF A01 CSCL 12A

ARM (ANATOMY), MATRICES (MATHEMATICS). ROBOTS.

TRANSFORMATIONS (MATHEMATICS), VECTORS (MATHEMATICS)

N84-13885"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

ACCELERATION OF CONVERGENCE OF VECTOR

SEQUENCES

A. SIDI, W. F. FORD, and D. A. SMITH (Duke Univ., Durham,

N.C.) Dec. 1983 27 p refs

(NAS3-23606; NSG-3160)

(NASA-TP-2193; E-1719; NAS 1.60:2193) Avail: NTIS HC

A03/MF A01 CSCL 12A

ALGORITHMS, CONVERGENCE, VECTORS (MATHEMATICS)

N84-34204"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

RATIONAL-SPLINE APPROXIMATION WITH AUTOMATIC

TENSION ADJUSTMENT

J. R. SCHIESS and P. A. KERR Oct. 1984 13 p refs

(NASA°TP-2366; L-15826; NAS 1.60:2366) Avail: NTIS HC

A02/MF A01 CSCL 12A

ALGORITHMS, APPROXIMATION, CURVE FITTING, LEAST

SQUARES METHOD, TENSION

N85-19733"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

MODELING THE INTERNAL COMBUSTION ENGINE

F. J. ZELEZNIK and B. J. MCBRIDE Mar. 1985 309 p refs

(NASA-RP-1094; E-996; NAS 1.61:1094) Avail: NTIS HC

A14/MF A01 CSCL 12A

A flexible and computationally economical model of the internal

corr_bustion engine was developed for use on large digital computer

systems. It is based on a system of ordinary differential equations

for cylinder-averaged properties. The computer program is capable

of multicycle calculations, with some parameters varying from cycle

to cycle, and has restart capabilities. It can accommodate a broad

spectrum of reactants, permits changes in physical properties, and

offers a wide selection of alternative modeling functions without

any reprogramming. It readily adapts to the amount of information

available in a particular case because the model is in fact a

hierarchy of five models. The models range from a simple model

requiring only thermodynamic properties to a complex model

demanding full combustion kinetics, transport properties, and
65 STATISTICS AND PROBABILITY

poppet valve flow characteristics. Among its many features the

model includes heat transfer, valve timing, supercharging, motoring,

finite burning rates, cycle-to-cycle variations in air-fuel ratio, humid

air, residual and recirculated exhaust gas, and full combustion

kinetics. Author

N85-28656"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

CONVERGENCE OF NEWTON'S METHOD FOR A SINGLE REAL

EQUATION

C. W. CAMPBELL Jun. 1985 23 p refs

(NASA-TP-2489; NAS 1.60:2489) Avail: NTIS HC A02/MF A01

CSCL 12A

CONVERGENCE, FUNCTIONS (MATHEMATICS), NONLINEAR

EQUATIONS, ROOTS OF EQUATIONS

N86-18060"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

THE ALGORITHMS FOR RATIONAL SPLINE INTERPOLATION

OF SURFACES

J. R. SCHIESS Jan. 1986 27 p refs

(NASA-TP-2536; L-16045; NAS 1.60:2536) Avail: NTIS HC

A03/MF A01 CSCL 20F

ALGORITHMS, COMPUTER PROGRAMS, DISPLAY DEVICES,

HIGH SPEED, SPLINE FUNCTIONS, TENSILE PROPERTIES,

TENSOR ANALYSIS

N86-27953"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

MODIFIED DENAVIT-HARTENBERG PARAMETERS FOR

BETTER LOCATION OF JOINT AXIS SYSTEMS IN ROBOT

ARMS

L K. BARKER Washington Jul. 1986 30 p

(NASA-TP-2585; L-16092; NAS 1.60:2585) Avail: NTIS HC

A03/MF A01 CSCL t2A

ARM (ANATOMY), AXES OF ROTATION, JOINTS (ANAl OMY),

MANIPULATORS, ROBOTICS, SHOULDERS

N86-28661"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

SOLUTION OF ELLIPTIC PARTIAL DIFFERENTIAL EQUATIONS

BY FAST POISSON SOLVERS USING A LOCAL RELAXATION

FACTOR. 1: ONE-STEP METHOD

S. C. CHANG May 1986 22 p Presented at the Ninth

International Conference on Numerical Methods in Fluid Dynamics,

Saclay, France, 25-29 Jun. 1984

(NASA-TP-2529; E-2461-1; NAS 1.60:2529) Avail: NTIS HC

A02/MF A01 CSCL 12A

ALGORITHMS, ELLIPTIC DIFFERENTIAL EQUATIONS,

ELLIPTIC FUNCTIONS, ITERATIVE SOLUTION, PARTIAL

DIFFERENTIAL EQUATIONS

N86-28662"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

PHYSICAL AND NUMERICAL SOURCES OF COMPUTATIONAL

INEFFICIENCY IN INTEGRATION OF CHEMICAL KINETIC RATE

EQUATIONS: ETIOLOGY, TREATMENT AND PROGNOSIS

D. T. PRATT (Washington Univ., Seattle) and K.

RADHAKRISHNAN May 1986 12 p

(NAG3-147)

(NASA-TP-2590; E-2587; NAS 1.60:2590) Avail: NTIS HC

A02/MF A01 CSCL 12A

ALGORITHMS, CHEMICAL REACTIONS, CODING,

COMPUTATION, COMPUTER PROGRAMS, REACTION KINETICS,

VAPOR PHASES

65

STATISTICS AND PROBABILITY

Includes data sampling and smoothing; Monte Carlo method; and

stochastic processes.

N78-31854"# National Aeronautics and Space Administration.

John F. Kennedy Space Center, Cocoa Beach, Fla.

SIMULATION STUDY OF THE POWER OF THE

KOLMOGOROFF-SMIRNOFF AND Z TESTS FOR THE

EXPONENTIAL DISTRIBUTION

J. B. GAYLE Sep. 1978 18 p refs

(NASA-TP-1311) Avail: NTIS HC A02/MF A01 CSCL 12A

COMPUTERIZED SIMULATION, EXPONENTIAL FUNCTIONS,

KOLMOGOROFF-SMIRNOFF TEST

N81-23838"# National Aeronautics and Space Administration.

Lyndon B. Johnson Space Center, Houston, Tex.

COMPUTER SIMULATION OF RANDOM VARIABLES AND

VECTORS WITH ARBITRARY PROBABILITY DISTRIBUTION

LAWS

V. M. BOGDAN (Catholic Univ.) Washington May 1981 43 p

refs

(NASA-TP-1859; S-504) Avail: NTIS HC A03/MF A01 CSCL

12A

COMPUTERIZED SIMULATION, PROBABILITY DISTRIBUTION

FUNCTIONS, RANDOM VARIABLES, VECTORS

(MATHEMATICS)

N81-27865"# National Aeronautics and Space Administration.

Dryden (Hugh L.) Flight Research Center, Edwards, Calif.

THE THEORY AND PRACTICE OF ESTIMATING THE

ACCURACY OF DYNAMIC FLIGHT-DETERMINED

COEFFICIENTS Final Report

R. E. MAINE and K. W. ILIFF Jul. 1981 63 p refs

(NASA-RP-1077; H-1128) Avail: NTIS HC A04/MF A01 CSCL

12A

Means of assessing the accuracy of maximum likelihood

parameter estimates obtained from dynamic flight data are

discussed. The most commonly used analytical predictors of

accuracy are derived and compared from both statistical and

simplified geometrics standpoints. The accuracy predictions are

evaluated with real and simulated data, with an emphasis on

practical considerations, such as modeling error. Improved

computations of the Cramer-Rao bound to correct large

discrepancies due to colored noise and modeling error are

presented. The corrected Cramer-Rao bound is shown to be the

best available analytical predictor of accuracy, and several practical

examples of the use of the Cramer-Rao bound are given.

Engineering judgement, aided by such analytical tools, is the final

arbiter of accuracy estimation. Author

N83-16095"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

GENERATION OF PSEUDO-RANDOM NUMBERS

L. W. HOWELL and M H. RHEINFURTH Dec. 1982 26 p

refs

(NASA-TP-2105; NAS 1.60:2105) Avail: NTIS HC A03/MF A01

CSCL 12A

GENERATORS, MONTE CARLO METHOD, PSEUDORANDOM

SEQUENCES, RANDOM NUMBERS

183
65 STATISTICSANDPROBABILITY

N83-27679"#National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

AN EFFICIENT ALGORITHM FOR GENERATING RANDOM

NUMBER PAIRS DRAWN FROM A BIVARIATE NORMAL

DISTRIBUTION

C. W. CAMPBELL Jun. 1983 17 p refs

(NASA-TP-2173; NAS 1.60:2173) Avail: NTIS HC A02/MF A01

CSCL 12A

DISTRIBUTION FUNCTIONS, MONTE CARLO METHOD,

RANDOM NUMBERS

N83-33631"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

ANALYSIS OF RANDOM SIGNAL COMBINATIONS FOR

SPACECRAFT POINTING STABILITY

L. HOWELL Aug. 1983 18 p refs

(NASA-TP-2216; NAS 1.60:2216) Avail: NTIS HC A02/MF A01

CSCL 12A

CONVOLUTION INTEGRALS, PROBABILITY DENSITY

FUNCTIONS, RANDOM SIGNALS, RANDOM VARIABLES

N85-16565"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SPLINE METHODS FOR APPROXIMATING QUANTILE

FUNCTIONS AND GENERATING RANDOM SAMPLES

J. R. SCHIESS and C. G. MATTHEWS (Computer Sciences

Corp.) Jan. 1985 34 p refs

(NASA-TP-2389; L-15850; NAS 1.60:2389) Avail: NTIS HC

A03/MF A01 CSCL 12A

APPROXIMATION, PROBABILITY DISTRIBUTION

FUNCTIONS, QUANTILES, RANDOM SAMPLING, SPLINE

FUNCTIONS

N86-19095"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

A STOCHASTIC MODEL FOR PARTICLE IMPINGEMENTS ON

ORBITING SPACECRAFT

L. W. HOWELL, JR. Jan. 1986 43 p refs

(NASA-TP-2550; NAS 1.60:2550) Avail: NTIS HC A03/MF A01

CSCL 12A

AEROSPACE ENVIRONMENTS, ANGULAR MOMENTUM,

COSMIC RAYS, MOMENTUM TRANSFER, PARTICLE

TRAJECTORIES, STOCHASTIC PROCESSES

66

SYSTEMS ANALYSIS

Includes mathematical modeling; network analysis; and operations

research.

N78-30896"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio,

PROCEDURES FOR GENERATION AND REDUCTION OF

LINEAR MODELS OF A TURBOFAN ENGINE

K. SELDNER and D. S. CWYNAR Aug. 1978 46 p refs

(NASA-TP-1261; E-9460) Avail: NTIS HC A03/MF A01 CSCL

12B

COMPUTERIZED SIMULATION, MATHEMATICAL MODELS,

TURBOFAN ENGINES

184

N81-I0789"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

STABILITY BOUNDARIES FOR SYSTEMS WITH

FREQUENCY-MODEL FEEDBACK AND COMPLACENCY

FILTER

L. K. BARKER Nov. 1980 43 p refs

(NASA-TP-1744; L-13787) Avail: NTIS HC A03/MF A01

CSCL 12B

AUTOMATIC GAIN CONTROL, BOUNDARIES, ELECTRIC

FILTERS, FEEDBACK CONTROL, LOW PASS FILTERS, PILOT

PLANTS

N81-12812"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

OPTIMAL REGULATION IN SYSTEMS WITH STOCHASTIC TIME

SAMPLING

R. C. MONTGOMERY and P. S. LEE Hampton, Va. Nov. 1980

29 p refs

(NASA-TP-1743; L-13507) Avail: NTIS HC A03/MF A01

CSCL 12B

AERODYNAMICS, MARKOV PROCESSES, STOCHASTIC

PROCESSES, TIME OPTIMAL CONTROL

N81-29902"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AUTOMATED DECISION MAKING AND PROBLEM SOLVING.

VOLUME 2: CONFERENCE PRESENTATIONS

E. HEER (Univ. of Southern California, Los Angeles) 1980 312

p refs Conf. held in Hampton, Va., 19-21 May 1980 2 Vol.

(NASA-CP-2180-VOL-2; L-14396-VOL.2) Avail: NTIS HC

A14/MFA01 CSCL 12B

ARTIFICIAL INTELLIGENCE, AUTOMATA THEORY,

CONFERENCES, DECISION MAKING, OPERATIONS RESEARCH,

PROBLEM SOLVING, SYSTEMS SIMULATION

N81-30889"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AUTOMATED DECISION MAKING AND PROBLEM SOLVING.

VOLUME 1: EXECUTIVE SUMMARY

E. HEER Aug. 1981 55 p refs Conf. held at Hampton, Va.,

19-21 May 1980 2 Vol.

(NASA-CP-2180-VOL-1; L-14396) Avail: NTIS HC A04/MF A01

CSCL 12B

ARTIFICIAL INTELLIGENCE, AUTOMATIC CONTROL,

CONTROL THEORY, DECISION MAKING, OPERATIONS

RESEARCH, PROBLEM SOLVING

N83-10876"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

NONLINEAR OPTIMIZATION WITH LINEAR CONSTRAINTS

USING A PROJECTION METHOD

T. FOX Sep, 1982 99p refs

(NASA-TP-2086; M-389; NAS 1.60:2086) Avail: NTIS HC

A05/MF A01 CSCL 12B

CONSTRAINTS, LINEAR SYSTEMS, NONLINEAR

PROGRAMMING, NONLINEAR SYSTEMS, OPTIMIZATION,

PROJECTIVE GEOMETRY

N83-35736*# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

DEVELOPMENT OF A DISTRIBUTED-PARAMETER

MATHEMATICAL MODEL FOR SIMULATION OF CRYOGENIC

WINO TUNNELS

J. S. TRIPP Sep. 1983 50 p refs

(NASA-TP-2177; L-15591; NAS 1.60:2177) Avail: NTIS HC

A03/MF A01 CSCL 12B

CRYOGENIC WIND TUNNELS, DISTRIBUTED PARAMETER

SYSTEMS, SIMULATION
N85-19784"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

IDENTIFICATION OF DYNAMIC SYSTEMS, THEORY AND

FORMULATION

R. E. MAINE and K. W. ILIFF Feb. 1985 138 p refs

(NASA-RP-1138; H-1255; NAS 1.61:1138; AGARDOGRAPH-300)

Avail: NTIS HC A07/MF A01 CSCL 12B

The problem of estimating parameters of dynamic systems is

addressed in order to present the theoretical basis of system

identification and parameter estimation in a manner that is complete

and rigorous, yet understandable with minimal prerequisites.

Maximum likelihood and related estimators are highlighted. The

approach used requires familiarity with calculus, linear algebra,

and probability, but does not require knowledge of stochastic

processes or functional analysis. The treatment emphasizes

unification of the various areas in estimation in dynamic systems

is treated as a direct outgrowth of the static system theory. Topics

covered include basic concepts and definitions; numerical

optimization methods; probability; statistical estimators; estimation

in static systems; stochastic processes; state estimation in dynamic

systems; output error, filter error, and equation error methods of

parameter estimation in dynamic systems, and the accuracy of

the estimates. Author

N85-28708"# National Aeronautics and Space Administration,

Washington, D.C.

ADDING COMPUTATIONALLY EFFICIENT REALISM TO MONTE

CARLO TURBULENCE SIMULATION

C. W. CAMPBELL May 1985 21 p refs

(NASA-TP-2469; M-485; NAS 1.60:2469) Avail: NTIS HC

A02/MF A01 CSCL 12B

COMPUTERIZED SIMULATION, FLIGHT SIMULATION, LOW

LEVEL TURBULENCE, MONTE CARLO METHOD

N85-33745"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

A FORMULATION AND ANALYSIS OF COMBAT GAMES

M. HEYMANN (Technion-lsrael Inst. of Tech., Haifa), M. D.

ARDEMA, and N. RAJAN (Stanford Univ., Calif.) Jun. 1985 44

p refs

(NASA-TP-2487; REPT-85022; NAS 1.60:2487) Avail: NTIS HC

A03/MF A01 CSCL 12B

COMBAT, GAME THEORY, MATHEMATICAL MODELS,

PROBABILITY THEORY

67

THEORETICAL MATHEMATICS

Includes topology and number theory.

N79-18679"# National Aeronautics and Space Administration.

Dryden (Hugh L.) Flight Research Center, Edwards, Calif.

A CHARACTERIZATION OF THE REAL ZEROS OF A

PARTICULAR TRANSCENDENTAL FUNCTION

D. R. HEDGLEY Mar. 1979 12 p refs

(NASA-TP-1420; H-1065) Avail: NTIS HC A02/MF A01 CSCL

12A

NUMERICAL ANALYSIS, REAL VARIABLES, TRANSCENDENTAL FUNCTIONS

N84-15880"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

THE GENERALIZED EULER-MASCHERONI CONSTANTS

O. R. AINSWORTH (Alabama Univ.) and L. W. HOWELL Jan.

1984 15 p refs

(NASA-TP-2264; NAS 1.60:2264) Avail: NTIS HC A02/MF A01

CSCL 12A

COMPUTATION, CONSTANTS, MEROMORPHIC FUNCTIONS,

POWER SERIES, SERIES EXPANSION

71 ACOUSTICS

7O

PHYSICS (GENERAL)

N80-29096"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

PROCEEDINGS OF THE ELEVENTH ANNUAL PRECISE TIME

AND TIME INTERVAL (PTTI) APPLICATION AND PLANNING

MEETING

S. C. WARDRIP, ed. 1979 703 p refs Meeting held in

Greenbelt, Md., 27-29 Nov. 1979; sponsored by NASA. Goddard

Space Flight Center, Naval Electronics Systems Command, Naval

Research Lab., Naval Observatory, and Defense Communications

Agency

(NASA-CP-2129) Avail: NTIS HC A99/MF A01 CSCL 14B

COMMUNICATION NETWORKS, CONFERENCES,

SYNCHRONISM, TIME MEASUREMENT, TIME SIGNALS

71

ACOUSTICS

Includes sound generation, transmission, and attenuation.

N77-30908"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

FINITE-DIFFERENCE THEORY FOR SOUND PROPAGATION IN

A LINED DUCT WITH UNIFORM FLOW USING THE WAVE

ENVELOPE CONCEPT

K. J. BAUMEISTER Washington Aug. 1977 64 p refs

(NASA-TP-1001; E-9149) Avail: NTIS HC A04/MF A01 CSCL

20A

ACOUSTIC DUCTS, FINITE DIFFERENCE THEORY, SOUND

PROPAGATION, UNIFORM FLOW

N77-30909"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

ACOUSTIC PERFORMANCE OF TWO 1.83-METER-DIAMETER

FANS DESIGNED FOR A WIND-TUNNEL DRIVE SYSTEM

P. R SODERMAN and V. R. PAGE Aug. 1977 76 p refs

Prepared in cooperation with US Army Air Mobility Research and

Development Lab., Moffett Field, Calif.

(NASA-TP-1008; A-6888) Avail: NTIS HC A05/MF A01 CSCL

20A

ACOUSTIC MEASUREMENT, AERODYNAMIC NOISE, FANS,

NOISE INTENSITY, WIND TUNNEL DRIVES

N78-12800"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

MEASUREMENTS OF THE TONAL COMPONENT OF CAVITY

NOISE AND COMPARISON WITH THEORY

P. J. W. BLOCK Nov. 1977 34 p refs

(NASA-TP-1013; L-11620) Avail: NTIS HC A03/MF A01

CSCL 20A

AIRCRAFT NOISE, CAVITATION FLOW, CAVITY

RESONATORS, FREQUENCY MEASUREMENT, NOISE

GENERATORS

185
71 ACOUSTICS

N78-12801"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AN EXPERIMENTAL EVALUATION OF THE APPLICATION OF

THE KIRCHHOFF FORMULATION FOR SOUND RADIATION

FROM AN OSCILLATING AIRFOIL

T. F. BROOKS Washington Dec. 1977 39 p refs

(NASA-TP-1048; L-11479) Avail: NTIS HC A03/MF A01

CSCL 20A

AEROACOUSTICS, AERODYNAMIC NOISE, KIRCHHOFF LAW

OF RADIATION, WING OSCILLATIONS

N78-17823"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

PREDICTION OF GROUND EFFECTS ON AIRCRAFT NOISE

S. P. PAO, A. R. WENZEL, and P. B. ONCLEY (MAN-Acoustics

and Noise, Inc.) Jan. 1978 42 p refs

(NASA-TP-1104; L-11833) Avail: NTIS HC A03/MF A01

CSCL 20A

AIRCRAFT NOISE, GROUND EFFECT (AERODYNAMICS),

SOUND PROPAGATION

N78-23877"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

NOISE TRANSMISSION THROUGH PLATES INTO AN

ENCLOSURE M.S. Thesis - George Washlngton Univ.

W. B. MCDONALD (Joint Inst. for Advancement of Flight Sciences,

Washington, D. C.), R. VAICAITIS, and M. K. MYERS (Joint Inst.

for Advancement of Flight Sciences, Washington, D.C.) May

1978 44 p refs

(NASA-TP-1173; L-11906) Avail: NTIS HC A03/MF A01

CSCL 20A

ELASTIC PLATES, NOISE PROPAGATION

N78-32816"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

HELICOPTER ACOUSTICS

Aug. 1978 399 p refs Presented at the Intern. Specialists

Symp., Hampton, Va., 22-24 May 1978; sponsored by the Am.

Helicopter Soc. and AROD

(NASA-CP-2052-PT-1; L-12339) Avail: NTIS HC A17/MF A01

CSCL 20A

AEROACOUSTICS, AIRCRAFT NOISE, CONFERENCES,

HELICOPTERS

N79-10843"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

HELICOPTER ACOUSTICS, PART 2

Aug. 1978 438 p refs Presented at the Intern. Specialists

Symp., Hampton, Va., 22-24 May 1978; sponsored by the Am.

Helicopter Soc. and AROD

(NASA-CP-2052-PT-2; L-12339-PT-2) Avail: NTIS HC A19/MF

A01 CSCL 20A

AEROACOUSTICS, AIRCRAFT NOISE, CONFERENCES,

HELICOPTERS

N79-13821"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

A THEORETICAL INVESTIGATION OF NOISE REDUCTION

THROUGH THE CYLINDRICAL FUSELAGE OF A TWIN-ENGINE,

PROPELLER-DRIVEN AIRCRAFT

R. B. BHAT and J. S. MIXSON Dec. 1978 47 p refs

(NASA-TP-1325; L-12225) Avail: NTIS HC A03/MF A01

CSCL 20A

CYLINDRICAL SHELLS, FUSELAGES, NOISE REDUCTION,

PROPELLER DRIVE

186

N79-14872"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

A COMPARISON OF THE NOISE PRODUCED BY A SMALL

JET ON A MOVING VEHICLE WITH THAT IN A FREE JET

T_ D. NORUM Dec. 1978 24 p refs

(NASA-TP-1326; L-12383) Avail: NTIS HC A02/MF A01

CSCL 20A

AUTOMOBILES, FREE JETS, JET AIRCRAFT NOISE, JET

FLOW, JET MIXING FLOW, NOISE SPECTRA

N79-14874"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

NOISE TRANSMISSION THROUGH FLAT RECTANGULAR

PANELS INTO A CLOSED CAVITY

C. K. BARTON and E. F. DANIELS Dec. 1978 29 p refs

(NASA-TP-1321; L-12439) Avail: NTIS HC A03/MF A01

CSCL 20A

AIRCRAFT NOISE, CAVITIES, FLAT SURFACES, LIGHT

AIRCRAFT, NOISE PROPAGATION, RECTANGULAR PANELS

N79-16641"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

FLUCTUATING LOADS MEASURED ON AN OVER-THE-WING

SUPERSONIC JET MODEL

C. M. WILLIS Jan. 1979 41 p refs

(NASA-TP-1366; L-12511) Avail: NTIS HC A03/MF A01

CSCL 20A

AERODYNAMIC CONFIGURATIONS, AIRCRAFT MODELS,

JET ENGINES, LOADS (FORCES), PRESSURE MEASUREMENT,

SUPERSONIC CRUISE AIRCRAFT RESEARCH

N79-17659"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

COMPUTATION OF ATMOSPHERIC ATTENUATION OF SOUND

FOR FRACTIONAL-OCTAVE BANDS

F. J. MONTEGANI Feb. 1979 32 p refs

(NASA-TP-1412; E-9763) Avail: NTIS HC A03/MF A01 CSCL

20A

ATMOSPHERIC ATTENUATION, COMPUTER PROGRAMS,

SOUND PROPAGATION, WAVE PROPAGATION

N79-18687"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

VARIABILITY OF ANNOYANCE RESPONSE DUE TO AIRCRAFT

NOISE

T. K. DEMPSEY and J. M. CAWTHORN Mar. 1979 77 p refs

(NASA-TP-1335; L-12483) Avail: NTIS HC A05/MF A01

CSCL 20A

AIRCRAFT NOISE, HUMAN TOLERANCES, NOISE

THRESHOLD, VARIABILITY

N79-19813"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

FLUCTUATING SURFACE PRESSURE AND ACOUSTIC

RADIATION FOR SUBSONIC NORMAL JET IMPINGEMENT

J. S. PREISSER Mar. 1979 56 p refs

(NASA-TP-1361; L-12412) Avail: NTIS HC A04/MF A01

CSCL 20A

JET IMPINGEMENT, PRESSURE, SOUND WAVES, SUBSONIC

SPEED, VARIATIONS

N79-20832"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECTS OF DURATION AND OTHER NOISE

CHARACTERISTICS ON THE ANNOYANCE CAUSED BY

AIRCRAFT-FLYOVER NOISE

D. A. MCCURDY and C. A. POWELL Mar. 1979 47 p refs

(NASA-TP-1386; L-12579) Avail: NTIS HC A03/MF A01

CSCL 20A

AIRCRAFT NOISE, EFFECTIVE PERCEIVED NOISE LEVELS,

NOISE TOLERANCE, PSYCHOACOUSTICS, PSYCHOLOGICAL

EFFECTS
N79-22849"#National Aeronautics andSpaceAdministration.

LangleyResearchCenter, Hampton, Va.

A CORRELATION OF MIXING NOISE FROM COANNULAR JETS

WITH INVERTED FLOW PROFILES

S. P. PAO Apr. 1979 127 p refs

(NASA-TP-1301; L-12155) Avail: NTIS HC A07/MF A01

CSCL 20A

DATA CORRELATION, FLOW DISTRIBUTION, JET AIRCRAFT

NOISE, JET MIXING FLOW

N79-24773"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

STATISTICAL COMPARISONS OF AIRCRAFT FLYOVER NOISE

ADJUSTMENT PROCEDURES FOR DIFFERENT WEATHER

CONDITIONS

A W. MUELLER and D. A. HILTON May 1979 35 p refs

(NASA-TP-1430; L-12626) Avail: NTIS HC A03/MF A01

CSCL 20A

AIRCRAFT NOISE, NOISE INTENSITY, NOISE SPECTRA,

STATISTICAL ANALYSIS

N79-32057"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EVALUATION OF A VORTEX MODEL OF TURBULENT CAVITY

FLOW

J. C. HARDIN and P. J. W. BLOCK Sep. 1979 47 p refs

(NASA-TP-1505; L-12684) Avail: NTIS HC A03/MF A01

CSCL 20A

AEROACOUSTICS, AERODYNAMIC NOISE, CAVITATION

FLOW, FLUID DYNAMICS, MATHEMATICAL MODELS, NOISE

MEASUREMENT, TURBULENCE, VORTICES

N80-11869"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

A CLOSED-FORM SOLUTION FOR NOISE CONTOURS

E. C. STEWART and T. M. CARSON Nov. 1979 40 p refs

(NASA-TP-1432; A-7660) Avail: NTIS HC A03/MF A01 CSCL

20A

AIRCRAFT NOISE, CONTOURS, NOISE REDUCTION

N80-13879"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EXPERIMENTAL STUDY OF ACOUSTIC LOADS ON AN

UPPER-SURFACE-BLOWN STOL AIRPLANE CONFIGURATION

C. M. WILLIS and J. A. SCHOENSTER Dec. 1979 57 p

(NASA°TP-1577; L-13167) Avail: NTIS HC A04/MF A01

CSCL 20A

AEROACOUSTICS, AERODYNAMIC LOADS, SHORT

TAKEOFF AIRCRAFT, SOUND PRESSURE, UPPER SURFACE

BLOWN FLAPS, WIND TUNNEL TESTS

N80-13880"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECTS OF SOUND LEVEL FLUCTUATIONS ON ANNOYANCE

CAUSED BY AIRCRAFT-FLYOVER NOISE

D. A. MCCURDY Dec. 1979 40 p refs

(NASA-TP-1576; L-13181) Avail: NTIS HC A03/MF A01

CSCL 20A

AIRCRAFT NOISE, HUMAN TOLERANCES, NOISE

INTENSITY, PSYCHOACOUSTICS, VARIATIONS

N80-14840"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EVALUATION OF HELICOPTER NOISE DUE TO B

BLADE-VORTEX INTERACTION FOR FIVE TIP

CONFIGURATIONS

D. R. HOAD Dec. 1979 80 p refs Prepared jointly with

AVRADCOM, Hampton, Va.

(DA PROJ. 1L2-62209-AH-76)

(NASA-TP-1608; AVRADCOM-TR-80-B-1; L-13207) Avail: NTIS

HC A05/MFA01 CSCL 20A

AIRCRAFT NOISE, BLADE TIPS, HELICOPTERS, NOISE

REDUCTION, VORTICES

71 ACOUSTICS

N80-18882"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

APPLICATION OF COHERENCE IN FAN NOISE STUDIES

J. R. BALOMBIN Feb, 1980 26 p refs

(NASA-TP-1630; E-157) Avail: NTIS HC A03/MF A01 CSCL

20A

ACOUSTICS, COHERENT RADIATION, INTAKE SYSTEMS,

SIGNAL PROCESSING

N80-23100"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

FORWARD ACOUSTIC PERFORMANCE OF A

SHOCK-SWALLOWING HIGH-TIP-SPEED FAN (OF-13)

J. G. LUCAS, R. P. WOODWARD, and M. J. MACKINNON May

1980 20 p refs

(NASA-TP-1668; E-202) Avail: NTIS HC A02/MF A01 CSCL

20A

ACOUSTIC MEASUREMENT, AERODYNAMIC CHARACTERISTICS, BLADE TIPS, NOISE REDUCTION, ROTOR AERODYNAMICS, SHOCK WAVE ATTENUATION, TURBOFANS

N80-27161"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

A NUMERICAL TECHNIQUE FOR CALCULATION OF THE NOISE

OF HIGH-SPEED PROPELLERS WITH ADVANCED BLADE

GEOMETRY

P. A. NYSTROM and F. FARASSAT Jul. 1980 33 p refs

(NASA-TP-1662; L-13535) Avail: NTIS HC A03/MF A01

CSCL 20A

COMPUTER PROGRAMS, HIGH SPEED, NOISE PREDICTION

(AIRCRAFT), PROPELLER BLADES

N80-28150"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

TIME-OF-DAY CORRECTIONS TO AIRCRAFT NOISE METRICS

S. CLEVENSON, ed. and W. T. SHEPHERD, ed. (FAA) Jun.

1980 81 p Workshop held in Hampton, Va., 11-12 Mar. 1980;

sponsored by NASA and DOT

(NASA-CP-2135; FAA-EE-80-3; L-13779) Avail: NTIS HC

AO5/MF A01 CSCL 20A

CONFERENCES, ENVIRONMENTAL QUALITY, NOISE

MEASUREMENT, NOISE PREDICTION (AIRCRAFT), NOISE

TOLERANCE

N80-32188"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EXPERIMENTAL INVESTIGATION OF THE RADIATION OF

SOUND FROM AN UNFLANGED DUCT AND A BELLMOUTH,

INCLUDING THE FLOW EFFECT

J. M. VILLE (George Washington Univ.) and R. J. SILCOX Aug.

1980 65 p refs

(NASA-TP-1697; L-13252) Avail: NTIS HC A04/MF A01

CSCL 20A

ENGINE INLETS, ENGINE NOISE, NOISE PROPAGATION

N81-14788"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ASSESSMENT OF GROUND EFFECTS ON THE PROPAGATION

OF AIRCRAFT NOISE: THE T-38A FLIGHT EXPERIMENT

W. L. WlLLSHIRE, JR. Dec. 1980 128 p refs

(NASA°TP-1747; L-13765) Avail: NTIS HC A07/MF A01

CSCL 20A

AIRCRAFT NOISE, FLIGHT TESTS, GROUND EFFECT

(AERODYNAMICS), NOISE PROPAGATION

N81-21873"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SUBJECTIVE FIELD STUDY OF RESPONSE TO IMPULSIVE

HELICOPTER NOISE

C. A. POWELL Apr. 1981 43 p refs

(NASA-TP-1833; L-14205) Avail: NTIS HC A03/MF A01

CSCL 20A

AIRCRAFT NOISE, EFFECTIVE PERCEIVED NOISE LEVELS,

187
71 ACOUSTICS

HELICOPTERS, NOISE PREDICTION (AIRCRAFT),

PSYCHOACOUSTICS

N81-22832"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AIRFRAME NOISE OF A SMALL MODEL TRANSPORT

AIRCRAFT AND SCALING EFFECTS

J. G. SHEARIN May t981 27 p refs

(NASA-TP-1858; L-14257) Avail: NTIS HC A03/MF A01

CSCL 20A

AEROACOUSTICS, AIRCRAFT NOISE, AIRFRAMES, BOEING

747 AIRCRAFT, NOISE PREDICTION (AIRCRAFT), SCALE

EFFECT

N81-24854"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

STOCHASTIC ANALYSIS OF SPECTRAL BROADENING BY A

FREE TURBULENT SHEAR LAYER

J. C. HARDIN and J. S. PREISSER May 1981 27 p refs

(NASA-TP-1816; L-14444) Avail: NTIS HC A03/MF A01

CSCL 20A

AEROACOUSTICS, AMPLITUDE MODULATION, FREE JETS,

POWER SPECTRA, SHEAR LAYERS, SOUND PROPAGATION

N81-33945"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

FLIGHT TEST OF A PURE-TONE ACOUSTIC SOURCE

A. W. MUELLER and J. S. PREISSER Oct. 1981 39 p refs

(NASA-TP-1898; L-14600) Avail: NTIS HC A03/MF A01

CSCL 20A

AIRCRAFT NOISE, FLIGHT TESTS, NOISE MEASUREMENT,

NOISE PROPAGATION

N81-33946"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

NOISE SUPPRESSION CHARACTERISTICS OF PERIPHERALLY

SEGMENTED DUCT LINERS

W. R. WATSON Sep. 1981 43 p refs

(NASA-TP-1904; L-14521) Avail: NTIS HC A03/MF A01

CSCL 20A

AIRCRAFT ENGINES, DUCTS, ENGINE NOISE, LININGS,

NOISE REDUCTION

N81-33947"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

COMPUTER PROGRAM TO PREDICT AIRCRAFT NOISE

LEVELS

B. J. CLARK Sep. 1981 146 p

(NASA-TP-1913; E-733) Avail: NTIS HC A07/MF A01 CSCL

20A

COMPUTER PROGRAMS, JET AIRCRAFT NOISE, NOISE

PREDICTION (AIRCRAFT), SOUND INTENSITY

N82-14879"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EXPERIMENTAL STUDY OF NOISE REDUCTION FOR AN

UNSTIFFENED CYLINDRICAL MODEL OF AN AIRPLANE

FUSELAGE

C. M WILLIS and E. F_ DANIELS Dec. 1981 36 p refs

(NASA-TP-1964; L-14878) Avail: NTIS HC A03/MF A01

CSCL 20A

AIRFRAMES, FUSELAGES, NOISE MEASUREMENT, NOISE

REDUCTION

N82-21036"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

FORWARD ACOUSTIC PERFORMANCE OF A MODEL

TURBOFAN DESIGNED FOR A HIGH SPECIFIC FLOW (OF-14)

J. G. LUCAS, R. P. WOODWARD, and C. J. MICHELS Mar.

1982 20 p refs

(NASA-TP-1968; E-777; NAS 1.60:1968) Avail: NTIS HC

A02/MF A01 CSCL 20A

ENGINE DESIGN, ENGINE NOISE, JET AIRCRAFT NOISE,

NOISE REDUCTION, TIP SPEED, TURBOFAN ENGINES

188

N82-21037"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

FLUCTUATING PRESSURES ON FAN BLADES OF A TURBOFAN

ENGINE: STATIC AND WIND-TUNNEL INVESTIGATIONS

J. A. SCHOENSTER Mar. 1982 48 p refs

(NASAoTP-1976; L-14913; NAS 1.60:1976) Avail: NTIS HC

A03/MF A01 CSCL 21E

ENGINE NOISE, NOISE MEASUREMENT, STATIC TESTS,

TURBINE BLADES, TURBOFAN ENGINES, WIND TUNNEL

TESTS

N82-24052"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

A STUDY OF RESONANT-CAVITY AND FIBERGLASS-FILLED

PARALLEL BAFFLES AS DUCT SILENCERS

P. T. SODERMAN Apr. 1982 68 p refs

(NASA-TP-1970; NAS 1.60:1970; AVRADCOM-TR-81-A-2) Avail:

NTIS HC A04/MF A01 CSCL 20A

ACOUSTIC ATTENUATION, BAFFLES, CAVITY

RESONATORS, DUCTS, GLASS FIBERS, SILENCERS, SOUND

PROPAGATION, WIND TUNNEL APPARATUS

N82-24942"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

AEROACOUSTIC PERFORMANCE OF AN EXTERNALLY

BLOWN FLAP CONFIGURATION WITH SEVERAL FLAP NOISE

SUPPRESSION DEVICES

D. J. MCKINZIE, JR. May 1982 30 p refs

(NASA-TP-1995; E-573; NAS 1.60:1995) Avail: NTIS HC

A03/MF A01 CSCL 20A

AEROACOUSTICS, AERODYNAMIC NOISE, EXTERNALLY

BLOWN FLAPS, JET AIRCRAFT NOISE, NOISE REDUCTION

N82-31069"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

NOISE TRANSMISSION LOSS OF AIRCRAFT PANELS USING

ACOUSTIC INTENSITY METHODS

M. C. MCGARY Aug. 1982 37 p refs

(NASA-TP-2046; L-15306; NAS 1.60:2046) Avail: NTIS HC

A03/MF A01 CSCL 20A

AIRCRAFT NOISE, AIRCRAFT STRUCTURES, PANELS,

SOUND TRANSMISSION, TRANSMISSION LOSS

N82-31070"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AIRPORT/COMMUNITY NOISE

D. G. STEPHENS, comp. 1982 40 p Proceedings of a

Workshop held at Hampton, Va., 25-26 Feb. 1982

(NASA-CP-2241; L-1545; NAS 1.55:2241) Avail: NTIS HC

A03/MF A01 CSCL 13B

AIRPORTS, ENGINE NOISE, JET AIRCRAFT NOISE, NOISE

POLLUTION, NOISE REDUCTION

N82-34189"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SUPERSONIC JET NOISE GENERATED BY LARGE SCALE

INSTABILITIES

J. M. SEtNER, D. K. MCLAUGHLtN (Dynamics Technology, Inc.),

and C. H. LtU Sep. 1982 45 p refs

(NASA-TP-2072; L-15307; NAS 1.60:2072) Avail: NTIS HC

A03/MF A01 CSCL 20A

AIRCRAFT NOISE, FLOW DISTORTION, FLOW STABILITY,

REYNOLDS NUMBER, SHEAR LAYERS, SUPERSONIC JET

FLOW

N82-34190"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

CIRCUMFERENTIALLY SEGMENTED DUCT LINES OPTIMIZED

FOR AXISYMMETRIC AND STANDING WAVE SOURCES

W. R. WATSON 1982 50 p refs

(NASA-TP-2075; L-15316; NAS 1.60:2075) Avail: NTIS HC

A03/MF A01 CSCL 20A

ACOUSTIC DUCTS, AXISYMMETRIC FLOW, LININGS, NOISE
REDUCTION, OPTIMIZATION, STANDINGWAVES, TURBOFAN

ENGINES

N83-10883"#National Aeronautics andSpaceAdministration.

LangleyResearchCenter, Hampton, Va.

FLIGHT EFFECTS OF FAN NOISE

D. CHESTNUTT, ed. Sep. 1982 128 p refs Presented at

the Workshop on Res. on the Simulation of In-Flight Fan Noise

and Flight Effects, Hampton, Va., 26-27 Jan. 1982

(NASA-CP-2242; L-15493; NAS 1.55:2242) Avail: NTIS HC

A07/MF A01 CSCL 20A

AIRCRAFT NOISE, CONFERENCES, ENGINE NOISE, INTAKE

SYSTEMS, NOISE REDUCTION

N83-11838"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

A NEW MEASUREMENT METHOD FOR SEPARATING

AIRBORNE AND STRUCTUREBORNE NOISE RADIATED BY

AIRCRAFT TYPE PANELS

M. C. MCGARY Sep. 1982 33 p refs

(NASA-TP-2079; L-15481; NAS 1.60:2079) Avail: NTIS HC

A03/MF A01 CSCL 20A

ACOUSTIC MEASUREMENT, AERODYNAMIC NOISE,

AIRCRAFT NOISE, PANELS, SOUND INTENSITY, STRUCTURAL

VIBRATION

N83-16149"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EMPIRICAL SOURCE NOISE PREDICTION METHOD WITH

APPLICATION TO SUBSONIC COAXIAL JET MIXING NOISE

W. E. ZORUMSKI and D. S. WEIR (Kentron International, Inc.,

Hampton, Va.) Dec. 1982 77 p refs

(NASA-TP-2084; L-15382; NAS 1.60:2084) Avail: NTIS HC

A05/MF A01 CSCL 20A

COAXIAL NOZZLES, JET AIRCRAFT NOISE, JET MIXING

FLOW, NOISE PREDICTION (AIRCRAFT), NOISE REDUCTION,

SOUND GENERATORS

N83-30164"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

THE WEDGE HOT-FILM ANEMOMETER IN SUPERSONIC

FLOW

J. M. SEINER May 1983 58 p refs

(NASA-TP-2134; L-15538; NAS 1.60:2134) Avail: NTIS HC

A04/MF A01 CSCL 20A

ANEMOMETERS, HEAT TRANSFER, SUPERSONIC FLOW,

TURBULENT FLOW

N83-33684"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

INVESTIGATION OF JET-INSTALLATION NOISE SOURCES

UNDER STATIC CONDITIONS

J. G. SHEARIN Aug. 1983 33 p refs

(NASA-TP-2181; L-15599; NAS 1.61:2181) Avail: NTIS HC

A03/MF A01 CSCL 20A

AEROACOUSTICS, JET AIRCRAFT NOISE, JET EXHAUST,

NOISE GENERATORS, WING FLAPS, WING NACELLE

CONFIGURATIONS

N83-34713"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

RESIDENTS' ANNOYANCE RESPONSES TO AIRCRAFT NOISE

EVENTS

T. K. DEMPSEY, D. G. STEPHENS, J. M. FIELDS (Bionetics Corp.),

and K. P. SHEPHERD (Bionetics Corp.) Sep. 1983 42 p refs

(NASA-TP-2121; L-15595; NAS 1.60:2121) Avail: NTIS HC

A03/MF A01 CSCL 20A

AIRCRAFT NOISE, AIRPORTS, JET AIRCRAFT NOISE, NOISE

MEASUREMENT

71 ACOUSTICS

N84-10913"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

INVESTIGATION OF EFFECTS OF MICROPHONE POSITION

AND ORIENTATION ON NEAR-GROUND NOISE

MEASUREMENTS

W. L. WILLSHIRE, JR. and P. A. NYSTROM Apr. 1982 45 p

refs

(NASA-TP-2004; L-15097; NAS 1.60:2004) Avail: NTIS HC

A03/MF A01 CSCL 20A

ACOUSTICS, MICROPHONES, MOUNTING, NOISE

MEASUREMENT, POSITION (LOCATION)

N84-13923"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

THE COMPRESSIBLE AERODYNAMICS OF ROTATING BLADES

BASED ON AN ACOUSTIC FORMULATION

L. N. LONG Dec. 1983 70p refs

(NASA-TP-2197; L°15652; NAS 1.60:2197) Avail: NTIS HC

A04/MF A01 CSCL 20A

COMPRESSIBILITY EFFECTS, PROPELLER BLADES,

ROTATING BODIES, ROTOR AERODYNAMICS

N84-15894"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

FLUID SHIELDING OF HIGH-VELOCITY JET NOISE

J. H. GOODYKOONTZ Jan. 1984 22 p refs

(NASA-TP-2259; E-1705; NAS 1.60:2259) Avail: NTIS HC

A02/MF A01 CSCL 20A

EXHAUST NOZZLES, HIGH TEMPERATURE GASES, JET

AIRCRAFT NOISE, JET EXHAUST, NOISE REDUCTION,

SHIELDING

N84-19049"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

SIMPLIFIED COMBUSTION NOISE THEORY YIELDING A

PREDICTION OF FLUCTUATING PRESSURE LEVEL

R. G. HUFF Feb. 1984 17 p refs

(NASA-TP-2237; E-1856; NAS 1.60:2237) Avail: NTIS HC

A02/MF A01 CSCL 20A

COMBUSTION PHYSICS, NOISE MEASUREMENT,

PRESSURE MEASUREMENT

N84-21277"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

TEST-ENGINE AND INLET PERFORMANCE OF AN AIRCRAFT

USED FOR INVESTIGATING FLIGHT EFFECTS ON FAN NOISE

R. A. GOLUB and J. S. PREISSER Apr. 1984 70 p refs

(NASA-TP-2254; L-15653; NAS 1.60:2254) Avail: NTIS HC

A04/MF A01 CSCL 20A

DISTORTION, ENGINE TESTS, FLOW DISTRIBUTION,

POTENTIAL FLOW, STATIC TESTS, TURBOFAN ENGINES, WIND

TUNNEL TESTS

N84-22363"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

STUDY OF STATOR-VANE FLUCTUATING PRESSURES IN A

TURBOFAN ENGINE FOR STATIC AND FLIGHT TESTS

A. W. MUELLER Apr. 1984 54 p refs

(NASA-TP-2217; L-15657; NAS 1.60:2217) Avail: NTIS HC

A04/MF A01 CSCL 20A

ENGINE NOISE. ENGINE TESTS, FLIGHT TESTS, PRESSURE

OSCILLATIONS, ROTOR AERODYNAMICS, STATORS,

TURBOFAN ENGINES, VANES

N84-25422"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECTS OF SIMULATED FLIGHT ON THE STRUCTURE AND

NOISE OF UNDEREXPANDED JETS

T. D. NORUM and J. G. SHEARIN May 1984 32 p refs

(NASA-TP-2308; L-15760; NAS 1.60:2308) Avail: NTIS HC

A03/MF A01 CSCL 20A

CONVERGENT NOZZLES, FLIGHT SIMULATION, JET

AIRCRAFT NOISE, JET MIXING FLOW

189
71 ACOUSTICS

N84-27543"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

A NEW METHOD FOR DETERMINING ACOUSTIC-LINER

ADMITTANCE IN A RECTANGULAR DUCT WITH GRAZING

FLOW FROM EXPERIMENTAL DATA

W. R WATSON JuL t984 19 p refs

(NASA-TP-2310; L-15779; NAS 1.60:2310) Avail: NTiS HC

A02/MF A01 CSCL 20A

ACOUSTIC DUCTS, ACOUSTIC MEASUREMENT,

AEROACOUSTICS, ELECTRICAL IMPEDANCE, FLOW

DISTRIBUTION, FLOW VELOCITY, GRAZING FLOW

N84-29662"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ROTORCRAFT NOISE

R. J. HUSTON, comp. Washington Jul. 1982 424 p refs

Proc. of the NASA/US Helicopter Ind. Workshop on Aerodyn. Noise

Prediction/Noise Reduction, Hampton, Va., 29-31 Mar. 1982

(NASA-CP-2234; L-15408; NAS 1.55:2234) Avail: NTIS HC

A18/MF A01 CSCL 20A

AERODYNAMIC NOISE, HELICOPTERS, NOISE REDUCTION,

PREDICTION ANALYSIS TECHNIQUES

N84-32124"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ANNOYANCE CAUSED BY PROPELLER AIRPLANE FLYOVER

NOISE

D. A. MCCURDY and C. A. POWELL Aug. 1984 52 p refs

(NASA-TP-2356; L-15796; NAS 1.60:2356) Avail: NTIS HC

A04/MF A01 CSCL 20A

AIRCRAFT NOISE, PROPELLER BLADES, PSYCHOACOUSTICS, TOLERANCES (PHYSIOLOGY)

N85-11788"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ANALYSIS OF NOISE MEASURED FROM A PROPELLER IN A

WAKE

P. J. W. BLOCK Nov. 1984 49 p refs

(NASA-TP-2358; L-15808; NAS 1.60:2358) Avail: NTIS HC

A03/MF A01 CSCL 20A

AERODYNAMIC NOISE, AIRCRAFT WAKES, NOISE

MEASUREMENT, PROPELLERS, WIND TUNNEL TESTS

N85-11789"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

LOW-FREQUENCY SOUND ABSORPTION MEASUREMENTS IN

AIR

A. J. ZUCKERWAR and R. W. MEREDITH (Old Dominion Univ.)

Nov. 1984 48 p refs

(NASA-RP-1128; L-15831; NAS 1.61:1128) Avail: NTIS HC

A03/MF A01 CSCL 20A

Thirty sets of sound absorption measurements in air at a

pressure of 1 atmosphere are presented at temperatures from 10

C to 50 C, relative humidities from 0 to 100 percent, and frequencies

from 10 to 2500 Hz. The measurements were conducted by the

method of free decay in a resonant tube having a length of 18.261

m and bore diameter of 0.152 m. Background measurements in a

gas consisting of 89.5 percent N2 and 10.5 percent At, a mixture

which has the same sound velocity as air, permitted the wall and

structural losses of the tube to be separated from the constituent

absorption, consisting of classical rotational and vibrational

absorption, in the air samples. The data were used to evaluate

the vibrational relaxation frequencies of N2 and/or 02 for each of

the 30 sets of meteorological parameters. Over the full range of

humidity, the measured relaxation frequencies of N2 in air lie

between those specified by ANSI Standard $1.26-1978 and those

measured earlier in binary N2H20 mixtures. The measured

relaxation frequencies could be determined only at very low values

of humidity, reveal a significant trend away from the ANSI standard,

in agreement with a prior investigation. Author

190

N85-19790"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

FLUCTUATING PRESSURES ON FAN BLADES OF A TURBOFAN

ENGINE, FLIGHT TEST INVESTIGATION

J. A. SCHOENSTER Feb. 1985 26 p refs

(NASA-TP-2381; L-15700; NAS 1.60:2381) Avail: NTIS HC

A03/MF A01 CSCL 20A

AIRCRAFT NOISE, FAN BLADES, TURBOFAN ENGINES,

WIND TUNNEL TESTS

N85-22109"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

NOISE TRANSMISSION LOSS OF A RECTANGULAR PLATE IN

AN INFINITE BAFFLE

L. A. ROUSSOS Mar. 1985 36 p refs Presented at the

107th Meeting of the Acoustical Society of America, Norfolk, Va.,

7-10 May 1984

(NASA-TP-2398; L-15861; NAS 1.60:2398) Avail: NTIS HC

A03/MF A01 CSCL 20A

AERODYNAMIC NOISE, GREEN'S FUNCTIONS, INTEGRAL

EQUATIONS, NOISE PROPAGATION, RECTANGULAR PANELS,

TRANSMISSION LOSS

N85-29694"# National Aeronautics and Space Administration.

Lyndon B. Johnson Space Center, Houston, Tex.

CORRELATION OF PREDICTED AND MEASURED SONIC BOOM

CHARACTERISTICS FROM THE REENTRY OF STS-1

ORBITER

F. GARCIA, JR., J. H. JONES (NASA. Marshall Space Flight

Center), and H. R. HENDERSON (NASA. Langley Research

Center) Jun. 1985 49 p refs

(NASA-TP-2475; S-544; NAS 1.60:2475) Avail: NTIS HC

A03/MF A01 CSCL 20A

ACOUSTIC MEASUREMENT, COLUMBIA (ORBITER),

REENTRY EFFECTS, SONIC BOOMS

N85-30767"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EFFECTS OF PROPELLER ROTATION DIRECTION ON

AIRPLANE INTERIOR NOISE LEVELS

C. M. WILLIS, W. H. MAYES, and E. F. DANIELS Washington

Jul. 1985 34 p refs

(NASA-TP-2444; L-15892; NAS 1.60:2444) Avail: NTIS HC

A03/MF A01 CSCL 20A

AIRCRAFT COMPARTMENTS, AIRCRAFT NOISE, NOISE

REDUCTION, PROPELLER BLADES, TURBOPROP AIRCRAFT

N86-12007"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

NUMERICAL TECHNIQUES IN ACOUSTICS

K. J. BAUMEISTER, comp. Oct. 1985 35 p refs Meeting

held in Miami Beach, Fla., 17-21 Nov. 1985; sponsored by the

ASME

(NASA-CP-2404; E-2758; NAS 1.55:2404) Avail: NTIS HC

A03/MF A01 CSCL 20A

ACOUSTICS, BOUNDARY INTEGRAL METHOD, FINITE

ELEMENT METHOD, NOISE (SOUND), NOISE PREDICTION,

SOUND PRESSURE, VIBRATION

N86-13056"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

A METHOD FOR DETERMINING ACOUSTIC-LINER

ADMITTANCE IN DUCTS WITH SHEARED FLOW IN

TWO-CROSS-SECTIONAL DIRECTIONS

W. R. WATSON Oct. 1985 40 p refs

(NASA-TP-2518; L-15997; NAS 1.60:2518) Avail: NTIS HC

A03/MF A01 CSCL 20A

ACOUSTIC DUCTS, ACOUSTIC IMPEDANCE, ACOUSTIC

MEASUREMENT, ELECTRICAL IMPEDANCE, FLOW

DISTRIBUTION, GRAZING FLOW, IMPEDANCE PROBES,

LININGS, RETARDING, SHEAR FLOW
N86-16040"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ANALYTICAL STUDY OF ACOUSTIC RESPONSE OF A

SEMIREVERBERANT ENCLOSURE WITH APPLICATION TO

ACTIVE NOISE CONTROL

T. L. PARROTT, D. B. SCHEIN (George Washington Univ.,

Hampton, Va.), and D. GRIDLEY (Naval Avionics Center,

Indianapolis, Ind.) Dec. 1985 48 p refs

(NASA-TP-2472; L-15944; NAS 1.60:2472) Avail: NTIS HC

A03/MF A01 CSCL 20A

MODAL RESPONSE, NOISE PROPAGATION, NOISE

REDUCTION, REVERBERATION

N86-16041"# National Aeronautics and Space Administration,

Langley Research Center, Hampton, Va.

LOCATION OF NOISE SOURCES USING A PHASE-SLOPE

METHOD

R. DELOACH and J. S. PREISSER Nov. 1985 49 p refs

(NASA-TP-2505; L-15793; NAS 1.60:2505) Avail: NTIS HC

A03/MF A01 CSCL 20A

ACOUSTIC MEASUREMENT, BROADBAND, GRADIENTS,

MICROPHONES, NOISE GENERATORS, POSITION (LOCATION)

N86-21280"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

NEW TECHNIQUES FOR EXPERIMENTAL GENERATION OF

TWO-DIMENSIONAL BLADE-VORTEX INTERACTION AT LOW

REYNOLDS NUMBERS

E. BOOTH, JR. and J. C. YU Mar. 1986 27 p refs

(NASA-TP-2551; L-15981; NAS 1.60:2551) Avail: NTIS HC

A03/MF A01 CSCL 20A

FLOW VISUALIZATION, TWO DIMENSIONAL FLOW,

UNSTEADY FLOW, VORTEX GENERATORS

N86-24391"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

INTRODUCTION TO TIME SERIES ANALYSIS

J. C. HARDIN Mar. 1986 168 p refs

(NASA-RP-1145; L-15958; NAS 1.61:1145) Avail: NTIS HC

AO8/MF A01 CSCL 20A

The field of time series analysis is explored from its logical

foundations to the most modern data analysis techniques. The

presentation is developed, as far as possible, for continuous data,

so that the inevitable use of discrete mathematics is postponed

until the reader has gained some familiarity with the concepts.

The monograph seeks to provide the reader with both the

theoretical overview and the practical details necessary to correctly

apply the full range of these powerful techniques. In addition, the

last chapter introduces many specialized areas where research is

currently in progress. Author

N86o24393"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

CONSIDERATION OF SOME FACTORS AFFECTING

LOW-FREQUENCY FUSELAGE NOISE TRANSMISSION FOR

PROPELLER AIRCRAFT

J. S. MIXSON and L. A. ROUSSOS Apr. 1986 28 p refs

(NASA-TP-2552; L-14994; NAS 1.60:2552) Avail: NTIS HC

A03/MF A01 CSCL 20A

AERODYNAMIC NOISE, AIRCRAFT NOISE, NOISE

PROPAGATION, NOISE SPECTRA, PLANE WAVES, SOUND

WAVES

N86-26162"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EXPERIMENTAL STUDY OF THE EFFECTS OF INSTALLATION

ON SINGLEAND COUNTER-ROTATION PROPELLER NOISE

P. J, W. BLOCK Apr. 1986 33 p refs Original contains

color illustrations

(NASA-TP-2541; L-16046; NAS 1.60:2541) Avail: NTIS HC

A03/MF A01 CSCL 20A

CONTRAROTATING PROPELLERS, NOISE (SOUND), NOISE

72 ATOMIC AND MOLECULAR PHYSICS

MEASUREMENT, PROPELLER SLIPSTREAMS, PYLONS,

UNSTEADY FLOW

N86-27043"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

PRESSURE PROBE AND HOT-FILM PROBE RSPONSES TO

ACOUSTIC EXCITATION IN MEAN FLOW

T. L. PARROTT and M. G. JONES (PRC Kentron, Inc., Hampton,

Va.) Jun. 1986 56 p refs

(NASA-TP-2581; L-16079; NAS 1.60:2581) Avail: NTIS HC

A04/MF A01 CSCL 20A

ACOUSTIC EXCITATION, ACOUSTIC MEASUREMENT,

DUCTED FLOW, HOT-FILM ANEMOMETERS, PRESSURE

OSCILLATIONS, PRESSURE SENSORS, SUBSONIC FLOW

N86-31337"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ACOUSTIC TREATMENT OF THE NASA LANGLEY 4- BY

7-METER TUNNEL: A FEASIBILITY STUDY

J. C. YU and A. L. ABRAHAMSON (Comtek, Grafton, Va.) Aug.

1986 38 p

(NASA-TP-2563; L-16037; NAS 1.60:2563) Avail: NTIS HC

A03/MF A01 CSCL 20A

ACOUSTIC PROPERTIES, AEROACOUSTICS, AIRCRAFT

NOISE, ANECHOIC CHAMBERS, FEASIBILITY ANALYSIS,

HELICOPTERS, WIND TUNNELS

N86-31341"# National Aeronautics and Space Administration,

Langley Research Center, Hampton, Va.

DIRECTIVITY AND TRENDS OF NOISE GENERATED BY A

PROPELLER IN A WAKE

P. J. W. BLOCK and C. L. GENTRY, JR. Sep. 1986 63 p

(NASA-TP-2609; L-16131; NAS 1.60:2609) Avail: NTIS HC

A04/MF A01 CSCL 20A

ACOUSTIC MEASUREMENT, AERODYNAMIC NOISE,

AIRCRAFT WAKES, DIRECTIVITY, PROPELLERS

72

ATOMIC AND MOLECULAR PHYSICS

Includes atomic structure, electron properties, and molecular

spectra.

N78-20927"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

THE OPTICAL ABSORPTION OF TRIATOMIC CARBON C3 FOR

THE WAVELENGTH RANGE 260 TO 560 NM

J. J. JONES Mar. 1978 61 p refs

(NASA-TP-1141; L-11871) Avail: NTIS HC A04/MF A01

CSCL 20H

ABSORPTION CROSS SECTIONS, CARBON,

ELECTROMAGNETIC ABSORPTION, TRIATOMIC MOLECULES

N79-25861"# National Aeronautics and Space Administration,

John F. Kennedy Space Center, Cocoa Beach, Fla.

ELECTRICAL ENCLOSURE HYDROGEN INTRUSION STUDY

P. J. WELCH and J. N. YANTSIOS Jun. 1979 34 p refs

(NASA-TP.1461; KSC-TR-72-1) Avail: NTIS HC A03/MF A01

CSCL 21B

CAPE KENNEDY LAUNCH COMPLEX, ELECTRIC

EQUIPMENT, ENCLOSURES, GASEOUS DIFFUSION,

HYDROGEN, PURGING

191
72 ATOMICANDMOLECULARPHYSICS

N80-26125"#National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

REVIEW OF SPECTROSCOPIC DATA FOR MEASUREMENTS

OF STRATOSPHERIC SPECIES

A. GOLDMAN, ed. (Denver Univ.) and J. M. HOELL, JR., ed.

Jun. 1980 34 p Workshop held at Hampton, Va., 29-30 Oct.

t979

(NASA-CP-2136; L-13768) Avail: NTIS HC A03/MF A01

CSCL 20H

ATMOSPHERIC COMPOSITION, GAS COMPOSITION,

MOLECULAR SPECTROSCOPY

N82-15853"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ATLAS OF ABSORPTION LINES FROM 0 TO 17 900 CM(-1)

J. H. PARK, L. S. ROTHMAN (AFGL), C. P. RINSLAND (Colt. of

William and Mary, Williamsburg, Va.), M. A. H. SMITH, D. J.

RICHARDSON (Systems and Applied Sciences Corp., Hampton,

Va.), and J. C. LARSEN (Systems and Applied Sciences Corp.,

Hampton, Va.) Washington Dec. 1981 209 p refs

(NASA-RP-1084; L-14720) Avail: NTIS HC A10/MF A01

CSCL 07D

Plots of absorption line strength versus line position for

wavenumbers from 0 to 17,900 cm(-1) are shown for 20

atmospheric gases (H20, CO2, 03, N20, CO, CH4, 02, NO, SO2,

NO2, NH3, HNO3, OH, HF, HCI, HBr, HI, CtO, OCS, H2CO). Also

shown are similar plots of lower-state energy values for adsorption

lines for the strongly adsorbing atmospheric gases (H20, CO2,

03, and CH4) for wavenumbers from 0 to 5000 cm(-1). MG.

73

NUCLEAR AND HIGH-ENERGY PHYSICS

Includes elementary and nuclear particles; and reactor theory.

N81-27899"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

OPTICAL-MODEL ABRASION CROSS SECTIONS FOR

HIGH-ENERGY HEAVY IONS

L. W. TOWNSEND Jul. 1981 18 p refs

(NASA-TP-1893; L-14554) Avail: NTIS HC A02/MF A01

CSCL 20H

EIKONAL EQUATION, GLAUBER THEORY, HEAVY IONS,

SCATTERING CROSS SECTIONS

N82-23003"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

HARMONIC WELL MATTER DENSITIES AND PAULI

CORRELATION EFFECTS IN HEAVY-ION COLLISIONS

L. W. TOWNSEND Apr. 1982 31 p refs

(NASA-TP-2003; L-15105; NAS 1.60:2003) Avail: NTIS HC

A03/MF A01 CSCL 20H

HARMONIC MOTION, HEAVY IONS, ION DENSITY

(CONCENTRATION), IONIC COLLISIONS, PAULI EXCLUSION

PRINCIPLE

N83-27809°# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

RATE PROCESSES IN GAS PHASE

C. F. HANSEN May 1983 263 p refs

(NASA-RP-1090; A-8817; NAS 1.61:1090) Avail: NTIS HC

A12/MF A01 CSCL 20H

Reaction-rate theory and experiment are given a critical review

from the engineers' point of view. Rates of heavy-particle,

collision-induced reaction in gas phase are formulated in terms of

the cross sections and activation energies for reaction. The effect

of cross section function shape and of excited state contributions

to reaction both cause the slope of Arrhenius plots to differ from

the true activation energy, except at low temperature. The master

equations for chemically reacting gases are introduced, and

dissociation and ionization reactions are shown to proceed primarily

from excited states about kT from the dissociation or ionization

limit. Collision-induced vibration, vibration-rotation, and pure rotation

transitions are treated, including three-dimensional effects and

conservation of energy, which have usually been ignored. The

quantum theory of transitions at potential surface crossing is

derived, and results are found to be in fair agreement with

experiment in spite of some questionable approximations

involved. Author

N83-23140"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

HEAVY-ION TOTAL AND ABSORPTION CROSS SECTIONS

ABOVE 25 MEVlNUCLEON

L. W. TOWNSEND, J. W. WILSON, and H. B. BIDASARIA (Old

Dominion Univ.) Apr. 1983 44 p refs

(NASA-TP-2138; L-15566; NAS 1.60:2138) Avail: NTIS HC

A03/MF A01 CSCL 20H

ABSORPTION CROSS SECTIONS, HEAVY IONS, NUCLEAR

INTERACTIONS, NUCLEON-NUCLEON SCATTERING

N84-13978"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

A SIMPLE MODEL OF SPACE RADIATION DAMAGE IN GAAS

SOLAR CELLS

J. W. WILSON, J. J. STITH (Virginia State Univ., Petersburg), and

L. V. STOCK (Old Dominion Univ., Norfolk, Va.) Dec. 1983 31

p refs

(NASA-TP-2242; L-15689; NAS 1.60:2242) Avail: NTIS HC

A03/MF A01 CSCL 20H

GALLIUM ARSENIDES, RADIATION DAMAGE,

SEMICONDUCTOR JUNCTIONS, SOLAR CELLS

N86-13064"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

REVIEW OF SPECTROSCOPIC PARAMETERS FOR UPPER

ATMOSPHERIC MEASUREMENTS

M. A. H. SMITH, ed. Oct. 1985 28 p refs Presented at the

Spectroscopic Parameters Workshop, Hampton, Va., 17-19 Oct.

1984

(NASA-CP-2396; L-16022; NAS 1.55:2396) Avail: NTIS HC

A03/MF A01 CSCL 04A

CONFERENCES, MOLECULAR SPECTROSCOPY, REMOTE

SENSING, UPPER ATMOSPHERE

N84-22396°# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AN ABRASION-ABLATION MODEL DESCRIPTION OF

GALACTIC HEAVY-ION FRAGMENTATION

L. W. TOWNSEND, J. W. WILSON, J. W. NORBURY (Old Dominion

Univ.), and H. B. BIDASARIA (Old Dominion Univ.) Apr. 1984

20 p refs

(NASA-TP-2305; L-15763; NAS 1.60:2305) Avail: NTIS HC

A02/MF A01 CSCL 03B

ABLATION, ABRASION, FRAGMENTATION, GALACTIC

RADIATION, HEAVY IONS, NUCLEAR INTERACTIONS,

QUANTUM MECHANICS

192
N84-26398"#National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

A STOCHASTIC MODEL FOR PHOTON NOISE INDUCED BY

CHARGED PARTICLES IN MULTIPLIER PHOTOTUBES OF THE

SPACE TELESCOPE FINE GUIDANCE SENSORS

L. W. HOWELL and H. F. KENNEL Jun. 1984 67 p refs

(NASA-TP-2337; NAS 1.60:2337) Avail: NTIS HC A04/MF A01

CSCL 03A

CERENKOV RADIATION, GUIDANCE SENSORS,

SPACEBORNE TELESCOPES, SPACECRAFT CHARGING

N85-17690"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

A T-MATRIX THEORY OF GALACTIC HEAVY-ION

FRAGMENTATION

J. W. NORBURY, L. W. TOWNSEND, and P. A. DEUTCHMAN

Jan. 1985 29 p refs

(NASA-TP°2363; L-15833; NAS 1.60:2363) Avail: NTIS HC

A03/MF A01 CSCL 038

ABLATION, ABRASION, COSMIC RAYS, FRAGMENTATION,

HEAVY IONS, MATRIX THEORY

N85-27865"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

TABLES OF NUCLEAR CROSS SECTIONS FOR GALACTIC

COSMIC RAYS: ABSORPTION CROSS SECTIONS

L. W. TOWNSEND and J. W. WILSON May 1985 33 p refs

(NASA-RP-1134; L-15891; NAS 1.61:1134) Avail: NTIS HC

A03/MF A01 CSCL 03B

A simple but comprehensive theory of nuclear reactions is

presented. Extensive tables of nucleon, deuteron, and heavy-ion

absorption cross sections over a broad range of energies are

generated for use in cosmic ray shielding studies. Numerous

comparisons of the calculated values with available experimental

data show agreement to within 3 percent for energies above 80

MeV/nucleon and within approximately 10 percent for energies

as low as 30 MeV/nucleon. These tables represent the culmination

of the development of the absorption cross section formalism and

supersede the preliminary absorption cross sections published

previously in NASA TN D-8107, NASA TP-2138, and NASA

TM-84636. Author

N86-21297"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SECOND QUANTIZATION TECHNIQUES IN THE SCATTERING

OF NONIDENTICAL COMPOSITE BODIES

J. W. NORBURY (Old Dominion Univ., Norfolk, Va.), L. W.

TOWNSEND, and P. A. DEUTCHMAN (Idaho Univ., Moscow) Jan.

1986 18 p refs

(NASA-TP-2522; L-16016; NAS 1.60:2522) Avail: NTIS HC

A02/MF A01 CSCL 30H

ANNIHILATION REACTIONS, ELASTIC SCATTERING,

NUCLEON-NUCLEON INTERACTIONS

N86-23388"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SYMMETRY CONSIDERATIONS IN THE SCATTERING OF

IDENTICAL COMPOSITE BODIES

J. W. NORBUFtY (Old Dominion Univ., Norfolk, Va.), L. W.

TOWNSEND, and P. A. DEUTCHMAN (Idaho Univ., Moscow)

1986 19p refs

(NASA-TP-2548; L-16035; NAS 1.60:2548) Avail: NTIS HC

A02/MF A01 CSCL 20H

COMPOSITE MATERIALS, HOLES (ELECTRON

DEFICIENCIES), MATHEMATICAL MODELS, PROJECTILES,

TARGETS

74 OPTICS

N86-30485"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

CROSS SECTION CALCULATIONS FOR SUBTHRESHOLD PION

PRODUCTION IN PERIPHERAL HEAVY-ION COLLISIONS

J. W. NORBURY (Old Dominion Univ., Norfolk, Va.), F. A.

CUCINOTTA, P. A. DEUTCHMAN (Idaho Univ., Moscow.), and L.

W. TOWNSEND Aug. 1986 27 p

(NSF PHY-84-11009)

(NASA-TP-2600; L-16129; NAS 1.60:2600) Avail: NTIS HC

A03/MF A01 CSCL 20H

CARBON 12, HEAVY IONS, NUCLEI (NUCLEAR PHYSICS),

PARTICLE COLLISIONS, PIONS

74

OPTICS

Includes light phenomena; and optical devices.

N78-11812"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

PERFORMANCE ANALYSIS OF GRAZING INCIDENCE IMAGING

SYSTEMS

C. E. WlNKLER and D. KORSCH (Teledyne Brown Engineering,

Huntsville, Ala.) Nov. 1977 40 p refs

(NASA-TP-1088; M-241) Avail: NTIS HC A03/MF A01 CSCL

20F

ABERRATION, IMAGING TECHNIQUES, INCIDENCE,

INCIDENT RADIATION, OPTICS, SYSTEM EFFECTIVENESS, X

RAY TELESCOPES

N78-12829"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ANALYSIS AND DESIGN OF A REFRACTIVE VIRTUAL IMAGE

SYSTEM

W. M. KAHLBAUM Washington Nov. 1977 76 p refs

(NASA-TP-1066; L-11678) Avail: NTIS HC A05/MF A01

CSCL 20F

FLIGHT SIMULATORS, IMAGE INTENSIFIERS, IMAGE TUBES,

LENS DESIGN, VISUAL PERCEPTION

N78-20948"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

OPTICAL AND HOLOGRAPHIC STORAGE PROPERTIES OF F3,

CU, AND MG-DOPED LITHIUM NIOBATE

M. E. BEATTY, III and B. D. MEREDITH Mar. 1978 18 p refs

(NASA-TP-1144; L-11964) Avail: NTIS HC A02/MF A01

CSCL 20F

DATA STORAGE, HOLOGRAPHY, LITHIUM NIOBATES,

OPTICAL DATA PROCESSING

N78-27906"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

INVESTIGATION OF LIGHT SCATTERING AS A TECHNIQUE

FOR DETECTING DISCRETE SOOT PARTICLES IN A

LUMINOUS FLAME

Jul. 1978 21 p refs

(NASA-TP-1235; L-12130) Avail: NTIS HC A02/MF A01

CSCL 20F

FLAMES, LIGHT SCATTERING, OPTICAL MEASURING

INSTRUMENTS, SOOT

193
74 OPTICS

N81-13739"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

SPATIAL FREQUENCY RESPONSE OF AN OPTICAL

HETERODYNE RECEIVER

D. M. ROBINSON and C. L. FALLS Dec. 1980 24 p refs

(NASA-TP-1763; L-14099) Avail: NTIS HC A02/MF A01

CSCL 20F

IMAGING TECHNIQUES, MODULATION TRANSFER

FUNCTION, OPTICAL HETERODYNING, OPTICAL TRANSFER

FUNCTION

N82-15894*# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

OPTICAL INFORMATION PROCESSING FOR AEROSPACE

APPLICATIONS

Dec. 1981 347 p refs Conf. held in Hampton, Va., 18-19

Aug. 1981

(NASA-CP-2207; L-15018) Avail: NTIS HC A15/MF A01

CSCL 20F

AIRCRAFT EQUIPMENT, CONFERENCES, INTEGRATED

OPTICS, OPTICAL DATA PROCESSING, OPTICAL

WAVEGUIDES

N83-13979"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

LARGE-APERTURE INTERFEROMETER USING LOCAL

REFERENCE BEAM

W. L. HOWLS Nov. 1982 20p refs

(NASA-TP-2060; E-1153; NAS t.60:2060) Avail: NTIS HC

A02/MF A01 CSCL 20F

INTERFEROMETERS, LENSES, PARABOLOID MIRRORS

N83-27846"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

DEVELOPMENT OF A SIMPLIFIED OPTICAL TECHNIQUE FOR

THE SIMULTANEOUS MEASUREMENT OF PARTICLE SIZE

DISTRIBUTION AND VELOCITY

J. L SMITH Jun. 1983 33 p refs

(NASA-TP-2185; M-413; NAS 1.60:2185) Avail: NTIS HC

A03/MF A01 CSCL 20F

FLUIDIZED BED PROCESSORS, LASER ANEMOMETERS,

OPTICAL MEASURING INSTRUMENTS, PARTICLE SIZE

DISTRIBUTION

N84-22402"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

OPTICAL INFORMATION PROCESSING FOR AEROSPACE

APPLICATIONS 2

R. L. STERMER, comp. Washington Mar. 1984 261 p refs

Conf. held in Hampton, Va., 30-31 Aug. 1983

(NASA-CP-2302; L-15754; NAS 1.55:2302) Avail: NTIS HC

A12/MF A01 CSCL 20F

AEROSPACE SCIENCES, CIRCUITS, CONFERENCES,

INFORMATION SYSTEMS, MATERIALS SCIENCE, OPTICAL

DATA PROCESSING, SIGNAL GENERATORS

N86-17140"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

SINGLE SCATTERING FROM NONSPHERICAL CHEBYSHEV

PARTICLES: A COMPENDIUM OF CALCULATIONS

W. J. WISCOMBE and A. MUGNAI (Colorado State Univ., Fort

Collins) Jan. 1986 282 p refs

(NASA-RP-1157; REPT-613; NAS 1.61:1157) Avail: NTIS HC

A13/MF A01 CSCL 20F

A large set of exact calculations of the scattering from a class

of nonspherical particles known as Chebyshev particles' has been

performed. Phase function and degree of polarization in random

orientation, and parallel and perpendicular intensities in fixed

orientations, are plotted for a variety of particles shapes and sizes.

The intention is to furnish a data base against which both

experimental data, and the predictions of approximate methods,

can be tested. The calculations are performed with the widely-used

Extended Boundary Condition Method. An extensive discussion of

194

this method is given, including much material that is not easily

available elsewhere (especially the analysis of its convergence

properties). An extensive review is also given of all extant methods

for nonspherical scattering calculations, as well as of the available

pool of experimental data. Author

N86-22390°# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

OPTICAL ELEMENTS FORMED BY COMPRESSED GASES:

ANALYSIS AND POTENTIAL APPLICATIONS

W. L. HOWLS 1986 24p refs

(NASA-TP-2555; E-2561; NAS 1.60:2555) Avail: NTIS HC

A02/MF A01 CSCL 20F

FLOW VISUALIZATION, GAS DYNAMICS, INTERFEROMETERS, LENSES, SCHLIEREN PHOTOGRAPHY

75

PLASMA PHYSICS

Includes magnetohydrodynamics and plasma fusion.

N78-20959"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

TEMPERATURE DISTRIBUTIONS OF A CESIUM-SEEDED

HYDROGEN-OXYGEN SUPERSONIC FREE JET

S. Y. WANG and J. M. SMITH Feb. 1978 24 p refs

(NASA-TP-1162; E-9267) Avail: NTIS HC A02/MF A01 CSCL

201

EMISSION SPECTRA, PLASMA JETS, TEMPERATURE

DISTRIBUTION

N78-21922"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

EFFECT OF ANODE-CATHODE GEOMETRY ON

PERFORMANCE OF THE HIP-1 HOT ION PLASMA

M. R. LAUVER Apr. 1978 25 p refs

(NASA-TP-1201; E-9386) Avail: NTIS HC A02/MF A0t CSCL

201

ANODES, HOLLOW CATHODES, ION TEMPERATURE,

MAGNETIC MIRRORS, PLASMA ELECTRODES

N78-26927"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

FLUCTUATION SPECTRA IN THE NASA LEWIS BUMPY-TORUS

PLASMA

C. M. SINGH, W. M. KRAWCZONEK, J. R. ROTH, J. Y. HONG,

and E. J. POWERS Jun. 1978 31 p refs

(NASA-TP-1257; E-8696) Avail: NTIS HC A03/MF A01 CSCL

201

MAGNETOHYDRODYNAMIC STABILITY, PLASMA

DIAGNOSTICS, PLASMA DIFFUSION, SPECTRUM ANALYSIS,

TOROIDAL PLASMAS

N78-30944"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

LOW-FREQUENCY FLUCTUATION SPECTRA AND

ASSOCIATED PARTICLE TRANSPORT IN THE NASA LEWIS

BUMPY-TORUS PLASMA

C. M, SINGH, W. M. KRAWCZONEK, J. R. ROTH, J. Y. HONG

(Texas Univ., Austin), Y. C. KIM (Texas Univ.,Austin), and E. J.

POWERS (Texas Univ., Austin) Aug. 1978 53 p refs

(NASA-TP-1258; E-9565) Avail: NTIS HC A04/MF A01 CSCL

201

FLUCTUATION THEORY, PLASMA DIAGNOSTICS, PLASMA

DIFFUSION, RADIAL DISTRIBUTION, TRANSPORT THEORY
N79-19867"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

ION CONFINEMENT AND TRANSPORT IN A TOROIDAL

PLASMA WITH EXTERNALLY IMPOSED RADIAL ELECTRIC

FIELDS

J. R. ROTH, W. M. KRAWCZONEK, E. J. POWERS (Texas Univ.

Austin), Y. C. KIM (Texas Univ., Austin), and H. Y. HONG (Texas

Univ., Austin) Mar. 1979 86 p refs

(NASA-TP-1411; E-9754) Avail: NTIS HC A05/MF A01 CSCL

201

ELECTRIC FIELDS, IONIC MOBILITY, PLASMA CONTROL,

TOROIDAL PLASMAS, TRANSPORT PROPERTIES

N84-25458"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

MAGNETOHYDRODYNAMIC POWER GENERATION

J. L. SMITH May 1984 36 p refs

(NASA-TP-2331; NAS 1.60:2331) Avail: NTIS HC A03/MF A01

CSCL 201

COMBUSTION, ELECTRIC FIELDS, FLOW DISTRIBUTION,

LIQUID METALS, MAGNETIC FIELDS, MAGNETOHYDRODYNAMICS

76

SOLID-STATE PHYSICS

Includes superconductivity.

N79-13886"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

IONIZED DOPANT CONCENTRATIONS AT THE HEAVILY

DOPED SURFACE OF A SILICON SOLAR CELL

I. WEINBERG, J. D_ BRODER, G A. MAZARIS, JR., and L. HSU

Dec. 1978 19p refs

(NSG-3014)

(NASA-TP-1347; E-9629) Avail: NTIS HC A02/MF A01 CSCL

10B

ADDITIVES, CONCENTRATION (COMPOSITION), METAL

OXIDE SEMICONDUCTORS, SOLAR CELLS

N83-21991"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

A STUDY OF PRODUCTION OF MISlBILITY GAP ALLOYS WITH

CONTROLLED STRUCTURES

R. A. PARR, M. H. JOHNSTON, J. A. BURKA, J. H. DAVIS, and

J.A. LEE Mar. 1983 43 p refs

(NASA-TP-2144; NAS 1.60:2144) Avail: NTIS HC A03/MF A01

CSCL 20L

ALLOYS, DIRECTIONAL SOLIDIFICATION (CRYSTALS),

METAL MATRIX COMPOSITES, SUPERCONDUCTIVITY

N85-24961"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

MONTE CARLO LATTICE MODELS FOR ADSORBED POLYMER

CONFORMATION

B.S. GOOD May 1985 12p refs

(NASA-TP-2453; E-2400; NAS 1.60:2453) Avail: NTIS HC

A02/MF A01 CSCL 20L

ADHESION, CRYSTAL LATTICES, METALS, MONTE CARLO

METHOD, POLYMERIC FILMS, RANDOM WALK, SURFACE

PROPERTIES

77 THERMODYNAMICS AND STATISTICAL PHYSICS

77

THERMODYNAMICS AND STATISTICAL PHYSICS

Includes quantum mechanics; theoretical physics; and Bose and

Fermi statistics.

N79-13901"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

AEROTHERMAL TESTS OF A HEAT-PIPE-COOLED LEADING

EDGE AT MACH 7

C. J. CAMARDA Nov. 1978 39 p refs

(NASA-TP-1320; L-12302) Avail: NTIS HC A03/MF A01

CSCL 20N

AEROTHERMODYNAMICS, COOLING, HEAT PIPES,

HYPERSONIC HEAT TRANSFER, LEADING EDGES, SPACE

SHUTTLE ORBITERS

N82-32186"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

THERMODYNAMIC AND TRANSPORT COMBUSTION

PROPERTIES OF HYDROCARBONS WITH AIR. PART 1:

PROPERTIES IN SI UNITS

S. GORDON Jul. 1982 397 p refs

(NASA-TP-1906; E-946; NAS 1.60:1906) Avail: NTIS HC

A17/MFA01 CSCL20M

COMBUSTION PHYSICS, HYDROCARBON COMBUSTION,

THERMODYNAMIC PROPERTIES, TRANSPORT PROPERTIES

N82-32187"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

THERMODYNAMIC AND TRANSPORT COMBUSTION

PROPERTIES OF HYDROCARBONS WITH AIR. PART 2:

COMPOSITIONS CORRESPONDING TO KELVIN

TEMPERATURE SCHEDULES IN PART 1

S. GORDON Jul. 1982 281 p refs

(NASA-TP-1907; E-947; NAS 1.60:1907) Avail: NTIS HC

A13/MF A01 CSCL 20M

CHEMICAL COMPOSITION, COMBUSTION PHYSICS,

HYDROCARBON COMBUSTION, THERMODYNAMIC

PROPERTIES, TRANSPORT PROPERTIES

N82-32188"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

THERMODYNAMIC AND TRANSPORT COMBUSTION

PROPERTIES OF HYDROCARBONS WITH AIR. PART 3:

PROPERTIES IN US CUSTOMARY UNITS

S. GORDON Jul. 1982 362 p refs

(NASA-TP-1908; E-948; NAS 1.60:1908) Avail: NTIS HC

A16/MF A01 CSCL 20M

COMBUSTION PHYSICS, HYDROCARBON COMBUSTION,

THERMODYNAMIC PROPERTIES, TRANSPORT PROPERTIES

N82-32189"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

THERMODYNAMIC AND TRANSPORT COMBUSTION

PROPERTIES OF HYDROCARBONS WITH AIR. PART 4:

COMPOSITIONS CORRESPONDING TO RANKINE

TEMPERATURE SCHEDULES IN PART 3

S. GORDON Jul. 1982 281 p refs

(NASA-TP-1909; E-949; NAS 1.80:1909) Avail: NTIS HC

A18/MFA01 CSCL20M

CHEMICAL COMPOSITION, COMBUSTION PHYSICS,

HYDROCARBON COMBUSTION, THERMODYNAMIC

PROPERTIES, TRANSPORT PROPERTIES

195
77 THERMODYNAMICS AND STATISTICAL PHYSICS

N83-23188"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

A CLASS OF NONIDEAL SOLUTIONS. 2: APPLICATION TO

EXPERIMENTAL DATA

F. J. ZELEZNIK and L. F. DONOVAN Apr. 1983 55 p refs

(NASA-TP-1930; E-020; NAS t.60:1930) Avail: NTIS HC

A04/MF A01 CSCL 20M

ELECTROLYTES, FUNCTIONS (MATHEMATICS), GIBBS FREE

ENERGY, LEAST SQUARES METHOD, SOLUTIONS,

THERMODYNAMIC PROPERTIES

N83-23189"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

A CLASS OF NONIDEAL SOLUTIONS. 1: DEFINITION AND

PROPERTIES

F. J. ZELEZNIK Apr. 1983 43 p refs

(NASA-TP-1929; E-021; NAS 1.60:1929) Avail: NTIS HC

A03/MF A01 CSCL 20M

ENTHALPY, HEAT OF SOLUTION, PHYSICAL CHEMISTRY,

SOLUTIONS, THERMODYNAMICS

80

SOCIAL SCIENCES (GENERAL)

Includes educational matters.

N82-14955"# National Aeronautics and Space Administration,

Washington, D.C.

ORDERS OF MAGNITUDE: A HISTORY OF NACA AND NASA,

1915- 1980

F, W. ANDERSON, JR. 1981 113 p refs

(NASA-SP-4403) Avail: NTIS MF A01; HC SOD $4,75 CSCL

05D

The history of NACA and NASA from 1915 to 1980 is narrated.

The impact of two world wars on aeronautics is reviewed, Research

activity before and during World War II is presented. Postwar

exploitation of new technologies is summarized. The creation of

NASA and a comprehensive space program is discussed. Long

range planning for a lunar mission is described. The Gemini project

is reviewed. The Apollo project and side effects includng NASA's

university and technology transfer programs are presented.

Numerous scientific and application satellite projects are reviewed.

The impact of budget reductions is explained. The value of space

exploration is emphasized. Development of the Space Shuttle is

reported. N .W.

N85-24994"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

THE IMPACT OF SCIENCE ON SOCIETY

J. BURKE, J. BERGMAN, and I. ASIMOV 1985 98 p Lectures

held in Williamsburg, Va., 1983

(NASA-SP-482; L-15858; NAS 1.21:482; LC-84-14159) Avail:

NTIS HC A05/MF A01; SOD HC $4.50 as SN033-000-00943-7

CSCL 05K

Four speeches delivered as part of a public lecture series to

assess the impact of science on society are presented. The

computerization of society, space exploration and habitation, the

mechanisms of technological change, and cultural responses are

addressed. For individual titles see N85-24995 through

N85-24998.

81

ADMINISTRATION AND MANAGEMENT

Includes management planning and research.

N79-16709"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

A CRITICAL REVIEW OF THE LIFE SCIENCES PROJECT

MANAGEMENT AT AMES RESEARCH CENTER FOR THE

SPACELAB MISSION DEVELOPMENT TEST 3

R. L. HELMREICH (Texas Univ., Austin), J. M. WILHELM (Texas

Univ., Austin), T. A. TANNER (California State Univ., Hayward), J.

E. SIEBER (Texas Univ., Austin), and S. F. BURGENBAUCH Jan.

1979 66p refs

(NSG-2065; NCA2-OR290-705)

(NASA-TP-1364; A-7536) Avail: NTIS HC A04/MF A01 CSCL

05A

PROJECT MANAGEMENT, SPACE MISSIONS, SPACELAB

N79-19912"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

MANAGEMENT SYSTEM, ORGANIZATIONAL CLIMATE AND

PERFORMANCE RELATIONSHIPS

B. D. DAVIS Feb. 1979 38 p refs

(NASA-TP-1417; M-281) Avail: NTIS HC A03/MF A01 CSCL

05A

DECISION MAKING, MANAGEMENT SYSTEMS,

PSYCHOLOGICAL FACTORS

N83-18551"# National Aeronautics and Space Administration,

Washington, D.C.

MANAGING NASA IN THE APOLLO ERA

A. S. LEVINE 1982 359 p refs

(NASA-SP-4102; NAS 1.2t:4102) Avail: NTIS HC A16/MF A01

CSCL 05A

The administration and organization are described and analyzed.

Policies on manpower and the budgetary process for contracting

for research development, the structure of NASA-DOD relations,

and program planning are discussed. S.L.

N85-16665"# National Aeronautics and Space Administration,

Washington, D.C.

THE MANAGEMENT OF RESEARCH INSTITUTIONS: A LOOK

AT GOVERNMENT LABORATORIES

H. MARK and A. LEVINE 1984 311 p refs

(NASA-SP-481; NAS 1.21:481) Avail: NTIS MF A01; SOD HC

$9.00 as SN-033-000-00937-2 CSCL 05A

Technology development; project management; employment

patterns; research productivity; legal status of support services;

functions of senior executives; the role of the sponsoring agency;

research diversification; obstacles to technical innovation;

organizational structures; and personnel management are

addressed. B.G.

N86-27108" National Aeronautics and Space Administration,

Washington, D.C.

MANAGEMENT: A BIBLIOGRAPHY FOR NASA MANAGERS

Apr. 1986 169p

(NASA-SP-7500(20); NAS 1.21:7500(20)) Avail: NTIS HC A08

CSCL 05A

This bibliography lists 707 reports, articles and other documents

introduced into the NASA scientific and technology information

system in 1985. Items are selected and grouped according to

their usefulness to the manager as manager. Citations are grouped

into ten subject categories: human factors and personnel issues;

management theory and techniques; industrial management and

manufacturing; robotics and expert syslems; computers and

information management; research and development; economics,

costs, and markets; logistics and operations management; reliability

and quality control; and legality, legislation, and policy. Author

196
82 DOCUMENTATIONANDINFORMATIONSCIENCE

82

DOCUMENTATION AND INFORMATION SCIENCE

Includes information management; information storage and retrieval

technology; technical writing; graphic arts; and micrography.

N78-12895"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

BIBLIOGRAPHY OF SUPERSONIC CRUISE AIRCRAFT

RESEARCH (SCAR)

S. HOFFMAN Nov. 1977 102 p Supersedes NASA-TM-X-73950;

N76-34039

(NASA-RP-1003; L-11603; NASA-TM-X-73950) Avail: NTIS HC

A06/MF A01 CSCL 05B

This bibliography documents publications of the supersonic

cruise aircraft research (SCAR) program that were generated during

the first 5 years of effort. The reports are arranged according to

systems studies and five SCAR disciplines: propulsion, stratospheric

emissions impact, structures and materials, aerodynamic

performance, and stability and control. The specific objectives of

each discipline are summarized. Annotation is included for all NASA

inhouse and low-number contractor reports. There are 444 papers

and articles included. Author

N79-13914" National Aeronautics and Space Administration,

Washington, D.C.

NASA GUIDELINES ON REPORT LITERATURE

1978 27p refs

(NASA-SP-7200) Avail: NTIS HC A03 CSCL 05B

NASA seeks for inclusion in its Scientific and Technical

Information System research reports, conference proceedings,

meeting papers, monographs, and doctoral and post graduate

theses which relate to the NASA mission and objectives. Topics

of interest to NASA are presented. GY.

N82-14960"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

TECHNICAL COMMUNICATION: PERSPECTIVES FOR THE

EIGHTIES, PART 1. PROCEEDINGS OF THE TECHNICAL

COMMUNICATIONS SESSIONS AT THE 32ND ANNUAL

MEETING OF THE CONFERENCE ON COLLEGE COMPOSITION

AND COMMUNICATION

J. C. MATHES, comp. (Michigan Univ., Ann Arbor) and T. E.

PINELLI, comp. Dec. 1981 307 p refs Conf. held in Dallas,

26-28 Mar. 1981

(NASA-CP-2203-PT-1; L-14899-PT-1) Avail: NTIS HC A14/MF

A01 CSCL 05B

COMMUNICATION THEORY, CONFERENCES, EDUCATION

GRAPHIC ARTS, LEARNING THEORY, TEACHING MACHINES

"[RAINING DEVICES, VERBAL COMMUNICATION

N82-15986"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

TECHNICAL COMMUNICATION. PERSPECTIVES FOR THE

EIGHTIES, PART 2

J. C. MATHES, comp. (Michigan Univ., Ann Arbor) and T. E.

PINELLI, comp. Dec. 1981 316 p refs Papers presented at

the 32nd Ann. Meeting of the Conf. on Colt. Composition and

Commun., Dallas, 26-28 Mar. 1981 2 Vol.

(NASA-CP-2203-PT-2; L-14899-PT-2) Avail: NTIS HC A14/MF

A01 CSCL 05B

COMMUNICATION THEORY, CONFERENCES, EDUCATION,

STANDARDS, TECHNICAL WRITING

N83-18559"# National Aeronautics and Space Administration,

Washington, D.C.

NASA ADMINISTRATIVE DATA BASE MANAGEMENT

SYSTEMS

Jan. 1983 285 p refs Conf. held in Pasadena, Calif., 26-27

May 1982

(NASA°CP-2254; NAS 1.55:2254) Avail: NTIS HC A13/MF A01

CSCL 05B

CONFERENCES, DATA BASE MANAGEMENT SYSTEMS,

DATA BASES, DATA MANAGEMENT, INFORMATION

RETRIEVAL, INFORMATION SYSTEMS

N83-22010" National Aeronautics and Space Administration,

Washington, D.C.

DATA BASES AND DATA BASE SYSTEMS RELATED TO

NASA'S AEROSPACE PROGRAM: A BIBLIOGRAPHY WITH

INDEXES

1983 172 p

(NASA-SP-7048; NAS 1.21:7048) Avail: NTIS HC $17.50

CSCL 05B

This bibliography lists 641 reports, articles, and other documents

introduced into the NASA scientific and technical information

system during the period January 1, 1981 through June 30, 1982.

The directory was compiled to assist in the location of numerical

and factual data bases and data base handling and management

systems. B.G.

N83-32671" National Aeronautics and Space Administration,

Washington, D.C.

NASA PUBLICATIONS GUIDE

1982 16p refs

(NASA-SP-7047; NAS 1.12/6:7047; NAS 1.21:7047) Avail:

NTIS HC A02 CSCL 05B

The publication programs and management policies of NASA

are described and the details that authors and publication

specialists need to know to carry out the agency's mission of

disseminating the scientific and technical information derived from

its activities are highlighted. Topics covered include the various

kinds of NASA formal publications; selection of publication medium;

printing and distribution; and requirements concerning style and

format standards, copyright transfers, the cover, color, and foldouts.

The sections of a report are delineated and editorial and page

make-up responsibilities are also discussed. A.R.H.

N83-33792"# National Aeronautics and Space Administration,

Washington, D.C.

RECORDS OF ACHIEVEMENT: NASA SPECIAL

PUBLICATIONS

1983 141 p Original contains color illustrations

(NASA-SP-470; NAS 1.21:470) Avail: NTIS and NASA Scientific

and Technical Information Facility, P.O. Box 8757, B.W.I. Airport,

Md. 21240 CSCL 05B

This annotated bibliography cites all NASA Special Publications

issued since 1961. The Reference Publications and Conference

Publications are included. Entries are arranged by SP number.

The entries are grouped in eight categories: general, handbooks

and data compilations, histories and chronologies, technology

utilization, management evaluation and analysis standards,

bibliographies, space vehicle design criteria, and specifications.

The Reference Publications and Conference Publications are listed

separately according to RP and CP number. Approximately 1400

entries are listed. Each entry includes the title, author, NASA

accession number, NASA SP, RP, or CP number, original sales

source, and publication date. An index of the SP, RP, and CP

numbers according to NASA subject category is provided. Highlights

of NASA's achievements since 1958 are included as a tribute to

NASA's 25th anniversary A.RH

197
82 DOCUMENTATIONADINFORMATIONSCIENCE

N84-21403"#National Aeronautics and Space Administration,

Washington, D.C.

NASA ADMINISTRATIVE DATA BASE MANAGEMENT

SYSTEMS, 1983

J. D. RADOSEVICH, ed. Apr. 1984 174 p refs Conf. held in

Greenbelt, Md., 25-26 May 1983

(NASA-CP-2304; NAS 1.55:2304; REPT-2) Avail: NTIS HC

A08/MF A01 CSCL 05B

CONFERENCES, DATA BASE MANAGEMENT SYSTEMS,

MANAGEMENT INFORMATION SYSTEMS, NASA PROGRAMS,

ON-LINE SYSTEMS

N84-33266"# National Aeronautics and Space Administration,

Washington, D.C.

NASA ADMINISTRATIVE DATA BASE MANAGEMENT

SYSTEMS, 1984

J. D. RADOSEVICH, ed. Sep. 1984 126 p refs Conf. held

in Hampton, Va., 6-7 Jun. 1984

(NASA-CP-2323; NAS 1.55:2323) Avail: NTIS HC A07/MF A01

CSCL 05B

CONFERENCES, DATA BASE MANAGEMENT SYSTEMS,

DISTRIBUTED PROCESSING, MANAGEMENT INFORMATION

SYSTEMS, NASA PROGRAMS, ON-LINE SYSTEMS

N85-12785" National Aeronautics and Space Administration,

Washington, D.C.

NASA THESAURUS SUPPLEMENT: A 3-PART CUMULATIVE

SUPPLEMENT TO THE 1982 EDITION OF THE NASA

THESAURUS

Jut. 1984 29 p

(NASA-SP-7051(SUPPL-2); NAS 1.21:7051(SUPPL-2)) Avail:

NTIS HC $6.50 CSCL 05B

The three part cumulative NASA Thesaurus Supplement to the

1982 edition of the NASA Thesaurus includes: part 1, hierarchical

listing; part 2, access vocabulary, and part 3, deletions. The

semiannual supplement gives complete hierarchies for new terms

and includes new term indications for terms new to this

supplement. E.A.K

N86-20168" National Aeronautics and Space Administration,

Washington, D.C.

NASA THESAURUS. VOLUME 1: HIERARCHICAL LISTING

1985 Edition

Sep. 1985 851 p

(NASA-SP-7053-VOL-1; NAS 1.21:7053-VOL-1) Avail: NTIS HC

$35.00

There are 16,835 postable terms and 3,765 nonpostable terms

approved for use in the NASA scientific and technical information

system in the Hierarchical Listing of the NASA Thesaurus. The

generic structure is presented for many terms. The broader term

and narrower term relationships are shown in an indented fashion

that illustrates the generic structure better than the more widely

used BT and NT listings. Related terms are generously applied,

thus enhancing the usefulness of the Hierarchical Listing. Greater

access to the Hierarchical Listing may be achieved with the

collateral use of Volume 2 - Access Vocabulary. Author

N86-20169" National Aeronautics and Space Administration,

Washington, D.C.

NASA THESAURUS. VOLUME 2: ACCESS VOCABULARY 1985

Edttlon

Sep. 1985 402 p

(NASA-SP-7053-VOL-2; NAS 1.21:7053-VOL-2) Avail: NTIS HC

$20.00

The Access Vocabulary, which is essentially a permuted index,

provides access to any word or number in authorized postable

and nonpostable terms. Additional entries include postable and

nonpostable terms, other word entries, and pseudo-multiword terms

that are permutations of words that contain words within words.

The Access Vocabulary contains 40,738 entries that give increased

access to the hierarchies in Volume 1 - Hierarchical Listing.

Author

N86-26243" National Aeronautics and Space Administration,

Washington, D.C.

SIGNIFICANT NASA INVENTIONS AVAILABLE FOR LICENSING

IN FOREIGN COUNTRIES

1986 81 p

(NASA-SP-7038(08); NAS 1.21:7038(08)) Avail: NTIS SOD HC

$5.00 as 033-000-00986-1 CSCL 05B

Abstracts of various NASA-owned inventions which are available

for foreign licensing in the identified countries are listed in

accordance with the NASA Patent Licensing Regulations. Instructions for requested applications are explained. B.G.

N86-28788" National Aeronautics and Space Administration,

Washington, D.C.

NASA PATENT ABSTRACTS BIBLIOGRAPHY: A CONTINUING

BIBLIOGRAPHY. SECTION 1: ABSTRACTS

Jul. 1986 52 p

(NASA-SP-7039(29)-SECT-1; NAS 1.21:7039(29)-SECT-I) Avail:

NTIS HC A04 CSCL 05B

Abstracts are provided for 115 patents and patent applications

entered into the NASA scientific and technical information system

during the period January 1986 through June 1986. Each entry

consists of a citation, an abstract, and in most cases, a key

illustration selected from the patent application. Author

N86-28789" National Aeronautics and Space Administration,

Washington, D.C.

NASA PATENT ABSTRACTS BIBLIOGRAPHY. A CONTINUING

BIBLIOGRAPHY. SECTION 2: INDEXES (SUPPLEMENT 29)

Jul. 1986 483p

(NASA-SP-7039(29)-SECT-2; NAS 1.21:7039(29)-SECT-2) Avail:

NTIS HC A21 CSCL 05B

Entries for over 4400 patents and patent applications citations

for the period May 1969 through June 1986 are listed. Subject,

invention, source, number, and accession number indexes are

included. B.G.

85

URBAN TECHNOLOGY AND TRANSPORTATION

Includes applications of space technology to urban problems;

technology transfer; technology assessment; and surface and mass

transportation.

N79-10942"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

PLANNING FOR AIRPORT ACCESS: AN ANALYSIS OF THE

SAN FRANCISCO BAY AREA

J. S. DAJANI, ed. (Stanford Univ., Calif.), J. V. JUCKER, ed., and

J. L. JONES (Stanford Univ.) May 1978 300 p refs

Stanford-NASA-ASEE Summer Faculty Fellowship Program on Eng.

System Design held at Moffett Field, Calif., 1977

(NGR-05-020-409)

(NASA-CP-2044; A-7347) Avail: NTIS HC A13/MF A01 CSCL

13F

AIRPORT PLANNING, SAN FRANCISCO BAY (CA), TRAFFIC,

URBAN TRANSPORTATION

N79-28062"# National Aeronautics and Space Administration.

Lyndon B. Johnson Space Center, Houston, Tex.

NASA JSC WATER MONITOR SYSTEM: CITY OF HOUSTON

FIELD DEMONSTRATION

R. E. TAYLOR, E. L. JEFFERS, and D. H. FRICKS Jul. 1979

57 p refs

(NASA-RP-1041; S-490; JSC-14832) Avail: NTIS HC A04/MF

A01 CSCL 13B

A water quality monitoring system with on-line and real time

operation similar to the function in a spacecraft was investigated.

A system with the capability to determine conformance to future

198
high effluent quality standards and to increase the potential for

reclamation and reuse of water was designed. Although all system

capabilities were not verified in the initial field trial, fully automated

operation over a sustained period with only routine manual

adjustments was accomplished. Two major points were

demonstrated: (1) the water monitor system has great potential in

water monitoring and/or process control applications; and (2) the

water monitor system represents a vast improvement over

conventional (grab sample) water monitoring techniques. S.E.S.

NSO-_B990*# Transportation Systems Center, Cambridge,

Mass.

IMPLICATIONS OF FUEL-EFFICIENT VEHICLES ON RIDE

QUALITY AND PASSENGER ACCEPTANCE: WORKSHOP

PROCEEDINGS Final Report, 6-8 Sep. 1979

A. M. WICHANSKY, ed. and A. R. KUHLTHAU, ed. (Virginia

Univ.) Aug. 1979 120 p refs Conf. held at Woods Hole,

Mass., 6-8 Sep. 1978

(NASA-CP-2096; DTS-532; DOT-TSC-RSPA-79-21) Avail: NTIS

HC A06/MF A01 CSCL 13F

ACCEPTABILITY, AUTOMOBILES, CONFERENCES, FUEL

CONSUMPTION, PASSENGER AIRCRAFT, RIDING QUALITY

N80-27219"# National Aeronautics and Space Administration,

Washington, D.C.

LESSONS OF THE NASA TECH HOUSE

H. ALLAWEY 1980 41 p Original contains color illustrations

(NASA-SP-442; LC-80-607024) Avail: NTIS MF A01; SOD HC

$3.00 CSCL 13B

The performance and effectiveness of the various systems

incorporated into the NASA Technology House are described and

evaluated in relation to the HUD reference house. The various

aerospace technologies used (advanced electronics, solar energy

utilization, water recycling, fire retardant materials) are discussed

as well as the improved materials, design configurations, and

construction techniques developed under other government

programs and by industry. Tabular data show the consumption

and conservation of electrial energy and water for each month

over one full weather cycle, during which time a family of four

was in residence. A.R.H.

88

SPACE SCIENCES (GENERAL)

N77-20977"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

THE STRUCTURE AND CONTENT OF THE GALAXY AND

GALACTIC GAMMA RAYS

C. E. FICHTEL, ed. and F. W. STECKER, ed. Washington

1977 356 p refs Symp. held at Greenbelt, Md., 2-4 Jun.

1976

(NASA-CP-002) Avail: NTIS HC A16/MF A01 CSCL 03B

ASTROPHYSICS, COSMIC RAYS, GALACTIC STRUCTURE,

GAMMA RAYS, INTERSTELLAR GAS

N77-33_3"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

RESULTS OF ANALYSES PERFORMED ON BASALT ADJACENT

TO PENETRATORS EMPLACED INTO VOLCANIC ROCK AT

AMBOY, CALIFORNIA, APRIL 1976

M BLANCHARD, T. BUNCH, A, DAVIS (San Jose State Univ.),

H. SHADE (LFE Corp.), J. ERLICHMAN (LFE Corp.), and G.

POLKOWSKI (LFE Corp.) Sep. 1977 18 p refs

(NASA-TP-1026) Avail: NTIS HC A02/MF A01 CSCL 03B

BASALT, CALIFORNIA, CHEMICAL ANALYSIS,

PENETRATION, PETROLOGY, ROCKS

88 SPACE SCIENCES (GENERAL)

N78-21019"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

A BIBLIOGRAPHY ON THE SEARCH FOR EXTRATERRESTRIAL

INTELLIGENCE

E F. MALLOVE (Analytic Sci. Corp., Reading, Mass.), M. M.

CONNORS, R. L. FORWARD (Hughes Res. Labs., Malibu, Calif.),

and Z. PAPROTNY (Orzeszkowej, Poland) Mar. 1978 135 p

refs

(NASA-RP-1021) Avail: NTIS HC A07/MF A01 CSCL 05B

This report presents a uniform compilation of works dealing

with the search for extraterrestrial intelligence. Entries are by first

author, with cross-reference by topic index and by periodical index.

This bibliography updates earlier bibliographies on this general

topic while concentrating on research related to listening for signals

from extraterrestrial intelligence. Author

N79-22979"# National Aeronautics and Space Administration.

Lyndon B. Johnson Space Center, Houston, Tex.

ALSEP TERMINATION REPORT

J. R. BATES, W. W. LAUDERDALE (General Electric Co.), and H.

KERNAGHAN (Kentron International, Inc.) Apr. 1979 161 p

refs

(NASA-RP-1036; S-480) Avail: NTIS HC A08/MF A01 CSCL

03B

The Apollo Lunar Surface Experiments Package (ALSEP) final

report was prepared when support operations were terminated

September 30, 1977, and NASA discontinued the receiving and

processing of scientific data transmitted from equipment deployed

on the lunar surface. The ALSEP experiments (Apollo 11 to Apollo

17) are described and pertinent operational history is given for

each experiment. The ALSEP data processing and distribution are

described together with an extensive discussion on archiving.

Engineering closeout tests and results are given, and the status

and configuration of the experiments at termination are

documented. Significant science findings are summarized by

selected investigators. Significant operational data and

recommendations are also included. G.Y.

N79-22980"# National Aeronautics and Space Administration.

Wallops Flight Center, Wallops Island, Va.

MOLECULES OF SIGNIFICANCE IN PLANETARY AERONOMY

H. MOHAN Jan. 1979 318 p refs

(NASA-RP-1030) Avail: NTIS HC A14/MF A01 CSCL 03B

This monograph is basically devoted to spectroscopic

information of the molecules of planetary interest. Only those

molecules have been dealt with which have been confirmed

spectroscopically to be present in the atmosphere of major planets

of our solar system and play an important role in the aeronomy

of the respective planets. An introduction giving the general

conditions of planets and their atmospheres including the gaseous

molecules is given. Some typical planetary spectra is presented

and supported with a discussion on some basic concepts of optical

absorption and molecular parameters that are important to the

study of planetary atmospheres. Quantities like dipole moments,

transition probabilities, Einstein coefficients and line strengths,

radiative life times, absorption cross sections, oscillator strengths,

line widths and profiles, equivalent widths, growth curves, bond

strengths, electronic transition moments, Franck-Condon factors

and r-centroids, etc., are discussed. Spectroscopic information and

relevant data of 6 diatomic (HF, HCL, CO, H2, 02, N2) and 6

potyatomic (CO2, N2), 03, HeO, NH3, CH4) molecules are

presented. L.S.

N79-34118"# National Aeronautics and Space Administration,

Washington, D.C.

SKYLAB'S ASTRONOMY AND SPACE SCIENCES

C. A. LUNDQUIST, ed, 1979 126 p Original contains color

illustrations

(NASA-SP-404) Avail: NTIS MF A01; SOD HC CSCL 03A

The capabilities of Skytab for multidisciplinary investigations are

reviewed. Experiments and results are discussed for observations

of stars and galaxies, energetic particles, interplanetary dust, Comet

Kohoutek, the earth's atmosphere, and the nature and effects of

199
88 SPACESCIENCES(GENERAL)

space environments on man. For individual titles, see N79-34119

through N79-34125.

N80-14977"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

HEAO SCIENCE SYMPOSIUM

C. DAILEY, ed. and W. JOHNSON, ed. Nov. 1979 463 p refs

Symp. held at Huntsville, Ala., 8-9 May 1979

(NASA-CP-2113) Avail: NTIS HC A20/MF A01 CSCL 03A

CONFERENCES, HEAO 1, HEAO 2, SPACEBORNE

ASTRONOMY, X RAY ASTRONOMY

N80-22130"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

SCIENTIFIC RESEARCH WITH THE SPACE TELESCOPE:

INTERNATIONAL ASTRONOMICAL UNION COLLOQUIUM NO.

54

M. S. LONGAIR (Mullard Radio Astronomy Obs.) and J. W.

WARNER Oct. 1979 331 p refs Colloq. held in Princeton,

N.J., 8-11 Aug. 1979; co-sponsored by COSPAR

(NASA-CP-2111) Avail: NTIS MF A0t; SOD HC CSCL 03B

ASTRONOMICAL SPECTROSCOPY, CONFERENCES,

COSMOLOGY, GALACTIC EVOLUTION, HUBBLE SPACE

TELESCOPE, SPACEBORNE ASTRONOMY

N81-11966"# National Aeronautics and Space Administration,

Washington, D.C.

VIKING ORBITER VIEWS OF MARS

M. H. CARR, W. A. BAUM, K. R. BLASIUS, G. A. BRIGGS, J. A.

CUTTS, T. C. DUXBURY, R. GREELEY, J, GUEST, H. MASURSKY,

B. A. SMITH et al. 1980 189 p refs Original contains color

illustrations

(NASA-SP-441) Avail: NTIS MF A01; SOD HC $9.50 CSCL

03B

Images acquired by the Viking orbiters, beginning in 1976 are

presented. The pictures represent only a small fraction of the

many thousands taken, and were chosen to illustrate the diverse

geology of Mars and its atmospheric phenomena. Specific topics

discussed include the Viking mission and its objectives, a brief

comparison of Earth and Mars, and surface features of Mars

including the great equatorial canyons, channels, volcanic and

deformational features, and craters. Martian moons, surface

processes, polar regions, and the Martian atmosphere are also

covered. J.M.S.

N81-20962"# National Aeronautics and Space Administration,

Washington, D.C.

BEYOND THE ATMOSPHERE: EARLY YEARS OF SPACE

SCIENCE

H. E. NEWELL 1980 512 p refs Original contains color

illustrations

(NASA-SP-4211) Avail: NTIS MF A01; SOD HC $11.00 CSCL

03C

From the rocket measurements of the upper atmosphere and

Sun that began in 1946, space science gradually emerged as a

new field of scientific activity. The course of the United State

space program is viewed in an historical context. Major emphasis

is on NASA and its programs. The funding, staffing, organization,

and priorities of the space program were reviewed. For individual

titles, see N81-20963 through N81-20984.

N82-25027"# National Aeronautics and Space Administration,

Washington, D.C.

B STARS WITH AND WITHOUT EMISSION LINES, PARTS 1

AND 2

A. UNDERHILL, ed. and V. DOAZAN, ed. 1982 533 p refs

In ENGLISH; FRENCH summary Prepared in cooperation with

Centre National de la Recherche Scientifique, Paris

(NASA-SP-456; NAS 1.21:456; LC-82-2313) Avail: NTIS HC

A23/MF A01 CSCL 03A

The spectra for B stars for which emission lines occur not on

the main sequence, but only among the supergiants, and those B

stars for which the presence of emission in H ahlpa is considered

200

to be a significant factor in delineating atmospheric structure are

examined. The development of models that are compatible with

all known facts about a star and with the laws of physics is also

discussed. For individual titles, see N82-25028 through

N82-25038.

N84-34332"# Maryland Univ., College Park.

SOLAR TERRESTRIAL PHYSICS: PRESENT AND FUTURE

D. M. BUTLER, ed. and K. PAPADOPOULOS, ed. Jun. 1984

586 p refs Workshop held in Berkeley Springs, W. Va., Dec.

1982, 6-10 Jun. and 30 Nov. 1983 Sponsored in cooperation

with NASA and NSF

(NASA-RP-1120; NAS 1.61:1120) Avail: NTIS HC A25/MF A01

CSCL 03B

The following topics relating to solar-terrestrial interactions are

considered: (1) reconnection of magnetic fields; (2) particle

acceleration; (3) solar magnetic flux; (4) magnetohydrodynamic

waves and turbulence in the Sun and interplanetary medium; (5)

coupling of the solar wind to the magnetosphere; (6) coronal

transients; (7) the connection between the magnetosphere and

ionosphere; (8) substorms in the magnetosphere; (9) solar flares

and the solar terrestrial environment; (10) shock waves in the

solar terrestrial environment; (11) plasma transport and convection

at high latitudes; and (12) high latitude ionospheric structure. For

individual titles, see N84-34333 through N84-34344.

N85-17755"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

THE ORIGIN OF NONRADIATIVE HEATING/MOMENTUM IN

HOT STARS

A. B. UNDERHILL, ed. and A. G. MICHALITSIANOS, ed.

Washington Jan. 1985 262 p refs Workshop held in

Greenbelt, Md., 5-7 Jun. 1984 Sponsored in part by American

Astronomical Society

(NASA-CP-2358; REPT-85B0136; NAS 1.55:2358) Avail: NTIS

HC A12/MF A01 CSCL 03B

CONFERENCES, EARLY STARS, HEATING, HOT STARS,

LATE STARS, MOMENTUM, STELLAR ATMOSPHERES,

STELLAR EVOLUTION, STELLAR TEMPERATURE

N85-18888"# Jet Propulsion Lab., California Inst. of Tech.,

Pasadena.

THE GEOLOGY OF THE TERRESTRIAL PLANETS

M. H. CARR, ed. (Geological Survey), R. S. SAUNDERS, R. G.

STROM (Geological Survey), and D. E. WILHELMS (Geological

Survey) Jun. 1984 322 p refs Original contains color

illustrations

(NASA-SP-469; NAS 1.21:469) Avail: NTIS MF A0t; SOD HC

$16.00 as SN-033-000-00900-3 CSCL 03B

The geologic history of the terrestrial planets is outlined in

light of recent exploration and the revolution in geologic thinking.

Among the topics considered are planet formation; planetary

craters, basins, and general surface characteristics; tectonics;

planetary atmospheres; and volcanism For individual titles see

N85-18889 through N85-18894.

N85-23457"# Cornell Univ., Ithaca, N.Y.

PLANETARY GEOLOGY IN THE 1980S

J. VEVERKA 1984 199 p refs

(NSG-7156)

(NASA-SP-467; NAS 1.21:467) Avail: NTIS HC A09/MF A01;

also available from NASA Information Center, Washington, D.C.

20546 $19.00 CSCL 03C

The geologic aspects of solar system studies are defined and

the goals of planetary geology are discussed. Planetary geology

is the study of the origin, evolution, and distribution of matter

condensed in the form of planets, satellites, asteroids, and comets.

It is a multidisciplinary effort involving investigators with

backgrounds in geology, chemistry, physics, astronomy, geodesy,

cartography, and other disciplines concerned with the solid planets.

The report is primarily restricted to the kinds of experiments and

observations made through unmanned missions. B.W.
N86-13239"#National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ale.

SECOND WORKSHOP ON SPACECRAFT GLOW

J. H. WAITE, JR., ed. and T. W. MOOREHEAD, ed. Sep. 1985

294 p refs Workshop held in Huntsville, Ala., 6-7 May 1985;

sponsored in part by the Universities Space Research

Association

(NASAoCP-2391; M-502; NAS 1.55:2391) Avail: NTIS HC

A13/MF A01 CSCL 03B

EMITTANCE, FLUID DYNAMICS, LUMINOSITY, PLASMA

PHYSICS, SPACE PLASMAS, SPACECRAFT ORBITS,

SPECTROSCOPY

N86-23493"# National Aeronautics and Space Administration,

Washington D C

INTERRELATIONSHIPS AMONG ClRCUMSTELLAR, INTERSTELLAR AND INTERPLANETARY DUST

J. A. NUTH, Ill, ed. and R. E. STENCEL, ed. Jan. 1986 351 p

refs Workshop held in Wye, Md., 27 Feb. - 1 Mar. 1985

(NASA-CP-2403; NAS 1.55:2403) Avail: NTIS HC A16/MF A01

CSCL 03B

ASTROPHYSICS, COSMIC DUST, INTERPLANETARY DUST,

INTERSTELLAR MATTER, STELLAR ENVELOPES, STELLAR

EVOLUTION

N86-27136"# National Aeronautics and Space Administration.

Lyndon B. Johnson Space Center, Houston, Tex.

SPACE STATION PLANETOLOGY EXPERIMENTS (SSPEX)

R. GREELEY, ed. (Arizona State Univ., Tempe) and R. J.

WILLIAMS, ed. May 1986 97 p Workshop held in Flagstaff,

Ariz., 20-22 Jun. 1985

(NCC9-14; NAS9-17023)

(NASA-CP-2424; S-554; NAS 1.55:2424) Avail: NTIS HC

A05/MF A01 CSCL 03A

METEOROIDS, ORBITAL SPACE STATIONS, PARTICLES,

PETROLOGY, PLANETOLOGY, SPACE EXPLORATION, WIND

(METEOROLOGY)

89

ASTRONOMY

Includes radio, gamma-ray, and infrared astronomy; and

astrometry.

N77-34063"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

RECOGNITION OF COMPACT ASTROPHYSICAL OBJECTS

H. OGELMAN, ed. and R. ROTHSCHILD, ed. 1977 200 p

refs

(NASA-SP-421) Avail: NTIS HC A09/MF A01 CSCL 03A

NASA's Laboratory for High Energy Astrophysics and the Dept.

of Physics and Astrophysics at the Univ. of Md. collaberated on a

graduate level course with this title. This publication is an edited

version of notes used as the course text. Topics include stellar

evolution, pulsars, binary stars, X-ray signatures, gamma ray

sources, and temporal analysis of X-ray data. J.L.H.

N79-24921"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

COLLISIONLESS GALAXY SIMULATIONS

F. HOHL, T. A. ZANG (Coll. of William and Mary, Williamsburg,

Va.), and J. B. MILLER (Old Dominion Univ.) Apr. 1979 149 p

refs

(NASA-RP-1037; L-12730) Avail: NTIS HC A07/MF A01

CSCL 03A

Three-dimensional fully self-consistent computer models were

used to determine the evolution of galaxies consisting of 100 000

simulation stars. Comparison of two-dimensional simulations with

three-dimensional simulations showed only a very slight stabilizing

89 ASTRONOMY

effect due to the additional degree of freedom. The addition of a

fully self-consistent, nonrotating, exponential core/halo component

resulted in considerable stabilization. A second series of computer

experiments was performed to determine the collapse and

relaxation of initially spherical, uniform density and uniform velocity

dispersion stellar systems. The evolution of the system was

followed for various amounts of angular momentum in solid body

rotation. For initally low values of the angular momentum satisfying

the Ostriker-Peebles stability criterion, the systems quickly relax

to an axisymmetric shape and resemble elliptical galaxies in

appearance. For larger values of the initial angular momentum

bars develop and the systems undergo a much more drastic

evolution. L.S.

N80-11966" National Aeronautics and Space Administration.

Lyndon B. Johnson Space Center, Houston, Tex.

AN EMISSION-LINE SURVEY OF THE MILKY WAY

R. A. R. PARKER, T. R. GULL (NASA Godderd Space Flight

Center), and R. P. KIRSCHNER (Mich. Univ.) Washington

1979 224 p

(NASA-SP-434) Avail: SOD HC $15.00 CSCL 03A

The instrumentation used in an examination of the ionization

structure of emission nebulae and of the galactic plane in general,

is described, as well as the characteristics of the prints obtained.

Reasonable exposure times were obtained with the use of an

image intensifier and five interference filters isolated the band

passes chosen for the survey. A rough map of each field is

presented with a print from the Becvar Skalnate Pleso covering

the same area. No systematic effort was made to identify and

mark each nebulosity. A new supernova remnant was discovered

in the field 1 = 65.5 deg, b = + 5 deg using this technique.

A.RH.

N80-18997"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

AN ASSESSMENT OF GROUND-BASED TECHNIQUES FOR

DETECTING OTHER PLANETARY SYSTEMS. VOLUME 1: AN

OVERVIEW

D. C, BLACK, ed. and W. E. BRUNK, ed. (NASA, Washington,

D.C.) Feb. 1980 48 p refs Workshop held at Cambridge,

Mass., Nov. 1979

(NASA-CP-2124-VOL-1; A-8002) Avail: NTIS HC A03/MF A01

CSCL 03A

ASTROMETRY, CONFERENCES, PLANETARY EVOLUTION,

RADIO ASTRONOMY, SOLAR SYSTEM, TECHNOLOGY

ASSESSMENT

N80-25224"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

AN ASSESSMENT OF GROUND-BASED TECHNIQUES FOR

DETECTING OTHER PLANETARY SYSTEMS. VOLUME 2:

POSITION PAPERS

D. C. BLACK and W. E. BRUNK Mar. 1980 253 p refs

Prepared in cooperation with NASA, Washington, D.C.

(NASA-CP-2124-VOL-2; A-8114) Avail: NTIS HC A12/MF A01

CSCL 03A

ASTROMETRY, ASTRONOMICAL TELESCOPES, EXTRASOLAR PLANETS

N82-31163"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

ADVANCES IN ULTRAVIOLET ASTRONOMY: FOUR YEARS

OF IUE RESEARCH

Y. KONDO, ed., J. M. MEAD, ed., and R. D. CHAPMAN, ed.

1982 653 p refs Proc. of Symp. held at Greenbelt, Md., 30

Mar. - 1 Apr. 1982

(NASA-CP-2238; NAS 1.55:2238) Avail: NTIS HC A99/MF A01

CSCL 03A

ASTRONOMICAL SPECTROSCOPY, GALAXIES, INTERSTELLAR MATTER, IUE, PLANETS, QUASARS, SOLAR SYSTEM,

STARS, ULTRAVIOLET ASTRONOMY

201
89 ASTRONOMY

N82-33296"# Space Telescope Science Inst., Huntsville, Ala.

THE SPACE TELESCOPE OBSERVATORY. SPECIAL SESSION

OF COMMISSION 44, IAU 18TH GENERAL ASSEMBLY

D. N. B. HALL, ed. 1982 138 p refs Conf. held in Patras,

Greece, Aug. 1982; sponsored by NASA and ESA

(NAS5-26555)

(NASA-CP-2244; NAS 1.55:2244) Avail: NTIS HC A07/MF A01

CSCL 03A

ASTRONOMICAL OBSERVATORIES, ASTRONOMICAL PHOTOGRAPHY, ASTRONOMICAL PHOTOMETRY, ASTRONOMICAL

SPECTROSCOPY, HUBBLE SPACE TELESCOPE, SPACEBORNE

ASTRONOMY, ULTRAVIOLET ASTRONOMY

N83-27939"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

LARGE DEPLOYABLE REFLECTOR SCIENCE AND

TECHNOLOGY WORKSHOP. VOLUME 2: SCIENTIFIC

RATIONALE AND TECHNOLOGY REQUIREMENTS

D. HOLLENBACH, ed. Jun. 1983 70 p refs Workshop held

at Pacific Grove, Calif., 21-25 Jun. 1982

(NASA-CP-2275-VOL-2; T-5349; NAS 1.55:2275-VOL-2) Avail:

NTIS HC A04/MF A01 CSCL 03A

CONFERENCES, INFRARED ASTRONOMY, REFLECTORS

N84-22516"# National Aeronautics and Space Administration,

Washington, D.C.

THE STAR SPLITTERS: THE HIGH ENERGY ASTRONOMY

OBSERVATORIES

W. H. TUCKER 1984 182 p refs

(NASA-SP-466; NAS 1.21:466; LC-83-16349) Avail: NTIS MF

A01; SOD HC $12.00 CSCL 03A

The nature of the high energy universe and the design of

instruments to analyze stellar and galactic radiation are described

in this history of the HEAO program and its scientific and technical

accomplishments. Topics covered include: creative violence, stellar

explosions, cosmic rays, superbubbles, stellar coronas, collapsed

stars, neutron stars, degenerate dwarf stars, black holes, X-ray

images of galaxies, galactic nuclei, spiral galaxies, galactic clusters,

the mystery of the missing mass, and cosmic fire. A.RH.

N84-26519"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

FAR INFRARED SUPPLEMENT: CATALOG OF INFRARED

OBSERVATIONS

D. Y. GEZARI, M. SCHMITZ (Computer Sciences Corp.), and J.

M. MEAD May 1984 97 p

(NAS5-24350)

(NASA-RP-1119; NAS 1.61:1119) Avail: NTIS HC A05/MF A01

CSCL 03A

The Far Infrared Supplement: catalog of infrared observations

summarizes all infrared astronomical observations at far infrared

wavelengths published in the scientific literature between 1965

and 1982. The Supplement list contains 25% of the observations

in the full catalog of infrared observations (C10), and essentially

eliminates most visible stars from the listings. The Supplement is

more compact than the main Catalog (it does not contain the

bibliography and position index of the C10), and is intended for

easy reference during astronomical observations. E.A.K.

N84,26520"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

CATALOG OF INFRARED OBSERVATIONS INCLUDING:

BIBLIOGRAPHY OF INFRARED ASTRONOMY AND INDEX OF

INFRARED SOURCE POSITIONS

D. Y, GEZARI, M. SCHMITZ (Computer Sciences Corp.), and J.

M MEAD May 1984 563 p

(NASA-RP-1118; NAS 1.61:1118) Avail: NTIS HCA24/MFA01

CSCL 03A

The Catalog of Infrared Observations and its Far Infrared

Supplement summarize all infrared astronomical observations at

infrared wavelengths published in the scientific literature between

1965 and 1982. The Catalog includes as appendices the

202

Bibliography of infrared astronomy which keys observations in the

Catalog with the original journal references, and the index of

infrared source positions which gives source positions for

alphabetically listed sources in the Catalog. The Catalog data base

contains over 85,000 observations of about 10,000 infrared

sources, of which about 2,000 have no known visible counterpart.

E.A.K

N84-28709"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

PROCEEDINGS OF THE LARGE DEPLOYABLE REFLECTOR

SCIENCE AND TECHNOLOGY WORKSHOP. VOLUME 1:

EXECUTIVE SUMMARY

C. A. LEIDICH and B. PITTMAN Jun. 1984 45 p refs

Workshop held at Pacific Grove, Calif., 21-25 Jun. 1982

(NASA-CP-2275-VOL-1; A-9152; NAS 1.55:2275-VOL-1) Avail:

NTIS HC A03/MF A01 CSCL 03A

CONFERENCES, INFRARED SPECTRA, SPACEBORNE

ASTRONOMY, SPACEBORNE TELESCOPES

N84-32318"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

LARGE DEPLOYABLE REFLECTOR SCIENCE AND

TECHNOLOGY WORKSHOP. VOLUME 3: SYSTEMS AND

TECHNOLOGY ASSESSMENT

C. A. LEIDICH, ed. and R. B. PITTMAN, ed. Jul. 1984 65 p

refs Workshop held in Pacific Grove, Calif,, 21-25 Jun. 1982 3

Vol.

(NASA-CP-2275-VOL-3; A-9341-VOL-3; NAS 1.55:2275-VOL-3)

Avail: NTIS HC A04/MF A01 CSCL 03A

ASTRONOMICAL OBSERVATORIES, ASTRONOMICAL

TELESCOPES, CONFERENCES, FUNCTIONAL DESIGN

SPECIFICATIONS, INFRARED ASTRONOMY, INFRARED

RADIATION, LARGE SPACE STRUCTURES, REFLECTORS,

SATELLITE DESIGN, SPACEBORNE TELESCOPES,

SUBMILLIMETER WAVES, TECHNOLOGY ASSESSMENT

N85-12833"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

ALGORITHM FOR ASTRONOMICAL, EXTENDED SOURCE,

SIGNAL-TO-NOISE RADIO CALCULATIONS

R. R. JAYROE Nov. 1984 23 p refs

(NASA-TP-2396; NAS 1.60:2396) Avail: NTIS HC A02/MF A01

CSCL 03A

ALGORITHMS, COMPUTER PROGRAMS, HUBBLE SPACE

TELESCOPE, NONPOINT SOURCES, SIGNAL TO NOISE RATIOS,

SPACEBORNE ASTRONOMY

N85-12834"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

ALGORITHM FOR ASTRONOMICAL, POINT SOURCE, SIGNAL

TO NOISE RATIO CALCULATIONS

R. R. JAYROE and D. J. SCHROEDER (Beloit Coll.) Nov. 1984

40 p refs

(NASA-TP-2397; NAS 1.60:2397) Avail: NTIS HC A03/MF A01

CSCL 03A

ALGORITHMS, COMPUTER PROGRAMS, HUBBLE SPACE

TELESCOPE, POINT SOURCES, SIGNAL TO NOISE RATIOS,

SPACEBORNE ASTRONOMY

N85-17848"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

AIRBORNE ASTRONOMY SYMPOSIUM. A SYMPOSIUM

COMMEMORATING THE TENTH ANNIVERSARY OF

OPERATIONS OF THE KUIPER AIRBORNE OBSERVATORY

H. A. THRONSON, JR., ed. (Wyoming Univ., Laramie) and E. F.

ERICKSON, ed. Dec. 1984 387 p refs Symp. held at

Moffett Field, Calif., 11-13 Jul. 1984; sponsored by NASA and the

Astronomical Society of the Pacific

(NASA-CP-2353; NAS 1.55:2353; REPT.85073) Avail: NTIS HC

A17/MF A01 CSCL 03A

ASTRONOMICAL OBSERVATORIES, CONFERENCES,
INFRAREDASTRONOMY, MILKYWAYGALAXY, SOLAR

SYSTEM, STARS

N85-17892"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

PROCEEDINGS OF THE WORKSHOP ON IMPROVEMENTS TO

PHOTOMETRY

W. J. BORUCKI, ed. and A. T. YOUNG, ed. Nov. 1984 260 p

refs Workshop held in San Diego, Calif., 18-19 Jun. 1984

(NASA-CPo2350; REPT-85052; NAS 1.55:2350) Avail: NTIS HC

A12/MFA01 CSCL03A

CONFERENCES, PHOTOMETRY, PRECISION

N85-20961"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

FUTURE OF ULTRAVIOLET ASTRONOMY BASED ON SlX

YEARS OF IUE RESEARCH

J. M. MEAD, ed., R. D. CHAPMAN, ed., and Y. KONDO, ed.

Dec. 1984 542 p refs Symp. held in Greenbelt, Md., 3-5 Apr.

1984

(NASA-CP-2349; REPT-85B0016; NAS 1.55:2349) Avail: NTIS

HC A23/MF A01 CSCL 03A

GALAXIES, INTERSTELLAR MATTER, IUE, NEBULAE, SOLAR

SYSTEM, STELLAR EVOLUTION, ULTRAVIOLET ASTRONOMY

N86-12168"# National Aeronautics and Space Administration,

Washington, D.C.

THE 1982-1984 ECLIPSE OF EPSILON AURIGAE

R. E. STENCEL, ed. Sep. 1985 115 p refs Working

meeting held in Tucson, Adz., 16-17 Jan. 1985

(NASA-CP-2384; NAS 1.55:2384; LC-85-13854) Avail: NTIS HC

A06/MF A01 CSCL 03A

ASTRONOMICAL PHOTOMETRY, ASTRONOMICAL

SPECTROSCOPY, AURIGA CONSTELLATION, ECLIPSING

BINARY STARS, ELECTROPHOTOMETRY

90

ASTROPHYSICS

Includes cosmology; celestial mechanics; space plasmas; and

interstellar and interplanetary gases and dust.

N77-12959"# National Aeronautics and Space Administration,

Washington, D.C.

EVOLUTION OF THE SOLAR SYSTEM

H. ALFVEN (Calif. Univ., San Diego) and G. ARRHENIUS (Scripps

Institution of Oceanography, San Diego) 1976 611 p refs

(NASA-SP-345) Avail: NTIS MF A01; SOD HC $11.00 CSCL

03B

The origin and evolution of the solar system are analyzed.

Physical processes are first discussed, followed by experimental

studies of plasma-solid reactions and chemical and mineralogical

analyses of meteorites and lunar and terrestrial samples.

N78-12925"# National Aeronautics and Space Administration,

Washington. D.C.

THE SOVIET-AMERICAN CONFERENCE ON COSMOCHEMISTRY OF THE MOON AND PLANETS, PART 1

J. H. POMEROY, ed. and N. J. HUBBARD, ed. 1977 503 p

refs Conf. held at Moscow, 4-8 Jun. 1974

(NASA-SP-370-PT-1; LC-75-600013) Avail: NTIS MF A01; SOD

HC CSCL 03B

The basic goal of the conference was consideration of the

origin of the planets of the solar system, based on the physical

and chemical data obtained by study of the material of the moon

and planets. Papers at the conference were presented in the

following sessions: (1) Differentiation of the material of the moon

and planets; (2) The thermal history of the moon; (3) Lunar

gravitation and magnetism; (4) Chronology of the moon, planets,

90 ASTROPHYSICS

and meteorites; (5) The role of exogenic factors in the formation

of the lunar surface; (6) Cosmochemical hypotheses about the

origin and evolution of the moon and planets; and (7) New data

about the planets Mercury, Venus, Mars, and Jupiter. For individual

titles, see N78-12926 through N78-12957.

N78-12958"# National Aeronautics and Space Administration,

Washington, D.C.

THE SOVIET-AMERICAN CONFERENCE ON COSMOCHEMISTRY OF THE MOON AND PLANETS, PART 2

J. H. POMEROY, ed. and N. J. HUBBARD, ed. 1977 423 p

refs Conf. held at Moscow, 4-8 Jun. 1974

(NASA-SP-370-PT-2; LC-75-600013) Avail: NTIS MF A01; SOD

HC CSCL 03B

The origin and evolution of the solar system is discussed based

on ground and satellite observations. For individual titles, see

N78-12959 through N78-12988.

N81-11970"# National Aeronautics and Space Administration.

Lyndon B. Johnson Space Center, Houston, Tex.

MOTION ABOUT THE STABLE LIBRATION POINTS IN THE

LINEARIZED, RESTRICTED THREE-BODY PROBLEM

D. MITTLEMAN (Oberlin Coll., Ohio) Sep. 1980 159 p refs

(NASA-RP-1065; S-500) Avail: NTIS HC A08/MF A01 CSCL

03B

The motion of a point particle in the neighborhood of a triangular

libration point (L sub 4 or L sub 5) in the linearized, restricted

problem of three bodies in the plane is described. The derivation

of the equations of motion is standard. From these equations,

three invariants of the motion are obtained; the Jacobi integral is

expressed linearly in terms of two of these. The trajectories for

varied initial conditions are drawn, and a complete geometric

description of the particle motion is given in elementary terms.

Each trajectory has an exterior boundary curve; its equation is

found. An approximation to this boundary curve was known; the

two curves are compared graphically. For certain initial conditions,

there is an interior region from which the trajectory is excluded;

the equation of the boundary of this region is given. M.G.

N81-25893"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

THE UNIVERSE AT ULTRAVIOLET WAVELENGTHS: THE FIRST

TWO YEARS OF INTERNATIONAL ULTRAVIOLET EXPLORER

R. D. CHAPMAN, ed. 1981 773 p refs Proceedings of a

syrup, held in Greenbelt, Md., 7-9 May 1980

(NASA-CP-2171) Avail: NTIS HC A99/MF A01 CSCL 03B

CONFERENCES, IUE, SPACEBORNE ASTRONOMY,

ULTRAVIOLET ASTRONOMY

N81-27008"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

THE SUN AS A STAR

S. D. JORDAN, ed. Jul. 1981 559 p refs Sponsored in part

by CNRS

(NASA-SP-450; REPT-81F0008; LC-81-600064) Avail: NTIS HC

$39.50/MF A01 CSCL 03B

Solar physics was reviewed in the context of the solar

atmoshere. The understanding of the solar atmosphere is linked

to stellar atmospheric research. Topics covered include: the

existence of the chromosphere, the corona, and the solar wind;

the interactive complex of convection, differential rotation, magnetic

field generation and concentration, and the activity cycle;

phenomena such as granulation, supergranulation, the 5 minute

oscillation, filigree, faculae, sunspots, spicules, prominences,

surges, and the spectacular flares. For individual titles, see

N81-27009 through N81-27026.

203
90 ASTROPHYSICS

N82-21118"# National Aeronautics and Space Administration,

Washington, D.C.

GAMMA RAY ASTROPHYSICS: NEW INSIGHT INTO THE

UNIVERSE

C. E. FICHTEL and J. I. TROMBKA Washington 1981 405 p

refs Original contains color illustrations

(NASA-SP-453; NAS 1.21:453; LC-81-600116) Avail: NTIS MF

A01; SOD HC $10.00 CSCL 03B

Gamma ray observations of the solar system, the galaxy and

extragalactic radiation are reported. Topics include: planets,

comets, and asteroids; solar observations; interstellar medium and

galactic structure; compact objects; cosmology; and diffuse

radiation. The instrumentation used in gamma ray astronomy in

covered along with techniques for the analysis of observational

spectra. For individual titles, see N82-21119 through N82-21132.

N83-32693"# National Aeronautics and Space Administration,

Washington, D.C.

THE A-STARS: PROBLEMS AND PERSPECTIVES.

MONOGRAPH SERIES ON NONTHERMAL PHENOMENA IN

STELLAR ATMOSPHERES

S. C. WOLFF 1983 25t p refs Prepared in cooperation

with Centre National da la Recherche Scientifique, Paris

(NASA-SP-463; NAS 1.21:463; LC-83-061448) Avail: NTIS HC

A12/MF A01 CSCL 03B

Normal A type stars, nonradiative heating in A type stars,

magnetic Ap stars. The Am stars, the delta Scu stars, A supergiants,

peculiar B type stars, and model atmospheres are addressed.

Author

N84-19253°# National Aeronautics and Space Administration,

Washington, D.C.

STELLAR ATMOSPHERIC STRUCTURAL PATTERNS

R. N. THOMAS 1983 394 p refs Prepared in cooperation

with CNRS, Paris

(NASA-SP-471; NAS 1.21:471; LC-83-20242) Avail: NTIS HC

A17/MFA01 CSCL 03B

The thermodynamics of stellar atmospheres is discussed.

Particular attention is given to the relation between theoretical

modeling and empirical evidence. The characteristics of distinctive

atmospheric regions and their radical structures are discussed.

For individual titles, see N84-19254 through N84-19259.

N84-20457"# National Aeronautics and Space Administration.

Goddard Inst. for Space Studies, New York, N.Y.

MOLECULAR CLOUDS AND GALACTIC SPIRAL STRUCTURE

T. M DAME Feb. 1984 278 p refs

(NASA-TP-2288; NAS 1.60:2288; REPT-980) Avail: NTIS HC

A13/MF A01 CSCL 03B

EMISSION SPECTRA, GALACTIC STRUCTURE, MOLECULAR

CLOUDS, SPIRAL GALAXIES

N85-15539"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

LOCAL INTERSTELLAR MEDIUM. INTERNATIONAL

ASTRONOMICAL UNION COLLOQUIUM NO. 81

Y_ KONDO, ed., F. C. BRUHWEILER, ed. (Catholic Univ. of America,

Washington, D.C.), and B. D. SAVAGE, ed. (Wisconsin Univ.,

Madison) Washington Nov. 1984 356 p refs Colloq. held

in Madison, Wisc., 4-6 Jun. 1984

(NASA-CP-2345; NAS 1.55:2345) Avail: NTIS HC A16/MF A01

CSCL 03C

ASTRONOMICAL MODELS, CONFERENCES, COSMOLOGY,

HIGH TEMPERATURE GASES, HUBBLE SPACE TELESCOPE,

INTERSTELLAR MATTER, SUN

204

N86-25307" National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

INTERNATIONAL ULTRAVIOLET EXPLORER ATLAS OF

O-TYPESPECTRA FROM 1200 TO 1900 ANGSTROM

N. R. WALBORN (Space Telescope Science Inst., Baltimore, Md.),

J. NICHOLS-BOHLIN, and R. J. PANEK (Wellesley Colt.) Dec.

1985 153 p

(NASA-RP-1155; NAS 1.61:1155) Avail: NTIS HC A08 CSCL

03B

The IUE archives provide an unprecedented sample of uniform,

high-quality ultraviolet stellar spectra. In particular, they contain

high-resolution SWP data for nearly 200 different O stars. We

have undertaken a survey of the 1200-1900 A region in about

120 of them having homogeneous optical spectral classifications

to investigate systematically the behavior of the ultraviolet features,

incuding the prominent stellar wind profiles and the degree to

which they correlate with the optical types. The standard extracted

spectrograms have been rebinned to a constant wavelength

resolution of 0.25A and uniformly normalized (not dereddened) at

the GSFC RDAF. They are then plotted at 10A/cm, with reseau,

photometric quality and echelle order junction flags available. This

atlas contains such plots for about 100 stars, arranged in

spectral-type, luminosity and peculiar object sequences. The results

show a high degree of correlation between the ultraviolet features,

both photospheric and stellar-wind, and the optical classifications

for the majority of the O-type stars. Author

91

LUNAR AND PLANETARY EXPLORATION

Includes planetology; and manned and unmanned flights.

N77-15961"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

A GEOLOGICAL BASIS FOR THE EXPLORATION OF THE

PLANETS

R. GREELEY, ed. and M. H. CARR, ed. (Geological Survey, Menlo

Park, Calif.) Washington 1976 117 p refs

(NGR-05-017-037; NASA ORDER W-13576)

(NASA-SP-417) Avail: NTIS HC A06/MF A01 CSCL 03B

The relevance of planetary geology in relation to the origin

and evolution of the solar system and of life is discussed.

Stratigraphy, structural geology and geochemistry of planets were

examined.

N77-27053"# National Aeronautics and Space Administration.

Lyndon B. Johnson Space Center, Houston, Tex.

LUNAR SAMPLE STUDIES

Washington 1977 72 p refs

(NASA-SP-418) Avail: NTIS HC A04/MF A01 CSCL 03B

Lunar samples discussed and the nature of their analyses are:

(1) an Apollo 15 breccia which is thoroughly analyzed as to the

nature of the mature regolith from which it derived and the time

and nature of the lithification process, (2) two Apollo 11 and one

Apollo 12 basalts analyzed in terms of chemistry,

Cross-lddings-Pirsson-Washington norms, mineralogy, and

petrography, (3) eight Apollo 17 mare basalts, also analyzed in

terms of chemistry, Cross-lddings-Pirsson-Washington norms,

mineralogy, and petrography. The first seven are shown to be

chemically similar although of two main textural groups; the eighth

is seen to be distinct in both chemistry and mineralogy, (4) a

troctolitic clast from a Fra Mauro breccia, analyzed and contrasted

with other high-temperature lunar mineral assemblages. Two

basaltic clasts from the same breccia are shown to have affinities

with rock 14053, and (5) the uranium-thorium-lead systematics of

three Apollo 16 samples are determined; serious terrestrial-lead

contamination of the first two samples is attributed to bandsaw

cutting in the lunar curatorial facility. Author
N77-28055"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

PIONEER ODYSSEY

R. O. FIMMEL Washington 1977 229 p refs

(NASA-SP-349) Avail: NTIS MF A01; SOD HC 9.85 CSCL

03B

The Pioneer Jupiter Mission is discussed in terms of objectives,

hazards, spacecraft design, and communication techniques. The

scientific payloads of both Pioneer 10 and Pioneer 11 designed

to gather knowledge on interplanetary space beyond Mars and on

the Jovian system are included. Mission accomplishments are

described, J.M.S.

N77-29046"# National Aeronautics and Space Administration,

Washington, D.C.

VOYAGER TO JUPITER AND SATURN

1977 62 p

(NASA-SP-420) Avail: NTIS HC A04/MF A01 CSCL 03B

The NASA Voyager mission to explore planets of the outer

solar system is summarized. The mission schedule and profiles

for encounters with Jupiter and Saturn, and possibly with Uranus

and Pluto are included along with a description of the spacecraft

and its trajectories. Scientific investigations to be made and the

instruments carried are also discussed. A.R.H.

N78-16973"# National Aeronautics and Space Administration.

Lyndon B. Johnson Space Center, Houston, Tex.

SUMMER WORKSHOP ON NEAR-EARTH RESOURCES

J. R. ARNOLD, ed. (Calif. Univ., La Jolla) and M. B. DUKE, ed.

Jan. 1978 107 p refs Workshop held at La Jolla, Calif., 6-13

Aug. 1977

(NASA-CP-2031; S-482; JSCo13139) Avail: NTIS HC A06/MF

A01 CSCL 03B

ASTEROIDS, EXTRATERRESTRIAL RESOURCES, LUNAR

SOIL, RESOURCES MANAGEMENT

N78-20042"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

VIKING LANDER IMAGING INVESTIGATION: PICTURE

CATALOG OF PRIMARY MISSION EXPERIMENT DATA

RECORD

R. B. TUCKER (Stanford Univ. Med. Center, Calif.) Feb. 1978

514 p refs

(NASA-RP-1007; L-11752) Avail: NTIS HC A22/MF A01

CSCL 03B

All the images returned by the two Viking Landers during the

primary phase of the Viking Mission are presented. Listings of

supplemental information which described the conditions under

which the images were acquired are included together with skyline

drawings which show where the images are positioned in the field

of view of the cameras. Subsets of the images are listed in a

variety of sequences to aid in locating images of interest. The

format and organization of the digital magnetic tape storage of

the images are described. The mission and the camera system

are briefly described. Author

N78-29007"# National Aeronautics and Space Administration,

Washington, D.C.

ASTEROIDS: AN EXPLORATION ASSESSMENT

D. MORRISON, ed. and W. C. WELLS, ed. 1978 295 p refs

Conf. held at Chicago, 19-2t Jan. 1978

(NASA-CP-2053) Avail: NTIS HC A13/MF A01 CSCL 03B

ASTEROIDS, MISSION PLANNING, PLANETARY EVOLUTION,

SOLAR SYSTEM, SPACE MISSIONS

91 LUNAR AND PLANETARY EXPLORATION

N78-30025" National Aeronautics and Space Administration,

Washington, D.C.

ATLAS OF MERCURY

M. E. DAVIES, ed. (Rand Corp.), S. E. DORNIK, ed., D. E. GAULT,

ed (NASA. Ames Res. Center), and R. G. STROM, ed. (Arizona

Univ.) 1978 135 p refs

(NASA-SP-423) Avail: NTIS MF A01; HC SOD CSCL 03B

The Mariner 10 spacecraft, its scientific mission, and surface

mapping techniques are described as well as the topographic

features of the planet Mercury as photographed by television

cameras during three flyby encounters. Shaded relief maps and a

computer generated photomosaic of 9 of the 15 cartographic

regions are presented. Subsequent material in the atlas includes

enlargements of portions of the photomosaics, individual high

resolution pictures, mosaics of small areas, and stereo pairs located

within the boundaries of the cartographic regions, Footprint

locations of individual pictures and stereo pairs are plotted on the

shaded relief maps. Current values of the more important orbital

and physical properties of Mercury are presented in tables.

A.R.H.

N79-12984" National Aeronautics and Space Administration,

Washington, D.C.

THE MARTIAN LANDSCAPE

1978 160 p Original contains color illustrations

(NASA*SP-425; LC-78-606041) Avail: HC SOD $12.00 CSCL

03B

A first person, anecdotal account of preparations for

photographing the Martian surface is related by the leader of

NASA's Lander Imaging Science TRe Team. Particular attention

is given to the design of the facsimile camera. Image sequencing,

picture calibration, reconstruction of color, and the search for

motion on Mars are discussed. Over 200 color and black and

white photographs taken by both tanders are included along with

a table showing the camera settings used. A stereopticon is

included for viewing 19 stereopairs in three dimension. A.R.H

N79-14978"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ATMOSPHERIC ENTRY AND FRAGMENTATION OF DENSE

METEOROIDS

T. D. BESS Jan. 1979 37 p refs

(NASA-TP-1333; L-12506) Avail: NTIS HC A03/MF A01

CSCL 03B

ATMOSPHERIC ENTRY, DENSITY (MASS/VOLUME),

FRAGMENTATION, METEOROIDS

N79-16757"# National Aeronautics and Space Administration,

Washington, D.C.

SECOND INTERNATIONAL COLLOQUIUM ON MARS:

ABSTRACTS FOR A COLLOQUIUM

1979 97 p refs Colloq. held at Pasadena, Calif., 15-18 Jan.

1979

(NASA-CP-2072) Avail: NTIS HC A05/MF A01 CSCL 03B

ABSTRACTS, BIBLIOGRAPHIES, MARS (PLANET),

PLANETOLOGY, SPACE EXPLORATION, VIKING MARS

PROGRAM

N79-16758"# Jet Propulsion Lab., California Inst. of Tech.,

Pasadena.

THE SATURN SYSTEM

D. M. HUNTEN, ed. (Ariz. Univ., Tucson) and D. MORRtSON, ed.

Dec. 1978 423 p Workshop held at the Reston Intern. Conf.

Ctr., Reston, Virginia, 9-11 Feb. 1978

(NAS7-100)

(NASA-CP-2068) Avail: NTIS HC A18/MF A01 CSCL 03B

CONFERENCES, INTERPLANETARY SPACECRAFT,

MAGNETOSPHERE, MISSION PLANNING, NATURAL

SATELLITES, SATURN ATMOSPHERE, SATURN PROJECT,

SATURN RINGS

205
91 LUNAR AND PLANETARY EXPLORATION

N80-11972"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

SPACE MISSIONS TO COMETS

M. NEUGEBAUER, ed. (JPL), D. K. YEOMANS, ed. (JPL), J, C.

BRANDT, ed., and R. W. HOBBS, ed. Washington 1979 229

p refs Conf. held at Greenbelt, Md., Oct. 1977

(NASA-CP-2089) Avail: NTIS HC Alt/MF A0t CSCL 03B

COMETS, CONFERENCES, FLYBY MISSIONS, SOLAR

SYSTEM, SPACE MISSIONS

N80-16009"# National Aeronautics and Space Administration.

Lyndon B. Johnson Space Center, Houston, Tex.

HANDBOOK OF LUNAR MATERIALS

R. J. WILLIAMS, ed. and J. J. JADWlCK, ed. (Lockheed Electronics

Co., Houston, Tex.) Feb. 1980 133 p refs

(NASA-RP-1057) Avail: NTIS HC A07/MF A01 CSCL 03B

The physical, chemical, thermodynamic, and geologic data on

lunar rocks, minerals, and processes are summarized, and a set

of data metals that might be extracted from lunar materials is

presented. Author

N80-16998" Nationat Aeronautics and Space Administration,

Washington, D.C.

ATLAS OF MARS: THE 1:5000000 MAP SERIES

R. M. BATSON, P. M. BRIDGES, and J. U INGE 1979 154 p

refs Prepared in cooperation with Geol. Surv., Flagstaff, Ariz.

(NASA ORDER W-13709; NASA ORDER W-08122; NASA

ORDER W-13687; NASA ORDER L-55232)

(NASA-SP-438; LC-79-600164) Avail: SOD HC $7.00 as

NAS1.21:438 CSCL 03B

Small.scale maps and photomosaics covering the entire surface

of the planet Mars are presented. The cartographic contents are

reduced-scale versions of the 1:5,000,000 topographic series of

30 quadrangles compiled by the U.S. Geological Survey in

cooperation with NASA. Most of the quadrangles were compiled

with data from the Mariner 9 spacecraft, gathered in 1972. A few

sheets, however, incorporated information derived from the two

Viking Orbiter spacecraft from 1976 through 1978. Several versions

of each quadrangle are shown. These versions include the

controlled photomosaics from which final map products were

derived, airbrushed shaded relief maps based on the photomosaics

and on a variety of special computer enhancements of pictures

not included in the mosaics, shaded relief maps with overprints of

albedo markings derived by special enhancements of selected

Mariner 9 images and contour maps derived from a wide variety

of nonimage data ranging from Earth-based radar to remote sensing

instruments on the Mariner 9 spacecraft. Discussions of mapping

procedures and a gazeteer of feature nomenclature on Mars are

included in appendices. A.R.H.

N80-26239"# Jet Propulsion Lab., California Inst. of Tech.,

Pasadena.

IMAGES OF MARS: THE VIKING EXTENDED MISSION

M. H. CARR (Geological Survey) and N. EVANS 1980 35 p

(NASA-SP-444) Avail: NTIS HC A01; SOD HC $2.25 CSCL

03B

Although the Viking spacecraft were designed to operate for

only 90 days, the two landers and one orbiter have been observing

seasonal changes in the Martian atmosphere and surface for almost

4 years (2 Martian years). Views of the planet, some taken as

recently as late 1979, show volcanoes, lava plains, channels,

canyons, plateaus, impact craters, wind erosion', global dust storms,

polar caps, clouds, and the surface features of Phobos and Deimos.

The latter image is the highest resolution picture ever taken of

another object from an orbiter or flying spacecraft. A.R.H.

206

N80-27260"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

PROJECT ORION: A DESIGN STUDY OF A SYSTEM FOR

DETECTING EXTRASOLAR PLANETS

D. C. BLACK, ed. 1980 214 p refs Original contains color

illustrations

(NASA-SP-436; LC.80-11728) Avail: NTtS MF A01; SOD HC

$5,50 CSCL 03B

A design concept for a ground based astrometric telescope

that could significantly increase the potential accuracy of

astrometric observations is considered. The state of current

techniques and instrumentation is examined in the context of

detecting extrasolar planets. Emphasis is placed on the direct

detection of extrasolar planets at either visual or infrared

wavelengths. The design concept of the imaging stellar

interferometer (ISI), developed under Project Orion, is described.

The Orion ISI employs the state-of-the-art technology and is

theoretically capable of attaining 0.00010 arc sec/yr accuracy in

relative astrometric observations. J.M.S.

N81-10910"# National Aeronautics and Space Administration,

Washington, D.C.

VOYAGE TO JUPITER

D. MORRISON and J. SAMZ 1980 204 p Original contains

color illustrations

(NASA-SP-439; LC-80-600126) Avail: NTIS MF A01; SOD HC

$7.50 CSCL 03B

Early observations of the Jovian system are reviewed as well

as the scientific objectives of the Pioneer and Voyager flyby

missions. Launch vehicles, spacecraft trajectories, and the

instruments carried are described. Photographs obtained by both

voyage spacecraft are presented along with day-by-day summaries

of the findings recorded by the various instruments and experiments

carried by each spacecraft. Pictorial maps of the Galilean satellites,

and lists of the Voyager science and managements teams are

included. A.R.H.

N81-15925"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

PIONEER: FIRST TO JUPITER, SATURN, AND BEYOND

R. O. FIMMEL, J. VANALLEN (Iowa Univ.), and E. BURGESS

1980 296 p refs Original contains color illustrations

(NASA-SP-446) Avail: NTIS MF A01; SOD HC $13.00 CSCL

03B

The Pioneer Program continues to achieve far beyond its original

objectives because of the successful missions of Pioneers 10 and

11 which have been in space over 8 years and 7 years, respectively.

An overview of the Pioneer Jupiter/Saturn mission is presented

including the planning process; technical aspects of the spacecraft

design and operation; and the scientific payloads and the

experiments conducted during interplanetary flight and the flyby

portion of the missions. Data obtained from the various experiments

are analyzed. The imaging photopolarimeter is described and

technical details of planetary images are examined. AR.H.

N81-25012"# Jet Propulsion Lab., California Inst. of Tech.,

Pasadena.

VIKING LANDER IMAGING INVESTIGATION DURING

EXTENDED AND CONTINUATION AUTOMATIC MISSIONS.

VOLUME 1: LANDER 1 PICTURE CATALOG OF EXPERIMENT

DATA RECORD Final Report

K. L. JONES, M. HENSHAW, C. MCMENOMY, A. ROBLES, P. C.

SCRIBNER, S. D. WALL, and J. W. WILSON Apr. 1981 655 p

(NASA-RP-1068; L-14054-VOL-1) Avail: NTIS HC A99/MF A0t

CSCL 03B

All images returned by Viking Lander 1 during the extended

and continuation automatic phases of the Viking Mission are

presented. Listings of supplemental information which describe the

conditions under which the images were acquired are included

together with skyline drawings which show where the images are

positioned in the field of view of the cameras. Subsets of the

images are listed in a variety of sequences to aid in locating

images of interest. The format and organization of the digital
magneticapestorageoftheimagesaredescribed aswellasthe

missionandthecamerasystem. AR.H.

N81-25992"#National Aeronautics andSpaceAdministration.

LangleyResearch Center, Hampton, Va.

VIKING SITE SELECTION AND CERTIFICATION

H. MASURSKY (Geological Survey, Flagstaff, Ariz.) and N. L.

CRABILL Washington 1981 39 p refs

(NASA-SP-429) Avail: NTIS HC A03/MF A01 CSCL 03B

The landing site selection and certification effort for the Viking

mission to Mars is reviewed from the premission phase through

the acquisition of data and decisions during mission operations

and the immediate postlanding evaluation. The utility and limitations

of the orbital television and infrared data and ground based radar

observation of candidate and actual landing sites are evaluated.

Additional instruments and types of observations which would have

been useful include higher resolution cameras, radar altimeters,

and terrain hazard avoidance capability in the landing system.

Suggestions based on this experience that might be applied to

future missions are included. J.D.H.

N82-16028"# Jet Propulsion Lab., California Inst. of Tech.,

Pasadena.

VIKING LANDER IMAGING INVESTIGATION DURING

EXTENDED AND CONTINUATION AUTOMATIC MISSIONS.

VOLUME 2: LANDER 2 PICTURE CATALOG OF EXPERIMENT

DATA RECORD

K. L. JONES, M HENSHAW, C. MCMENOMY, A. ROBLES, P. C.

SCRIBNER, S. D. WALL, and J. W. WILSON Apr. 1981 566 p

refs 2 Vol.

(NASA-RP-1068-VOL-2; L-14054) Avail: NTIS HC A24/MF A01

CSCL 03B

Images returned by the two Viking landers during the extended

and continuation automatic phases of the Viking Mission are

presented. Information describing the conditions under which the

images were acquired is included with skyline drawings showing

the images positioned in the field of view of the cameras. Subsets

of the images are listed in a variety of sequences to aid in locating

images of interest. The format and organization of the digital

magnetic tape storage of the images are described. A brief

description of the mission and the camera system is also

included. Author

N82-25043"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

VIBRATIONAL-ROTATIONAL SPECTROSCOPY FOR PLANETARY ATMOSPHERES, VOLUME 1

M. J. MUMMA, ed., K. FOX, ed. (Tennessee Univ.), and J.

HORNSTEIN, ed. (Computer Sciences Corp.) Apr. 1982 416 p

refs Proceedings of Workshop held at Annapolis, 17-19 Mar.

1980

(NASA-CP-2223-VOL-1; NAS 1.55:2223-VOL-1) Avail: NTIS HC

A18/MF A01 CSCL 03B

EARTH ATMOSPHERE, INFRARED RADIOMETERS, JUPITER

ATMOSPHERE, LASER SPECTROSCOPY, MARS ATMOSPHERE,

MOLECULAR SPECTRA, PLANETARY ATMOSPHERES,

SPECTROMETERS, VIBRATIONAL SPECTRA

N82-26134"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

VIBRATIONAL-ROTATIONAL SPECTROSCOPY FOR PLANETARY ATMOSPHERES, VOLUME 2

M. J. MuMMA, ed., K. FOX, ed. (Tennessee Univ.), and J.

HORNSTEIN, ed. (Computer Sciences Corp.) Apr. 1982 242 p

refs Proceedings of Workshop held at Annapolis, Md., 17-19

Mar. 1980

(NASA-CP-2223-VOL-2; NAS 1.55:2223) Avail: NTIS HC

A!I/MF A04 CSCL 03B

ATMOSPHERIC COMPOSITION, CONFERENCES, HYDROGEN, LINE SPECTRA, METHANE, PLANETARY ATMOSPHERES

91 LUNAR AND PLANETARY EXPLORATION

N82-26152"# National Aeronautics and Space Administration,

Washington, D.C.

VOYAGES TO SATURN

D. MORRISON 1982 232 p refs

(NASA-SP-451; NAS 1.21:451; LC-81-600073) Avail: NTIS HC

A11/MF A01 CSCL 03B

The Voyager mission to Saturn is explained in detail. A history

of Saturn observations from ancient times to the present is given.

The Voyager spacecraft and their instruments are described. An

overview of planetary astronomy is presented. The text is

supplemented by numerous black and white and color photographs.

The Saturn satellites are discussed in detail, and preliminary

pictorial maps of the satellites are given. R.J.F.

N83-12031"# Arizona Univ., Tucson. Lunar and Planetary Lab.

NASA CATALOGUE OF LUNAR NOMENCLATURE

L. A. ANDERSSON and E. A. WHITAKER Washington Oct.

1982 172 p

(NGL-03-002-191)

(NASA-RP-1097; NAS 1.61:1097) Avail: NTIS HC A08/MF A01

CSCL 03B

Lunar nomenclature is cataloged. It includes letter designations

for subsidiary craters, and uses a more familiar spelling from eight

names. The listed features are divided into three main groups for

cataloging purposes, namely: (1) craters, (2) noncrater features;

and (3) minor and miscellaneous features. S.L.

N83-25636" Geological Survey, Flagstaff, Ariz.

A CATALOG OF SELECTED VIKING ORBITER IMAGES

R. L. TURNER and R. D. CARROLL Feb. 1983 402 p refs

(NASA-RP-1093; NAS 1.61:1093) Avail: NTIS HC A17 CSCL

03B

This collection of Viking Orbiter photomosaics is designed to

facilitate identification and location of the various pictures with

respect to the surface of Mars. Only a representative set of the

nearly 50,000 images taken by the two Viking Orbiters, and

computer-processed prior to December 1978, are contained in

the mosaics and in the picture listings. Author

N83-30340"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

PIONEER VENUS

R O. FIMMEL, L. COLIN, and E. BURGESS 1983 254 p refs

Original contains color illustrations

(NASA-SP-461; NAS 1.21:461) Avail: NTIS MF A01; SOD HC

$11.00 CSCL 03B

Venus before Pioneer, the Pioneer Venus mission, Pioneer

Venus spacecraft, scientific investigation, mission to Venus

scientific results, and results of Soviet studies of Venus are

addressed. A chronology of exploration of Venus from Earth before

the Pioneer Venus mission and Venus nomenclature and mythology

are provided. Author

N84-32330" Jet Propulsion Lab., California Inst. of Tech.,

Pasadena.

PHOBOS: CLOSE ENCOUNTER IMAGING FROM THE VIKING

ORBITERS

T. C. DUXBURY, J. D. CALLAHAN, and A. C. OCAMPO Jul.

1984 56 p

(NASA-RP-1109; NAS 1.61:1109) Avail: NTIS HC A04 CSCL

03B

The shape and orbital characteristics of Phobos, the larger

and innermost of Mars' two irregular moons, are discussed and

illustrated. Also presented are the high resolution pictures of

Phobos that were obtained during the close flybys of Viking Orbiters

1 and 2 The viewing geometry is also given for each picture.

E.R.

207
91 LUNAR AND PLANETARY EXPLORATION

N84-34363"# National Aeronautics and Space Administration,

Washington, D.C.

TRENDS IN PLANETARY DATA ANALYSIS. EXECUTIVE

SUMMARY OF THE PLANETARY DATA WORKSHOP

N. EVANS Sep. 1984 46 p Workshop held in Greenbelt, Md.,

29 Nov. - 2 Dec. 1983

(NASA-CP-2333; NAS 1.55:2333) Avail: NTIS HC A03/MF A01

CSCL 03B

DATA BASES, DATA MANAGEMENT, DATA REDUCTION,

DATA SYSTEMS, IMAGE ANALYSIS, PLANETOLOGY, USER

REQUIREMENTS

N84-34366"# National Aeronautics and Space Administration,

Washington, D.C.

PLANETARY DATA WORKSHOP, PART 1

Oct. 1984 143 p Workshop held in Greenbelt, Md., 29 Nov. -

1 Dec. 1983 2 Vol.

(NASA-CP-2343-PT-1; NAS 1.55:2343-PT-1) Avail: NTIS HC

A07/MF A01 CSCL 03B

CONFERENCES, DATA BASE MANAGEMENT SYSTEMS,

PLANETS, SPACE EXPLORATION, SPACE OBSERVATIONS

(FROM EARTH), SPACEBORNE EXPERIMENTS

N84-34376"# National Aeronautics and Space Administration,

Washington, D.C.

PLANETARY DATA WORKSHOP, PART 2

Oct. 1984 133 p Workshop held in Greenbelt, Md., 29 Nov. -

1 Dec. 1983 2 VoI.

(NASA-CP-2343-PT-2; NAS 1.55:2343-PT-2) Avail: NTIS HC

A07/MF A01 CSCL 03B

COMMUNICATING, COMPUTER GRAPHICS, COMPUTER

NETWORKS, COMPUTER SYSTEMS DESIGN, COMPUTER

SYSTEMS PROGRAMS, CONFERENCES, DATA BASE

MANAGEMENT SYSTEMS, DATA MANAGEMENT, DATA

PROCESSING, DATA STORAGE, DATA SYSTEMS, GEOMETRY,

IMAGE PROCESSING

N84-35242"# National Aeronautics and Space Administration,

Washington, D.C.

VOYAGER 1 AND 2 ATLAS OF SIX SATURNIAN SATELLITES

R. M. BATSON et al. 1984 175 p refs Original contains

color illustrations

(NASA ORDER WO-8395; NASA ORDER W-13709)

(NASA-SP-474; NAS 1.21:474; LC-84-11580) Avail: NTIS HC

A08 CSCL 03B

Maps, compiled with data gathered primarily by Voyager 1 and

2 spacecraft, are presented which show the diversity among six

of the Saturnian moons. Mimas and Enceladus are mapped in

detail. Pretimary maps are given for the other four satellites.

Diameter, density, albedo, and distance from mother planet, among

much more data, is given for each moon. E.R.

N84-35248"# National Aeronautics and Space Administration,

Washington, D.C.

ON MARS: EXPLORATION OF THE RED PLANET, 1958 -

1978

E. C. EZELL, ed. and L. N. EZELL, ed. 1984 545 p refs

Original contains color illustrations

(NASA-SP-4212; NAS 1.21:4212; LC-82-22302) Avail: NTIS MF

A01; SOD HC $20.00 as 033-000-00869-4 CSCL 03B

The exploration of Mars is covered by the following topics:

Mariner spacecraft and launch vehicles, search for Martian life;

Voyager spacecraft; creation of Viking; Viking Orbiter and its Mariner

inheritance; Viking lander; building a complex spacecraft; selecting

landing sites; site certification, and data from Mars. For individual

titles see N84-35249 through N84-35259.

208

N85-11927"# Jet Propulsion Lab., California Inst. of Tech.,

Pasadena.

URANUS AND NEPTUNE

J. T. BERGSTRALH, ed. Washington Oct. 1984 605 p refs

Workshop held in Pasadena, Calif., 6-8 Feb. 1984

(NASA-CP-2330; NAS 1.55:2330) Avail: NTIS HC A99/MF A01;

SOD HC CSCL 03B

CONFERENCES, MAGNETOSPHERE, NEPTUNE (PLANET),

PLANETARY RINGS, SPECTRUM ANALYSIS, URANUS (PLANET),

VOYAGER PROJECT

N85-21099"# Jet Propulsion Lab., California Inst. of Tech.,

Pasadena.

CONCLUSION OF VIKING LANDER IMAGING INVESTIGATION:

PICTURE CATALOG OF EXPERIMENT DATA RECORD

S D. WALL and T. C. ASHMORE Mar. 1985 175 p refs

(NASA-RP-1137; L-15925; NAS 1.61:1137) Avail: NTIS HC

AO4/MF A01 CSCL 03B

The images returned by the two Viking landers during the Viking

Survey Mission are presented in this report. Listing of supplemental

information which describe the conditions under which the images

were acquired are included. Subsets of the images are listed in a

variety of sequences to aid in locating images of interest. The

format and organization of the digital magnetic tape storage of

the images are described. A brief description of the mission and

the camera system is also included. Author

N85-22323"# National Aeronautics and Space Administration,

Washington, D.C. The Planetary Cartography Working Group.

PLANETARY CARTOGRAPHY IN THE NEXT DECADE (1984 -

1994)

1984 71 p refs

(NASA-SP-475; NAS 1.21:475) Avail: NTIS HC $10.00/MF A01

CSCL 03A

The cartographic products required to support science and

planetary exploration during the next 10 years were assessed.

Only major map series or first order maps needed to characterize

the surface physiography of a planet or satellite were considered.

Included in these considerations are maps needed as bases for

plotting geologic, geophysical, and atmospheric phenomena and

for planning future planetary exploration. These products consist

of three types of maps: controlled photomosaics, shaded relief

maps, and topographic contour maps. E.A.K.

N86-11137"# Jet Propulsion Lab., California Inst. of Tech.,

Pasadena.

GALILEO: EXPLORATION OF JUPITER'S SYSTEM

T. V. JOHNSON, C. M. YEATES, L. COLIN (NASA. Ames Research

Center), F. P. FANALE (Hawaii Univ.), L. FRANK (iowa Univ.),

and D. M. HUNTEN (Arizona Univ.) Jun. 1985 179 p refs

(NASA-SP-479; NAS 1.21:479) Avail: NTIS HC A09/MF A01

CSCL 03B

The scientific objectives of the Galileo mission to the Jovian

system is presented. Topics discussed include the history of the

project, our current knowledge of the system, the objectives of

interrelated experiments, mission design, spacecraft, and

instruments. The management, scientists, and major contractors

for the project are also given. Author
92

SOLAR PHYSICS

Includes solar activity, solar flares, solar radiation and sunspots.

N79-20961"# National Aeronautics and Space Administration,

Washington, D.C.

SUN, WEATHER, AND CLIMATE

J. R. HERMAN and R. A. GOLDBERG 1978 365 p refs

(NASA-SP-426; LC-78-606053) Avail: NTIS MF A01; SOD HC

CSCL 03B

The general field of Sun-weatherclimate relationships, that is,

apparent weather and climate responses to solar activity is

introduced and theoretical and experimental suggestions for further

research to identify and investigate the unknown causal

mechanisms are provided. Topics of discussion include: (1)

solar-related correlation factors and energy sources; (2) long-term

climatic trends; (3) short-term meteorological correlations; (4)

miscellaneous obscuring influences; (5) physical processes and

mechanisms; (6) recapitulation of sun-weather relationships; and

(7) guidelines for experiments. For individual titles, see N79-20962

through N79-20969.

N79-22991"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

A NEW SUN: THE SOLAR RESULTS FROM SKYLAB

J. A. EDDY and R. ISE, ed. Washington 1979 220 p Original

contains color illustrations

(NASA-SP-402) Avail: NTIS MF A01; SOD HC $10.50 CSCL

03B

The highlights of the new and exciting pictures of the sun as

taken by Skylab astronauts are presented. Topics of discussion

and pictures include: (1) the nearest star; (2) the masks of the

sun; (3) the sun from space; (4) the solar telescope on Skylab;

and (5) the solar results from Skylab - the quiet sun and the

active Sun. G.Y.

N80-17944"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

STUDY OF THE SOLAR CYCLE FROM SPACE

Feb. 1980 366 p refs Symp. held at Wellesley, Mass., 14-15

Jun. 1979; sponsored in part by Am. Astron. Soc.

(NASA-CP-2098; REPT-780t) Avail: NTIS HC A16/MF A01

CSCL 03B

ASTROMETRY, CONFERENCES, MISSION PLANNING,

SOLAR CYCLES, SPACEBORNE ASTRONOMY, SUN

N81-13912"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md,

ENVIRONMENTAL ANALYSIS OF THE CHEMICAL RELEASE

MODULE

J. P. HEPPNER and M. DUBIN Nov. 1980 131 p refs

(NASA-TP-1750; REPT-80-F-5120) Avail: NTIS HC A07/MF

A01 CSCL 13B

ATMOSPHERIC CHEMISTRY, ATMOSPHERIC PHYSICS,

CHEMICAL CLOUDS, ENVIRONMENT EFFECTS, SPACE

SHUTTLE PAYLOADS

N81-23004" National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

AN ATLAS OF SOLAR SPECTRA BETWEEN 1175 AND i950

ANGSTROMS RECORDED ON SKYLAB WITH THE NRL'S

APOLLO TELESCOPE MOUNT EXPERIMENT

L. COHEN Mar. 1981 566 p

(NASA-RP-1069) Avail: SOD HC $31.00 CSCL 03B

Spectra of selected solar regions were recorded by the Naval

Research Laboratory slit spectrograph on the Apollo Telescope

Mount aboard Skylab. This atlas of those spectra is intended as

a guide to the formulation of experiments and analysis of data

obtained by extreme ultraviolet spectrographs and may be valuable

to investigators analyzing International Ultraviolet Explorer spectra

92 SOLAR PHYSICS

and data from Solar Maximum Mission and High Resolution

Telescope Spectrograph. The slit spectrograph was used to cover

the range 1175 A to 1950 A with a spectral resolution of 0.06 A

and a spatial resolution at Sun center of 2 deg by 30 deg.

Microdensitometer tracings of spectra from (1) a quiet region, (2)

an active region, (3) a coronal hole, and (4) a flare are included

and were computer processed to include the characteristic curve

of the film. Line identifications for prominent features are included

as welt as a reference scale permitting the user to obtain absolute

intensities. J.M.S.

N82-17014"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

VARIATIONS OF THE SOLAR CONSTANT

S. SOFIA, ed. Dec. 1981 285 p refs Workshop held in

Greenbelt, Md., 5-7 Nov. 1980

(NASA-CP-2191) Avail: NTIS HC A13/MF A01 CSCL 03B

CONFERENCES, PERIODIC VARIATIONS, SOLAR

CONSTANT, STELLAR STRUCTURE

N83-13048"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

THE PINHOLE/OCCULTER FACILITY

J. R. DABBS, E. A. TANDBERG-HANSSEN, and H. S. HUDSON

(California Univ., San Diego) Oct. 1982 16 p

(NASA-TP-2089; NAS 1.60:2089) Avail: NTIS HC A02/MF A01

CSCL 03B

SOLAR ACTIVITY, SOLAR CORONA, SOLAR WIND, X RAY

ASTRONOMY

N83-25646"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

THE PINHOLE/OCCULTER FACILITY

E. A. TANDBERG-HANSSEN, ed., H. S. HUDSON, ed. (California

Univ., San Diego), J. R. DABBS, ed., and W. A. BAITY, ed.

(California Univ., San Diego) Apr. 1983 55 p refs

(NASA-TP-2168; NAS 1.60:2168) Avail: NTIS HC A04/MF A01

CSCL 03B

CORONAGRAPHS, OCCULTATION, PINHOLES, SOLAR

PHYSICS, SPACE SHUTTLE PAYLOADS, X RAY ASTRONOMY

N84-13067"# Jet Propulsion Lab., California Inst. of Tech.,

Pasadena.

SOLAR WIND FIVE

M NEUGEBAUER, ed. Washington Nov. 1983 688 p refs

Conf. held in Woodstock, Vt., 1-5 Nov. 1982

(NASA-CP-2280; NAS 1.55:2280) Avail: NTIS HC A99/MF A01

CSCL 03B

CONFERENCES, ENERGETIC PARTICLES, MAGNETIC FIELD

CONFIGURATIONS, MAGNETOHYDRODYNAMIC TURBULENCE,

SOLAR CORONA, SOLAR WIND

N84-24520"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

A COMPARATIVE LOOK AT SUNSPOT CYCLES

R. M. WILSON May 1984 177 p refs

(NASA-TP-2325; NAS 1.60:2325) Avail: NTIS HC A09/MF A01

CSCL 03B

REGRESSION ANALYSIS, SOLAR ACTIVITY, SUN, SUNSPOT

CYCLE

N84-27635"# National Aeronautics and Space Administration,

Washington, D.C.

SOLAR IRRADIANCE VARIATIONS ON ACTIVE REGION TIME

SCALES

B. J. LABONTE, ed. (Hawaii Univ. at Manoa, Honolulu), G. A.

CHAPMAN, ed. (California State Univ., Northridge), H. S HUDSON,

ed. (California Univ. at San Diego, La Jolla), and R. C. WILLSON,

ed. (JPL) Washington May 1984 310 p refs Proc. of

workshop held in Pasadena, Calif., 20-21 Jun. 1983

(NASA-CP-2310; NAS 1.55:2310) Avail: NTIS HC A14/MF A01

CSCL 03B

IRRADIANCE, LIMB DARKENING, SOLAR ACTIVITY

209
92 SOLAR PHYSICS

EFFECTS, SOLAR TERRESTRIAL INTERACTIONS, SPECTRUM

ANALYSIS

N85-29869"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

MEASUREMENTS OF SOLAR VECTOR MAGNETIC FIELDS

M. J. HAGYARD, ed. Washington May 1985 477 p refs

Conf. held in Huntsville, Ala., 15-18 May 1984; sponsored by NASA,

Alabama Univ., and NOAA Original contains color illustrations

(NASA-CP-2374; M-484; NAS 1.55:2374) Avail: NTIS HC

A21/MF A0t CSCL 03B

DATA REDUCTION, DISPLAY DEVICES, FORCE-FREE

MAGNETIC FIELDS, MAGNETIC FLUX, PHOTOSPHERE, SOLAR

ATMOSPHERE, SOLAR CORONA, SOLAR MAGNETIC FIELD,

VECTORS (MATHEMATICS)

N85-34729"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

NINTEENTH INTERNATIONAL COSMIC RAY CONFERENCE. SH

SESSIONS, VOLUME 4

F. C. JONES, comp. Washington Aug. 1985 543 p refs

Conf. held in La Jolla, Calif., 11-23 Aug. 1985 8 Vol.

(NASA-CP-2376-VOL-4; NAS 1.55:2376-VOL-4) Avail: NTIS HC

as boxed set only $200/MF A01 per volume or E99 per entire

set CSCL 03B

CONFERENCES, COSMIC RAYS, HELIOSPHERE,

INTERPLANETARY MEDIUM, PARTICLE ACCELERATION,

SOLAR CORPUSCULAR RADIATION, SOLAR FLARES

N86-24614"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

SOLAR FLARES AND CORONAL PHYSICS USING P/OF AS A

RESEARCH TOOL

E. TANDBERG, ed., R. M. WILSON, ed., and R. M. HUDSON, ed.

(California Univ., San Diego, La Jolla) Apr. 1986 307 p refs

Workshop held in Huntsville, Ala., 8-10 May 1985

(NASA-CP-2421; M-523; NAS 1.55:2421) Avail: NTIS HC

A14/MF A01 CSCL 03B

OCCULTATION, PINHOLES, SOLAR CORONA, SOLAR

FLARES, SOLAR PHYSICS, SOLAR X-RAYS

93

SPACE RADIATION

Includes cosmic radiation; and inner and outer earth's radiation

belts.

N79-27057"# Texas Univ, Austin.

CATALOG OF FAR-ULTRAVIOLET OBJECTIVE-PRISM

SPECTROPHOTOMETRY: SKYLAB EXPERIMENT S-019,

ULTRAVIOLET STELLER ASTRONOMY

K. G. HENIZE, J. D WRAY, S. B. PARSONS, and G. F.

BENEDICT May 1979 545 p refs Prepared in cooperation

with Texas Univ. at Austin

(NAS9-13176; NAS8-13176; NAS8-31459; NSG-7371)

(NASA-RP-1031; S-495) Avail: NTIS HC A03/MF A01 CSCL

03B

Ultraviolet stellar spectra in the wavelength region from 1300

to 5000 A (130 to 500) were photographed during the three manned

Skylab missions using a 15 cm aperture objective-prism telescope.

The prismatic dispersion varied from 58 A mm/1 at 1400 A to

1600 A mm/1 at 3000 A. Approximately 1000 spectra representing

500 stars were measured and reduced to observed fluxes. About

100 stars show absorption lines of Si IV, C IV, or C 11. Numerous

line features are also recorded in supergiant stars, shell stars, A

and F stars, and Woff-Rayet stars. Most of the stars in the catalog

are of spectral class B, with a number of O and A type stars and

a sampling of WC, WN, F and C type stars. Spectrophotometric

results are tabulated for these 500 stars Author

210

N82-33320'# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

EARTH RADIATION SCIENCE SEMINARS

J. B. HALL, JR., comp. Aug. 1982 175 p refs Seminars

held at Hampton, Va., Jun. 1980 - Oct. 1981

(NASA-CP-2239; L-15483; NAS 1.55:2239) Avail: NTIS HC

A08/MF A01 CSCL 03B

CARBON DIOXIDE CONCENTRATION, CONFERENCES,

EARTH RADIATION BUDGET EXPERIMENT, INSOLATION,

RADIOMETERS

N83-29169"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

HEAVY ION TRANSPORT IN THE STRAIGHT AHEAD

APPROXIMATION

J. W. WILSON Jun. 1983 22 p refs

(NASA-TP-2178; L-15623; NAS 1.60:2178) Avail: NTIS HC

A02/MF A01 CSCL 03B

APPROXIMATION, HEAVY tONS, TRANSPORT PROPERTIES

N84-21485"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

MEAN EXCITATION ENERGIES FOR STOPPING POWERS IN

VARIOUS MATERIALS USING LOCAL PLASMA OSCILLATOR

STRENGTHS

J. W. WILSON, Y. J. XU (Old Dominion Univ.), E. KAMARATOS

(Christopher Newport Coll.), and C. K. CHANG (Christopher

Newport Coll.) Mar. 1984 38 p refs

(NCC1-42; NSG-1614)

(NASA-TP-2271; L-15731; NAS 1.60:2271) Avail: NTIS HC

A03/MF A01 CSCL 03B

ABSORBERS (MATERIALS), ENERGY TRANSFER,

EXCITATION, PLASMA OSCILLATIONS, STOPPING POWER

N85-33901"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

NINTEENTH INTERNATIONAL COSMIC RAY CONFERENCE.

CONFERENCE PROGRAM AND AUTHOR INDEX

F. C. JONES, comp. Washington Aug. 1985 259 p Conf.

held in La Jell& Calif., 11-23 Aug. 1985

(NASA-CP-2376; NAS 1.55:2376) Avail: NTIS HC as boxed set

only $200/MF A01 per volume or E99 per entire set CSCL 03B

CONFERENCES, COSMIC RAYS, EXTRATERRESTRIAL

RADIATION, INDEXES (DOCUMENTATION)

N85-33902"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

NINTEENTH INTERNATIONAL COSMIC RAY CONFERENCE.

OG SESSIONS, VOLUME 1

F. C. JONES, comp Washington Aug. 1985 409 p refs

Conf. held in La Jolla, Calif., 11-23 Aug. 1985 8 Vol.

(NASA-CP-2376-VOL-1; NAS 1.55:2376-VOL-1) Avail: NTIS HC

as boxed set only $200/MF A01 per volume or E99 per entire

set CSCL 03B

CONFERENCES, COSMIC RAYS, DIFFUSE RADIATION,

GAMMA RAY ASTRONOMY, GAMMA RAYS, POINT SOURCES

N85-34006"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

NINTEENTH INTERNATIONAL COSMIC RAY CONFERENCE.

OG SESSIONS, VOLUME 2

F. C. JONES, comp. Washington Aug. 1985 441 p refs

Conf. held in La Jolla, Calif., 11-23 Aug. 1985 8 Vol.

(NASA-CP-2376-VOL-2; NAS 1.55:2376-VOL-2) Avail: NTIS HC

as boxed set only $200/MF A01 per volume or E99 per entire

set CSCL 03B

ANTIPROTONS, CONFERENCES, COSMIC RAYS, ENERGY

SPECTRA, ISOTOPES, NUCLEI (NUCLEAR PHYSICS)
N85-34862"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

NINETEENTH INTERNATIONAL COSMIC RAY CONFERENCE.

OG SESSIONS, VOLUME 3

F. C. JONES, comp. Washington Aug. 1985 530 p refs

Conf. held in La Jolla, Calif., 11-23 Aug. 1985 8 Vol.

(NASA-CP-2376-VOL-3; NAS 1.55:2376-VOL-3) Avail: NTIS HC

as boxed set only $200/MF A01 per volume or E99 per entire

set CSCL 03B

CONFERENCES, COSMIC RAYS, NUCLEAR INTERACTIONS,

PARTICLE ACCELERATION

N85-34991"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

NINETEENTH INTERNATIONAL COSMIC RAY CONFERENCE.

SH SESSIONS, VOLUME 5

F. C. JONES, comp. Washington Aug. 1985 589 p refs

Conf. held in La Jolla, Calif., 11-23 Aug. 1985 8 Vol.

(NASA-CP-2376-VOL-5; NAS 1.55:2376-VOL-5) Avail: NTIS HC

as boxed set only $200/MF A01 per volume or E99 per entire

set CSCL 03B

CONFERENCES, COSMIC RAYS, HELIOSPHERE, PERIODIC

VARIATIONS, SOLAR CORPUSCULAR RADIATION, SOLAR

NEUTRINOS

N85-35848"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

NINETEENTH INTERNATIONAL COSMIC RAY CONFERENCE.

HE SESSIONS, VOLUME 6

F. C. JONES, comp. Washington Aug. 1985 496 p refs

Conf. held in La Jolla, Calif., 11-23 Aug. 1985 8 Vol.

(NASA-CP-2376-VOL-6; NAS 1.55:2376-VOL-6) Avail: NTIS HC

as boxed set only $200/MF A01 per volume or E99 per entire

set CSCL 03B

CONFERENCES, COSMIC RAYS, HIGH ENERGY

INTERACTIONS, NUCLEI (NUCLEAR PHYSICS), PARTICLE

INTERACTIONS, PARTICLE PRODUCTION

N85-35968"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

NINETEENTH INTERNATIONAL COSMIC RAY CONFERENCE.

HE SESSIONS, VOLUME 7

F. C. JONES, comp. Washington Aug. 1985 398 p refs

Conf. held in La Jolla, Calif., 11-23 Aug. 1985 8 Vol.

(NASA-CP-2376-VOL-7; NAS 1.55:2376-VOL-7) Avail: NTIS HC

as boxed set only $200/MF A01 per volume or E99 per entire

set CSCL 03B

CONFERENCES, COSMIC RAY SHOWERS, COSMIC RAYS,

GAMMA RAYS, HIGH ENERGY INTERACTIONS

N85-36066"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

NINETEENTH INTERNATIONAL COSMIC RAY CONFERENCE.

HE SESSIONS, VOLUME 8

F. C. JONES, comp. Washington Aug. 1985 387 p refs

Conf. held in La Jolla, Calif., 11-23 Aug. 1985 8 Vol.

(NASA-CP-2376-VOL-8; NAS 1.55:2376-VOL-8) Avail: NTIS HC

as boxed set only $200/MF A01 per volume or E99 per entire

set CSCL 03B

CONFERENCES, COSMIC RAYS, MAGNETIC MONOPOLES,

MUONS, NEUTRINOS

N86-21492"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, Va.

ELECTROMAGNETIC DISSOCIATION EFFECTS IN GALACTIC

HEAVY-ION FRAGMENTATION

J. W. NORBURY and L. W. TOWNSEND Feb. 1986 48 p

refs

(NASA-TP-2527; L-16033; NAS 1.60:2527) Avail: NTIS HC

A03/MF A01 CSCL 03B

COULOMB COLLISIONS, DISSOCIATION, GALACTIC COSMIC

RAYS, HEAVY IONS, RADIATION SHIELDING

99 GENERAL

N86-28904"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

NINETEENTH INTERNATIONAL COSMIC RAY CONFERENCE

PAPERS. GENERAL INDEX, VOLUME 10

F. C. JONES, comp, Jul. 1986 104 p Conference held in La

Jolla, Calif., 11-23 Aug. 1985

(NASA-CP-2376-VOL-10; NAS 1.55:2376-VOL-10) Avail: NTIS

HC as boxed set only $200/MF A01 per volume or E99 per

entire set CSCL 03B

CONFERENCES, COSMIC RAYS, EXTRATERRESTRIAL

RADIATION, INDEXES (DOCUMENTATION)

N86-31483"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, Md.

NINETEENTH INTERNATIONAL COSMIC RAY CONFERENCE.

CONFERENCE PAPERS: INVITED RAPPORTEUR, HIGHLIGHT,

MISCELLANEOUS, VOLUME 9

F. C. JONES, comp. Feb. 1986 555 p Conference held in La

Jolla, Calif., 11-23 Aug. 1985

(NASA-CP-2376-VOL-9; NAS 1.55:2376-VOL-9) Avail: NTIS HC

as boxed set only $200/MF A01 per volume or E99 per entire

set CSCL 03B

COSMIC RAYS, ELEMENTARY PARTICLES, GAMMA RAYS

99

GENERAL

N77-16981"# National Aeronautics and Space Administration,

Washington, D.C.

ORIGINS OF NASA NAMES

H. T. WELLS, S. H. WHITELEY, and C. E. KAREGEANNES

1976 237 p refs

(NASA-SP-4402; LC-75-600069) Avail: NTIS MF A01; SOD HC

$3.65 CSCL 05B

Names are selected for NASA spaceflight projects and programs

from various sources. Some have their foundations in mythology

and astrology or legend and folklore. Some have historic

connotations; others are based on a description of their mission,

often resulting in an acronym. Included are names of launch

vehicles, spacecraft, manned spaceflight programs, sounding

rockets, and NASA field installations. This study is limited to names

of approved projects through 1974; it does not include names of

numerous projects which have been or are being studied or projects

that were canceled or postponed before reaching actual flight.

Author

N77-33030"# National Aeronautics and Space Administration,

Washington, D.C.

ESSAYS ON THE HISTORY OF ROCKETRY AND

ASTRONAUTICS: PROCEEDINGS OF THE THIRD THROUGH

THE SIXTH HISTORY SYMPOSIA OF THE INTERNATIONAL

ACADEMY OF ASTRONAUTICS, VOLUME 1 History Report,

1590- 1957

R. C. HALL, ed Sep. 1977 244 p refs Syrup. held at Mar

del Plata, Arg, 10 Oct. 1969; Constance, West Ger., 11-12 Oct.

1970; Brussels, 23 Sep. 1971 and Vienna, 13 Oct. 1972 2 Vot.

(NASA-CP-2014-VOL-1) Avail: NTIS MF A01; SOD HC CSCL

22A

ASTRONAUTICS, HISTORIES, MILITARY TECHNOLOGY,

ROCKET FLIGHT

211
99 GENERAL

N77-33048"# National Aeronautics and Space Administration,

Washington, DC.

ESSAYS ON THE HISTORY OF ROCKETRY AND

ASTRONAUTICS: PROCEEDINGS OF THE THIRD THROUGH

THE SIXTH HISTORY SYMPOSIA OF THE INTERNATIONAL

ACADEMY OF ASTRONAUTICS, VOLUME 2 History Report,

1590- 1957

R C. HALL, ed. 1977 476 p refs Symp. held at Mar. del

Plata, Arg, 10 Oct. 1969; Constance, West Ger., 11-12 Oct. 1970;

Brussels, 23 Sep. 1971; and Vienna, 13 Oct. 1972 2 VoL

(NASA-CP-2014-VOL-2) Avail: NTIS MF A01; SOD HC CSCL

19G

HISTORIES, ROCKET ENGINE DESIGN, ROCKET

PROPELLANTS, SOLID PROPELLANT ROCKET ENGINES

N78-12997"# National Aeronautics and Space Administration,

Washington, D.C.

ASTRONAUTICS AND AERONAUTICS, 1974: A CHRONOLOGY

NASA History Series

N L. BRUN 1977 323 p refs

(NASA-SP-4019; LC-65-60308) Avail: NTIS MF A01; SOD HC

$4.90 CSCL 05A

The 14th volume in the NASA series of day-by-day records of

aeronautical and space events has somewhat narrowed its scope

and selectivity in its brief accounts from immediately available,

open sources. This year the emphasis is even more directly focused

on concrete air and space activities. The text continues to reflect

some events in other agencies and countries. Author

N78-23010"# National Aeronautics and Space Administration,

Washington, D.C.

FOURTH NASA INTER-CENTER CONTROL SYSTEMS

CONFERENCE

Jan. 1978 504 p refs Conf. held at Boston, 4-5 Nov. 1969

(NASA-CP-007) Avail: NTIS HC A22/MF A01 CSCL 12B

AIRCRAFT CONTROL, COMMAND AND CONTROL, FLIGHT

CONTROL

N79-15887"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

HUMAN NEUROLOGICAL DEVELOPMENT: PAST, PRESENT

AND FUTURE

R PELLIGRA, ed. Nov. t978 60 p refs Symp. held at

Moffett Field, Calif., 18 May 1978; sponsored in part by Inst. for

the Achievement of Human Potential, Philadelphia, Pa. Original

contains color illustrations

(NASA-CP-2063; A-7630) Avail: NTIS HC A04/MF A01 CSCL

06P

BIOLOGICAL EVOLUTION, CHILDREN, CLINICAL MEDICINE,

CONFERENCES, LIFE SUPPORT SYSTEMS, NEUROLOGY,

THERAPY

N80-20003"# National Aeronautics and Space Administration.

Ames Research Cenler, Moffett Field, Catif.

CONFERENCE OF REMOTE SENSING EDUCATORS

(CORSE-78)

Washington Mar. 1978 664 p refs Conf. held at Stanford,

Calif., 26-30 Jun. 1978

(NASA-CP-2102; A-7755) Avail: NTIS HC A99/MF A01 CSCL

051

COMPUTER ASSISTED INSTRUCTION, CONFERENCES,

DATA PROCESSING, EDUCATION, IMAGE PROCESSING,

PHOTOGRAMMETRY, TECHNOLOGY TRANSFER

212

N81-12978"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, Ohio.

IMPACT FOR THE 80'S: PROCEEDINGS OF A CONFERENCE

ON SELECTED TECHNOLOGY FOR BUSINESS AND

INDUSTRY

Nov. 1980 238 p Conf. held in Cleveland, 14-15 May 1980

(NASA-CP-2149; E-489) Avail: NTIS HC A11/MF A01 CSCL

05A

CONFERENCES, ELECTRIC HYBRID VEHICLES, ELECTRIC

MOTOR VEHICLES, ENERGY TECHNOLOGY, PROPULSION

SYSTEM PERFORMANCE

N81-14944"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, Ala.

SPACE PLASMA PHYSICS ACTIVE EXPERIMENTS

W. T. ROBERTS, ed. Oct. 1980 239 p refs Presented at

first meeting of the Spacelab Space Plasma Phys Expt. Working

Group, Marshall Flight Center, Ata., 23-24 Sep. 1980

(NASA-CP-2165) Avail: NTIS HC A11/MF A01 CSCL 201

CONFERENCES, EXPERIMENT DESIGN, PLASMAS

(PHYSICS), SPACE PLASMAS, SPACEBORNE EXPERIMENTS,

SPACELAB PAYLOADS

N81-16973"# National Aeronautics and Space Administration,

Washington, D.C.

ASTRONAUTICS AND AERONAUTICS, 1975. A

CHRONOLOGY

N. L. BRUN and E. H. RITCHIE 1979 331 p

(NASA-SP-4020; LC-65-60308) Avail: NTIS MF A01; SOD HC

$7.00 CSCL 05D

The major NASA launches are presented including the sounding

rocket launches. Also included are the satellites, space probes,

and manned space flights for the year. TM.

N81-21995"# National Aeronautics and Space Administration,

Washington, D.C.

A CATALOG OF NASA SPECIAL PUBLICATIONS

1981 110 p

(NASA-SP-449) Avail: NTIS HC A06/MF A01 CSCL 05B

A list of all of the special publications released by NASA are

presented. The list includes scientific and technical books covering

a wide variety of topics, including much of the agencies research

and development work, its full range of space exploration programs,

its work in advancing aeronautics technology, and many associated

historical and managerial efforts. A total of 1200 titles are

presented. R.CT.

N84-25602"# National Aeronautics and Space Administration,

Washington, D.C.

ASTRONAUTICS AND AERONAUTICS, 1976. A

CHRONOLOGY

E H RITCHtE 1984 392 p

(NASA-SP-4021; NAS 1.21:4021) Avail: NTIS HC A17/MF A01

CSCL 05D

A chronology of events concerning astronautics and aeronautics

for the year 1976 is presented. Some of the many and varied

topics include the aerospace industry, planetary exploration, space

transportation system, defense department programs, politics, and

aerospace medicine. The entries are organized by the month and

presented in a news release format. MA.C.

N85-35142"# National Aeronautics and Space Administration,

Washington, D.C.

A SPACEFARING PEOPLE: PERSPECTIVES ON EARLY

SPACEFLIGHT

A. ROLAND 1985 158 p refs Proc. of a Conf. on the

History of Space Activity, New Haven, Conn., 6-7 Feb. 1981 Its

the NASA History Series

(NASA-SP-4405; NAS 1.12/6:4405; LC-84-979) Avail: NTIS HC

A08/MF A01; also available SOD HC $3.50 as 033-000-009-33-0

CSCL 22A

The early years of space flight are discussed. An historical

perspective is offered. Satellites and politics, management of large
99 GENERAL

scale technology, the state of the literature of space, the domestic

and international ramifications of space activity, and rationales for

space exploration are discussed. For individual titles see N85-35143

through N85-35150.

N86-16185"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, Calif.

SEARCHING THE HORIZON: A HISTORY OF AMES RESEARCH

CENTER, 1940-1976

E, A. MUENGER 1985 314 p refs

(NASA-SP-4304; NAS 1.21:4304) Avail: NTIS MF A01; SOD HC

$13.00 as 033-000-0096-6 CSCL 05D

A history of the Ames Research Center from 1940 to 1976 is

presented. The evolution and some of the facility's

accomplishments are recounted. GL.C.

N86-31524"# National Aeronautics and Space Administration,

Washington, D.C.

ASTRONAUTICS AND AERONAUTICS, 1977: A CHRONOLOGY

E. H. RITCHIE 1986 323 p

(NASA-SP-4022; NAS 1.21:4022) Avail: NTIS HC A14/MF A01

CSCL 05D

This publication is a chronology of events during the year 1977

in the fields of aeronautical and space research, development,

activity, and policy. It includes appendixes, an index, and

illustrations. Chronological entries list sources for further inquiry.

Author

213

NASAScientificandTechnical Publications

TypicalSubjectIndexListing

SUBJECT INDEX

1977-1986

I SUBJECT ]

1 ACCOMMODATION

d1__EMagn_tude of visual accommodahon to a head up

isplay n - I I

ASA-TP 179_1 _ NAS_A_ ,3 N81 771

1 I

I I I _uMBER I

The Sublect heading _s a key to the Sublect content

of the document. The title is used to provide a

descnpt=on of the subject matter When the title _s

insufficiently descriptive of the document content,

the title extension is added, separated from the Idle

by three hyphens The {NASA or AIAA) accession

number and the page number are included in each

entry to assist the user in locating the abstract m

the abstract section, If applicable, a repod number

=s also included as an aid _n _dentifylng the

document. Under any one subiect heading, the

access=on numbers are arranged =n sequence with

the AIAA access=on numbers appeanng hrst

A

A STARS

The A-stars: Problems and perspectives. Monograph

series on nonthermal phenomena in stellar atmospheres

[NASA-SP-4631 p 204 N83-32693

ABERRATION

Performance analysis of grazing incidence imaging

systems --- X ray telescope aberrations

{NASA-TP-10881 p 193 N78-11812

ABLATION

An abrasion-ablation model description of galactic

heavy-ion fragmentation

{NASA-TP-23051 p t92 N84-22396

A T-matrix theory of galactic heavy-ion fragmentation

[NASA-TP-2363} p 193 N85-t7690

ABLATIVE MATERIALS

Hydrogen film cooling of a small hydrogen-oxygen thrust

chamber and its effect on erosion rates of various ablative

materials

{NASA-TP-1098} p 76 N78-13124

ABRASION

Friction and wear with a single-crystal abrasive grit of

silicon carbide in contact with iron base binary alloys in

oit: Effects of alloying element and its content

[NASA-TP-1394] p 120 N79-17227

An abrasion-ablation model description of galactic

heavy-ion fragmentation

[NASA-TP-2305} p 192 N84-22396

A T-matrix theory of galactic heavy-ion fragmentation

INASA-TP-2363] p 193 N85-17690

Abrasion behavior of aluminum and composite skin

coupons, stiffened skins and stiffened panels

representative of transport airplane structures

[NASA-TP-2520] p 38 N86-13316

ABSORBERS (MATERIALS)

Mean excitation energies for stopping powers in various

materials using local plasma oscillator strengths

INASA-TP-2271 ] p 210 N84-21485

ABSORPTANCE

Comparative accuracy of the AIbedo, transmission and

absorption for selected radiative transfer approximations

INASA-RP-1160] p 156 N86-22022

ABSORPTION

Measurements of spectral attenuation coefficients in the

lower Chesapeake Bay

[NASA-TP-2130J p 168 N83-24133

ABSORPTION CROSS SECTIONS

The optical absorption of triatomic carbon C3 for the

wavelength range 260 to 560 nm

INASA-TP-1141] p 191 N78-20927

Heavy-ion total and absorption cross sections above

25 MeV/nucteon

{NASA-TP-21381 p 192 N83-23140

Tables of nuclear cross sections for galactic cosmic rays:

Absorption cross sections

{NASA-RP-t134J p 193 N85-27665

ABSORPTION SPECTRA

Emittance and absorptance of NASA ceramic thermal

barrier coating system --- for turbine cooling

{NASA-TP-t 1901 p43 N78-26148

Atlas of absorption lines from 0 to 17 900 cm(-1)

[NASA-RP-1084] p 192 N82-15853

Visible absorbance spectra: A basis for in situ and

passive remote sensing of phytoplankton concentration

and community composition

[NASA-TP-2094J p 168 N83-19411

ABSORPTIVITY

Measurements of spectral attenuation coefficients in the

lower Chesapeake Bay

INASA-TP-21301 p 168 N83-24133

Intensity and absorbed-power distribution in a cylindrical

solar-pumped dye laser

INASA-TP-23211 p 118 N84-23878

ABSTRACTS

Second International Colloquium on Mars: Abstracts

for a colloquium --- bibliography

[NASA-CP-2072J p 205 N79-t6757

NASA Space Biology Program Eighth annual

sympos_um's ,roqram and abstracts

{ NASA-CP-2299 J p 16g N84-18829

Bibliography of Supersonic Cruise Research (SCR)

program from 1980 to 1983

[NASA-RP-1117 ] p 24 N84-27674

ACCELERATED LIFE TESTS

Capacitor Technologies, Applications and Reliability

INASA-CP-2186t p 102 N81-26372

ACCELERATION (PHYSICS)

The effects of motion and g-seat cues on pilot simulator

performance of three piloting tasks

INASA-TP-1601 } p 34 N80-15069

Effects of motion base and g-seat cueing of simulator

pilot performance

INASA-TP-2247 t p 37 N84-18189

Recovery of pyroshock data from distorted acceleration

records

INASA-TP-24941 p 75 N85-31141

Compressible, unsteady lifting-surface theory for a

helicopter rotor in forward flight

INASA-TP-2503} p 27 N86-18289

ACCELEROMETERS

An active nutation damper for spacecraft

[NASA-TP-1108] p 65 N78-t5143

ACCEPTABILITY

Implications of fuel-efficient vehicles on ride quality and

passenger acceptance: Workshop proceedings

[NASA-CP-20961 p 199 N80-18990

ACCIDENT INVESTIGATION

Controls, Displays, and Information Transfer for General

Aviation IFR Operations

{NASA-CP-2279} p 4 N84 12029

ACCOMMODATION

Magnitude of visual accommodation to a head-up

display

[NASA-TP-17_6] p 173 N81-17711

ACCUMULATORS

Efficiency enhancement of octave-bandwidth traveling

wave tubes by use of multistage depressed collectors

[NASA-TP-t416] p 101 N79-17139

Efficiency enhancement of dual-mode 1raveling wave

tubes at saturation and in the linear range by use of

spent-beam refocusing and multistage depressed

collectors

[NASA-TP-1486] p 101 N79-28420

Performance of computer-designed small-sized

four-stage depressed collector for operation of dual-mode

traveling wave tube

INASA-TP-18321 p 102 N81-30360

Expenmental verification of the multistage depressed

collector design procedure for a high-perveance,

helix-type, traveling-wave tube --- in communications

satellites

i NASA-TP-2162i p 102 N83-25985

Performance of computer-designed small-size

multistage depressed collectors for a high-perveance

traveling wave tube

I NASA-TP-22481 p t02 N84-15394

Secondary electron emission characteristics of

iomtextured copper and high-purdy isotropic graphite

surfaces

i NASA-TP-2342] p 95 N84-28989

Secondary-electron-emission losses in multistage

depressed collectors and traveling-wave-tube efficiency

improvements with carbon collector electrode surfaces

I NASA-TP-2622] p 103 N86-32629

ACCURACY

The theory and practice of estimating the accuracy of

dynamic flight-determined coefficients

I NASA-RP-10771 p 183 N81-27865

The window ol visibility: A psychological theory of fidelity

in time sampled visual motion displays

I NASA-TP 2211 I p 172 N83-33538

Sile selection and directional models of deserts used

for ERBE validahon targets

I NASA-TP-25401 p 167 N86-23160

ACEE PROGRAM

Advanced aerodynamics_ Selected NASA research

I NASA-CP-2208 J p 4 N84-27660

ACEE Composite Structures Technology: Review of

selected NASA research on composite materials and

structures

I NASA-CP-2321 ] p 83 N84-29969

ACID RAIN

Analytic model lor washout of HCI(g) from dispersing

rocket exhaust clouds

INASA-TP-1801 I p 149 N81-24601

ACIDS

Ouantitahve mapping by remote sensing of an ocean

acid-waste dump

[NASA-TP-1275} p 147 N78-33617

ACOUSTIC ATrENUATION

Evaluation of approximate methods for the prediction

of noise shielding by airframe components

[ NASA-TP-1004 ] p 46 N80-15129

Experimcnfa_ evaluation of a spinning-mode

acoustic-treatment design concept for aircraft inlets ---

suppression of YF-f 02 engine fan noise

] NASA [P 16131 p 46 N80-21323

A study o( resonanl-cavity and fiberglass-filled parallel

baffles as duct silencers --- for wind tunnels

iNASA-fP-1970] p 188 N82-24052

ACOUSTIC DUCTS

Finite-d#ference theory for sound propagation in a lined

duct wllh uniform flow using the wave envelope concept

I NASA-TP-IO01} p 185 N77-30908

interaction of a turbulent-jel noise source with transverse

modes in a rectangular duct

INASA-TP-t248] p 1 N78-25049

Circumlerentially segmented ducl lines optimized for

ax_symmetric and standing wave sources --- reducing noise

from turbofan engines galerkin method acoustic

attenuation

{NASA-TP-20751 p 188 N82-34190

A new method lor determining acoustic-liner admittance

in a rectangular duct with grazing flow from experimental

dala

I NASA TP 2310] p 190 N84-27543

A method for delermining acoustic-liner admittance in

ducts with sheared flow in two-cross-sechonal directions

INASATP25t81 p 190 N86-13056

A-1
ACOUSTIC EMISSION SUBJECT INDEX

ACOUSTIC EMISSION

Analytical Ultrasonics in Materials Research and

Testing

[NASA.CP.2383] p 126 N86-22962

ACOUSTIC EXCITATION

Pressure probe and hot-film probe rsponses to acoustic

excitation in mean flow

[NASA-TP-258f] p 191 N86-27043

ACOUSTIC IMPEDANCE

A theory for predicting boundary impedance and

resonance frequencies of slotted-wall wind tunnels,

including plenum effects

INASA-TP-t880] p 17 N81-29096

A method for determining ecoustic-liner admittance in

ducts with sheared flow in two-cross-sectional directions

[NASA-TP-2518] p 190 N86-13056

ACOUSTIC MEASUREMENT

Acoustic performance of two t 83-meter-diameter fans

designed for • wind-tunnel drive system

[NASA-TP-1008J p 185 N77-30909

Forward acoustic performance of a shock-swallowing

high-tip-speed fan (QF-13)

[NASA-TP-1668] p 187 N80-23100

A new measurement method for separating airborne and

structureborne noise radiated by aircraft type panels

[NASA-TP-2079] p 189 N83-11838

A new method for determining acoustic-liner admittance

in a rectangular duct with grazing flow from experimental

data

[NASA-TP-2310J p 190 N84-27543

Low-frequency sound absorption measurements in air

[NASA-RP-1128] p 190 N85-1t789

Correlation of predicted and measured sonic boom

characteristics from the reentry of STS-1 orbiter

[NASA-TP-2475] p 190 N85-29694

A method for determimng acoustic-liner admittance in

ducts with sheared flow in two-cross-sectional directions

[NASA-TP-2518] p 190 N86-13056

Location of noise sources using a phase-slope

method

[NASA-TP-2505] p 191 N86-t604t

Pressure probe and hot-film probe rsponsos to acoustic

excitation in mean flow

{NASA-TP-2581 I p 191 N86-27043

Directwity and trends of noise generated by a propeller

in a wake

[NASA-TP-26Og] p 191 N86-31341

ACOUSTIC PROPERTIES

Effect of design changes on aerodynamic and acoustic

performance of translating-centerbody sonic inlets

[ NASA-TP-t 132] p7 N78-17998

Powered-Lift Aerodynamics and ACOUStics ---

conferences

[NASA-SP-406] p 8 N78-24046

Preliminary vibration, acoustic, and shock design and

test criteria for components on the Lightweight External

Tank (LWT)

INASA-RP-10741 p 71 N91-19218

Vibration, acoustic, and shock design end test criteria

for components on the Solid Rocket Boosters (SRB],

Lightweight External Tank (LWT), end Space Shutt}e Main

Engines [SSME)

[NASA.RP.1127I p 134 N85.10405

Acoustic treatment of the NASA Langley 4- by 7-meter

tunnel: A feasibilit7 study

[NASA-TP-2563] p 191 N86-31337

ACOUSTIC SIMULATION

Laboratory study of annoyance to combined airplane

and road-fraffic noise

[NASA-TP-1478J p 148 N79-32743

ACOUSTIC VELOCITY

Thermodynamic properties of nitrogen gas derived from

measurements of sound speed -.. for cryogenic wind

tunnels

[NASA-RP-t051] p 97 N90.14257

Charts for determining potential minimum sonic-boom

overprassures for supersonic cruise aircraft

{NASA-TP-1820] p 17 N81-21016

Sound speed measurements in liquid oxygen-liquid

nitrogen mixtures

[NASA-TP-24641 p 98 N85-35307

ACOUSTICS

Advances in engineering science, volume 3

{NASA-CP-2001-VOL-3] p 98 N77-10305

Overall loudness of steady sounds according to theory

end experiment

[NASA-RP-tO01 J p 171 N79-25753

Application of coherence in fen noise studies

[NASA-TP-1630J p 187 N80-18882

The 1980 Aircraff Safeb/ and Operating Problems, pe.rt

2

[NASA-CP-2170-PT-2] p 29 N81-19056

Application o! a computerized vibroacoustic data bank

for random v_bration criteria development

[NASA-TP-1998] p 73 N82-20238

Investigation of effects of microphone position and

orientation on near-ground noise measurements

[NASA-TP-2004} p 189 N84-10913

Numerical Techniques in Acoustics

[NASA-CP-2404] p 190 N86-12007

ACTIVE CONTROL

Advanced aerodynamics and active controls. Selected

NASA research

[NASA-CP-2172] p 3 N81-19001

Comparison of analytical end wind-tunnel results for

flutter end gust response of a transport wing with active

controls

[NASA-TP-2010] p 131 N82-26703

Validation of an Active Gear, Flexible Aircraft Take-oft

and Landing analysis (AGFATL)

[NASA-TP-2353] p 37 N84-32378

ACTUATOR DISKS

Analysis of supersonic stall bending flutter in axial-flow

compressor by actuator disk theory

[NASA-TP-t3451 p 10 N79.13003

ACTUATORS

Single-stage electrOhydraulic servosystem for actuating

on airflow valve with frequencies to 500 hertz

[NASA-TP-1678} p 56 N80.29369

Analysis and simulation of a magnetic bearing

suspension system for a laborstor7 model annular

momentum control device

[NASA-TP-1799] p 99 N81-20311

The 15th Aerospace Mechanisms Symposium

[NASA-CP-2181] p 130 N81-22388

The 16th Aerospace Mechanisms Symposium

[NASA-CP-2221] p 99 N82-23344

The 17th Aerospace Mechanisms Symposium

[NASA-CP-2273] p 131 N83-24881

ADAPTATION

Space Physiology and Medicine

[NASA.SP-447] p 170 N83.25349

ADAPTIVE CONTROL

Propulsion Controls, 1979 --- air breathing engine

control

[NASA-CP-2137] p 47 N81-12090

Adaptive _entification and control of structural dynamics

systems using recursive lattice filters

[ NASA-TP-2371 ] p 75 N85-31142

ADAPTIVE FILTERS

Evaluation of a total energy-rate sensor on a transport

airplane

[NASA-TP-2212] p 40 N84.12164

ADDITIVES

Effectiveness of various organometallics as antiwear

additives in mineral oil

{NASA-TP-10961 p 91 N78-12222

Ionized dopant concentrations at the heavily doped

surface of a silicon solar cell

[NASA.TP-1347] p 195 N7g-13886

Evaluation and auger analysis of a

zinc-dialkyl-dithiophosphate antiwear additNe in several

diester lubricants

[NASA-TP-1544] p 93 N79-3235g

Effect of Yttria additives on properties of

pressuretess-sintered silicon nitdde

[NASA-TP-1899] p 94 N81-31366

Effect of aluminum phosphate additions on composition

of three-component plasma-sprayed solid lubricant

[NASA.TP.1990] p 88 N82-21298

Effect of lubricant extreme-pressure additives on surface

fatigue life of AISI 9310 spur gears

[NASA-TP-2408] p 124 N85-13234

Effect of five lubricenta on life of AISI 9310 spur gears

[NASA-TP-24191 p 116 N85.t60gg

Current evaluation of the tripropsilant concept

[NASA.TP.2602] p 78 N86-28124

ADHESION

Role of alloying elements in adhealve transfer and friction

of copper-base alloys

[NASA-TP-1256] p 86 N78-26198

Effect of nitrogen-containing plasma on adherence,

friction, and wear of radiofrequency-sputtered titanium

carbide coatings

[NASA-TP-1377] p 92 N79-15184

Improved adherence of sputtered titanium carbide

coatings on nickel, and titanium.base alloys

[NASA-TP-1450] p 78 N79-22194

Adhesion and friction of iron-base binary alloys in contact

with silicon carbide in vacuum

[NASA-TP-1604J p 87 N80-15234

Wear mechanism based on adhesion

[NASA-TP-2037] p 122 N82-32737

TriboIogy in the 80's. Volume 2: Sessions 5 - 8

{ NASA-CP-2300-VOL-2] p 124 N84-25047

Adhesion between polymers and evaporated gold and

nickel films

[NASA-TP-2360] p 96 N84-31379

Humidity effects on adhesion of nickel-zinc ferrile in

elastic contact with magnetic tape and itself

{NASA-TP-2449} p 96 N85-21359

Monte Carlo lattice models for adsorbed polymer

conformation

{NASA-TP-2453] p 195 N85-24961

ADHESION TESTS

Adhesion between polymers and evaporated gold and

nickel films

[NASA-TP-2360] p 96 N84-31379

ADHESIVE BONDING

Graphite/Polyimide Composites --- conference on

Composites for Advanced Space Transportation

Systems

[NASA-CP-2079J p 80 N79-30297

TriboIogy in the 80's Volume 1: Sessions 1 to 4

[NASA-CP-2300-VOL-1 ] p 124 N84-23891

Effect of preforming sdherends on static and fatigue

strength of bonded composite single-lap joints

[NASA-TP-2324] p 133 N84-26053

A cracked orthotropic sheet stiffened by a semi-infinite

orthotrop_c sheet

[NASA-TP-2455] p 134 N85-32339

ADHESIVES

Graphite/Polyimide Composites --- conference on

Composdes for Advanced Space Transportation

Systems

[NASA-CP-2079] p 80 N79-30297

High Temperature Polymer Matrix Composites

[NASA-CP-2385] p 83 N86-t1260

ADSORPTION

Adsorption and chemical reaction of gaseous mixtures

of hydrogen chloride and water on aluminum oxide and

application to solid-propellant rocket exhaust clouds

[NASA-TP-1105] p 84 N78-22188

AERIAL PHOTOGRAPHY

High altitude perspective --- cost-reimbursable services

using NASA U-2 aircraft

[NASA-SP-427] p 138 N78-31508

AERIAL RECONNAISSANCE

Applications systems verification and transfer project.

Volume 3: Operational applications of satellite snow cover

observations in California

{NASA-TP-1824] p 140 N82-20619

Applications systems veritication end transfer prolect.

Volume 4: Operational applications of satellite snow cover

observations. Colorado Field Test Center

[NASA.TP.1825] p 140 N82-20620

Applications systems verification and transfer project.

Volume 5: Operational applications of satellite snow-cover

observations, northwest United States

[NASA-TP-f826] p 140 N82-20621

Applications systems verification and transfer project.

Volume 7: Cost/benefit analysis for the ASVT on

operational applications of satellite snow-cover

observations

[NASA-TP-1828] p 141 N82-20623

Earth resources: A continuing bibliography with indexes,

issue 50

[NASA-SP-7041(50)J p 143 N86-31940

AEROACOUSTICS

An experimental evaluation of the application of the

Kirchhoff formulation for sound radiation from an oscillating

airfoil

[NASA.TP-1048] p 186 N7S-f2801

Powered-Lift Aerodynamics and Acoustics ---

conferences

[NASA-SP-406] p 8 N78-24046

Helicopter Acoustics

[NASA-CP-2052-PT-1] p 186 N78-32816

Helicopter Acoustics, part 2 --- conferences

[NASA.CP-2052.PT.2] p 186 N79-10843

Evaluation of a vortex model of turbulent cavity flow

--- for computing noise generation of fluid flow

[NASA.TP.1505] p 187 N79.32057

Experimental study of acoustic loads on an

upper.surface.blown STOL airplane configuration ---

Langley full-scale wind tunnel teats

INASA-TP-1577] p 187 N80-t387g

Airframe noise of a small model transport aircraft and

scaling effects --- Boeing 747

[NASA.TP.1858] p 188 N81-22832

Stochastic analysis of spectral broadening by a free

turbulent shear layer

[NASA-TP-1916] p 188 N81-24854

Aeroecoustic performance of an externally blown flap

configuration with several flap noise suppression devices

INASA-TP-1995] p 188 N82-24942

Investigation of jet-installation noise sources under static

conditions

INASA-TP-2181 I p 189 N83-33684

A new method for determining acoustic-liner admittance

in a rectangular duct with grazing flow from experimental

data

[NASA-TP-2310] p 190 N84.27543

Acoustic treatment of the NASA Langley 4- by 7-meter

tunnel: A feasibility study

{NASA-TP-2563J p 191 N86-31337

A-2
SUBJECT INDEX AERODYNAMIC CHARACTERISTICS

AEROASSIST

O'I-V Propulsion _ssues

[NASA-CP-2347] p 67 N85-16989

AERODYNAMIC CHARACTERISTICS

Theoretical parametric study of the relative advantages

of wiogiats and wiog-tip extensions

[NASA.TP-t020] p 5 N77-33112

Effect of coolant flow ejection on aerodynamic

performance of low-aspect-ratio vanes. 2: Performance

with coolant flow election at temperature ratios up to 2

[NASA-TP-1057] p6 N78-11008

Aerodynamic characteristics at Mach numbers from 0.33

to 1.20 of a wing-body design concept for a hypersonic

research airplane

[NASA-TP-1044] p 6 N78-12038

Supersonic aerodynamic characteristics of a Sparrow

3 type missile model with wing controls and comparison

with existing tail-control results

[NASA-TP-t078] p 6 N78-12041

Effects of roughness size on the position of

boundary-layer transition and on the aerodynamic

characteristics of a 55 deg. swept delta wing at supersonic

speeds

[NASA-TP-1027] p 7 N78-13016

Longitudinal aerodynamic characteristics at Mach 060

to 2,86 of a fighter configuration with strut braced wing

[NASA-TP-1102J p 7 N78-16000

Effect of cooling-hole geometry on aerodynamic

performance of a film-cooled turbine vane tested with cold

air in a two-dimensional cascade

[NASA-TP-1136] p 8 N78-20080

Effect of winglets on a first-generation jet transport wing

5: Stability characteristics of a full-span wing with a

generalized fuselage at high subsonic speeds

[NASA-TP-t 163 ] p8 N78-20081

Two-dimensional cold-air cascade study of a film-cooled

turbine stator blade. 4: Comparison of experimental and

analytical aerodynamic results for blade with 12 rows of

0.076-centimeter-(0.030-inch-) diameter holes having

streemwise ejection angles

[NASA-TP-1151 ] p 42 N78-20130

Two-dimensional cold-air cascade study of a film-cooled

turbine stator blade. 5: Comparison of experimental and

analytical aerodynamic results for blade with 12 rows of

0.038-centimeter-{0.015 inch) diameter coolant holes

having streamwise ejection angles

[NASA-TP-1204] p 42 N78-20133

Effects of stores on longitudinal aerodynamic

characteristics of s fighter at supersonic speeds

[NASA-TP-1175] p 8 N78-22028

Powered-Liff Aerodynamics and Acoustics ---

conferences

[NASA-SP-406] p 8 N78-24046

Aerodynamic characteristios at Mech number 0.2 of a

wing-body concept for a hypersonic research airplane

[NASA-TP-1189] p 8 N78.25059

Effects of specwise nozzle geometry and location on

the longitudinal aerodynamic characteristics of a

vectored-engine-over-wing configuration at subsonic

speeds

[NASA-TP-1215] p8 N78-25060

Preliminary study of a large span-distributed.load

flying.wing cargo airplane concept

[NASA.TP.1158) p 32 N78.2507g

Longitudinal aerodynamic characteristics of a fighter

model wifh a close-coupled canard at Mech numbers from

0.40 to 120

[NASA.TP.1206] p 53 N78-27136

Aerodynamic characteristics at Mech 6 of a wing-body

concept for a hypersonic research airplane

[NASA-TP-f24g] p 9 N78-30055

Theoretical estimation of the transonic aerodynamic

charactedstios of a supercrttical-wing transport model with

trailing-edge controls

[NASA-TP-1253} p g N78-30056

Aerodynamic characteristics of a hypersonic research

airplane concept having a 70 deg swept double-delta wing

at Mach number 0,2

[NASA-TP-1252] p 9 N78-31045

Aerodynamic derivatives for an oblique wing aircraft

estimated from flight data by using a maximum likelihood

technique

[NASA-TP-1336] p 10 N78-33054

Aerodynamic performance of a 1.35-pressure-ratio

axial.flow fan stage

[NASA-TP-1299] p 10 N79-10022

Effects of wing leading-edge flap deflections on subsonic

longitudinal aerodynamic characteristics of a wing-fuselage

configuration with s 44 dog swept wing

[NASA-TP-t351J p 10 N79-13002

Flight comparison of the transonic agility of the F-111A

airplane end the F-f 11 supercriticai wing airplane

[NASA-TP-1368] p 54 N79-13056

Low-speed aerodynamic characteristics of a

16-percent-thick variable-geometry airfoil designed for

general aviation applications

[NASA-TP-13241 p 10 N79-14018

Theoretical evaluation of high-speed aerodynamics for

arrow.wing configurations

[NASA.TP-1358] p 10 N79-14023

Stability and control characteristics of a monoplanar

elliptic missile model at Mach numbers from 1,60 to 286

[NASA-TP-1352] p 11 N79-17808

Space shuttle aftarbody aerodynamics/plume simulation

data summary

[NASA-TP-1384] p 11 N79-17810

Expertmental investigation of three helicopter rotor

airfoils designed analytically --- in the Langley 6 by 19

inch and 6 by 28 inch transonic wind tunnels

[NASA-TP-1396] p 11 N79-22037

Aerodynamic characteristics at Mach numbers of 1.5,

1.8, and 2.0 of s blended wing-body configuration with

and without integral canards

[NASA-TP-1427] p 12 N79-23013

Effects of wing leading-edge deflection on low-speed

aerodynamic characteristics of a low-aspect-ratio highly

swept arrow-wing configuration -- wind tunnel tests

[NASA-TP-1434] p 12 N79-26020

Performance evaluation method for dissimilar aircraft

designs --- using the square of the wing span for

nondimensional comparisons of aerodynamic

characteristics

[NASA-RP-f042] p 2 N79-30139

Theoretical and experimental investigation of

ground-induced effects for a low-aspect-ratio highly swept

arrow-wing configuration

[NASA-TP-1508] p 54 N79-31223

Longitudinal aerodynamic characteristics of a

vectored-engine-over-wing configuration at subsonic

speeds -- Langley V/STOL tunnel tests

[NASA-TP-1533] p 12 N79-33164

Wind-tunnel/flight correlation study of aerodynamic

characteristics of a large flexible supersonic cruise airplane

CXB-70-f). 1: Wind-tunnel tests of a 003-scale model

at Mach numbers from 06 to 2.53

[ NASA-TP-1514J p33 N80-11068

Aerodynamic characteristics of a hypersonic research

airplane concept having a 70 deg swept double-delta wing

at Mach numbers from 080 to 1 20. with summary of data

from 0.20 to 6.0 --- Langley 8-ff transonic wind tunnel

[NASA-TP-1552} p 13 N80-12064

Application of supersonic linear theory and hypersonic

impact methods to three nonsiander hypersonic airplane

concepts at Mech numbers from 1.10 to 2.86

[NASA-TP-1539] p 13 N80-12065

Summary of low-speed longitudinal aerodynamics of two

powered close-coupled wing-canard fighter configurations

--- conducted in Langley C/STOL tunnel

[NASA-TP-1535] p 13 N80-12994

Effects of fuselage forebody geometry on low-speed

lateral-directional characteristics of twin-tai_ fighter model

at high angles of attack

[NASA-TP-1592] p 13 N80-13002

Effects of relaxed static longitudinal stability on a

single-stage-to.orbit vehicle design

[NASA-TP-1594] p 55 N80-13052

Wind-tunnel/flight correlation study of aerodynamic

characteristics of • large flexible supersonic cruise airplane

(XB-701) 2; Extrapolation of wind-tunnel data to full.scale

conditions

[NASA-TP-1515] p 13 N80-16032

Prediction method for two-dimensional aerodynamic

losses of cooled vanes using integral boundary-layer

parameters

[NASA-TP-1823] p 14 N80-17030

Comparison of analytical and flight test identified

aerodynamic derivatives for • tandem-rotor transport

helicopter

[NASA-TP-1581] p 34 N80-17060

An experimental investigation of two large annular

diffusers with swirling and distorted inflow

[NASA-TP-1828] p 14 N80-17984

Wind-tunnel/flight correlation study of aerodynamic

characteristics of a large flexible supersonic cruise airplane

(XB-70.1). 3: A comparison between characteristics

predicted from wind-tunnel measurements and those

measured in flight

[NASA-TP-1516] p 14 N80-17986

Supersonic wings with significant leading-edge thrust at

cruise

[NASA-TP-1632] p 14 N80-2127g

Aerodynamic performances of three fan stator designs

operating with rotor having tip speed of 337 meters per

second and pressure ratio of 154 Relation of analytical

code calculations to experimental performance

[NASA-TP-1614] p 46 N80-21324

Forward acoustic performance of a shock-swallowing

high-tip-speed fen (QF-13)

[NASA.TP-1668] p 187 N80-23100

investigation of axisymmetric and nonaxisymmetric

nozzles installed on • O, 10 scale F-18 prototype airplane

model --- wind tunnel tests

{NASA-TP-1638] p 15 N80-24267

Aerodynamic characteristics of three helicopter rotor

airfoil sections at Reynolds number from model scale to

futl scale at Mach numbers from 0.35 to 0.90 --- conducted

in Langley 6 by 28 inch transonic tunnel

{NASA-TP-1701 ] p 15 N80-32333

Estimation of wing nonlinear aerodynamic

characteristics at supersonic speeds

[NASA-TP-1718] p 15 N81-10004

Low-speed aerodynamic performance of

508-centimeter-diameter noise-suppressing inlets for the

Quiet, Clean. Short-haul Experimental Engine (OCSEE] ---

Lewis 9- by 15-foot low speed wind tunnel tests

[NASA-TP-11781 p 47 N81-11037

Pseudosteady-state analysis of nonlinear aircraft

maneuvers

INASA-TP-1758] p 56 N81-13065

Aeropropulaive characteristics of twin nonaxisymmethc

vectoring nozzles installed with forward-swept and

aft-swept wings --- in the Langley 16 Foot Transonic

Tunnel

[NASA-TP-1778] p 16 N81-19019

Reasons for low aerodynamic performance of

13.5-centimeter-tip-diameter aircraft engine starter

turbine

{NASA-TP-1810] p 48 N81-20076

Experimental and analytical study of the longitudinal

aerodynamic characteristics of analytically end empirically

designed Strake-wing configurations at subcritical

speeds

[NASA-TP-1803] p 17 N81-25040

Aerodynamic tests and analysis of a turbojet-boosted

launch vehicle concept (spacejet) over a Mach number

range of t 50 to 2.86 --- Langley Unitary Plan Wind Tunnel

Tests

{ NASA-TP- 1888 ] p 17 N81-29098

Wing-alone aerodynamic characteristics for high angles

of attack of supersonic speeds

[NASA-TP-18891 p 18 N81-30087

Cornering characteristics of the nose-gear tire of the

space shuttle orbiter

[NASA-TP-t917J p 130 N82-10430

Effects of vortex flaps on the low-speed aerodynamic

characteristics of an arrow wing

[NASA-TP-1914] p 3 N82-11013

Force and moment, flow-visualization, and

boundary-layer tests on e shuttle orbiter model at Mach

6

[NASA-TP-1952] p 18 N82-13106

Computer program for aerodynamic and biading design

of multistage axial-flow compressors

INASA-TP-1946] p 49 N82-15039

Effects of wing-leading-edge modifications on a

full.scale, low-wing general aviation airplane: Wind-tunnel

investigation of high-angle-of.attack aerodynamic

characteristics --- conducted in Langley 30- by 60-feot

tunnel

{NASA-TP-20t 1] p 4 N82-26217

Longitudinal aerodynamic characteristics of an elliptical

body with a horizontal tail at Mech numbers from 2,3 to

463

[NASA-TP.2024] p 19 N82-26232

Laser anemometer measurements in an annular

cascade of core turbine vanes and comparison with

theory

[NASA.TP.2018] p 20 N82.26234

Low-speed aerodynimic characteristics of a

17-percent-thick medium speed airfoil designed for general

aviation applications

[NASA-TP-1786] p 20 N83-16290

Aerodynamic effect of • honeycomb rotor tip shroud

on a 508-centimeter-tip-diameter core turbine

[NASA.TP.2112] p4g N83.17547

A common geometric data-base approach for

computer.aided manufacturing of wind-tunnel models and

theoretical aerodynamic analysis

[NASA-TP-21511 p 21 N83.22166

Effects of twin-vertical-tail parameters on twJn-eogine

aflerbody/nozzle aerodynamic characteristics --- Langley

16-ff transonic tunnel tests

[NASA-TP-2158J p 21 N83-24478

Effect of empennage location on twin-engine

afterbody-nozzle aerodynamic characteristics at Mech

Numbers from 0,6 to 1,2 --- wind tunnel tests

INASA-TP-2116} p 21 N83-25666

Low-speed aerodynamic performance of an

aspect-ratio.t0 supercritical-wing transport model

equipped with • full-span slat and part-span and full-span

double.sloffod flaps

[NASA-TP-1805] p 21 N83-30390

A-3
AERODYNAMIC COEFFICIENTS SUBJECT INDEX

Well-tempereture effects on the aerodynamics of a

hydrogen-fueled transport concept in Mach 8 blowdown

and shock tunnels

NASA-TP-2159] p 21 N83-30391

Theoretical and experimental investigation of supersonic

aerodynamic characteristics of a twin-fuselage concept

NASA-TP-2184] p 22 N83-32776

Aerodynamic cherectenstics of a series of bodies with

variations in nose camber

NASA-TP-2206J p 22 N83-34904

Breking and cornering studies on an air cushion landing

system

NASA-TP-2196] p 36 N83-34935

Low-speed aerodynamic characteristics of a highly

swept, untwisted uncambered arrow wing

NASA-TP-2176] p 22 N83-36000

Aerodynamic characteristics, including effect of body

shape, of a Msch 6 aircraft concept

NASA-TP-2235] p 22 N84-t3164

Wing planform effects at supersonic speeds for an

advanced hghter configuration

NASA-TP-2269] p 23 N84-20486

STABCAR: A program for finding charecteristic root

systems having transcendental stability matrices

NASA-TP-2165] p 179 N84-27461

Effect of fuselage upwash on the supersonic longitudinal

aerodynamtc charactenatlcs of 2 fighter configurations

NASA-TP-2330 J p 24 N84-27676

KC- 135 Winglet Program Review

JNASA-CP-2211 ] p 24 N84-27686

Two-dimensional aerodynamic characteristics of an

airfoil designed for two

[ NASA-TP-1965 } p 24 N84-27694

Two-dimensionel aerodynamtc cherecteristics of three

rotorcreff airfoils at Msch numbers from 0.35 to 0.90

[NASA-TP-2000] p 24 N84-28743

Application of the ONERA model of dynamic stall

[NASA-TP-2399] p 25 N85-t2862

Downwash in the plane of symmetry of an elliptically

loaded wing

[NASA-TP-2414] p 25 N85-15693

Effect of aerodynamic and angle.of-attack uncertainties

on the May 1979 entry flight control system of the Space

Shuttle from Msch 8 to 1.5

[NASA-TP-2365} p 69 N85-t5778

Wind-tunnel investigation of a full-scale

canard-configured general aviation airplane

INASA-TP-2382] p 25 N85-19925

Wind-tunnel evaluation of a 2t-percent-scale powered

model of a prototype advanced scout helicopter

INASA-TP-2420] p 26 N85-28923

Low-speed tests of a high-aspect-rabo,

supercritical-wing transport model equipped with a high-lit1

flap system in tfte Langley 4- by 7.meter and Ames 12-foot

pressure tunnels

[NASA-TP-2097] p 26 N85-310t0

Quest for performance: The evolution of modern

aircraft

[NASA-SP-468J p 5 N95-32089

Effect of aileron deflecbons on the aerodynamic

characteristics of a semispan model of a subsonic

energy-efficient transport

[NASA-TP-2478] p 27 N86-11186

Aerodynamic characteristics of a high-wing transport

configuration with a over-the-wing nacelle-pylon

arrangement

[NASA-TP-2497J p 27 N86-16193

Aerodynamic characteristics of severa_ current

helicopter tail boom cross sections including the effect

of spoilers

[NASA-TP-2506] p 27 N86-20349

Low-speed stability and control characteristics of a

transport model wtth aft-fuselage-mounted advanced

turboprops

[NASA-TP-2535] p 59 N86-22580

Aerodynamic characteristics of a supersonic fighter

aircraft model at Mach 0.40 to 2.47

[NASA-TP-2580) p 28 N86-23561

Effects of upper-surface nacelles on longitudinal

aerodynamic characteristics of high-wing transport

configuration

{ NASA-TP-2579J p 28 N86-23562

AERODYNAMIC COEFFICIENTS

Measured end predicted shock shapes and aerodynamic

coefficients for blunted cones at incidence in helium at

Mach 20.3

{NASA-TP-13951 p 106 N79-20345

Measured and predicted sftock shapes and aerodynamic

coefficients for blunted cones at incidence in air at Mach

5.9

INASA-TP-1652] p 108 N80-23600

Flight evaluation of stabilizabon and command

augmentation system concepts and cockpit displays during

approach and landing of powered-lift STOL aircraft

INASA-TP-t55t I p 56 N81-tt044

Determination of the

hybersonic-continuum/rarefied-tlow drag coefficient of the

Viking lander capsule 1 aeroshell from flight data

I NASA-TP-1793] p 3 N81-14961

High Reynolds number research - 1980

INASA-CP-2183] p 18 N81-31130

Determination of airplane model structure from flight data

by using modified stepwise regression

[NASA-TP-1916] p 56 N82-t0041

Wind-tunnel results for a modified 17-percent-thick

low-speed airfoil section

INASA-TP-1919] p 18 N82-t1033

Low-speed aerodynamic performance of a

high-aspect-ratio supercritical-wing transport model

equipped with full-span slat and part-span double-slotted

flaps

INASA-TP-1580] p 19 N82-15015

Flight-measured laminar boundary-layer transition

phenomena including stability theory analysis

I NASA-TP-2417 j p25 N85-21t 18

AERODYNAMIC CONFIGURATIONS

Proceedings of the SCAR Conference, part I

{ NASA-CP-001-PT-1 ] p I N77-17996

Spin-tunnel investigation of the spinning charecteristics

of typical single-engine general aviation airplane designs.

1. Low-wing model A: Effects of tail configurations

[NASA-TP-10091 p 5 N77-33111

Effect of design changes on aerodynamic and acoustic

perfOrmance of translating-cecterbody sonic inlets

[NASA-TP-1132J p 7 N78-t7998

Simplified sonic-boom prediction -- using aerodynamic

configuration charts and calculators or slide rules

[NASA-TP-1122] p 7 N78-20078

Fluctuating loads measured on an over-the-wing

supersonic jet model

INASA-TP-t366] p 186 N79-16641

An experimental and theoretical investigation of the

effect of nonmetric over-the-wing nacelles on wing-body

aerodynamics

INASA-TP-tS03J p 12 N79-29146

Performance evaluation method for dissimilar aircraft

designs --- using the square of the wing span for

nondimensional comparisons of aerodynamic

characteristics

[NASA-RP-1042] p 2 N79-30139

Performance of two-stage fan with a first-stage rotor

redesigned to account for the presence of a part-span

damper

[NASA-TP-14831 p 45 N79-30191

Leading-edge deflection optimization for a highly swept

arrow wing configuration

INASA-TP-1777} p 16 N81-14974

Solution of complex nonlinear problems by a generalized

application of the method of base and comparison

solutions with applications to aerodynamics problems

INASA-TP-1857] p 17 N81-22019

Effect of simulated in-flight thrust reversing on

vertical-tail loads of F-18 and F-15 eirplane models ---

conducted in the Langley 16-foot transonic tunnel

I NASA-TP-1890 J p 18 N81-30086

High Reynolds number research - 1980

INASA-CP-2183] p 18 N81-31130

An analytical procedure for computing smooth

transitions between two specified cross sections with

applications to blended wing body configuration

INASA-TP-2012} p 19 N82-25193

Effect of tail-fin span on stability and control

characterisbcs of a Canard-controlled missile at supersonic

Mach numbers

INASA-TP-2157] p 21 N83-2795g

Aerodynamic characteristics of a series of bodies with

variations in nose camber

I NASA-TP.2206] p 22 N83-34904

Aerodynamtc design for improved manueverabdity by

use of three-dimensional transonic theory

I NASA-TP-2282 ] p23 N84-t 8161

Aeropropulsive characteristics of

nonaxisymmetric-nozzle thrust reversers at Math numbers

from 0 to 1.20

[NASA-TP-2306] p 23 N84-2453B

Simulator study of fhght characteristics of several large,

dissimilar, cargo transport airplanes during approach and

landing

I NASA-TP-2357 ] p 58 N85-11002

Space Shuttle orbiter trimmed center-of-gravity

extension study

INASA-TP-2284J p 67 N85-19003

Parametric study of a canard-configured transport using

conceptual design optimization

INASA-TP-24001 p 37 N85-19979

Sere{analytic modeling ol aerodynamic shapes

INASA-TP-2413] p 25 N85-21120

Supersonic aerodynamic characteristics of canard,

tailless, and aft-tail configurations for 2 wing planforms

INASA TP-24341 p 26 N85-27822

Static and dynamic pressure measurements on a NACA

0012 aidoil in the Ames High Reynolds Number Facility

{NASA-TP-24851 p 26 N85-27823

Aerodynamic charectenstics of a distract wing-body

configuration at Mach 6: Experiment, theory, and the

hypersonic isolation principle

[NASA-TP-2467] p 27 N85-33107

Energy efficient transport technology: Program summary

and bibliography

[NASA-RP-t 135_ p37 N85-33116

NASA and general aviation

[NASA-SP-485] p 38 N86-30720

AERODYNAMIC DRAG

Dynamic behavior of a beam drag-force anemometer

[NASA-TP-1687] p 114 N60-24595

Determination of the

hypersonic-continuum/rarefied-flow drag coefficient of the

Viking lander capsule 1 aeroshell from flight data

[NASA-TP-17931 p 3 N81-14961

Optimization and performance calculation of

dual-rotation propellers

[NASA-TP-1948] p 3 N82-14049

Comparison of experimental and theoretical turbulence

reduction characteristics for screens, honeycomb, and

honeycomb-screen combinations

INASA-TP-1958] p 19 N82-14055

Investigation of installateon effects of single-engine

convergent-divergent nozzles

INASA-TP-2078] p 20 N83-1t059

AERODYNAMIC FORCES

Analysis of prefluffer and posffluffer characteristics with

motion-matched aerodynamic forces

lNASA-TP-1232] p 127 N78-28481

Classical aerodynamic theory

INASA-RPol050] p 13 N80-15033

An analytical techmque for approximating unsteady

aerodynamics in the time domain

INASA-TP-1738t p 130 N81-tt422

Pressures, forces, moments and shock shapes for a

geometrically matched sphere-cone and hyperboloid at

Mach 20.3 in helium --- 22-inch aerodynamics leg of the

Langley hypersonic helium tunnel facility

{NASA-TP-2100] p 110 N83-16675

Aerodynamic force measurements with a strain-gage

balance in a cryogenic wind tunnel

INASA-TP-2251 ] p 22 N84-t3162

Generalization of the subsonic kernel function in the

s-plane, with applications to flutter analysis

[NASA-TP-2292] p 23 N84-20480

AERODYNAMIC HEAT TRANSFER

Aerodynamic heating in gaps of thermal protection

system tile arrays in laminar and turbulent boundary

layers

[NASA-TP-1187] p 105 N78-28373

AERODYNAMIC HEATING

The use of computer-generated color graphic images

for transient thermal analysis --- for hypersonic aircraft

lNASA-TP-14551 p 107 N79-30518

Aerothermal performance of radiatively and actively

cooled panel at Math 66

INASA-TP-t5951 p 107 N80-t3402

Aerothermal environment in chordwise gaps between

split elevons at Mach 68

[NASA-TP-t7831 p 109 N81-15237

Aerodynamic heating on the corrugated surface of a

102 deg half-angle blunted cone at Mach 6,7

[NASA-TP-1928] p 109 N82-13383

Computational Aspects of Heat Transfer in Structures

INASA-CP-2216] p 109 N82-23473

Experimental and predicted heating distributions for

biconics at incidence in air at Msch 10

[NASA-TP-23341 p 112 N85-t2313

Aerothermal tests of a 125 percent cone at Msch 6.7

for various Reynolds numbers, angles of attack and nose

shapes --- conducted in Langley 8-fool high temperature

tunnel

INASA-TP-2345] p 112 N85-17322

AERODYNAMIC INTERFERENCE

Experiments in a three-dimensional adaptive-wail wind

tunnel

INASA-TP-2210] p 22 N83-3490£,

An experimental invesligation of nacelle-pylon

installation on an unswept wing at subsonic and fransontc

speeds

[NASA-TP-2246] p 23 N84-18162

Wind Tunnel Wall Interference Assessment and

Correction, 1983

[NASA.CP-23191 p 25 N65-t201t

Effect of underwing aft-mounted nacelles on the

longitudinal aerodynamic characterishcs of a high-wing

transport airplane

[NASA-TP-24471 p 27 N86-20345

Installation effects of long-duct pylon-mounted nacelles

on a twin-jet transport model with swept supercritical

wing

[NASA-TP-24571 p 27 N86-20346

A-4
SUBJECT INDEX AERONAUTICAL ENGINEERING

AERODYNAMIC LOADS

Dynamic stall experiments on the NACA 0012 airfoil

[NASA-TP-11001 p 7 N78-t7000

Comparison of concurrent strain gage- and pressure

transducer-measured flight loads on a lifting reentry vehicle

and correlation with wind tunnel predictions

[NASA-TP-1331} p 10 N78-33053

A modification to lineanzed theory for prediction of

pressure Ioadings on lifting surfaces at high supersonic

Mach numbers and large angles of attack

[NASA-TP-1406] p 11 N79-17806

Experimental study of acoustic loads on an

upper-surface-blown STOL airplane configuration ---

Langley full.scale wind tunnel tests

[NASA-TP-1577] p 187 N80-13879

Analytic investigation of effect of end-wail contouring

on stator performance

[NASA-TP-1943] p 19 N82-14051

System analysis approach to deriving design criteria

(loads) for Space Shuttle and its payloads• Volume 1:

General statement of approach

[NASA-TP-1949} p 66 N82-14203

A conceptual framework for using Doppler radar

acquired atmospheric data for flight simulation

{NASA-TP-21921 p 36 N83-27977

KC-135 Winglet Program Review

[NASA-CP-2211 I p 24 N84-27686

Rotorcraft Dynamics 1984

[NASA-CP-2400] p 38 N86-15280

AERODYNAMIC NOISE

Flutter Testing Techniques

{NASA-SP-415] p t N77-21022

Acoustic performance of two 1.83-metar-diameter fans

designed for a wind-tunnel drive system

[NASA-TP-1008J p 185 N77-30909

Mean velocity, turbulence intensity, and scale in a

subsonic turbulent jet impinging normal to a large flat

plate

[NASA-TP-t037] p 104 N77-32431

An experimental evaluation of the application of the

Kirchhoff formulation for sound radiation from an oscillating

airfoil

[NASA-TP-1048] p 186 N78-12801

Simulated flight effects on noise characteristics of a fan

inlet with high throat Mach number

INASA-TP-1199J p42 N78-20132

Evaluation of a vortex model of turbulent cavity flow

--- for computing noise generation of fluid flow

[NASA-TP-15051 p 187 N79-32057

Aeroacoustic performance of an externally blown flap

configuration with several flap noise suppression devices

[NASA-TP-1995J p 188 N82-24942

A new measurement method for separating airborne and

structureborne noise radiated by aircraft type panels

{NASA-TP-2079] p 189 N83-11838

Effect of low-frequency tones and

turbulent-boundary-layer noise on annoyance

[NASA-TP-2202] p 172 N83-34579

Correlations of supersonic boundary-layer transition on

cones including effects of large axial variations in

wind-tunnel noise

[ NASA-TP-22291 p t 11 N84-17534

Rotorcraft noise

[NASA-CP-2234] p 190 N84-29662

Analysis of noise measured from a propeller in a wake

[NASA-TP-2358J p 190 N85-t1788

Noise transmission loss of a rectangular plate in an

infinite baffle

INASA-TP-2398] p 190 N85-22109

Consideration of some factors affecting low-frequency

fuselage noise transmission for propeller aircraft

[NASA-TP-25521 p 191 N86-24393

Directivity and trends of noise generated by a propeller

• in a wake

[NASA-TP-2609] p 191 N86-31341

AERODYNAMIC STABILITY

Entry dynamics of space shuffle orbiter with longitudinal

stability and control uncertainties at supersonic and

hypersonic speeds

[NASA-TP-1084] p 70 N77-33259

Effects of control inputs on the estimation of stability

and control parameters of a light airplane

fNASA-TP-t043) p 53 N78-13071

Improvement of maneuver aerodynamics by spanwise

blowing

[NASA-TP-10651 p 7 N78-14997

Effect of winglets on a first-generation jet transport wing.

5: Stability charactecstics of a full-span wing with a

generalized fuselage at high subsonic speeds

[NASA-TP-11631 p 8 N78-20081

Flight evaluation of the transonic stability and control

characteristics of an airplane incorporating a supercritical

wing

[ NASA-TP-1167 J p 53 N78-20140

Determination of stability and control parameters of a

light airplane from flight data using two estimation methods

--- equation error and maximum likelihood methods

[NASA-TP-1306] p 11 N79-20071

Dynamic response of a Mach 2.5 axisymmetric inlet and

turbojet engine with a poppet*value controlled inlet stability

bypass system when subjected to internal and external

airflow transients

INASA-TP-1531 ] p 45 N80-14t23

Full-scale wind tunnel-investigation of the Advanced

Technology Light Twin-Engine airplane (ATLIT) --- Langley

full scale tunnel

[NASA-TP-1591 ] p 14 N80-22266

Flight evaluation of stabilization and command

augmentation system concepts and cockpit displays during

approach and landing of powered-lift STOL aircraft

[NASA-TP-1551] p 56 N81-11044

Experimental and theoretical supersonic

lateral-directional stability characteristics of a simplified

wing-body configuration with a series of vertical-tail

arrangements

[NASA-TP-1878J p 17 N81-29095

Space Shuttle separate-surface control-system study

(NASA-TP-2340] p 58 N84-28801

Static and dynamic pressure measurements on a NACA

00t2 airfoil in the Ames High Reynolds Number Facility

INASA-TP'2485J p 26 N85-27823

Rotorcraft Dynamics 1984

I NASA-CP-24001 p 38 N86-15280

Low-speed stability and control characteristics of a

transport model with aft-fuselage-mounted advanced

turboprops

[NASA-TP-2535} p 59 N86-22580

AERODYNAMIC STALLING

Dynamic stall experiments on the NACA 0012 airfoil

[NASA-TP-1100] p 7 N78-17000

Simulation study of the oscillatory longitudinal motion

of an airplane at the stall

[NASA-TP-1242J p 54 N78-30141

A laser velocimetar flow survey above a stalled wing

[NASA-TP-12661 p 10 N79-14019

Exploratory study of the effects of wing-leading-eqge

modifications on the stall/spin behavior of a light general

aviation airplane

[NASA-TP-1589} p 33 N80-13026

Simulator study of stall/post-stall characteristics of a

fighter airplane with relaxed longitudinal static stability ---

F-16

INASA-TP-1538] p 55 N80-14136

Spin tests of a single-engine, high-wiog light airplane

[NASA-TP-1927} p 35 N82-16068

Performance of single-stage axial-flow transonic

compressor with rotor and stator aspect ratios of 1.63

and 1 77, respectively, and with design pressure ratio of

2.05

(NASA-TP-2001 J p 49 N82-22269

Effects of wing-leading-edge modifications on a

full-scale, low-wing general aviation airplane: Wind-tunnel

investigation of high-angle-of-attack aerodynamic

characteristics --- conducted in Langley 30- by 60-foot

tunnel

INASA-TP-2011J p 4 N82-26217

Application of the ONERA model of dynamic stall

[ NASA-TP-23991 p25 N85-12862

night investigation of stall, spin and recovery

characteristics of a low-wing, single-engine, T-tail light

airplane

[NASA-TP-2427} p 37 N85-25248

AERODYNAMICS

High Reynolds Number Research

[NASA-CP-2009) p 59 N77-27139

A survey of computational aerodynamics in the United

States

[NASA-SP-394 ] p 6 N78-11007

Future Computer Requirements for Computational

Aerodynamics

fNASA-CP-20321 p 176 N78-19778

Numerical study Of transonic flow over oscillating airfoils

using the full potential equation

[NASA-TP-11201 p 8 N78-21055

Advanced Technology Airfoil Research, volume 1, part

1 --- conference on development of computational codes

and test facilities

INASA-CP-2045-PT-1 I p 11 N79-20030

Science and Technology of Low Speed and Motorless

Flight. Third international Symposium

IL-t2973J p 2 N79-27070

inclusion of unsteady aerodynamics in longitudinal

parameter estimation from flight data --- use of vortices

and mathematical models for parameterization from flight

characteristics

INASA-TP-1536j p 13 N80-12995

Classical aerodynamic theory

[NASA-RP-1050] p 13 N80-15033

Application of two design methods for active flutter

suppression and wind-tunnel test results

[NASA-TP-t6531 p 129 N80-22737

Proceedings of the Aero-Optics Symposium on

Electromagnetic Wave Propagation from Aircraft

[NASA-CP-2121] p 108 N80-25588

Experimental performance and analysis of

15 04-centimeter-tip-diameter, radial-inflow turbine with

work factor of 1.126 and thick blading

[NASA-TP-1730] p 47 N80-33410

Optimal regulation in systems with stochastic time

sampling

(NASA-TP-1743] p 184 N81-12812

Evaluation of flow quality in two large NASA wind tunnels

at transonic speeds

[NASA-TP-1737] p 108 N81-13303

Bibliography of Supersonic Cruise Research (SCR)

program from 1977 to mid- 1980

(NASA-RP-t0631 p 16 N81-14973

The high-speed frontier. Case histories of four NACA

programs, 1920 - t 950

[NASA-SP-445] p 3 N81-15969

Supersonic Cruise Research 1979, part 1

[NASA-CP-2108-PT-1 J p 3 N81-17981

A computer technique for detailed analysis of mission

radius and maneuverability characteristics of fighter

aircraft

[NASA-TP-1837] p 17 N81-20026

The aerodynamics of bodies in a rarefied ionized gas

with applications to spacecraft environmental dynamics

[NASA-TP-1933] p 72 N82-15116

Design cntaria for flightpath and airspeed control for

the approach and landing of STOL aircraft

[NASA-TP-1911 } p 57 N82-20187

Advanced aerodynamics. Selected NASA research

[NASA-CP-2208] p 4 N84-27660

Ninteenth Aerospace Mechanisms Symposium

[NASA-CP-2371 J p 134 N85-33512

A cumulative index to a continuing bibliography on

aeronautical engineering

[NASA-SP-7037(196)I p 5 N86-23552

Vortex Flow Aerodynamics, volume 1

(NASA-CP-2416-VOL-t ] p 28 N86-27190

Aeronautical engineenng: A continuing bibliography with

indexes (supplement 204)

[NASA-SP-7037(204) I p 5 N86-32389

AEROELASTICITY

Flutter Testing Techniques

[NASA-SP-415} p 1 N77-21022

High Reynolds Number Research

INASA-CP-2009] p 59 N77-27139

Measurement of model aeroelastic deformations in the

wind tunnel at transonic speeds using

stereophotogrammetry

[NASA-TP-10101 p 31 N78-10048

Analysis of preflutter and posfflutler characteristics with

motion-matched aerodynamic forces

[NASA-TP-1232] p 127 N78-28481

A method for obtaining practical flutter-suppression

control laws using results of optimal control theory

{NASA-TP-1471 ] p 128 N79-28614

Wind-tunnel experiments on divergence of

forward-swept wings

[NASA-TP-t685] p 34 N80-29287

An analytical technique for approximating unsteady

aerodynamics in the time domain

(NASA-TP-17381 p 130 N81-11422

Comparison of analytical and wind-tunnel results for

flutter and gust response of a transport wing with active

controls

INASA-TP-2010] p 131 N82-26703

An assessment of the capability to calculate tilting

prop-rotor aircraft performance, loads and stability

[NASA-TP-22911 p 37 N84-19333

Generalization of the subsonic kernel function in the

s-plane, with applications to flutter analysis

[NASA-TP-2292] p 23 N84-20480

Formulation of blade-flutter spectral analyses in

stationary reference frame

{NASA-TP*2296J p 51 N84-20562

AERONAUTICAL ENGINEERING

Aircraft Safety and Operating Problems --- conference

[NASA-SP-4161 p 28 N77-18081

A survey of computational aerodynamics in the United

States

[NASA-SP-394] p 6 N78-11007

The 13th Aerospace Mechanisms Symposium

INASA-CP-2081] p 128 N79-22539

The 1980 Aircraft Safety and Operating Problems, part

1

[NASA-CP-2170-PT-1 } p 29 N81-19035

Records of achievement: NASA special publications

[NASA-SP-470} p 197 N83-33792

Astronautics and aeronautics, 1976. A chronology

[NASA-SP-4021 I p 212 N84-25602

A-5
AERONAUTICS SUBJECT INDEX

Model research: The National Advisory Committee for

Aeronautics, 1915-1958, volume 1

[NASA-SP-4103-VOL-t J p 4 N85-23683

Model research, the National Advisory Committee for

Aeronautics, 1915-1958, volume 2

[NASA-SP.-4103-VOL-2] p 4 N85-23684

A cumulative index to a continuing bibliography on

aeronautical engineehng

{NASA.SP-7037(196)] p 5 N86-23552

Astronautics and aeronautics, 1977: A chronology

[NASA-SP*4022] p 213 N86-31524

Aeronautical engineering: A continuing bibliography w_th

inpexes (supplement 204)

{NASA-SP.7037(204)] p 5 N86-32389

AERONAUTICS

Agricultural aviation research

[NASA-CP-2025] p 1 N78-12999

Proceedings of the First Annual Meteorological and

Environmental Inputs to Aviation Systems Workshop

{NASA.CP.2028] p 158 N78-19711

Astronautics and Aeronautics, 1975, A chronology

(NASA-SP-4020] p 212 N81-16973

Proceedings: Fifth Annual Workshop on Meteorological

and Environmental Inputs to Aviation Systems

{NASA.CP.2192} p 3 N82-21139

Fuel economy in aviation

(NASA-SP-462] p 36 N84-15144

On the frontier: Flight research at Dryden 1946-1981

[NASA-SP-4303] p 4 N85-17934

Flight investigation of stall, spin and recovery

charactehstics of a low-wing, single-engine, T-tail light

airplane

[NASA-TP-2427] p 37 N85-25248

AERONOMY

Molecules of significance in planetary aeronomy

[NASA-RP-1030] p 199 N79-22980

Compendium of meteorology scientific issues of 1950

still outstanding

[NASA-RP-1167] p 156 N86-25900

AEROSOLS

Atmospheric aerosols: Their Optical Properties and

Effects

[NASA-CP-2004] p 15t N77o15563

Atmospheric aerosols: Their Optical Properties and

Effects [supplement)

INASA-CP-2004-SUPPL] p 151 N77-15564

Lidar backscattering measurements of background

stratospheric aerosols

[NASA-TP-1381 ] p 152 N79-17388

The NASA-Ames Research Center stratospheric aerosol

model. 2. Sensitivity studies and comparison with

observatories

[NASA-TP-1363} p 160 N79-21720

The NASA-AMES Research Center stratospheric

aerosol model, t Physical processes and computational

analogs

{NASA-TP-t362J p 160 N79-21721

Programs for calculating cell parameters in electron and

X-ray diffraction --- to identify stratospheric aerosols

NASA-TP-1529] p 148 N79-30844

Measurement techniques tot trace metals in coal-plant

effluents: A brief review

NASA-RP-f047] p 148 N79-33811

Stratospheric aerosol modification by supersonic

transporl operat=oes with climate implications

NASA-RP-1058] p 16t N80-18726

SAGE measurements of the stratospheric aerosol

dispersion and loading from the Soutriere Volcano

NASA-TP-1922] p 153 N82-12687

SAM 2 measurements of the polar stratospheric aerosol,

volume 1: October to April 1979

NASA-RP-1O81 ] p 153 N82-13592

The Third international Cloud Condensation Nuclei

Workshop --- conference

NASA-CP-22121 p 115 N82-15383

SAM 2 Measurements of the Polar Stratospheric

Aerosol, volume 2, Ap_'il 1979 to October 1979

NASA-RP-1088-VOL-2] p 153 N82-19734

Atmospheric Effects and Potential Climatic Impact of

Ihe 1980 Eruptions of Mount St Helena

NASA-CP-2240 j p 136 N83-11534

SAM 2 measurements of the polar stratospheric aerosol.

Volume 3: October 1979 to April 1980

NASA-RP-11061 p 154 N83-27520

SAM 2 measurements of the polar stratospheric aerosol

Volume 4: April 1980 to October 1980

NASA-RP-t 1071 p 164 N83 28796

Airborne lidar measurements of El Chichon stratospheric

aerosols, October 1982 to November 1982

NASA-RP-11361 p 155 N85-t9550

SAM 2 measurements of the polar stratospheric aerosol,

volume 5

NASA-RP-11401 p 155 N85-25970

SAM 11measurements ot the polar stratospheric aerosol

Volume 6: April to October t981

NASA-RP-1141 I p 155 N85-27422

SAGE aerosol measurements. Volume 1: February 21,

1979 to December 31. 1979

{NASA-RP-t144} p 155 N86-11700

Airborne lidar measurements of El Chichon stratospheric

aerosols

[NASA-RP-1148} p 155 N86-13650

Airborne Lidar measurements of aerosols, mixed layer

heights, and ozone during the 1980 PEPE/NEROS summer

field expenment

[NASA-RP-1143] p 150 N86-16748

Single scattering from nonspherical Chebyshev

particles: A compendium of calculations

{NASA.RP.11571 p 194 N86-17140

SAGE Aerosol Measurements. Volume 2:1 January -

31 December 1980

[NASA-RP-1149] p 156 N86-23088

Atrborna tider measurements of El Chichon atratoehperic

aaroeols

{NASA-RP-1166} p 156 N86-27835

SAM 2 measurements of the polar stratospheric aerosol,

volume 2

[NASA-RP-1164] p 157 N86-28562

SAM 2 measurements of the polar stratospheric aerosol,

volume 8

[NASA-RP-t t651 p 157 N86-29428

AEROSPACE ENGINEERING

Space settlements: A design study

[NASA-SP-413] p 60 N77-21106

Proceedings of the ASPE/MSFC Symposium on

Engineering and Productivity Gains from Space

Technology

[NASA-CP-2019} p 98 N77-30273

The 12th Aerospace Mechanisms Symposium

[NASA-CP-20801 p 120 N79-21352

The 1 lth Aerospace Mechanisms Symposium

[NASA-CP-2038] p t20 N79-21374

Space resources and space settlements

[NASA-SP-428] p 62 N79-32225

The 1979 Goddard Space Flight Center Battery

Workshop

[NASA-CP-2117 ] p 145 N80-20820

Proceedings of the 141h Aerospace Mechanisms

Symposium

[NASA-CP-21271 p 99 N80-23495

Aerospace Applications of Microprocessors

INASA-CP-2158J p 177 N81-11644

Beyond the atmosphere: Early years of space

science

[NASA-SP-4211 } p 200 N81-20962

Records of achievement: NASA special publications

[NASA-SP-470} p 197 N83-33792

The 18th Aerospace Mechanisms Symposium

[NASA-CP-2311 I p t33 N84-25078

Astronautics and aeronautics, 1976 A chronology

[NASA-SP-40211 p 212 N84-25602

Reduction method for thermal analysis of complex

aerospace structures

[ NASA-TP-2373 ] p 112 N85-16066

Searching the horizon: A history of Ames Research

Center, 1940-1976

[NASA-SP-4304] p 213 N86-16185

Technology for large space systems: A bibliography with

indexes (supplement 14)

INASA-SP-7046(14)] p 63 N86-28104

AEROSPACE ENVIRONMENTS

Nuclear waste disposal in space

{NASA-TP-t225J p 144 N78-23571

Spacecraft Charging Technology, 1978

{NASA CP 2071 i p 71 N79-24001

Space resources and space settlements

{NASA-SP-4281 p 62 N79-32225

Avenues and incentives for commercial use of a

tow-gravity environment

[NASA-TP-19251 p 94 N81-33292

Performance of an ablator for Space Shuttle inorb, t repair

in an arc-plasma airstream

I NASA-TP-2150 l p 74 N83-22317

Space Physiology and Medicine

[NASA-SP-4471 p 170 N83-25349

Long Duration Exposure Facitity (LDEF). Mission 1

Experiments

[NASA-SP-473} p 67 N84-24632

Space Photovolfaic Research and Technology 1985:

High Efficiency, Space Environment, and Array

Technology

I NASA-CP-2408] p 146 N86-17839

A stochastic model for particle impingements on orbiting

spacecraft

(NASA-TP-2550] p 184 N86-19095

AEROSPACE INDUSTRY

Combustion Fundamentals Research

INASA-CP-2268] p 50 N83-29208

AEROSPACE MEDICINE

The Apollo-Soyuz Test Proiect: Medical report

[NASA-SP-4111 p 170 N77-30735

The use of nonhuman primates in space

{NASA-CP-005] p 169 N78-11663

The 14th Annual Conference on Manual Control --- digital

simulation of human Operator dynamics

[NASA-CP-2060] p 173 N79-15588

Space Gerontology

[NASA.CP.2248] p 170 N83.16018

Space Physiology and Medicine

[NASA-SP-447] p 170 N83-25349

Astronautics and aeronautics, 1976, A chronology

[NASA-SP-4021} p 212 N84-25602

The human factor: Biomedicine in the manned space

program to 1980

[NASA-SP-4213] p 170 N86-2f097

Aerospace Medicine and Biology: A Cumulative Index

to the 1965 Issues

[NASA-SP-7011(280)] p 170 N86-23265

Aerospace medicine and biology: A continuing

bibliography with indexes (supplement 288)

[NASA-SP-7011(288)] p 171 N86-32088

AEROSPACE SCIENCES

Beyond the atmosphere' Early years of space

science

[NASA-SP-4211 ] p 200 N81-20962

STEP Experiment Requirements

( NASA-CP-2294 ] p87 N84-17211

Optical Information Processing for Aerospace

Applications 2

[NASA-CP-2302] p 194 N84-22402

AEROSPACE SYSTEMS

System analysis approach to deriving design cdteda

(Loads) for Space Shuttle and its payloads, Volume 2:

Typical examples

[NASA-TP-1950] p 66 N82-15106

Ninteenth Aerospace Mechanisms Symposium

[NASA-CP-2371] p 134 N85-33512

A spasefaring people: Perspectives on early

specefhght

[NASA-SP-4405) p 212 N85-35142

AEROSPACE TECHNOLOGY TRANSFER

Proceedings of the Workshop on an Electromagnetic

Positioning System in Space

[NASA-CP-20691 p 61 N79-13069

Lessons of the NASA Tech House

[NASA-SP-4421 p 199 N80-27219

STEP Experiment Requirements

[NASA-CP-2294} p 67 N84-17211

AEROSPACE VEHICLES

Evaluation of a tow-density polyimide foam in e dynamic,

high temperature environment

[NASA-TP-10491 p 91 N78-12223

System analysis approach to deriving design criteria

(Loads) for Space Shuttle and its payloads Volume 2:

Typical examples

[NASA-TP-1950] p 66 N82-15106

Studies of implicit and explicit solution techniques in

transient thermal analysis of structures

INASA-TP-20381 p 110 N82-31646

IPAD: Integrated Programs for Aerospace-vehicle

Desff:Jn

{NASA-CP-21431 p 179 N83-17115

Experimental design of an intedaboratory study for trace

metal analysis of liquid fluids --- for aerospace vehicles

[NASA-TP-21481 p 85 N83-24575

AEROTHERMODYNAMICS

Aerofhermal tests of a heat-pipe-cooled leading edge

at Mach 7 --- hypersonic heat transfer for space shuttle

orbiters

INASA-TP-13201 p 195 N79-13901

Aerothermal performance of radiativety and actively

cooled panel at Mach 66

INASA-TP-1595] p 107 N80-13402

Aerothermal environmenl m chordwise gaps between

split elevons al Math 6.8

(NASA-TP-1783] p 109 N81-15237

Performance ol a Haynes 188 metallic standoff thermal

protection system at Mach 7

INASA-TP-18021 p 72 N81-21116

Thermat and aerothermal performance of a titanium

multiwall thermal protection system

INASA-TP-1961 J p 72 N82-14277

Shuttle Performance: Lessons Learned, part 1

[NASA-CP-2283-PT-1 I p 69 N84-10115

Shuttle Performance: Lessons Learned, part 2

[NASA-CP-2283-PT-21 p 69 N84-10144

Space Shuttle wind tunnel testing program

[NASA-RP-1125} p 74 N85-11127

Experimental and predicted heating distributions for

biconics at incidence in air at Mach 10

[NASA-TP-23341 p 112 N85-12313

Structural Integrity an0 Durability of Reusable Space

Propulsion Systems

l NASA-CP-2381 ] p 78 N85-27941

A-6
SUBJECT INDEX

AFTERBODIES

Flight-measured aftarbody pressure coefficients from an

airplane having twin side-by*side jet engines for Mach

numbers from 0.6 to 1.6

[NASA-TP-1549] p 13 N80-11035

Viscous.inviscid calculations of jet entrainment effects

on the subsonic flow over nozzle afferbodies

[NASA-TP-1626] p 14 N80-22261

Effects of axisymmetric and normal air jet plumes and

solid plume on cylindrical afterbody pressure distributions

at Mach numbers from 1 65 to 2.50

[NASA-TP-2005] p 19 N82-22215

Effects of twin-vertical-tail parameters on twin-engine

afferbody/nozzle aerodynamic charactanstics --- Langley

16-if transonic tunnel tests

[NASA-TP-2158] p 21 N63-24478

Effect of empennage location on twin-engine

afterbody-nozzle aerodynamic characteristics at Msch

Numbers from 0.6 to 1.2 --- wind tunnel tests

[NASA-TP-2116] p 21 N83-25666

AFTERBURNING

Altitude test of several afterburner configurations on a

turbofan engine with a hydrogen heater to simulate an

elevated turbine discharge temperature

[ NASA-TP-1068 ] p41 N76-11106

Effects of entrained water and strong turbulence on

aftarburning within solid rocket motor plumes

[NASA-TP-1111] p 147 N78-15596

Measurements and predictions of flyover and static noise

of a TF30 afferburning turbofan engine

[NASA-TP-1372] p 43 N79-13045

Operating condition and geometry effects on

low.frequency afterburner combustion instability in a

turbofan at altitude

[NASA.TP-1475] p 44 N79-25022

AGING (BIOLOGY)

Space Gerontology

(NASA-CP-2248] p 170 N83-16018

AGING (MATERIALS)

Long-term thermal aging of 2 graphite-polyimide

composite materials

[NASA-TP-2369] p 83 N85-12094

AGRICULTURE

Agricultural aviation research

[NASA-CP-2025] p I N78-12999

The use of LANDSAT digital data and

computer-implementad techniques for an agricultural

application

[NASA-RP-1016t p 138 N76-21568

Western Regional Remote Sensing Conference

Proceedings, 1979

[NASA-CP-2148] p 139 N81-21440

A comparative statistical study of long-term agroclimatic

conditions affecting the growth of US winter wheat:

Distributions of regional monthly average precipitation on

the Great Plains and the state of Maryland and the effect

of agroclimatic conditions on yield in the state of Kansas

[NASA-TP-1724] p 163 N81-22658

An experimental and theoretical investigation of

deposition patterns from an agricultural airplane

[NASA*TP-2348] p 25 N64-33379

AGROCLIMATOLOGY

A comparative statistical study of long-term agroclimatic

conditions affecting the growth of US winter wheat:

Distnbutions of regional monthly average precipitation on

the Great Plains and the state of Maryland and the effect

of agroclimatic conditions on yietd in the state of Kansas

[NASA-TP-1724] p 163 N81-22658

AILERONS

Description of an experimental (hydrogen peroxide)

rocket system and its use in measuring aileron and rudder

effectiveness of a light airplane

[NASA-TP-16471 p 55 N80-22358

Effect of aileron deflections on the aerodynamic

characteristics of a semispan model of a subsonic

energy-efficient transport

[ NASA-TP-2478 J p 27 N86-11166

AIR

Computer program for obtaining thermodynamic and

transport properties of air and products of combustion of

ASTM-A-1 fuel and air

[NASA-TP-1160] p 97 N78-20351

Chemical kinetic analysis of hydrogen-air ignition and

reaction times

[NASA-TP-1856I p 85 N61-27223

Low-frequency sound absorption measurements in air

[NASA-RP-1128] p 190 N65-11789

AIR BREATHING BOOSTERS

Mach 6 flow field surveys beneath the forebody of an

airbreathing missile

[NASA-TP-2491] p 28 N86-23558

AIR BREATHING ENGINES

Propulsion Controls, 1979 --- air breathing engine

control

[NASA-CP-2137] p 47 N81-12090

Proposed fast-responsa oxygen monitoring and control

system for the Langley 8-foot high-temperature tunnel

[NASA-TP-2218] p 116 N64-11460

Aeronaubcal facilities catalogue. Volume 2: Airbreathing

propulsion and flight simulators

[NASA.RP.1133] p 60 N86-f8328

AIR CONDITIONING

Simulation model of a single-stage lithium bromide-water

absorption cooling unit

INASA-TP-1296t p 86 N78-30205

AIR COOLING

Cold air performance of a

12.766-centimeter-tip-diameter axial-Now cooled turbine.

2: Effect of air ejection on turbine performance

[NASA-TP-1018] p 5 N77-30089

Cold-air performance of free-power turbine designed for

112-kilowatt automotive gas-turbine engine. 1: Design

Stator-vane-chord setting angle of 35 dog

[NASA-TP-1007J p 42 N78-16053

Computer program for generating input for analysis of

impingement-cooled, axial-flow turbine blade

[NASA-TP-1603] p 107 N80-15361

Effects of a ceramic coating on metal temperatures of

an sir-cooled turbine vane

[NASA-TP-1598] p 107 N80-17397

Nonlinear, three-dimensional finite-element analysis of

air-cooled gas turbine blades

[NASA-TP-t669] p 129 N80-22734

Extension of similarity test procedures to cooled engine

components with insulating ceramic coatings

[NASA-TP-1615) p 108 N80-24577

Review and status of heat-transfer technology for

internal passages of air-cooled turbine blades

JNASA-TP-2232] p 111 N84-21828

AIR CURRENTS

NASA/MSFC FY-82 atmosphenc processes research

review

[NASA-CP-2259] p 165 N83-19391

AIR CUSHION LANDING SYSTEMS

Braking and cornering studies on an air cushion landing

system

[NASA-TP-2196J p 36 N63-34935

AIR DATA SYSTEMS

Comparison of predicted and experimental real-gas

pressure distributions on space shuttle orbiter nose for

shuttle entry air data system

[NASA.TP-1627] p t4 N80-21260

Wind tunnel investigation of an all flush orifice air data

system for a large subsonic aircraft --- conducted in s

Langley 8 foot transonic pressure tunnel

[NASA-TP-1642J p 36 N80-23304

Subsonic tests of an all-flush-pressure-orifice air data

system

[NASA-TP-1871] p 39 N81-26144

AIR FLOW

Comparison of calculated and altitude-facility-measured

thrust and airflow of two prototype F100 turbofan

engines

[NASA-TP-1373] p 43 N79-13044

Aerodynamic performance of axial-flow fan stage

operated st nine inlet guide vane angles --- to be used

on vertical tift aircraft

[NASA-TP-1510] p 45 N79-31214

Turbojet-exhaust-nozzle secondary-airflow pumping as

an exit control of an inlet-stability bypass system for a

Mach 2.5 axisymmetric mixed-compression inlet --- Lewis

10- by 10-ft. supersonic wind tunnel test

[NASA-TP-1532] p 46 N80-14124

Single-stage electrohydraulic sarvosystem for actuating

on airflow valve with frequencies to 500 hertz

[NASA-TP-1678] p 56 Ng0-29369

Preliminary tests of an advanced high-temperature

combustion system

[NASA-TP-2203] p 50 N83-33893

Expanded operational capabilities of the Langley Mach

7 Soramjet test facility

INASA-TP-2186] p 60 N83-36039

Evaluation of e total energy-rate sensor on a transport

airplane

[NASA-TP-2212] p 40 N84-12164

Review and status of heat-transfer technology for

internal passages of air-cooled turbine blades

[NASA-TP-2232] p 111 N84-21828

Slip-boundary equations for multicomponent

nonequilibrium airflow

[NASA-TP.2452| p 113 N66-14530

AIR INTAKES

A throat-bypass stability-bleed system using relief valves

to increase the transient stability of s mixed-compression

inlet --- YF-12 aircraft inlet tests in the Lewis 10 by 10 ft

supersonic wind tunnel

[NASA-TP-t063J p 45 N79-28176

The high-speed frontier, Case histories of four NACA

programs, 1920 - 1950

[NASA-SP-445] p 3 N81-15969

AIR TRAFFIC CONTROL

AIR JETS

Velocity field of a round jet in a cross flow for various

jet injection angles and velocity ratios --- Langley V/STOL

tunnel

{NASA-TP-1506] p 107 N79-32500

Effects of axisymmetric and normal air jet plumes end

solid plume on cylindrical afterbody pressure distributions

at Mach numbers from 1.65 to 2.50

[NASA-TP-2005] p 19 N62-22215

AIR NAVIGATION

Joint University Program for Air Transportation

Research, 1961

[NASA-CP-2224 ] p 3 N82-26199

AIR POLLUTION

Aimraff Piston Engine Exhaust Emission Symposium

INASA-CP-2005] p 41 N77-17081

Aircraft engine emissions --- conference

[NASA-CP-2021] p 41 N76-11063

A gas filter correlation monitor for CO, CH4, and HCI

[NASA-TP.1113] p 113 N76-13408

A high-pressure premixed fiat-flame burner for chemical

process studies --- of pollutant formation in hydrocarbon

flames

[NASA-TP-1318] p 84 N79-14177

Ozone measurement system for NASA global air

sampling program

[NASA-TP-1451 ] p 148 N79-22654

Effect of primary-zone equivalence ratio on pollutant

formation

[NASA-TP-t463J p 44 N79-23086

Sulfate and nitrate collected by filter sampling near the

tropopause

[NASA-TP-1567] p 149 N60-14561

Pollutant emissions from flat-flame burners at high

pressures

[NASA-TP-1673] p 85 N80-25392

Two-dimensional model studies of the effect of

supersonic aircraft operations on the stratospheric ozone

content

[NASA-RP-1064] p 149 N81-17622

Report of the NASA working group on trOpOspheric

program planning

[NASA-RP-t062] p 153 N81-23742

Application of a Gaussian multilayer diffusion model to

characterize dispersion of vertical HCI column density in

rocket exhaust clouds

[NASA.TP-1956] p 149 N82.14672

Atmospheric Effects and Potential Climatic Impact of

the 1980 Eruptions of Mount St. Helena

[NASA-CP-2240] p 136 N83-11534

AIR QUALITY

A diagnostic model for studying daytime urban air quality

trends

[NASA-TP-1843] p 149 N61-22587

Applying modeling Results in designing a global

tropospheric experiment

[NASA-CP-2235] p 153 N82-29796

Airborne measurements of launch vehicle effluent of

STS-2 launch on November 12, 1981 at Cape Canaveral,

Florida

[NASA-TP-2260] p 150 N84-18764

AIR SAMPLING

Sulfate and nitrate collected by filter sampling near the

tropepeuse

[NASA-TP-1567] p 149 N80-t4581

Analysis of atmospheric ozone levels at commercial

airplane cruise altitudes in winter and spring, 1976 - 1977

-- Global Atmospheric Sampling Program

[NASA-TP-1807] p 163 N81-21685

AIR TRAFFIC

Effect of lead-aircraft ground-speed on self-spacing

performance using s cockpit display of traffic information

[NASA-TP-2194] p 40 N83-36028

AIR TRAFFIC CONTROL

Precision positional data of general aviation air traffic

in terminal air space

[NASA-RP-1020] p 1 N78-25048

Proceedings, Third Annual Workshop on Meteorological

and Environmental Inputs to Aviation Systems

[NASA-CP-2104] p 160 N60-14633

Flight investigation of cockpit -displayed traffic

information utilizing coded symbology in an advanced

operational environment

[NASA-TP-t684] p 36 N80-27360

Development and test results of a flight management

algorithm for fuel conservative descents in a time-based

metered traffic environment

[NASA-TP-1717] p 39 N80-33404

Proceedings: Fourth Annual Workshop on

Meteorological and Environmental Inputs to Aviation

systems

[NASA-CP-2139] p 162 N81-14555

Effect of display size on utilization of traffic situation

display for self-spacing task --- transport aircraft

[NASA-TP-1885] p 30 N81-29109

A-7
AIR TRANSPORTATION

Proceedings: Fifth Annual Workshop on Meteorological

end Environmental Inputs to Aviation Systems

JNASA-CP-2192 p 3 N82-21139

Analysis and Monte Carlo simulation of near-terminal

aircraft flight paths

[NASA-TP-tg97 p 31 N82-23233

Helical automatic approaches of helicopters with

microwave landing systems

{NASA-TP-2109J p 31 N83-18704

Proceedings: Sixth Annual Workshop on Meteorological

and Environmental Inputs to Aviation Systems

INASA-CP-2274 p 4 N83-33827

Simulation of cockpit-display concept for executing a

wake-vortex avoidance procedure

INASA-TP-2300 p 40 N84-21542

A cockpit-display concept for executing a multiple

glide-slope approach for wake-vorfex avoidance

{ NASA-TP-2386 p 40 N85-16869

Simulation studies of time-control procedures for the

advanced air traffic control system

{NASA-TP-2493 p 30 N85-32101

NASA and general aviation

{NASA-SP-485} p 38 N86-30720

AIR TRANSPORTATION

CTOL Transport Technology, 1978 ---conferences

(NASA-CP-2036-PT-2J p 1 N78-29046

Joint University Program for Air Transportation

Research, 1980

[NASA-CP-2176} p 3 N81-21999

AIR WATER INTERACTIONS

WETAIR: A computer code for calculating

thermodynamic and transport properties of air-water

mixtures

[NASA-TP-1466] p 178 N79-23688

The role of satellite altimetry in climate studies

[NASA-TP-15701 p 161 N80-16676

Fronbers of Remote Sensing of the Oceans end

Troposphere from Air end Space Platforms

{NASA-CP-2303} p 142 N84-27262

Global Biology Research Program: Biogeochemical

Processes in Wetlands

INASA-CP-2316} p 169 N84-30665

North Atlantic Deep Water Formation

[NASA-CP-2367] p 169 N85-26028

Understanding climate: A strategy for climate modeling

and predictability research, 1985-1995

[NASA-RP.1158} p 166 N86-13866

Surface radiation budget for climate applications

[NASA-RPol169J p 167 N86-28574

AIRBORNE EQUIPMENT

Validation Methods Research for Fault-Tolerant Avionics

and Control Systems Working Group Meeting, 2

{NASA-CP-2130] p 176 N80-23008

Exploratory Meeting on Airborne Doppler Lidar Wind

Velocity Measurements

INASA-CP-2140} p 162 N80-26999

MARS 1414 recorder environmental tests

INASA-TP-1709] p 115 N80-30716

Airborne Lidar measurements of aerosols, mixed layer

heights, and ozone during the 1980 PEPE/NEROS summer

field experiment

[NASA-RP-tt43) p 150 N86-16748

AIRBORNE/SPACEBORNE COMPUTERS

Dsscnption of the VTOL Approach and Landing

Technology (MALT) CH-47 research system

{NASA-TP-1436] p 54 N79-29195

Ruggedized minicomputer hardware and software

topics, 1981: Proceedings of the 4th ROLM MtL-SPEC

Computer User's Group Conference

{NASA-CP-2206} p 180 N82-14829

AIRCRAFT

GRtD30: Computer program for fast generation of

multilevel, three-dimensional boundary-conforming O-type

computational gnds

[NASA-TP-tg20] p 18 N81-31128

STABCAR: A program for finding characteristic root

systems having transcendental stability matrices

{NASA-TP-2165} p 179 N84-27461

On the frontier: Flight research at Dryden 1946-1981

[NASA-SP-4303] p 4 N85-17934

AIRCRAFT ACCIDENTS

Light sirptane crash tests at three flight-path angles

[NASA-TP-12101 p 127 N78-26494

Some human factors issues in the development and

evaluation of cockpit alerting end warning systems

[NASA-RP-t055] p 173 N80-15821

Assessment of Carbon Fiber Electrical Effects

{NASA*CP-2119] p 80 N80-tg193

Risk to the public from carbon fibers released in civil

aircraff accidents

{NASA*SP-448} p 81 N81-18096

Correlation and assessment of structural airplane crash

date with flight parameters at impact

{NASA-TP-2083] p 131 N83-14521

A-8

Controls, Displays, and Information Transfer for Generat

Aviation tFR Operations

[NASA-CP-22791 p 4 N84-12029

Survey of NASA research on crash dynamics

[NASA-TP-22981 p 133 N84-2t901

Full-Scale Transport controlled Impact Demonstration

{NASA-CP-2395J p 135 N86-21933

Impact data from a transport aircraft during a controlled

_mpact demonstration

{NASA-TP-2589] p 38 N86-30721

AIRCRAFT APPROACH SPACING

Effect of display size on utilization of traffic situation

display for self-spacing task --- transport aircraft

{NASA-TP-1885} p 30 N81-29109

Evaluation of Microwave Landing System (MLS) effect

on the delivery performance of a fixed-path metering and

spacing system

[NASA-TP-1844} p 31 N81-29111

Simulation study of traffic-sensor noise effects on

utilization of traffic situation display for self-spacing task

(NASA-TP.2082] p 40 N83-18723

AIRCRAFT BRAKES

Behavior of aircraft antiskid braking systems on dry and

wet runway surfaces. A slip-velocity-controlled.

pr essur e-biss- modulatad system

[NASA-TP-1051 J p 33 N80-12084

Behavior of aircraft antiskid braking systems on dry and

wet runway surfaces: Hydromechanically controlled

system

{NASA-TP-1877} p 35 N81-30112

Dynamics of aircraft antiskid braking systems ---

conducted at the Langley aircraft landing loads and traction

facility

[NASA-TP-1959] p 35 N82-18204

Tire tread temperatures during antiskid braking and

cornering on a dry runway

[NASA-TP-2009] p 35 N82-24t93

AIRCRAFT COMPARTMENTS

Ozone concentration in the cabin of a Gates Leaqet

measured simultaneously with atmospheric ozone

concentrations

[NASA-TP-1340] p 148 N78-33618

Ozone Contamination in Aircraft Cabins

[NASA.CP.2066] p 29 N79.21021

Procedures for estimating the frequency of commercial

airline flights encountenng high cabin ozone Ievels

I NASA-TP-1560 ] p29 N79-33171

Analysis of atmosphenc ozone levels at commercial

airplane cruise altitudes in winter and spring, 1976 - 1977

--- Global Atmospheric Sampling Program

[NASA-TP-t807] p 163 N81.21685

Effects of propeller rotation direction on airplane intenor

noise levels

[NASA-TP-2444} p 190 N85-30767

AIRCRAFT CONFIGURATIONS

Configuration heating for a hypersonic research airplane

concept having a 70 deg swept double-delta wing

[NASA-TP-1143] p 105 N78-23389

Aerodynamic derivatives for an oblique wing aircraft

estimated from flight data by using a maximum likelihood

technique

[NASA-TP-1336} p 10 N78-33054

Flutter analysis of an airplane with multiple structural

nonlinearities in the control system

[NASA-TP-1620] p 58 N80-24324

A common geometnc data-base approach for

computer-aided manufacturing of wind-tunnel models and

theoretical aerodynamic analysis

{NASA-TP-2151| p 21 N83-22166

Effect of empennage location on twin-engine

afterbody-nozzle aerodynamic characteristics at Mach

Numbers from 0.6 to 1.2 --- wind tunnel tests

{NASA-TP-2116} p 21 N83-25666

Investigation of trailing-edge-flap, spanwise-biowing

concepts on an advanced fighter configuration

[NASA-TP-2250] p 23 N84-18164

Wing planform effects at supersonic speeds for an

advanced fighter configuration

[NASA-TP-2269] p 23 N84-20486

Quest for performance: The evolution of modern

aircraft

[NASA-SP-468J p 5 N85-32089

AIRCRAFT CONSTRUCTION MATERIALS

Selected NASA research in composite Materials and

structures

{ NASA-CP-2142) p80 N80-28436

Laminar Flow Control. The Research and Technology

Studies 1981

INASA-CP-2218] p 19 N82-20149

Advanced Materials Technology

INASA-CP-2251I p 79 N83-12147

Compression panel studies for supersonic cruise

vehicles

[NASA-TP-1617] 13 82 N83-28099

SUBJECT INDEX

Fabrication and evaluation of brazed titanium.clad

Borsic/aluminum compression panels

{NASA-TP-t573J p 82 N83-28100

Fricti0rl and wear behavior of aluminum and composite

airplane,skins

[NASA-TP-2262] p 37 N84-17175

ACEE Composite Structures Technology: Review of

selected NASA research on composite materials and

structures

I NASA-CP-2321 ] p 83 N84-29969

High Temperature Polymer Matrix Composites

INASA-CP-2385] p 83 N86-11260

AIRCRAFT CONTROL

Analytical study of ride smoothing benefits of control

system configurations optimized Ior pilot handling

qualities

[ NASA-TP-t 148} p53 N78-18076

Simulator evaluation of a flight-path-angle control system

for a transport airplane with direct lift control

[ NASA-TP-1116] p53 N78-20139

Flight evaluation of the transonic stability and control

characteristics of an airplane incorporating a supercritical

wing

tNASA-TP-11671 p 53 N78-20140

Pilot-model analysis and simulation study of effect of

control task desired control response

] NASA-TP-1140 } p 53 N78-20143

Fourth NASA Inter-Center Control Systems

Conference

INASA-CP-007J p 212 N78-23010

A flight investigation of the stability, control, and handling

qualities of an augmented jet flap STOL airplane

[NASA-TP-1254] p 53 N78-26151

Determination of stability and control parameters of a

light airplane from flight data using two estimation methods

--- equation error and maximum likelihood methods

{NASA-TP-1306] p 11 N79-20071

Fixed-base simulation study of decoupled longitudinal

controls during approach end landing of a medium jet

transport in the presence of wind shear

{NASA-TP-1519} p 58 N79-33218

Full-scale wind tunnel-investigation of the Advanced

Technology Light Twin-Engine airplane (ATLIT) --- Langley

full scale tunnel

{NASA-TP-1591 j p 14 N80-22266

Maximum likelihood method for estimating airplane

stability and control parameters from flight data in

frequency domain

I NASA-TP-1637} p 55 N80-24323

Flutter analysis of an airplane with multiple structural

nonlinearities in the control system

[NASA-TP-1620J p 55 N80-24324

Control-system techniques for improved departure/spin

resistance for fighter aircraft

INASA-TP-16891 p 2 N80-29244

Simulation comparison of a decoupled longitudinal

control system and a velocity vector control wheel steering

system during landings in wind shear

{NASA-TP-t734I p 56 N81-12109

An analytical study of the longitudinal response of

airplanes to positive wind shear

INASA-TP-1765] p 56 N81-20082

Effects of cable geometry and alrcraff attitude on the

accuracy of a magnetic leader cable system for aircraft

guidance during rollout and turnoff

[NASA-TP-1978] p 3t N82-22239

Relative control effectiveness technique with application

to sirplane control coordination

{NASA-TP-2416) p 37 N85-23753

AIRCRAFT DESIGN

Systems reliability issues for future aircraft

INASA-CP'003] p 175 N77-22808

Spin-tunnel investigation of the spinning characteristics

of typical single-engine general aviation airplane designs

1 Low-wing model A: Effects of tail configurations

[NASA-TP-1009} p 5 N77-33111

Lightning protection of aircraft

{NASA-RP-1008] p 29 N78-11024

Wake Vortex Minimization

[NASA-SP-409] p 6 N78-12017

GEMPAK: An arbitrary aircraft geometry generator

(NASA-TP-1022 J p 32 N78-16042

Proceedings of the First Annual Meteorological and

Environmental Inputs to Aviation Systems Workshop

INASA-CP-20281 p 158 N78-19711

Preliminary study of a large span-distributed-load

flying-wing cargo airplane concept

[NASA-TP-1158 ] p 32 N78-25079

Modal control theory and application 10 sircraff lateral

haodiing qualities design

NASA-TP-1234J p 53 N78-25101

CTOL transport technology, 1978 --- conferences

NASA-CP-2036-PT-1 ] p 1 N78-27046

CTOL Transport Technology, 1978 .-.conferences

NASA-CP-2036-PT.2] p 1 N78-29046
SUBJECT INDEX AIRCRAFT MANEUVERS

An assessment of the effect of supersonic aircraft

operations on the stratospheric ozone content

[NASA-RP-t0261 p 159 N78-30774

Recent Advances in Structures for Hypersonic Flight,

part 1 --- conferences

[NASA-CP-2065-PT-1 } p 128 N79-21422

Wind-tunnel investigation of the validity of a

sonic-boom-minimization concept --- Langley Unitan/Plan

Wind Tunnel tests for supersonic transport design

[NASA-TP-1421 ] p 12 N80-10102

Effects of fuselage forebody geometry on low-speed

lateral-directional characteristics of twin-tail fighter model

at high angles of attack

[NASA-TP-1592] p 13 N50-13002

Parametric study of variation in cargo-airplane

performance related to progression from current to

spanloader designs

{NASA-TP-1625} p 34 N80-21318

Subsonic aircraft: Evolution and the matching of size

to performance

[NASA-RP-1060] p 2 N80-29245

Low-speed aerodynamic characteristics of a 13 percent

thick medium speed airfoil designed for general aviation

applications

[NASA-TP-1498] p 16 N81-12015

Economic evaluation of flying-qualities design criteria for

a transport configured with relaxed static stability

[NASA-TP-1760} p 56 N81-13968

The high-speed frontier. Case histories of four NACA

programs, 1920 - 1950

[NASA-SP-445} p 3 N81-15969

Supersonic Cruise Research 1979, part 1

INASA-CP-2108-PT-1 } p 3 N81-17981

Advanced aerodynamics and active controls, Selected

NASA research

INASA-CP-2172] p 3 N81-19001

A procedure for designing forebodies with constraints

on cross-section shape and axial area distribution

[NASA-TP-1881 ] p 17 N81-26078

Vehicle concepts and technology requirements for

buoyant heavy-lift systems

[NASA-TP-1921 ] p 35 N81-31155

Electric Flight Systems

INASA-CP-2209 ] p3 N82-19134

Application of modal control to wing-flufter

suppression

{NASA-TP-1983} p 57 N82-24209

Small transport aircraft technology

{NASA-SP-460) p 36 N83-20931

Wave drag as the objective function in transonic fighter

wing optimization

{NASA-TP-2265] p 23 N84-17127

NASA Aircraft Controls Research, 1983

{NASA-CP-2296] p 58 N84-20567

Astronautics and aeronautics, 1976. A chronology

{NASA-SP-4021} p 212 N84-25602

ACEE Composite Structures Technology: Review of

selected NASA research on composite materials and

structures

{NASA-CP-2321 } p 63 N84-29969

Parametric study of a canard-configured transporl using

conceptual design optimization

[NASA-TP-2400} p 37 N85-19979

Energy efficient transport technology: Program summary

and bibliography

[NASA-RP-1135 } p37 N85-33116

Searching the horizon: A history of Ames Research

Center, 1940-1976

[NASA-SP-4304] p 213 N86-16185

Vortex Flow Aerodynamics, volume 1

[NASA-CP-2416-VOL-1 I p 28 N86-27190

NASA and general aviation

INASA-SP-485] p 38 N86-30720

AIRCRAFT ENGINES

Effect of fin passage length on optimzation of cylinder

head cooling fins

[NASA-TP-1054] p 104 N77-32432

Aircraft engine emissions --- conference

INASA-CP-2021 ] p 41 N78-11063

The rotary combustion engine: A candidate for general

aviation -- conferences

INASA-CP-2067] p 44 N79-15961

Generation of linear dynamic models from a digital

nonlinear simulation

[NASA-TP-1388] p 2 N79-16796

Premixed Prevaporized Combustor Technology Forum

[NASA-CP-2078] p 44 N79-24994

Aeropropulsion 1979 --- conferences

INASA-CP-2092] p 45 N80-10205

General Aviation Propulsion

[NASA-CP-2126] p 46 N80-22327

Cold-air investigation of a 4 1/2 stage turbine with

stage-loading factor of 4.66 and high specific work output,

2: Stage group performance

[NASA-TP-1688} p 47 N80-25338

Propulsion Controls, 1979 --- air breathing engine

control

{NASA-CP-2137] p 47 N81-t2090

Reasons for low aerodynamic performance of

13,5-centimeter-tip-diameter aircraft engine starter

turbine

{NASA-TP-1810] p 48 N81-20076

Aircraft Engine Diagnostics

[NASA-CP-2190} p 48 N81-31196

Noise suppression characteristics of peripherally

segmented duct liners

[NASA-TP-1904} p 168 N81-33946

Electric Flight Systems

{NASA-CP-2209] p 3 N82-19134

Some design considerations for solar-powered aircraft

{NASA-TP-1675} p 36 N82-32350

Analysis of a topping-cycle, aircraft, gas-turbine-engine

system which uses cryogenic fuel

INASA-TP-2294] p 51 N84-21549

Effects of inlet distortion on a static pressure probe

mounted on the engine hub in an F-15 airplane

[NASA-TP-2411] p 52 N65-22394

NASA and general aviation

[NASA-SP-485J p 38 N86-30720

AIRCRAFT EQUIPMENT

Miniature flow-direction and airspeed sensor for

airplanes and radio controlled models in spin studies

[NASA-TP-1467} p 38 N79-23081

Evaluation of a computer-generated perspective tunnel

display for flight path following

{NASA-TP-1736] p 39 N81-13958

Optical Information Processing for Aerospace

Applications

{NASA-CP-2207} p 194 N82-15894

Simulation studies of time-control procedures for the

advanced air traffic control system

[NASA-TP-2493J p 30 N85-3210t

AIRCRAFT FUELS

Jet aircraft hydrocarbon fuels technology

[NASA-CP-2033] p 97 N78-19325

Aircraft Research and Technology for Future Fuels

{NASA-CP-2146] p 47 N80-29300

Aviation Gasolines and Future Alternatives

{NASA-CP-2267] p 97 N83-22442

Analysis of a topping-cycle, aircraft, gas-turbine-engine

system which uses cryogenic fuel

[NASA-TP-2294] p 51 N84-21549

Full-Scale Transport controlled Impact Demonstration

{NASA-CP-2395} p 135 N86-21933

AIRCRAFT GUIDANCE

Effects of cable geometry and aircraft attitude on the

accuracy of a magnetic leader cable system for aircraft

guidance during rollout and turnoff

[NASA-TP-1978} p 31 N82-22239

Results from tests, with van-mounted sensor, of

magnetic leader cable for aircraft guidance during roll-out

and turnoff

INASA-TP-2092} p 40 N83-16338

A comparison of two position estimate algorithms that

use ILS Iocalizer and DME information Simulation and

flight test results

[NASA-TP-2281 ] p 31 N84-17165

NASA Aircraft Controls Research, 1983

[NASA-CP-2296} p 58 N84-20567

Simulation studies of time-control procedures for the

advanced air traffic control system

[NASA-TP-2493] p 30 N85-32101

AIRCRAFT HAZARDS

An Assessment of Technology for Turbojet Engine Rotor

Failures

INASA-CP-2017} p 41 N76-10065

Proceedings of the 2rid Annual Workshop on

Meteorological and Environmental Inputs to Aviation

Systems

[NASA-CP-2057] p 159 N79-17413

Aircraft icing

[NASA-CP-2086] p 12 N79-23912

Lightning Technology: Proceedings of a technical

symposium

{NASA-CP-2128] p 161 N80-21927

Simulator study of vortex encounters by a twin-engine,

commercial, jet transporf airplane

[NASA-TP-1966] p 57 N82-19225

NASA/MSFC FY-83 Atmospheric Research Review

{NASA-CP-2288] p 165 N83-36587

Statistical analysis of direct-strike lightning data (1980

to 1982)

{NASA-TP-2252] p 167 N86-24090

AIRCRAFT INSTRUMENTS

Measurement of aircraft speed and altitude

{NASA-RP-f0461 p 34 N80-24296

Simulator study of conventional general aviation

instrument displays in path-following tasks with emphasis

on pilot-induced oscillations

[NASA-TP-17761 p 39 N81-14997

Flight evaluation of a simple total energy-rate system

with potential wind-shear application

I NASA-TP-18541 p 39 N81-24058

Simulator evaluation of separation of display parameters

in path-followiog tasks

[NASA-TP-19151 p 39 N81-33203

Restructurable Controls

INASA-CP-2277] p 57 N83-33896

Simulator study of pilot-aircraft-display system response

obtained with a three-dimensional-box pictorial display

INASA-TP-21221 p 40 N84-f3182

AIRCRAFT LANDING

Validation of a Flexible Aircraft Take-Off and Landing

Analysis {FATOLA)

[NASA-TP-10251 p 31 N78-10049

Effects of landing approach methods and separation

intervals on single runway landing capacity

[ NASA-TP-1112} p29 N78-13029

Effect of winglets on a first-generation jet transport wing.

4: Stability characteristics for a full-span model at Mach

0.30

NASA-TP-1119 ] p 7 N78-17997

Development of systems and techniques for landing an

aircraft using onpoard television

NASA-TP-1171 ] p 32 N78-20114

Ground distance covered during airborne horizontal

deceleration of an airplane

NASA-TP-1157 } p32 N78-20115

Flight investigation of piloting techniques and crosawind

limitations using a research type orosswind landing gear

NASA-TP-1423} p 12 N79-23012

Effect of image tilt of a virtual image display on simulated

transport touchdown performance

NASA-TP-1520} p 33 N79-33189

Landing approach airframe noise measurements and

analysis

NASA-TP-1602] p 2 N80-15028

Application of the concept of dynamic trim control to

automatic landing of carrier aircraft --- utilizing digital

feedforaward control

[NASA-TP-1512] p 55 N80-19126

Simulation comparison of a decoupled longitudinal

control system and a velocity vector control wheel steering

system during landings in wind shear

[NASA-TP.1734] p 56 N81-12109

Flight-test evaluation of STOL control and flight director

concepts in a powered-lift aircraft flying curved

decelerating approaches

[NASA-TP-1641} p 56 N81-19131

Analysis and Monte Cado simulation of near-terminal

aircraft flight paths

{NASA-TP-1997} p 31 N82.23233

Planar equations of rollout motion for an aircraft with

free or steerable landing gears

[NASA-TP-1984] p 35 N82-23244

Evaluation of g seat augmentation of fixed-base/moving

base simulation for transport landings under two visually

imposed runway width conditions

[NASA-TP-21351 p 36 N83-22191

Simulator study of flight characteristics of a large

twin-fuselage cargo transport airplane during approach and

landing

[NASA-TP-2183] p 57 N84-12190

Flight-test of the glide-slope track and flare-control laws

for an automatic landing system for a powered-lift STOL

airplane

[NASA-TP-2128} p 57 N84-13198

Total energy-rate feedback for automatic glide-slope

tracking during wind-shear penetration

|NASA-TP-2412| p 58 N85-23801

AIRCRAFT MANEUVERS

Improvement of maneuver aerodynamics by spanwise

blowing

[NASA-TP-1065} p 7 N78-14997

Sonic-boom wave-front shapes and curvatures

associated with maneuvering flight

[NASA-TP-1611} p 13 N80-14045

Theory for computing the size and shape of a region

of influence associated with a maneuvering vehicle

{NASA-TP-1648] p 15 N80-24261

Pseudosteady-state analysis of nonlinear aircraft

maneuvers

{NASA-TP-1758J p 56 N81-13065

A computer technique for detailed analysis of mission

radius and maneuverability characteristics of fighter

aircraft

[NASA-TP-1837} p 17 N81-20026

Application of a performance modeling technique to an

airplane with variable sweep wings

{NASA-TP-1855} p 35 N81-24048

Wave drag as the objective function in transonic fighter

wing optimization

[NASA-TP-2265] p 23 N84.17127

Body and canard effects on an attached-flow maneuver

wing at Mach 1.62

{NASA-TP-22491 p 23 N84-16163

A-9
AIRCRAFT MODELS SUBJECT INDEX

AIRCRAFT MODELS

Longitudinal aerodynamic characteristics of a fighter

model with a close-coupled canard at Mach numbers from

0.40 to 1.20

lNASA-TP-12061 p 53 N78-27136

Fluctuating loads measured on an over-the-wing

supersonic iet model

INASA-TP-1366] p 186 N79-16641

Low-speed wind-tunnel parametric investigation of flight

spoilers as trailing-vortex-alleviation devices on a transport

aircraft model

INASA*TP-1419} p 11 N79-22038

Computer formulations of aircraft models for simulation

studies

INASA-TP-14701 p 2 N79-23008

Similitude requirements and scaling relationships as

applied to model testing

INASA-TP-1435] p 33 N79-30176

Effect of wingleta on a first.generation iet transport wing.

6: Stability charectenatics for a full-span model at subsonic

speeds --- conducted in Langley 8 foot transonic pressure

tunnel

{NASA-TP-1330] p 12 N80-10101

Fuselage and nozzle pressure diatnbutions on a

1 / 12-scale F- 15 propulsion model at transonic speeds ---

conducted in langley 16 foot transonic tunnel

JNASA-TP-1521 } p 13 N80-11036

Wind-tunnel/flight correlation study of aerodynamic

characteristics of a large flexible supersonic cruise airplane

CXB-70-t), 1: Wind-tunnel tests of a 0.03-scale model

at Mech numbers from 06 to 2.53

INASA-TP-1514J p 33 N80-11068

Determination of airplane model structure from flight data

by using modified stepwise regression

INASA-TP-1916} p 56 N82-t0041

determination of airplane model structure from flight data

using splines and stepwise regression

[NASA-TP-2126J p 57 N83-19758

Vortex Flow Aerodynamics. volume 1

[NASA-CP-2416-VOL-1 I p 28 N8S-27190

AIRCRAFT NOISE

Measurements of the tonal component of cavity noise

and comparison wffh theo_ --- aircraft noise

[NASA-TP-10131 p 185 N78-12800

Prediction of ground effects on sircraff noise

[NASA-TP-11041 p 186 N78-17823

Study of the use of a nonlinear, rate-limited filter on

pilot control signals

INASA-TP-1147] p 53 N78-20142

Optimal guidance and control for investigating aircraft

noise-impact reduction

INASA-TP-12371 p 53 N78-23100

Helicopter Acoustics

INASA-CP-2052-PT-1] p 186 N78-32816

Helicopter Acoustics, part 2 --- conferences

[NASA-CP-2052-PT-2} p 186 N79-10843

Noise transmission through flat rectangular panels into

a closed cavity --- light aircraft noise

tNASA-TP-1321 ] p 186 N79-14874

Variability of annoyance response clue to aircraft noise

INASA-TP-1335] p 186 N79-18687

Effects of duration and other noise characteristics on

the annoyance caused by aircraft-flyover noise

{NASA-TP-13861 p t86 N79-20832

Statistical comparisons of aircraft flyover noise

adjustment procedures for different weather conditions

[NASA-TP-1430} p 187 N79-24773

Effects of road traffic background noise on judgments

ot individual airplane noises

l NASA-TP- 1433 ] p 148 N79-28796

Laboratory study of annoyance to combined airplane

and road-traffic noise

INASA-TP-14781 p 148 N79-32743

A closed-form solution for noise contours

tNASA-TP-14321 p 187 N80-tt869

Effect of noise spectra and a listening task upon

passenger annoyance in a helicopter interior no_se

environment

INASA-TP-1590J p 171 N80-13769

Effects of sound level fluctuations on annoyance caused

by aircraft-flyover noise

INASA-TP-1576J p 187 N80-13880

Evaluation of helicopter noise due to b blade-vortex

interaction for five tip configurations --- conducted in the

Langley V/STOL tunnel

[NASA-TP-t608J p 187 N80-14840

Landing approach airframe noise measurements and

analysis

INASA-TP-1602J p 2 Na0-tf028

Theo*'etical predtctlon of nonlinear propagation effects

on noise signatures generated by subsonic or supersonic

propeller or rotor-blade tips

INASA-TP-1660] p 14 N80-22265

General Aviation Propulsion

INASA'CP'21261 p 46 N80-22327

Annoyance due to multiple airplane noise exposure

NASA-TP-1706 p 149 N80-28946

Effects of conversation interference on annoyance due

to aircraft noise

NASA-TP-1712 p 149 N80-29911

Assessment of ground effects on the propagation of

aircraft noise: The T-38A flight experiment

NASA-TP-1747 p 187 N81-14788

Subjective field study of response 1o impulsive helicopter

noise

NASA-TP-1833 p 187 N81-21873

Airframe noise of a small model transport aircraft and

scaling effects --- Boeing 747

NASA-TP-1858 p 188 N81-22832

Flight test of pure-tone acoustic source --- aircraft

noise

NASA-TP-1898 p 188 N81-33945

Effects of activity interference on annoyance due to

aircraft noise

NASA-TP-t938 p 149 N82-12654

Effects of repetition rate and impulsiveness of simulated

helicopter rotor noise on annoyance

NASA-TP-1969 p 150 N82-19707

Noise transmission loss of aircraft panels using acoustic

intensity methods

[NASA-TP-2046] p 188 N8;=.3t069

Supersonic jet noise generated by large scale

instabilities

[NASA-TP-20721 p 188 N82.34189

Flight effects of fan noise

[NASA-CP-2242J p 189 N83-10883

A new measurement method for separating airborne and

structureborne noise radiated by aircraft type panels

[NASA-TP-2079] p 189 N83-11838

Multiple-event airplane noise annoyance

[NASA-TP-2101} p 150 N83-16951

Residents' annoyance responses to aircraft noise

events

|NASA-TP-2121] p 189 N83-34713

Evaluation of ride quality prediction methods for

helicopter interior noise and vibration environments

[NASA-TP-226t] p 172 N84o20155

Annoyance caused by propeller airplane flyover noise

[NASA-TP-23561 p 190 NS4-32124

Fluctuating pressures on fan blades of a turbofan engine,

flight test investigation

INASA-TP-2381] p 190 N85-19790

Effects of propeller rotation direction on airplane interior

noise levels

[ NASA-TP-2444I p t90 N85-30767

Consideration of some factors affecting low-frequency

fuselage noise transmission for propeller aircraft

[NASA.TP-2552] p 191 N86-24393

Acoustic treatment of the NASA Langley 4- by 7-meter

tunnel: A feasibility study

[NASA-TP-2563] p 191 N86-31337

AIRCRAFT PARTS

Fundamentals of Gas Turbine combustion

[NASA-CP-20871 p 44 N79-25016

Analytical investigation of the landing dynamics of a large

airplane with a load-control system in the main landing

gear

[NASA-TP-t555] p 33 N80-13025

AIRCRAFT PERFORMANCE

Agricultural aviation research

{NASA-CP-2025J p 1 N78-12999

Study of the use of a nonlinear, rate-limited filter on

pdot control signals

[NASA-TP-11471 p 53 N78-20142

Performance evaluation method lor dissimilar aircraft

designs --- using the square of the wing span for

nondimensional comparisons of aerodynamic

characteristics

[NASA-RP-1042J p 2 N79-30139

Parametric study of variation in cargo-airplane

performance related to progression from current to

spanioader designs

[NASA-TP-1625] p 34 N80-21318

Full-scale wind tunnel-investigation of the Advanced

Technology Light Twin*Engine airplane (ATLIT) --- Langley

full scale tunnel

INASA-TP-1591] p 14 N80-22266

Theory for computing the size and shape of a region

of influence associated w_th a maneuvering vehicle

[NASA-TP-1648] p 15 N80-24261

Subsonic aircraft: Evolution and the matching of size

to performance

[NASA-RP-1060I p 2 N80-29245

Application of a pedormance modeling technique to an

airplane with variable sweep wings

[NASA-TP-1855] p 35 N81-24048

Some design considerations for solar-powered aircraft

{NASA-TP-t675] p 36 N82-32350

KC-135 Winglet Program Review

lNASA-CP-2211 ] p 24 N84-27686

AIRCRAFT PILOTS

Airline pilot scan patterns during simulated tLS

approaches

INASA-TP-1250} p 171 N79-19682

AIRCRAFT POWER SUPPLIES

Advanced secondary power system for transport

aircraft

[NASA-TP-2463J p 52 N85-28944

AIRCRAFT RELIABILITY

Systems reliability issues for future aircraft

{NASA-CP-003J p 175 N77-22808

AIRCRAFT SAFETY

Aircraft Safety and Operating Problems --- conference

[NASA-SP-416] p 28 N77-1808t

Lightning protection of aircraft

[NASA-RP-tO08| p 29 N78-11024

Proceedings: Fourth Annual Workshop on

Meteorological and Environmental Inputs to Aviation

systems

[NASA-CP-2139] p 162 N81-14555

The 1980 Aircraft Safety and Operating Problems, part

1

{NASA-CP-2170-PT-lJ p 29 N81-19035

Crash tests of four low-wing twin-engine airplanes with

truss-reinforced fuselage structure

[NASA-TP-2070] p 131 N83-t0442

Summary Proceedings of a Wind Shear Workshop

[NASA-CP-2270] p 165 N83-25265

Crash tests of three identical low-wing single-engine

airplane

[NASA-TP-2190] p 30 N83-34921

Meteorological and Environmental Inputs to Aviation

Systems

[NASA-CP-2388J p 166 N86-11735

AIRCRAFT SPECIFICATIONS

Helicopter Handling Qualities

[NASA-CP-2219] p 30 N82-23208

NASA/aircraft industry standard specification for

graphite fiber toughened thermoset resin composite

material

[NASA-RP-t 142 ] p83 N85-26923

AIRCRAFT SPIN

Exploratory study of the effects of wing-leading-edge

modifications on the stall/spin behavior of a light general

aviation airplane

[NASA-TP-1589] p 33 N80-13026

Flight investigation of stall, spin and recovery

characteristics of a low-wing, single-engine, T-tail light

airplane

[NASA-TP-2427J p 37 N85-25248

AIRCRAFT STABILITY

Effect of winglets on a first-generation jet transport wing.

4: Stability charactenstics for a full-span model at Mach

0.30

[NASA-TP-1119 ] p7 N78-t 7997

A flight investigation of the stability, control, and handling

qualities of an augmented jet flap STOL airplane

INASA-TP.1254] p 53 N78-26151

Flight-determined stability and control derivatives for the

F-111 Tact research aircraft

[NASA-TP-1350] p 54 N79-10068

Maximum likelihood method for estimating airplane

stability and control parameters from flight data in

frequency domain

INASA-TP-1637] p 55 N80-24323

An analytical study of the longitudinal response of

airplanes to positP.,e wind shear

[NASA-TP-1765} p 56 N81-20082

An assessment of the capability to calculate tilting

prop-rotor aircraft performance, loads and stability

INASA-TP-2291J p 37 N84-19333

Relative control effectiveness technique with application

to airplane control coordination

(NASA-TP-2416J p 37 N85-23753

AIRCRAFT STRUCTURES

Recent Advances in Structures for Hypersonic Flight,

part 1 --- conferences

INASA-CP-2065-PT-1 ] p 128 N79-21422

Evaluation of approximate methods for the prediction

of noise shielding by airframe components

[NASA-TP-fO04J p 46 N80-15129

Selected NASA research in composite Materials and

structures

{ NASA-CP-2142J p 80 N80-28436

Supersonic Cruise Research 1979, part 2 --- airframe

structures and matenals, systems integration, economic

analysis

[NASA-CP-2108-PT-2J p 3 N81-18005

Noise transmission loss of aircraft panels using acoustic

intensity methods

[NASA-TP-2046] p 188 N82-31069

Flightweight radiantly and actively cooled panel:

Thermal and structural performance

[NASA-TP-2074t p 131 N83-11513

Advanced Materials Technology

[NASA-CP-2251 } p 79 N83-12147

A-10
SUBJECT INDEX AIRSPEED

Determination of airplane model structure from flight data

using splines and stepwise regression

[NASA-TP-2126] p 57 N83-19758

Standard tests for toughened resin composites, revised

edition

[NASA-RP-1092-REV} p 82 N83-31730

Failure Analysis and Mechanisms of Failure of Fibrous

Composite Structures

[NASA-CP-2278] p 82 N83-33957

ACEE Composite Structures Technology: Review of

selected NASA research on composite materials and

structures

[NASA-CP-2321] p 83 N84-29969

Quest for performance: The evolution of modern

aircraft

[NASA-SP-468] p 5 N85-32089

Full.Scale Transport controlled Impact Demonstration

[NASA-CP-2395] p 135 N86-21933

AIRCRAFT SURVIVABILITY

Restructurable Controls

[NASA-CP-22771 p 57 N83-33896

AIRCRAFT TIRES

Friction characteristics of three 30 by 11.5-14.5, type

8, aircraft tires with various tread groove patterns and

rubber compounds

[NASA.TP.t080] p 32 N78-13043

Behavior of aircraft antiskid braking systems on dry and

wet runway surfaces. A slip.velocity-controlled,

pressure-bias-modulated system

[NASA-TP-1051] p 33 N80-12084

Wear, friction, and temperature characteristics of an

aircraft tire undergoing braking and cornering

[NASA-TP-1569] p 29 N80-13013

Tire stiffness and damping determined from static and

free-vibration tests --- aircraft tires

[NASA-TP-1671] p 29 N80.27302

Static and yawed-roiling mechanical properties of two

type 7 aircraft tires

[NASA-TP-1863] p 130 N81-24471

Behavior of aircraft antiskid braking systems on dry and

wet runway surfaces: Hydromechanioally controlled

system

[NASA-TP-1877] p 35 N81.30112

Dynamics of aircraft antiskid braking systems .--

conducted at the Langtey aircraft landing loads and traction

facility

[NASA-TP-1959] p 35 N82-18204

Tire tread temperatures during antiskid braking and

cornering on a dry runway

[NASA-TP-2009] p 35 N82-24193

Temperature distribution in an aircraft tire at low ground

speeds

[NASA-TP-2195] p 132 N83-33217

A study of the cornering forces generated by aircraft

tires on a tilted, free-swiveling nose gear

[NASA-TP-2481] p 135 N86-11522

AIRCRAFT WAKES

Wake Vortex Minimization

[NASA-SP-409] p 6 N78-12017

A Scanning laser-velocimeter technique for measuring

two-dimensional wake-vortex velocity distributions ---

Langtey Vortex Research Facility

[NASA-TP-1661 ] p 114 N80-24594

Simulator study of vortex encounters by a twin-engine,

commercial, jet transport airplane

[NASA-TP-1966] p 57 N82-19225

Analysis of noise measured from a propeller in a wake

[NASA-TP-2358] p t 90 N85-t 1788

Vortex wake alleviation studies with a vanable twist

wing

[NASA-TP-2442] p 5 N86-16187

Directivity and trends of noise generated by a propeller

in a wake

[NASA-TP-2609] p 191 N86-31341

AIRFOIL PROFILES

Low-speed aerodynamic characteristics of a

16-percant-thick variable-geometry airfoil designed for

general aviation applications

[NASA-TP-13241 p 10 N79-14018

Approximation concepts for numerical airfoil

optimization

[NASA-TP-t370J p 11 N79-18915

Experimental investigation of three helicopter rotor

airfoils designed analytically --- in the Langley 6 by 19

inch and 6 by 28 inch transonic wind tunnels

[NASA-TP-1396] p 11 N79-22037

Classical aerodynamic theory

[NASA-RP-1050] p 13 N80-15033

Wind-tunnel results for a modified 17-percent-thick

low-speed airfoil section

[NASA-TP-1919] p 18 N82-11033

Wind-tunnel investigation of the effects of blade tip

geometry on the interaction of torsional loads and

performance for an articulated helicopter rotor

[NASA-TP-lg26J p 18 N82-13107

Optimization and performance calculation of

dual-rotation propellers

[NASA-TP-19481 p 3 N82-14049

Computer program for aerodynamic and blading design

of multistage axial-flow compressors

[NASA-TP-1946] p 49 N82-15039

Low-speed aerodynamic characteristics of a

17-percent-thick medium speed airfoil designed for general

aviation applications

[NASA-TP-t786J p 20 N83-16290

Experimental investigation of a t0-percent-thick

helicopter rotor airfoil section designed with a viscous

transonic analysis code

[NASA-TP-1864] p 21 N83-30389

AIRFOILS

Dynamic stall experiments on the NACA 0012 airfoil

[NASA.TP-tl00I p 7 N78-17000

Numerical study of transonic flow over oscillating airfoils

using the full potential equation

[NASA.TP-t120J p 8 N78-21055

Application of shock tubes to transonic airfoil testing

at high Reynolds numbers

[NASA-TP-1268| p 10 N79-12013

Advanced technology airfoil research, volume 1, part 2

[NASA.CP.2045.PT.2] p 2 N79-19989

Advanced Technology Airfoil Research, volume 1, parr

1 -.- conference on development of computational codes

and test facilities

[NASA-CP-2045-PT-1] p 11 N7g-20030

Onset of condensation effects with an NACA 0012-64

airfoil tested in the Langley 0.3.mater transonic cryogenic

tunnel

[NASA-TP-1385J p 12 N79-22043

Advanced technology airfoil research, volume 2 ---

conferences

[NASA-CP-2046] p 14 N80-21283

Compariscn of elastic and elastic-plastic structural

analyses for cooled turbine blade airfoils

[NASA-TP-t679J p 129 N80-27719

Aerodynamic characteristics of three helicopter rotor

airfoil sections at Reynolds number from model scale to

full scale at Mach numbers from 0,35 to 0,90 --- conducted

in Langley 6 by 28 inch transonic tunnel

{NASA-TP.1701] p 15 N80-32333

Mean-flow and turbulence measurements in the vicinity

of the trailing edge of an NACA (63 sub 1)-012 airfoil

[NASA-TP-1845] p 109 N81-23410

Low-speed aerodynamic characteristics of a

17-percent-thick medium speed airfoil designed for general

aviation applications

[NASA-TP-1786] p 20 N83.16290

Design and experimental results for a flapped

natural-laminar-flow airfoil for general aviation

applications

[NASA-TP-1865] p 21 N83-30386

Wind-tunnel investigation of leading-edge thrust on

arrow wings in supersonic flow

[NASA-TP-2167I p 21 N83-31577

Airfoil interaction with impinging vortex

[NASA-TP-2273J p 23 N84-18159

Formulation of blade-flutter spectral analyses in

stationary reference frame

{NASA-TP-2296J p 51 N84-20562

Advanced aerodynamics, Selected NASA research

[NASA-CP-22081 p 4 N84-27660

Two-dimensional aerodynamic characteristics of three

rotorcraft airfoils at Mach numbers from 0.35 to 0.90

[NASA-TP-2000] p 24 N84-28743

Static and dynamic pressure measurements on a NACA

0012 airfoil in the Ames High Reynolds Number Facility

[NASA-TP-2485] p 26 N85-27823

Vortex wake alleviation studies with a variable twist

wing

[NASA-TP-2442] p 5 N86-16187

The application to airfoils of a technique for reducing

orifice-induced pressure error st high Reynolds numbers

[NASA-TP-2537] p 27 N86-20351

Studies of condensation effects on airfoil testing in the

Langley 0 3-meter transonic cryogenic tunnel

INASA-TP-2509] p 113 N86-20720

R4 airfoil data corrected for sidewall boundary-layer

effects in the Langley 0 3-meter transonic cryogenic

tunnel

[NASA-TP-2565] p 28 N86-24662

Experimental evaluation of two turning vane designs for

high-speed corner of 0.1-scale model ol NASA Lewis

Research Center's proposed altitude wind tunnel

[NASA.TP-2570] p 60 N86-28101

AIRFRAME MATERIALS

An integrated computer procedure for sizing composite

airframe structures

[NASA-TP-1300] p 178 N79-17580

Preliminary design procedure for insulated structures

subjected to transient heating

[NASA-TP-1534] p 128 N80-12438

Supersonic Cruise Research 1979, part 2 --- airframe

structures and materials, systems integration, economic

analysis

[NASA-CP-2108-PT-2J p 3 N81-18005

Fabrication and evaluation of brazed titanium-clad

borsic/aluminum skin-stringer panels

{NASA-TP-1674 } p82 N83-28098

Full-scale crash-test evaluation of two load-limiting

subfloors for general aviation airframes

[NASA-TP-2380] p 134 N85-13267

AIRFRAMES

Airflow and thrust calibration of an F100 engine, S/N

P68005g, at selected flight conditions

[ NASA-TP-106g] p42 N78-21112

Aerothermal performance of rad{atively and actively

cooled panel at Mach 6.6

{NASA-TP-1595] p 107 N80-13402

Landing approach airframe noise measurements and

analysis

[NASA-TP-1602J p 2 N80-15028

Airframe noise of a small model transport aircraft and

scaling effects --- Boeing 747

[NASA-TP-1858] p 188 N81-22832

Experimental study of noise reduction for an unstiffened

cylindrical model of an airplane fuselage

[NASA-TP-1964] p 188 N82-14879

Gain selection method and model for coupled propulsion

and airframe systems

|NASA.TP.2067] p 57 N83.11139

Expanded operational capabilities of the Langley Mach

7 Scramjef test facility

[NASA-TP-2186] p 60 N83-36039

Survey of NASA research on crash dynamics

[NASA-TP-2298] p 133 N84-21901

Validation of an Active Gear, Flexible Aircraft Take-off

and Landing analysis (AGFATL)

[NASA-TP-2353] p 37 N84-32378

A formulation of rotor-airframe coupling for design

analysis of vibrations of helicopter airframes

[NASA-RP-1089] p 133 N84.33832

AIRPORT PLANNING

Planning for airport access: An analys_s of the San

Francisco Bay area

[NASA-CP-2044] p 198 N79.10942

A new theory for rapid calculation of the ground pattern

of the incident sound intensity produced by a maneuvering

jet airplane

[NASA-TP.t733] p 15 N80-32334

AIRPORTS

Precision positional data of general aviation air traffic

in terminal air space

{NASA-RP-1020| p 1 N78-25048

Analysis and Monte Carlo simulation of near-terminal

aircraft flight paths

[NASA-TP-1997 ] p31 N82-23233

Airport/Community Noise

[NASA-CP-2241] p 188 N82-31070

Standard tests for toughened resin composites, revised

edition

{NASA-RP-1092-REV] p 82 N83-31730

Residents' annoyance responses to aircraft noise

events

INASA-TP-2121J p 189 N83-34713

NASA/MSFC FY-83 Atmospheric Research Review

[NASA-CP-2288] p 165 N83-36587

AIRSHIPS

Vehicle concepts and technology requirements for

buoyant heaw-lift systems

[NASA-TP-1921] p 35 N81-31185

AIRSPEED

A flight evaluation of a trailing anemometer for low-speed

calibrations of airspeed systems on research aircraft

|NASA.TP-t 135] p 32 N78-18044

Miniature flow-direction and airspeed sensor for

airplanes and radio controlled models in spin studies

{ NASA-TP-1467 | p 38 N79-23081

Science and Technology of Low Speed and Motodess

Flight Third International Symposium

{L-12973} p 2 N79-27070

Measurement of aircraft speed and altitude

[NASA-RP-tO46J p 34 N80-24296

Development and flight test results of an autothrottle

control system at Msch 3 cruise

[NASA-TP-1621] p 56 N80-26328

Subsonic tests of an sll-flush-pressure-onfice air data

system

[NASA-TP-1871] p 39 N81-26144

Design criteria for flight.path and airspeed control for

the approach and landing of STOL aircraft

[NASA-TP-1911 ] p 57 N82-20187

An experimental and theoretical investigation of

deposition patterns from an agricultural airplane

[NASA-TP-23481 p 25 N84.33379

A-11
AITKEN NUCLEI SUBJECTINDEX

AfTKEN NUCLEf

Condensation nuclei (Altken Particle) measurement

system used in NASA global atmospheric sampling

program

INASA-TP-14151 p 148 N79 18479

ALABAMA

The MSFC/UAH Data Management Symposium

INASA-CP-2040] p 177 N78 74659

ALBEDO

A tulorial solution Io scattering of radlalion in a lhirl

atmosphere bounded below by a diffusely reflecting.

absorbing surface

INASA-TP-2077] p 154 N82-33918

Comparative accuracy of the Atbedo, transmission and

absorption for selected radiative transfer approximations

{NASA-RP-1160] p 156 N86-22022

Surface radiation budget for climate applications

{NASA-RP-1169] p 167 N86-28574

ALGAE

Charactanstic vector analysis of mflechon ratio spectra:

New tachmque for analysis Of ocean color data

[NASA-TP-2428] p 143 N85-23237

ALGEBRA

A cracked orthotropic sheet stiffened by a semiqnfinite

orthotrOpiC sheet

[NASA-TP-2455] p I34 N85-32339

ALGORITHMS

An alternating direction implicit method for the Control

Data STAR-100 vector computer

[NASA-TP-12821 p 182 N78-31836

Algohthm for fixed-range optimal trajectories

[NASA-TP-t565J p 30 N80-28329

Development and test results of a flight management

algohlhm for fuel conservative descents in a time-based

metered traffic environment

l NASA-TP-1717 J p 39 N80-33404

Temporal and spatial inconsistencies of time _piit

finite-difference schemes

(NASA-TP-1790| p 182 N81-22754

Reduced order feedback control equations for linear time

and frequency domain analysis

INASA-TP-faf8J p 72 N81-25140

An algorithm for minimum-cost set-point ordering in a

cryogenic wind tunnel

[NASA-TP-1923) p 59 N82-t 1090

NOSS altimeter algorithm specifications

INASA-RP-1083] p 168 N82 16683

Establishment of a rotor model basis

INASA-TP-2026] p 36 N82-29311

User's guide for the Solar Backscattered Ultraviolet

(SBUV) instrument first year ozone-S data set

INASA-RP-10951 p 164 N82-29826

Studies of implicit and explicit solulior_ techniques in

transient thermal analysis of struclures

[ NASA-TP-2038 ] p t f0 N82-31646

Acceleration of convergence of vector sequences

[NASA-TP-2193] p 182 N84-13885

A companson of two posit=on estimate algorithms that

usa ILS IDealizer and DME information Simulation and

flight test results

INASA-TP-2281 ] p 31 N84-17165

An algohthm for maximum likelihood estimation using

an efficient method for approximating sensitivities

[NASA-TP-2311 ] p58 N84-25717

Rational-spline approximation with automatic tension

adjustment

INASA'TP'2366] p 182 N84-34204

Compahson of numerical techniques for integration of

stiff ordinary differential equations artsmg in combustion

chemistry

[NASA-TP-2372] p 51 N85-10065

Algorithm for astronomical, extended source

signal-to-noise radio calculations

INASA-TP-2396] p 202 N85-t2833

Algorithm for astronomical, point source, s_g.a_ to noise

ratio calcufations

NASA-TP-2397] p 202 N85-12834

An evaluation and comparison of verbcaq prone data

from the VtSSR Atmospheric Sounder (VAS)

NASA-TP-2426J p 166 N85-16351

Piloted simulation of an algorithm for onboard control

of time-optimal intercept

NASA-TP-2445] p 58 N85-28949

An image compression survey and algonthm switching

based on scene acbvity

NASA-TP-2458] p 27 N85-33106

The algorithms for rational spline interpolahon of

surfaces

NASA-TP-2536] p 183 N86-18060

A methodology for airplane parameter estimation and

confidence interval delerminatton m nonlinear estimahon

_roblems

NASA-RP-t153J p 58 N86-22579

Hy'orid routing technique for a fau4t-to[eratd, integrated

information network

[NASA-TP-2605] p 180 N86.27947

Solution of elliptic partial differential equatidns by fast

Poisson solvers using a local relaxation factor 1: One-step

method

I NASA-TP-2529 t p 183 N86-28661

Physical and numerical sources of computational

inefficiency in integration of chemical kinetic rate

equations: Etiology, treatment and prognosis

I NASA-TP-2590} p 183 N86-28662

ALKALINE BATTERIES

Control of volume resistivity in inorganic organic

separators

I NASA-TP-1439] p 84 N79-22246

Performance of alkaline battery cells used in emergency

locater transmitters

INASA-TP'2277] p 103 N84-20759

ALL-WEATHER LANDING SYSTEMS

Helical automatic approaches of helicopters with

microwave tanding systems

[NASA-TP-2109t p 31 N83-18704

ALLOYS

Effects of thermomechanical processing on strength and

toughness of iron - 12-percent-nickel - reactive metal alloys

af -196 C

[NASA-TP-1308] p 86 N78-31213

Study of austanitic stainless steel welded with low alloy

steel filler metal --- tensile and impact strength tests

[NASA-TP-1460] p 87 N79-28288

Elastic-plastic finite-element analyses of thermally

cycled double-edge wedge specimens

tNASA-TP-19731 p 130 N82-20566

A study of production of misibildy gap alloys with

controlled structures

[NASA-TP-21441 p 195 N83-21991

ALTERNATING DIRECTION IMPLICIT METHODS

An alternating direction implicit method for the Control

Data STAR-100 vector computer

[NASA-TP-t282J p 182 N78-31836

ALTIMETERS

Remote sensing of Gulf Stream using GEOC-3 radar

altimeter

tNASA-TP-1209J p 167 N78-21737

The rote of satellite altimetry in climate studies

{NASA-TP-15701 p 161 N80-16676

Geopotential Research Mission (GRM)

I NASA-CP-2390) p 155 N86-12852

ALTITUDE

MARS 1414 recorder environmental tests

INASA-TP-t709J p 115 N80-30716

ALTITUDE CONTROL

Pilot-model analys_s and simulation study of effect of

control 1ask desired control response

I NASA-TP-1140 } p53 N78-20143

Handbook on astronaut crew motion disturbances for

control system design --- in skylab

INASA-RP-t025} p 71 N79-27237

ALTITUDE TESTS

Altitude test of several afferbumor configurations on a

turbofan engine with a hydrogen heater to simulate an

elevated turbine discharge temperature

i NASA-TP-1068] p41 N78-11106

Altitude calibratidn of an F100, S/N P6800'63, turbofan

engine

I NASA-TP-1228] p 42 N78-23095

Experimental evaluation of twO turning vane designs for

high-speed corner of 0 l-scale model of NASA Lewis

Research Centar's proposed altitude wind tunnel

[NASA-TP-2570] p 60 N86-28101

ALUMINUM

Tensile stress-strain behavior of boron/aluminum

laminates

[ NASA-TP-1117] p79 N78-18135

Effects of fabrication and joining processes on

compressive strength of boron/aluminum and

borsic/aluminum structural panels

[NASA-TP-1121 I p 80 N78-20256

Friction and wear of selected metals and alloys in sliding

contact with AISI 440 C stainless steel in liquid methane

and in liquid natural gas

INASA-TP-ltS0J p 119 N78-20512

Wear of single-crystal silicon carbide in contact with

various metals in vacuum

INASA-TP-1198] p 92 N78-21295

Pressureless sintered Sialons with low amounts of

sintaring aid

1NASA-TP-12461 p 92 N78-25215

Low toxic corrosion inhibitors for aluminum in fresh

water

I NASA-TP-1279] p 86 N78-28226

Wear of aluminum and hypoeutectic aluminum-silicon

alloys in boundary-lubricated pin-on disk sliding

1NASA-TP-1442] p 87 N79-21184

Scanning-electron-microscope study of

normal-impingement erosion of ductile metals

I NASA-TP-1EO9] p 87 N80-16141

Mechanical impact tests of materials in oxygen effects

of contamination --- Teflon, stainless steel, and

aluminum

[NASA-TP-1571 ] p 97 N80-2t551

Mechanical property charactenzatidn of

Borsic/aluminum laminates at room and elevated

temperatures

[NASA-TP-1761 ] p 81 N81-16130

Experimental and analytical investigation of the fracture

processes of boron/aluminum laminates containing

notches

[ NASA-TP-2187] p 82 N83-33956

Cavitatidn pitting and erosion of aluminum 6061-T6 in

mineral od water

{NASA-TP-2146] p 123 N83-35400

Effects of chromium and aluminum on mechanical and

oxidation properties of iron-nickel-base superalloys based

on CG-27

[NASA-TP-2443] p 90 N85-21323

An electrochemical study of the corrosion behavior of

primer coated 2219-T87 aluminum

[NASA-TP-2459] p 90 N85-22662

Effect of low-velocity or ballistic impact damage on the

strength of thin composite and aluminum shear panels

[NASA-TP-2441 ] p 83 N85-26924

Abrasion behavior of aluminum and composite skin

coupons, stiffened skins and stiffened panels

representative of transport afrptane structures

[NASA-TP-2520] p 38 N86-13316

ALUMINUM ALLOYS

Characterization of large 2219 aluminum alloy hand

forgings for the space shuttle solid rocket booster

[NASA-TP-t383| p 87 N79-16950

Effects of geometec variables on rub characteristics of

Ti-6AI-4V

[NASA-TP-t835J p 88 N81-20245

Advanced Materials Technology

[NASA-CP-2251 ] p 79 N83-12147

Morphology of an aluminum alloy eroded by a jel of

angular particles impinging at normal incidence

[NASA-TP-2139J p 89 N83-24641

Fabncation and evaluation of brazed titanium-clad

Borsic/aluminum compression panels

[NASA-TP-1573] p 82 N83-28100

Time dependence of solid-particle impingement erosion

of an aluminum alloy

[NASA-TP-2169] p 89 N83-32908

Metallurgical characterization of the fracture of several

high strength aluminum alloys

[NASA-TP-1086] p 85 N84-11230

Galvanic coupling between D6AC steel, 6061-T6

aluminum. Inconel 718 and graphite-epoxy composite

material: Corrosion occurrence and prevention

[NASA-TP-2236] p 89 N84-13263

Fhction and wear behavior of aluminum and composite

airplane skins

INASA-TP-2262] p 37 N84-17175

Microstructure and orientation effects on properties of

discontinuous silicon carbide/aluminum composites

INASA-TP'2302] p 79 N84-26749

ALUMINUM BORON COMPOSITES

Fracture toughness of boron/aluminum laminates with

various proporfidns of 0 dog and plus or minus 45 deg

[NASA-TP-f 707 ] p81 N81-11115

Long-term thermal degradation and alloying constituent

effects on five boron/aluminum composites

[NASA-TP-1977] p 81 N82-22317

ALUMINUM OXIDES

Formulation of electrically conductive thermal-control

coatings

{NASA-TP-1218] p 78 N78-21216

Adsorption and chemical reaction of gaseous mixtures

of hydrogen chloride and water on aluminum oxide and

application to solid-propellant rocket exhaust clouds

[ NASA-TP-f 105] p84 N78-22188

Enhanced hydrophilicity of chlorided aluminum oxide

_articulatas

NASA-TP-13121 p 84 N79-12178

Effects of temperature, thermal exposure, and fatigue

on an alumina/aluminum composite

NASA-TP-1795] p 81 N81-14001

Plastic deformation at surface during unlubricated

sliding

NASA-TP-2036] p 122 N83-11496

Oxidation and emittance of superalloys in heat shield

applications

NASA-TP-2578J p 90 N86-26412

AMBIENT TEMPERATURE

MARS 1414 recorder environmental tests

NASA-TP-1709] p 115 N80-30716

Surface fatigue life and failure charactehstics of EX-53,

CBS 1000M. and AiSI 9310 gear materials

NASA-TP-25131 p 125 N86-12609

A-12
SUBJECT INDEX ANTISKID DEVICES

AMMONIA

DIAL with heterodyne detection including speckle noise:

Aircraft/shuttle measurements of O3, H20, and NH3 with

pulsed tunable CO2 lasers

[NASA-TP*17251 p 115 N80-30717

AMMONIUM CHLORIDES

Optical observations of unidirectional solidification in

microgravity

[NASA-TP-2110] p 88 N83-16492

AMORPHOUS MATERIALS

Friction and surface chemistry of some ferrous-base

metallic glasses

[NASA-TP-1991 ] p 88 N82-21301

Sliding induced crystallization of metallic glass

(NASA-TP-2140] p 88 N83-21110

AMPLITUDE MODULATION

Carrier-interference ratios for frequency sharing between

frequency-modulated

band television systems

[NASA-TP-f 264 ] p69 N78-28159

Stochastic analysis of spectral broadening by a free

turbulent shear layer

[NASA-TP-1815J p 188 N81-24854

ANALOG DATA

Instrument to average 100 data sets

(NASA-TP-10551 p 100 N78-11301

Magnetic Tape Recording for the Eighties

(NASA-RP-1075 J p 118 N82-29579

ANALYSIS (MATHEMATICS)

Studies of implicit and explicit solution techniques in

transient thermal analysis of structures

[NASA-TP-2038| p 110 N82-31646

A numerical simulation of three-dimensional flow in an

adaptive wall wind tunnel

[NASA-TP-2351 ] p 24 N84-28750

ANECHOIC CHAMBERS

Evaluation of approximate methods for the prediction

of noise shielding by airframe components

(NASA-TP-1004] p 46 N80-15129

Acoustic treatment of the NASA Langley 4- by 7-meter

tunnel: A feasibility study

[NASA-TP-25531 p 191 N86-31337

ANEMOMETERS

A flight evaluation of a trailing anemometer for low-speed

calibrations of airspeed systems on research aircraft

[NASA-TP-1135] p 32 N78-18044

Dynamic behavior of a beam drag-force anemometer

(NASA-TP-1687] p 114 N80-24595

The wedge hot-film anemometer in supersonic flow

[NASA-TP-2134] p 189 N83-30164

ANGLE OF ATTACK

Inviscid, nonediabatic flow fields over blunt, sonic corner

bodies for outer planet entry conditions by a method of

integral relations

[NASA-TP-1133] p 104 N78-18363

Miniature flow-direction and airspeed sensor for

airplanes and radio controlled models in spin studies

[NASA-TP-1467] p 38 N79-23081

Effects of fuselage forebody geometry on low-speed

lateral-directional characteristics of twin-tail fighter model

at high angles of attack

[NASA-TP-1592) p 13 N80-13002

Low-speed aerodynamic characteristics of a 13 percent

thick medium speed airfoil designed for general aviation

applications

(NASA-TP-1498J p 16 N81-12015

Experimental and theoretical aerodynamic

characteristics of two hypersonic cruise aircraft concepts

at Mach numbers of 2.96, 3.96, and 4.53

(NASA-TP-17671 p 16 N81-12021

Kinematic properties of the helicopter in coordinated

turns

( NASA-TP-t 7731 p 35 N81-22039

Wing-alone aerodynamic charactenstics for high angles

of attack of supersonic speeds

{NASA-TP-1889J p 18 N81-30087

Force and moment, flow-visualization, and

boundary-layer tests on a shuttle orbiter model at Mach

6

[NASA-TP-1952] p 16 N82-13106

Effects of wing-leading-edge modifications on a

full-scale, low-wing general aviation airplane: Wind-tunnel

investigation of high-angle-of-attack aerodynamic

characteristics --- conducted in Langley 30- by 60-foot

tunnel

(NASA-TP-2011 I p 4 N82-26217

Calculation of inviscid Itow over shuttle-like vehicles at

high angles of attack and comparisons with experimental

data

[NASA-TP-2103J p 110 N83-24808

Wind-tunnel free-flight investigation of a model of a

forward-swept-wing fighter configuration

[NASA-TP-22301 p 57 N84-17184

Experimental investigation of tangential blowing applied

to a subsonic V/STOL inlet

(NASA-TP-22971 p 23 N84-20493

Effect of aerodynamic and angle-of-attack uncertainties

on the blended entry flight control system of the Space

Shuttle from Mach 10 to 25

[NASA-TP-2283 j p 56 N84-23652

Effect of aerodynamic and angle-of-attack uncertainties

on the May 1979 entry flight control system of the Space

Shuttle from Mach 8 to 1 5

[NASA-TP-2365] p 69 N85-15778

Low-speed stability and control wind-tunnel

investigahons of effects of spanwise blowing on fighter

flight characteristics at high angles of attack --- Langely

12-tt low-speed tunnel and 30- by 60-It tunnel

( NASA*TP-2431 ] p 28 N85-23708

Performance and surge limits of a TF30-P-3 turbofan

engine/axisymmetric mixed-compression inlet propulsion

system at Mach 25

INASA'TP'2461 ) p 52 N85-25261

ANGULAR ACCELERATION

Experiments in sensing transient rotational acceleration

cues on a flight simulator

INASA-TP-1537) p 33 N80-10193

ANGULAR DISTRIBUTION

Joint research effort on vibrations of twisted plates,

phase 1: Final results

INASA-RP-1150] p 135 N86-t0579

ANGULAR MOMENTUM

Evaluation of a laboratory test model annular momentum

control device

[NASA-TP-1142] p 96 N78-18252

Flight investigation of stall, spin and recovery

characteristics of a low-wing, single-engine. T-tail light

airplane

{NASA-TP-2427] p 37 N85-25248

A stochastic model for particle impingements on orbiting

spacecraft

[NASA-TP-2550] p 184 N86-19095

ANIMALS

NASA Space Biology Program. Eighth annual

symposium's program and abstracts

(NASA-CP-2299| p 169 N84-18829

NASA Space Biology Program: 9th Annual

Symposium

(NASA-CP-2336] p 159 N85-26054

ANIONS

Flight comparison of the transonic agility of the F-111A

airplane and the F-111 supercritical wing airplane

[NASA-TP-13661 p 54 N79-13056

Recent Advances in Structures for Hypersonic Flight.

part 2

{NASA-CP-2065-PT-2) p 128 N79-21435

A unique facility for V/STOL aircraft hover testing *-*

Langley Impact Dynamics Research Facility

( NASA-TP-14731 p 59 N79-29199

Simulation of _ubncating behavior of a thioether liquid

lubricant by an electrochemical method

[NASA-TP-2316J p 95 N84-23764

ANISOTROPIC PLATES

An improved transverse shear deformation theory for

laminated antisotropic plates

[NASA-TP-19031 p 130 N82-11488

ANISOTROPY

Anisotropic friction and wear of single*crystal

manganese-zinc ferrite in contact with itself

[NASA-TP-1339] p t20 N79-10425

Anisotropic friction, deformation, and fracture of

single-crystal silicon carbide at room temperature

(NASA-TP-1525] p 93 N79-30380

ANNEALING

Annealing of radiation damage in 0.1- and

2-ohm-centimeter Silicon solar cells

[NASA-TP-1559J p 145 N79-33572

ANNIHILATION REACTIONS

Second quantization techniques in the scattering of

nonidentical composite bodies

(NASA-TP-2522J p 193 N86-21297

ANNUAL VARIATIONS

A comparative statistical study of long-term agroclimatic

conditions affecting the growth of US winter wheat:

Distributions of regional monthly average precipitation on

the Great Plains and the state of Maryland and the effect

of agroclimatic conditions on yield in the state of Kansas

I NASA-TP-1724 ] p 163 N81-22658

SAM 2 Measurements of the Polar Stratospheric

Aerosot, volume 2. April 1979 to October 1979

[NASA-RP-t088-VOL-21 p 153 N82-19734

ANNULAR DUCTS

Velocity gradient method for calulating velocities in an

axisymmetric annular duct

[NASA-TP-2029] p 20 N82-29270

ANNULAR FLOW

Laser anemometer measurements in an annular

cascade of core turbine vanes and comparison with

theory

[NASA-TP-2018) p 20 N82-26234

ANNULAR NOZZLES

Performance of a short annular dump diffuser using

suction*stabilized vortices at inlet Mach numbers to 0.41

[ NASA-TP-1194) p42 N78-20131

Performance of a vortex-controlled diffuser in an annular

swirl-can combustor at inlet Mach numbers up to 0.53

[NASA-TP-1452 J p 44 N79-22099

ANODES

Effect of anode-cathode geometry on performance of

the HIP-t hot ion plasma -- magnetic mirrors

[NASA-TP-1201 ] p 194 N78-21922

ANOMALIES

Thermal anomalies of the transmitter experiment

package on the communications technology satellite

(NASA-TP-1410] p 69 N79-21120

ANORTHOSITE

Lunar sample studies --- breccias basalts, and

anodhosites

INASA-SP-4181 p 204 N77-27053

ANTARCTIC REGIONS

SAM 2 Measurements of 1he Polar Stratospheric

Aerosol, volume 2 April 1979 to October 1979

{NASA-RP-1088-VOL-2J p 153 N82-19734

Antartic sea ice, 1973 1978: Satellite

passive-microwave observations

[NASA-SP*4591 p 168 N84-10718

ANTENNA ARRAYS

Large space systems technology, 1980, volume 1

[NASA-CP*2168] p 66 N81-19164

ANTENNA DESIGN

Large Space Systems Technology. 1979 --- antenna and

space platform systems conference

[NASA-CP-2118] p 66 N80-19145

Solar power satellite system sizing tradeoffs

[NASA-TP-1804] p 145 N81-18493

The microwave radiometer spacecraft: A design study

[NASA-RP-f079] p 73 N82-t6153

Large Space Systems Technology, part 2. 1981

[NASA-CP-2215-PT-2J p 66 N82-19257

Large Space Antenna Systems Technology, part 1

[NASA-CP-2269-PT-1 ) p 67 N83-26853

Analys_s of rectangular microstrip antennas

(NASA-TP-2276) p 100 N84-20735

Large Space Antenna Systems Technology, 1984

(NASA-CP-2368*PT-t ] p 67 N85-23813

Large Space Antenna Systems Technology, 1984

[NASA-CP-2368-PT-2] p 68 N85-23840

ANTENNA RADIATION PATTERNS

Diversity techniques for omnidirectional telemetry

coverage of the HiMAT research vehicle

(NASA-TP-1830} p 39 N81.20074

Analysis of rectangular microstrip antennas

(NASA-TP-2276] p 100 N84-20735

ANTENNAS

The 15th Aerospace Mechanisms Symposium

[NASA-CP-21811 p 130 Nat-22388

Large Space Systems Technology, part 2, 1981

(NASA-CP-2215-PT-2| p 66 N82-19257

SET1 science working group report

[ NASA-TP-22441 p 175 N84-22178

Reduction method for thermal analysis of complex

aerospace structures

[NASA-TP-23731 p 1t2 N85-18066

Decoupled and linear quadratic regulator control of a

large, flexible space antenna with an observer in the control

loop

[NASA-TP-24841 p 75 N86-16250

Application of the LQG/LTR technique to robust

controller synthesis for a large flexible space antenna

[NASA-TP-2560J p 75 N86-30800

Effects of model error on control of large flexible space

antenna with comparisons of decoupled and linear

quadratic regulator control procedures

[NASA-TP-2604] p 75 N86-30801

ANTHROPOMETRY

Anthropometric source book. Volume 1: Anthropometry

for designers

[NASA-RP-1024] p 172 N79-11734

ANTIFRICTION BEARINGS

Instability in Rotating Machinery

{NASA-CP-2409] p 126 N86-30160

ANTIMISTING FUELS

Full-Scale Transport controlled Impact Demonstration

lNASA-CP-2395j p 135 N88-21933

ANTIPROTONS

Ninteenth International Cosmic Ray Conference. OG

sessions, volume 2

[NASA-CP-2376-VOL-2] p 210 N85-34006

ANTISKID DEVICES

Behavior of aircraft antiskid braking systems on dry and

wet runway surfaces A slip-velocity-controlled,

pressure-bias-modulated system

[NASA-TP-1051 ] p 33 N80-12084

A-13
APOLLO APPLICATIONS PROGRAM SUBJECT INDEX

Behavior of aircraft antiskid braking systems on dr't and

wet runway surfaces: Hydromechenicatly controlled

system

INASA-TP-1877] p 35 N81-30112

Dynamics of aircraft antiskid braking systems ---

conducted at the Langley aircraft landing loads and traction

facility

[NASA.TP-195g] p 35 N82-18204

APOLLO APPLICATIONS PROGRAM

Skyiab: A chronology

[NASA-SP-4011 ] p 61 N78-25115

APOLLO FLIGHTS

Chariots for Apollo: A history of manned lunar

spacecraft

[NASA-SP-4205] p 62 N79-28203

APOLLO LUNAR SURFACE EXPERIMENTS PACKAGE

ALSEP termination report

NASA-RP-1036] p 199 N79-22979

APOLLO PROJECT

Apollo over the moon: A view from orbit

"NASA-SP-382] p 61 N78-21174

Moonport: A history of Apollo launch facilities and

operations

NASA-SP-4204] p 64 N79-12127

Chariots for Apollo: A history of manned lunar

spacecraft

NASA-SP-4205 J p 62 N79-28203

The Apollo spacecraft: A chronology volume 4, 21

January 1966 - 13 July 1974

NASA-SP*4009-VOL-4] p 98 N80-20437

Stages to Saturn: A technological history o1 the

Apollo/Saturn launch veh=ctes

NASA-SP-4206) p 72 N81-29154

APOLLO SOYUZ TEST PROJECT

The Apollo-Soyuz Test Project Medical report

[NASA-SP-411J p 170 N77-30735

Apollo-Soyuz test project, Volume 1: Astronomy, earth

atmosphere end gravity field, life sciences, and materials

processing

lNASA-SP-412] p 60 N78-17088

The partnership: A history of the Apolio-Soyuz test

project

[NASA-SP-4209] p 61 N7g-10074

Apotio-Soyuz test project, Volume 2: Earth observations

and photography

[NASA-SP-412-VOL-2} p 138 N80-10538

APOLLO SPACECRAFT

The Apollo spacecraft: A chronology volume 4, 21

January 1966- 13 July 1974

JNASA-SP-4009*VOL*41 p 98 N80-20437

APOLLO TELESCOPE MOUNT

An atlas of solar spectra between 1175 and 1950

angstroms recorded on Skyleb with the NRL's Apollo

telescope mount experiment

[NASA-RP-1069] p 209 N81-23004

APPLICATIONS OF MATHEMATICS

Inversion Methods in Atmospheric Remote Sounding

[NASA-CP-O04] p t5t N78-12586

APPROACH

Effects of landing approach methods and separation

intervals on single runway landing capacity

[ NASA-TP-1112 ] p29 N76-13029

Analysis of fuel-conservative curved decelerating

approach trajectories for powered-lift and CTOL jet

aircraft

( NASA-TP*1650] p2 N8O-t 9022

Simulator study of flight characteristics of a large

twin-fuselage cargo transport airplane during approach and

landing

{NASA-TP-2183] p 57 N84-12190

A comparison of two position estimate algorithms that

use ILS Iocalizer and DME information. Simulation and

flight test results

[NASA-TP-2281 ] p 31 N84-17165

A cockpit-display concept for executing a multiple

glide-slope approach for wake-vortex avoidance

[ NASA-TP-2386] p 40 N85-16869

Ground-based and in-fl=.ght simulator studies of flight

characteristics of a twin-fuselage passenger transport

airplane during approach and landing

[NASA-TP-2451 ] p 68 N85-34144

APPROACH AND LANDING TESTS (STS)

Orbiter landing loads math model description and

correlation with ALT flight data

[NASA-RP-10561 p 71 N80-16091

Simulator study of the effect of control-system time

delays on the occurrence of pdot-induced oscillations and

on pilot tracking performance with a space-shuttle-orbiter

configuration

TNASA-TP-1588) p 34 N80-21317

Dynamics stability derivatives of space shuttle orbiter

obtained from wind-tunnel and approach and landing flight

tests

INASA-TP-1634] p 55 N80-21336

Flight evaluation of stabilization and command

augmentation system concepts and cockpit displays during

approach and landing of powered-lift STOL aircraft

[NASA-TP-1551J p 56 N81-11044

Comparison of Space Shuttle Orbiter low-speed static

stability and control derivatives obtained from wind-tunnel

and approach and landing flight tests

[NASA-TP-1779] p 56 N81-I3066

APPROACH CONTROL

Ground-based and in-flight simulator studies of

low-speed handling characteristics of two supersonic

cruise transport concepts

[NASA-TP.1240] p 32 N78-27111

Heed-up transition behavior of pilots during simulated

low-visibility approaches

INASA-TP-1618) p 173 N80-26039

Heed-up transition behavior of pilots with and without

head-up display in simulated low-visibility approaches

[NASA-TP-1720] p 173 N81-13635

Cognitive issues in head-up displays

[NASA-TP-1711) p 173 N81-13636

Flight-test evaluation of STOL control and flight director

concepts in a powered-lift aircraft flying curved

decelerating approaches

NASA-TP-1641] p 56 N81-19131

Design criteria for flightpath and airspeed control for

the approach and landing of STOL aircraft

NASA-TP-1911J p 57 N82-20187

Helical automatic approaches of helicopters with

microwave landing systems

NASA-TP-2109] p 31 N83-18704

Automated rendezvous and docking: A parametric

study

NASA*TP-2314] p 74 N84-23677

APPROXIMATION

Applied Routh approximation

NASA-TP-1231 ] p 98 N78-22257

A distributed vortex method for computing the vortex

field of a missile

NASA-TP-1183] p 8 N78-25058

Approximation methods for combined thermal/structural

design

NASA-TP-1428} p 128 N79-25427

Evaluation of approximate methods for the prediction

of noise shielding by airframe components

NASA-TP-1004] p 46 N80-t512g

Solution of complex nonlinear problems by a generalized

application of the method of base and comparison

solutions with applications to aerodynamics problems

[NASA-TP-18571 p 17 N81-22019

Heavy ion transport in the straight ahead

approximation

[NASA-TP-2178] p 210 N83-2916g

An algorithm for maximum likelihood estimation using

an efficient method for approximating sensitivities

{NASA-TP-2311 I p 58 N84-25717

Rationel-spline approximation with automatic tension

adjustment

[NASA-TP-2366] p 182 N84-34204

Spline methods for approximating quantile functions and

generating random samples

[NASA-TP-238g] p t84 N65-16565

Comparative accuracy of the Albedo, transmission and

absorption for selected radiative transfer approximations

( NASA-RP-1160 ] p 156 N86-22022

ARC HEATING

Exploratory investigation of two resin-matrix composites

subjected 1o arc-tunnel heating

I NASA-TP-14291 p80 N79-23141

ARC MELTING

A mechanical property and stress corrosion evaluation

ol WM-ESR*VAR work strengthened and direct double

aged Inconel 718 bar material

INASA-TP-2634] p 68 N86-30753

ARCHITECTURE

Lessons of the NASA Tech House

[NASA-SP-442] p 199 N80-27219

ARCHITECTURE (COMPUTERS)

Parallel. Asynchronous Executive (PAX): System

concepts, facilities, and architecture

{NASA-TP-2179J p 180 N83-28921

AREA NAVIGATION

Evaluation of Microwave Landing System (MLS) effect

on the delivery performance of a fixed-path metering and

spacing system

I NASA-TP-1844 ) p31 N81-291 t 1

Development and evaluation of a Kalman-filter algorithm

for terminal area navigation using sensors of moderate

accuracy

[ NASA-TP-2035] p 31 N83-29193

A comparison of two position estimate algorithms that

use ILS Iocalizer and DME information Simulation and

flight test results

INASA-TP-22811 p 31 N84-17165

ARGON

Nitriding of titanium and titanium: 8 percent aluminum,

1 percent molybdenum, I percent vanadium alloy with an

ion*beam source

INASA-TP'2149] p 69 N83-24640

ARITHMETIC

Concurrent error detecting cedes for arithmetic

processors

[ NASA-TP-1528 ] p 177 N79-30947

ARIZONA

Applications systems verification and transfer project,

Volume 2: Operational applications of satellite snow-cover

observations and data-collection systems in the Arizona

test site

[NASA-TP-1823] p 140 N82-20618

ARM (ANATOMY)

Vector*algebra approach to extract Oenavit-Hartenberg

parameters of assembled robot arms

INASA-TP*2191 J p 182 N83-34661

Modified Denavit-Hartenberg parameters for better

location of joint axis systems in robot arms

[NASA-TP-2585] p 183 N86-27953

ARROW WINGS

Effect o1 a simulated engine let blowing above an arrow

wing at Mach 2.0

[NASA-TP-1050] p 6 N78-10030

Theoretical evaluation of high-speed aerodynamics for

arrow-wing configurations

[NASA-TP-1358] p 10 N79-14023

Effects ot wing leading-edge deflection on low-speed

aerodynamic characteristics of a low-aspect-ratio highly

swept arrow-wing configuration --- wind tunnel tests

[NASA-TP-1434J p 12 N79-26020

Theoretical and experimental investigation of

ground-induced effects for a low-aspect-ratio highly swept

arrow-wing configuration

[NASA-TP-15081 p 54 N79-31223

Leading-edge deflection optimization for a highly swept

arrow wing configuration

[NASA-TP-1777] p 16 N81-14974

Effects of vortex flaps on the low-speed aerodynamic

characteristics o1 an arrow wing

( NASA-TP-t 914 ] p3 N82-11013

Low-speed aerodynamic characteristics of a highly

swept, untwisted uncambered arrow wing

I NASA-TP-2176] p 22 N83-36000

ARTIFICIAL INTELLIGENCE

Marking parts to aid robot vision

INASA-TP-1819] p 176 N81-21775

Automated decision making and problem solving.

Volume 2: Conference presentations

[NASA-CP-2180*VOL-2] p 184 N81-29902

Automated Decision Making and Problem Solving.

Volume 1: Executive Summary

[NASA-CP-2180-VOL-1J p 184 N81-30889

Advanced Automation for Space Missions

[NASA-CP-2255} p 76 N83-15348

Kinematic control of robot with degenerate wrist

lNASA-TP-2341 ] p 181 N84-28539

ARTIFICIAL SATELLITES

Interactive des;,gn and analysis of future large spacecraft

concepts

[NASA-TP-lg37J p 72 N82-14276

Far travelers: The exploring machines

I NASA-SP-480] p 63 N85-33126

ASCENT PROPULSION SYSTEMS

Effect of propulsion system charactenstics on ascent

performance of dual-fueled single-stage earth-to-orbit

transports

[ NASA-TP-1115] p65 N78-1310g

Analysis of Jimsphere pairs for use in assessing Space

Vehicle ascent capability

(NASA-TP-2573 J p 28 N86-21506

ASCENT TRAJECTORIES

Shuffle Performance: Lessons Learned, part 1

[NASA-CP-2283*PT-t ] p 69 N84-10115

Shuttle Performance: Lessons Learned, part 2

I NASA-CP-2283-PT-2 } p69 N84-10144

ASPECT RATIO

Effects of diffusion factor, aspect ratio and solidity on

overall performance of 14 compressor middle stages ---

the effects of varying both diffusion through the rotor and

compressor blades and blade aspect ratio

INASA-TP-1523J p 45 N79-33210

Low-speed aerodynamic performance of a

high-aspect-ratio supercritical-wing transport model

equipped with full-span slat and part-span double-slotted

flaps

INASA-TP-1580J p 19 N82-15015

Performance of single-stage axial-flow transonic

compressor with rotor and stator aspect ratios of 1 63

and 1.78, respectively, and with design pressure ratio of

1.82

INASA-TP-1974 i p49 N82-19222

A-14
SUB,lEG TINDEX ATMOSPHERIC COMPOSITION

Joint research effort on vibrations of twisted plates.

phase 1: Final results

[NASA-RP-11501 p 135 N86-10579

ASSEMBLY LANGUAGE

Interactive debug program for evaluation and

modification of assembly-language software

[NASA-TP-1441 } p 178 N79-21798

ASTEROIDS

Summer Workshop on Near-Earth Resources

I NASA-CP-2031J p 205 N78-16973

Asteroids: An Exploration Assessment

INASA-CP-2053} p 205 N78-29007

The geology of the terrestrial planets

[NASA-SP-469] p 200 N85-18888

ASTROOYNAMICS

Fifth Annual Flight Mechanics/Estimation Theory

Symposium

[NASA-CP-2152J p 64 N81-11070

ASTROMETRY

Study of the Solar Cycle from Space

[NASA-CP-20981 p 209 N80-17944

An assessment of ground-based techniques for

detecting other planetary systems. Volume 1: An overview

--- workshop conclusions

{NASA-CP-2124-VOL-t ] p 201 N80-18997

An Assessment of Ground-Based Techniques for

Detecting Other Planetary Systems Volume 2: Position

papers

[NASA-CP-2124-VOL*21 p 201 N80-25224

ASTRONAUTICS

Essays on the History of Rocketry and Astronautics:

Proceedings of the Third through the Sixth History

Symposia ol the International Academy of Astronautics,

volume 1

{NASA-CP-2014-VOL-t j p 211 N77-33030

Astronautics and Aeronautics, 1975. A chronology

{NASA-SP-40201 p 212 N81-16973

ASTRONOMICAL CATALOGS

An atlas of solar spectra between 1175 and 1950

angstroms recorded on Skylab with the NRL's Apollo

telescope mount experiment

[NASA-RP-1069] p 209 N81-23004

A Catalog of Selected Viking Orbiter Images

[NASA-RP-1093] p 207 N83-25636

International Ultraviolet Explorer Atlas of O-typespeetra

from 1200 to 1900 angstrom

[NASA-RP-1155] p 204 N86-25307

ASTRONOMICAL MODELS

B Stars with and without emission lines, parts 1 and 2

[NASA-SP-458] p 200 N82-25027

Local Interstellar Medium. International Astronomical

Union Colloquium No, 81

[NASA-CP-2345} p 204 N85-15539

ASTRONOMICAL OBSERVATORIES

The Space Telescope Observatory. Special session of

Commission 44, IAU 18th General Assembly

[NASA-CP-2244} p 202 N82-33296

Large Deployable Reflector Science and Technology

Workshop. Volume 3: Systems and Technology

Assessment

[NASA-CP-2275-VOL-31 p 202 N84-32318

Airborne Astronomy Symposium. A symposium

commemorating the tenth anniversary of operations of lhe

Kuiper Airborne Observatory

[NASA-CP-2353] p 202 N85-17848

ASTRONOMICAL PHOTOGRAPHY

An emission-line survey of the Milky Way

[NASA-SP-434 ] p 201 N80-11966

The Space Telescope Observatory Special session of

Commission 44, IAU 18th General Assembly

[NASA-CP-2244] p 202 N82-33296

ASTRONOMICAL PHOTOMETRY

The Space Telescope Observatory Special session of

Commission 44, JAU 18th General Assembly

[NASA-CP-2244] p 202 N82-33296

Astronomical Microdensitometry Conference

[NASA-CP-23171 p t16 N84-28020

The 1982-1984 Eclipse of Epsilon Aurigae

[NASA-CP-23841 p 203 N86-12168

ASTRONOMICAL SPECTROSCOPY

Scienlific research with the space Telescope:

International Astronomical Union Colloquium no 54 --

conferences

{NASA-CP-2111 I p 200 N80-22130

Advances in Ultraviolet Astronomy: Four Years of PUE

Research

INASA-CP-22381 p 201 N82-31163

The Space Telescope Observatory. Special session of

Commission 44, IAU 15th General Assembly

{NASA-CP-2244 j p 202 N82-33296

The 1982-1984 Eclipse of Epsilon Aurigae

{NASA-CP-2384] p 203 N88-12168

ASTRONOMICAL TELESCOPES

An Assessment of Ground-Based Techniques for

Detecting Other Planetary Systems Volume 2: Position

papers

I NASA-CP-2124-VOL-2] p 20t N80-25224

Project Orion: A design study of a system for detecting

extrasolar planets

[NASA-SP-4361 p 206 N80-27260

The star splitters: The high energy astronomy

observatories

[NASA-SP-466i p 202 N84-22516

Large Deployable Reflector Science and Technology

Workshop, Volume 3: Systems and Technology

Assessment

[NASA-CP-2275-VOL-31 p 202 N84-32318

ASTRONOMY

Astronautics and aeronautics, 1976 A chronology

{NASA-SP-4021 ] p 212 N84-25602

ASTROPHYSICS

A geological basis for the exploration of the planets

[NASA-SP-417] p 204 N77-15961

The structure and content of the gataxy and galactic

gamma rays

I NASA-CP-002] p 199 N77-20977

Recognition of compact astrophysical objects

{NASA-SP-421 ] p 201 N77-34063

Gamma Ray Astrophysics: New insight into the

universe

I NASA-SP-453 ] p204 N82-21118

Stellar atmospheric structural patterns

[NASA-SP-471 ] p 204 N84-19253

The star splitters: The high energy astronomy

observatories

[NASA-SP-4661 p 202 N84-22516

Interrelationships among Circumstellar, Interstellar and

Interplanetary Dust

[NASA-CP-24031 p 201 N86-23493

ASYMMETRY

Mechanics of liquid helium in a partially filled rotating

dewar in low gravity with application to Gravity Probe-B

[NASA-TP-2124] p 110 N83-16680

ASYMPTOTIC SERIES

An asymplotic expansion approach to the inverse

radiative transfer problem --- to infer concentration profiles

of the atmosphere from measurements made onboard a

satellite

[NASA-TP-15871 p 152 N80-13730

ATLANTIC OCEAN

Satellite-derived global oceanic rainfall atlas (1973 and

1974)

INASA-SP-4101 p 157 N77-19709

North Atlantic Deep Water Formation

I NASA-CP-23671 p 169 N85-26028

ATLIT PROJECT

Full-scale wind tunnel-investigation of the Advanced

Technology Light Twin-Engine airplane (ATLIT) --- Langley

full scale tunnel

[NASA-TP-1591 I p 14 N80-22266

ATMOSPHERIC A'I-rENUATION

Computation of atmospheric attenuation of sound for

fractional-octave bands

INASA-TP-1412} p 186 N79-17659

Atmospheric solar absorption measurements in the 9

to 1 t mu m region using a diode laser heterodyne

spectrometer

[NASA-TP-1726] p 153 N80-33998

Radio-wave propagation for space communications

systems

{NASA-TP-1770] p 70 N81-18082

ATMOSPHERIC CHEMISTRY

The NASA Ames Research Center one- and

two-dimensional stratospheric models Part 1: The

one-dimensional model

[NASA-TP-1002] p 158 N77-32688

The NASA Ames Research Center one- and

two-dimensional stratospheric models Part 2 The

two-dimensional model

fNASA-TP-t003] p 158 N77-32689

Man's impact on the troposphere: Lectures in

tropospheric chemistry

{NASA-RP-10221 p 151 N79-10634

A coupled radiative-convective-photochemical model of

the stratosphere

INASA-TP 14181 p 136 N79-22580

Shuttle atmospheric lidar research program

INASA-SP-433} p 117 N80-11414

Environmental analysis of the chemrcal release module

--- space shuttle payload

INASA-TP-1750} p 209 N81-13912

Carbon-catalyzed oxidation of SO2 by NO2 and air

I NASA-TP-2014 j p 85 N82-22330

Proceedings Ot a Workshop on Assessment of

Techniques for Measuring Tropospheric N sub x O sub y

[NASA-CP-2292] p 154 N84-13706

Proceedings of a Workshop on Research Needs in

Heterogeneous Tropospheric Chemistry

lNASA-CP-2320] p 137 N84-28131

Proceedings of a Workshop on Polar Stratospheric

Clouds: Their Role in Atmospheric Processes

{NASA-CP-2318] p 154 N84-32952

Assessment of Techniques for Measuring Tropospheric

H sub x O sub y

[ NASA-CP-23321 p 158 N85-14336

Present state of knowledge of the upper atmosphere:

An assessment report; processes that control ozone and

other climatically important trace gases

{NASA-RP-11621 p 156 N86-25911

ATMOSPHERIC CIRCULATION

Stratospheric warmings: Synoptic, dynamic and

general-circulation aspects

{NASA-RP-1017J p t58 N78-18630

Synoptic analyses, 5-, 2-, 1-, and 0.4-millibar surfaces

for July 1978 through June 1977

[NASA-RP-1032| p 159 N79-19569

Shuttle atmospheric lidar research program

JNASA-SP-433] p 117 N80-11414

Thunderstorm-environment interactions determined with

three-dimensional trajectories

INASA-RP-1054] p 161 N80-16675

The Numerical Studies Program for the Atmospheric

General Circulation Experiment (AGCE) for Spscelab

Flights

[NASA-CP-22001 p 163 N82-12715

Proceedings of a Workshop on Research Needs in

Heterogeneous Tropospheric Chemistry

[NASA-CP-2320] p 137 N84-28131

NASA/MSFC FY-84 Atmospheric Processes Research

Review

{NASA-CP-2329] p 166 N84-34829

Globai Scale Atmospheric Processes Research Program

Review

{NASA-CP-23441 p 166 N85-14360

Current Scientific Issues in Large Scale Atmospheric

Dynamics

{NASA-CP-2410] p 167 N86-24082

ATMOSPHERIC COMPOSITION

Inversion Methods in Atmospheric Remote Sounding

{NASA-CP-004J p 151 N78-12586

Apotlo-Soyuz test project. Volume 1: Astronomy, earth

atmosphere and gravity field, life sciences, and materials

processing

[NASA-SP-4t2} p 80 N78-17088

An evaluation of in situ ozone sensor performance during

a cold frontal passage

{NASA-TP-12391 p 158 N78-27706

Ozone concentration in the cabin of a Gates Leartet

measured simultaneously with atmospheric ozone

concentrations

INASA-TP-1340] p 148 N78-33618

STRATCOM 8 Data Workshop and supplement

INASA'CP-2043] p 136 N79-23461

Shuttle atmospheric lidar research program

INASA-SP-433] p 117 N80-11414

An asymptotic expansion approach to the inverse

radiative transfer problem --- to infer concentration profiles

of the atmosphere from measurements made onboard a

satellite

{NASA-TP-1587} p 152 N80-13730

Orbit dynamics and geographical coverage capabilities

of satellite-based solar Occultation experiments for global

monitoring of stratospheric constituents

[NASA-TP-1606] p 64 N80-19142

Review of Spectroscopic Data for Measurements of

Stratospheric Species

[NASA-CP-21361 p 192 N80-26125

High Resolution Infrared Spectroscopy Techniques for

Upper Atmospheric Measuremenls

{NASA-CP-21341 p 152 N80-27866

Atlas of absorption lines from 0 to 17 900 cm(-1)

[NASA-RP-10841 p 192 N82-15853

Vibrational-Rotational Spectroscopy for Planetary

Atmospheres, volume 2

[ NASA-CP-2223-VOL-21 p 207 N82-26134

Tropospheric Passive Remote Sensing

I NASA-CP-2237 ] p 115 N82-26637

Applying modeling Results in designing a global

tropospheric experiment

INASA'CP'2235} p 153 N82-29796

Airborne lidar measurements of El Chichon stratospheric

aerosols, October 1982 to November 1982

[NASA-RP-1138] p 155 N85-19550

The evolution of complex and higher organisms

[NASA-SP-478J p 169 N85-32708

Potential spin-offs of the carbon dioxide observational

platform system (CO-OPS) for remote sensing

opportunities

{NASA-TP-2510} p 68 N85-34149

SAGE aerosol measurements Volume 1: February 21,

1979 to December 31, 1979

INASA-RP-1144J p 155 N96-11700

A-15
ATMOSPHERICFFECTS SUBJECT INDEX

Present state of knowledge of the upper atmosphere:

An assessment report; processes that control ozone and

other climatically important trace gases

INASA-RP-t162] p 1,56 N86-25911

Thermosphere Dynamics Workshop. volume 2

{NASA-CP-23891 p 137 N86-29301

ATMOSPHERIC EFFECTS

Atmosphenc aerosols: Their Optical Properties and

Effects (supplement)

l NASA-CP-2004-SUPPL I p t 51 N77-t 5564

Lubrication and failure mechanisms of molybdenum

dnsuffide films 1: Effect of atmosphere

t NASA-TP-t 343] p92 N79-t3158

Almosphenc effects on CO2 laser propagation

tNASA-TP-13571 p 152 N79-13607

Stratospheric aerosol modification by supersonic

transport operations with chmate implications

[NASA-RP-1058] p 161 N80-15726

Application of a Gaussian multilayer diffusion model to

characterize duspersion of vertical HCI column density in

rocket exhaust clouds

[NASA-TP-1956] p 149 N82-t4672

Proceedings: Fifth Annual Workshop on Meteorological

and Enwronmental inputs to Aviation Systems

I NASA-CP-2192) p 3 N82-2t 139

Caplunng energy from the w_od

1NASA-SP-4551 p 146 N62-28783

Report of Workshop on Mount Saint Helens: Fts

Atmospheric Effects and Potential Climatic Impact

]NASA-SP-4581 p 154 N82-32915

Atmosphenc constraint statistics for the Space Shuttle

mqsslon planning

INASA-TP-20691 p 69 N82-33417

Atmospheric Effects and Potential Climate Impact of

the t 980 Eruptions of Mount St. Hetens

INASA-CP-22401 p 136 N83-11534

ATMOSPHERIC ELECTRICITY

Exploratory Meeting on Atmospheric Electrncity and

Severe Storms

{ NASA-CP-20561 p 151 N78-29669

Middle atmosphere eleotrodynamics: Report of the

workshop on the Role of the Electrodynamics of the Middle

Atmosphere on Solar Terrestrial Coupling

[NASA-CP-2090] p 152 N79-25608

Summary of the NASA/MSFC FY-79 Severe Storm and

Local Weather research rewew --- cloud physics,

atmospheric electricity, and mesoscale/storm dynamics

reserach

INASA-CP-2t05] p 160 N79-33722

NASAJMSFC FY-80 Atmospheric Processes Research

Review

INASA-CP.21451 p 153 N80-28965

ATMOSPHERIC ENTRY

Entry dynamucs ot space shuttle orbiter wnth

lateral-directional stability and controf uncertamhes at

supersonic and hypersonuc speeds

{NASA-TP-10111 p 70 N78-13f19

Almospheruc entry and fragmentation of dense

meteorotds

[NASA-TP-1333] p 205 N79-14978

Determination of the

hypersonic-continuum/rarefied-flow drag coefficient of the

Viking lander capsule 1 aeroshell from flight data

[NASA-TP-1793} p 3 N81-14961

Pressures, forces, moments and shock shapes for a

geometrically matched sphere-cone and hyperboloid at

Math 20 3 in helnum --- 22-inch aerodynamics leg ol the

Langley hypersomc helium tunnel facility

INASA-TP-2tO0} p 110 N83-16675

Performance of an ablator for Space Shuttle inorbil repair

_n an arc-plasma atrstream

{NASA-TP-2t50} p 74 N83-22317

ATMOSPHERIC ENTRY SIMULATION

Analysis of space shuttle orbiter entry dynamics from

Math I0 to Maeh 2 5 with the November 1976 flight control

system

INASA-TP.t667] p 71 N80-29417

ATMOSPHERIC HEAT BUDGET

Analyses of earth radlahon budget data from unrestricted

broadband radiometers on the ESSA 7 saleilite

[NASA-TP-1402] p 160 N79-22709

ATMOSPHERIC HEATING

Stratosphenc warmnngs: Synoptic, dynamic and

general-elf cu_atlon aspects

INASA-RP-1017} p 158 N78-18630

A simplified method lor calculating the atmospheric

heating rate by absorption of solar radiation in the

stratosphere and mesosphere

INASA-TP-1398} p 159 N79-16493

Energet_es of a sudden stratospheric warming s_mulated

with a three-dimensional, spectral, quasi-geostrophlc

model

tNASA-TP-18471 p 163 N6t-23761

ATMOSPHERIC MODELS

The 1976 standard atmosphere above 86-km altitude:

Recommendations of task group 2 to COESA

{NASA-SP-3981 p 157 N77-10755

The NASA Ames Research Center one- and

two-dimensional stratosphehc models Part 1: The

one-dimensional model

{NASA-TP-t0021 p 158 N77-32688

The NASA Ames Research Center one- and

two-dimensional stratospheric models Part 2: The

two-dimensional model

{NASA-TP-t0031 p 158 N77-32689

The NASA-Ames Research Center stratospheric aerosol

model. 2 Sensitivity studies and comparison with

observatories

[NASA-TP-1363] p 160 N79-21720

The NASA-AMES Research Center stratospheric

aerosol model 1 Physical processes and computational

analogs

INASA-TP-t362] p t60 N79-21721

The wave structures ol the Eady model of baroclinic

instabdlity

INASA-TP-t548] p 160 N79-32796

The stratosphere: Present and future

INASA-RP-1049] p 161 Na0-t4641

A diagnostic model for studying daylime urban air quality

trends

[ NASA-TP-18431 p 149 N81-22587

Energetics of a sudden stratospheric warming simulated

with a three-dimensional, spectral, quasi-geostrophic

model

INASA-TP-18471 p 163 N81-23761

A spatial model of wind shear and turbulence for flight

simulation

{NASA-TP-23131 p 165 N84-24044

Proceedings ol a Workshop on Research Needs in

Heterogeneous Tropospheric Chemistry

{NASA-CP-23201 p 137 N84-28131

NASA/MSFC FY-84 Atmospheric Processes Research

Review

[NASA-CP-23291 p t66 N84-34829

Understanding climate: A strategy for climate modeling

and predictability research, 1985-1995

INASA-RP-1158} p 166 N86-13866

Present state of knowledge of the upper atmosphere:

An assessment report; processes that control ozone and

other climatically important trace gases

INASA-RP-1162} p t56 N86-25911

Surface radiation budget for climate applications

INASA-RP-1169} p 167 N86-28574

ATMOSPHERIC MOISTURE

VISSR Atmospheric Sounder (VAS) Research Review

{NASA-CP-2253J p 165 N83-24028

ATMOSPHERIC PHYSICS

NASA Workshop on Solar-Terrestrial Sludnes lrom a

Manned Space Station

[NASA-CP-2024] p 136 N77-32549

Environmental analysis of the chemical release module

--- space shut'tie payload

INASA-TP-t750] p 209 N81-13912

Energetics of a sudden stratospheric warming simulated

with a three-dimensional, spectral, guasi-geostrophic

model

[NASA-TP-1847] p 163 N81-23761

The Numerical Studies Program for the Atmosphernc

General Circulation Experiment (AGCE) for Spacelab

Flights

[NASA-CP-22001 p 163 N82-12715

ATMOSPHERIC RADIATION

Proceedings of a Workshop on Polar Stratosphenc

Clouds: Their Role in Atmospheric Processes

INASA-CP-2318] p 154 N84-32952

Introduction to the theory of atmospheric radiative

transfer

[ NASA-RP-t 156} p 157 N86-27839

ATMOSPHERIC REFRACTION

Atmospheric aerosols: Their Optical Properties and

Effects (supplement)

{NASA-CP-2004-SUPPL] p t51 N77-t5564

ATMOSPHERIC SCATTERING

A tutorial solution to scattering of radiation in a thin

atmosphere bounded below by a diffusely reflecting,

absorbing surface

!NASA-TP-2077] p 154 N82-33918

Single scattering from nonsphencal Chebyshev

particles: A compendium of calculations

lNASA-RP-1157 / p 194 N86-17140

Introduction to the theory of atmospheric radiative

transfer

[NASA-RP-11561 p 157 N86-27839

ATMOSPHERIC SOUNDING

Atmospheric structure determined from salellite data

INASA-RP-1071 ] p 162 N81-16678

Comparisons between Nimbus 6 satellite and

rawinsonde soundings for several geographical areas

iNASA-RP-1073] p 163 N81-t6679

VAS Demonstration Sounding Workshop: The

Proceedings of a satellite sounding workshop

INASA-CP-21571 p t63 N81-19709

Goddard Laboratory for Atmospheric Science, collected

reprints 1978-1979, volume 1

INASA-TP-t788-VOL-l} p 163 N81-21686

VISSR Atmospheric Sounder (VAS) Research Review

I NASA-CP-2253] p 165 N83-24028

NASA/MSFC FY-84 Atmosphere Processes Research

Review

[NASA-CP-2329} p 166 N84-34829

VAS demonstration: (VISSR Atmospheric Sounder)

description

[NASA-RP-11511 p 166 N86-13867

ATMOSPHERIC STRATIFICATION

Airborne Ludar measurements ol aerosols, mixed layer

heights, and ozone during the 1980 PEPE/NERDS summer

field experiment

{NASA-RP-1143] p 150 N86-16748

ATMOSPHERIC TEMPERATURE

Energetics of a sudden stratospheric warming simulated

with a three-dimensional, spectral quasi-geostrophic

model

[NASA-TP-18471 p 163 N81-23761

ATMOSPHERIC TURBULENCE

Evaluation of a wind-tunnel gust response technique

including correlations with analytical and flight test

results

{NASA-TP-1501 i p 2 N80-11028

A conceptual framework for using Doppler radar

acquired atmospheric data for flighl simulation

[ NASA-TP-21921 p 36 N83-27977

A spatial model of wind shear and turbulence for flight

simulation

[NASA-TP-23131 p 165 N84-24044

ATMOSPHERICS

The mechanics of atmospheric systems derived through

vertical and horizontal analysis of parametric data

[NASA-TP-10721 p 158 N78-15641

ATOMIC CLOCKS

Proceedings of the Thirteenth Annual Precise Time and

Time Interva_ {PTTI) Applications and Planning Meeting

[ NASA-CP-22201 p 118 N82-20494

Proceedings of the 141h Annual Precise Time and Time

Interval (PTFI) Applications Plannung Meeting

I NASA-CP-2265 ] p 118 N83-35351

ATOMIC PHYSICS

Rate processes nn gas phase

[NASA-RP-1090] p 192 N83-27609

ATS 6

The ATS-6 power system: Hardware implementation

and orbital performance

{NASA-TP-1023J p 76 N77-32229

Significant initial results from the environmental

measurements experiment on ATS-6

INASA-TP-1101 I p 65 N78-15142

ATS-6 engnneering performance report Volume 2: Orbit

and attitude controls

[NASA-RP-1080-VOL-21 p 73 N82-16146

ATS-6 engineering performance report Volume 3:

Telecommunications and power

[NASA-RP-1080-VOL-3] p 73 N62-16149

ATe-6 engineerqng performance report Volume 4:

Television experiments

[NASA-RP-1080.VOL.41 p 73 N82-15150

ATe-6 engineering performance report Volume 5:

Propagation experiments

[NASA-RP-IO80*VOL-51 p 73 N82-16151

ATS-6 engmeenng performance report Volume 6:

Scientific experiments

[NASA-RP-1080-VOL-6] p 73 N82-15152

ATTENUATION

Measurements of spectrat attenuation coeffioents in the

lower Chesapeake Bay

[NASA-TP-21301 p 168 N83-24133

ATTITUDE (INCLINATION)

Experimental studies of effects of tltt and structural

asymmetry on vibration characteristics of thnn-wall circular

cylinders partly titled with hQu,d

I NASA-TP-121 t I p 127 N78-28480

Crash tests of four udenticai high-wing single-engine

airplanes

[ NASA-TP-1699] p 35 N80-30296

A study of the cornering forces generated by mrcraft

tires on a tilted, free-swiveling nose gear

{NASA.TP-2481 ] p 135 N86-11522

ATTITUDE CONTROL

The N-BOO2 user's and programmer's manual

INASA-TP-1145] p 70 N78-21200

A digital computer program for the dynamic interaction

simulation of controls and structure (DISCOS), volume t

{NASA-TP-1219-VOL-1 I p 70 N78-25123

A digital computer program for the dynamnc _nteraction

s,mutatlon of controls and structure (DISCOS}. volume 2

{NASA-TP-1219-VOL-2} p 70 N78-25124

A-16
SUBJECT INDEX

Flight evaluation of stabilization and command

augmentation system concepts and cockpit displays during

approach and landing of powered-lift STOL aircraft

INASA'TP-1551 } p 56 N81-t1044

Decoupled control of a long flexible beam in orbit

[NASA-TP-1740] p 71 N81-13082

Large space systems technology, 1981 ---

conferences

{NASA-CP-2215-PT-1] p 66 N82-18275

Integrated Flywheel Technology, 1983

[NASA-CP-2290J p 77 N84-12228

Regions of attraction and ultimate boundedness for

linear quadratic regulators with nonlinearities

[NASA-TP-2322J p 181 N84-28538

An Assessment of Integrated Flywheel System

Technology

[NASA-CP-2346] p 78 N85-13850

ATTITUDE INDICATORS

Peripheral Vision Horizon Display (PVHD)

[NASA-CP-2306] p 40 N85-10044

ATTRACTION

Regions of attraction and ultimate boundedness for

linear quadratic regulators with nonlinearities

[NASA-TP-23221 p 181 N84-28538

AUDIOLOGY

Physiological, Psychological, and Social Effects of

Noise

[NASA-RP-1115] p 174 N84-29465

AUDIOMETRY

Physiological, Psychological, and Social Effects of

Noise

[NASA-RP-1115J p 174 N84-29465

AUDITORY DEFECTS

Physiological, Psychological, and Social Effects of

Noise

[NASA-RP-11151 p 174 N84-29465

AUDITORY PERCEPTION

Overall loudness of steady sounds according to theory

and experiment

[NASA-RP-1001 J p 171 N79-25753

Effect of noise spectra and a listening task upon

passenger annoyance in a helicopter interior noise

environment

INASA-TP-1590] p 171 N80-13769

AUDITORY STIMULI

Overall loudness of steady sounds according to theory

and experiment

[NASA-RP-1001 ] p 171 N79-25753

Multiple-event airplane noise annoyance

[NASA-TP-2101] p 150 N83-16951

AUDITORY TASKS

Evaluation of several secondary tasks in the

determination of permissible time delays in simulator visual

and motion cues

[NASA-TP-t214} p 32 N78-30089

Simulator study of the effect of visual-motion time delays

on pilot tracking performance with an audio side task

[NASA-TP-1216] p 32 N78-30090

AUGER SPECTROSCOPY

Transfer of molybdenum disulfide to various metals

[NASA-TP-1019] p 98 N77-30296

Auger spectroscopy analysis of lubrication with zinc

dialkyidithiophosphate of several metal combinations in

sliding contact

[NASA-TP-t489] p 92 N79-27308

Evaluation and auger analysis of a

zinc-dialkyl-dithiophosphate antiwear additive in several

diester lubricants

[NASA-TP-15441 p 93 N79-32359

Surface chemistry and friction behavior of the silicon

carbide (0001) surface at temperatures to 1500 deg C

[NASA-TP-1813J p 94 N81-19300

AUGMENTATION

NASA Aircraft Controls Research, 1983

[NASA-CP-2296] p 58 N84-20567

AURIGA CONSTELLATION

The 1982-1984 Eclipse of Epsilon Aurigae

[NASA-CP-2384] p 203 N86-12168

AURORAL ARCS

Circuit transients due to negative bias arcs on a

high-voltage solar array in low Earth orbit

{NASA-TP-2407] p 75 N85-14858

AURORAL ZONES

Thermosphere Dynamics Workshop, volume 2

[NASA-CP-2389] p 137 N86-29301

AUSTENITE

Effect of double vacuum melting and retained austenite

on rolling-element fatigue life of AMS 5749 bearing steel

[NASA-TP-1060] p 119 N77-33520

AUSTENITIC STAINLESS STEELS

Study of austenitic stainless steel welded with low altoy

steel filler metal --- tensile and impact strength tests

[NASA-TP-1460] p 87 N79-28288

Fracture temperature and flaw growth in nitronic 40 at

cryogenic temperatures

[NASA-TP-2312] p 89 N84-23750

AUTOMATA THEORY

Marking parts 1o aid robot vision

INASA-TP-1819] p 176 N81-21775

Automated decision making and problem solving

Volume 2: Conference presentations

INASA-CP-2180-VOL-2} p 184 N81-29902

AUTOMATIC CONTROL

Validation Methods Research for Fault-Tolerant Avionics

and Control Systems: Working Group Meeting, 2

INASA.CP.2130J p 176 N80-23008

Navigation, guidance, and control for helicopter

automatic landings

INASA-TP'1849] p 55 N80-23326

Automated Decision Making and Problem Solving

Volume 1: Executive Summary

JNASA-CP-2180-VOL-1 ] p 184 N81-30889

Concept for a power system controller for large space

electrical power systems

[NASA-TP-lg39} p 77 N82-11109

Space power subsystem automation technology

[NASA-CP-2213] p 77 N82-21254

Advanced Automation for Space Missions

J NASA-CP-2255t p 76 N83-15348

Human Feclors Considerations in System Design

[NASA-CP-2246J p 173 N83-18238

Proposed fast-response oxygen monitoring and control

system for the Langley 8-foot high-temperature tunnel

[NASA-TP-2218} p 116 N84-11460

Flight-test of the glide-slope track and flare-control laws

for an automatic landing system for a powered-litt STOL

airplane

[NASA-TP-2128J p 57 N84-t3198

Baseline experiments in teleoperator control

[NASA-TP-2547 J p 174 N86-26836

AUTOMATIC FLIGHT CONTROL

Study of the application of an implicit model-following

flight controller to lift-fan VTOL aircraft

{NASA-TP-10401 p 53 N78-t6063

A nonlinear trajectory command generator for a digital

flight-control system

[NASA-TP-1221 I p 54 N79-13057

Flight tests of the total automatic flight control system

('rafcos) concept on a DHC-6 Twin Otter aircraft

[NASA-TP-15131 p 55 N80-17081

Production of Reliable Flight Crucial Software: Validation

Methods Research for Fault Tolerant Avionics and Control

Systems Sub-Working Group Meeting

[NASA-CP-2222] p 179 N82-24845

Development and evaluation of a Kalman-filter algorithm

for terminal area navigation using sensors of moderate

accuracy

[NASA-TP-2035] p 31 N83-29193

Restructurable Controls

{NASA-CP-2277J p 57 N83-33896

AUTOMATIC GAIN CONTROL

Stability boundaries for systems with frequency-model

feedback and complacency filter

[NASA-TP-1744] p 164 N81-10789

Joint University Program for Air Transportation

Research, 1981

[NASA-CP-2224] p 3 N82-26199

Gain selection method and model for coupled propulsion

and airframe systems

JNASA-TP-2067] p 57 N83-11139

AUTOMATIC LANDING CONTROL

Application of the concept of dynamic trim control to

automatic landing of carrier aircraft --- utilizing digital

feedforeward control

INASA-TP-1512} p 55 N80-19126

Navigation, guidance, and control for helicopter

automatic landings

[NASA-TP-1649] p 55 N80-23326

Helical automatic approaches of helicopters with

microwave landing systems

[NASA-TP-2109} p 31 N83-18704

AUTOMATIC PILOTS

Development and flight test results of an autothrottle

control system at Mech 3 cruise

[NASA-TP-1621 _ p 56 N80-26328

Analysis of space shuttle orbiter entry dynamics from

Mach 10 to Mach 2 5 with the November 1976 flight control

system

{NASA-TP-1667J p 71 N80-29417

AUTOMATIC TEST EQUIPMENT

Three-axis electron-beam test facility

{NASA-TP-1836J p 101 N81-20359

AUTOMOBILE ENGINES

Cold-air performance of free-power turbine designed for

112-kilowat1 automotive gas-turbine engine 1: Design

Stator-vane-chord setting angle of 35 deg

INASA'TP'IO07 I p 42 N78-16053

Multiroller traction drive speed reducer: Evaluation for

automotive gas turbine engine

[NASA-TP-2027] p 122 N82-26678

AXIAL FLOW TURBINES

AUTOMOBILES

A comparison of the noise produced by a small jet on

a moving vehicle with that in a free jet --- jet mixing

noise

[NASA-TP-1326] p 186 N79-14872

Implications of fuel-efficient vehicles on ride quality and

passenger acceptance: Workshop proceedings

[NASA-CP-2096} p 199 N80-18990

AUXILIARY POWER SOURCES

Electnc Flight Systems

[NASA-CP-2209] p 3 N82-19134

Aircraft Electric Secondary Power

INASA-CP-2282] p 50 N84-10055

AVIONICS

Avionics and controls research and technology

JNASA-CP-2061 ] p 1 N79-15898

Validation Methods for Fault-Tolerant avionics and

control systems, working group meeting t

[NASA-CP-2114] p 176 N80-12741

Validation Methods Research for Fault-Tolerant Avionics

and Control Systems Sub-Working Group Meeting. CARE

3 peer review

[NASA-CP-2167] p 176 N81-15702

The 1980 Aircraft Safety and Operating Problems, part

2

[NASA-CP-2170-PT-21 p 29 N81-t9056

Helicopter Handling Qualities

[NASA-CP-2219] p 30 N82-23208

Production of Reliable Flight Crucial Software: Validation

Methods Research for Fault Tolerant Avionics and Control

Systems Sub-Working Group Meeting

{NASA-CP-2222] p 179 N82-24845

Space Shuttle Technical Conference, part 2

(NASA-CP-2342-PT-2} p 63 N85-16937

NASA and general aviation

[NASA-SP-485J p 38 N86-30720

AXES OF ROTATION

Three-axis electron-beam test facility

[NASA-TP-1836] p 101 N81-20359

Modified Denavit-Hartenberg parameters for better

location of joint axis systems in robot arms

[NASA-TP-2585] p 183 N86-27953

AXIAL FLOW

Aerodynamic performance of a 135-pressure-ratio

axial.flow fan stage

INASA-TP-1299J p 10 N7g-10022

Capillary and acceleration wave breakup of liquid jets

in axial-flow airstreams

[NASA-TP-1791] p 109 N81-16417

Performance of single-stage axial-flow transonic

compressor with rotor and stator aspect ratios of 1.63

and 1.77, respectively, and with design pressure ratio of

2.05

[NASA-TP-2001 ] p 49 N82-22269

STGSTK; A computer code for predicting multistage

axial flow compressor performance by a meanline stage

stacking method

INASA-TP-2020J p 49 N82-25250

AXIAL FLOW TURBINES

Cold air performance of a

12.766-centimeter-tip-diameter axial-flow cooled turbin e.

2: Effect of air ejection on turbine performance

[NASA-TP-t018] p 5 N77-30089

Cold-air performance of a

12.766.centimeter-tip-diameter axial-flow cooled turbin e.

3: Effect of rotor tip clearance on overall performance

of a solid blade configuration

[NASA-TP-1032J p 5 N77-32082

Design and performance of a

427-meter-per-second-tip-speed two-stage fan having a

2.40 pressure ratio

[NASA-TP-1314] p 43 N78-33109

TACT 1: A computer program for the transient thermal

analysis of a cooled turbine blade or vane equipped with

a coolant insert. 2. Programmers manual

[NASA-TP-1391 J p 106 N79-18288

Aerodynamic performance of 1 38-pressure-ratio,

variable-pitch fan stage

(NASA-TP-1502] p 45 N79-31213

Aerodynamic performance of axial-flow fan stage

operated at nine inlet guide vane angles --- to be used

on vertical lift aircraft

[NASA-TP-1510J p 45 N79-31214

Computer program for generating input for analysis of

impingement-cooled, axial-flow turbine blade

[NASA-TP-1603J p 107 N80-15361

Improved method for calculating transonic velocities on

blade-to-blade stream surfaces of a turbomachine

[NASA-TP-1772] p 17 N81-22017

Rotor tip clearance effects on overall and blade-element

performance of axial-flow transonic fan stage

[NASA-TP-2049] p 49 N82-33389

Analytical and experimental investigation of stator

endwall contouring in a small axial-flow turbine. 1: Stator

performance

[ NASA-TP-2023 ] p4g N83-11125

A-17
AXIAL LOADS

Analytical and experimental investigation of stator

endwall countouring in a sinai/axial-flow turbine

NASA-TP-23091 p 51 N84-32388

AXIAL LOADS

Fracture toughness of boron/aluminum laminates with

various proportions of 0 deg and plus or minus 45 deg

NASA-TP-1707 ] p81 N81-11115

AXIAL STRAIN

Stress-concentration factors for finite orthotropic

laminates with a circular hole and uniax+al loading

NASA-TP-1469] p 80 N79-23140

AXlSYMMETRtC BODIES

Static internal performance charactarisbcs of two thrust

reverser concepts for axisymmetric nozzles

NASA-TP-2025] p 20 N82-26235

Aeropropulslve characteristics of Mach numbers up to

22 of 5.xisymmetnc and nonaxisymmetnc nozzles installed

on an F-18 model

NASA-TP-20441 p 20 N82-3029t

AXISYMMETRIC FLOW

Solution of sxisymmetrio and two-dimensional inviscid

flow over blunt bodies by the method of lines

NASA-TP-1154] p 105 N78-22332

Calculation of laminar heabng rates on

three-dimensional configurations using the axisymmetnc

analogue

INASA-TP-1698] p 108 N80-337t9

Steady and nonsteedy supersonic turbulent sfferbody

flow

[NASA-TP-1769] p 16 N81-16977

The Numerical Studies Program for the Atmospheric

General Circulation Experiment (AGCE) for Spaceleb

Flights

[NASA-CP-2200} p 163 N82-12715

Experimental and analytical investigation of

axisymmetric supersonic cruise nozzle geometry at Mech

numbers from 060 to 1.30

INASA-TP-1953] p 19 N82-14052

Effects of axisymmetric and normal air ;el plumes end

solid plume on cylindrical afferbody pressure distributions

at Math numbers from 1.65 to 2.50

INASA-TP-2005] p 19 N82-22215

Circumferentially segmented duct lines optimized for

axnsymmetric and standing wave sources --- reducing noise

from turbofan engines gelerkin method acoustic

attenuation

INASA-TP-2075] p 186 N62-34190

Tenth NASTRAN User's Colloquium

[NASA-CP-2249} p 131 N83-12452

Static investigation of two STOL nozzle concepts with

pitch thrust-vectoring capability

{NASA-TP-2559J p 28 N86-23559

AZIMUTH

Simulation study of traffic-sensor noise effects on

utilization of traffic situation display for self-spacing task

1NASA-TP-2082} p 40 N83-18723

B

B STARS

B Stars with and without emission lines, parts 1 and 2

{NASA-SP-456] p 200 N82-25027

B-F0 AIRCRAFT

Wind-tunnel/flight correlation study of aerodynamic

characteristics of a large flexible superson+c cruise airplane

CXB-70-1) 1 Wind-tunnel tests of a 0,03-scale model

at Mach numbers from 0 6 to 2.53

[ NASA-TP-t 514 j p33 N80-11068

Wind-lunnel/flight correlation study of aerodynamic

characteristics of a large flexible supersonic cruise airplane

(XB-701) 2: Extrapolaticn of wind-tunnet data to futl-scale

condilions

{NASA-TP-1515] p 13 N80-16032

Wind-tunnel/flight correlation study of aerodynamic

characteristics of a large flexible supersonic cruise airplane

(XB-70-t) 3: A comparison between characteristics

predicted from wind-tunnel measurements and those

measured in fhght

INASA-TP-15161 p 14 N80-17986

Superson=c cruise technology

tNASA-SP-472J p 4 N85-28912

BACKGROUND NOISE

Effects of road traffic background noise on judgments

of individual airplane noises

JNASA-TP-1433J p 148 N79-28796

Aliased noise in radiometric measurements

I NASA-TP-1639} p t 14 N80-22660

BACKSCATTERING

Lidar beckscattering measurements of background

stratospheric aerosols

[NASA-TP-1381 } p 152 N79-17388

Ozone climatology senes. Volume 1: Atlas of total

ozone, April 1970 - December 1976

[NASA-RP-t098] p 154 N83-16992

A-18

NASAtMSFC FY-84 Atmospheric Processes Research

Review

INASA-CP-2329] p 166 N84-34829

Airborne Lidar measurements of aerosols, mixed layer

heights, and ozone during the 1980 PEPE/NEROS summer

field experiment

INASA-RP-1143] p 150 N86-16748

Airborne lidar measurements of El Chichon stratoshperic

aerosols

[NASA-RP-11661 p 156 N86-27835

BACTERIA

Description and field test of an in situ coliform monitoring

system

[NASA-TP-13341 p 148 N79-14591

BAFFLES

A study of resonant-cavity and fiberglass-filled parallel

baffles as duct silencers --- for wind tunnels

[NASA-TP-1970] p 188 N82-24052

Liquid management in low gravity using baffled rotating

containers

(NASA-TP-2263] p 111 N84-15427

BALL BEARINGS

Statistical model for asperity-contact time fraction in

elastohydrodynamic lubrication

[NASA-TP-1130] p 119 N78-18429

Predicted end experimental performance of

jet.lubricated 120-millimeter-bore ball bearings operating

to 2.5 million DN

{NASA-TP-1196J p 119 N78-20513

Rolling-element fatigue life of AISI M-50 and 18.4.1

balls

[NASA-TP.12021 p 119 N76-21473

Some effects of composition on friction and wear of

graphite-fiber-reinforced potyimide liners in plain sphencal

bearings

{NASA-TP-12291 p 119 N78-25433

Ferrographic analysis of wear debris from full-scale

bearing fatigue tests

{NASA-TP-1511] p 121 N79-31605

Comparison of predicted and measured

elastohydrodynamic film thickness in • 20-millimeter-bore

ball bearing

[NASA-TP-1542] p 121 N79-32552

Correlation of asperity contact-time fraction with

elastohydro,dynamic film thickness in a 20-millimeter-bore

ball bearing

[NASA-TP-1547] p 121 N79-33476

Operating characteristics of high-speed, jet-lubricated

35-mitlimetor-bore bell bearing with a

single-outer-land-guided cage

{NASA-TP-16571 p 121 N80-21753

Effect of cage design on characteristics of

high-speed-jet-lubricated 35-millimeter-bore ball bearing ---

lurbojet engines

{NASA-TP-17321 p 121 N80-33749

Performance of jet- and inner-ring-lubricated 35

millimeter bore ball bearings operating to 2,5 million DN

{NASA-TP-1806} p 122 N81-19458

Life analysis of multiroller planetary traction drive

INASA-TP-1710} p 122 N81-20423

Rolling-elemenl fatigue life of AMS 5900 balls

INASA-TP-2080} p 122 N83-16758

Comparison of predicted and experimental thermal

performance of angular-contact ball bearings

[NASA-TP-2275J p 123 N84-18654

Effect of two inner-hog oil-flow distribution schemes on

the operating characteristics of a 35 millimeter bore ball

bearing to 2,5 million DN

{NASA-TP-2404] p 124 N85-13233

Mechanics of a gaseous film barrier to lubricant wetting

of elastohydrodynemicaity lubricated conjunctions

[NASA-TP-25001 p 125 N85-32330

BALLISTICS

Effect of low-velocity or ballistic impact damage on the

strength of thin composite and aluminum shear panels

{NASA-TP-2441 } p 83 N85-26924

BALLS

Characterization of wear debris generated in accelerated

rolling-element fatigue tests

INASA-TP-1203} p 119 N78-21470

BANDWIDTH

Analysis of rectangular microstrip antennas

INASA-TP-22761 p 100 N84-20735

BAROCLINIC INSTABILITY

NASA/MSFC FY-84 Atmosphenc Processes Research

Review

INASA-CP-2329} p 166 N84-34829

Three-dimensional bareclinic instability of a Hadley cell

for small Richardson number

[NASA-TP-2450} p 166 N65-20605

BAROCLINIC WAVES

The wave structures of the Eady model of baroclinic

instability

I NASA-TP-1548 / p 160 N79-32796

SUBJECT INDEX

The Numerical Studies Program for the Atmospheric

General Circulation Experiment (AGCE) for Spacelab

Flights

[NASA-CP-2200J p 163 N82-12715

Current Scientific Issues in Large Scale Atmospheric

Dynamics

[NASA-CP-2410J p 167 N86-24082

BAROCLINITY

The effects of curvature and viscosity on baroclinic

instability: A two-layer model

{NASA-TP-1328} p 159 N78-32641

Baroclinic instability with variable gravity: A perturbation

analysis

{NASA-TP-1586J p 136 N80-15445

BARRIER LAYERS

Feasibility study of tungsten as a diffusion barrier

between nickel-chromium-aluminum and Gamma/Gamma

prime - Delta eutectic alloys

INASA-TP-1131 j p 86 N78-15230

BASALT

Lunar sample studies --- breccias baselts, end

anorthosites

[NASA.SP-418] p 204 N77-27053

Results of analyses performed on basalt adjacent to

penetrators emplaced into volcanic rock at Amboy,

California, April 1976

[NASA-TP-1026J p 199 N77-33003

BATCH PROCESSING

GCKP84-general chemical kinetics code for gas-phase

flow and batch processes including heat transfer effects

[NASA-TP-2320] p 85 N84-32446

BEADS

Solid spherical glass particle impingement studies of

plastic materials

[NASA-TP-2161) p 95 N83-24695

Time dependence of solid-particle impingement erosion

of an aluminum alloy

[NASA.TP-2169) p 89 N83-32908

Erosion of iron-chromium alloys by glass particles

[ NASA-TP-2354} p 90 N84-28965

Fabrication and evatuabon of suparplestically

formed/weld-brazed corrugated compression panels wtth

beaded webs

[NASA-TP-2512} p 90 N86-13406

BEAMS (RADIATION)

Textured carbon on copper: A novel surface with

extremely low secondary electron emission

characteristics

[NASA-TP-2543} p 96 N86-15394

BEAMS (SUPPORTS)

Evaluation of a hybrid, anisotropio, multileyored,

quadrilateral finite element

{NASA-TP-12361 p 127 N78-28482

Swing-arm beam erector (SABER) concept for single

astronaut assembly of space structure

{NASA-TP-2379J p 75 N85-19015

Nonlinear equations for dynamics of pretwisted beams

undergOing small strains and large rotations

[NASA-TP-2470] p 134 N85-27258

Joint research effort on vibrations of twisted plates,

phase 1: Final results

{NASA-RP-1150} p 135 N86-10579

BEARING ALLOYS

Effect of double vacuum melting and retained austenite

on rolling-element fatigue life of AMS 5749 bearing steel

[NASA-TP-1060] p 119 N77-33520

Long-term hot-hardness characterisbcs of five

through-hardened beanng steels

[NASA-TP-1341 I p 87 N78-33196

Effect of carbide distribution on rolling-element fatigue

life of AMS 5749

iNASA-TP-2189} p 123 N83-33166

BEARINGS

Effect of geometry on hydrodynamic film thickness

{NASA-TP-1287} p 119 N78-30585

A microprocessor-based table lookup approach for

magnetic bearing linearization

[NASA-TP-1838J p 101 N81-22281

Rolling-element fatigue life with traction fluids end

automatic transmission fluid in a high-speed rolling-contact

rig

[NASA-TP-20501 p 122 N83-13457

Passive eddy-current damping as a means of vibration

control in cryogenic turbomachinery

{NASA-TP-25621 p 68 N86-24722

BED REST

Physiological responses of women to simulated

weightlessness: A review of the first female bed-rest

study

(NASA-SP-430J p 170 N79-13686

BENDING FATIGUE

Analysis of surface cracks in finite plates under tension

or bending toads

[NASA-TP-1578] p 129 N80-13512
SUBJECT INDEX BLUNT BODIES

BENZENE

Chemical kinetic modeling of benzene and toluene

oxidation behind shock waves

[NASA-TP-1472] p 84 N79-28259

Fuel-rich catalytic combustion: A soot-free technique

for in situ hydrogen-like enrichment

[NASA.TP-2498] p 85 N85-31244

BERYLLIUM

Fnction and wear of selected metals and alloys in sliding

contact with AISt 440 C stainless steel in liquid methane

and in liquid natural gas

[NASA-TP-1150] p 119 N78-20512

BETA FACTOR

Fabrication and evaluation of cold/formed/watdbrazed

beta-titanium skin-stiffened compression panels

[NASA-TP-2201] p 89 N83-35100

BIAS

Circuit transients due to negative bias arcs on a

high.voltage solar array in low Earth orbit

[NASA-TP.2407] p 75 N85-14858

BIBLIOGRAPHIES

Secondary aerospace battaries and battery materials:

A bibliography, 1969. 1974

[NASA-SP-7044] p 144 N77.16437

Cryogenic foam insulation: Abstracted publications

[NASA-RP-1002] p 79 N78-11200

Bibliography of Supersonic Cruise Aircraft Research

(SCAR)

[NASA.RP.1003] p 197 N78-12895

A bibliography on the search for extraterrestrial

intelligence

[NASA.RP-f021] p 199 N78-21019

eGO program summary, supplement 1 --- updated

bibliography for all eGO missions and scientific results

from eGO 5 and 6 missions

[NASA.SP-7601.SUPPL-1] p 151 N79-13601

Anthropometric source book. Volume 3: Annotated

bibliography of anthropometry

[NASA-RP-1024-VOL-3) p 173 N79-13712

Second International Colloquium on Mars: Abstracts

for a colloquium --- bibliography

[NASA-CP-2072] p 205 N79-16757

Survey and bibliography on attainment of laminar flow

control in air using pressure gradient and suction, volume

1

[NASA-RP-1035] p 107 N79-33438

Bibliography of Supersonic Cruise Research (SCR)

program from 1977 to mid-1980

[NASA-RP-1063] p t6 N81-14973

A catalog of NASA special publications

[NASA-SP-449] p 212 N81-21995

Data bases and data base systems related to NASA's

Aerospace Program: A bibliography with indexes

[NASA-SP-7048] p 197 N83-22010

Records of achievement: NASA special publications

[NASA-SP-470] p 197 N83-33792

Energy: A continuing bibliography with indexes, issue

40, January 1984

[NASA-SP-7043(40)l p 146 N84-21977

Catalog of infrared observations including: Bibliography

of infrared astronomy and index of infrared source

positions

[NASA-RP-1118} p 202 N84-26520

Bibliography of Supersonic Cruise Research (SCR)

program from 1980 to 1983

[NASA-RP-1117] p 24 N84-27674

The human factor: Biomedicine in the manned space

program to 1980

[NASA-SP-4213] p 170 N86-21097

Aerospace Medicine and Biology: A Cumulative tndex

to the 1985 Issues

[NASA-SP-7011(280)] p 170 N86-23265

A cumulative index to a continuing bibliography on

aeronautical engineering

[NASA-SP-7037(196)] p 5 N86-23552

Management: A bibliography for NASA Managers

[NASA-SP-7500(20)] p 196 N86-27108

NASA patent abstracts bibliography: A continuing

bibliography. Section 1: Abstracts

[NASA-SP-7039(29)-SECT-1 ] p 198 N86-28788

NASA Patent Abstracts Bibliography. A continuing

bibliography. Section 2: Indexes (Supplement 29)

[NASA-SP-7039(29)-SECT-2] p 198 N86-28789

Astronaubcs and aeronautics, 1977: A chronology

[NASA-SP-4022] p 213 N86-31524

Earth resources: A continuing bibliography with indexes,

issue 50

[NASA-SP-7041(50)) p 143 N86-31940

Aerospace medicine and biology: A continuing

bibliography with indexes (supplement 288)

[NASA-SP-7011(288)] p 171 N86-32088

Aeronautical engineering: A continuing bibliography with

indexes (supplement 204)

[NASA-SP-7037{204)] p 5 N86-32389

BINARY ALLOYS

Geometric relationships for homogenization in

single-phase binary alloy systems

[NASA-TP-1349| p 87 N79-13137

Effect of concentration dependence of the diffus=on

coefficient on homogenization kinetics in multiphese binary

alloy systems

[NASAoTP-1281] p 87 N79-13138

Adhesion and friction of iron-base binary alloys in contact

with silicon carbide in vacuum

[NASA.TP-1604] p 87 N80-15234

BIOASTRONAUTICS

Space Gerontology

{NASA-CP-2248] p 170 N83-16018

The cosmic history of the biogenic elements and

compounds

[NASA-SP-476] p 175 N85-28562

BIODYNAMICS

The use of nonhuman primates in space

{NASA-CP-O05] p 169 N78-11663

Twentieth Annual Conference on Manual Control,

volume 1

[NASA-CP-2341-VOL-1 ] p 174 N85-14487

BIOGEOCHEMISTRY

Report of the NASA working group on tropospheric

program planning

[NASA-RP-1062] p 153 N81.23742

Global Biology Research Program: Biogeochemical

Processes in Wetlands

[NASA-CP-2316] p 169 N84-30665

BIOLOGICAL EFFECTS

Apollo.Soyuz test project. Volume 1: Astronomy, earth

atmosphere and gravity field, life sciences, and materials

processing

[NASA-SP-412] p 60 N78-17088

Controlled ecological life support system - biological

problems

[NASA-CP-2233] p 173 N82-24836

The cosmic history of the biogenic elements and

compounds

[NASA.SP.476] p 175 N85-28562

Aerospace Medicine and Btotogy: A Cumulative Index

to the 1985 Issues

[ NASA-SP-70t 1(280) ] p 170 N86-23265

Aerospace medicine and biology: A continuing

bibliography with indexes (supplement 288)

[NASA-SP-7011(288)] p 171 N86-32088

BIOLOGICAL EVOLUTION

Human Neurological Development: Past, Present and

Future

{NASA-CP-2063} p 212 N79-15887

Life in the Universe

[NASA-CP-2156] p 175 N82-20884

The 1st Symposium on Chemical Evolution and the

Origin and Evolution of Life

[NASA-CP-2276] p 79 N83-24556

Search for the universal ancestors

{NASA-SP-477] p 175 N85-32777

Second Symposium on Chemical Evolution and the

Origin of Life

(NASA-CP-2425] p 175 N86-26844

BIOMASS

Proceedings of the National Conference on Energy

Resource Management Volume 2: Applications

[E83-10336] p 142 N83-26176

BIOMEDICAL DATA

Biomedical results from Skylab

[NASA-SP-377) p 169 N77-33780

The human factor: Biomedicine in the manned space

program 1o 1980

[NASA-SP-4213] p 170 N86-21097

BIOMETRICS

Anthropometric source book Volume 2: A handbook

of anthropometric data

[NASA-RP-1024-VOL-2J p 172 N79-13711

Anthropometric source book. Volume 3: Annotated

bibliography of anthropometry

[NASA-RP-1024-VOL-3] p 173 N79-13712

BIOPROCESSlNG

Second Symposium on Space Industrialization --- space

commercialization

[NASA-CP-2313] p 63 N85-11011

BIOSYNTHESIS

NASA Space Biology Program Eighth annual

symposium's program and abstracts

[NASA-CP-22991 p 169 N84-18829

BIPOLAR TRANSISTORS

Programmable, automated transistor test system

[NASA-TP-2554] p 103 N86-21755

BIREFRINGENCE

Pockels-effect cell for gas-flow simulation

[NASA-TP*2007] p 115 N82-23515

BIT ERROR RATE

High-density digital recording

[NASA-RP-11111 p 103 N86-14498

BLACK BODY RADIATION

A blackbody-pumped CO2-N2 transfer laser

[NASA-TP-2347| p 118 N84-31617

BLADE TIPS

Cold-air pedormance of a

12 766-centimeter-tip-diameter axial-flow cooled turbin e

3: Effect of rotor tip clearance on overall performance

of a solid blade configuration

[NASA-TP-1032] p 5 N77-32082

In-place recalibration technique applied to a

capacitance-type system for measuring rotor blade tip

clearance

[NASA-TP-1110] p42 N78-22101

Experimental investigation of effects of blade tip

geometry on loads and performance for an articulated rotor

system

[NASA-TP.1303] p 33 N79-15938

Evaluation of helicopter noise due to b blade-vortex

interaction for five t0p configurations --- conducted in the

Langley V/STOL tunnel

[NASA-TP-1608] p 187 N80.14840

Forward acoustic performance of a shock-swallowlng

high-tip-speed fan (QF-13)

[NASA.TP-1668] p 187 N80-23100

Effects of geometric variables on rub characteristics of

Ti-6AI.4V

[NASA-TP-1835] p 88 N81.20245

Wind-tunnel investigation of the effects of blade tip

geometry on the interaction of torsional loads and

performance for an articulated helicopter rotor

[NASA-TP-1926] p 18 N82-13107

Analytic investigation of effect of end.wall contouring

on stator performance

[NASA-TP-1943] p 19 N82-14051

Rotor tip clearance effects on overall and blade.element

performance of axial.flow transonic fan stage

[NASA-TP-2049] p 49 N82-33389

Aerodynamic effect of a honeycomb rotor tip shroud

on a 50.8-centimeter-tip-diameter core turbine

[NASA.TP-2112] p 49 N83-17547

BLADES

Suckling and structural efficiency of sandwich-blade

stiffened composite compression panels

[NASA-TP-1269] p 127 N78-32492

BLOCKING

Current Scientific issues in Large Scale Atmosphehc

Dynamics

[NASA-CP-2410] p 167 N86-24082

BLOOD

Design of a blood-freezing system for leukemia

research

[NASA-TP-1165] p 169 N78-18673

BLUNT BODIES

A study of the sonic-boom characteristics of a blunt body

at a Mech number of 4.14

[NASA-TP-1015] p 1 N77-32072

Effects of mass addition on blunt.body boundary-layer

transition and heat transfer

[NASA-TP-1139] p 104 N78-16326

Forebody and afferbody solutions of the Nav_er-Stokes

equations for supersonic flow over blunt bodies in a

generalized orthogonal coordinate system

[NASA-TP-1075] p 104 N78-18362

Invisck:l, nonadiabatic flow fields over blunt, sonic corner

bodies for outer planet entry conditions by a method of

integral relations

[NASA-TP-1133] p 104 N78-18363

Solution of axisymmetric and two-dimensional inviscid

flow over blunt bodies by the method of lines

[NASA-TP-1154] p 105 N78-22332

Sonic-boom minimization with nose-bluntness

relaxation

[NASA-TP-1348] p 10 N79-15000

Measured and predicted shock shapes and aerodynamic

coefficients for blunted cones at incidence in helium st

Mach 20.3

(NASA-TP-1395] p 106 N79-20345

A hybridized method for computing

high-Reynolds-number hypersonic flow about blunt

bodies

[NASA-TP-1497] p 107 N79-33441

Application of a numerically generated orthogonal

coordinate system to the solution of inviscid axisymmetdc

supersonic flow over blunt bodies

{NASA-TP-1619] p 14 N80-19031

Measured and predicted shock shapes and aerodynamic

coefficients for blunted cones at incidence in air at Mach

59

[NASA-TP-1652] p 108 N80-23600

A study of the sonic-boom characteristics of a blunt body

at a Mach number of 6

[NASA-TP-1787] p 3 N81-13915

Aerodynamic heating on the corrugated surface of a

10,2 dog half-angle blunted cone at Mach 67

[NASA-TP-1928) p 109 N82-13383

A-19
BOAT'rAILS SUBJECT INDEX

Wind-tunnel investigation of leading-edge thrust on

arrow wings in supersonic flow

{NASA-TP-2167J p 21 N83-31577

BOATTAILS

Computation of transonic boattail flow with separation

JNASA-TP-1070] p 7 N78-13017

Boundary-layar separation on isolated boattail nozzles

[NASA-TP-1226] p 9 N78-30052

investigation of the flow field surrounding circular-arc

boat'tail nozzles at subsonic speeds

[NASA-TP-1633] p 14 N80-22262

Numerical solutions of the Navier-Stokes equations for

transonic afterbody flows

INASA-TP-17841 p 16 N81-t39t9

Experimental and analytical investigation of

axisymmetric supersonic cruise nozzle geometry at Mach

numbers from 060 to t 30

[NASA-TP-1953J p 19 N82-14052

BODY MEASUREMENT (BIOLOGY)

Anthropometdc source book. Volume 2: A handbook

of anthropometric data

{NASA-RP-t024-VOL-2J p 172 N7g-1371t

Anthropometnc source book. Volume 3: Annotated

bibliography of anthropometry

[NASA-RP-1024-VOL-3} p 173 N79-13712

BODY-WING AND TAIL CONFIGURATIONS

GEMPAK: An arbitrary aircraft geometry generator

[NASA-TP-1022] p 32 N78-16042

Aerodynamic characteristics st Mech 6 of a wing-body

concept for a hypersonic research airplane

[NASA-TP-1249] p 9 N78-30055

Expenmentat and theoretical supersonic

lateral-directional stability characteristics of a simplified

wing-body configuration with a series of vertical-tail

arrangements

[NASA-TP-18781 p 17 N81-29095

Fuselage and nozzle pressure distributions of a

1/12-scale F-15 propulsion model at transonic speeds

Effect of fuselage modifications and nozzle variables

[NASA-TP-2333] p 24 N84-32354

Supersonic aerodynamic characteristics of canard,

tailless, and aft-tail confi.gurat=ons for 2 wing planforms

[NASA-TP-2434] p 26 N85-27822

BODY-WING CONFIGURATIONS

Aerodynamic characteristics at Math number 0.2 of a

wing-body concept for a hypersonic research airplane

INASA-TP-t 189J p8 N78-25059

Effects of wing leading-edge flap deflections on subsonic

longitudinal aerodynamic characteristics of s wing-fuselage

configuration with a 44 deg swept wing

[NASA-TP-t351 ] p t0 N79-13002

Aerodynamic characteristics at Mach numbers of 1.5.

1.8, and 2.0 Of a blended wing-body configuration with

and without integral canards

[NASA-TP-1427J p 12 N79-23013

An analytical procedure for computing smooth

transitions between two specified cross sections with

applications to blended wing body configuration

[NASA-TP-2012] p 19 N82-25t93

Aaropropulsive characteristics of twin

single-expansion-ramp vectoring nozzles installed with

forward-swept wings and canards --- transonic tunnel

tests

[NASA-TP-2133] p 20 N83-22161

Body and canard effects on an attached-flow maneuver

wing at Mach t.62

[NASA-TP-2249] p 23 N84-18163

Effects of upper-surtace nacelles on longitudinal

aerodynamic characteristics of high-wing transport

configuration

INASA-TP-2579| p 28 N86-23562

BOEING 720 AIRCRAFT

Impact data from a transport aircraft during e controlled

impact demonstration

[NASA-TP-2589J p 38 N86-30721

BOEING 747 AIRCRAFT

Airframe noise of a small mode_ transport aircraft and

scaling effects --- Boeing 747

{NASA-TP-1858] p 188 N81-22832

BOLTS

Experimental data on single-bolt joints in quasi isotropic

graphite/potyimide laminates

[NASA-TP-20f5} p 81 N82-25325

BONDING

Advances in engineering science, volume 1

[NASA-CP-200f-VOL-1I p 98 N77-10230

BOOMS (EQUIPMENT)

Vibration characteristics of a deployable

controllable-geometry truss boom

[NASA-TP-2160] p t32 N83-28491

BOOSTER ROCKET ENGINES

Thermodynamic and chemical parameters of the

exhaust effluents from the HARPOON booster motor

INASA-TP-1280] p 147 N78-28682

Feasibility study of LtTVC for shuttle SRB

[NASA-TP-19t2] p 77 N81-33231

BORIDES

Friction and wear of radiofrequency-sputtered borides,

silicides, and carbides

INASA-TP-1156] p 91 N78-20338

BORON

Tensile stress-strain behavior of boron/aluminum

laminates

INASA-TP-11"I7] p 79 N78-18135

Effects of fabrication and joining processes on

compressive strength of boron/aluminum and

borsic/aluminum structural panels

[ NASA-TP-1 t 21 ] p 80 N78-20256

Experimental and analytical investigation of the fracture

processes of boron/aluminum laminates containing

notches

[NASA.TP-2187] p 82 N83-33956

BORON REINFORCED MATERIALS

Long-tarm thermal degradation and alloying constituent

effects on five boron/aluminum composites

[NASA-TP-1977] p 81 N82-22317

Fabrication and evaluation of brazed titanium-clad

Borsic/alumiflum compression panels

[NASA-TP-1573] p 82 N83-28100

BORSIC (TRADENAME)

Mechanical property characterization of

Elorsic/aluminum laminates at room and elevated

temperatures

[NASA-TP-1761 ] p 81 N81-16130

Fabrication and evaluation of brazed titanium-clad

bors_c/aluminum skin-stringar panels

[NASA-TP-1674] p 82 N83-28098

BOUNDARIES

Stability boundaries for systems with frequency-model

feedback and complacency filter

[NASA-TP-t744J p 184 N81-I0789

BOUNDARY ELEMENT METHOD

Research in structural and solid mechanics. 1982

[NASA-CP-2245] p 131 N82-33739

Nonlinear Structural Analysis

[NASA-CP-2297] p 133 N84-3t688

BOUNDARY INTEGRAL METHOD

Numerical Techniques in Acoustics

[NASA-CP-240.4] p 190 N86-12007

BOUNDARY LAYER CONTROL

Survey and bibliography on attainment of laminar flow

control in air using pressure gradient and suction, volume

t

[NASA-RP-1035] p 107 N79-33438

Static and trans,,ent performance of YF-t 02 engine with

up to 14 percent core airbioed for the quiet short-haul

research aircraft

{NASA-TP-1692] p 47 N80-25339

Amplified crossflow disturbances in the laminar boundary

layer on swept wings with suction

[NASA-TP-1902] p 109 N82-11391

Laminar Flow Control. The Research and Technology

Studies 1981

[NASA-CP-2218J p 19 N82-20149

Studies of sidewall boundary layer in the Langley 0.3

meter transonic cryogenic tunnel with and without

suction

[NASA-TP-2096_ p 110 N83-20031

Experimental investigation of tangential blowing applied

to a subsonic V/STOL inlet

[NASA-TP-2297] p 23 N84-20493

Aerodynamic design of the contoured wind-tunnel liner

for the NASA supercntical, laminar-flow-control,

swept-wing experiment

[NASA-TP-23351 p 24 N84-33377

BOUNDARY LAYER EQUATIONS

Critical study of h_har order numerical methods for

solving the boundary-layer equations

[NASA-TP-1302| p 106 N79-t3305

Calculation of laminar heating rates on

three-dimensional configurations using the axieymmetric

analogue

{NASA-TP-1698] p 108 N80-33719

Slip-boundary equations for multicomppnent

nonequiliorium airflow

[NASA-TP-2452} p t13 N86-14530

BOUNDARY LAYER FLOW

Inverse boundary-layer theory and companson with

experiment

[NASA-TP.t208} p 106 N78-32385

Aerothermal analysis of a wing-elevon cove with variable

leakage

[NASA-TP-1703] p 108 N80-32692

Wind-tunnel measurements and comparison with flight

of the boundary layer and heat transfer on a hollow cylinder

at Mach 3

[NASA.TP-1789] p 16 N81-14975

GRID30: Computer program for fast generation ol

multilevel, three-dimensional boundary-conforming O-type

computational grids

[NASA-TP-1920J p 18 NBt-31128

High Reynolds number research - 1980

{NASA-CP-2183} p 18 N8t-31130

Gorfter vortices and transition in wall boundary layers

of two Milch 5 nozzles

[NASA-TIp-t8691 p 109 N81-3150g

Force and moment, flow-visualization, and

boundary-layer tests on a shuttle orbiter model at Mach

6

INASA-TP-19521 p 18 N82-13106

Wall-temperature effects on the aerodynamics of a

hydrogen-fueled transport concept in Mach 8 blowdown

and shock tunnels

{NASA-TP-21591 p 2t N83-30391

BOUNDARY LAYER SEPARATION

Boundary-layer separation on isolated boattail nozzles

{ NASA-TP-1226 J p9 N78-30052

Investigation of flow characteristics over missile bodies

at supersonic speeds

INASA-TP-1579] p 13 N80-t3001

Some flow phenomena associated with aligned,

sequential apertures with Borda-type inlets --- inlet

pressure and flow separation

[NASA-TP-t792} p 109 N81-24387

Effect of leading-edge load constraints on the design

and performance of supersonic wings

INASA-TP-2446] p 26 N85-29923

BOUNDARY LAYER STABILITY

Status of linear boundary-layer stab=hty and the e to the

nth method, with emphasis on swept-wing applications

[ NASA-TP- 1645 ] p 108 N80-22633

The application to airfoils of a techn_ue for reducing

orifice-induced pressure error at high Reynolds numbers

INASA-TP-2537J p 27 N86-2035f

BOUNDARY LAYER TRANSITION

Effects of roughness size on the pos4tion of

boundary-layer transition and on the aerodynamic

characteristics of a 55 deg. swept delta wing at supersonic

speeds

INASA-TP-t027] p 7 N78-f3016

Effects of mass addition on blunt-body boundary-layer

transition and heat transfer

NASA-TP-tf391 p 104 N78-16326

Characteristics of Mach 10 transitional and turbulent

boundary layers

NASA-TP-1243| p 106 N79-14328

Noise reduction in a Mach 5 wind tunnel with a

rectangular rod-wall sound shield

NASA-TP-1672I p t08 N80-26622

In-flight transition measurement on a 10 deg cone at

Mach numbers from 05 to 20

NASA-TP-1971 ] p 19 N82-26227

Free-stream noise and transibon measurements on a

cone in a Mach 35 pilot low-disturbance tunnel

NASA-TP-2180 ] p 111 N83-34229

Correlations of supersonic boundary-layer transition on

cones including effects of large axial variations in

wind-tunnel noise

[NASA-TP-2229 ] p 111 N84-17534

Aerotbermal tests of a 12.5 percent cone at Mach 6.7

for various Reynolds numbers, angles of attack and nose

shapes --- conducted in Langley 8-foot high temperature

tunnel

[NASA-TP-23451 p 1 f2 N85-17322

Flight-measured _aminar boundary-layer transition

phenomena including stability theory analysis

[NASA-TP-2417J p 25 N85-2tt18

Transition in Turbines

[NASA-CP-2386J p 113 N85-31433

BOUNDARY LAYERS

Prediction method for two-dimensional aerodynamic

losses of cooled vanes using integral boundary-layer

parameters

[NASA*TP-1623] p t4 N80-17030

Description and calibration of the Langley unitary plan

wind tunnet

INASA-TP-19051 p 18 N82-12035

Pressures measured in flight on the aft fuselage and

exlarnal nozzle of a twin-jet fighter

[NASA-TP-2017] p 2t N83-25665

Mach 6 flow field surveys beneath the forebody of an

airbreathing missile

[NASA-TP-2491 ] p 28 N86-23558

R4 airfoil data corrected for sidewall boundary-layer

effects in the Langley 03-meter transomc cryogenic

tunnel

[NASA-TP-2565J p 28 N86-24662

BOUNDARY LUBRICATION

Wear of aluminum and hypoeutectic aluminum-silicon

alloys in boundary-lubricated pin-on disk sliding

[ NASA-TP-1442 } p 87 N79-2t t 84

Steady-state wear and friction in boundary lubrication

studies

[NASA-TP-1658) p 93 N80-22493

Steady-state boundary lubrication with formulated

C-ethers to 260 C

[NASA-TP-t812] p 94 N81-21193

A-20
SUBJECT INDEX CANTILEVER BEAMS

Lubrication of machine elements

[NASA-RP-11261 p 124 N84-31640

BOUNDARY VALUE PROBLEMS

Numerical grid generation techniques ---conference

[NASA-CP-2166] p 182 N81-14690

Numerical Boundary Condition Procedures

[NASA-CP-2201] p 182 N81-33856

BRAKING

Wear, fricUon, and temperature characteristics of an

aircraft tire undergoing braking and cornering

[NASA-TP-1569I p 29 N80-13013

Dynamics of aircraft antiskid braking systems ---

conducted at the Langley aircraft landing loads and traction

facility

{ NASA-TP-1959] p35 N82-18204

Tire tread temperatures durin 9 antiskid braking and

cornering on a dry runway

[NASA-TP-2009J p 35 N82-24193

Brakin 9 and cornenn 9 studies on an air cushion landing

system

(NASA-TP-2198] p 36 N83-34935

BRAYTON CYCLE

Technology for Bayton-cycle powerplants using solar

and nuclear energy

INASA-TP-25581 p 78 N86-21577

BRAZING

Fabrication and evaluation of brazed titanium-clad

borsic/aluminum skin-stringer panels

{NASA-TP-1674] p 82 N83-28098

Fabrication and evaluation of superplasticalty

formed/weld-brazed corrugated compression panels with

beaded webs

[NASA-TP-2512] p 90 N86-13406

BRECCIA

Lunar sample studies --- breccias basalts, and

anorthosites

[NASA-SP-418] p 204 N77-27053

BRIGHTNESS TEMPERATURE

Sea-surface temperature and salinity mapping from

remote microwave radiometric measurements of

brightness temperature

[NASA-TP-1077] p 168 N79-28863

Antartic sea ice, 1973 1976: Satellite

passive-microwave observations

[NASA-SP-459] p 168 N84-10718

BROADBAND

SETI science working group report

[NASA-TP-2244] p 175 N84-22178

Location of noise sources using a phase-slope

method

[NASA-TP-2505] p 191 N86-16041

BUBBLES

Fluid surface behavior in low gravity, Center

discretionary fund no. 83-21

[NASA-TP-2486] p 113 N85-28260

BUCKLING

Effect of end-ring sbftness on buckling of

pressure-loaded stiffened conical shells

[NASA-TP-1079] p 127 N78-12475

Stress analysis and buckling of J-stiffened

graphite-epoxy panel

[NASA-TP-1607] p 129 N80-18427

Buckling test of a 3-meter-diameter corrugated

graphite-epoxy nng-stiffened cylinder

[NASA-TP-2032] p 131 N82-28665

Buckling and failure characteristics of graphite-polyimide

shear panels

[NASA-TP-2153] p 82 N83-24561

A solution procedure for behavior of thick plates on a

nonlinear foundation and postbuckling behavior of long

plates

[NASA-TP-2174] p 132 N83-34373

Buckling loads of stiffened panels subjected to combined

longitudinal compression and shear: Results obtained with

PASCO, EAL, and STAGS computer programs

[NASA-TP-2215] p 132 N84-16585

An approximate buckling analysis for rectangular

orthotropic plates with centrally located cutouts

[NASA-TP-2528] p 135 N86-20856

BUDGETING

Managing NASA in the Apollo era

{NASA-SP-4102] p 196 N83-18551

BUFFER STORAGE

A design approach to real-time formatting of high speed

multispectral image data

[NABA-TP-1870] p 178 N81-25690

BUFFETING

Flight-measured buffet characteristics of a supercritical

wing and a conventional wing on a variable-sweep

airplane

[NASA-TP-1244] p 8 N78-23056

BUILDINGS

An evaluation of the NASA Tech House, including live-in

test results, volume 1

[NASA-TP-1564] p 145 N80-11559

Lessons of the NASA Tech House

[NASA-SP-442] p 199 N80-27219

BUMPERS

Meteoroid bumper experiment on Explorer 46

[NASA-TP-1879] p 72 N81-29155

BUOYANCY

A mobile work station concept for mechanically aided

astronaut assembly of large space trusses

{NASA-TP-2108] p 74 N83-19808

BUOYS

Free Drifting Buoys

[NASA-CP-2003] p 167 N77-16675

BURNERS

A high-pressure premixed flat-flame burner for chemical

process studies --- of pollutant formation in hydrocarbon

flames

INASA-TP-1318] p 84 N79-14177

Pollutant emissions from fiat-flame burners at high

pressures

INASA-TP-1673] p 85 N80-25392

BYPASSES

A throat-bypass stability-bleed system using relief valves

to increase the transient stability of a mixed-compression

inlet --- YF-12 aircraft inlet tests in the Lewis 10 by 10 ft

supersonic wind tunnel

{NASA-TP-1083] p 45 N79-28176

Dynamic response of a Mach 2.5 axisymmetric inlet and

turbojet engine with a poppet-value controlled inlet stability

bypass system when subjected to internal and external

airflow transients

[NASA-TP-1531 ] p 45 N80-14123

C

C-135 AIRCRAFT

The effects of motion and g-seat cues on pilot simulator

performance of three piloting tasks

[NASA-TP-1601I p 34 N80-15069

Wind tunnel investigation of an all flush orifice air data

system for a large subsonic aircraft --- conducted in a

Langley 8 foot transonic pressure tunnel

[NASA-TP-1642] p 38 N80-23304

KC.135 Winglet Program Review

[NASA-CP-2211 ] p 24 N84-27686

C-15 AIRCRAFT

Quiet powered-lift propulsion

[NASA-CP-2077] p 46 N80-15t27

CABIN ATMOSPHERES

Ozone concentration in the cabin of a Gates Learjet

measured simultaneously with atmospheric ozone

concentrations

[NASA-TP-1349] p t48 N78-33618

Analysis of atmospheric ozone levels at commercial

airplane cruise altitudes in winter and spring, 1976 - 1977

--- Global Atmospheric Sampling Program

[NASA-TP-1807J p 163 N81-21685

CABLES (ROPES)

Results from tests, with van-mounted sensor, of

magnetic leader cable for aircraft guidance during roll-out

and turnoff

[NASA-TP-2092] p 40 N83-16338

CALCIUM

The Regulatory Functions of Calcium and the Potential

Role of Calcium in Mediating Gravitational Responses in

Cells and Tissues

[NASA-CP-2286] p 169 N84-11720

CALCULATORS

Simplified sonic-boom prediction --- using aerodynamic

configuration charts and calculators or slide rules

[NASA*TP-lt22) p 7 N78-20078

Planning fuel-conservative descents with or without time

constraints using a small programmable calculator:

Algorithm development and flight test results

[NASA-TP-2085} p 40 N83-17535

CALIBRATING

A flight evaluation of a trailing anemometer for low-speed

calibrations of airspeed systems on research aircraft

[NASA-TP-1135] p 32 N78-18044

Airflow and thrust calibration of an F100 engine, S/N

P680059, at selected flight conditions

[NASA-TP-1069] p 42 N78-21112

A small gas inlet system for orbital mass-spectrometer

calibrations

{NASA-TP-t1701 p 114 N78-21430

A feasibility study of ion implantation techniques for mass

spectrometer calibration

[NASA-TP-1185] p 114 N78-21431

Total ozone measurement: Intercomparison of

prototype New Zealand filter instrument and Dobson

spectrophotometer

[NASA-TP-1277] p 114 N78-28412

Condensation-nuclei (Aitken Particle) measurement

system used in NASA global atmospheric sampling

program

[NASA-TP-1415I p 148 N79-18479

NASA Metrology and Calibration, 1980

{NASA-CP-2174] p 115 N81-23432

LANDSAT-4 Science Investigations Summary, including

December 1983 Workshop results, volume 1

[E84-10166} p 137 N84-30359

Results of the first complete static calibration of the

RSRA rotor-load-measurement system

[NASA-TP-2327] p 37 N84-31111

CALIFORNIA

Results of analyses performed on basalt adjacent to

penetrators emplaced into volcanic rock at Amboy,

California, April t976

[NASA-TP-1026] p 199 N77-33003

CALORIMETERS

Evaluation of a bulk calorimeter and heat balance for

determination of supersonic combustor efficiency

[NASA-TP-1739] p 48 N81-13058

New method 1or determining heats of combustion of

gaseous hydrocarbons

[NASA-TP-2531 ] p 117 N86-20753

CAMBER

Aerodynamic characteristics of a series of bodies with

variations in nose camber

[NASA-TP-2206] p 22 N83-34904

CAMBERED WINGS

Pressure and force data for a flat wing and e warped

conical wing having a shockless recompression at Math

1.62

[NASA-TP-1759] p 17 N81-22016

Body and canard effects on an attached-flow maneuver

wing at Mach 1.62

[NASA-TP-2249] p 23 N84-18163

CANARD CONFIGURATIONS

Effects of deflected thrust on the longitudinal

aerodynamic characteristics of a close-coupled

wing-canard configuration --- in the Langley V/STOL

tunnel

[NASA-TP-1090] p 6 N78-13014

Wind-tunnel investigation at Mach numbers from 1.90

to 2.86 of a canard-controlled missile with ram-air-jet

spoiler roll control --- in the Langley Unitary Plan Wind

Tunnel

[NASA-TP-1124} p 7 N78-20079

Longitudinal aerodynamic characteristics of a fighter

model with a close-coupled canard at Math numbers from

0.40 to 1.20

[NASA-TP-1206] p 53 N78-27136

Wind-tunnel investigation at supersonic speeds of a

canard-controlled missile with fixed and free-rolling tail

fins

[NASA-TP-1316] p 9 N78.32067

Subsonic dynamic stability characteristics of two

close-coupled canard-wing configurations

[NASA-TP-1291 J p 9 N78-33050

A study of canard-wing interference using experimental

pressure data at transonic speeds

[NASA-TP-1355] p 10 N79-15902

An experimental wind-tunnel investigation of a

ram-air-spoiler roll-control device on a forward-control

missile at supersonic speeds

[NASA-TP-1353] p 11 N79-17809

Aerodynamic characteristics at Mach numbers of 1.5,

1.8, and 2.0 of a blended wing-body configuration with

and without integral canards

[NASA-TP-1427] p 12 N79-23013

Summary of low-speed longitudinal aerodynamics of two

powered close-coupled wing-canard fighter configurations

--- conducted in Langley C/STOL tunnel

{NASA-TP-1535] p 13 N80-12994

Aeropropulsive charactenstics of twin

single-expansion-ramp vectoring nozzles installed with

forward-swept wings and canards --- transonic tunnel

tests

[NASA-TP-2133 p 20 N83-22161

Body and canard effects on an attached-flow maneuver

wing at Mach 1.62

[NASA-TP-2249 p 23 N84-18163

Space Shuttle orbiter trimmed center-of-gravity

extension study

[NASA-TP-2284 p 67 N85-19003

Wind-tunnel investigation of a full-scale

canard-configured general aviation airplane

[NASA-TP-2382] p 25 N85-19925

Parametric study of a canard-configured transport using

conceptual design optimization

{NASA-TP-2400 p 37 N85-19979

Supersonic aerodynamic characteristics of canard,

tailless, and aft-tail configurations for 2 wing planforms

[NASA-TP-2434 p 26 N85-27822

CANCER

Hyperthermia as an Antineoplastic Treatment Modality

[NASA-CP-2051 p 170 N79-10728

CANTILEVER BEAMS

Operating characteristics of a cantilever-mounted

resilient-pad gas-lubricated thrust bearing

[NASA-TP-1438} p 120 N79-22518

A-21
CANTILEVER PLATES SUBJECT INDEX

Dynamic behavior of a beam drag-force anemometer

[NASA-TP.1687} p 114 N80-24595

Vibration characteristics of a deployable

controllabte-geometry truss boom

[NASA-TP-2160] p 132 N83-28491

CANTILEVER PLATES

Joint research effort on vibrations of twisted piates,

phase 1: Final results

{NASA-RP-1150] p 135 N86-t0579

CAPACITANCE

ln-place recaflbration technique applied to a

capacitance.type system for measuring rotor blade tip

clearance

[NASA-TP-11 t0 j p42 N78-22101

CAPACITORS

Capacitor Technologies, Applications and Reliability

{NASA.CP.2186] p t02 N81-26372

CAPE KENNEDY LAUNCH COMPLEX

Moonport: A history of Apollo launch facilities and

operations

[NASA-SP-4204] p 64 N79-12127

Electrical enclosure hydrogen intrusion study --- purging

Cape Kennedy Launch Complex 39

[NASA-TP-146t] p 191 N79-25861

CAPILLARY FLOW

Analytical and numerical studies of the thermocapillary

flow in a uniformly floating zone

[ NASA-TP-2576] p 113 N86-23851

Measurement of viscosity o! gaseous mixtures at

atmospheric pressure

I NASA-TP-2582] p 117 N86-24962

CAPILLARY WAVES

Capillary ancl acceleration wave breakup of liquid jets

in axial-flow airstreams

[NASA-TP-17911 p 109 N81-16417

CARBIDES

Friction and wear of radiofrequency-sputtered borides,

silicides, and carbides

[NASA-TP-1156} p 91 N78-20338

Effect of carbide distnbution on rolling-element fatigue

life of AMS 5749

[NASA-TP-2189} p 123 N83-33166

CARBON

Effect of carbon content on friction and wear of cast

irons

{NASA-TP-1052] p 85 N77-32286

The optical absorption of triatomic carbon C3 for the

wavelength range 260 to 560 nm

[NASA-TP-t14t] p 191 N78-20927

Carbon-catalyzed oxidation of SO2 by NO2 and air

[NASA-TP-2014J p 85 N82-22330

Textured carbon on copper: A novel surface with

extremely low secondary electron emission

charectenstics

[NASA-TP-2543] p 96 N86-15394

CARBON DIOXIDE

Potential spin-offs of the carbon dioxide observational

platform system (CO-OPS) lot remote sensing

opportunities

{NASA-TP-2510} p 68 N85-34149

CARBON DIOXIDE CONCENTRATION

Earth Radiation Science Seminars

[NASA-CP-2239} p 210 N82-33320

Potential spin-offs of the carbon dioxide observational

platform system (CO-OPS) for remote sensing

opportunities

[NASA-TP-2510] p 68 N85-34149

CARBON DIOXIDE LASERS

Atmospheric effects on CO2 laser propagation

[NASA-TP-1357} p 152 N79-13607

DIAL with heterodyne detection including speckle noise:

Aircraft/shuffle measurements of 03, H20, and NH3 with

pulsed tunable CO2 lasers

{NASA-TP-1725] p 115 NaO-30717

A blackbody-pumped CO2-N2 transfer laser

[NASA-TP-2347} p 118 N84-31617

CARBON FIBER REINFORCED PLASTICS

Graphite/Polyimide Composites --- conference on

Composites for Advanced Space Transportation

Systems

{NASA-CP-2079] p 80 N79-30297

Elevated-temperature application of the IITRI

compression test fixture for graphite/polyimide filamentary

composites

INASA-TP-1496] p 80 N79-32277

CARBON FIBERS

Carbon Fiber Risk Analysis --- conference

{ NASA-CP-2074] p 80 N79-22196

Assessment of Carbon Fiber Electrical Effects

{NASA-CP-2119] p 80 N80-19193

Risk to the public from carbon fibers released in civil

aircraft accidents

t NASA-SP-448 } p81 N81-t 8096

CARBON MONOXIDE

A gas filter correlation monitor for CO, CH4, and HCI

[NASA-TP-t1131 p 113 N78-13408

Carbon monoxide measurement in the global

atmospheric sampling program

[NASA-TP-1526} p 148 N79-31841

Effect ot pressure on structure and NO sub X formation

in CO-air diffusion flames

INASA-TP-t448J p 84 NB0-t3191

CARBON STEELS

Effects of erodant partmle shape and various heat

treatments on erosion resistance of plain carbon steel

[ NASA-TP-17551 p87 N81-16210

CARBON 12

Cross section cafculations for subthreshold pion

production in peripheral heavy-ion collisions

[NASA-TP-2600] p 193 N86-30485

CARBON-CARBON COMPOSITES

Reinforced carbon-carbon oxidation behavior in

convective and radiative environments

[NASA-TP-1284} p 106 N78-30555

Theoretical basis for design of thermal-stress-free

fasteners

[NASA-TP-2226] p 132 N84-13614

CARBURIZING

Evaluation of CBS 600 carburized steel as a gear

material

[NASA-TP-1390J p 120 N79-14389

CARGO AIRCRAFT

PreLiminary study of a _arge span-distributed-load

flying-wing cargo airplane concept

{NASA-TP-t158J p 32 N78-25079

Parametric study of variation m cargo-airplane

performance related to progression from current to

spanioeder designs

{NASA-TP-1625] p 34 N80-21318

Simulator study of flighl characteristics of a large

twin-fuselage cargo transport airplane during approach and

landing

{NASA-TP-2183] p 57 N84-t2190

CARIBBEAN SEA

SAGE measurements of the stratospheric aerosol

dispersion and loading from the Soufriere Votcano

INASA-TP-1922] p 153 N82-12687

CASCADE CONTROL

Application of special-purpose digital computers to

rotorcraff real-time simulation

[NASA-TP-12671 p 32 N78-27113

CASCADE FLOW

Effect of coolant flow ejection on aerodynamic

performance of tow-aspect-ratio vanes. 2: Performance

with coolant flow ejection at temperature ratios up to 2

[NASA-TR-t0571 p 6 N78-11008

Two-dimensiona_ cold-air cascade study of a film-cooled

turbine stator blade 4: Comparison of experimental end

analytical aerodynamic results for blade with 12 rows of

O.076-centimeter-(O.O30-inch-) diameter holes having

streamwise ejection angles

[NASA-TP-115t I p 42 N78-20130

Two-dimensional cold-air cascade study of a film-cooled

turbine ststor blade, 5: Comparison of experimental and

analytical aerodynamic results for blade with 12 rows of

O,038-centimeter-(0015 inch) diameter coolant holes

having streamwise ejection angles

I NASA-TP-t204J p 42 N78-20133

CAS2D: FORTRAN program for nonrotating

blade-to-blade, steady, potential transonic cascade flows

INASA-TP-t705J p 15 N80-27284

Computer program for calculating full potential transonic,

quasi-three-dimensional flow through a rotating

turbomachinery blade row

INASA-TP-2030} p 20 N82-28247

Flow visualization study of the horseshoe vortex in a

turbine stator cascade

INASA-TP-1884} p 110 N82-30498

The aerodynamic performance of several flow control

devices for interna_ flow systems

[NASA-TP-1972] p 59 N83-17560

Experimental evaluation of two turning vane designs for

high-speed corner of 0,t-scale model of NASA Lewis

Research Center's proposed altitude wind tunnel

{NASA-TP-2570] p 60 N86-28101

CASCADE WIND TUNNELS

Effect of Cooling-hole geometry on aerodynamic

performance of e film-cooled turbine vane tested with cold

air in a two-dimensionaI cascade

{ NASA-TP-1136 } p 8 N78-20080

CASE HISTORIES

The high-speed frontier Case histories of lour NACA

programs, 1920 - 1950

{NASA-SP-445] p 3 N81-15969

CAST ALLOYS

Effect of carbon content on friction and wear of cast

irons

JNASA-TP-1052J p 85 N77-32285

CATALOGS (PUBLICATIONS)

A catalog of NASA special publications

[ NASA-SP-449 i p2t2 N81-21995

Far infrared supplement: Catalog of infrared

observations

{NASA-RP-1119} p 202 N84-2651g

Catalog of infrared observations including: Bibliography

of infrared astronomy and index of infrared source

positions

[NASA-RP-t118] p 202 N84-26520

Aeronautical facilities catalogue, Volume 2: Airbreathing

propulsion and flight simulators

J NASA-RP-t 133} pS0 N86-18928

CATALYSIS

Carbon-catalyzed oxidation of SO2 by NO2 and sir

[ NASA-TP-2014} p85 N82-22330

Fuel-rich catalytic combustion: A soot-free technique

for in situ hydrogen-like enrichment

[NASA-TP-2498] p 85 N85-31244

CATALYSTS

Carbon-catalyzed oxidation of SO2 by NO2 and air

{NASA-TP-2014 ] p85 N82-22330

CATALYTIC ACTIVITY

Catalytic decomposition of methanol for onboard

hydrogen generation

[NASA-TP-t247] p 97 N78-25236

CATHODES

Spacecraft transmitter reliability

{NASA-CP-2159] p 76 N81-16119

CAUCHY INTEGRAL FORMULA

A method for modifying two-dimensional adaptive

wind-tunnel walls including analytical end experimental

verification

{NASA-TP-2081 J p 59 N83-18770

CAULKING

Performance of an ablator for Space Shuffle inorbit repair

in an arc-plasma airstream

[NASA-TP-2150] p 74 N83-223t7

CAVITATION CORROSION

Universal approach to analysis ol cavitation and

liquid-impingement erosion data

{NASA-TP-2061 ] p 88 N83-15413

Cavitation pitting and erosion of aluminum 6061-T6 in

mineral oil water

INASA-TP-2146] p 123 N83-35400

Empirical relations for cavitation and liquid impingement

erosion processes

INASA-TP-2339} p 90 N84-31349

Characterization of erosion of metallic materials under

cavitation attack in a mineral oil

[NASA-TP-2368] p 124 N84-32825

CAVITATION FLOW

Measurements of the tonal component of cavity noise

and comparison with theory --- aircraft noise

{NASA-TP-1013] p 185 N78-12800

Evaluation of a vortex model of turbulent cavity flow

--- for computing noise generation of fluid flow

[NASA-TP-15051 p 187 N79-32057

CAVITIES

Noise transmission through fiat rectangular panels into

a closed cavity --- light aircraft noise

[NASA-TP-1321 ] p 186 N79-14874

CAVITY RESONATORS

Measurements of the tonal component of cavity noise

and comparison with theory --- aircraft noise

{NASA-TP-t0t3] p 185 N7S-12800

Three-dimensional relativistic field-electron interaction

in a mutticavfty high-power klystron. 1: Basic theory

{NASA-TP-1992] p 102 N82-22439

A study of resonant-cavity and fiberglass-filled parallel

baffles as duct silencers -- for wind tunnels

[NASA-TP-1970] p 188 N82-24052

CELESTIAL BODIES

Recognition of compact astrophysical objects

[NASA-SP-421 ] p 201 N77-34063

Gamma Ray Astrophysics: New insight into the

universe

{ NASA-SP-453] p 204 N82-21118

CELESTIAL GEODESY

A geological basis for the exploration of the planets

[NASA-SP-417} p 204 N77-15961

CELLS (BIOLOGY)

The Regulatory Functions of Calcium and the Potential

Role of Calcium in Mediating Gravitational Responses in

Celts end Tissues

[ NASA-CP-22861 p 169 N84-11720

Controlled Ecological Life Support System, Life Support

Systems in Space ]'ravel

tNASA-CP-2378] p 174 N85-29531

CENTAUR PROJECT

Vapor ingestion in Centaur liquid-hydrogen tank

{NASA-TP-1061 I p 104 N77-33444

CENTER OF GRAVITY

Space Shuttle orbiter trimmed center-of-gravity

extension study

[NASA-TP-2284 I p 67 N85-tgo03

A-22
SUBJECT INDEX

CHROMIUM

CENTRAL PROCESSING UNITS

Concept for a power system controller for large space

electrical power systems

[NASA.TP-1939] p 77 N82-11109

CENTRIFUGAL COMPRESSORS

Experimental performance of a

13,65-centimeter-tip-diameter tandem.bladed swaptback

cantnfugal compressor designed for a pressure ratio of 6

[NASA-TP-1091] p 6 N78-11002

CERAMIC BONDING

Thermal stress analysis of ceramic gas-path seat

components for aircraft turbines

[NASA-TP-1437] p 92 N79-21205

CERAMIC COATINGS

Emittance and absorptance of NASA ceramic thermal

barrier coating system --- for turbine cooling

[NASA-TP-1190] p 43 N78-26148

Low-cycle fatigue of thermal.barrier coatings at 982 dog

C

[NASA-TP.1322] p 43 N79-13046

Extension of similarity test procedures to cooled engine

components with insulating ceramic coatings

[NASA-TP-1615] p 108 N80-24577

Gas turbine ceramic-coated-vane concept with

convection-cooled porous metal core

[NASA-TP-1942] p 48 N82-14090

Thermal and aerothermat performance of a titanium

multiwall thermal protection system

[NASA-TP.1961 ] p 72 N82-14277

CERAMICS

Preseureless sintered Sialons with low amounts of

sintering aid

[NASA-TP-1246] p 92 N78.25215

Ceramic coating effect on liner metal temperatures of

film-cooled annular combustor

[NASA-TP-1323] p 44 N79-14098

Effect of oxygen-nitrogen ratio on sinterability of

Sialons

[NASA-TP-1382] p 92 N79-21204

Industry tests of NASA ceramic thermal barrier coating

--- for gas turbine engine applications

{NASA-TP-t425} p 44 N79-25023

Modules of rupture and oxidation resistance of

$12.55AI0,6OO.72N3.52 sialon

[NASA-TP-1490] p 93 N79-27309

Effects of a ceramic coating on metal temperatures of

an sir-cooled turbine vane

[NASA-TP-1598] p 107 N80-17397

Effect of Yttria additives on properties of

pressureless-sintered silicon nitride

[NASA-TP-1899] p 94 N81-31366

Occurrence of spherical ceramic debris in indentation

and sliding contact

[NASA-TP-20481 p 95 N82-32491

Further industrial tests of ceramic thermal barrier

coatings

[NASA-TP-2057] p 49 N83-10045

Analysis of gap heating due to stepped tiles in the shuttle

thermal protection system

[NASA-TP-2209} p 74 N83-31713

Effect of strain isolator pad modulus on inptane strain

in Shuttle Orbiter thermal protection system tiles

[NASA-TP-2141 ] p 132 N83-33216

A method for developing design diagrams for ceramic

and glass materials using fatigue data

[NASA-RP-1174] p 126 N86-32763

CERENKOV RADIATION

A stochastic model for photon noise induced by charged

particles in multiplier phototubes of the space telescope

fine guidance sensors

[NASA-TP-2337] p 193 N84-26398

CESIUM OXIDES

Effects of oxide additions and temperature on

sinterability of milled silicon nitride

{NASA-TP-1644] p 93 N80-21532

CH-47 HELICOPTER

Description of the VTOL Approach and Landing

Technology (VALT) CH-47 research system

[NASA-TP-1436} p 54 N79-29195

Comparison of analytical and flight test identified

aerodynamic derivatives for a tandem*rotor transport

helicopter

[NASA-TP-1581 } p 34 N80-17060

CH-54 HELICOPTER

Development and validation of a piloted simulation of

a helicopter and external sling load

[NASA-TP-1285] p 32 N79-14083

CHANNEL FLOW

Effects of flow separation and cove leakage on pressure

and heat-transfer distributions along a wing-cove-elevon

configuration at Math 69 - Langley 8-ft high temperature

tunnel test

INASA-TP-21271 p 111 N83-28378

Analysis of gap heating due to stepped tiles in the shuttle

thermal protection system

INASA-TP-2209} p 74 N83-31713

CHAPMAN-ENSKOG THEORY

Measurement of viscosity of gaseous mixtures at

atmospheric pressure

[NASA-TP-2582] p 117 N86-24962

CHARACTERIZATION

Characterization of large 2219 aluminum alloy hand

forgings for the space shuttle solid rocket booster

[NASA-TP-1383] p 87 N79-t6950

High Temperature Polymer Matrix Composites

rNASA-CP-2385] p 83 N86-11260

CHARGE CARRIERS

Semiconductor photoelectrochemist ry

[NASA-TP-2088] p 146 N83-18024

CHARGE DISTRIBUTION

Semiconductor photoelectrochemistry

[NASA-TP-2088] p 146 N83-18024

CHARGE TRANSFER

Semiconductor photoetectrochemistry

[NASA-TP-2088] p 146 N83-18024

CHARTS

Simplified sonic-boom prediction --- using aerodynamic

configuration charts and calculators or slide rules

[NASA-TP-1122] p 7 N78-20078

CHEBYSHEV APPROXIMATION

Single scattering from nonspherical Chebyshev

particles: A compendium of calculations

[NASA-RP-1157] p 194 N86-17140

CHEMICAL ANALYSIS

Results of analyses performed on basalt adjacent to

penetrators emplaced into volcanic rock at Amboy,

California, April 1976

{NASA-TP-t026] p 199 N77-33003

Performance tests of a gas blending system based on

mass-flow controllers

[NASA-TP-1896J p 97 N81-29246

CHEMICAL BONDS

Friction and metal transfer for single-crystal silicon

carbide in contact with various metals in vacuum

[NASA-TP-1191] p 91 N78-21294

CHEMICAL CLOUDS

Environmental analysis of the chemical release module

--- space shuttle payload

[NASA-TP-t750J p 209 N81-13912

Analytic model for washout of HCl(g) from dispersing

rocket exhaust clouds

{NASA-TP-1801 ] p 149 N81-24601

CHEMICAL COMPOSITION

Thermodynamic and transport combustion properties of

hydrocarbons with air Part 2: Compositions corresponding

to Kelvin temperature schedules in part 1

{NASA-TP-19071 p 195 N82-32187

Thermodynamic and transport combustion properties of

hydrocarbonswithair Parl4: Compositionscorresponding

to Rankine temperature schedules in part 3

[NASA-TP-190gj p 195 N82-32189

Visible absorbance spectra: A basis for in situ and

passive remote sensing of phytoplankton concentration

and community composition

[NASA-TP-2094J p 168 N83-19411

Effects of alloy composition on cyclic flame hot-corrosion

attack of cast nickel-base superanoys at 900 deg C

{NASA-TP-2338] p 89 N84-26783

Erosion of iron-chromium alloys by glass particles

{NASA-TP-2354] p 90 N84-28965

CHEMICAL COMPOUNDS

Low toxic corrosion inhibitors for aluminum in fresh

water

l NASA-TP-12791 p86 N78-28226

CHEMICAL ENGINEERING

Microgravity Polymers

[NASA-CP-23921 p 96 N86-28194

CHEMICAL EQUILIBRIUM

Combustion gas properties Part 3: Hydrogen gas fuel

and dry a_r

INASA-TP-24771 p 52 N85-3t058

CHEMICAL EVOLUTION

Life in the Universe

[NASA-CP-2156] p 175 N82-20884

The 1st Symposium on Chemical Evolution and the

Origin and Evolution of Life

[NASA-CP-22761 p 79 N83-24556

Search for the universal ancestors

[NASA-SP-477J p 175 N85-32777

Second Symposium on Chemical Evolution and the

Origin of Life

[NASA-CP-2425} p 175 N86-26844

CHEMICAL PROPERTIES

Handbook of tuner materials

{ NASA-RP-1057 ] p206 N80-16009

Recent trends in aviation turbine fuel properlies

[NASA-TP-2056] p 97 N83-11340

Overview of zirconia with respect to gas turbine

applications

[NASA-TP-22861 p 95 N84-21740

Lubrication of machine elements

INASA-F:IP-1126] p 124 N84-31640

CHEMICAL REACTIONS

Adsorption and chemical reaction of gaseous mixtures

of hydrogen chloride and water on aluminum oxide and

application to solid-propellant rocket exhaust clouds

[NASA-TP.1105] p 84 N78-22188

Chemical kinetic models for combustion of hydrocarbons

and formation of nitric oxide

[NASA-TP-1794] p 85 N81-14017

Chemical kinetic analysis of hydrogen-air ignition and

reacbon times

INASA-TP-1856] p 85 N81-27223

Surface chemistry and wear behavior of single-crystal

silicon carbide sliding against iron at temperatures to 1500

C _n vacuum

{NASA.TP.1947] p 94 N82-19374

Mechanism of lubrication by trtoresylphosphata (TCP)

[NASA-TP-2053] p 85 N83-18863

Combustion Fundamentals Research

[NASA-CP.2268] p 50 N83-29208

Simulation of lubricating behavior of a thloethar liquid

lubricant by an electrochemical method

[NASA-TP.2316] p 95 N84-23764

Chemical mechanisms and reaction rates for the

initiation of hot corrosion of IN-738

{NASA.TP.2319] p 90 N84-28958

Friction behavior of silicon in contact with titanium, nickel,

silver and copper

[NASA-TP-2362] p 96 N84-33590

Physical and numerical sources of computational

inefficiency in integration of chemical kinetic rate

equations: Etiology, treatment and prognosis

[NASA.TP-2590] p 183 N86.28662

CHEMICAL REACTORS

A high-pressure premixed flat-flame burner for chemical

process studies -.- of pollutant formation in hydrocarbon

flames

[NASA.TP.1318] p 84 N79.14t77

CHEMISORPTION

Enhanced hydrophilicity of chlorided aluminum oxide

particulates

[NASA-TP-1312] p 84 N79-12178

CHESAPEAKE BAY (US)

Application of Remote Sensing to the Chesapeake Bay

Region. Volume 2: Proceedings

[NASA-CP-006-PT-2] p 138 N78-21526

Application of Remote Sensing to the Chesapeake Bay

Region. Volume 1: Executive summary

[NASA-CP-006-PT-1] p 138 N78-23537

Chesapeake Bay Plume Study: Superflux 1980

{NASA-CP-2188] p 168 N82-10661

CHILDREN

Human Neurological Development: Past, Present and

Future

[NASA-CP-2063} p 212 N79-15887

CHLORINE

Effect of trichlorofluoromethane and molecular chlorine

on Ozone formation by simulated solar radiation

[NASA-TP-1093] p 84 N78-12167

CHLORINE COMPOUNDS

Chlorofluoromethanes and the stratosphere

[NASA-RP-1010] p 151 N77-31694

Effect of trichlorofluoromethene and molecular chlorine

on ozone formation by simulated solar radiation

[NASA-TP-1093] p 84 N78-12167

CHLOROCARBONS

Effect of nitric oxide on photochemical ozone formation

in mixtures of air with molecular chlorine and with

t richlor ofluoromethane

[NASA-TP-t 192] p84 N78-20281

CHLOROPHYLLS

Laboratory tank studies of a single species of

phytoptankton using a remote sensing fluorosensor

I NASA-TP-1821 } p 139 N81-20492

Oceanic Lidar

[NASA-CP-2194} p 168 N81-31801

Characteristic vector analysis of inflection ratio spectra:

New technique for analysis of ocean color data

[NASA-TP-2428} p 143 N85-23237

CHOKES (FUEL SYSTEMS)

Flow through aligned sequential orifice type inlets

[NASA-TP-1967] p 109 N82-20467

CHOKES (RESTRICTIONS)

Two-phase choked flow of cryogenic fluids in

converging-diverging nozzles

INASA-TP-1484} p t07 N79-29468

Computer analysis of flow perturbations generated by

placement of choke bumps in a wind tunnel

[NASA-TP-1892J p 18 N81-30088

CHROMIUM

Erosion of iron-chromium alloys by glass particles

[ NASA-TP-2354J p 90 N84-28965

Effects of chromium and aluminum on mechanical and

oxidation properties of iron-nickel-base superalloys based

on CG-27

[ NASA-TP-2443 ] p 90 N85-21323

A-23
CHROMIUM ALLOYS SUBJECT INDEX

CHROMIUM ALLOYS

Friction and wear characteristics of iron-chromium alloys

in contact with themselves and silicon carbide

tNASA-TP-1387] p t20 N79-14387

Mechanical properties and oxidation and corrosion

resistance of reduced-chromium 304 stainless steel

alloys

[ NASA-TP-t 557 ] p87 N80-11188

CHRONOLOGY

Astronautics and aeronautics, 1974: A chronology

INASA-SP-40t9] p 212 N78-12997

Astronautics and Aeronautics, 1975. A chronology

{NASA-SP-4020] p 212 N81-16973

CIRCUIT BOARDS

Evaluation of multilayer printed wiring boards by

metafiographic techniques: An illustrated guide to the

preparation and inspection of plated-through hole test

coupons based on the requirements of MiI-P-$5110D

[NASA-RP-1161J p 126 N86-26639

CIRCUIT BREAKERS

High-voltage, high-power, solid-state remote power

controllers tor aerospace applications

INASA-TP-2437 J p 78 N85-21263

CIRCUIT DIAGRAMS

The PR2D {Place, Route in 2-Dimensions) automatic

layout computer program handbook

[NASA-RP-1029] p 179 N81-12760

CIRCUIT PROTECTION

Circuit transients due to negative bias arcs on e

high-voltage solar array in low Earth orbit

{NASA-TP-2407J p 75 N85-14858

CIRCUIT RELIABILITY

Procedures for precap visual inspection

INASA-RP-11221 p 103 N85-13156

CIRCUITS

Optical Information Processing for Aerospace

Applications 2

[NASA-CP-2302] p 194 N84-22402

CIRCULAR CYLINDERS

Experimental studies of effects of tilt and structural

asymmetry on vibration characteristics of thin-wall circular

cylinders partly filled with liquid

[NASA-TP-12111 p 127 N78-28480

Flow in a torsionally Oscillating tilled cylinder

[NASA-TP-2115] p 1t0 N83-16674

A method for modifying two-dimensional adaptive

wind-tunnel walls including analytical and experimental

verificetton

INASA-TP-2081 ] p 59 N83-t8770

CIRCULAR PLATES

Gaussian step-pressure loading of rigid viscopiashc

plates

I NASA*TP-11231 p 127 N78-20536

CITRUS TREES

Aenal color infrared photography: Appiioations in

citriculture --- Florida

[NASA-RP-10£,71 p 139 N8t-21437

CIVIL AVIATION

Precision positional data of general aviation air traffic

in terminal air space

[NASA-RP-t020I p I N78-25048

Risk to the public from carbon fibers released in civil

aircraft accidents

INASA-SP-448] p 81 N81-18096

Guidelines for line-ohented flight training, volume 2

I NASA-CP-2184-VOL-2) p30 N82-13123

An Operational evaluation of head up displays for civil

transport operations. NASA/FAA phase 3 report

[NASA-TP-18151 p 40 N82-33381

Small transport aircraft technology

[NASA-SP-460] p 36 N83-20931

Aviation Gasolines and Future Alternatives

INASA-CP-22671 p 97 N83-22442

Flight Training Technology for Regional/Commuter

Aidine Operations: Regional Airline ASSOCiation/NASA

Workshop Proceedings

[NASA-CP-2348] p 30 N85-18009

NASA and general aviation

[NASA-SP-485] p 38 N86-30720

CLASSIFICATIONS

NASA guidelines on report literature

[NASA-SP-7200] p 197 N79-13914

Wildlend inventory and resource modeling for Douglas

and Carson City Counties, Nevada, using LANDSAT and

digital terrain data

{E83-10302] p 142 N83-27293

CLEAR AIR TURBULENCE

Power spectral measurements of clear-air turbulence

to long wavelengths for altitudes up to 14,000 meters

[NASA-TP-19791 p 164 N82-24790

CLEARANCES

Cold-air performance of a

12766-centimeter-tip-diameter axial-flow cooled turbine

3: Effect of rotor tip clearance on overall performance

of a solid blade configuration

I NASA-TP-10321 p 5 N77-32082

In-piece recalibration technique applied to a

capacitance-type system for measuring rotor blade tip

clearance

[NASA-TP-11101 p 42 N78-22101

Rotor tip clearance effects on overall and blade-element

pedormance of axial-flow transonic fan stage

[NASA-TP-204g] p 49 N82-33389

Film thickness measurement for spiral groove and

Rayleigh step lift pad self-acting face seals

[NASA-TP-2058] p 49 N83-11126

CLIMATE

Fourth National Aeronautics and Space Administration

Weather and Climate Program Science Review

INASA-CP-2076] p 159 N79-20633

Sun, weather, and climate

INASA-SP-426] p 209 N79-20961

Stratospheric aerosol modification by supersonic

transport operations with climate implications

INASA-RP-t058] p 161 N80-15726

Report of Workshop on Mount Saint Helens: its

Atmospheric Effects and Potential Climatic impact

[ NASA-SP-4581 p 154 N82-32915

Atmospheric Effects and Potential Climatic Impact of

the 1980 Eruptions of Mount St. Helens

[NASA-CP-2240] p 136 N83-11534

Surface radiation budget for climate applications

INASA-RP-11691 p 167 N86-28574

Proceedings of the Second Pilot Climate Data System

Workshop

INASA-CP-2430] p 137 N86-29282

CLIMATOLOGY

Stratospheric warmings: Synoptic, dynamic and

general-circulation aspects

[NASA-RP-tO17J p 158 N78-18630

An evaluation of in situ Ozone sensor performance during

a cold frontal passage

[ NASA-TP-t 239 j p 158 N78-27706

Synoptic analyses, 5-, 2-, 1-, and 0 4-millibar surfaces

for July 1976 through June 1977

INASA-RP-1032] p 159 N79-19569

Third National Aeronautics and Space Administration

Weather and climate program science review

INASA-CP-2029] p 159 N79-20575

Earth Radiation Budget Science, 1978 ---conferences

{NASA-CP-2100] p 160 N79-32797

Thunderstorm-environment interactions determined with

three-dimensional trajectories

[NASA-RP-1054J p 161 N80-16675

The role of satellite altimetry in climate studies

[NASA-TP-1570] p 161 N80-16678

Ozone Trend Detectability

[NASA-CP-2189] p 153 N82-10624

Ozone climatology series. Volume 1: Atlas ol total

ozone, April 1970 - December t976

[NASA-RP-t0981 p 154 N83-16992

Climatology of ozone at altitudes from 19,000 at 59,000

feet based on combined GASP and ozonesonde data

[NASA-TP-2303] p 166 N84-31865

A new NASA/MSFC mission analysis global cloud cover

data base

[NASA-TP.2448] p 166 N85-21878

SAM 2 measurements of the polar stratospheric aerosol,

volume 5

[NASA-RP-1140] p 155 N85-25970

Understanding climate: A strategy for c_imate modeling

and predictability research, 1985-1995

INASA-RP-1158} p 166 N86-13866

Compendium of meteorology scientific issues of 1950

still outstanding

[NASA-RP-1167] p 156 N86-25900

CLIMBING FLIGHT

Parametric study of ascent pedormance of a verbcally

launched hydrogen-fueled single-stage reusable

transport

{NASA-TP-1045} p 65 N78-10186

Theoretical study of the effect of wind velOCity gradients

on longitudinal stability and control in climbing and level

flight

[NASA-TP-1332) p 54 N79-14t10

Sensitivity analysis of the space shuttle to ascent wind

profiles

[NASA-TP-1988] p 69 N82-20236

CLINICAL MEDICINE

Human Neurological Developmenh Past. Present and

Future

[NASA-CP-2063} p 212 N79-158B7

CLOCKS

Validation of a feu_t-tolerant clock synchronization

system

[NASA-TP-2346J p 180 N84-34198

CLOSED ECOLOGICAL SYSTEMS

Controlled Ecological Life Support System: Use of

Higher Plants

[NASA-CP-2231 I p 173 N82-24834

Controlled Ecological Life Support System: Research

and Development Guidelines

INASA-CP-22321 p 173 N82-24835

Controlled ecological life support system - biological

problems

[NASA-CP-22331 p 173 N82-24838

Controlled Ecological Life Support System. First

Principal Investigators Meeting

[NASA-CP-2247] p 174 N83-30016

Controlled Ecological Life Support System. Life Support

Systems in Space Travel

INASA-CP-2378J p 174 N85-29531

CLOUD COVER

A new NASA/MSFC mission analysis global cloud cover

data base

[NASA-TP-2448] p 166 N85-21878

SAM 2 measurements of the polar stratospheric aerosol,

volume 2

[NASA-RP-1164] p 157 N86-28562

CLOUD PHYSICS

Earth Radiation Budget Science, 1978 --- conferences

[NASA-CP-2100] p 160 N79-32797

Summary of the NASA/MSFC FY-79 Severe Storm and

Local Weather research review --- cloud physics.

atmospheric electricity, and mesoscale/storm dynamics

reserach

[NASA-CP-2105J p 160 N79-33722

The Third International Cloud Condensation Nuclei

Workshop --- conference

INASA-CP-2212] p 115 N82-15383

Proceedings of a Workshop on Research Needs in

Heterogeneous Tropospheric Chemistry

[NASA-CP-2320] p 137 N84-28131

CLOUDS

Cloud-encounter and particle-concentration variabilities

from GASP data

[NASA-TP-1886} p 164 N82-15677

VlSSR Atmospheric Sounder (VAS) Research Review

INASA-CP-22531 p 165 N83-24028

Space shuffle exhaust cloud properties

INASA-TP-2258] p 154 N84-14606

SAM II measurements of the polar stratospheric aerosol.

Volume 6: April to October 1981

INASA-RP-1141] p 155 N85-27422

Comparative accuracy of the Albedo, transmission and

absorption for selected radiative transfer approximations

[NASA-RP-1160} p 156 N86-22022

CLOUDS (METEOROLOGY)

NASA/MSFC PY-84 Atmospheric PrOCesses Research

Review

{NASA-CP-2329J p 166 N84-34829

CLUMPS

Calculation of composition distribution of ultrafine

IOn-H20-H2SO4 clusters using a modified binary ton

nucleation theory

{NASA-TP-2031 I p 150 N82-27867

Simplified free-energy calculation for ion-induced

heteromolecutar nucleation

[NASA-TP-2039] p 150 N82-28839

COAL

Erosion/corrosion of turbine airfoil materials in the

high-velocity effluent of a pressurized fluidized coal

combustor

[NASA-TP*1274 ] p86 N78-28225

COAL GASIFICATION

Analysis o! potential benefits of integrated-gasifier

combined cycles for a utility system

[ NASA-TP-2172 ] p 146 N83-36549

COAL UTILIZATION

Measurement techniques for trace metals in coal-plant

effluents; A brief review

[NASA-RP-1047] p 148 N79-33611

COALESCING

An analysis of shock coalescence including

three-dimensional effects with application to sonic boom

extrapolation

INASA'TP'2214] p t 11 N84-22906

COASTAL ECOLOGY

Literature review of organic matter transport from

marshes

[E83-10352I p 142 N83-29750

COASTAL ZONE COLOR SCANNER

Oceanic Lidar

[NASA-CP-2194J p 168 N81-31801

COATINGS

Morphology of gold and copper ion-plated coatings

I NASA-TP-1262] p86 N78-26199

Effect of nitrogen-containing plasma on adherence,

friction, and wear of radiofrequency-sputtered titanium

carbide coatings

INASA-TP-13771 p 92 N79-15184

COAXIAL NOZZLES

Empirical source noise prediction method with

application to subsonic coaxial jet mixing noise

JNASA-TP-20841 p 189 N83-16149

A-24
SUBJECT INDEX COMBUSTION PHYSICS

COBALT

Thermal-fatigue and oxidation resistance of

cobalt-modified Udimet 700 alloy

[NASA-TP-25911 p 135 N86-28464

COBALT ALLOYS

Performance of a Haynes 188 metallic standoff thermal

protection system at Mach 7

[NASA-TP-1802] p 72 N81-21116

Preliminary study of thermomechanical fatigue of

polycrystalline MAR-M 200

[NASA-TP-2280] p 89 N84-17350

Analysis of thermoelectric properties of

high-temperature complex alloys of nickel-base, iron-base

and cobalt-base groups

[NASA-TP-2278] p 89 N84-t8370

Effects of alloy composition on cyclic flame hot-corrosion

attack of cast nickel-base superalloys at 900 deg C

[NASA-TP-2338] p 89 N84-26783

COCKPIT SIMULATORS

A general aviation simulator evaluation of a

rate-enhanced instrument landing system display

[NASA-TP-1960] p 39 N82-14085

Influence of display and control compatibility on

pilot-induced oscillations

[NASA-TP-1936} p 172 N82-14804

Simulator study of a pictorial display for general aviation

instrument flight

[NASA-TP-1963J p 39 N82-20180

Effect of lead-aircraft ground-speed on self-spacing

performance using a cockpit display of traffic information

[NASA-TP-2194] p 40 N83-36028

COCKPITS

Effects of curved approach paths and advanced displays

on pilot scan patterns

[NASA-TP-t846J p 171 N81-23791

Helicopter Handling Qualities

{NASA-CP-2219J p 30 N82-23208

Simulation of a cockpit-display concept for executing a

wake-vortex avoidance procedure

[NASA-TP-2300] p 40 N84-21542

Technical Workshop: Advanced Helicopter Cockpit

Design

[NASA-CP-235t ] p 31 N85-14806

A cockpit-display concept for executing a multiple

glide-slope approach for wake-vortex avoidance

[NASA.TP-2386] p 40 N85-16869

CODING

Physical and numerical sources of computational

inefficiency in integration of chemical kinetic rate

equations: Etiology, treatment and prognosis

[NASA-TP-2590J p 183 N86-28662

COEFFICIENT OF FRICTION

Effectiveness of various organometallics as antiwear

additives in mineral oil

[NASA-TP-t096] p 91 N78-12222

Fdction and wear of several compressor ges-path seal

movements

NASA-TP-1128] p 86 N78-15229

Friction and wear of polyethylene oxide polymer having

a range of molecular weights

NASA-TP-1129 p 91 N78-15278

Friction and metal transfer for single-crystal silicon

carbide in contact with various metals in vacuum

NASA-TP-1191 p 91 N78-21294

Effect of oxygen and nitrogen interactions on friction

of single-crystal silicon carbide

NASA-TP-t265 p 92 N78-28247

Anisotropic friction and wear of single-crystal

manganese-zinc ferrite in contact with itself

NASA-TP-1339 p 120 N79-10425

Lubrication and failure mechanisms of molybdenum

disulfide films. 1: Effect of atmosphere

NASA-TP-1343 p 92 N79-13158

Lubricating and wear mechanisms for a hemisphere

sliding on polyimide-bonded graphite fluoride film

NASA-TP-1524 p 93 N79-30381

Adhesion and fhction of iron-base binary alloys in contact

with silicon carbide in vacuum

NASA-TP-1604 p 87 N80-15234

Correlation of ideal and actual shear strengths of metals

with their friction properties

[NASA-TP-1891 p 94 N81-27282

Relationship between the ideal tensile strength and the

friction properties of metals in contact with nonmetals and

themselves

[NASA-TP-1883] p 94 N81-33293

Friction and wear of iron in corrosive metal

INASA'TP-1985I p 88 N82-20291

Mechanism of lubrication by tricresylphosphate (TCP)

[NASA-TP-2053] p 85 N83-t8863

Friction and morphology of magnetic tapes in sliding

contact with nickel-zinc ferrite

INASA-TP-2267} p 95 N84-16334

Mechanism of lubrication by tdcresylphosphate (TCP)

[NASA-TP-2274] p 123 N84-18653

COEFFICIENTS

Measurement of viscosity of gaseous mixtures at

atmospheric pressure

[ NASA-TP-2582] p t 17 N86-24962

COGNITION

Cognitive issues in head-up displays

[NASA-TP-1711] p 173 N81-13636

COHERENT RADIATION

Nuclear-Pumped Lasers --- efficient conversion of

energy liberated in nuclear reactions to coherent

radiation

INASA-CP-2t07] p 117 N80-13438

Application of coherence in fan noise studies

[NASA.TP-1630] p 187 N80-18882

COLD FLOW TESTS

Des0gn and cold-air test of single-stage uncooled turbine

with high work output

[NASA-TP-1680] p 46 N80-25337

Cold-air investigation of a 4 1/2 stage turbine with

stage-loading factor of 4.66 and high specific work output.

2: Stage group performance

[NASA-TP-t688] p 47 N80-25338

COLD SURFACES

Experimental aerodynamic heating to simulated space

shuttle tiles in laminar and turbulent boundary layers with

vadable flow angles at a nominal Math number of 7

[NASA-TP-2307] p 113 N85-34351

COLD WORKING

Fabrication and evaluation of cold/formed/weldbrazed

beta-titanium skin-stiffened compression panels

[NASA-TP-2201 ] p 89 N83-35100

COLLISION AVOIDANCE

Flight investigation of cockpit-displayed traffic

information utilizing coded symboIogy in an advanced

operational environment

[NASA-TP-1684] p 38 N80-27360

COLMSIONLESS PLASMAS

The aerodynamics of bodies in a rarefied ionized gas

with applications to spacecraff environmental dynamics

[NASA-TP-t933J p 72 N82-15t 16

COLLISIONS

Orbital Debris

(NASA-CP-2360] p 63 N85-21188

COLOR PHOTOGRAPHY

Aenal color infrared photography: Applications in

citriculture --- Flodda

[NASA-RP-tO67] p 139 N8t-21437

COLUMBIA (ORBITER)

Correlation of predicted and measured sonic boom

characteristics from the reentry of STS-1 orbiter

[NASA-TP-2475} p 190 N85-29694

COMBAT

Computer-automated opponent for manned air-to-air

combat simulations

[NASA-TP-1518] p 176 N79-33855

A formulation and analysis of combat games

[NASA-TP-2487] p 185 N85.33745

COMBINED CYCLE POWER GENERATION

Analysis of potential benefits of integrated-gasifier

combined cycles for a utility system

[NASA-TP-2172| p 146 N83-36549

COMBUSTIBLE FLOW

Modeling Interface Motion Of Combustion (MINOC). A

computer code for two-dimensional, unsteady turbulent

combustion

[NASA-TP-2132] p 50 N83-32806

COMBUSTION

Experimental and analytical study of nitric oxide

formation dunng combustion of propane in a jet-stirred

combustor

[NASA-TP-t181 } p 84 N78-23172

Lithium/sulfur dioxide cell and battery safety

[NASA-RP-t099] p 146 N83-14684

Preliminary tests of an advanced high-temperature

combustion system

[NASA-TP-2203] p 50 N83-33893

Effects of percentage of blockage and flameholder

downstream counterbores on lean combustion limits of

premixed, prevaporized propane-air mixture

[ NASA-TP-2227] p 50 N83-34941

Assessment of Alternative Aircraft Fuels

[NASA-CP-2307] p 51 N84-23630

Magnetohydrodynsmic power generation

I NASA-TP-2331 I p 195 N84-25458

Combustion gas properties. 2: Natural gas fuel and

dry air

[NASA-TP-2435] p 52 N85-21168

Combustion gas properties. Part 3: Hydrogen gas fuel

and dry air

{NASA-TP-2477] p 52 N85-31058

Turbine Engine Hot Section Technology (HOST)

[ NASA-CP-2289 J p 135 N86-11495

COMBUSTION CHAMBERS

Reverse-flow combustor for small gas turbines with

pressure-atomizing fuel injectors

INASA-TP-1260] p 43 N78-27130

Ceramic coating effect on liner metal temperatures of

film-cooled annular combustor

INASA-TP-1323] p 44 N79-14098

Performance of a vortex-controlled diffuser in an annular

swirl-can combustor at inlet Mach numbers up to 0.53

[NASA-TP-1452] p 44 N79-22099

Effect of primary-zone equivalence ratio on pollutant

formation

[NASA-TP-1463] p 44 N79-23086

Premixed Prevaporized Combustor Technology Forum

[NASA-CP-2078] p 44 N79-24994

Fundamentals of Gas Turbine combustion

[NASA-CP-2087) p 44 N79-25016

Effect of degree of fuel vaporization upon emissions

for a ptemixed partially vaporized combustion system ---

for gas turbine engines

[NASA-TP-1582] p 46 N80-14125

Low-pressure performance of annular, high-pressure (40

aim) high-temperature (2480 K) combustion system

[NASA-TP-1713] p 47 N80-32396

Spectral flame radiance from a tubular-can combustor

[NASA-TP-t722) p 48 N81-tgt21

Performance of semi-transportation-cooled liner in

high-temperature-rise combustors

[NASA-TP-1806] p 48 N81-21077

Analysis of effect of tiameholder characteristics on lean,

premixed, partially vaporized fuel-air mixtures quality and

nitrogen OXides emissions

[NASA-TP-t842J p 48 N8t-24065

Effect of fuel injector type on performance and emissions

of reverse-tiow combustor

[NASA-TP-t9451 p 49 N82-15040

Preliminary tests of an advanced high-temperature

combustion system

[NASA-TP-2203] p 50 N83-33893

Effects of percentage of blockage and flameholder

downstream counterbores on lean combustion limits of

premixed, prevaponzed propane-sir mixture

[NASA-TP-2227) p 50 N83-34941

Advanced High Pressure O2/H2 Technology

[NASA-CP-2372] p 78 N85-26862

COMBUSTION CHEMISTRY

Comparison of numerical techniques for integration of

stiff ordinary differential equations arising in combustion

chemistry

[NASA.TP.2372] p 51 N85-10065

COMBUSTION EFFICIENCY

Modular instrumentation system for real-time

measurements and control on reciprocating engines

INASA-TP-1757] p 101 N81-11315

Evaluation of a bulk calorimeter and heat balance for

determination of supersonic combustor efficiency

[NASA-TP-1739] p 48 N81.13058

Performance of semi-transportation-cooled liner in

high- tamperature-rise combustors

[NASA-TP-1806] p 48 N81-21077

Analysis of effect of flameholder characteristics on lean,

premixed, partially vaporized fuel-sir mixtures quality and

nitrogen oxides emissions

[NASA-TP-t842] p 48 N81-24065

Effect of flameholder pressure drop on emissions and

performance of premixed-prevaporized combustors

[NASA-TP-2131] p 50 N83-23309

Comparison of numerical techniques for integration of

stiff ordinary differential equations arising in combustion

chemistry

[NASA-TP-23721 p 51 N85-10065

COMBUSTION PHYSICS

Conceptual model of turbulent flameholdiog for scram jet

combustors

[NASA-TP-1543I p 47 N80-33409

Thermodynamic and transport combustion properties of

hydrocarbons wdh air, Part 1 : Properties in SI units

[NASA-TP-1906] p 195 N82-32186

Thermodynamic and transport combustion properties of

hydrocarbons with air. Pert 2: Compositions corresponding

to Kelvin temperature schedules in part 1

[NASA-TP-1907) p t95 N82-32187

Thermodynamic and transport combustion properties of

hydrocarbons with air. Part 3: Properties in US customary

units

[NASA-TP-1908] p 195 N82-32188

Thermodynamic and transport combustion properties of

hydrocarbons with air. Part 4: Compositions corresponding

to Rankine temperature schedules in part 3

[NASA-TP-lg09J p 195 N82-32189

Combustion Fundamentals Research

{NASA-CP-2268] p 50 N83-29208

Simplified combustion noise theory yielding a prediction

of fluctuating pressure level

[NASA-TP-2237] p 189 N84-19049

Combustion Fundamentals Research

[NASA-CP-2309] p 51 N84-20525

A-25
COMBUSTION PRODUCTS SUBJECT INDEX

COMBUSTION PRODUCTS

Computer program for obtai_ng thermOdynamic and

transport properbes of ,,Jr end products of combustion of

ASTM-A-1 fuel and air

(NASA-TP-tt60] p 97 N78.20351

Erosion/corrosion of turbine airfoil materials in the

high.velocity effluent of a pressurized fiuidizad coal

combustor

[NASA-TP-1274] p 86 N78-28225

Thermodynamic and chemical parameters of the

exhaust effluents from the HARPOON booster motor

lNASA-TP-1280] p 147 N78-28682

Effect of primary-zone equivalence ratio on ponutant

formation

lNASA-TP-1463] p 44 N79-23086

Combustion gas properbes I-ASTM jet A fuel and dry

air

INASA-TP-2359] p 51 N85.10064

CombusL'on gas propert*es. 2: Natural gas fuel and

dry air

[NASA-TP-2435J p 52 N85-21168

Fuel-rich catalytic combustion: A soot-free technique

for in situ hydrogen-like enrichment

[NASA-TP-2498] p 85 N85-31244

COMBUSTION STABILITY

Operating condition and geometry effects on

tow-frequency afterburner combustion instability in a

turbofan st altitude

[NASA-TP-14751 p 44 N79-25022

COMETS

Space missions to comets

[NASA-CP-2089] p 206 N80-11972

The geology of the terrestrial pisnets

[NASA-SP-469] p 200 N85-18888

COMFORT

An investigation of r_e quality rating scales

[NASA-TP-1064] p 171 N78-11696

Effect of vibration duration on human discomfort ---

passenger comfort and random vibration

[NASA-TP-1283] p 171 N78-327t7

A user-oriented and computerized model for estimating

vehicle ride quality

[NASA.TP-2299] p t72 N84-22162

COMMAND AND CONTROL

Fourth NASA Inter-Center Control Systems

Conference

[NASA-CP-007} p 212 N78-23010

Diversity techniques for omnidirectional telemetry

coverage of the HiMAT research vehicle

[NASA-TP-1830] p 39 N81-20074

Guidelines for line-oriented flight training, volume 1

I NASA-CP-2184J p 30 N81-30101

Human Factors Cons!derations in System Design

[NASA-CP-2246] p 173 N83-18238

COMMERCIAL AIRCRAFT

CTOL transport technology, 1978 --- conferences

[NASA-CP-2036-PT-1 ] p I N78-27046

Procedures for estimating the frequency of commercial

airline flights encountering high cabin ozone levels

[NASA.TP.1560] p 29 N79.33171

Analysis of otmospheric ozone levels at commercial

airplane cruise altitudes in winter and spring, 1976 - 1977

--- Global Atmospheric Sampling Program

[NASA-TP-1807] p 163 N81-21685

Ruggodtzad minicomputer hardware and software

topics, 198t: Proceedings of the 4th ROLM MIL-SPEC

Computer Usar's Group Conference

[NASA-CP-2208] p 180 N82-1482g

S_mulator study of vortex encounters by a twin.engine,

commercial, jet transport airplane

[NASA-TP-1966] p 57 N82-19225

An Operational evaluation of head up dtlkollyo for civil

transport operations. NASA/FAA phase 3 report

[NASA-TP-1815J p 40 N82-33381

Minimum-fuel, 3-dimensional flightpeth guidance of

transfer jots

[NASA-TP-2326] p 58 N84-32394

COMMUNICATING

Planetary Data Workotmp, pert 2

( NASA-CP.2343.PT.2] p 208 N84.34376

COMMUNICATION

Second Symposium on Space Industrialization --- space

commercialization

{ NASA-CP-2313] p63 N85-11011

Space Shuttle Technical Conference, part 2

{NASA-CP-2342-PT-2] p 63 N85-16937

COMMUNICATION NETWORKS

Proceedings of the Eleventh Annual Precise Time and

Time Interval (PTTI) Application and Planning Meeting ---

conference

[NASA-CP-212g] p 185 N80-29096

Propagation effects on satellite systems at frequencies

below 10 GHz, a handbook for satellite systems design,

1 st edition

{NASA-RP-11081 p 100 N84-13397

Hybrid routing technique for a fault-tolerant, integrated

information network

{NASA.TP.2605] p 180 N86-27947

COMMUNICATION SATELLITES

Design of a video teleconference facility for a

synchronous satellite communications link

[NASA-TP-1376] p 100 N7g-14275

Experimental verification of the multistage depressed

collector design I_*OCedura for • high-perveance.

helix-type, troveling.wove tube --- in communications

satellites

[NASA-TP-2162] p 102 N83-25985

Propagation effects on satellite systems at frequencies

below t0 GHz. a handbook for satellite systems design,

1 st edition

[NASA-RP-1106] p 100 N84-13397

COMMUNICATION THEORY

Technical communication: Perspectives for the eighties,

part I Proceedings of the technical communications

sessions at the 32nd Annual Meeting of the Conference

on College Composition and Communication

[NASA-CP-2203-PT-t] p 197 N82-14960

Technical communication. Perspectives for the Eighties,

part 2

{NASA-CP-2203-PT-2] p 197 N82-15986

COMMUNICATIONS TECHNOLOGY SATELLITE

Thermal characteristics of the 12-gigahertz, 200-watt

output stage tube for the communications technology

satellite

[NASA-TP-13441 p 69 N78-33137

Thermal anomalies of the transmitter experiment

package on the communications technology satellite

[ NASA.TP-14t0 ] p69 N79-21120

Description and orbit data of voriable-conductance

heat-pipe system for the communications technology

satellite

[NASA-TP-1465] p 107 N79-30516

COMMUNITIES

A summation and inhibition model of annoyance

response to multq)le community noise sources

[NASA-TP-1479] p 146 N79-32744

COMPARATORS

Thermal-conductivity measurements of

tungsten-fiber-reibforced superelloy composites using a

thermal-conductivity comperator

[NASA-TP-1445] p 80 N79-28234

COMPARISON

Mechanical behavior and fracture characteristics of

off-axis fiber composites. 2: Theory and comparisons

[NASA-TP-1082] p 79 N78-16098

COMPONENT RELIABILITY

Proceedings of the Thirteenth Annual Precise Time and

Time interval (PTTI) Applications and Planning Meeting

[NASA.CP-2220] p 118 N82-20494

Procedures for precop visual inspection

[NASA-RP-1122] p 103 N85-13156

Reliability bounds for fault-tolerant systems with

competing responses to component failures

[NASA-TP-2409] p 126 N85-23090

COMPOSITE MATERIALS

Machonioel behavior ond fracture characteristics of

off-axis fiber composites. 1: Experimental investigation

--- at the Lewis Research Center

[NASA-TP-t 0at ] p79 N78-13138

Some effects of composition on friction and wear of

graphite-fiber.reinforced polyimido liners in plain spherical

bearings

[NASA.TP-1229] p t19 N78-25433

An integrated computer procedure for sizing composite

airframe structures

[NASA-TP-1300] p 178 N79-17580

Stress-concentration foctors for finite orthotropic

laminates with • circular hole end uniaxial Ioodlng

[NASA-TP-146g} p 80 N79-23140

Thermal-conductivity measurements of

tungsten-fiber-reinforced superelloy composites using •

thermal-conductivity comparotor

[NASA.TP.1445] p 80 N79-28234

Assessment of Carbon Fiber Electrical Effects

[NASA.CP-2119] p 80 N80-19193

Moisture determination in composite materials using

positron lifetime techniques

INASA-TP-168t ] p 80 N80-27428

Mechanical property characterization of

Borsic/aluminum laminates at room and elevated

temperatures

{NASA-TP-1761] p 81 N81.16130

Analysis and simulation of a magnetic bearing

suspension system for a laboratory model annular

momentum control device

[NASA-TP-17gg] p 99 N81-20311

Tribological characteristics of a composite total-surface

hip replacement

[NASA-TP-1853J p 94 N82-16239

tNHYD: Computer code for intraply hybrid composite

design. A users manuel

[ NASA-TP-22391 p 82 N84-13224

Buckling loads of stiffened panels subjected to combined

longitudinal compression and shear: ResultS obtained with

PASCO, EAL, and STAGS computer programs

[NASA-TP-2215] p 132 N84-16585

Structural efficiency studies of corrugated compression

panels with curved caps and beaded webs

[NASA-TP-2272] p 132 N84-18675

Effect of preforming adherends on static and fatigue

strength of bonded composite single-lap joints

[NASA-TP-2324] p 133 N84-26053

ACEE Composite Structures Technology: Review of

selected NASA research on composite materials and

structures

I NASA-CP-2321 J p 83 N84-29969

A cracked orthotropic sheet stiffened by a semi-infinite

orthotropic sheet

[NASA-TP-2455] p 134 N85-32339

High Temperature Polymer Matrix Composites

I NASA-CP-2385] p 83 N86-11260

Analytical Ultrasonics in Materials Research and

Tesbng

INASA-CP-2383] p 126 N86-22962

Symmetry considerations in the scattering ol identical

composite bodies

I NASA-TP-2548] p 193 N86-23388

Pocketing mechanics of SRM nozzle liner

[NASA-TP-2577] p 135 N86-23974

COMPOSITE STRUCTURES

Buckling and structural efficiency of sandwich.blade

stiffened composite compression panels

INASA-TP-1269] p 127 N78-32492

Failure Analysis and Mechanisms of Failure of Fi_ous

Composite Structures

INASA'CP'2278] p 82 N83o33957

COMPOSITE WRAPPING

Effect of low-stiffness cioseout overwrap on rocket

thrust-chamber life

[NASA-TP-1456] p 77 N79-23132

COMPRESSIBILITY EFFECTS

The compressible aerodynamics of rotating blades

based on an acoustic formulation

INASA-TP-2197) p 189 N84-13923

COMPRESSIBLE BOUNDARY LAYER

Calculation methods for compressible turbulent

boundary layers, 1976

[NASA-SP-4221 p 104 N78-13371

COMPRESSIBLE FLOW

Compressible flow across narrow passages:

Comparison of theory and experiment for face seals

INASA-TP-1346] p 120 N79-10424

Progress in turbulence modeling for complex flow fields

including effects of compressibility

[NASA-TP-1517] p 107 N80-20527

WIND: Computer program for calculation of three

dimensional potential compressible flow about wind turbine

rotor blades

[NASA-TP-1729] p 15 N80-33357

Computer program for aerodynamic and biading design

of multistage axiel-flow compressors

[NASA-TP-1946] p 49 N82-15039

Compressible, unsteady lifting-surface theory for •

helicopter rotor in forward flight

[NASA-TP-2503] p 27 N86-t828g

COMPRESSION LOADS

Effect of end-nng stiffneos on buckling of

pressure-loaded stiffened conw.el shells

[NASA-TP-1079] p 127 N78-12475

Tests of graphite/potyimide sandwich panels in uniaxial

edgewise compression

[NASA-TP-1785] p 81 N81-16129

Buckling loads of stiffened panels subjected to combined

longitudinal compression and shear: Results obtained with

PASCO, EAL. and STAGS computer programs

INASA-TP-2215] p 132 N84-16585

Fabrication and evaluation of ouparplastically

formed/weld-brazed corrugated compression panels with

beaded webs

[NASA-TP-2512] p 90 N86-t3406

COMPRESSION TESTS

Elevated-temperature application of the IITRI

compression test fixture for graphite/potylmide filamentary

composites

[NASA-TP-1496t p 80 N79-32277

COMPRESSIVE STRENGTH

Effects of fabrication and joining processes on

compressive strength of boron/aluminum and

bors_c/aluminum structural panels

lNASA-TP-1121 ] p 80 N78-20256

Structural efficiency studies of corrugated compression

panels with curved caps and beaded webs

INASA-TP-2272] p 132 N84-18675

A-26
SUBJECT INDEX

COMPUTER PROGRAMS

COMPRESSOR BLADES

Aerodynamic performance of 1.38-pressure.ratio,

variable-pitch fan stage

[NASA-TP-1502] p 45 N79-31213

Effects of diffusion factor, aspect ratio and solidity on

overall pedormance of 14 compressor middle stages ---

the effects of varying both diffusion through the rotor and

compressor blades and blade aspect ratio

[NASA-TP-1523] p 45 N79-332t0

Computer program for aerodynamic and blading design

of multistage axial-flow compressors

[NASA-TP-1946] p 49 N82-15039

Performance of single-stage axial-flow transonic

compressor with rotor and stator aspect ratios of 1.63

and 1.78, respectively, end with design pressure ratio of

t .82

[NASA-TP-1974] p 49 N82o19222

COMPRESSOR EFFICIENCY

Cold-air performance of a

12.766-centimeter-tip-diameter axial-flow cooled turbine.

3: Effect of rotor tip clearance on overall performance

of a solid blade configuration

[NASA-TP-1032] p 5 N77-32082

Design and overall performance of four highly loaded,

high speed inlet stages for an advanced high-pressure-ratic

core compressor

[NASA-TP-1337] p 43 N78-33108

Off-design correlation for losses due to part-span

dampers on transonic rotors

[NASA-TP-1693} p 47 N80-28352

STGSTK: A computer code for predicting multistage

axial flow compressor performance by a meantine stage

stacking method

[NASA-TP-20201 p 49 N82-25250

COMPRESSOR ROTORS

Performance of a transonic fan stage designed for a

low meridional velocity ratio

[NASA-TP-1298] p 43 N78-33107

Design and overall performance of four highly loaded,

high speed inlet stages for an advanced high-pressure-ratio

core compressor

[NASA-TP-1337] p 43 N78-33108

Design and performance of a

427-meter-per-second-tip-speed two-stage fan having a

2.40 pressure ratio

[NASA-TP-1314] p 43 N78-33109

Effect of casing treatment on performance of • two-stage

high-pressure-ratio fan

[NASA-TP-1409] p 44 N79-16852

Effect of rotor meridional velocity ratio on response to

inlet radial and circumferential distortion

[NASA-TP-1278] p 45 N79-28177

Performance of two-stage fan with a first-stage rotor

redesigned to account for the presence of a part-span

damper

[NASA-TP-1483] p 45 N79-30191

Effects of diffusion factor, aspect ratio end solidity on

OVerall performance of 14 compressor middle stages ---

the effects of varying both diffusion through the rotor end

compressor blades and blade aspect ratio

[NASA-TP-1523] p 45 N79-33210

Performance of single-stage axial-flow transonic

compressor with rotor end stator aspect ratios of t,63

and 1.78, respectively, and with design pressure ratiO of

1.82

[NASA-TP-1g74] p 48 N82-19222

High-speed laser anemometer system for intrerotor flow

mapping in turbomechinery

[NASA-TP-1663] p 115 N82-19521

Performance of single-stage axial-flow transonic

compressor with rotor and stator aspect ratios of 1,63

and t.77, respectively, and with design pressure ratio of

2,05

[NASA-TP-2001 ] p 49 N82-22269

Comparison of two- end three-dimensional flow

computations with laser anemometer measurements in s

transonic compressor rotor

[NASA-TP-1931] p 22 N83-32774

Lewis Research Center spin rig and its use in vibration

analysis of rotating systems

[NASA-TP-2304) p 51 N84-24578

COMPRESSORS

Fnction and wear of several compressor gas-path seal

movements

[NASA-TP-1128J p86 N78-15229

Performance of a tandem-rotor/tandem-stator

conical-flow compressor designed for a pressure ratio of

3

[NASA-TP-2034] p 20 N83-11058

COMPUTATION

Computation of transonic boaffail flow with separation

[NASA-TP-t070] p 7 N78-13017

Calculation of laminar heating rates on

three-dimensional configurations using the axisymmetric

analogue

[NASA-TP-1698} p 108 N80-33719

Computational Aspects of Heat Transfer in Structures

[NASA-CP-2216] p 109 N82-23473

The generalized Euler-Maseheroni constants

[NASA-TP-2264] p 185 N84-15880

Research in Structures and Dynamics, 1984

[NASA-CP-2335J p 134 N85-10377

Physical and numerical sources of computational

inefficiency in integration of chemical kinetic rate

equations: Etiology, treatment and prognosis

[NASA-TP-2590] p 183 N86-28662

COMPUTATIONAL FLUID DYNAMICS

Aerodynamic characteristics of a hypersonic research

airplane concept having a 70 deg swept double-delta wing

at Mach numbers from 0.80 to 1.20, with summary of data

from 0.20 to 6.0 --- Langley 8-ff transonic wind tunnel

[NASA-TP-15521 p 13 N80-12064

Velocity-split Navier-Stokes solution procedure for

incompressible high Reynolds number external flows

[NASA-TP-1655] p 108 N80-21702

Development and validation of a combined rotor

fuselage induced flow field computational method ---

Langley V/STOL tunnel

(NASA-TP-1656] p 15 N80-25296

Solution of complex nonlinear problems by a generalized

application of the method of base and comparison

solutions with applications to aerodynamics problems

(NASA-TP-18571 p 17 N81-22019

Fundamental heat transfer research for gas turbine

engines

( NASA-CP-2 t 78 ] p 48 N81-24063

Numerical Boundary Condition Procedures

[NASA-CP-2201] p 182 N8t-33856

Computer program for calculating full potential transonic,

quasi-three-dimensional flow through a rotating

turbomechinery blade row

[NASA-TP-2030] p 20 N82-28247

Combustion Fundamentals Research

[NASA-CP-2309J p 51 N84-20525

A crit,,cal evaluation of various turbulence models as

applied to internal fluid flows

INASA-TP-2474] p 112 N85-25757

Interactive algebraic grid-generation technique

[NASA-TP-2533] p 177 N86-23282

Numerical modeling of physical vapor transport in s

vertical cylindrical ampoule, with and without gravity

[NASA-TP-26201 p 96 N86-29040

COMPUTATIONAL GRIDS

Computational Geometry and Computer-Aided Design

[NASA-CP-2379] p 177 N85-28563

COMPUTER AIDED DESIGN

Research in computerized structural analysis and

synthesis

[NASA-CP-2059] p 128 N79-10448

Lubrication of optimized-design tapered-roller bearings

to 2.4 million DN

[NASA.TP.1714] p 121 N80.29734

The PR2D (Place, Route in 2-Dimensions) automatic

layout computer program handbook

[NASA-RP-1029] p 179 N81-12760

Pressure and force data for a flat wing and e warped

conical wing having a shockiess recompression at Mech

1.82

[NASA-TP-1759] p 17 N81-22016

Performance of computer-designed smell.sized

four-stage depressed collector for operation of dual-mode

traveling wave tube

[NASA-TP-1832] p 102 N81-30360

Research in nonlinear structural end solid mechanics

[NASA-CP-2147-SUPPL] p 130 N82.t1489

Interactive design end analysis of future large spacecraft

concepts

[NASA.TP-t9371 p 72 N82.14276

Computer program for aerodynamic and bledlng design

of multistage axial-flow compressors

[NASA-TP-1946] p 49 N82-15039

A general solution to the hidden-line problem ... to

graphically represent aerodynam,c stability derivatives

[NASA-RP-f085] p 176 N82-2t907

Automated procedure for developing hybrid computer

simulations of turbofan engines. Part 1: General

description

[NASA.TP-1851 ] p f 79 N82-33020

IPAD: Integrated Programs for Aerospace-vehicle

Design

[NASA-CP-2143] p 179 N83-17115

AESOP: An interactive computer program for the design

of linear quadratic regulators and Kalman filters

[NASA-TP-2221 ] p 181 N84-t6843

Computer-Aided Geometry Modeling

(NASA-CP-22721 p 177 N84-22179

IPAD 2: Advances in Distributed Data Base Managemenl

for CAD/CAM

[NASA-CP-2301 ] p 180 N84-22299

Computational Geometry and Computer-Aided Design

(NASA-CP-2379J p 177 N85-28563

Advanced secondary power system for transport

aircraft

[NASA-TP-2463} p 52 N85-28944

intersection of three-dimensional geometric surfaces

[NASA-TP-2454] p 177 N85-31839

Verification of computer-aided designs of traveling-wave

tubes utilizing novel dynamic refocusers and graphite

electrodes for the multistage depressed collector

{NASA-TP-2524] p 103 N86-13643

COMPUTER AIDED MANUFACTURING

IPAD: Integrated Programs for Aerospace-vehicle

Design

[NASA-CP-2143] p 179 N83-t7115

A common geometric data-base approach for

computer-aided manufectuhng of wind-tunnel models and

theoretical aerodynamic analysis

[NASA-TP-2151 ] p 21 N83-22166

tPAD 2: Advances in Distributed Data Base Management

for CAD/CAM

INASA'CP-2301 } p 180 N84-22299

COMPUTER ASSISTED INSTRUCTION

Conference of Remote Sensing Educators

(CORSE-78)

[NASA-CP-21021 p 212 N80-20003

COMPUTER COMPATIBLE TAPES

Magnetic Tape Recording for the Eighties

[NASA-RP-t075] p 116 N82-29579

COMPUTER GRAPHICS

The use of computer-generated color graphic images

for transient thermal analysis --- for hypersonic aircraft

[NASA-TP-1455J p 107 N79-30518

Procedure for extraction of disparate data from maps

into computerized data bases

[NASA-RP-1048] p 177 N79-33858

INFORM: An interactive data collection and display

program with debugging capability

[NASA-TP-1424] p 177 N80-16742

Simulator study of e pictorial display for general aviation

instrument flight

[NASA-TP-1963] p 39 N82-20180

A general solution to the hidden-line problem --- to

graphically represent aerodynamic stability derivatives

[NASA-RP-1085} p 176 N82-21907

Computer Science Research at Langley

[NASA-CP-2236] p 176 N82-26996

The window of visibility: A psychological theory of fidelity

in time-sampled visual motion displays

[ NASA-TP-2211 ] p 172 N83-33538

Computer-Aided Geometry Modeling

[NASA-CPo2272} p 177 N84-22179

Planetary Date Workshop, pert 2

[NASA-CP-2343-PT-2] p 208 N84-34376

Intersection of three-dimensional geometric surfaces

[NASA-TP-2454] p 177 N85-31839

Graphical techniques to assist in pointing and control

studies of orbiting spacecraft

[NASA-TP-2575] p 63 N86-21559

interactive algebraic grid-generation technique

[NASA-TP-2533] p 177 N86-23282

COMPUTER NETWORKS

Fault tolerant computing: A preamble for assuring

viability of large computer systems

[NASA-TP-1087J p 177 N77-33868

NASF transposition network: A computing network for

unscrambling p-ordared vectors

[NASA-TP-1426] p 180 N79-21822

Planetary Date Workshop, pert 2

[NASA-CP-2343-PT.2] p 208 N84.34376

Proceedings of the Second Pilot Climate Data System

Workshop

[NASA-CP-2430] p 137 N88-29282

COMPUTER PROGRAMMING

Advances in engineering science, volume 2

(NASA-CP-2001-VOL-2] p 98 N77-t0265

Analytical investigation of the lending dynamics of a large

airplane with a load-control system in the main landing

gear

INASA-TP-t555] p 33 N80.13025

CYBER 200 Applications Seminar

[NASA*CP-2295] p 179 N84-20208

Research in Structures and Dynamics, 1984

[NASA.CP.2335] p 134 N85-10377

Space Station Software Issues

[NASA-CP-2361] p 179 N85-20689

COMPUTER PROGRAMS

Proceedings of the 1977 MACSYMA users' conference

(NASA)

{NASA-CP-2012] p 176 N77-28750

Standardization, certification, maintenance, and

dissemination of large scale engineering software

systems

[NASA-CP-2015] p 178 N77-33876

Validation of a Flexible Aircraft Take-Off and Landing

Analysis (FATOLA)

[NASA-TP-1025] p 31 N78-fO049

A-27
COMPUTER STORAGE DEVICES SUBJECT INDEX

Sixth NASTRAN Users' Colloquium

{NASA-CP 20181 p 127 N78-12443

GEMPAK: An arbitrary aircraft geometry generator

[NASA-TP-t022] p 32 N78-16042

Computer program for obtaining thermodynamic and

transport properties of air and products of combustion of

ASTM-A-1 fuel and air

INASA-TP-1160] p 97 N78-20351

Application of a two-dimensional parabolic computer

program to prediction of turbulent reacting flows

{NASA-TP-11691 p 105 N78-20463

Predicted and experimental performance of

jet-lubricated f20-mitlimeter-bore ball bearings operating

to 25 million DN

INASA-TP-1196] p 119 N78-20513

Comparison of two computer programs by predicting

turbulent mixing of helium in a ducted supersonic

airstream

{NASA-TP-11661 p 105 N78-22333

ORACLS: A system for linear-quadratic-Gaussian

control law design

INASA-TP-ft06] p 181 N78-22809

FORTRAN program for calculating coolant flow and

metal temperatures of a full-coverage-film-cooled vane or

blade

[ NASA-TP-1259 ] p 43 N78-28099

TACTt, a computer program for the transient thermal

analysis of a cooled turbine blade or vane equipped with

a coolant msert_ 1 Users manual

INASA-TP-1271 } p 105 N78-28374

DYGABCD: A program for calculating linear A, B, C,

and D matrices from a nonlinear dynamic engine

simulation

[NASA-TP-1295} p 43 N78-33110

Guide to a condensed form of NASTRAN

INASA-RP-f019} p 178 N78-33791

Tools for Embedded Computing Systems Software

I NASA-CP-2064 } p 178 N79-13736

An integrated computer procedure for sizing composite

airframe structures

{NASA-TP-13001 p 178 N79-17580

Computation of atmospheric attenuation of sound for

fractional-octave bands

[NASA-TP-t412] p 186 N79-17659

TACT 1: A computer program for the transient thermal

analysis of a cooled turbine blade or vane equipped with

a coolant insert. 2. Programmers manual

[NASA-TP-1391 I p 106 N79-18288

Advanced Technology Airfoil Research, volume 1, part

1 --- conference on development of computational cedes

and test facilities

[NASA-CP-2045-PT-t ] p 11 N79-20030

Interactive debug program for evaluation and

modification of assembly-language software

[NASA-TP-t441 ] p 178 N79-21798

Analytical prediction with multidimensional computer

programs and experimental verification of the

performance, at a vanety of operating conditions, of two

traveling wave tubes with depressed collectors

INASA-TP-1449} p t0t N79-22375

WETAIR: A computer cede for calculating

thermodynamic and transport properties of air-water

mixtures

[NASA-TP-f4661 p 178 N79-23688

Programs for calculating cell parameters in electron and

X-ray diffraction --- to identify stratospheric aerosols

{NASA-TP-15291 p 148 N79-30844

Processing of on-board recorded data for quick analysis

of aircraft performance --- rotor systems research

aircraft

{NASA-RP-10431 p 33 N79-33191

Computer program for generating input for analysis of

impingement-cooled, axial-flow turbine blade

{NASA-TP-1603] p 107 N80.15361

Aerodynamic performances of three fan stator designs

operating with rotor having tip speed of 337 meters per

second and pressure ratio ot t 54 Relation of analytical

code calculations to experimental performance

[ NASA-TP-1614 ] p46 N80-21324

Viscous-inviscid calculations ol jet entrainment effects

on the subsonic flow over nozzle afterbodies

INASA-TP-1626} p 14 N80-22261

A numerical technique for calculation of the noise of

high-speed propellers with advanced blade geometry

INASA-TP-1662] p 167 N60-27161

CAS2D: FORTRAN program for nonrotating

blade-to-blade, steady, potential transonic cascade flows

INASA-TP-1705} p 15 N80-27284

Algorithm for fixed-range optimal trajectories

{NASA-TP-1565} p 30 N80-28329

WIND: Computer program for calculation of three

dimensional potential compressible flow about wind turbine

rotor blades

{NASA-TP-f7291 p 15 N80-33357

Development and test results of a flight management

algorithm for fuel conservative descents in a time-baaed

metered traffic environment

tNASA-TP 17171 p 39 N80-33404

Estimation of wing nonlinear aerodynamic

characteristics at supersonic speeds

INASA-TP-17181 p 15 N81-10004

Aerospace Applications ot Microprocessors

INASA-CP-21581 p 177 N8t-11644

An improved viscous characteristics analysis program

INASA-TP-f289] p 108 Nat-t2356

User's manual for MMLE3, a general FORTRAN program

for maximum likelihood parameter estimation

[NASA-TP-15631 p 176 N81-12744

The PR2D (Place, Route in 2-Dimensions} automatic

layout computer program handbook

[NASA-RP-1029] p 179 N81-12760

MEGA16 - Computer program for analysis and

extrapolation of stress-rupture data

INASA-TP-1809] p 130 N81-23486

Programmer's manual for MMLE3, a general FORTRAN

program for maximum likelihood parameter estimation

l NASA-TP-f 6901 p 176 N81-276f 3

Computer analysis of flow perturbations generated by

placement of choke bumps in a wind tunnel

INASA-TP-t892J p 18 N81-30088

GRID30: Computer program for fast generation of

multilevel, three-dimensional boundary*conforming O-type

computational gnds

{NASA-TP-19201 p 18 N81-31128

Computer program for pulsed thermocouples with

corrections for radiation effects

[NASA-TP-1895} p 179 N81-33838

Computer program to predict aircraft noise _evels

INASA-TP-19131 p 188 N81-33947

Some observations on e new numerical method for

SO_Vln_ Navier-Stokes equations

{NASA-TP-f934] p t6 N_,2-11032

Numerical analysis of the scramjet-inlet flow field by

using two-dimensional Navier-Stokes equations

{NASA-TP-1940] p 48 N82-13142

STGSTK: A computer code for predicting multistage

axial flow compressor perlormance by a meanline stage

stacking method

[NASA-TP-2020] p 49 N82-25250

Computer program for calculating full potential transonic,

quasi-three-dimensional flow through a rotating

turbomachinery blade row

I NASA-TP-2030} p 20 N82-28247

Automated procedure for developing hybnd computer

simulations of turbofan engines. Part 1: General

description

I NASA-TP-1851 } p 179 N62-33020

IPAD: Integrated Programs for Aerospace-vehicle

Design

{NASA-CP-2143] p 179 N83-17115

Design analysis of a self-acting spiral-groove nng seal

for counter-rotating shafts

{NASA TP-2142J p 50 N83-25712

Theoretical and experimental investigation of superson*c

aerodynamic characteristics of a twin-fuselage concept

{ NASA-TP-21841 p 22 N83-32776

Eleventh NASTRAN User's Colloquium

INASA-CP-2284} p 132 N84-15590

Buckling loads of stiffened panels subjected to combined

longitudinal compression and shear: Results obtained with

PASCO, EAL, end STAGS computer programs

[NASA-TP-2215J p 132 N84-16585

Topics in the optimization of millimeter-wave mixers

I NASA-TP-22871 p 103 N84-20758

Devetopmenl of a simplified procedure for cyclic

structural analysqs

{NASA-TP-22431 p 133 N84-20878

A user-oriented and computerized model for estimating

vehicle ride quality

{NASA-TP-22991 p 172 N84-22162

STABCAR: A program for finding characteristic root

systems having transcendental stability matrices

[NASA-TP-2165] p 179 N84-2746f

Validation of an Active Gear, Flexible Aircraft Take-off

and Landing analysis (AGFATL)

[NASA-TP-23531 p 37 N84-32378

Analytical and experimental investigation of stator

endwatl countouring in a small axial-flow turbine

lNASA-TP'2309] p 51 N84-32388

GCKP84-generat chemical kinetics code for gas-phase

flow and batch processes including heat transfer effects

[NASA-'rP-2320] p 85 N84-32446

An experimental and theoretical investigation of

deposition patterns from an agricultural airplane

[ NASA-TP-2348] p 25 N84-33379

Transonic flow analysis for rotors Part f:

Three-dimensional quasi-steady, full-potential calculation

I NASA-TP-2375-PT 1 } p 25 N85-10914

STARS: A general-purpose finite element computer

program for analysis of engineering structures

INASA-RP-1129] p 134 N85-11378

Algorithm for astronomical, extended source,

s_gnal-to-noiso radio calculations

I NASA-TP-2396] p 202 N85-12833

Algorithm for astronomical, point source, signal to noise

ratio calculations

I NASA-TP-23971 p 202 N85-12834

Modeling the internal combustion engine

INASA-RP-10941 p 182 N85-19733

Combustion gas properties Part 3: Hydrogen gas fuel

and dry air

[NASA-TP-2477] p 52 N85-31058

The algorithms for rational spline interpolation of

surfaces

INASA-TP-2536] p 183 N86-t8060

Star 48 solid rocket motor nozzle analyses and

instrumented firings

[NASA-TP-2572} p 68 N86-20460

Integrated Composite Analyzer (ICAN): Users and

programmers manual

i NASA-TP-2515 ] p 83 N86-21614

Space Station Software Recommendations

INASA-CP-2394] p 180 N86-23314

Physical and numerical sources of computational

inefficiency in integration of chemical kinetic rate

equations: Etiology, treatment and prognosis

[NASA-TP-2590} p 183 N86-28662

COMPUTER STORAGE DEVICES

Ruggedized minicomputer hardware and software

topics, 1981: Proceedings of the 4th ROLM MIL-SPEC

Computer User's Group Conference

I NASA-CP-22061 p 180 N82-14829

COMPUTER SYSTEMS DESIGN

Future Computer Requirements for Computational

Aerodynamics

[NASA-CP-2032] p 176 N78-19778

Validation Methods for Fault-Tolerant avionics and

control systems, working group meeting 1

INASA-CP-21141 p 176 N80-1274t

Validation Methods Research for Fault.Tolerant Avionics

and Control Systems: Working Group Meeting, 2

[ NASA-CP-2130 } p 176 N80-23008

An analytical procedure for computing smooth

transitions between two specified cross sections with

applications to blended wing body configuration

[NASA-TP-2012] p 19 N82-25193

Human Factors Considerations in System Design

{NASA-CP-2246] p 173 N83-18238

Planetary Data Workshop. part 2

INASA-CP-2343-PT-2} p 208 N84-34376

COMPUTER SYSTEMS PERFORMANCE

Production of Reliable Flight Crucial Software: Validation

Methods Research for Fault Tolerant Avionics and Control

Systems Sub-Working Group Meeting

] NASA-CP-2222] p t79 N82-24845

Validation of a fault-tolerant clock synchronization

system

INASA-TP-2346] p 180 N84-34198

An image compression survey and algorithm switching

based on scene activity

(NASA-TP-2458} p 27 N85-33106

COMPUTER SYSTEMS PROGRAMS

The N-BOD2 user's and programmer's manual

[NASA-TP-t145} p 70 N78-21200

Tools for Embedded Computing Systems Software

{NASA-CP-2064} p 178 N79-13736

INFORM: An interactive data collection and display

program with debugging capability

{NASA-TP-14241 p 177 N80-16742

Planetary Data Workshop, part 2

I NASA-CP-2343-PT-21 p 208 N84-34376

MINDS: A microcomputer interactive data system for

8086-basod controllers

I NASA-TP-2378} p 179 N85-t 7576

COMPUTER TECHNIQUES

Engineering and Scientific Data Management

{ NASA-CP-2055} p 178 N78-33776

Mathematical Modeling of Diverse Phenomena

{NASA-SP-437} p 182 N80-13839

A computer technique for detailed analysis of mission

radius and maneuverability characteristics of fighter

aircraft

{NASA-TP+18371 p 17 N81-20026

Computer Science Research at Langley

{NASA-CP-22361 p 176 N82-26996

The LANDSAT tutorial workbook: Basics of satellite

remote sensing

{E83-t000f} p 141 N83-10458

Twelfth NASTRAN Users' Colloquium

INASA-CP-2328} p 133 N84-32864

Research in Structures and Dynamics, 1984

{NASA-CP-2335] p 134 N85-10377

A-28
SUBJECT INDEX CONFERENCES

Planning fuel-conservative descents in an airline

environmental using a small programmable calculator:

Algorithm development and flight test results

{NASA-TP-2393 J p 40 N85-26705

COMPUTERIZED SIMULATION

Development and verification of real-time, hybrid

computer simulation of F100-PW-100(3) turbofan engine

[NASA-TP-t034J p 41 N77-31154

F100 multivariabte control synthesis program:

Evaluation of a multivariable control using a real-time

engine simulation

[NASA-TP-1056} p 41 N77-33169

Simulation studies of wide and medium field of view

earth radiation data analysis

[NASA-TP-tt82] p 158 N78-23679

A digital computer program for the dynamic interaction

simulation of controls and structure (DISCOS), volume t

[NASA-TP-1219-VOL-I ] p 70 N78-25123

A digital computer program for the dynamic interaction

simulation of controls and structure (DISCOS), volume 2

{NASA-TP-t219-VOL-21 p 70 N78-25124

Application of special-purpose digital computers to

rotorcraft real-time simulation

[NASA-TP-1267} p 32 N78-27113

Simulation model of a single-stage lithium bromide-water

absorption cooling unit

[ NASA-TP-1296] p86 N78-30205

Procedures for generation and reduction of linear models

of a turbofan engine

[NASA-TP-1261 I p 184 N78-30896

Simulation study of the power of the

Kotmogoroft-Smirnoff and Z tests for the exponential

distribution

INASA-TP-13111 p 183 N78-31854

DYGABCD: A program for calculating linear A, B, C.

and D matrices from a nonlinear dynamic engine

simulation

INASA-TP-1295] p 43 N78-33110

Research in computerized structural analysis and

synthesis

{NASA-CP-20591 p 128 N79-10448

Computer formulations of aircraft models for simulation

studies

[NASA-TP-1470J p 2 N79-23008

Collisionless galaxy simulations

JNASA-RP-1037 T p 201 N79-24921

Modets of human operators in vision dependent tasks

INASA-CP-2103] p 171 N79-33838

Computer-automated opponent for manned air-to-air

combat simulations

[NASA-TP-1518J p 176 N79-33855

An experimental evaluation of head-up display formats

{NASA-TP-15501 p 39 N80-28349

Simulation development and evaluation of an improved

longitudinal velocity vector control wheel steering mode

and electronic display format

{ NASA-TP-1664 I p 39 N80-30305

Development and validation of a hybrid-computer

simulator for a transonic cryogenic wind tunnel

INASA-TP-1695j p 59 N80-31413

Development of the reentry flight dynamics simulator

for evaluation of space shuttle orbiter entry systems

[NASA-TP-1700) p 71 N80-32429

Development and test results of a flight management

algorithm for fuel conservative descents in a time-based

metered traffic environment

[NASA-TP-1717_ p 39 N80-33404

Anatysis and simulation of a magnetic bearing

suspension system for a laboratory model annular

momentum control device

[NASA-TP-1799i p 99 N81-20311

Computer simulation of random variables and vectors

with arbitrary probability distribution laws

[NASA-TP-1859} p 183 N81-23838

Application of a performance modeling technique to an

airplane with variable sweep wings

{NASA-TP-t855J p 35 N81-24048

New features and applications of PRESTO, a computer

code for the performance of regenerative, superheated

steam turbine cycles

JNASA-TP-1954r p 145 N82-16477

A general sotution to the hidden-line problem --- to

graphically represenl aerodynamic stability derivatives

[NASA-RP-1085] p 176 N82-21907

Automated procedure for deveJoping hybrid computer

simulations of turbofan engines. Part 1: General

description

[NASA-TP-1851 ] 13 179 N82-33020

Summary Proceedings of a Wind Shear Workshop

t NASA-CP-22701 p 165 N83-25265

Effect of lead-aircraft ground-speed on self-spacing

performance using a cockpit display of traffic information

] NASA-TP-2194 I p 40 N83-36028

CYBER 200 Applications Seminar

J NASA-CP-2295r p 179 N84-20208

NASA Aircraft Controls Research, 1983

{NASA-CP-22961 p 58 N84-20567

Simulation of a cockpit-display concept for executing a

wake-vorlex avoidance procedure

[NASA-TP-2300} p 40 N84-21542

Effect of aerodynamic and angle-of-attack uncertainties

on the blended entry flight control system of the Space

Shuttte from Mach 10 to 2.5

JNASA-TP-22831 p 58 N84-23652

Automated rendezvous and docking: A parametric

study

[NASA-TP-2314J p 74 N84-23677

A spatial model of wind shear and turbulence for flight

simulation

{ NASA-TP-2313 j p 165 N84-24044

A numerical simulation of three-dimensional flow in an

adaptive wall wind tunnel

[NASA-TP-23511 p 24 N84-28750

Thirteenth Space Simulation Conference The Payload:

Testing for Success

{NASA-CP-2340} p 74 N84-34468

Translational control of a graphically simulated robot arm

by kinematic rate equations that overcome elbow joint

singularity

{NASA-TP-23761 p 181 N85-15446

Kinematic rate control of simulated robot hand at or

near wrist singularity

JNASA-TP-2440} p 181 N85-27575

Adding computationally efficient realism to Monte Carlo

turbulence simulation

[NASA-TP-24691 p 185 N85-28708

Piloted simulation of an algorithm for onboard controt

of time-optimal intercept

{NASA-TP-2445] p 58 N85-28949

Simulation studies of time-control procedures for the

advanced air traffic control system

INASA-TP-24931 p 30 N85-32t01

Investigation of solid plume simulation criteria to produce

flight plume effects on multibody configuration in wind

tunnel tests

INASA-TP-25691 p 28 N86-21507

CONCENTRATION (COMPOSITION)

Ozone concentration in the cabin of a Gates Learjet

measured simultaneously with atmospheric ozone

concentrations

INASA-TP-1340] p 148 N78-33618

Effect of concentration dependence of the diffusion

coefficient on homogenization kinetics in multiphase binary

alloy systems

{NASA-TP-1281 J p 87 N79-13138

Ionized dopant concentrations at the heavily doped

surface of a silicon solar cell

[NASA-TP-1347} p 195 N79-13886

Ozone measurement system for NASA global air

sampling program

[NASA-TP-1451] p 148 N79-22654

An asymptotic expansion approach to the inverse

radiative transfer problem --- to infer concentration profiles

of the atmosphere from measurements made oeboard a

satellite

[NASA-TP-1587] p 152 N80-13730

Nitrogen dioxide vapor penetration of chlorobutyl rubber

SCAPE under operational conditions

{NASA-TP-1605} p85 N80-16118

CONCENTRATORS

Design and fabrication of a low-specific-weight parabolic

dish solar concentrator

JNASA-TP-1152] p 75 N78-17145

CONCRETES

Crash tests of three identical Iow-wiog single-engine

airplane

{NASA-TP-2190J p 30 N83-34921

CONDENSATION NUCLEI

Studies of condensation effects on airfoil testing in the

Langley 0.3-meter transonic cryogenic tunnel

[ NASA-TP-25091 p 113 N86-20720

CONDENSING

Condensation-nuclei (Aitken Particle) measurement

system used in NASA global atmospheric sampling

program

INASA-TP-1415] p 148 N79-18479

Outgassing data for spacecraft materials

{NASA-RP-1061 j p 80 N80-30441

The Third International Cloud Condensation Nuclei

Workshop --- conference

{NASA-CP-2212} p 115 N82-15383

Outgassing data for selecting spacecraft materials

I NASA-RP-1124 J p82 N84-26751

CONDITIONS

Numerical Boundary Condition Procedures

[NASA-CP-2201 ] p 182 N81-33856

CONDUCTION

Hybrid perturbation/Bubnov-Galerkin technique for

nonlinear therma} analysis

{NASA-TP-21451 p 111 N84-22907

CONDUCTORS

Secondary-electron-emission properties of conducting

surfaces with application to multistage depressed

collectors for microwave amplifiers

{NASA-TP-10971 p 86 N78-tt230

CONES

Aerodynamic heating on the corrugated surface of a

10,2 deg half-angle blunted cone at Mach 6.7

[NASA-TP-1928} p 109 N82-13383

Theoretical basis for design of thermal-stress-free

fasteners

[NASA-TP-22261 p 132 N84-13614

Correlations of supersonic boundary-layer transition on

cones including effects of large axial variations in

wind-tunnel noise

[NASA-TP-2229} p 111 N84-17534

Aerothermal tests of a 12.5 percent cone at Math 67

for various Reynolds numbers, angles of attack and nose

shapes --- conducted in Langley 8-foot high temperature

tunnel

INASA-TP-2345} p 112 N85-17322

CONFERENCES

Advances in engineering science, volume 1

JNASA-CP-2001-VOL-1 ] p 98 N77-10230

Advances in engineering science, volume 2

INASA-CP-2001-VOL-21 p 98 N77-10265

Advances in engineering science, volume 3

[NASA-CP-2001-VOL-3} p 98 N77-10305

Atmospheric aerosols: Their Optical Properties and

Effects (supplement)

{NASA-CP-2004-SUPPL] p 151 N77-15564

Aircraft Piston Engine Exhaust Emission Symposium

[NASA-CP-2005J p 41 N77-17081

Proceedings of the SCAR Conference, part 1

{NASA-CP-001-PT-1 ] p I N77-17996

Proceedings of the SCAR Conference, part 2

{NASA-CP-00t-PT-2} p 1 N77-18019

Aircraft Safety and Operating Problems --- conference

INASA-SP-416] p 28 N77-18081

Flutter Testing Techniques

INASA-SP-415] p 1 N77-21022

Space settlements: A design study

[NASA-SP-4131 p 60 N77-21106

Systems reliabihty issues for future aircraft

{NASA-CP-003] p 175 N77-22808

High Reynolds Number Research

[NASA-CP-2009I p 59 N77-27139

Proceedings of the 1977 MACSYMA users' conference

(NASA)

{NASA-CP-2012J p 176 N77-28750

Proceedings of the ASPE/MSFC Symposium on

Engineering and Productivity Gains from Space

Technology

J NASA-CP-2019] p 98 N77-30273

Standardization. certification, maintenance, and

dissemination of large scale engineenng software

systems

{NASA-CP-2015J p 178 N77-33876

An Assessment of Technology for Turbojet Engine Rotor

Failures

{NASA-CP-2017 p 41 N78-10068

Aircraft engine emissions --- conference

JNASA-CP-2021 p 41 N78-1t063

The use of nonhuman primates in space

J NASA-CP-005 p 169 N78-11863

Wake Vortex Minimization

[NASA-SP-409 p 6 N78-120t7

Sixth NASTRAN Users' Colloquium

[NASA-CP-2018 p 127 N78-12443

Inversion Methods in Atmospheric Remote Sounding

JNASA-CP-O04 p 151 N78-t2586

The Soviet-American Conference on Cosmochemistry

of the Moon and Planets, part 1

{NASA-SP-370-PT-f I p 203 N78-12925

Solar Cell High Efficiency and Radiation Damage

I NASA-CP-2020 j p 144 N78-t 3527

Proceedings of the 1977 NASA/ISHM Microelectronics

Conference

[NASA-CP-2027] p 101 N78-16266

AIAA/MSFC Symposium on Space Industrialization:

Proceedings

[ NASA-CP-20261 p 60 N78-18088

Guntersville Workshop on Solar-Terrestrial Studies

{NASA-CP-20371 p 144 N78-19600

Future Computer Requirements for Computational

Aerodynamics

INASA-CP-2032J p 176 N78-19778

Application ol Remote Sensing to the Chesapeake Bay

Region. Volume 2: Proceedings

JNASA-CP-006-PT-21 p 138 N78-2152{5

Active Microwave Users Workshop Report

{NASA-CP-20301 p 138 N78-21562

Application of Remote Sensing to the Chesapeake Bay

Region Volume 1: Executive summary

{NASA-CP-O06-PT.1 I p f38 N78-23537

A-29
CONFERENCES

Powered-Lifl Aerodynamics and Acoustics ---

conferences

( NASA-SP-406] p 8 N78-24046

CTOL transport technology, 1978 --- conferences

t NASA_CP.2036-PT-1 j p I N78-27046

Emerging Energy Alternatives for the Southeastern

States

[NASA-CP-20421 p 144 N78-28615

CTOL Transport Technology, 1978 ---conferences

INASA-CP-2036"PT'2] p 1 N78-29046

Exploratory Meeting on Atmospheric Electricity and

Severe Storms

[NASA-CP-2056] p 151 N78-29669

YFot 2 experiments symposium, volume 1

[NASA-CP'2054"VOL-t ] p g N78-32055

Seventh NASTRAN Users Colloquium

[NASA'CP'2062] p 127 N78-32466

Helicopter Acoustics

[NASA-CP-2052-PT-t} p 185 N78-32816

Engineering and Scientific Data Management

{NASA-CP-2055] p 178 N78-33776

Large Space Systems Technology, volume 1

[NASA-CP-2035-VOL-t ] p 65 N79-10078

Large Space Systems Technology, volume 2

[ NASA-CP-2035-VOL-2 ] p66 N79-10097

Future Orbital Power Systems Technology

Requirements

INASA-CP-2058] p 76 N79-10122

Hypertherm_a as an Antineoplastic Treatment Modality

I NASA-CP-2051 } p t70 N79-10728

Helicopter Acoustics, part 2 --- conferences

INASA-CP-2052-PT-2] p 186 N79-10843

Proceedings of the Workshop On an Electromagnetic

Positioning System in Space

I NASA-CP-2069J p 61 N79-13069

Flight Mechanics/Estimation Theory Symposium

/NASA-CP-2050J p 64 N79-14121

The 14th Annual Conference on Manual Control --- digit el

s*mulat_on of human operalor dynamics

INASA-CP-2060} p 173 N79-15588

Human Neurologlca_ Development: Past, Present and

Future

INASA-CP-2063J p 212 N79-15887

Avionics and controls research and technology

[NASA-CP-20611 p t N79-15898

The rotary combustion engine A candidate for general

avlahon - conferences

l NASA-CP-2067 ] p 44 N79-15961

Soil Moisture Workshop

[ NASA CP-2073 ] p 138 N79-16329

The Saturn System

i NASA-CP-2068 ] p 205 N79-16758

Proceedings of the 2rid Annual Workshop on

Meteorologicab and Environmental _nputs to Aviation

Syslems

I NASA-CP 20571 p 159 N79-17413

Ninth Conference on Space Simulation

]NASA CP 2007] p 61 N79-19013

Advanced Technology Airfoil Research. volume 1, part

1 -.- conference on development of oomputationa_ codes

and test facilities

!NASA-CP-2045-PT 1 I p 11 N79-20030

Govelnment/Industry Workshop on Payload Loads

Technology

I NASA-CP-20751 p 62 N79-20162

Proceedings ol the NASA/Florida _nstitute of

Technology Environmental Engineering Conference on

Nitrogen Tetroxide - with emphasis on space shuttle

INASA-CP-2049j p 136 N79+20424

Third Nahonal Aeronautics and Space Administration

Weather and climate program sc=ence review

INASA CP-2029i p t59 N79-20575

Fourth National Aeronautics and Space Admlnrstration

Weather and Climate Program Science Review

[ NASA CP 2076 ] p 159 N79-20633

The 121h Aerospace Mechanisms Symposium

INASA-CP-2080] p 120 N79-21352

The 11th Aerospace Mechamsms Symposium

INASA-CP-20381 p 120 N79-21374

Recent Advances in Structures for Hypersonic Fhghl,

pad t --- conlerences

I NASA CP 2065 PT 11 p 128 N79-2t422

Recent Advances m Structures for Hypersonic Flight,

part 2

}NASA CP-2065-PT-2] p 128 N79-21435

The 1977 Goddard Space Flight Center Battery

Workshop

INASA-CP-20411 p 144 N79 21565

Carbon Fiber Risk Analysis --- conference

[ NASA-CP-2074 ] p 80 N79-22196

The 131h Aerospace Mechanisms Symposium

I NASA-CP-2081] p 128 N79-22539

The science and technology of low speed and motorless

Ihght, part t

I NASA.CP-2085 PT 1 I p 2 N79-23889

Aircraft icing

[ NASA-CP-2086 ] p 12 N79-23912

Spacecraft Charging Technology, 1978

[NASA-CP-2071 I p 71 N79-24001

Premixed Prevaporized Combustor Technology Forum

INASA-CP-20781 p 44 N79-24994

Proceedings of the USAF/NASA International

Spacecraft Contamination Conference

INASA-CP'2039] p 62 N79-25048

Middle atmosphere electrodynamics: Report of the

workshop on the Role of the Electrodynamics of the Middle

Atmosphere on Solar Terrestrial Coupling

[NASA-CP-2090} p 152 N79-25608

Proceedings o! workshops to define engineehng

requirements for a space vacuum research fecility

[NASA-CP.2091] p 62 N79.26076

Flight Mechanics/Estimation Theory Symposium --- with

application to autonomous navigation and attitude/orbit

determination

[NASA-CP-2082] p 64 N79-26082

Science end Technology of Low Speed and Motorless

Flight, Third International Symposium

[L-12973] p 2 N79-27070

The 1 tth Annual Battery Workshop

[NASA-CP-20881 p 144 N79-28669

Graphite/Polyimide Composites --- conference on

Composites for Advanced Space Transportation

Systems

INASA-CP-2079] p 80 N79-30297

Proceedings: Workshop on the Need for Lightning

Observations from Space

INASA-CP'2095] p 152 N79-30869

Conference on Fire Resistant Materials: A compilation

of presentations and papers

[ NASA-CP-2094 } p 29 N79-31166

Solar Celt High Efficiency and Radiation Damage,

1979

INASA.CP-20971 p 144 N79-32640

Earth Radiation Budget Science, 1978 ---conferences

INASA-CP-21001 p 160 N79-32797

Summary of the NASA/MSFC FY-79 Severe Storm and

Local Weather research review --- cloud physics.

atmospheric electricity, and mesoscale/storm dynamics

reserech

[NASA-CP-2105J p 160 N79-33722

Workshop on Thrust Augmenting Ejectors

[NASA-CP-20931 p 13 N80-I0107

Aeropropulsion 1979 --- conferences

I NASA-CP-20921 p 45 N80-10205

Space missions to comets

I NASA-CP-20891 p 206 N80-11972

Preliminary applications and evaluation results

Lixiscope: Proceedings of the Lixiscope Conference

INASA-CP-2112] p 114 N80-12384

Flight Technology Improvement --- spaceborne optical

radiometric instruments, attitude control, and

electromechanical and power subsystems

I NASA-CP-2101 I p 75 N80-13152

Nuclear-Pumped Lasers --- efficient conversion of

energy liberated in nuclear reactions to coherent

radiation

{NASA-CP-2107 l p 1t7 N80-13438

Proceedings, Third Annual Workshop on Meteorological

and Environmental Inpuls to Aviation Systems

[NASA-CP-21041 p 160 N80-14633

HEAD Science Symposium

INASA-CP-2113t p 200 N80-14977

Quiet powered-lilt propulsion

1 NASA CP-20771 p 46 N80-15127

Proceedings of Shuttle Environmental Effecls Program

Review --- conferences

INASA-CP-2110] p 149 N80-15649

Study of the Solar Cycle from Space

I NASA-CP-2098] p 209 N80-17944

implications of fuel-efficient vehicles on ride quality and

passenger acceptance: Workshop proceedings

INASA-CP-2096] p 199 N80-18990

An assessment Of ground-based techniques for

detecting other planetary systems Volume 1 Anoverview

--- workshop conclusions

INASA-CP-2124-V©L-1 I p 201 N80-18997

Large Space Systems Technology, 1979 --- antenna and

space platform systems conference

INASA-CP-2118] p 66 N80-19145

Conference of Remote Sensing Educators

1CORSE-78)

/NASA-CP-2102] p 212 N80-20003

The 1979 Goddard Space Fhght Center Battery

Workshop

INASA-CP-21171 p 145 N80-20820

Advanced technology airfoil research, volume 2 --

conferences

INASA-CP-20461 p 14 N80-21283

Lighlning Technology Proceedings of a technical

symposium

INASA-CP 2128i p 161 N80-21927

SUBJECT INDEX

Scientific research with the space Telescope:

international Astronomical Union Colloquium no. 54 ---

conferences

{ NASA-CP-2111 ] p 200 N80-22130

Resource management on the fhght deck ---

conferences

[NASA-CP-2120] p 29 N80-22283

General Aviation Propulsion

INASA-CF-21261 p 46 N80-22327

Thermal Energy Storage: Fourth Annual Review

Meeting

[NASA-CP-2125 } p 145 N80-22788

Proceedings ol the 14th Aerospace Mechanisms

Symposium

[NASA-CP-2127] p 99 N80-23495

Remote Sensing and Problems of the Hydrosphere. A

Focus for Future Research --- conferences

[NASA-CP-2132] p 168 N80-23956

Eighth NASTRAN User's Colloquium

[NASA-CP-2131 } p 129 N80-24648

Proceedings of the Aero-Optics Symposium on

Electromagnetic Wave Propagation from Aircraft

INASA-CP-2121 ] p 108 N80-25588

Operational Applications of Satellite Snowcover

Observations

[E80-101671 p 139 N80-25742

Exploratory Meeting on A=rborne Doppler Lidar Wind

Velocity Measurements

[NASA-CP-21401 p t62 N80-26999

High Resolution Infrared Spectroscopy Techniques for

Upper Atmospheric Measurements

INASA-CP-2134] p 152 N80-27866

Time-of-Day Corrections to Aircraft Noise Metrics

INASA-CP-2135} p t87 N80-28150

Flight Mechanics/Estimation Theory Symposium

[NASA-CP-2123} p 64 N80-28389

Selected NASA research in composite Materials and

structures

INASA-CP-2142] p 80 N80-28436

Radio interlerometry: Techniques for Geodesy ---

conference

[NASA-CP-2115J p 139 N80-28798

NASA/MSFC FY-80 Atmospheric Processes Research

Review

I NASA-CP-21451 p 153 Ng0-28965

Proceedings of the Eleventh Annual Precise Time and

Time Interval (pTTI) Application and Planning Meeting ---

conference

[NASA-CP-21291 p 185 N80-29096

Aircraft Research and Technology for Future Fuels

I NASA-CP-2146] p 47 N80-29300

Heterodyne systems and technology, part 1 ---

conferences

INASA-CP-2138-PT-1 j p 117 N90-29652

Rotordynamic Instability Problems in high-performance

turbomach_nery

INASA-CP-2133] p 121 N80-29706

Large Space Systems/Low-Thrust Propulsion

Technology

{NASA-CP-2144J p 77 N80o31449

Synchronous Energy Technology

INASA-CP'2154t p 77 N80-33465

Ninth NASTRAN Users' Colloquium

[NASA-CP-2151 I p 129 N80-33782

First Scientific Working Group Meeting Of Airborne

Doppler Lidar Wind Velocity Measurement Program

t NASA-CP-2161 I p 162 N81-10697

Fifth Annual Flight Mechemcs/Estimalion Theory

Symposium

INASA-CP-21521 p 64 N81-11070

Propulsion Controls, 1979 --- air breathing engine

control

{NASA-CP-21371 p 47 N81-12090

Impact for lhe 80's: Proceedings of a Conference on

Selected Technology for Business and Industry

[NASA-CP-21491 p 212 N81-12978

The 1 tlh Space Simulation Conference

i NASA-CP-2150 ] p99 N81-14138

Proceedings: Fourth Annual Workshop on

Meteorological and Environmental Inputs to Aviation

systems

INASA-CP-2139] p 162 N81-14558

Numerical grid generation techniques ---conlerence

INASA CP-2166] p 182 N81-14690

Space plasma physics active experiments

INASA-CP-21651 p 212 N81-14944

Solar Power Satellite Microwave Transmission and

Reception

INASACP-21411 p 145 N61 16533

Space Photovo_taic Research and Technology 1980

High Efficiency, Radiation Damage and B_anket

Technology

I NASA-CP 21691 p 145 N8t-17531

Supersonic Cruise Research 1979, part 1

[NASA-CpI2108-PT-1 [ p 3 N81-17981

A-30
SUBJECT INDEX CONFERENCES

Supersonic Cruise Research 1979, part 2 --- airframe

structures and materials, systems integration, economic

analysis

[NASA-CP-2109-PT-2] p 3 N81-18005

Advanced aerodynamics and active controls Selected

NASA research

[NASA-CP-2172] p 3 N81-19001

The 1980 Aircraft Safety and Operating Problems, part

1

[NASA-CP-2170-PT-1 } p 29 N81-19035

The 1980 Aircraft Safety and Operating Problems, part

2

[NASA-CP-2170-PT-2} p 29 N81-19056

The 1980 Large space systems technology. Volume

2: Base technology

[NASA-CP-2168-VOL-2] p 66 N8t-19196

Microwave remote sensing of snowpack properties

[NASA-CP-2153J p 139 N81-19511

VAS Demonstration Sounding Workshop: The

Proceedings of a satellite sounding workshop

[NASA-CP-2157J p 163 N81-19709

Western Regional Remote Sensing Conference

Proceedings, 1979

[NASA.CP.2148] p 139 N81-2144G

The 1980 Goddard Space Flight Center Battery

Workshop

[NASA-CP*2177} p 145 N81-21493

Joint University Program for Air Transportation

Research, 1980

[NASA-CP-2176] p 3 N81-21999

The 15th Aerospace Mechanisms Symposium

[NASA-CP-2181 } p 130 N81-22388

NASA Metrology and Calibration, 1980

[NASA-CP-2174J p 115 N81-23432

Fundamental heat transfer research for gas turbine

engines

{NASA-CP-2178} p 48 N81-24063

The Universe at Ultraviolet Wavelengths: The first two

years of International Ultraviolet Explorer

[NASA-CP-2171 j p 203 N81-25893

Structural dynamics and control of large space structures

--- conference

[NASA-CP-2187} p 66 N81-26166

Capacitor Technologies, Applications and Reliability

[NASA-CP-2186] p 102 N81-26372

Proceedings of the 12th Annual Precise Time and Time

Interval (PTTI) Applications and Planning Meeting

I NASA-CP-21751 p 117 N81-27467

Automated decision making and problem solving

Volume 2: Conference presentations

INASA-CP-2180-VOL-21 p 184 N81-29902

High Reynolds number research - 1980

[NASA-CP-2183] p 18 N81-31130

Aircraft Engine Diagnostics

|NASA-CP-2190] p 48 N81o31196

Oceanic Lidar

[NASA-CP-2194] p 168 N81-31801

Field Study for Remote Sensing: An instructor's

manual

|NASA-CP-2155] p 136 N8t-32564

Numerica_ Boundary Condition Procedures

[NASA-CP-2201 ] p 182 N81-33856

Multigrid Methods

[NASA-CP-22021 p 182 N8t-33879

Sixth Annual Flight Mechanics/Estimation Theory

Symposium

{ NASA-CP-22051 p 62 N82-t0064

Ozone Trend Detectability

[NASA-CP-21891 p 153 N82-10624

Chesapeake Bay Plume Study: Superflux 1980

{NASA-CP-21881 p 168 N82-10661

Spacecraft Dynamics as Relaled to Laboratory

Experiments in Space --- conference

[NASA-CP-21991 p 72 N82-12109

Guidelines for line-oriented fright training, volume 2

{NASA-CP-2184-VOL-21 p 30 N82-13123

Spacecraft Charging Technology, 1980

{NASA-CP-2182] p 72 N82-t4213

Ruggedized minicomputer hardware and software

topics, 1981 Proceedings of the 4th ROLM MIL-SPEC

Computer User's Group Conference

[ NASA-CP-2206 J p 180 N82-14829

Technical communication: Perspectives for the eighties,

part t Proceedings of the technical communications

sessions at the 32nd Annual Meeting of the Conference

on College Composition and Commumcatlon

[NASA-CP-2203-PT-1 I p 197 N82-14960

Office of Space Terrestrial Applications

(OSTA)/Applications Data Service (ADS) data systems

standards

INASA-CP-21961 p 65 N82-15095

The Third International Cloud Condensation Nuclei

Workshop --- conference

INASA-CP-22121 p 115 N82-15383

Optical Information Processing for Aerospace

Applications

I NASA-CP-2207 J p f 94 N82-15894

Technical communication Perspectives for the Eighties,

part 2

[NASA-CP-2203-PT-21 p 197 N82-15986

Variations of the Solar Constant --- conference

[NASA-CP-2191 I p 209 N82-17014

Large space systems technology, 1981 ---

conferences

{NASA-CP-2215-PT-1 I p 66 N82-18275

Space Laser Power Transmission System Studies ---

conferences

{NASA-CP-2214] p 117 N82-18578

Cryogenic Technology, part 1 --- conference

proceedings: cryogenic wind tunnel design and

instrumentation

[NASA-CP-2122-PT-1 } p 99 N82-20357

Cryogenic Technology, part 2 --- conference

proceedings; cryogenic wind tunneI design and

instrumentation

{ NASA-CP-2 t22-PT-21 p99 N82-20358

The 1981 Goddard Space Flight Center Battery

Workshop

[NASA-CP-2217] p 102 N82-20402

Space power subsystem automation technology

|NASA-CP-2213] p 77 N82-21254

Western Regional Remote Sensing Conference

Proceedings, 1981

{E82-10104] p 141 N82-22546

Helicopter Handling Qualities

{NASA-CP-2219] p 30 N82-23208

Meteorological satellites: Past, present, and future

INASA-CP-2227] p 164 N82-24781

Production of Reliable P_ight Crucial Software: Validation

Methods Research for Fault Tolerant Avionics and Control

Systems Sub-Working Group Meeting

INASA-CP-2222] p 179 N82-24845

Wind-Tunnel/Flight Correlation, 1981

[ NASA-CP-2225 ] p 19 N82-25196

Vibrational-Rotational Spectroscopy for Planetary

Atmospheres, volume 2

[NASA-CP-2223-VOL-21 p 207 N82-26134

Float Zone Workshop

[NASA-CP-22261 p 62 N82-26330

Compufer Science Research at Langley

[NASA-CP-22361 p 176 N82-26996

Abstracts of papers presented at the Eleventh

International Laser Radar Conference

[NASA-CP-22281 p 115 N82-27706

Earth Radiation Science Seminars

I NASA-CP-22391 p 210 N82-33320

Flight effects of fan noise

(NASA-CP-22421 p 189 N83-10883

Advanced Materials Techno}ogy

[NASA-CP-2251 I p 79 N83-12147

Advanced Automation for Space Missions

[NASA-CP-22551 p 76 N83-15348

Space Photovoltaic Research and Technology 1982:

High Efficiency. Radiahon Damage, and Blanket

Technology

INASA-CP-22561 p 146 N83-f5806

Human Factors Considerations in System Design

INASA-CP-2246] p 173 N83-18238

NASA Administrative Data Base Management

Systems

INASA-CP-22541 p 197 N83-18559

Cryogenic Wind Tunnel Models Design and

Fabrication

[ NASA-CP-2262 ! p 59 N83-18748

Large Horizontal Axis Wind Turbines

INASA-CP-22301 p 146 N83-1923t

Advanced Power Transmission Technology

1NASA-CP-22101 p 123 N83-20119

Tire Modeling

INASA-CP-2264 I p 131 N83-21391

Eastern Regional Remote Sensing Applications

Conference

IE83*10201 I p 141 N83-21419

Structural Dynamics and Control of Large Space

Structures, 1982

! NASA-CP-2266 J p 67 N83-22256

Aviation Gasolines and Future Alternatives

I NASA-CP-2267 ] p 97 N83-22442

The 1st Symposium on Chemical Evolution and the

Origin and Evolution of Life

I NASA-CP-2276 ] p 79 N83-24556

The 171h Aerospace Mechanisms Symposium

I NASA-CP-2273 I p 131 N83-24881

Proceedings of the National Conference on Energy

Resource Management Volume t Techniques,

Procedures and Dala Bases

[E83-10335j p 141 N83-26155

Proceedings ot the National Conference on Energy

Resource Management Votume 2: Applications

lEa3 10336] p 142 N83-26176

Large Space Antenna Systems Technology, part 1

[NASA-CP-2269-PT-1 i p 67 N83-26853

Large Space Antenna Systems Technology, part 2

INASA-CP-2269-PT-2] p 67 N83-26879

Large Deployable Reflector Science and Technology

Workshop. Volume 2: Scientific RationaleandTechnology

Requirements

[NASA-CP-2275-VOL-2J p 202 N83-27939

The Multispectraf Imaging Science Working Group.

Volume 3: Appendices

[E83-10351] p 142 N83-28506

Combustion Fundamentals Research

{NASA-CP-22681 p 50 N83-29208

Controlled Ecological Life Support System. First

Principal Investigators Meeting

[NASA-CP-2247] p 174 N83-30016

NASA/MSFC FY-83 Atmospheric Processes Research

Review

[NASA-CP-2281J p 165 N83-33494

Restructurable Controls

[NASA-CP-2277] p 57 N83-33896

Failure Analysis and Mechanisms of Failure of Fibrous

Composite Structures

[NASA-CP-2278] p 82 N83-33957

Nonlinear Constitutive Relations for High Temperature

Applications

{NASA-CP-2271] p 132 N83-34351

Aircraft Electric Secondary Power

[NASA-CP-22821 p 50 N84-10055

Shuttle Performance: Lessons Learned, part 1

[NASA-CP-2283-PT-1 J p 69 N84-10115

Shuttle Performance: Lessons Learned, part 2

INASA-CP-2283-PT-2J p 69 N84-10144

Joint University Program for Air Transportation

Research, 1982

[ NASA-CP-2285] p 4 N84-11099

The Regulatory Functions of Calcium and the Potential

Role of Calcium in Mediating Gravitational Responses in

Cells and Tissues

[NASA-CP-22861 p 169 N84-11720

Controls, Displays, and Information Transfer for General

Aviation IFR Operations

[NASA-CP-2279] p 4 N84-12029

Integrated Flywheel Technology, 1983

[NASA-CP-22°JOI p 77 N84-12228

Solar Wind Five

[NASA-CP-2280j p 209 N84-13067

Refrigeration for Cryogenic Sensors

I NASA-CP-22871 p 99 N84-I5327

Eleventh NASTRAN User's Colloquium

[NASA-CP-2284] p 132 N84-15590

STEP Experiment Requirements

[NASA-CP-2294 ] p 67 N84-17211

Spaceborne Gravity Gradiometers

{NASA-CP-2305] p 136 N84-18716

NASA Space Biology Program EK:Jhth annual

symposium's program and abstracts

[NASA-CP 22991 p 169 N84-18.829

CYBER 200 Applications Seminar

[NASA-CP-22951 p 179 N84-20208

Combustion Fundamentals Research

[NASA-CP-23091 p 51 N84-20525

NASA Administrative Data Base Management Systems,

1983

I NASA-CP-2304 } p 198 N84-2t403

Computer-Aided Geometry Modeling

I NASA-CP-22721 p 177 N84-22179

IPAD 2: Advances in Distributed Data Base Management

for CAD/CAM

I NASA-CP-2301 ] p 180 N84-22299

Optical Informal=on Processing for Aerospace

Applications 2

I NASA-CP_2302 J p 194 N84-22402

Assessment of Alternative Aircraft Fuels

I NASA-CP-23071 p 51 N84-23630

Tribology in the 80's Volume 2: Sessions 5 - 8

I NASA-CP-2300-VOL-21 p 124 N84-25047

Advanced aerodynamics Selected NASA research

[ NASA-CP-2208 ] p 4 N84-27660

KC-135 Winglet Program Review

I NASA-CP-2211 I p 24 N84-27686

Get away special experimenter's symposium

INASA-CP-23241 p 63 N84-27758

Proceedings of the Large Deployable Reflector Science

and Technology Workshop Volume 1: Executive

Summary

[NASA-CP-2275-VOL-1 I p 202 N84-28709

Space Photovoltaic Research and Technology 1983

High Efficiency, Radtation Damage, and Blanket

Technology

I NASA-CP-23141 p 146 N84-29307

ACEE Composile Structures Technology: Review of

selected NASA research On composite materials and

structures

I NASA CP 2321 I p 83 N84-29969

A-31
CONFIDENCE SUBJECT INDEX

Geodynam_cs

{NASA-CP-23251 p 137 N84-30475

Nonlinear Struclural Analysis

{NASA-CP-2297} p 133 N84-31688

Large Deployable Reflector Science and Technology

Workshop Volume 3: Systems and Technology

Assessment

l NASA-CP-2275-VOL-31 p 202 N84-32318

Twelfth NASTRAN Users' Colloquium

{NASA-CP-23281 p 133 N84-32864

Proceedings o1 a Workshop on Polar Stratospheric

Clouds: Their Role in Atmospheric Processes

INASA-CP-2318} p 154 N84-32952

NASA Administrative Data Base Management Systems,

1984

I NASA-CP-2323 i p 198 N84-33266

Solar Terrestrial Physics: Present and Future

I NASA-RP-t 1201 p 200 N84-34332

Planetary Data Workshop, part 1

I NASA-CP-2343-PT-t p p 208 N84-34366

Planelar/Data Workshop, part 2

l NASA-CP-2343-PT-2J p 208 N84-34376

Fundamentals of Alloy Sohdification Applied to Industrial

Processes

{ NASA-CP-2337t p 90 N84-34589

NASA/MSFC FY 84 Atmospheric Processes Research

Review

{NASA-CP-2329 i p 166 N84-34829

Peripheral Vision Horizon Display (PVHD)

{ NASA-CP-2306 ] p 40 N85-10044

Second Symposium on Space Industrialization --- space

commercialization

{NASA-CP-2313] p 63 N85-11011

The Multispectral Imaging Science Working Group

Volume 2: Working group reporls

IE85-I00021 p 142 N85-11405

Uranus and Neptune

{ NASA-CP-2330} p 208 N85-11927

Wind Tunnel Wall Interference Assessment and

Correction, 1983

[NASA-CP-23191 p 25 N85-12011

Tough Composite Materials

[ NASA-CP-23341 p83 N85-12941

An Assessment of Inlegraled Flywheel System

Technology

I NASA-CP-23461 p 78 N85-13850

Space Power

_NASA-CP-2352} p 78 N85-13880

Rotordynamic Instabdity Problems in High-Performance

Turbomachmery

INASA-CP-2338] p 124 N85-14116

Assessment of Techniques for Measuring Tropospheric

H sub x O sub y

i NASA-CP-23321 p 155 N85-14336

Twentieth Annual Conference on Manual Control,

volume 1

INASA-CP-2341-VOL-t I p 174 N85-14487

Twentieth Annual Conference on Manual Control,

volume 2

JNASA-CP-234t-VOL-2} p 174 N85-14535

Technical Workshop Advanced Helicopter Cockpit

Design

[NASA-CP-2351 ] p 31 N85-14806

Local Interstellar Medium. International Astronomical

Union Colloquium No 81

[NASA-CP-2345) p 204 N85-15539

International Aerospace and Ground Conference on

Lightning and Static Electricity, 1984 technical papers

Supplement

[NASA-CP-2356] p 166 N85-16343

Space Shuffle Technical Conference, part 2

[NASA-CP-2342-PT-2} p 63 N85-16937

DTV Propulsion Issues

{NASA-CP-2347} p 67 N85-16989

The Ongin of Nonradiative Heating/Momentum in Hot

Stars

{NASA-CP-2358] p 200 N85-17755

Airborne Astronomy Symposium A symposium

commemorating the tenth anniversary of operations of the

Kuiper Airborne Observatory

[NASA-CP-2353} p 202 N85-17848

Proceedings of the Workshop on Improvements to

Photometry

{NASA-CP-2350} p 203 N85-17892

Flight Training Technology for Regional/Commuter

Airline Operations: Regional Aidine Association/NASA

Workshop Proceedings

{NASA-CP-2348} p 30 N85-18009

Applications of Tethers in Space, volume 1

[NASA-CP-2364} p 125 N85-20339

Applications of Tethers in Space, volume 2

[NASA-CP-2365} p 125 N85-20361

LANDSAT-4 Scnence Characterization Early Results

Volume 2, part 1 Thematic Mapper (TM)

{E85-10068J p 143 N85-20508

Orbital Debris

l NASA-CP-23601 p 63 N85-21188

Spacecraft Environmental Interactions TechnolOgy,

1983

{NASA-CP'23591 p 75 N85-22470

LANDSAT-4 Science Charactenzation Early Results.

Volume 4: Applications --- agriculture, soils land use,

geology, hydrology, wetlands, water quality, biomass

identification, and snow mapping

[E85-I0070] p 143 N85-23186

Remote Sensing of Snow and Evapotranspiration

[NASA-CP-2363J p 143 N85-23223

Large Space Antenna Systems Technology, 1984

[NASA-CP-2368-PT-1] p 67 N85-23813

Large Space Antenna Systems Technology, 1984

[NASA-CP-2368-PT-2} p 68 N85-23840

Thirteenth NASTRAN Users' Colloquium

[NASA-CP-23731 p 134 N85-25863

NASA Space Biology Program: 9th Annual

Symposium

[NASA-CP-2336J p 169 N85-2e054

Advanced High Pressure O2/H2 Technology

[NASA-CP-2372} p 78 N85-26862

Structural Integrity and Durability of Reusable Space

Propulsion Systems

INASA-CP-2381 I p 78 N85-27941

Peer Review of a Formal Verilication/Design Proof

Methodology

[NASA-CP-23771 p 179 N85-28609

Controlled Ecological Lile Support System Life Support

Systems in Space Travel

{NASA-CP-2378 J p 174 N85-29531

The 1984 Goddard Space Flight Center Battery

Workshop

[NASA-CP-2382} p 103 N85-31371

Nonlinear Constitutive Relations for High Temperature

Application, 1984

NASA-CP-23891 p 134 N85-31530

Ninteenth Aerospace Mechanisms Symposium

NASA-CP-2371 _ p 134 N85-33512

Ninteenth International Cosmic Ray Conference

Conference program and author index

NASA-CP-2376J p 210 N85-33901

Ninteenth International Cosmic Ray Conference. OG

sessions, volume 1

NASA-CP-2376-VOL-f I p 210 N85-33902

Ninteenth International Cosmic Ray Conference. OG

sessions, volume 2

NASA-CP-2376-VOL-2} p 210 N85-34006

Ninteenth International Cosmic Ray Conference SH

sessions, volume 4

NASA-CP-2376-VOL-4 ] p 210 N85-34729

Nineteenth International Cosmic Ray Conference. OG

sessions, volume 3

NASA-CP-2376-VOL-31 p 211 N85-34862

Nineteenth International Cosmic Ray Conference. SH

sessions, volume 5

NASA-CP-2376-VOL-51 p 211 N85-34991

Nineteenth International Cosmic Ray Conference. HE

Sessions, volume 6

NASA-CP-2376-VOL-8} p 211 N85-35848

Nineteenth International Cosmic Ray Conference HE

Sessions, volume 7

I NASA-CP-2376-VOL-7 I p 21 t N85-35968

Nineteenth International Cosmic Ray Conference HE

sessions, volume 8

NASA-CP-2376-VOL-8] p 211 N85-36066

Welding, Bonding and Fastening, 1984

[NASA-CP-2387] p 79 N86-11227

Geopotential Research Mission (GRM)

[NASA-CP-2390 ] p 155 N86-12852

Review of spectroscopic parameters for upper

atmosphehc measurements

[NASA-CP-2396] p 192 N86-13064

Solar Terrestrial Observatory Space Station Workshop

Report

{NASA-CP-2411 I p 76 N86-19349

Full-Scale Transport controlled Impact Demonstration

[NASA-CP-2395] p t35 N86-21933

Analylical Ultrasonics in Materials Research and

Testing

{NASA-CP-2383} p 126 N86-22962

Current Scientific Issues in Large Scale Atmospheric

Dynamics

t NASA-CP-24101 p 167 N86-24082

D_gitat Electronic Engine Control (DEEC) Flight

Evaluation in an F- 15 Airplane

{ NASA-CP-2298} p 52 N86-25342

Nineteenth [nternationa_ Cosmic Ray Conference

papers General index, volume 10

{NASA-CP-2376-VOL-t0} p 211 N86-28904

Proceedings of the Second Pilot Climate Data System

Workshop

lNASA-CP-2430 J p 137 N86-29282

The MSFC/UAH Data Management Symposium

{ NASA-CP-20401 p 177 N78-74659

Flight Mechanics/Estimation Theory Symposium

I NASA-CP-20021 p 61 N78-76855

CONFIDENCE

A methodology for airplane parameter estimation and

confidence interval determination in nonlinear estimation

problems

I NASA-RP-1153] p 58 N86-22579

CONFIGURATION MANAGEMENT

Space Station Software Issues

I NASA-CP-2361 } p 179 N85-20689

CONFORMAL MAPPING

Numerical grid generation techniques --conference

[NASA-CP-2166J p 182 N81-14690

CONICAL BODIES

Experimental and predicted heating distributions for

biconics at incidence in air at Mach 10

[NASA-TP-23341 p 112 N85-12313

CONICAL FLOW

Pressure and force data for a flat wing and a warped

conical wing having a shockless recompression at Mach

1 62

[NASA-TP-17591 p 17 N81-22016

Performance of a tandem-rotor/tandem-stator

conical-flow compressor designed for a pressure ratio of

3

{NASA-TP-20341 p 20 N83-11058

CONICAL SHELLS

Effect of end-ring stiffness on buckling of

pressure-loaded stiffened conical shells

[NASA-TP*f0791 p 127 N78-12475

CONSISTENCY

Temporal and spatial inconsistencies of time-split

finite-difference schemes

[NASA-TP-17901 p 182 N81-22754

CONSTANTS

The generalized Euler-Mascheront constants

I NASA-TP-2264 J p 185 N84-15880

An integral representation ol the generalized

Euler-Mascheroni constants

{NASA-TP-24561 p 177 N85-23305

CONSTITUTIVE EQUATIONS

Materials constitutive models for nonlinear analysis of

thermally cycled structures

[NASA-TP-2055] p 131 N83-12449

Nonldnear Constitutive Relations for High Temperature

Application, 1984

{NASA-CP-2369] p 134 N85-31530

CONSTRAINTS

Economic evaluation of flying-qualities design criteria for

a transport configured with relaxed static stability

INASA-TP-17601 p 56 N81-13968

Nonhnear ophmization with linear constraints using a

projection method

[ NASA-TP-20861 p 184 N83-10876

CONSTRUCTION MATERIALS

Vibration characteristics of walls and a plate glass

window representative of those of a wood-frame house

INASA-TP-14471 p 128 N79-24372

CONSUMABLES (SPACECREW SUPPLIES)

Food Service and Nutrition for the Space Station

[NASA-CP-23701 p 174 N85-24733

CONTACT POTENTIALS

Evaluation of high-contact-rat_o spur gears with profile

modification

{NASA-TP-t458J p 120 N79-31604

CONTACT RESISTANCE

Elastohydrodynamic lubncation of elliptical contacts for

matenals of low elastic modulus 2: Starved

conjunction

[NASA-TP-1273} p 119 N78-28458

CONTAMINANTS

Pollutant emissions from flat-flame burners at high

pressures

I NASA-TP-1673J p 85 N80-25392

Stochastic differential equations and turbulent

dispersion

[NASA-RP-1103} p 110 N83-22546

Experimental design of an interlaboralory sludy for trace

metat analysis of liquid fluids --- for aerospace vehicles

INASA-TP-2148} p 85 N83-24575

CONTAMINATION

Ozone Contamination in Aircraft Cabins

[NASA-CP-2066i p 29 N79-2t021

Mechanical impact tests of materials in oxygen effects

of contamination --- Teflon, stainless steel and

aluminum

INASA-TP-1571 j p 97 N80-21551

Thirteenth Space Simulation Conference The Payload:

Testing for Success

I NASA-CP-23401 p 74 N84-34468

CONTINUOUS NOISE

LANDSAT-4 and LANDSAT-5 mult_spectral scanner

coherent noise characterization and removal

[NASA-TP-2595] p 143 N86-31945

A-32
SUBJECT INDEX CONVERGENT-DIVERGENT NOZZLES

CONTINUUM FLOW

Determination of the

hypersonic-continuum/rarefied-flow drag coefficient of the

Viking lander capsule 1 aeroshell from flight data

[NASA-TP-1793] p 3 N81-14961

CONTOURS

A closed-form SOlution for noise contours

[NASA-TP-1432] p 187 N80-11869

Analytic investigation of effect of end-wall contouring

on stalor performance

INASA-TP-1943] p 19 N82-14051

Analytical and experimental investigation of stator

and'wall contouring in a small axial-flow turbine 1: Stator

performance

INASA-TP-2023] p 49 N83-11125

Perfect bell nozzle parametric and optimization curves

[NASA.RP.1104] p 77 N83-24549

Analytical and experimental investigation of stator

endwall countouring in a small axial-flow turbine

[NASA-TP-2309] p 51 N84-32388

CONTRACT MANAGEMENT

Managing NASA in the Apollo era

[NASA-SP-4102] p 196 N83-18551

CONTRAROTATING PROPELLERS

Experimental study of the effects of installation on

singleend counter-rotation propeller noise

[NASA-TP-2541] p 191 N86.26162

CONTROL CONFIGURED VEHICLES

Analytical study of ride smoothing benefits of control

system configurations optimized for pilot handling

qualities

[NASA-TP-1148] p 53 N78-18076

CONTROL DATA (COMPUTERS)

An alternating direction implicit method for the Control

Data STAR-100 vector computer

[NASA-TP-1282] p 182 N78-31836

Space Shuttle separate-surface control-system study

[NASA-TP-2340] p 58 N84-28801

CONTROL EQUIPMENT

Evaluation of a laboratory test model annular momentum

control device

[NASA-TP-1142] p 98 N78-18252

The 171h Aerospace Mechanisms Symposium

[NASA-CP-2273] p 131 N83.2488t

CONTROL MOMENT GYROSCOPES

Decoupled and linear quadratic regulator control of a

large, flexible space antenna with an observer in the control

loop

[NASA-TP-2484] p 75 N86-16250

Effects of model error on control of large flexible space

antenna with comparisons of decoupled and linear

quadratic regulator control procedures

[NASA-TP-2604] p 75 N86-30801

CONTROL SIMULATION

Results from flight and simulator studies of a Mech 3

cruise longitudinal eutopiiot

[NASA-TP-1180] p 53 N78-21160

Fixed-base simulation study of decoupiod longitudinal

controls during approach and landing of a medium jet

transport in the presence of wind shear

[NASA-TP-1519] p 55 N79-33218

Analysis of space shuttle ort_ter entry dynamics from

Mach 10 to Mech 2.5 with the November 1976 flight control

system

[NASA-TP-1667] p 71 N80-29417

An application of mulfivariable design techniques to the

control of the national transonic facility

[NASA-TP-1887] p 181 N81-29840

A general aviation simulator evaluation of a

rate-enhanced instrument landing system display

[NASA-TP-1960] p 39 N82-14085

CONTROL STABILITY

Entry dynamics of space shuttle orbiter with longitudinal

stability and control uncertainties at supersonic end

hypersonic speeds

[NASA-TP-1084] p 70 N77-33259

Effect of nozzle and vertical-tail variables on the

performance of a 3-surface F-15 model at transonic Mach

numbers --- Langley 16 foot transonic tunnel

[NASA-TP-2043] p 20 N82-32320

Wind-tunnel investigation of a full-scale

canard-configured general aviation airplane

[NASA-TP-2382J p 25 N85-19925

A method to stabilize linear systems using sigenvsiue

gradient information

[NASA-TP-2479] p 181 N86-13946

Low-speed stability and control characteristics of a

transport model with aft-fuselage-mounted advanced

turboprops

{NASA-TP-2535J p 59 N86-22580

CONTROL SURFACES

Water-tunnel and analytical investigation of the effect

of strake design variables on strake vortex breakdown

characteristics

[NASA-TP-1676] p t5 N80-28304

Force and moment, flow-visualization, and

boundary-layer tests on a shuttle orbiter model at Mach

6

(NASA-TP-1952] p 18 N82-'13106

Wind-tunnel investigation of a full-scale

canard-configured general aviation airplane

[NASA-TP-2382] p 25 NS5-19925

Vortex wake alleviation studies with • variable twist

wing

[NASA-TP-2442] p 5 N86o16187

CONTROL SYSTEMS DESIGN

Problems experienced and envisioned for dynamica_

physical systems

{NASA-TP-2508] p 68 N86-11215

Graphical techniques to assist in pointing and control

studies of orbiting spacecraft

[NASA-TP-25751 p 63 N86-21559

Technology for large space systems: A bibliography with

indexes (supplement 14)

[NASA-SP-7046(14)] p 63 N86.28104

Effects of model error on control of large flexible space

antenna with comparisons of decoupled and linear

quadratic regulator control procedures

[NASA-TP-2604] p 75 N86-30801

CONTROL THEORY

ORACLS: A system for linear-quadratic-Gaussian

control taw design

[NASA-TP-1106] p 151 N78-22809

Modal control theory and application to aircraft lateral

handling qualities design

[NASA-TP-t234] p 53 N78-25101

Generation of linear dynamic models from a digital

nonlinear simulation

[NASA-TP-1388] p 2 N79.16796

A method for obtaining practical flutter-suppression

control laws using results of optimal control theory

[NASA-TP-147t | p 128 N79-28614

Application of two design methods for active flutter

suppression and wind-tunnel test results

(NASA-TP-1653] p 129 N80.22737

Realizable optimal control for a remotely piloted research

vehicle --- stability augmentation

[NASA-TP-1654] p 181 N80-25039

Control-systam techniques for improved departure/spin

resistance for fighter aircraft

[NASA-TP-1689] p 2 N80-29244

Propulsion Controls, 1979 --- air breathing engine

control

[NASA-CP-2137] p 47 N81-12090

Large space systems technology, 1980, volume 1

[NASA-CP-2168] p 66 N81-19164

A method for obtaining reduced-order control laws for

high-order systems using optimization techniques

[NASA-TP-1L-76] p 181 N81-30851

Automated Decision Making and Problem Solving.

Volume 1: Executive Summary

[NASA-CP-2f80-VOL-t] p 184 N81-30889

Application of modal control to wing-flufter

suppression

[NASA-TP-1983} p 57 N82-24209

Global differential geometry: An introduction for control

engineers

[NASA-RP-t091J p 176 N82-29904

Rotordynamic instability Problems in High-Pertormance

Turbomachinery

[NASA-CP-2250] p 122 N83-15629

Structural Dynamics and Control of Large Space

Structures, 1982

[NASA-CP-2266] p 67 N83-22256

F100 multivariable control synthesis program Computer

implementation of the FIO0 muttivariable control

algorithm

[NASA-TP-2231 ] p 51 N84-1 t 171

Controls, Displays, and Information Transfer for General

Aviation IFR Operations

[NASA-CP-2279] p 4 N84-12029

Generalization of the subsonic kernel function in the

s-plane, with applications to flutter analysis

INASA-TP-2292] p 23 N84-20480

Space Shuttle separate.surface contrel-system study

[NASA-TP-2340] p 58 N84-28801

Research in Structures and Dynamics, t 984

[NASA-CP-2335J p 134 N85-10377

CONTROL UNITS (COMPUTERS)

Validation Methods Research for Fault-Tolerant Avionics

and Control Systems: Working Group Meeting. 2

[NASA.CP-2130] p 176 N80-23008

CONTROLLABILITY

Effects of control inputs on the estimation of stability

and control parameters of a light airplane

[NASA-TP-1043} p 53 N78-13071

Study of the application of an implicit model-following

flight controller to rift-tan VTOL aircraft

[NASA.TP-1040] p 53 N78-16063

Modal control theory end application to aircraft lateral

handling qualities design

[NASA-TP-1234] p 53 N78-25101

Ground-based and in-flight simulator studies of

low-speed handling characteristics of two supersonic

cruise transport concepts

[NASA-TP-1240] p 32 N78-27111

A comparison of the V/STOL handling qualities of the

VAK-191B with the requirements of AGARD report 577

and MIL-F-83300

[NASA-TP-1494] p 54 N79-27182

Precision controllability of the YF-t 7 airplane

[NASA-TP-t677] p 55 N80-23327

Measurement of the handling characteristics of two light

airplanes

[NASA-TP-1636] p 56 N80-25345

Helicopter Handling Qualities

[NASA-CP-2219] p 30 N82-23208

Ground-based and in.flight simulator studies of flight

characteristics of a twin-fuselage passenger traosporl

airplane during approach and landing

[NASA-TP-2451J p 58 N85-34144

CONTROLLED ATMOSPHERES

Ice crystal growth in a dynamic thermal diffusion

chamber

[NASA-TP-1651 J p 162 N80-23934

Controlled Ecological Life Support System. Life Support

Systems in Space Travel

[NASA-CP-2378] p 174 N85-29531

CONTROLLERS

Realizable optimal control for a remotely piloted research

vehicle --- stability augmentation

[NASA-TP-1654] p 181 N80-25039

Self-tuning regulators for multicyclic control of helicopter

vibration

[NASA.TP.1996] p 57 N82-20188

Regions of attraction and ultimate boundedness for

linear quadratic regulators with nonlinearities

[NASA-TP-2322] p 181 N84-28538

CONVECTION

Forced and natural convection in laminar-jet diffusion

flames --- normal-gravity, inverted-gravity and zero-grevity

flames

(NASA-TP-1841) p 109 N81-24388

Gas turbine ceramic-coaled-vane concept with

convection-cooled porous metal core

[NASA-TP-1942] p 48 N82-14090

Hybrid parturbation/Bubnov-Galerkin technique for

nonlinear thermat analysis

[NASA-TP-21451 p 111 N84-22907

A preliminary study of numerical simulation of

thermosolutal convection of interest to crystal growth

[NASA-TP-2394] p 112 N85-13175

CONVECTIVE FLOW

Convective rainfall estimation from digital GOES-t

infrared data

INASA-RP-1034] p 160 N79-3t885

North Atlantic Deep Water Formalion

{NASA-CP-2367J p 169 N85-26028

Thermosphere Dynamics Workshop, volume 2

[NASA-CP-2389] p 137 N86-29301

CONVECTIVE HEAT TRANSFER

Method for calculating convective heat-transfer

coefficients OVer turbine vane surfaces

[NASA-TP-1134] p 104 N78-17338

Aerothermal analysis of a wing-elevon cove with variable

leakage

[NASA-TP-1703] p 108 N80-32692

CONVERGENCE

A method for modifying two-dimensional adaptive

wind-tunnel walls including analytical and experimental

venfioation

[NASA-TP-2081] p 59 N83-18770

Acceleration of convergence of vector sequences

INASA-TP-21931 p 182 N84-13885

Convergence of Newton's method for a single real

equation

[NASA-TP-2489J p 183 N85-28656

CONVERGENT NOZZLES

Effects of simulated flight on the structure and noise

of underexpanded jets

[NASA-TP-2308] p 189 N84-25422

Static internal performance of a two-dimensional

convergent nozzle with thrust-vectoring capability up to

60 deg

[NASA-TP-239t ] p 25 N85-18951

CONVERGENT-DIVERGENT NOZZLES

Effect of several geometnc parameters on the static

internal performance of three nonaxisymmetric nozzle

concepts

[NASA-TP-1468] p 12 N79-26022

Two-phase choked flow ol cryogenic fluids in

converging-diverging nozzles

INASA-TP-1484] p 107 N79-29468

A-33
CONVERSATION SUBJECT INDEX

TI_ effoct of throat contounng on two-dimensional

converging-diverging nozzles at static conditions

[NASA-TP-1704] p 15 N80-29250

Invesbgabon of convergent-dNergent nozzles applicable

to reduced-power supersonic cruise aircraft

[NASA-TP-1766] p 16 N81-14972

Effects of sidewall geometry on the installed

performance of nonaxisymmetnc convergent-divergent

exhaust nozzles

[NASA-TP-1771] p 16 N81-15976

Aeropropulsfve characteristics of twin nonaxisymmetric

vectoring nozzles installed with forward-swept and

aft-swept wings --- in the Langley 16 Foot Transonic

Tunnel

[NASA-TP-1778] p 16 N81-19019

Experimental end analytical investigation of

esisymmetric supersonic cruise nozzle geometry at Mech

numbers from 060 to I 30

[NASA-TP-19531 p tg N82-14052

Performance cherectenstics of axisymmetric

convergent-divergent exhaust nozzles with longitudinal

slots in the divergent

[NASA-TP-2013] p 19 N82-26231

Aeropropulsive charectanst_cs of Mech numbers up to

2.2 of azisymmetric and nonaxisymmetric nozzles installed

on an F-18 model

[NASA-TP-2044) p 20 N82-30291

Investigation of installation effects of single-engine

convergent-divergent nozzles

[NASA-TP-2078} p 20 N83-11059

Investigation of installation effects on twin-engine

convergent-divergent nozzles

{NASA-TP-2205] p 22 N84-13152

Static internal performance including thrust vectoring

and reversing of two-dimensional convergent-divergent

nozzles

[NASA-TP-2253] p 23 N84-18185

Static investigation of several yaw vectoring concepts

on nonaxisymmetric nozzles

[NASA-TP-24321 p 26 N85-28924

CONVERSATION

Effects of conversation interference on annoyance due

to aircraft noise

[NASA-TP-1712} p 149 N80-29911

CONVOLUTION INTEGRALS

Comparison of data inversion techniques for remotely

sensed wide-angle observations of Earth emitted

radiation

{NASA-TP-t924J p 164 N82-13620

AnalysJs of random signal combinations lor spacecraft

pointing stability

[NASA-TP-22161 p 184 N83-33631

COOLANTS

Influence of coolant tube curvature on film cooling

effectiveness as detected by infrared imagery

[NASA-TP-1546] p 45 N80-110.87

Flightwaight radiantly and actively cooled panel:

Thermal and structural performance

[NASA-TP-2074] p 131 N83-11513

Film-cooling effectiveness with developing coolant flow

through straight and curved tubular passages

[NASA-TP-2062] p 110 N83-12360

Aerodynamic effect of a honeycomb rotor tip shroud

on • SO.8-centimeter-tip-diameter core turbine

[NASA-TP-2112] p 49 N83-17847

COOLING

Aerothermal tests of a heat-pipe-cooled leading edge

at Mech 7 --- hypersonic heat transfer for space shuttle

orbiters

[NASA-TP-1320] p 195 N79-13901

TACT 1: A computer program for the transient thermal

analysis of a cooled turbine blade or vane equipped with

a coolant insert. 2. Programmers manual

[NASA-TP-1391 ] p 106 N79-18288

Influence of coolant tube curvature on film cooling

effectiveness as detected by infrared =magery

{ NASA-TP- 1546 j p 45 N80-11087

Performance of jet- and inner-nng-lubncated 35

millimeter bore ball bearings operating to 2.5 million DN

{NASA-TP-1808} p 122 N81-19458

Preliminary tests of an advanced high-temperature

combustion system

[NASA-TP-22O3] p 50 N83-33893

COOLING FINS

Effect of fin passage length on optimzation of cylinder

head Cooling fins

[NASA-TP-f0541 p 104 N77-32432

COOLING SYSTEMS

Effect of cooling-hole geometry on aerodynamic

performance of a film-cooled turbine vane tested with cold

sir in a two-dimensional cascade

[NASA-TP-1136J p 8 N7B-20080

Simulation model of a single-stage lithium bromide-water

absorption cooling unit

{NASA-TP-12961 p 86 N78-30205

Aerothermai performance of radiative;y and actively

cooled panel at Mech 6.6

[NASA-TP°1595] p 107 N80-13402

COORDINATE TRANSFORMATIONS

Forebody end afterbody solutions of the Navier-Stokes

equations for supersonic flow over blunt bodies in a

generalized orfhogonel coordinate system

[NASA-TP-1075] p 104 N78-18362

Numerical grid generation techniques ---conference

[NASA-CP-2166] p t82 N81-14690

COORDINATES

Application of a numerically generated orthogonal

coordinate system to the solution of inviscid axisymmetric

supersonic flow over blunt bodies

[NASA-TP-1619] p 14 N80-19031

Computer-Aided Geometry Modeling

[NASA-CP-2272] p 177 N84-22179

COPOLYMERS

Ultra-high molecular weight silphenylene-siloxane

polymers

[NASA-TP-2295] p 95 N84-19564

COPPER

Friction and wear of selected metals and alloys in sliding

contact with AISt 440 C stainless steel in liquid methane

and in liquid natural gas

[NASA-TP-1150I p 119 N78-20512

Wear of single-crystal silicon carbide in contact with

various metals in vacuum

I NASA-TP-t 198 ] p 92 N78-21295

Morphology of gold and copper ion-plated coatings

INASA-TP-1262] p 86 N78-26199

Effect of tow-stiffness closeout overwrap on rocket

thrust-chamber life

[NASA-TP-1456] p 77 N79-23132

Scanning-electron-microscope study of

normal-impingement erosion of ductile metals

I NASA-TP- 16091 p87 N80-16141

Secondary electron emission characteristics of

ion-textured copper and high-purity isotropic graphite

surfaces

{NASA-TP-2342] p 95 N84-28989

Textured carbon on copper: A novel surface with

extremely idw secondary electron emission

characteristics

[NASA-TP-2543J p 96 N86-18394

COPPER ALLOYS

Fnction and wear of selected metals and alloys in sliding

contact with AISI 440 C stainless steel in liquid methane

and in liquid natural gas

[NASA-TP-1150] p 119 N78-20512

Rote of stloying elements in adhesive transfer and friction

of copper-base alloys

[NASA-TP-1256J p 86 N78-26198

CORONAGRAPHS

The PinholelOcculter Facility

[NASA-TP-2168] p 209 N83-25646

CORRELATION

Analysis of gap heating due to stepped tiles in the shuttle

thermal protection system

[NASA-TP-22091 p 74 N83-31713

Airborne measurements of launch vehicle effluent of

STS-2 launch on November 12, 1981 at Cape Canaveral,

Florida

(NASA-TP-22601 p 150 N84-18764

CORRELATION COEFFICIENTS

Regression analysis of traction characteristics of traction

fluids

[NASA-TP-2154] p 123 N83-24862

CORROSION

Influence of corrosive solutions on microherdness and

chemistry of magnesium oxide /001/surfaces

[NASA-TP-2040] p 122 N82-31691

An electrochemical method for determining hydrogen

concentrations in metals and some applications

[ NASA-TP-2113 ] p 88 N83-16491

Friction and wear of iron in sulfuric acid

[NASA-TP-2289] p 99 N84-217t6

Friction and wear of nickel in sulfuric acid

[NASA-TP-2290J p 89 N84-21721

CORROSION PREVENTION

Low toxic corrosion inhibitors for aluminum in fresh

water

[NASA-TP-1279] p 86 N78-28226

Galvanic coupling between D6AC steel, 6061.T6

aluminum, Inconel 718 and graphite-epoxy composite

material: Corrosion occurrence and prevention

[NASA-TP-2236J p 89 N84-13263

CORROSION RESISTANCE

Characterization of wear debris generated in accelerated

rolling-element fatigue tests

[NASA-TP-1203] p 119 N78-21470

Erosion/corrosion of turbine airfoit materials in the

high-velocity effluent of e pressurized fluidized coal

combustor

[NASA-TP-1274] p 86 N78-28225

Mechanical properties and oxidation and corrosion

resistance of reduced-chromium 304 stainless steel

alloys

[NASA-TP-1587] p 87 N80-11188

Effect of carbide distribution on roiling-element fatigue

life of AMS 5749

[NASA-TP-2189] p 123 N83-33166

The variation of corrosion potential with time for coated

metal surfaces

[NASA-TP-2636J p 91 N86-30837

CORROSION TESTS

Friction and wear of iron in corrosive metal

I NASA-TP-1985] p 88 N82-20291

Effects of alloy composition on cyclic flame hot-corrosion

attack of cast nickekbase superalloys at 900 deg C

{NASA-TP-2338] p 89 N84-26783

An electrochemical study of the corrosion behavior of

primer coated 2219-T87 aluminum

[NASA-TP-2459] p 90 N85-22662

CORRUGATED PLATES

Aerodynamic heating on the corrugated surface of S

10.2 deg half-angle blunted cone at Mech 6.7

[NASA-TP-f928J p 109 N82-13383

Pressure and heating-rate distributions on a corrugated

surface in a supersonic turbulent boundary layer

INASA-TP-1024] p 111 N84-10504

Fabrication and evaluation of superptasticatty

formed/weld-brazed corrugated compression panels with

beaded webs

INASA-TP-2512] p 90 N86-13406

CORRUGATED SHELLS

Design detail verification tests for a lightly loaded

open-corrugation graphite-epoxy cylinder

INASA-TP-1981] p 130 N82-20567

Buckling test of a 3-meter-diameter corrugated

graphite-epoxy ring-stiffened cytinder

[NASA-TP-2032] p 131 N82-28665

CORRUGATING

Structural efficiency studms of corrugated compression

panels with curved caps and beaded webs

[NASA-TP-2272] p 132 N84-18675

COSMIC DUST

Interrelationships among Circumslellar, Interstellar and

Interplanetary Dust

[NASA-CP-2403J p 201 N86-23493

COSMIC RAY SHOWERS

Nineteenth International Cosmic Ray Conference. HE

Sessions, volume 7

[NASA-CP-2376-VOL-7] p 211 N85-35968

COSMIC RAYS

The structure and content of the galaxy and galactic

gamma rays

NASA-CP-002J p 199 N77-20977

A T-matrix theory of galactic heavy-ion fragmentation

NASA-TP-2363] p 193 N85-17690

Ninteenth International Cosm¢c Ray Conference.

Conference program end author index

NASA-CP-2376] p 210 N85-33901

Nintaenth International Cosmic Ray Conference OG

sessions, volume 1

NASA-CP-2376-VOL-1] p 210 N85-33gO2

Ninteenth International Cosmic Ray Conference. OG

sessions, volume 2

NASA-CP-2376-VOL-2] p 210 N85-34006

Ninteenth International Cosmic Ray Conference. SH

sessions, volume 4

NASA-CP-2376-VOL-4J p 210 N85-34729

Nineteenth International Cosmic Ray Conference. OG

sessions, volume 3

NASA-CP-2376-VOL-3] p 211 N85-34862

Nineteenth International Cosmic Ray Conference. SH

sessions, volume 5

NASA-CP-2376-VOL-51 p 211 N85-34991

Nineteenth International Cosmic Ray Conference HE

Sessions, volume 6

NASA-CP-2376-VOL.61 p 211 N85-35848

Nineteenth International Cosmic Ray Conference HE

Sessions, volume 7

NASA-CP-2376-VOL-71 p 211 N85-35968

Nineteenth international Cosmic Ray Conference HE

sessions, volume 8

(NASA-CP-2376-VOL-S] p 211 N85-36066

A stochastic model for paFticle impingements on orbiting

spacecraft

[NASA-TP-255OJ p 184 N86-19095

Nineteenth international Cosmic Ray Conference

papers. General index, volume 10

I NASA-CP-2376-VOL-t01 p 211 N86-28904

Nineteenth International Cosmic Ray Conference

Conference papers: Invited rapporfeur, highlight,

miscellaneous, volume 9

[NASA-CP-2376-VOL-9J p 211 N86-31483

A-34
SUBJECT INDEX CRYOGENIC WIND TUNNELS

COSMOLOGY

Scientific research with the space Telescope:

International Astronomical Union Colloquium no. 54 ---

conferences

[NASA-CP-2111 ] p 200 N80-22130

Gamma Ray Astrophysics: New insight into the

universe

I NASA-SP-453} p 204 N82-21118

Local Interstellar Medium. International Astronomical

Union Colloquium No 81

[NASA-CP-2345] p 204 N85-15539

COST ANALYSIS

Two-impulse reorientation of asymmetric spacecraft

[NASA-TP-1554] p 64 N80-13135

Use of constrained optimization in the conceptual design

of a medium-range subsonic transport

[NASA-TP-1762] p 35 N81-16039

Solar power satellite system sizing tradeoffs

[NASA-TP-1804] p 145 N81-18493

Analysis of costs of gallium arsenide and silicon solar

arrays for space power applications

[NASA-TP-f811} p 77 N61-20173

Vehicle concepts and technology requirements for

buoyant heavy-lift systems

[NASA-TP-192f ] p 35 N81-31185

Applications systems verification and transfer project.

Volume 7: Cost/benefit analysis for the ASVT on

operational applications of satellite snow-cover

observations

[NASA-TP-t828J p 141 N82-20623

COST EFFECTIVENESS

Comparative analyses of space-to-space central power

stations

{NASA-TP-1955} p 66 N82-14202

COST REDUCTION

Algorithm for fixed-range optimal trajectories

[NASA-TP-f565] p 30 N80-26329

An algorithm for minimum-cost sat-point ordering in a

cryogenic wind tunnel

[NASA-TP-1923] p 59 N82-11090

COULOMB COLLISIONS

Electromagnetic dissociation effects in galactic

heavy-ion fragmentation

[NASA-TP-2527] p 211 N86-21492

COUPLING

Middle atmosphere electrodynamics: Report of the

workshop on the Role of the Electrodynamics of the Middle

Atmosphere on Solar Terrestrial Coupling

[NASA-CP-2090] p 152 N79-25608

Radiating dipole model of interference induced in

spacecraft circuitry by surface discharges

[NASA-TP-2240} p 74 N84-16247

A formulation of rotor-airframe coupling for design

analysis of vibrations of helicopter airframes

[NASA-RP-10891 p 133 N84-33832

COWLINGS

The high-speed frontier Case histories of four NACA

programs, 1920 - 1950

{NASA-SP-445] p 3 N81-15969

CRACK INITIATION

A cracked orthotropic sheet stiffened by a semi-infinite

orthotropic sheet

[NASA-TP-2455] p 134 N85-32339

CRACK PROPAGATION

Advances in engineering science, volume f

[NASA-CP-2001-VOL.t I p 98 N77-10230

Fracture temperature and flaw growth in nifronic 40 at

cryogenic temperatures

[NASA-TP-23f2] p 69 N84-23750

A cracked orthotropic sheet stiffened by a semi-infinite

orthotropic sheet

[NASA-TP-2455] p 134 N85-32339

CRACK TIPS

A cracked orthotropic sheet stiffened by a semi-infinite

orthotropic sheet

[NASA-TP-2455] p 134 N65-32339

CRACKING (FRACTURING)

Influence of fretting on flexural fatigue of 304 stainless

steel and mild steel

[NASA-TP-1193} p 86 N78-21269

Method for estimating crack-extension resistance curve

from residual strength data

[NASA-TP-1753] p 129 N81-11417

CRACKS

Rotordynamic Instability Problems in High-Performance

Turbomachinery

[NASA.CP-2250} p 122 N63-f5629

Engineering and design properties of thallium-doped

sodium iodide and selected properties of sodium-doped

cesium iodide

{NASA-RP-11311 p 99 N84-33613

CRASH INJURIES

Correlation and assessment of structural airplane crash

data with flight parameters at impacf

[NASA-TP-2063J p 131 N83-t4521

CRASH LANDING

Light airplane crash tests at impact velocities of t 3 and

27 m/sac

[NASA-TP-1042] p 29 N78-10034

Light airplane crash tests at three flight-path angles

[NASA-TP-1210] p 127 N78-26494

Light airplane crash tests at three pitch angles

[NASA-TP-f481 } p f26 N80-11505

Crash tests of four identical high-wing single-engine

airplanes

[NASA-TP-1699] p 35 N80-30296

Abrasion behavior of aluminum and composite skin

coupons, stiffened skins and stiffened panels

representative of transport airplane structures

{NASA-TP-25201 p 38 N86-13316

CRASHES

Light airplane crash tests at three roll angles

{NASA-TP-14771 p t28 N80-10512

Crash tests of four low-wing twin-engine airplanes with

truss-reinforced fuselage structure

[NASA-TP-2070} p 131 N83-10442

Correlation and assessment of structursi airplane crash

data with flight parameters at impact

[NASA-TP-2083} p 131 N83-14521

Crash tests of three identical Iow-wiog single-engine

airplane

[NASA-TP-2190] p 30 N83-34921

Full-Scale Transport controlled Impact Demonstration

[NASA-CP-2395} p 135 N86-21933

Impact data from a transport aircraft during a controlled

impact demonstration

[NASA-TP-2589] p 38 N86-30721

CRASHWORTRINESS

Crash tests of four low-wing twin-engine airplanes with

truss-reinforced fuselage structure

INASA-TP-2070] p f3t N83-f0442

Full-scale crash-test evaluation of two load-limiting

subfloors for general aviation airframes

[NASA-TP-2380} p 134 N85-f3267

Full-Scale Transport controlled Impact Demonstration

[NASA-CP-23951 p 135 N86-21933

Impact data from a transport aircraft during a controlled

impact demonstration

{NASA-TP-2589] p 38 N86-30721

CREEP ANALYSIS

Long.time creep behavior of the tantalum alloy Astar

81tC --- as a function of stress, temperature, and grain

size

[NASA-TP-1691 I p 87 N80-32489

CREEP SUCKLING

Buckling and structural efficiency of sandwich-blade

stiffened composite compression panels

[NASA-TP-1269} p 127 N78-32492

CREEP PROPERTIES

Long-time creep behavior of the niobium alloy C-103

{NASA-TP-1727] p 67 N80-33555

Creep and residual mechanical properties of cast

suparelloys and oxide dispersion strengthened alloys

[NASA.TP.1781] p 87 Naf.19273

An update of the total-strain version of SRP

[NASA-TP-2499] p 90 N86-t2295

CREEP RUPTURE STRENGTH

Modules of rupture and oxidation resistance of

Sl 2.55AIO.6OO.72N3.52 siaicn

[NASA-TP-1490} p 93 N79-27309

MEGAt6 - Computer program for analysis and

extrapolation of stress-rupfure data

[NASA-TP-1809} p 130 N81-23486

CRITICAL FLOW

Depressudzation and two-phase flow of water containing

high levels of dissolved nitrogen gas

[NASA-TP-1839] p f09 N81-28389

CRITICAL VELOCITY

Cold-sir investigation of first stage of 4-1/2-stage, fan

drive turbine with average stage-loading factor of 4.66

{NASA-TP-1780] p 48 Nef-f6050

CROP GROWTH

Analysis of data systems requirements for global crop

production forecasting in the 1985 time frame

[NASA-TP-tf64J p f36 N78-18497

A comparative statistical study of tong-term agroctimatic

conditions affecting the growth of US winter wheat:

Distributions of regional monthly average precipitation on

the Great Plains and the state of Maryland and the effect

of agroclimatic conditions on y_eld in the state of Kansas

{NASA-TP-17241 p 163 N81-22658

CROSS FLOW

Induced velocity field of a jet in a crossflow

{NASA-TP-f0671 p 105 N78-26392

Flight investigation of piloting techniques and crosswind

limitations using a research type crosswind landing gear

[NASA-TP-1423} p 12 N79-23012

Velocity field of a round jet in a cross flow for various

jet injection angles and vetocity ratios --- Langley V/STOL

tunnel

INASA-TP-1506} p 107 N79-32500

Pressure and force data for a ftat wing and a warped

conical wing having s shockless recomproseion at Mach

f .62

[NASA-TP-1759] p 17 N8f-22016

Influence of thermal boundary conditions on heat

transfer from a cylinder in cross flow

{NASA-TP-1894} p 109 N8f-29384

Amplified crossflow disturbances in the laminar boundary

layer on swept wings with suction

[NASA-TP-f902] p f09 N82-11391

Crossflow effects on steady and fluctuating pressures

on an ogive-cylinder cone-frustum model in supersonic

separated flow

{NASA-TP-fg51J p 18 N82-t3'IO8

Body and canard effects on an attached-flow maneuver

wing at Mech 1.62

{NASA-TP-2249] p 23 N84-18163

CROSSLINKING

Three methods for in situ cross-linking of polyvinyl

alcohol films for application as ion-conducting membranes

in potassium hydroxide electrolyte --- battery separators

{NASA-TP-1407] p 78 N79.2flt28

CRUCIFORM WINGS

An experimental wind-tunnel investigation of a

ram-air-spoiler roll-control device on s forward-control

missile at supersonic speeds

INASA-TP-1353} p 11 N79-t7809

Effect of Reynolds number on stability characteristics

of a cruciform wing-body

INASA-TP-16831 p 15 N80-27283

CRUDE OIL

Assessment of AfternstNe Aircraft Fuels

INASA-CP'2307] p 51 N84-23630

CRYOGENIC COOLING

An algorithm for minimum-cost set-point ordering in a

cryogenic wind tunnel

INASA-TP-1923} p 59 N82-1t090

Refrigeration for Cryogenic Sensors

INASA-CP-2287] p 99 N84-15327

CRYOGENIC EQUIPMENT

Cryogenic foam insulation: Abstracted publications

{NASA-RP-1002} p 79 N78-11200

Theoretical contamination of cryogenic satellite

telescopes

{NASA-TP-t 177 } p 65 N78-21 '193

Transient shutdown analysis of low-temperature thermal

diodes

{NASA-TP-1369] p 106 N79-18287

Cryogenic Technology, part 1 --- conference

proceedings; cryogenic wind tunnel design and

instrumentation

[NASA-CP-2122-PT-f } p 99 N82-20357

Cryogenic Technology. part 2 --- conference

proceedings; cryogenic wind tunnel design and

instrumentation

{NASA-CP-2'I22-PT-2] p 99 N82-20358

CRYOGENIC FLUID STORAGE

Purging of a tank-mounted multilayer insulation system

by gas diffusion

[NASA-TP-1127] p 65 N78-17127

CRYOGENIC FLUIDS

Two*phase choked flow of cryogenic fluids in

converging-diverging nozzles

[NASA-TP-1484] p 107 N79-29468

OTV Propulsion Issues

[NASA-CP-2347] p 87 N85-16989

CRYOGENIC ROCKET PROPELLANTS

Vapor ingestion in Centaur liquid-hydrogen tank

[NASA.TP-f 061 } p 104 N77-33444

Modeling of space vehicle propellant mixing --- cryogenic

propellants

[NASA-TP-2107] p 97 N83-f6545

CRYOGENIC WIND TUNNELS

High Reynolds Number Research

{NASA-CP-2009] p 59 N77-27139

Onset of condensation effects with an NACA 0012-64

airfoil tested in the Langley 0.3-meter transonic cryogenic

tunnel

{NASA-TP-f385J p 12 N79-22043

Thermodynamic properties of nitrogen gas derived from

measurements of sound speed --- for cryogenic wind

tunnels

{NASA-RP-t05f I p 97 N80-14257

A theoretical analysis of s_mulafed transonic boundary

layers in cryogenic-nitrogen wind tunnels

{NASA-TP-1631 ] p 59 N80-19131

Effects of various assumptions on the calculated liquid

fraction in isentrop.c saturated equilibrium expansions

[NASA-TP-1682J p 106 N80-25615

Development and validation of a hybrid.computer

simulator for a transonic cryogenic wind tunnel

INASA-TP-1695] p 59 N80-31413

A fan pressure ratio correlation in terms of Mach number

and Reynolds number for the Langley 0.3 meter transonic

cryogenic tunnel

tNASA-TP-1752] p 16 N81-10005

A-35
CRYOGENICS SUBJECT INDEX

An application of multivariable des_n techniques to the

control of the national transonic facility

INASA-TP-18871 p 181 N81-29840

Simulation of ideal-gas flow by nitrogen and other

selected gases at cryogenic temperatures --- transonic flow

in cryogenic wind tunnels

INASA-TP-1901 J p 109 N81-32418

An algorithm for minimum-cost set-point ordering in a

cryogenic wind tunnel

INASA-TP-1923J p 59 N82-11090

Cryooenic Technology, part t --- conference

proceedings; cryogenic wind tunnel design and

instrumentation

[NASA-CP-2122-PT-l} p 99 N82-20357

Cryogenic Technology, part 2 --- conference

proceedings; cryogenic wind tunnel design and

instrumentation

[NASA-CP-2122-PT-2} p 99 N82-20358

Flow Visualization and Laser Velocimetry for Wind

Tunnels

[NASA-CP-2243J p 116 N82-32663

Cryogenic Wind Tunnel Models Design and

Fabrication

I NASA-CP-2262] p 59 N83-18748

Studies of sidewall boundary layer in the Langley 0.3

meter transonic cryogenic tunnel with and without

suction

[NASA-TP-2096) p 110 N83-20031

Development of a distributed-parameter mathematical

model for simulation of cryogenic wind tunnels

INASA-TP-2177} p 184 N83-35736

Aerodynamic force measurements with a strain-gage

balance in a cryogenic wind tunnel

INASA-TP-2251} p 22 N84-f3162

Studies of condensation effects on airfoil testing in the

Langley 03-meter transonic cryogenic tunnel

INASA-TP-2509] p 113 N86-20720

R4 airfoil data corrected for sidewall boundary-layer

effects in the Langley 0.3-meter transonic cryogenic

tunnel

[NASA-TP-2565J p 28 N86-24662

Dynamic measurement of total temperature, pressure

and velocity in the Langley 03-meter transonic cryogenic

tunnel

INASA'TP-25841 p 60 N86-24709

CRYOGENICS

Passive eddy-current damping as a means of vibration

control in cryogenic turbomaohinery

INASA-TP-2562} p 68 N86-24722

CRYSTAL DEFECTS

Solar Cell High Efficiency and Radiation Damage

[NASA-CP-2020] p 144 N78-13527

CRYSTAL GROWTH

Ice crystal growth in a dynamic thermal diffusion

chamber

[NASA-TP-1651 } p 162 N80-23934

Float Zone Workshop

INASA-CP-2179} p 62 N81-19144

Float Zone Workshop

[NASA-CP-2226] p 62 N82-26330

Approximate analysis of thermal convection _n a

crystal-growth cell for Spacelab 3

NASA-TP-20t6 p 62 N82-29335

A potantial-energy scaling model to simulate the initial

stages of thin-film growth

NASA-TP-2102 p 88 N83-18895

Fundamentals of Alloy Solidification Applied to Industrial

Processes

NASA-CP-2337 p 90 N84-34589

A preliminary study of numerical simulation ot

thermosotutal convection of interest to crystal growth

NASA-TP-2394 p 112 N85-13175

Analytical and numerical studies of the thermocapillary

flow in a uniformly floating zone

NASA-TP-2576 p 113 N86-2385t

Numehcal modeling of physical vapor transport in a

vertical cylindrical ampoule, with and without gravity

NASA-TP-2620 p 96 N86-29040

CRYSTAL LATTICES

Monte Carlo lattice models for adsorbed polymer

conformation

{NASA-TP-24531 p 195 N85-2496t

CRYSTAL OPTICS

Pockels-effect cell for gas-flow simulation

{ NASA-TP-2007 } p 115 N82-23515

CRYSTAL STRUCTURE

Changes in surface chemistry ot silicon carbide (0001)

surface with temperature and their effect on friction

{NASA-TP-17561 p 94 N81-14079

Characterization of erosion of metallic materials under

cavitation attack m a mineral oil

{NASA-TP-236.81 p 124 N84-32825

CRYSTAL SURFACES

Friction and deformation behavior of single-crystal

silicon carbide

INASA-TP-1053] p 91 N77-33350

Anisotropic friction, deformation, and fracture of

single-crystal silicon carbide at room temperature

I NASA-TP-1525J p 93 N79-30380

Influence of mineral oil and additives on microhardness

and surface chemistry of magnesium oxide (001) surface

I NASA-TP-1986] p94 N82-20316

Analysis of the physical atomic forces between noble

gas atoms, alkali ions and halogen ions

I NASA-TP-2568 ] p 90 N86-26413

CRYSTALLIZATION

Sliding induced crystallization of metallic glass

I NASA-TP-2140 ] p88 N83-21110

CUES

Effects Of visual and motion simulation cueing systems

on pilot performance during takeoffs with engine failures

(NASA-TP-1365} p 32 N79-14082

Motion/visual cueing requirements for vortex encounters

during simulated transport visual approach and landing

INASA-TP-2136} p 36 N83-22192

Effects of motion base and g-seat cueing of simulator

pilot perlormance

I NASA-TP*2247] p 37 N84-18189

CURING

Formulationcure technology for ultrahigh molecular

weight silphenytene-siloxane polymers

[NASA-TP-2476] p 96 N85-26990

CURRENT DENSITY

Improved, low cost inorganic-organic separators for

rechargeable silver-zinc batteries

[NASA-TP-1476] p 84 N79-25181

Three-axis electron-beam test facility

{NASA-TP-1836] p 101 N81-20359

CURRENT DISTRIBUTION

Performance of computer-designed small-sized

four-stage depressed collector for operation of dual-mode

traveling wave tube

[NASA-TP-1832] p 102 N81-30360

CURVATURE

The effects of curvature and viscosity on baroclinic

instability: A two-layer model

[NASA-TP-1328} p 159 N78-32641

Sonic-boom wave-front shapes and ou_atures

associated with maneuvering flight

{NASA-TP-1611 } p 13 N80-14045

Structural efficiency studies of corrugated compression

panels with curved caps and beaded webs

{NASA-TP-2272} p 132 N84-18675

CURVE FITTING

Instrument to average 100 data sets

INASA-TP-f055} p 100 N79-1t301

Rational-spline approximation with automatic tension

adjustment

{NASA-TP-2366J p 182 N84-34204

CUSHIONS

Effect of strain isolator pad modulus on inplane strain

in Shuttle Orbiter thermal protection system tiles

{NASA-TP-2141 } p 132 N83-33216

CYCLES

Global Biology Research Program: Biogeochemical

Processes in Wetlands

{NASA-CP-2316] p 169 N84-30665

CYCLIC LOADS

Simplified method for nonlinear structural analysis

[NASA-TP-2208} p 132 N83-34372

Development of a simplified procedure for cyclic

structural analysis

[NASA-TP-2243} p 133 N84-20878

Local strain redistribution corrections for a simplified

inelastic analysis procedure based on an elastic

finite-element analysis

INASA'TP-2421 } p f34 N85-20396

CYCLOGENESIS

Current Scientific Issues in Large Scale Atmospheric

Dynamics

{NASA-CP-2410] p 167 N86-24082

CYCLONES

NASA/MSFC FY-84 Atmospheric Processes Research

Review

{NASA-CP-2329] p 166 N84-34829

CYLINDRICAL BODIES

In-flight boundary-layer measurements on a hotlow

cylinder at a Mach number of 3.0

{NASA-TP-f764} p 108 N81-12361

Influence of thermal boundary conditions on heat

transfer from a cylinder in cross flow

l NASA-TP-1894 } p 109 N81-29384

Crossfiow effects on steady and fluctuating pressures

on an og=ve-cylinder cone-frustum model in supersonic

separated flow

[ NASA-TP-1951 } p 18 N82-t3f08

CYLINDRICAL SHELLS

A theoretical investigation of noise reduction through

the cylindrical fuselage of a twin-engine, propeller-driven

aircraft

INASA-TP-13251 p 186 N79-13821

Wind-tunnel measurements and comparison with flight

of the boundary layer and heat transfer on a hollow cylinder

at Mach 3

[NASA-TP-17891 p 16 N81-14975

Design detail verification tests for a lightly loaded

open-corrugation graphite-epoxy cylinder

[NASA-TP-1981 ] p 130 N82-20567

Buckling test of a 3-meter-diameter corrugated

graphite-epoxy ring-stiffened cylinder

[NASA-TP-20321 p 131 N82-28665

Flow in a torsionally oscillating filled cylinder

[NASA-TP-2115} p 110 N83-16674

Liquid management in low gravity using baffled rotating

containers

INASA'TP-2263 ] p 111 N84-15427

CYLINDRICAL TANKS

Axial jet mixing of ethano_ in cylindrical containers during

weightlessness

[NASA-TP-1487J p 97 N79-28350

Contoured tank outlets for draining of cylindrical tanks

in tow-gravity environment --- Lewis Research Center Zero

Gravity Facility

INASA-TP-1492] p 107 N79-29467

D

DAMAGE ASSESSMENT

Crash tests of four identical high-wing single-engine

airplanes

{NASA-TP-1699} p 35 N80-30296

DAMPERS

Performance of two-stage fan with larger dampers on

first-stage rotor

{NASA-TP-t399J p 44 N79-23967

DAMPERS (VALVES)

Off-design correlation for losses due to part-span

dampers on transonic rotors

{NASA-TP-16931 p 47 N80-28352

Damping seals for turbomachinery

{ NASA-TP-19871 p 49 N82-20183

DAMPING

Damping in tapered annular seals for an incompressible

fluid

{NASA-TP-16461 p 121 N80-19495

Tire stiffness and damping determined from static and

free-vibration tests --- aircraft tires

{NASA-TP-1671 I p 29 N80-27302

Comparison of analytical and wind-tunnel results for

flutter and gust response of a transport wing with active

controls

INASA-TP-2010I p 131 N82-26703

Passive eddy-current damping as a means of vibration

control in cryogenic turbomachinery

INASA-TP-2562] p 68 N86-24722

DATA AGOUISlTION

National geodetic satellite program, part 1

[NASA-SP-365-PT-1 } p 151 N78-11545

National geodetic satellite program, part 2

[ NASA-SP-365-PT-2 } p 151 N78-11552

Wind tunnel investigation of an all flush orifice air data

system for a large subsonic aircraft --- conducted in a

Langley 8 foot transonic pressure tunnel

{NASA-TP-16421 p 38 N80-23304

Power spectral measurements of clear-air turbulence

to long wavelengths for altitudes up to 14,000 meters

{NASA-TP-19791 p 164 N82-24790

Handbook of sensor technical characteristics

(NASA-RP-10871 p 115 N82-29577

The Snowmelt-Runoff Model (SRM) user's manual

{NASA-RP-1100] p 141 N93-23660

Experiments in a three-dimens_onal adaptive-walt wind

tunnel

[NASA-TP-2210} p 22 N83-34906

Solar absorptance and thermal emittance of some

common spacecraft thermal-control coatings

(NASA-RP-1121 ] p 82 N84-23698

Climatology of ozone at attitudes from 19,000 at 59,000

feet based on combined GASP and ozone,sonde data

INASA-TP-2303J p 166 N84-31865

Full-Scale Transport controlled impact Demonstration

I NASA-CP-2395] p 135 N86-21933

Proceedings of the Second Pilot Climate Data System

Workshop

[NASA-CP-24301 p 137 N86-29282

DATA BASE MANAGEMENT SYSTEMS

NASA Admimstrative Data Base Management

Systems

[NASA-CP-22541 p 197 N83-18559

Data bases and data base systems related to NASA's

Aerospace Program: A bibliography with indexes

[ NASA-SP-70481 p 197 N83-22010

NASA Administrative Data Base Management Systems,

t983

[NASA-CP-23041 p 198 N84 21403

A-36
SUBJECT INDEX

IPAD 2: Advances in Distributed Data Base Management

for CAD/CAM

[NASA-CP-2301 } p 180 N84-22299

NASA Administrative Data Base Management Systems,

1984

[NASA-CP-2323 J p 198 N84-33266

Planetary Data Workshop, part 1

[NASA-CP-2343-PT-1 I p 208 N84-34366

Planetary Data Workshop, part 2

[NASA-CP-2343-PT-2] p 208 N84-34376

DATA BASES

Engineering and Scientific Data Management

[NASA-CP-2055J p 178 N78-33776

Procedure for extraction of disparate data from maps

into computerized data bases

{NASA-RP-10481 p 177 N79-33858

Office of Space Terrestrial Applications

(OSTA)/Applications Data Service (ADS) data systems

standards

{NASA-CP-2196] p 65 N82-18095

Application of a computerized vibroaooustic data bank

for random vibration criteria development

[NASA-TP-1998] p 73 N82-20238

NASA Administrative Data Base Management

Systems

{NASA-CP-2254] p 197 N83-18559

Data bases and data base systems related to NASA's

Aerospace Program: A bibliography with indexes

{NASA-SP-7048] p 197 N83-22010

Proceedings of the National Conference on Energy

Resource Management. Volume 1: Techniques,

Procedures and Data Bases

(E83-103351 p 141 N83-26158

Far infrared supplement: Catalog of infrared

observations

[NASA-RP-11191 p 202 N84-26519

Catalog of infrared observations including: Bibliography

of infrared astronomy and index of infrared source

positions

[NASA-RP-1118] p 202 N84-26520

Global Biology Research Program: Siogeochemical

Processes in Wetlands

NASA-CP-23161 p 169 N84-30668

Trends in Planetary Data Analysis. Executive summary

of the Planetary Data Workshop

NASA-CP-23331 p 208 N84-34363

Conclusion of Viking Lander imaging investigation:

Picture catalog of experiment data record

NASA-RP-1137] p 208 N85-21099

A new NASA/MSFC mission analysis global cloud cover

data base

NASA-TP-2448J p 166 N85-21878

Aerodynamic characteristics of a supersonic fighter

aircraft model at Mach 0.40 to 2,47

NASA-TP-2580] p 28 N86-23561

DATA COLLECTION PLATFORMS

Nimbus 6 Random Access Measurement System

applications experiments

[NASA-SP-457] p 165 N83-14835

DATA COMPRESSION

An image compression survey and algorithm switching

based on scene activity

[NASA-TP-2458] p 27 N85-33106

DATA CONVERSION ROUTINES

Procedure for extraction of disparate data from maps

into computerized data bases

[NASA-RP-1048] p 177 N79-33858

An improved viscous characteristics analysis program

[NASA-TP-1289] p 108 N81-12356

DATA CORRELATION

instrument to average 100 data sets

[NASA-TP-1055] p 100 N78-11301

Correlation of laser veloometer measurements over a

wing with results of two prediction techniques --- in the

Langley V/STOL tunnel

[NASA-TP-1168] p 105 N78-21410

The NASA-Ames Research Center stratospheric aerosol

model 2 Sensitivity studies and comparison with

observatories

[NASA-TP-1363] p 160 N79-21720

A correlation of mixing noise from coannular jels with

inverted flow profiles

INASA-TP-1301 I p 187 N79-22849

Wind-tunnel/flight correlation study of aerodynamic

characteristics of a large flexible supersonic cruise airplane

(XB-70-1). 3: A comparison between characteristics

predicted from wind-tunnel measurements and those

measured in flight

INASA-TP-1516] p 14 N80-17986

Wind-Tunnel/Flight Correlation, 1981

INASA-CP-2225] p 19 N82-25196

LANDSAT-4 Science Investigations Summary, including

(December 1983 Workshop results, volume 1

IE84-10166} p 137 N84-30359

Climatology of ozone at altitudes from 19,000 at 59,000

feet based on combined GASP and ozonesonde data

INASA-TP-2303J p 166 N84-31865

Simulator study of flight characteristics of several large,

dissimilar, cargo transport airplanes during approach and

landing

[NASA-TP-2357J p 58 N85-11002

Ozone Correlative Measurements Workshop

INASA-CP-2362] p 137 N85-23112

DATA INTEGRATION

Proceedings of the National Conference on Energy

Resource Management. Volume 1: Techniques,

Procedures and Data Bases

[E83-10335] p 141 N83-26155

DATA LINKS

Design of a video tetaconference facility for a

synchronous satellite communications link

INASA-TP-1376] p 100 N79-14278

ATS-6 engineering performance report. Volume 5:

Propagation experiments

[NASA-RP-1080-VOL-5] p 73 N82-'16151

DATA MANAGEMENT

Engineering and Scientific Data Management

INASA-CP'2055] p 178 N78-33776

NASA Administrative Data Base Management

Systems

INASA-CP-2254] p 197 N83-18559

Trends in Planetary Data Analysis. ExecutNe summary

of the Planetary Data Workshop

INASA-CP'2333] p 208 N84-34363

Planetary Data Workshop, part 2

[NASA-CP-2343-PT-2] p 208 N84-34376

Proceedings of the Second Pilot Climate Data System

Workshop

[NASA-CP-2430] p 137 N86-29282

The MSFC/UAH Data Management Symposium

[NASA-CP-2040] p 177 N78-74689

DATA PROCESSING

inversion Methods in Atmospheric Remote Sounding

INASA-CP-004] p 151 N78-12586

Simulation studies of wide and medium field of view

earth radiation data analysis

[ NASA-TP-1182J p 158 N78-23679

Effects of visual and motion simulation cueing systems

on pilot performance during takeoffs with engine failures

{ NASA-TP-13651 p 32 N79-14082

Processing of on-board recorded data for quick analysis

of aircraft performance --- rotor systems research

aircraft

[NASA-RP-t043] p 33 N7g-33191

Conference of Remote Sensing Educators

(CORSE-78)

[ NASA-CP-2102 J p 212 N80-20003

The time-space relationship of the data point (Pixels)

of the thematic mapper and multispectral scanner or the

myth of simultaneity

[NASA-TP-1715J p 76 N80-28424

High speed lookup table approach to radiometric

calibration of multispecfrel image data

INASA-TP-1741 I p 76 N80-33463

NASA Wallops Flight Center GEOS-3 altimeter data

br oces.mng report

INASA-RP-1066J p 139 N81-11438

Digital processing of remotely sensed images

[NASA-SP-4311 p 139 N81-20489

Human Factors Considerations in System Design

[NASA-CP-2246J p 173 N83-18238

Second Eastern Regional Remofe Sensing Applications

Conference

[E83-10t89] p 141 N83-19141

Planetary Data Workshop, part 2

[NASA-CP-2343-PT-2] p 208 N84-34376

Introduction to time series analysis

[NASA-RP-1145] p t91 N86-24391

DATA PROCESSING EQUIPMENT

Sample data effects of high-pass filters

[NASA-TP-17971 p 35 N81-16040

DATA RECORDING

High-density digital recording

INASA-RP-1111 ] p 103 N86-14498

DATA REDUCTION

Convective rainfal] estimation from digital GOES-1

infrared data

INASA-RP-1034] p 160 N79-31885

Procedure for extraction of disparate data from maps

into computerized data bases

[NASA-RP-t048] p 177 N79-33858

Deconvolution and analysis of wide-angle iongwave

radiation data from Nimbus 6 Earth radiation budget

experiment for the first year

INASA-TP-1746] p 162 N81-13593

The theory and practice of estimating the accuracy of

dynamic flight-determined coefficients

INASA-RP-1077] p 183 N81-27865

DECOUPLING

Comparison of data inversion techniques for remotely

sensed wide-angle observations of Earth emitted

radiation

[NASA-TP-1924} p 164 N82-13620

Wildland inventory and resource modeling for Douglas

and Carson City Counties, Nevada, using LANDSAT and

digital terrain data

[E83-10302] p 142 N83-27293

Trends in Planetary Data Analysis. Executive summary

of the Planetary Data Workshop

[NASA-CP*2333} p 208 N84-34363

Measurements of Solar Vector Magnetic Fields

{NASA-CP-2374} p 210 N85-29869

DATA RETRIEVAL

Astronomical Microdensitometry Conference

[ NASA-CP-2317 ] p t 16 N84-28020

Proceedings of the Second Pilot Climata Data System

Workshop

[NASA-CP-2430} p 137 N86-29282

DATA STORAGE

Optical and holographic storage properties of F3, Cu,

and Mg-doped lithium niobata

[NASA-TP-1144} p 193 N78-20948

Astronomical MK;rodensitometry Conference

INASA-CP-2317} p 116 N84-28020

Planetary Data Workshop, part 2

[NASA-CP-2343-PT-21 p 208 N84-34376

DATA SYSTEMS

Analysis of data systems requirements for global crop

production forecasting in the 1985 time frame

[NASA-TP-t1641 p 138 N78-18497

Trends in Planetary Data Analysis. Executive summary

of the Planetary Data Workshop

[NASA-CP-2333] p 208 N84-34363

Planetary Data Workshop, part 2

[NASA-CP-2343-PT-2J p 208 N84-34376

Proceedings of the Second Pilot Climate Data System

Workshop

[NASA-CP-2430] p 137 N86o29282

DATA TRANSMISSION

Nimbus 6 Random Access Measurement System

applications experiments

[NASA*SP-4571 p 165 N83-14835

An image compression survey and algorithm switching

based on scene activity

[NASA-TP.24581 p 27 N85-33106

DEBRIS

Occurrence of spherical ceramic debds in indentation

and sliding contact

[NASA-TP-2048] p 95 N82-32491

Characterization of soil and postlaunch pad debris from

Cape Canaveral launch complex and analysis of soil

interact_n with aqueous HCI

{NASA-TP-2076] p 150 N83-12595

DECELERATION

Ground distance covered during airborne horizontal

deceleration of an airplane

[NASA-TP-1157] p 32 N78-20115

Companson of experimental and theoretical turbulence

reduction characteristics for screens, honeycomb, and

honeycomb-screen combinations

[NASA-TP-1958] p 19 N82-14058

DECISION MAKING

Management system, organizational climate and

performance relationships

[NASA-TP-1417] p 198 N79-19912

Automated decision making and problem solving.

Volume 2: Conference presentations

[NASA-CP-2180-VOL-2] p 184 N81-29902

Automated Decision Making and Problem Solving.

Volume 1: Executive Summary

[NASA-CP-2180-VOL-1 ] p 184 N81-30889

Management: A bibliography for NASA Managers

[NASA-SP-7500(20)] p 196 N86-27108

Twenty-First Annual Conference on Manual Control

[NASA-CP-2428] p 174 N86-32976

DECODING

A decoding procedure for the Reed-Solomon codes

[NASA-TP-1286] p 180 N78-30862

DECOMPOSITION

Catalytic decomposition of methanol for onboard

hydrogen generation

[NASA-TP-t247] p 97 N78-25236

DECOUPUNG

Effects of errors on decoupled control systems

[NASA-TP-1184] p 53 N78-27138

Decoupiod control of a long flexible beam in orbit

[NASA-TP-1740] p 71 N81-13082

Decoupiod control analysis of a large flexible space

antenna with linear quadratic regulator comparisons

[NASA-TP-2293] p 74 N84-23675

Decoupted and linear quadratic regulator control of a

large, flexible space antenna with an observer in the control

loop

[NASA-TP-24841 p 75 N86-16250

A-37
DEFECTS

DEFECTS

Evaluation of muitilayer printed wiring boards by

metaltographic techniques: An illustrated guide to the

preDate/ion and inspection of plated-through hole test

coupons based on the requirements of MiI-P-55110D

[NASA-RP-1161J p 126 N86-26639

DEFENSE COMMUNICATIONS SYSTEM (DCS)

The 1 tth Space Simulation Conference

{NASA-CP-2150] p 99 N81-14138

DEFENSE PROGRAM

Astronautics and aeronautics, 1976 A chronology

[NASA-SP-4021 ] p 212 N84-25602

DEFLECTION

Effects of deflected thrust on the longitudinal

aerodynamic characteristics of a close-coupled

wing-canard configuration --- in the Langley V/STOL

tunnel

{NASA-TP-10°J0] p 6 N78-13014

Pressure and thermal distributions on wings and adjacent

surfaces induced by elevon deflections at Mach 6

[NASA-TP.1356] p 106 N79-20344

Leading-edge deflection optimization for a highly swept

arrow wing configuration

[NASA-TP-1777} p 16 N81-14974

DEFORMATION

On the nonlinear deformation geometry of

Euler-Bornoulli beams --- rotary wings

[NASA-TP-1566] p 129 N80-20619

Research in nonlinear structural and sOlid mechanics

[NASA-CP-2147] p 129 N80-32756

Some effects of thermal-cycle-induced deformation in

rocket thrust chambers

{NASA-TP-1834J p 77 N81-20176

Fhction and morphology of magnetic tapes in sliding

contact with nickel-zinc fernte

INASA-TP-2267J p 95 N84-16334

Mixed models and recug=on techniques for

large-rotation, nonlinear anatysis of shells of revolution with

application to tires

[NASA-TP-2343] p 133 N84-34773

Nonlinear equations for dynamics of pretw_sted beams

undergoing small strains and large rotations

INASA-TP-2470] p 134 N85-27258

DEGRADATION

Interface control and mechanical property improvements

in silicon carbide/titanium composites

{NASA-TP-206E,] p 81 N82-31451

Analysis of a MIL-L-27502 lubricant from a gas-turbine

engine test by size-exclusion chromatography

{NASA-TP-2063J p 95 N83-16528

DEGREES OF FREEDOM

Aerodynamic derivatives for an oblique wing aircraft

estimated from flight data by using a maximum likelihood

technique

INASA-TP-1336J p 10 N78-33054

Simulator evaluation of separation of display parameters

in path-following tasks

[NASA-TP-1915] p 39 N81-33203

Research in structural and solid mechanics, 1982

[NASA-CP-2245J p 131 N82-33739

Effect of aerodynamic and angle-ot*attack uncertainties

on the blended entry flight control system of the Space

Shuttle from Mach 10 to 25

(NASA-TP-2283J p 58 N84-23652

Effect of aerodynamic and angle-of-attack uncertainties

on the May 1979 entry flight control system of the Space

Shuttle from Mach 8 to 1 5

I NASA-TP-2365 J p 69 N85-15779

Ground-based and in-fl_Jhl simulator studies of flight

characteristics of a Iwm-fuselage passenger transport

airplane during approach and landing

[ NASA-TP=2451 I p 58 N85 34144

DEICERS

Joint University Program for Air Transportation

Research. 1981

(NASA-CP-2224) p 3 N82-26199

DEIMOS

Images of Mars- The Viking extended mission

JNASA-SP-4441 p 206 N80 26239

DELTA WINGS

Effects of roughness size on the posit=on of

boundary-layer transition and on the aerodynamE

characteristics ol a 55 deg swap( delta wing at supersonic

speeds

INASA-TP-t027I p 7 N78-13016

Configuration healing for e hypersonic research airplane

concept having a 70 deg swept double-delta wing

JNASA-TP-t143J p f05 N78-23389

Aerodynamic characteristics of a hypersontc research

airplane concept having a 70 deg swept double-delta wing

at Mach number 02

INASA-TP 1252j p 9 N78.31045

Estlmabon of leading-edge thrust for supersomc wings

of arbitrary planform

INASA-TP-12701 p 9 N78-33051

A-38

A modification to linearized theory for prediction of

pressure Ioadings on lifting surfaces at high supersonic

Mach numbers and large angles of attack

[NASA-TP-1406} p 11 N79-17806

Aerodynamic characteristics of a hypersonic research

airplane concept having a 70 deg swept double-delta wing

at Macb numbers from 0.80 to 120, with summary of data

Irom 0.20 to 60 --- Langley 8*it transonic wind tunnel

[NASA-TP-1552] p 13 N80-12064

Lee-side flow over delta wings at supersonic speeds

[NASA-TP-2430] p 26 N95-29921

Experimental and theoretical study of the longitudinal

aerodynamic characteristics of delta and double-delta

wings at Mach numbers of 1.60, 1.90, and 2.16

[NASA-TP-2433] p 26 N85-29922

DENSITY (MASS/VOLUME)

Atmospheric entry and fragmentation of dense

meteoroids

[NASA-TP.1333] p 2.05 N79-14978

DENSITY DISTRIBUTION

Volume-energy parameters and turbulent-flow density

fluctuations

[NASA-TP-1595] p 107 N80-17398

DENSITY MEASUREMENT

Computerized video densitometry method for rapid

analysis of infrared photographic images --- temperature

distribution across a turbine blade

[NASA-TP-1686] p 114 N80-25635

DEPLOYMENT

The 15th Aerospace Mechanisms Symposium

[NASA-CP-2181] p 130 N81-22388

The 17th Aerospace Mechanisms Symposium

[NASA-CP-2273J p 131 N83-24881

Vibration characteristics of a deployable

controllable-geometry truss boom

[NASA-TP-2160J p 132 N83-28491

DEPOLARIZATION

Radio-wave propagation for space communications

systems

[NASA-TP-1770] p 70 N81-ta082

DEPOSITION

Experimental and theoretical deposition rates from

salt-seeded combustion gases of a Mach 0.3 burner rig

[ NASA-TP-2225] p 111 N84-19741

An experimental and theoretical investigation of

deposition patterns from an agricultural airplane

[NASA-TP-2348] p 25 N84-33379

DESCENT

Reference energy-altitude descent guidance: Simulator

evaluation --- aircraft descent and fuel conservation

[NASA-TP-2383} p 40 N85-16868

Planning fuel-conservative descents in an airline

environmental using a small programmable calculator:

Algorithm development and flight test results

INASA-TP-2393] p 40 N85-26705

DESCENT TRAJECTORIES

Analysis of fuel-conservative curved decelerating

approach trajectories for powered-lift and CTOL jet

aircraft

[ NASA-TP-1650 ] p 2 N80-19022

Planning fuel-conservative descents with or without time

constraints using a small programmable calculator:

Algorithm development and flighl test results

[ NASA-TP-20851 p 40 N83-17535

DESERTS

Site selection and directional models of deserts used

for ERBE validation targets

i NASA-TP-2540 ] p 167 N86-23160

DESIGN

Human Factors Considerations in System Design

[NASA-CP-22461 p 173 NB3-18238

DESIGN ANALYSIS

Preliminary study of a large span-distributed-toad

flying-wing cargo airplane concept

[ NASA-TP-11581 p 32 N78-25079

Advanced Technology Airfoil Research. volume 1. pad

1 --- conference on development of computational codes

and test facilittes

INASA-CP-2045-PT-1 I p 1 I N79-20030

Experimental performance and analysis of

15 04 centimeter-tip-diameter, radial-tnftow turbine with

work lector of I 126 and thick blading

INASA TP.1730J p 47 N80-33410

Viking '75 spacecraft design and test summary Volume

3 Engineering lest summary

[NASA-RP-1027-VOL-3] p 71 N81-11102

Economic evaluation of flying-qualities design criteria for

a transport configured with relaxed static stability

INASA-TP-17601 p 56 N8t-13968

Use of constrained optimization in the conceptual design

of a medium-range subsonic transport

INASA-TP 17621 p 35 N81 16039

Cold-air investigation of first stage of 4-1/2-stage, fan

drive turbine with average stage-loading factor of 4.66

I NASA-TP-17801 p48 N81-16050

SUBJECT INDEX

System analysis approach to denying design criteria

(Loads) for Space Shuttle and its payloads. Volume 2:

Typical examples

{NASA-TP-1950] p 66 N82-15106

Large Horizontal-Axis Wind Turbines

[NASA-CP-2230J p 146 N83-f9231

Design guide for high pressure oxygen systems

{NASA-RP-1113] p99 N83-32990

Nonlinear Constitutive Re,aligns tor High Temperature

Applications

[NASA-CP-2271] p 132 N83-34351

The lath Aerospace Mechanisms Symposium

INASA-CP-2311] p 133 N84-25078

Advanced aerodynamics. Selected NASA research

[NASA-CP-2208] p 4 N84-27660

Two-dimensional aerodynamic characteristics of an

airfoil designed for two

[NASA-TP-1965] p 24 N84-27694

Astronomical Microdensitometry Conference

[NASA-CP-2317] p 116 N84-28020

Peer Review of a Formal Venfication/Design Proof

Methodology

[NASA-CP-2377] p 179 N85-28609

High Temperature Polymer Matrix Composites

[NASA-CP-2385] p 83 N86-11260

Gearing

[NASA-RP-1152] p t25 N86.14612

Fourteenth NASTRAN Users' Colloquium

[NASA-CP-241g] p 135 N86-25823

A method for developing design diagrams for ceramic

and glass materials using fatigue data

[NASA-RP-t174] p 126 N86-32763

DEW

Water vapor measurement system in global atmospheric

sampling program, appendix

[NASA-TP-2051 J p 150 N83-13643

DIAGRAMS

A method for developing design diagrams for ceramic

and glass materials using fatigue data

{ NASA-RP-1174 ] p 126 N86-32763

DIALLYL COMPOUNDS

Evaluation and auger analysis of a

zinc-dialkyl-dithiophosphate antiwear additive in several

diester lubricants

{NASA-TP-1544] p 93 N79-32359

DICTIONARIES

Origins of NASA names

[NASA-SP-4402] p 211 N77-16981

Space Transportation System and associated payloads:

Glossary, acronyms, and abbreviations

[ NASA-RP*t059 J p68 N81-16111

Space Transportation System and associated payloads:

Glossary, acronyms, and abbreviations

I NASA-RP-1059-REV J p69 N85-19007

DIELECTRIC PROPERTIES

Spacecraft Charging Technology, 1980

INASA-CP-2182] p 72 N82-14213

DIESEL ENGINES

Further industrial tests of ceramic thermal barrier

coatings

INASA-TP-2057] p 49 N83-10045

DIFFERENTIAL EQUATIONS

The NASA Ames Research Center one- and

two-dimensional stratospheric models Part 1: The

one-dimensional model

I NASA-TP-10021 p 158 N77-32688

The NASA Ames Research Center one- and

two-dtmensional stratospheric models. Part 2: The

two-dimensional model

INASA-TP-t003J p 158 N77-32689

Existence and uniqueness ol solutions to a class of

nonlinear-operator-differential equations arising in

automated spaceship navigation

INASA-TP-18601 p 70 N81-23182

Stochastic differential equations and turbulent

dispersion

{NASA-RP-11031 p 110 N83-22546

Modeling the interne) combustion engine

INASA-RP-tO94J p 182 N85-t9733

DIFFERENTIAL GEOMETRY

Global differential geometry: An introduction for control

engineers

JNASA-RP-1091 I p 176 N82-29904

DIFFRACTION PATTERNS

Programs for calculating cell parameters in electron and

X-ray diffraction --- to identify stratospheric aerosols

[ NASA-TP-15291 p 148 N79-30844

DIFFUSE RADIATION

Ninteenth International Cosmic Ray Contereoce OG

sessions, volume 1

[NASA-CP-2376-VOL-11 p 210 N85 33902

DIFFUSERS

Perlormance of a vortex_controlled diffuser in an annular

swirl-can combustor at inlet Mach numbers up to 0.53

INASA TP-1452f p 44 N79-22099
SUBJEC T INDEX

DIFFUSION

Feasibility study of tungsten as a diffusion barrier

between nickel-chromium-aluminum and Gamma/Gamma

prime - Delta eutectic alloys

[NASA-TP-t 131 "1 p 86 N78-15230

Effects of diffusion factor, aspect ratio and solidity on

overall performance of 14 compressor middle stages ---

the effects of varying both diffusion through the rotor and

compressor blades and blade aspect ratio

[NASA-TP-1523] p 45 N7g-33210

DIFFUSION COEFFICIENT

Effect of concentration dependence of the diffusion

coefficient on homogenization kinetics in multiphase binary

alloy systems

[NASA-TP-1281 ] p 87 N79-13138

Moisture diffusion parameter characteristics for epoxy

composites and neat resins

[NASA-TP-t474J p 80 N79-29241

DIFFUSION FLAMES

Effect of pressure on structure and NO sub X formation

in CO-air diffusion flames

[NASA.TP.1448] p 84 N80.13191

Forced and natural convection in laminar-jet diffusion

flames --- normal-gravity, inverted-gravity and zero-gravity

flames

[NASA-TP-1841 ] p 109 N81-24388

DIFFUSION WELDING

Elastic constants for superplastically

formed/diffusion-bonded corrugated sandwich core

[NASA-TP-1562] p 129 N80-23677

Joint design for improved fatigue life of diffusion-bonded

box-stiffened panels

[NASA-TP-2480] p 135 N85-33537

DIGITAL COMPUTERS

The N-BOD2 user's and programmer's manual

[NASA-TP-1145] p 70 N78-21200

Development of the reentry flight dynamics simulator

for evaluation of space shuttle orbiter entry systems

[NASA-TP-1700] p 71 N80-32429

CYBER 200 Applications Seminar

[NASA-CP-2295] p 179 N84-20208

DIGITAL DATA

The use of LANDSAT digital data and

computer-implemented techniques for an agricultural

application

[NASA-RP-10161 p 138 N78-21568

Convective rainfall estimation from digital GOES-1

infrared data

[NASA-RP-f034] p 160 N79-31885

Processing of on-board recorded data for quick analysis

of aircraft performance --- rotor systems research

aircraft

[NASA-RP-1043] p 33 N79-33191

Magnetic Tape Recording for the Eighties

[NASA-RP-t075] p 116 N82-29579

LANDSAT-4 Science Characterization Early Results.

Volume 4: Applications --- agriculture, soils land use,

geology, hydrology, wetlands, water quality, biomass

identification, and snow mapping

[E85-10070] p 143 N85-23186

DIGITAL NAVIGATION

Development and evaluation of a Kalman-filter algorithm

for terminal area navigation using sensors of moderate

accuracy

[NASA-TP-2035] p 31 N83-29193

DIGITAL SIMULATION

Generation of linear dynamic models from a digital

nonlinear simulation

[NASA-TP-1388] p 2 N79-16796

DIGITAL SYSTEMS

A rotor-mounted digital instrumentation system for

helicopter blade flight research measurements

[NASA-TP-1146] p 38 N78-20128

A nonlinear trajectory command generator for a digital

flight-control system

[NASA-TP-1221 ] p 54 N79-13057

Digital processing of remotely sensed images

[NASA-SP-431 ] p 139 N81-20489

Comparison of simulator fidelity model predictions with

in-simulator evaluation data

[NASA-TP-2106] p 36 N83-18715

Airborne Lidar measurements of aerosols, mixed layer

heights, and ozone during the 1980 PE PE/NEROS summer

field experiment

[NASA-RP-1143] p 150 N86-16748

DIGITAL TECHNIQUES

Application of the concept of dynamic trim control to

automatic landing of carrier aircraft --- utilizing digital

feedforeward control

[NASA-TP-15121 p 55 N80-19126

An application of multivariable design techniques to the

control of the national transonic facility

{NASA-TP-1887J p 181 N81-29840

Geometric interpretations of the Discrete Fourier

Transform (DFT)

[NASA-TP-2332] p 177 N84-24114

Lewis Research Center spin rig and its use in vibration

analysis of rotating systems

[NASA-TP-2304] p 51 N84-24578

Conclusion of Viking Lander Imaging Investigation:

Picture catalog of experiment data record

[NASA-RP-1137] p 208 N85-21099

Semianalytic modeling of aerodynamic shapes

INASA.TP-2413] p 25 N85-21120

Spectral reflectances of natural targets for use in remote

sensing studies

[NASA-RP-1139] p 143 N85-30450

High-density digital recording

[NASA-RP-1111] p 103 N86-14498

Digital Electronic Engine Control (DEEC) Flight

Evaluation in an F-15 Airplane

[NASA-CP-2298] p 52 N86-25342

DIMENSIONAL ANALYSIS

Modeling of space vehicle propeflant mixing --- cryogenic

propellants

[NASA-TP-2107] p 97 N83-16545

DIODES

Transient shutdown analysis of low-temperature thermal

diodes

fNASA-TP-13691 p 106 N79-18287

Heterodyne systems and technology, part 1 ---

conferences

[NASA-CP-2138-PT-1 ] p 117 N80-29652

Atmospheric solar absorption measurements in the 9

to 11 mum region using a diode laser heterodyne

spectrometer

[ NASA-TP-1726] p 153 N80-33998

DIRECTIONAL CONTROL

Relatwe control effectiveness technique with application

to airplane control coordination

[NASA-TP-2416] p 37 N85-23753

DIRECTIONAL SOLIDIFICATION (CRYSTALS)

A Study of production of misioi_ity gap alloys with

controlled structures

[NASA-TP-2144] p 195 N83-21991

DIRECTIONAL STABILITY

Entry dynamics of space shuttle orbiter with

lateral-directional stability and control uncertainties at

supersonic and hypersonic speeds

[NASA-TP-10111 p 70 N78-13119

Experimental and theoretical supersonic

lateral-directional stability characteristics of a simplified

wing-body configuration with a series of vertical-tail

arrangements

[NASA-TP-1878] p 17 N81-29095

The application of parameter estimation to flight

measurements to obtain lateral-directional stability

derivatives of an augmented let-flap STOL airplane

[NASA-TP-20331 p 57 N83-t6350

DIRECTIVITY

Directivity and trends of noise generated by a propeller

in a wake

[NASA-TP-2609] p 191 N86-31341

DISKS (SHAPES)

Liquid jet impingement normal to a disk in zero gravity

[NASA-TP-1017] p 104 N77-30413

Effect of sliding speed and contact stress on tribologicat

properties of ultra-high-molecular-weight polyethylene

[NASA-TP-20591 p 95 N83-14269

DISPERSING

Stochastic differential equations and turbulent

dispersion

[NASA-RP-t 103 ] p 110 N83-22546

DISPLACEMENT

Modal analysis of a nonuniform stnng with end mass

and variable tension

[NASA-TP-2198] p 67 N83-32826

An approximale buckling analysis for rectangular

orthotropic plates with centrally located cutouts

[NASA-TP-2528] p 135 N86-20856

DISPLAY DEVICES

Flight-test evaluation of two electronic display formats

for approach to landing under instrument conditions

[NASA-TP-1085J p 38 N78-13054

Effect of image ti!t of a virtual image display on simulated

transport touchdown performance

[NASA-TP-15201 p 33 N79-33189

Application of modified profile analysis to function testing

of simulated CTOL transport touchdown-performance

data

[NASA-TP-1541 ] p 33 N80-11069

Flight investigation of cockpit-displayed traffic

information utilizing coded symboiogy in an advanced

operational environment

{NASA-TP-1684 ] p 38 N80-27360

Simulation development and evaluation of an improved

longitudinal velocity vector control whee_ steering mode

and electronic display format

[NASA-TP-16641 p 39 N80-30305

Evaluation of a computer-generated perspective tunnel

display for flight path following

INASA-TP.1736] p 39 N81-13958

DOPPLER RADAR

Effect of display size on utilization of traffic srtuation

display for self-spacing task --- transport aircraff

{NASA-TP-t885J p 30 N81-29109

A general aviation simulator evaluation of a

rate-enhanced instrument landing system display

INASA-TP'1960] p 39 N82-14085

Ruggedized minicomputer hardware and software

topics. 1981: Proceedings of the 4th ROLM MIL-SPEC

Computer User's Group Conference

[ NASA-CP-2206I p 180 N82-14829

Simulator study of a pictorial display for general aviation

instrument flight

lNASA-TP-1963] p 39 N82-20180

Human Factors Considerations in System Design

[NASA-CP-2246} p 173 N83-18238

Motion/visual cueing requirements for vortex encounters

during simulated transport visual approach and landing

[NASA-TP-2136] p 36 N83-22192

The window of visibility: A psychological theory of fidelity

in time-sampled visual motion displays

[NASA-TP-2211] p 172 N83-33538

Effect of lead-aircraft ground-speed on self.spacing

performance using a cockpit display of traffic information

[NASA-TP-2194) p 40 N83-36028

Controls, Displays, and Information Transfer for General

Aviation IFR Operations

iNASA-CP-2279] p 4 N84-12029

Simulator study of pilot-aircraft-display system response

obtained with a three-dimensional-box pictonal display

{NASA-TP-21221 p 40 N84-13182

Peripheral Vision Horizon Display (PVHD)

{NASA-CP-2306} p 40 N85-10044

A cockpit-display concepf for executing a multiple

glide-slope approach for wake-vortex avoidance

{NASA-TP-23861 p 40 N85-16869

Measurements of Solar Vector Magnetic Fields

[NASA-CP-23741 p210 N85-29869

The algorithms for rational spline interpolation of

surfaces

[NASA-TP-2536] p 183 N86-18060

DISSOCIATION

Homogeneous reactions of hydrocarbons, silane, and

chlorosilanes in radiofrequency plasmas at low

pressures

JNASA-TP-2301 J p 79 N84-20643

Electromagnetic dissociation effects in galactic

heavy-ion fragmentation

[ NASA-TP-25271 p 211 N86-21492

DISSOLVED GASES

Depressurization and two-phase flow of water containing

high levers of dissolved nitrogen gas

[NASA-TP-18391 p 109 N81-28389

North Attantic Deep Water Formation

[NASA-CP-2367] p 169 N85-26028

DISTORTION

Test-engine and inlet performance of an aircraft used

for investigating flight effects on fan noise

[NASA-TP-2254] p 189 N84-21277

DISTRIBUTED PARAMETER SYSTEMS

Development of a distributed_parameter mathematioal

model for simulation of cryogenic wind tunnels

[NASA-TP-2177} p 184 N83-35736

DISTRIBUTED PROCESSING

Parallel, Asynchronous Executive (PAX): System

concepts, facilities, and architecture

{NASA-TP-2179] p 180 N83-28921

Joint University Program for Air Transportation

Research, 1982

{ NASA-CP-22851 p 4 N84-11099

NASA Administrative Data Base Management Systems,

1984

[NASA-CP-2323] p 198 N84-33266

Real-Time Multiprocessor Programming Language

(RTMPL) user's manual

[NASA-TP-2422] p 179 N85-28610

DISTRIBUTION FUNCTIONS

An efficient algorithm for generating random number

pairs drawn from a bivariate normal distribution

I NASA-TP-21731 p 184 N83-27679

DIVIDING (MATHEMATICS)

Solution of the symmetric eigenproblem AX-lambda

BX by delayed division

I NASA-TP-25141 p 135 N86-20857

DOCUMENTS

NASA publications guide

[NASA-SP-7047] p 197 N83-32671

Records of achievement: NASA special publications

[NASA-SP-470J p 197 N83-33792

DOPPLER EFFECT

Laser Doppler Velocimetry Workshop

{NASA-CP-20841 p 117 N79-22455

DOPPLER RADAR

First Scientific Working Group Meeting of Airborne

Doppler Lidar Wind Velocity Measurement Program

[NASA-CP-2161 ] p 162 N81-10637

A-39
DOWNWASH

Summary Proceedings of a Wind Sheer Workshop

[NASA-CP-2270] p 165 N83-25265

A conceptual framework for us;ng Doppler radar

acquired atmospheric data for flight simulation

{NASA-TP-21921 p 36 N83-27977

NASA/MSFC FY-83 Atmospheric Processes Research

Review

NASA-CP-228t } p 165 N83-33494

NASA/MSFC FY-84 Atmosphenc Processes Research

Review

[NASA-CP-23291 p 166 N84-34829

EMDWRWASH

Development and validahon of a combined rotor

fuselage induced flow field computational method ---

Langley V/STOL tunnel

INASA-TP-t6561 p 15 NS0-25296

Downwash in the plane of symmetry of an elliptically

loaded wing

INASA-TP-2414] p 25 N85-15693

DRAG

An experimental and theoretical investigation of the

effect of nonmetric over-the-wing nacelles on wing-body

aerodynamics

[NASA-TP-1503] p 12 N79-29t46

Design and experimental results for a

natural-laminar-flow airfoil for general aviation

applications

I NASA-TP-f861 } p 17 N81-24022

Airfoil interaction with impinging vortex

INASA-TP-2273} p 23 N84-18'159

Drag of two-Dimensional small-amplitude symmetric and

asymmetric wavy walls in turbulent boundary layers

I NASA-TP-2318 ] p 112 N84-25944

DRAG MEASUREMENT

Wind-tunnel measurements and comparison with flight

of the boundary layer and heat transfer on a hollow cylinder

at Mach 3

{NASA-TP-1789_ p 18 N81-14975

Flow through very porous screens

INASA-TP-2436] p 112 N85-20270

DRAG REDUCTION

EffeCt of winglets on a first-generation jet transport wing.

6: Stability characteristics for a full-span model at subsonic

speeds --- conducted in Langley 8 foot transonic pressure

tunnel

{NASA-TP-1330} p 12 N80-10101

Comparison of experimental and theoretical turbulence

reduction characteristics for screens, honeycomb, and

honeycomb-screen combinations

{NASA-TP-tg581 p lg N82-14055

Wave drag as the oblective function in transonic fighter

wing optimization

[NASA-TP-2265} p 23 N84-17127

Exploratory wind-tunnel investigation of a

wmgtip-mounted vortex turbine for vortex energy

recovery

{NASA-TP-24681 p 26 N85-26667

DRAINAGE

Draining character_st_s of hemispherioalty bot_orr_d

cylinders in a low-gravity environment

{NASA-TP-12971 p 106 N78-31384

Contoured tank outlets for draining of cylindrical tanks

in tow.gravity envwonment --- Lew_s Research Center Zero

Gravity Facility

[NASA-TP-t492} p 107 N7g.29467

The Snowmelt-Runoff Model (SRM) users manual

[NASA-RP-1100] p 141 N83.23660

DRAWINGS

Intersection of three-dimensional geometric surfaces

[NASA.TP-2454] p 177 N85-31839

DRONE AIRCRAFT

Advanced aerodynamics and active controls, Selected

NASA research

[NASA-CP-2172] p 3 N8f-19001

DROP SIZE

Venturi nozzle effects on fuel drop size and nitrogen

oxide emissions

[NASA-TP-2028_ p 49 N82-3132g

DUAL AIR DENSITY EXPLORER

A small gas inlet system for orbital mass-spectrometer

calibrations

[NASA-TP-117DI p 114 N78-21430

DUAL WING CONFIGURATIONS

Optimization and performance calculation of

dual-rotation propellers

{NASA-TP-t948) p 3 N82-14049

DUCT GEOMETRY

installation effects of long-duct pylon-mounted nacelles

on s twin-jet transport model with swept superoritical

wing

[NASA-TP-2457} p 27 N86-20346

DUCTED BODIES

Experimental evaluation of a pilot mulbnozzle-duct

apparatus

[NASA-TP-13191 p 59 N79-16877

A-40

DUCTED FLOW

Comparison of two computer programs by predicting

turbulent mixing of helium in a dotted supersonic

eirstream

[NASA-TP-I166J p 105 N78-22333

Velocity gradient method for calutating velocities in an

axisymmetdc annular duct

tNASA-TP-2029} p 20 N82-29270

Pressure probe and hot4ilm probe rsponses to acoustic

excitation in mean flow

INASA-TP-2581 I p 191 N86-27043

DUCTS

Noise suppression charactenst,,cs of peripherally

segmented duct liners

[NASA-TP-tg04] p 188 N81-33946

A study of resonant-cavity and fit0erglass-filled parallel

baffles as duct silencers --- for wind tunnels

{NASA-TP-1970] p 188 N82-24052

The aerodynamic performance of several flow control

devices for internal flow systems

I NASA-TP-1972 ] p59 N83-t7560

Vortex-generating coolant-flow-passage design for

increased film-cooling effectiveness and surface

coverage

[NASA-TP-2388J p 112 N85-12314

DWELL

Analytical techniques of pilot scanning behavior and their

application

[NASA-TP-2525] p 172 N86-27920

DYE LASERS

Laboratory tank studies of a single species of

phytoplenkton using a remote sensing fluorosensor

[NASA-TP-1821 j p 139 N81-20492

Intensity and absorbed-power distnbution in a cylindrical

solar-pumped dye laser

[NASA-TP-2321] p 118 N84-23878

DYNAMIC CHARACTERISTICS

Rotordynamic Instability Problems in High-Performance

Turbom&chinery

[NASA-CP-2250] p 122 N83-15629

Kinematic control of robot with degenera'e wrist

[NASA-TP-2341 ] p 181 N84-28539

DYNAMIC CONTROL

Analytical investigation of the landing dynamics of a large

airplane with a load-control System in the main landing

gear

[NASA-TP-1555] p 33 N80-13025

Application of the concept of dynamic trim control to

automatic landing of carrier aircraft --- utilizing digital

fsedforewerd control

[NASA-TP.1512] p 55 N80-19'126

Modeling, Analysis, and Optimization Issues for Large

Space Structures

_NASA-CP-2258] p66 NB3-t8819

Kinematic control of robot with degenerate wrist

[NASA-TP-2341 ] p 181 N84-28539

Thirteenth Space Simulation Conference. The Payload:

Tesling for Success

[NASA-CP-2340] p 74 N84-34468

DYNAMIC LOADS

Wind Turbine Structural Dynamics

[NASA.CP-2034) p 144 N78-19616

System analysis approach to deriving design criteria

(Loads) for Space Shuttle and its payloads. Volume 2:

Typical examples

[NASA-TP-1950] p 66 N82-15106

Experimental investigation Of active loads control for

aircraft lending gear

[NASA-TP.2042] p 36 N82-31321

DYNAMIC MODELS

Generation of linear dynamic models from a digital

nonlinear simulation

{NASA-TP-1388] p 2 N79.16796

Earth Radiation Budget Science, 1978 ---conferences

[NASA-CP-2100] p 160 N79-32797

Mechanics of a gaseous film barrier to lubricant wetting

of etastohydrodynamically lubricated conjunctions

[NASA-TP-2500] p 125 N85-32330

DYNAMIC RESPONSE

Dynamic stall expenments on the NACA 0012 airfoil

{NASA-TP-t 100] p 7 N78-17000

Predicting dynamic performance limits for servosystems

with saturating nonlineanties

[NASA-TP.1488) p 54 N79-28186

Damping in tapered annular seals for an incompressible

fluid

[NASA.TP-1646] p 121 N80-19495

Dynamic behavior of a beam drag-force anemometer

{NASA-TP-16871 p 114 N80-24595

Vibration characteristics of a steadily rotating slender

nng

[NASA-TP-1775] p 130 N81-14343

Pitfalls and guidelines for the numerical evaluation of

moderate-order system frequency response

[NASA-TP-1814] p 72 N81-25t38

SUBJECT INDEX

Time and frequency domain analysis of sampled data

controllers via mixed operation equations

INASA-TP-1817J p 72 N81-25139

Dynamics of aircraft anbskid braking systems ---

conducted at the Langley aircraft landing loads and traction

facility

[NASA-TP-1959J p 35 N82-18204

Comparison Of er_lytlcsI and wind-runner results for

flutter and gust response of a transport wing with active

controls

{NASA-TP-2010] p 131 N82-26703

Research _n structural and solid mechanics, 1982

[NASA-CP-2245] p 131 N82-3373g

Vibration studies of a lightweight three-sided membrane

suitable for space application

[NASA-TP-20gS] p 131 N83-16785

Modeling, Analysis, and Optimization Issues for Large

Space Structures

I NASA-CP-2258 ] p66 N83-18819

Elevenlh NASTRAN User's Coitoquium

[ NASA-CP-22841 p 132 N84-15590

Dynamic behavior of spiral-groove and Rayle_gh-Step

self-acting face seals

INASA-TP-2266} p 51 N84-16181

Rapid estimation of frequency response functions by

close-range photogrammetry

{NASA-TP-2471 } p 116 N86-1257g

Dynamic response of film thickness in spiral-groove face

seals

[NASA-TP-25441 p 52 N86-15313

DYNAMIC STABILITY

Static and dynamic stability analysis of the space shuttle

vehicle-orbiter

[ NASA-TP-11791 p68 N78-20176

Subsonic dynamic stability characteristics of two

close-coupled canard-wing configurations

{NASA-TP-1291 I p 9 N78-33050

Dynamics stability derivatives Of space shuttle orbiter

obtained from wind-tunnel and approach and landing flight

tests

[NASA-TP-1634] p 55 N80-21336

DYNAMIC STRUCTURAL ANALYSIS

Advances in engineenng science, volume 2

INASA-CP-2OOI-VOL-2] p 98 N77-10265

Wind Turbine Structural Dynamics

{NASA-CP-2034] p 144 N78-19616

Evaluation of a hybrid, anisotropic, multilayered,

quadrilateral finite element

[NASA-TP-t238J p 127 N78-28482

Research in computerized structural analysis and

synthesis

[NASA-CP-2059] p 128 N79-10448

Structural dynamics and control of large space structures

--- conference

INASA-CP-21871 p 66 NSt-26166

Wind turbine dynamics

[NASA-CP-2185] p 146 N82-23684

Modeling, Analysis, and Optimization Issues for Large

Space Structures

[NASA-CP-2258] p 66 N83-18819

Structural Dynamics and Control of Large Space

Structures, 1982

[NASA-CP-2266] p 67 N83-22256

Survey of NASA research on crash dynamics

[NASA-TP-2298] p 133 N84-2'1901

Lewis Research Center s_in rig and its use in vibrebon

analysis of rotating systems

[NASA-TP-2304] p 51 N84-24578

Research in Structures and Dynamics, 1984

[NASA.CP-2335} p 134 N85.10377

STARS: A general.purpose finite element computer

program for analysis of engineering structures

[NASA-RP-11291 p 134 N85-11378

Large Space Antenna Systems Technology, 1984

[NASA.CP-2368.PT-f ] p 67 N85-23813

Large Space Antenna Systems Technology, t 984

[NASA-CP-2368-PT-2] p 68 N85-23840

Nonlinear equations for dynamics of pretwisted beams

undergoing small strains and large rotations

{NASA-TP-2470] p 134 N85-27258

Adeptive'.dentificat_on end control of structural dynamics

systems using recursive leilice filters

[NASA-TP-2371 ] p 75 N85-31 t42

Fourteenth NASTRAN Users' Colloquium

{NASA*CP-2419] p 135 N86-25823

DYNAMIC TESTS

Important factors in the maximum hkelihood analysis of

flight test maneuvers

[NASA-TP-1459] p 54 N79-22t 13

Tire stiffness and damping determined from static and

free-vibration tests --- aircraft tires

[NASA-TP-f671 ] p 29 N80-27302

Tire Modehng

INASA-CP-2264] p 131 N83-21391
SUBJECT INDEX

Thirteenth Space Simulation Conference. The Payload:

Testing for Success

[NASA-CP-2340] p 74 N84-34468

E

E GLASS

Tribologicai characteristics of a composite total-surface

hip replacement

[NASA-TP-1853] p 94 N82-16239

EARLY STARS

The Origin of Nonradiative Heating/Momentum in Hot

Stars

[NASA-CP-2358] p 200 N85-17755

EARTH (PLANET)

The Soviet-American Conference on Cosmochemistry

of the Moon and Planets, part 2

[NASA-SP-370-PT-2] p 203 N78-12958

The geology of the terrestrial planets

[NASA-SP-469] p 200 N85-18888

EARTH ATMOSPHERE

Guntersville Workshop on Solar-Terrestrial Studies

[NASA-CP-2037] p 144 N78-19600

Analyses of earth radiation budget data from unrestricted

broadband radiometers on the ESSA 7 satellite

[NASA-TP-1402] p 160 N79.22709

Godd&rd Laboratory for Atmospheric Science, collected

reprints 1978-1979, volume 1

[NASA-TP-1788-VOL-1 ] p 163 N81-21686

The Numerical Studies Program for the Atmospheric

General Circulation Experiment (AGCE) for Spacelab

Flights

[NASA-CP-2200] p 163 N82-12715

Vibrational-Rotational Spectroscopy For Planetary

Atmospheres, volume 1

[NASA-CP-2223-VOL-1 I p 207 N82-25043

NASA/MSFC FY-84 Atmospheric Processes Research

Review

[NASA-CP-2329J p 166 N84-34829

EARTH CORE

On the tidal oscillations of the liquid core of the earth

[NASA-TP-1223} p 15t N78-21691

EARTH CRUST _

Application of space technology to crustal dynamics and

earthquake research

[NASA-TP-1464] p 152 N79-31864

Geopotentiai Research Mission (GRM)

[NASA-CP-2390] p 155 N86-12852

EARTH HYDROSPHERE

Remote Sensing and Problems of the Hydrosphere

[NASA-CP-2109] p 168 N80-12718

Remote Sensing and Problems of the Hydrosphere, A

FocUS for Future Research --- conferences

[NASA-CP-2132t p 168 N80-23956

Godderd Laboratory for Atmospheric Sciences,

collected reprints 1978 - 1979, volume 2

[NASA-TP-1788-VOL-21 p 163 N81-21693

EARTH IONOSPHERE

Summary of the NASA/MSFC FY-79 Severe Storm and

Local Weather research review --- cloud physics,

atmospheric electricity, and mesoscale/storm dynamics

reserach

[NASA-CP-2105] p 160 N79-33722

Solar Terrestrial Physics: Present and Future

[NASA-RP-1120] p 200 N84-34332

EARTH LIMB

Description of data on the Nimbus 7 LIMS map archive

tape: Temperature and geopotential height

[NASA-TP-2553] p 167 N86-25924

EARTH OBSERVATIONS (FROM SPACE)

Apolio-Soyuz test project. Volume 2: Earth observations

and photography

[NASA-SP-412-VOL-2] p 138 N80-10538

Skylab explores the Earth

[NASA-SP-380] p 140 N82-12492

NASA/MSFC FY-81 Atmospheric Processes Research

Review

[NASA-CP-2204] p 164 N82-16660

Applying modeling Results in designing a global

tropospheric experiment

[NASA-CP-2235] p 153 N82-29796

EARTH ORBITS

Analysis of costs of gallium ersenide and silicon solar

arrays for space power applications

[NASA-TP-1811 ] p 77 N81-20173

Life test of • nickel cadmium battery with a

protection/reconditioning circuit

[NASA-TP-1873J p 77 N81-24167

Comparative analyses of space-to-space central power

stations

[ NASA-TP-1955 J p66 N82-14202

Spacecraft Environmental Interactions Technology,

1983

[NASA-CP-2359J p 75 N85-22470

Procedure for estimating orbital debris risks

INASA-TP-2507] p 69 N85-33169

EARTH RADIATION BUDGET

Analyses of earth radiation budget data from unrestricted

broadband radiometers on the ESSA 7 satellite

[NASA-TP-1402] p 160 N79-22709

Earth Radiation Budget Science, 1978 ---conferences

[NASA-CP-2100] p 160 N79-32797

Deconvolution and analysis of wide-angle Iongwave

radiation data from Nimbus 6 Earth radiation budget

experiment for the first year

[NASA-TP-1746] p 162 N81-13593

El Nino and outgoing Iongwave radiation: An atlas of

Nimbus-7 Earth radiation budget observations

[ NASA-RP-1163] p 157 N86-29425

EARTH RADIATION BUDGET EXPERIMENT

Deconvolution and analysis of wide-angle Iongwave

radiation data from Nimbus 6 Earth radiation budget

experiment for the first year

[NASA-TP-17461 p 162 N81-13593

Earth Radiation Science Seminars

{NASA-CP-2239] p 210 N82-33320

Site selection and directional models of deserts used

for ERBE validation targets

{NASA-TP-2540] p 167 N86-23160

Surface radiation budget for climate applications

{NASA-RP-1169] p 167 N86-28574

El Nino and outgoing Iongwave radiation: An atlas of

Nimbus-7 Earth radiation budget observations

[NASA-RP-1163] p 157 N86-29425

EARTH RESOURCES

Educator's guide for Mission to Earth: LANDSAT views

the world

INASA.SP.360] p 138 N80-10537

EARTH RESOURCES PROGRAM

Active Microwave Users Workshop Report

[NASA-CP-2030J p 138 N78-21562

Earth resources: A continuing bibliography with indexes,

issue 50

[NASA-SP-7041(50)I p 143 N86-31940

EARTH ROTATION

The NASA Geodynamics Program: An overview

[NASA-TP-2147] p 154 N84-10675

EARTH SURFACE

An introduction to orbit dynamics and its application to

satellite-based earth monitoring systems

[ NASA-RP-f009 ] p64 N78-12113

Simulation study of a geometric shape factor technique

for estimating earth-emitted radiant flux densities from

wide-field-of.view radiation measurements

[NASA-TP-1629] p 161 N80-20986

The Heat Capacity Mapping Mission (HCMM)

anthology

[E84-10051 ] p 142 N84-14563

EARTH-MOON SYSTEM

The evolution of complex and higher organisms

[NASA-SP-478J p 169 N85-32708

EARTHQUAKES

Application of space technology to crustal dynamics and

earthquake research

[NASA-TP-1464] p 152 N79-31864

ECLIPSING BINARY STARS

The 1982-1984 Eclipse of Epsiton Aurigae

[NASA-CP-2384] p 203 N86-12168

ECOLOGY

Radar, Insect Population Ecology, and Pest

Management

[NASA-CP-2070] p 169 N79-19592

Proceedings of Shuttle Environmental Effects Program

Review --- conferences

[NASA-CP-2110] p 149 N80-15649

ECONOMIC ANALYSIS

Economic evaluation of flying-qualities design criteria for

a transport configured with relaxed static stability

[NASA-TP-17601 p 56 N81-13968

Supersonic Cruise Research 1979, part 2 --- airframe

structures and materials, systems integration, economic

analysis

[NASA-CP-2108-PT-21 p 3 N81-18005

ECONOMIC FACTORS

Noise and ecohomic characteristics of an advanced

blended supersonic transport concept

[NASA-TP-2073] p 4 N82-31294

Second Symposium on Space Industnalization --- space

commercialization

[NASA-CP-2313] p 63 N85-11011

ECOSYSTEMS

On the habitability of Mars: An approach to planetary

ecosynthesis

[NASA-SP-414J p 175 N77-12718

Chesapeake Bay Plume Study: Superflux 1980

[NASA-CP-2188] p 168 N82-10661

Atmospheric Effects and Potential Climatic Impact of

the 1980 Eruptions of Mount St. Helena

[ NASA-CP-2240 ] p 136 N83-11534

ELASTIC DEFORMATION

EDDY CURRENTS

Passive eddy-current damping as a means of vibration

control in cryogenic turbomachinery

[NASA-TP-2562] p 68 N86-24722

EDUCATION

Educator's guide for Mission 10 Earlh: LANDSAT views

the world

[NASA-SP-360] p 138 N80-10537

Conference of Remote Sensing Educators

(CORSE-78)

[NASA-CP-2102) p 212 N80-20003

Field Study for Remote Sensing: An instructor's

manual

[NASA.CP-2155] p 136 N81-32564

TechniCal communication: PerspectNes for the elghtios,

part 1. Proceedings of the technical communications

sessions at the 32nd Annual Meeting of the Conference

on College Composition and Communication

[NASA-CP-2203-PT-1] p 197 N82-14960

Technical communication, Perspectives for the Eighties,

part 2

[NASA-CP-2203-PT-2] p 197 N82-15986

The LANDSAT tutorial workbook: Basics of satellite

remote sensing

[E83-10001] p 141 N83o10458

CORSE-81: The 1981 Conference on Remote Sensing

Education

[E83-10179] p 141 N83-17942

EFFECTIVE PERCEIVED NOISE LEVELS

Effects of duration and other noise characteristics on

the annoyance caused by aircraft-flyover noise

[NASA-TP-1386] p 186 N79-20832

Subjective field study of response to impulsive helicopter

noise

[NASA-TP-1833] p 187 N81-21873

EFFICIENCY

Space Photovoitaic Research and Technology 1985:

High Efficiency, Space Environment, and Array

Technology

[ NASA-CP-2408] p 146 N86-17839

EFFLUENTS

Coordinated aircraft and ship surveys for determining

impact of river inputs on great lakes waters, Remote

sensing results

[NASA-TP-1694] p 149 N80-27832

Report of Workshop on Mount Saint Helena: Its

Atmospheric Effects and Potential Climatic Impact

[NASA-SP-458J p 154 N82-32915

Airborne measurements of launch vehicle effluent:

Launch of Space Shuttle (STS.t) on 12 Aphl 1981

[NASA-TP.2090] p 150 N83-16952

EGRESS

The 15th Aerospace Mechanisms Symposium

INASA-CP-2181] p 130 N81.22388

EIGENVALUES

Eigenvatue/eigenvector assignment using output

feedback

[NASA-TP.1118] p 180 N78-18823

Modal control theory and application to aircraft lateral

handling qualities design

INASA-TP-1234] p 53 N78-25101

Gain selection method and model for coupled propulsion

and airframe systems

[NASA-TP-2067] p 57 N83-11139

A method to stabilize linear systems using eigenvalue

gradient information

[NASA-TP-2479] p 181 N86-13946

Solution of the symmetric eigenproblem AX=lambda

BX by delayed division

[NASA-TP-2514] p 135 N86.20857

EIGENVECTORS

Eigenvalue/eigenvector assignment using output

feedback

{NASA.TP-1118] p 180 N78-18823

Modal control theory and application to aircraft lateral

handling qualities design

[NASA-TP-1234] p 53 N78-25101

EIKONAL EQUATION

Optical-model abrasion cross sections for high-energy

heavy ions

[NASA-TP-1893] p 192 N81-27899

EJECTORS

Workshop on Thrust Augmenting Ejectors

[NASA-CP-2093] p 13 N80-10107

EL NINO

El Nino end outgoing Iongwave radiation: An atlas of

Nimbus-7 Earth radiation budget observations

INASA-RP-1163] p 157 N86-29425

ELASTIC BENDING

An improved transverse shear deformation theory for

laminated entisotropic plates

[NASA-TP-1903] p 130 N82-11488

ELASTIC DEFORMATION

Friction and deformation behavior of single-crystal

silicon carbide

[NASA-TP-1053] p 91 N77-33350

A-41
ELASTIC PLATES SUBJECT INDEX

Measurement of model aaroelastic deformations in the

wind tunnel at transonic speeds using

stereophotogrammetry

[NASA-TP-IOf0] p 31 N76-10048

Simplified method for nonlinear structural analysis

[NASA-TP-2208] p 132 N83-34372

Her'tzlan contact in two and three dimensions

[NASA*TP-2473] p 125 N85-32331

ELAlrTIC PLATES

Noise transmission through plates into an enclosure

[NASA-TP-1173] p 186 N78-23877

Antty_a of _dace cracks in finite pietea under tension

or bending loads

[NASA-TP-1578] p 129 N80-13512

ELASTIC PROPERTIES

Elarltlc consents for supeq_tsstically

formed/d4ffusion-bonded corrugated sandwich core

[NASAoTP-1582] p 129 N80-23677

Fracture toughness of boron/aluminum laminates with

various proportions of 0 deg and plus or minus 45 deg

[NASA-TP-t 707] p81 N81.11115

Elastic-plastic finite.element analyses of thermally

cycled douSe-edge wedge specimens

[NASA.TP-1973] p 130 N82.20566

Development of in situ stiffness properties for shuttle

booatar filament wound case

[NASA-TP-2377] p 83 N84-33521

ELASTIC ticATTERING

Second qusntization techniques in the scattenng of

nonidentical composite bodies

[NASA-TP-2522] p 193 N86-21297

ELASTOHYDRODYNAMICS

Statistical model for aspenty-contact time fraction in

elastohydrodynsmic lubrication

[NASA*TP-1130] p 119 N78-18429

Farrographic anely_s of wear particles from sliding

elastohydrodynamic expenmenta

[NASA-TP-1230] p 119 N78-22377

Minimum film thickness in elliptical contacts for different

regimes of fluid-film lubrication

[NASA-TP-1342J p 119 N76-33447

Comparison of predicted and measured

elastohydrodynsmic film thiokness in a 20-rnillimetar-bore

l_,It beSrm9

[NASA-TP-1542] p 121 N79-32552

Correlation of asperity contact*time fraction with

elastohydrodynamic film thickness in a 2Q-millimeter-bore

pall bearing

[NASA.TP-1547] p 121 N79-33476

Fnctionel heating due to asperity interaction of

eiestohydrodynamic line-contact surfaces

(NASA-TP-1882] p 122 N82-25514

Elastohydrodynamic lubrmation of rectangular contacts

|NASA*TP-2t 11 ] p 123 N83-16759

Regression analysis of traction characteristics of traction

fluids

|NASA-TP-2154] p 123 N83-24862

Elastohydrodynamic COntacts, Effects of dents and

grooves on traction and local film thickness

|NASA-TP-2175[ p 123 N83-28453

Lubrication of machine elements

|NASA-RP-1126| p 124 N84-31640

Surface roughness effects in etastohydrodynam_c

contacts

INASA-TP'2488J p 125 N85-32329

Mechanics of a gaseous film barrier to lubricant wetting

of eiestohydrodynamicsily lubricated conjunctions

[NASA-TP-2500} p 125 N85-32330

ELASTOMERS

Formuietion/cure technology lot ultrahigh molecular

weight silphenylene-siloxane polymers

[NASA.TP-2476] p 96 N85-26990

ELASTOPLASTICI'tW

Comparison of elastic and elastic-plastic structural

analyses for cooled turbine blade airfoils

INASA-TP-167g] p 129 N80-27719

Elastic-plsstic finite-element analyses of thermally

cycled single-edge wedge specimens

(NASA*TP- 1982 _ p 130 N82-20565

Research in structural and solid mechanics, 1982

[NASA-CP-2245 J p 131 N82-33739

Tenth NASTRAN User's CollOquium

[NASA-CP-2249] p 131 N83-12452

ELECTRETS

Research in the use of electrets m measunng effluents

from rocket exhaust of the space shuttle (6.4 percent

scaled model) and Viking 1 launch

|NASA.TP-1073] p 147 N78-11517

ELECTRIC BATTERIES

The 1977 Goddard Space Fhght Center Battery

Workshop

[NASA*CP-2041 ] p 144 N79-21565

The 1979 Goddard Space Flight Center Battery

Workshop

[NASA-CP-2117 J p t45 N80-20820

The 1981 Goddard Space Flight Center Battery

Workshop

[NASA-CP-2217] p 102 N82-20402

ELECTRIC CONDUCTORS

Formulation of electrically conductive thermal.control

coatings

[NASA.TP.1218] p 78 N78-21216

ELECTRIC CONTROL

Single.stage olectrohydrsullc servosystam for actuating

on airflow valve wffh frequencies to 500 hertz

[NASA-TP-1678] p 56 N80.29369

ELECTRIC DIPOLES

Radiating dipole model of interference induced in

spacecraft circuitry by surface discharges

[NASA-TP-2240] p 74 N84-16247

ELECTRIC DIBCHARGES

Effect of hole geometry and Electric-Discharge

Machining |EDM) on airflow rates through small diameter

boles in turbine blade material

[NASA-TP-1716] p 47 N81-12089

LMa test 01 a nickel cadmium t_tt_ with s

protection/recondltioning circuit

[NASA.TP-1873] p 77 N81-24187

ELECTRIC EQUIPMENT

Electrical enclosure hydrogen intrusion study .-. purging

Cape Kennedy Launch Complex 39

(NASA.TP-1461] p lgl N7g.25861

Assessment of Carbon Fiber Electrlcsl Effects

[NASA-CP-2119] p 80 N80.19193

ELECTRIC FIELD6

ton confinement and transport in a tofo_si plasma with

externally imposed radial electric fields

|NASA-TP-1411] p 195 N79.19867

MiG_lte atmosphere electrodynsmica: Report of the

workshop on the Role of the Electrodynamics of the Middle

Atmosphere on Solar Terrestrial Coupling

[NASA-CP-2Og0] p 152 N79.25608

Pockels-effect cell for gas-flow simutabon

[NASA-TP-2007] p 115 N82-23515

Radiating dipole model of interference induced in

spacecraft circuitry by surface discharges

INASA-TP-2240] p 74 N84-16247

Magnetohydrodynamic power generation

[ NASA-TP-2331 ] p 195 N84-25458

Thermosphere Dynamics Workshop, volume 2

[NASA-CP-2389] p 137 N86-29301

ELECTRIC FILTERS

Stability boundaries for systems with frequency-model

feedback and complacency filter

[NASA-TP-1744] p 184 N81-10789

ELECTRIC GENERATORS

Future Orbital Power Systems Technology

Requirements

INASA-CP-2058] p 76 N79-10122

Large Wind Turbine Design Charactenstics and R and

D Requirements

[NASA-CP-2106] p 145 N80-16453

Electric Flight Systems

[NASA-CP-2209] p 3 N82.19134

Energy saving concepts relating to induction

generators

I'NASA-TP-1719] p I46 N82-32859

Aircraft Electric Secondary Power

_NASA-CP-2262| p 50 N64-10055

Technology for Bayton-cycio powerplants using solar

and nuclear energy

[NASA.TP-2558| p 76 N86-21577

ELECTRIC HYBRID VEHICLES

Impact for the 80's: Proceedings of a Conference on

Selected Technology for Susiness and Industry

|NASA-CP-2149J p 212 N81-12978

ELECTRIC MOTOR VEHICLES

Solubdity, stability, and electrochemical studies of

sulfur-sulfide solutions in organic solvents

[NASA-TP-1245] p 144 N78.28624

impact for the 80's: Proceedings of a Conference on

Selected Technology for Business and Industry

[NASA-CP-2149] p 212 N81-12978

ELECTRIC MOTORS

Electric Flight Systems

[NASA-CP-2209] p 3 N82-19134

ELECTRIC NETWORKS

Concept for a power syslem controller for large space

etectncal power systems

{NASA-TP-1939J p 77 N82-t1109

ELEC11RIC POTENTIAL

Verification of computer-aided designs of traveling-wave

tubes utilizing novel dynamic refocusers and graphite

electrodes for the multistage depressed collector

[NASA-TP-2524] p 103 N86-13643

ELECTRIC POWER PLANTS

Capturing energy from the wind

[NASA-SP.455] p 146 N82-28783

ELECTRIC POWER SUPPLIES

Concept report: Microprocessor control of etectncal

power system

[NASA-TP-1016J p 100 N77-30367

Space power subsystem automation technology

INASA-CP-2213J p 77 N82-21254

Aimraft Electric Secondary Power

[NASA-CP-2282] p 50 N84-10055

ELECTRIC PROPULSION

Analysis of costs of gallium arsenide and silicon solar

arrays for apace power applications

|NASA-TP-1811 | p 77 Nat-20173

ELECTRIC SWITCHES

High.voltage, high-power, solid.state remote power

controllers for aerospace applications

[NASA-TP-2437] p 78 N85-21263

ELECTRICAL IMPEDANCE

A new method for determining acoustic-liner admittance

in a rectangular duct with grazing flow from experimental

data

[NASA-TP-2310] p 190 N84-27543

A method for determining acoustic-liner sdmittanca in

ducts with sheared flow in two-cross-secttonsi directions

[NASA.TP.2518] p 190 N86-13056

ELECTRICAL PROPERTIES

Capacitor Technologies. Applications and Reliability

[NASA-CP-2186] p 102 N81-26372

ELECTRICAL RESISTIVITY

Control of volume resistivity in inorganic organic

separators

[NASA.TP-1439| p 84 N79-22246

ELECTRO-OPTICS

Pockets-effect celt for gas-flow simulation

|NASA.TP-2007] p 115 N82.23515

ELECTROCHEMICAL CELLS

Solubility, stability, and electrochemical studies of

solfur-sulfide solutions in organic solvents

|NASA-TP-1245| p 144 N78-28624

The 1980 Godderd Space Flight Center Battery

Workshop

|NASA-CP-2177| p 145 N61-21493

Simulation of lubricating behavior of a thioether liquid

lubricant by an electrochemical method

[NASA-TP-2316] p g5 N84-23764

ELECTROCHEMICAL CORROSION

Galvanic coupling between D6AC steel, 6061-T6

aluminum, Inconel 718 and graphite-epoxy composite

metanal: Corrosion occurrence and prevention

I NASA-TP-2236] p 89 N84-13263

An electrochemical study of the corrosion behawor of

pnmer coated 22t 9-T87 aluminum

[NASA-TP-24591 p 90 N85-22662

ELECTROCHEMISTRY

Secondary aerospace batteries and battery materials:

A bibliography, t969 - 1974

[NASA-SP-7044J p 144 N77-16437

The 1 lth Annual Battery Workshop

[NASA-CP-20881 p 144 N79-28669

The 1979 Goddard Space Flight Center Sattery

Workshop

[NASA-CP-2117] p 145 N80-20820

The variation of corrosion potential with time for coated

metal surfaces

[NASA-TP-26361 p 91 N86-30837

ELECTRODES

Secondary-electron-emission properties of conducting

surfaces with application to multistage depressed

colieclors for microwave amplifiers

INASA-TP-1097| p 86 N78-t1230

Semiconductor photoeiect r oc hemistry

{NASA-TP*2088| p 146 N83-ta024

Performance of computer-designed smell-size

multistage depressed collectors for a high-perveance

traveling wave tube

|NASA-TP-2248_ p 102 N84-15394

Secondary electron emission characteristics of

ion-textured copper and high-purity isotropic graphite

surfaces

[NASA-TP-2342J p 95 N84-28989

Verification of computar-aided designs of traveling-wave

tubes utctizing novel dynamic refocusers and graphite

electrodes for the multistage depressed collector

INASA-TP-2524] p t03 N86-13643

Secondary-electron-emission (osses in multistage

depressed collectors and traveling*wave-tube efficiency

improvements with carbon collector electrode surfaces

[NASA-TP-2622] p t03 N86-32629

ELECTRODYNAMICS

Middle atmosphere electrodynamics: Report of the

workshop on the Role of the Electrodynamics of the Middle

Atmosphere on Solar Terrestna] Coupling

[ NASA-CP-20g0] p 152 N79-25608

Applications of Tethers in Space, volume 2

[ NASA-CP-2365] p 125 N85-20361

A-42
SUBJECT INDEX ENERGY ABSORPTION

Spacecraft Environmental Interactions Technology,

1983

[NASA-CP-2359] p 75 N85-22470

Applications of Tethers in Space: Workshop

proceedings, volume 1

[NASA.CP.2422-VOL-1] p 126 N86-28407

ELECTROLESS DEPOSITION

Electroless-pieting technique for fabricating thin.wail

convective heat-transfer models

[NASA-TP-23491 p 112 N84.31561

ELECTROLYSIS

An electrochemical method for determining hydrogen

concentrations in metals and some applications

[NASA-TP-2113] p 88 N83.16491

ELECTROLYTES

The 1981 Goddard Space Flight Center Batter,/

Workshop

[NASA-CP-2217] p 102 N82-20402

A class of nonidaal solutions 2: Application to

experimental data

[NASA-TP-1930] p 196 N83-23188

ELECTROMAGNETIC ABSORPTION

The optical absorption of trietomic carbon C3 for the

wavelength range 260 to 560 nm

[NASA-TP-1141] p 191 N78-20927

ELECTROMAGNETIC ACCELERATION

Rail accelerators for space transportation: An

experimental investigation

[NASA-TP-2571] p 78 N86-28123

ELECTROMAGNETIC COMPATIBILITY

Design guidelines for assessing and COntrolling

spacecraft charging effects

[NASA.TP.2361 ] p 74 N84-33452

ELECTROMAGNETIC FIELDS

Three-dimensional relativistic field-electron interaction

in a multicavity high-power ktystron 1: Basic theory

[NASA-TP-1992] p 102 N82-22439

ELECTROMAGNETIC INTERACTIONS

Applications of Tethers in Space, volume 2

(NASA-CP-2365] p 125 N85-20361

ELECTROMAGNETIC INTERFERENCE

Carrier-interference ratios for frequency sharing between

frequency-modulated

band television systems

[NASA-TP-1264] p 69 N78-28159

ELECTROMAGNETIC MEASUREMENT

Statistical analysis of direct-strike lightning data (1980

to 1982)

[NASA-TP-2252] p 167 N86-24090

ELECTROMAGNETIC NOISE

DIAL with heterodyne detection including speckle noise:

Aircraft/shuttle measurements of O3, H20, and NH3 with

pulsed tunable CO2 lasers

[NASA-TP-1725] p 115 N80-30717

ELECTROMAGNETIC PULSES

Proceedings of the Workshop on an Electromagnetic

Positioning System in Space

[NASA-CP-2069] p 61 N79-13069

Design guidelines for assessing and controlling

spacecraft charging effects

[NASA-TP-2361 j p 74 N84-33452

ELECTROMAGNETIC RADIATION

RF radiation produced by intracloud lightning

discharges

[NASA-TP-1454] p 160 N79-22708

ELECTROMAGNETIC SHIELDING

Lightning Technology: Proceedings of a technical

symposium

[NASA-CP-2128] p 161 N80-21927

ELECTROMAGNETIC SPECTRA

Skylab EREP investigations summary

[NASA-SP-399] p 136 N79-17279

SETI science working group report

[NASA-TP-2244] p 175 N84-22178

ELECTROMAGNETIC WAVE TRANSMISSION

Proceedings of the Aero-Optics Symposium on

Electromagnetic Wave Propagation from Aircraft

[NASA-CP-2121 ] p 108 N80-25588

ELECTROMECHANICAL DEVICES

The 13th Aerospace Mechanisms Symposium

[NASA-CP-2081J p 128 N79-22539

Flight Technology improvement --- spaceborna optical

radiometric instruments, attitude control, and

etectromechanicat and power subsystems

INASA -CP'21011 p 75 N80-13152

The 17th Aerospace Mechanisms Symposium

[NASA-CP-2273] p 131 N83-24881

ELECTRON BEAMS

Efficiency enhancement of octave-bandwidth traveling

wave tubes by use of multistage depressed collectors

{NASA-TP-1416] p 101 N79-17139

Multistage depressed collector with efficiency of 90 to

94 percent for operation of a dual-mode traveling wave

tube in the linear region

[NASA-TP-1670] p 101 N80-21669

Three-axis electron.beam test facility

[NASA-TP-1836J p 101 N81-20359

Analytical prediction and experimental verification of

performance at various operating conditions of a

dual-mode traveling wave tube with multistage depressed

collectors

[NASA-TP-1831] p 102 N81-28352

ELECTRON BUNCHING

Three-dimensidnat relativistic field-electron interaction

in a multicavity high-power klystron Part 2: Working

Equations

[NASA-TP-2008] p 102 N82.23397

ELECTRON DIFFRACTION

Programs for calculating cell parameters in electron and

X-ray diffraction --- to identity stratospheric aerosols

[NASA-TP-t52g] p 148 N79.30844

ELECTRON DISTRIBUTION

Significant initial results from the environmental

measurements experiment on ATS-6

[NASA.TP-1101] p 65 N78-15142

ELECTRON EMISSION

Secondary-electron-emission properties of conducting

surfaces with application to multistage depressed

collectors for microwave amplifiers

[NASA-TP-1097] p 86 N78-11230

Spacecraft Charging Technology, 1980

[NASA-CP-2182] p 72 N82-t4213

Beam impingement angle effects on secondary electron

emission characteristics of textured pyrolytic graphite

[NASA.TP-2285] p 95 N84.18400

Verification of computer-aided designs of traveling.wave

tubes utilizing novel dynamic refocusers and graphite

electrodes for the multistage depressed collector

[NASA-TP-2524] p 103 N86-13643

Textured carbon on copper: A novel surface with

extremely low secondary electron emission

characteristics

[NASA-TP-2543] p 98 N86-15394

Secondary-electron-emission losses in multistage

depressed collectors and traveling-wave-tube efficiency

improvements with carbon collector electrode surfaces

[NASA-TP-2622] p 103 N86-32629

ELECTRON ENERGY

Multistage depressed collector with efficiency of 90 to

94 percent for operation of a dual-mode traveling wave

tube in the linear region

[NASA-TP-1670] p 101 N80-21669

ELECTRON GUNS

Design of high-perveance confined-flow guns for

periodic-permanent-magnet-focused tubes

[NASA-TP-1485} p 101 N79-27400

ELECTRON IRRADIATION

Spacecraft Charging Technology, 1980

[NASA-CP-2182] p 72 N82-14213

ELECTRON MICROSCOPES

Correction factors for on-line microprobe analysis of

multielement alloy systems

[NASA-RP-10OT] p 86 N78-15236

ELECTRON MICROSCOPY

Scanning-electron-microscope study of

normal-impingement erosion of ductile metals

[NASA-TP-16091 p 87 N80-16141

ELECTRON SCA3-FERING

Three-dimensional relativistic field-electron interaction

in a multicavity high-power klystron. Part 2: Working

Equations

[NASA-TP-2008] p 102 N82-23397

ELECTRON TRAJECTORIES

Three-dimensional relativistic field-electron interaction

in a multicavity hlgh-power klystron, 1: Basic theory

[NASA-TP-19921 p 102 N82-22439

ELECTRON TRANSITIONS

Friction and transfer of copper, silver, and gold to iron

in the presence of various adsorbed surface films

[NASA-TP-1392] p 120 N79-14386

ELECTRONIC COUNTERMEASURES

Experimental venficetion of the multistage depressed

collector design procedure for a high-perveance,

helix-type, traveling-wave tube --- in communications

satellites

[NASA-TP-2182] p 102 N83-25985

ELECTRONIC EQUIPMENT

Lightning protection of aircraft

INASA-RP-1008J p 29 N78-11024

Handbook of sensor technical charactenstics

[NASA-RP-1087J p 115 N82-29877

Development of an instrument for real-time computation

of indicated mean effective pressure

INASA-TP-2238] p 102 N84-16461

Shock response spectra variational analysis for

pyrotechnic qualification testing of flight hardware

INASA'TP-2315] p 74 N84-23676

ELECTRONIC EQUIPMENT TESTS

Three-axis electron-beam test facility

INASA-TP-18361 p 10t N81-20359

ELECTRONIC FILTERS

LANDSAT-4 and LANDSAT-5 multispactrel scanner

coherent noise characterization and removal

[NASA-TP-2595] p 143 N86-31945

ELECTRONIC RECORDING SYSTEMS

Simulated electronic heterodyne recording and

processing of pulsed.laser holograms

[NASA-TP-1444] p 114 N7g-21329

ELECTROPHOTOMETRY

The 1982.1984 Eclipse of Epsifon Aurigee

[NASA-CP-2384] p 203 N86-12188

ELECTROPLATING

An electrochemical method for determining hydrogen

concentrations in metals and some applicetions

[NASA-TP-2113J p 88 N83.16491

ELECTROSLAG REFINING

A mechanical property and stress corrosion evaluatidn

of VIM-ESR-VAR work strengthened and direct double

aged Inconel 718 bar material

[NASA-TP-2634] p 68 N86.30753

ELECTROSTATIC CHARGE

Jupiter probe charging study

[NASA.TP-1263] p 70 N7g.1514g

ELECTROSTATIC PROBES

Development and design of three monitoring instruments

for spacecraft charging

[NASA-TP-f800] p 76 N81-31282

ELEMENTARY PARTICLES

Nineteenth International Cosmic Ray Conference.

Conference papers: Invited redporteur, highlight,

miscellaneous, volume g

[NASA.CP.2376.VOL-9] p 211 N88-31483

ELEVATORS (CONTROL SURFACES)

Experimental and analytical transonic flutter

characteristics of a geared-elevator configuration

[NASA-TP-1666] p 34 N80-25321

ELEVONS

Pressure and thermal distributions on wings and adjacent

scdeces induced by elevon deflections at Mech 6

[NASA.TP-1356] p 106 N79-20344

Aerothermat analysis of a wing-elevon cove with variable

leakage

[NASA-TP-t703] p 108 N80-32692

Aorothermal environment in chordwise gaps between

split elevons at Mach 6.8

[NASA-TP-1783] p 109 N81-15237

ELLIPTIC DIFFERENTIAL EQUATIONS

Solution of elliptic partial differenbal equations by fast

Poisson solvers using a local relaxation factor. 1: O_e-step

method

[NASA-TP-2529} p 183 N86-28661

ELLIPTIC FUNCTIONS

Solution of elliptic partial differential equations by fast

Pdisson solvers using a local relaxation factor. 1 : One.step

method

[NASA-TP-2529] p 183 N86.28661

ELLIPTICITY

Downwash in the plane of symmetry of an etliptically

loaded wing

[NASA-TP-2414] p 25 N85-15693

EMERGENCY LOCATOR TRANSMrn'ERS

Performance of alkaline battery cells used in emergency

Iocetor transmifters

[NASA-TP-2277] p 103 N84-2075g

EMISSION

Pollutant emissions from flat-flame burners at high

pressures

{NASA-TP-1673] p 85 N80-25392

EMISSION SPECTRA

Temperature distributions of a cesium.seeded

hydrogen-oxygen supersonic free jet

[NASA-TP-1162] p 194 N78-20959

An emission-line sunley of the Milky Way

[NASA-SP-434] p 201 N80-11966

B Stars with and without emission lines, parts 1 and 2

[NASA-SP-456] p 200 N82-25027

Molecular clouds and galactic spiral structure

[NASA-TP-2288] p 204 N84-20457

EMII-FANCE

Second Workshop on Spacecraft Glow

[NASA-CP-2391 ] p 201 N86-13239

Oxidation and emittance of superaUoys in heat shield

applications

[NASA-TP-2578] p 90 N86-26412

ENCLOSURES

Electrical enclosure hydrogen intrusion study --- purging

Cape Kennedy Launch Complex 39

[NASA-TP-1461 ] p 191 N79-25861

ENERGETIC PARTICLES

Solar Wind Five

[NASA-CP-2280] p 209 N84-13067

ENERGY ABSORPTION

Intensity and absorbed-power distribution in a cylindrk?_tl

solar-pumped dye laser

[NASA-TP-2321 ] p 118 N84-23878

A-43
ENERGY BUDGETS

ENERGY BUDGETS

Earth Radiation Budget Science, 1975 --conferences

INASA-CP-2100] p 160 N79-32797

Comparison o1 data inversion techniques for remotely

sensed w_de-angie observations of Earth emitted

radiation

INASA-TP-1924] p 164 N82-13620

ENERGY CONSERVATION

An evaluation of the NASA Tech House, including live-in

test results, volume 1

{NASA-TP-1564] p 145 N80-11559

Planning fuel-conservatNe descents in an airline

environmental using a small programmable calculator:

Algorithm development and flight test results

INASA'TP'2393] p 40 N85-26705

Energy efficient transpod technology: Program summary

and bibliography

_NASA-RP-1135] p 37 N55-33116

ENERGY CONVERSION

Summary of atmospheric wind design critana for wind

energy conversion system development

[NASA-TP.t389] p 159 N79.14678

Large Wind Turbine DesKjn Characteristics and R and

D Requirements

[NASA-CP-2106} p 145 N80-16453

Semiconductor photoelectrochemistry

INASA-TP-L:>0881 p 146 N83-18024

Solar-simulator-pumped atomic iodine laser kinetics

[ NASA-TP-2t 821 p 118 N83-32044

Exploratory wind-tunnel invesbgation of a

wingtip-mounted vortex turbine for vodex energy

recovery

[NASA-TP-2468] p 26 N85-26667

ENERGY CONVERSION EFFICIENCY

Solar Cell High Efficiency and Radiation Damage

[NASA-CP-2O20] p 144 N78-13527

Solar Cell High Efficiency and Radiation Damage.

1979

[NASA-CP-2097J p 144 N79-32640

Nuclear-Pumped Lasers --- efficient conversion of

energy liberated in nuclear reactions to coherent

radiation

[NASA-CP-21071 p 117 N80-13435

Multistage depressed collector with efficiency of 90 to

94 percent for operation of a dual-mode traveling wave

tube in the linear region

[NASA-TP-167OJ p 101 N80-21669

Solar power satellite system s=zing tredeoffs

INASA-TF-1804] p 145 N81-18493

ENERGY DISSIPATION

Frictienai heatm 9 due to asperity interaction of

elastohydrodynamic line-contact surfaces

[NASA-TP-1882] p 122 N82-25514

Incidence loss for fan turbine rotor blade in

two.dimens*onel cascade

INASA-TP-2188] p 50 N83-30431

ENERGY METHODS

Application of two design methods for active flutter

suppression and wind-tunnel test results

[NASA-TP-1653] p 129 N80-22737

ENERGY POLICY

Solar Cell High Efficiency and Radiation Damage

[NASA-CP-2020] p 144 N78-13527

Emerging Energy Alternatives for the Southeastern

States

[NASA-CP-20421 p 144 N78.28615

Summary of atmospheric wind design criteria for wind

energy conversion system development

[NASA-TP-1389] p 159 N79.14678

Thermal Energy Storage: Fourth Annual Review

Meeting

[NASA-CP-2125J p 145 N80-22788

Energy sawng concepts relating to induction

generators

[NASA-TP-1719) p 146 N82.3285g

Large Horizontal-Axis Wind Turbnes

[NASA.CP.2230] p 146 N53-19231

Energy: A continuing biblK)graphy with indexes, issue

40. January 1984

[NASA-SP-7043(40)J p 146 N84-21977

ENERGY REQUIREMENTS

Evaluation of s total energy-rata sensor on s transpod

airplane

[NASA-TP-2212| p 40 N84-12164

ENERGY SOURCES

Solar Cell High Efficiency end Radiation Damage

[NASA-CP-2020] p 144 N78-13527

Emerging Energy Alternatives for the Southeastern

States

[NASA-CP-2042) p 144 N78-28615

Proceedings of the National Conference on Energy

Raso_'ce Management. Volume 1: Techniques,

Procedures and Data Bases

JE83-10335) p 141 N83-26155

A-44

Proceedings of the Netionel Conference on Energy

Resource Management. Volume 2: Applications

[E83-t0336J p 142 N83.26176

ENERGY SPECTRA

Ninteenth International Cosmic Ray Conference OG

sessions, volume 2

{NASA-CP-2376-VOL-2J p 210 N85-34006

ENERGY STORAGE

A design handbook for phase change thermal control

and energy storage devices --. selected paraffins

[NASA-TP.t074] p 104 N78-15434

The 1983 Goddard Space Flight Center Batlery

Workshop

[NASA-CP-2331] p 103 N84-33668

An Assessment of Integrated Flywheel System

Technology

[NASA-CP-2346] p 75 N85-13850

ENERGY TECHNOLOGY

Advances in engineering science, volume 3

[NASA-CP-20OI-VOL.3] p 98 N77-10305

Proceedings of the ASPE/MSFC Symposium on

Engineering and Productivity Gains from Space

Technology

[NASA-CP-2019] p 98 N77-30273

Large Wind Turbine Design Characteristics and R and

D Requirements

[NASA-CP-2106] p 145 N80-16453

Thermal Energy Storage: Fourth Annual Review

Meeting

{NASA-CP-2125] p 145 N80-22788

Impact for the 80's: Proceedings of s Conference on

Selected Technology for Business and Industry

[NASA-CP.2149] p 212 N81-12978

Energy: A continuing bibliography with indexes, issue

40, Janoan/1984

[NASA-SP-7043(40)} p 146 N84-21977

ENERGY TRANSFER

An analytical and experimental investigation of s 1+8

by 3.7 meter Freshet lens solar concentrator

[NASA-TP-1005] p t44 N77-30617

A microprocessor-based table Iookbp approach for

magnetic bearing linearizatien

{NASA-TP-1838] p 101 N81-22281

Mean excitation energies for stopping powers in venous

materials using local plasma oscillator strengths

[NASA-TP.2271] p 210 N84-21485

Understanding climate: A strategy for climate modeling

and predictability research, 1955-1995

[NASA-RP-1158| p 166 N86-13866

ENGINE AIRFRAME INTEGRATION

Effects of twin-vedical-tail parameters on twin-angina

afterbody/nozzie aerodynamic characteristics --- Langley

16-fl transonic tunnel tests

[NASA-TP-2158] p 21 N83-24478

A formulation of rotor-airframe coupling for design

analysis of vibrations of helicopter airframes

[NASA-RP-1089] p 133 N84-33832

Aerodynamic characteristics of a high-wing transport

configuration with a over-the.wing nacelle-pylon

arrangement

[NASA-TP-2497J p 27 N86-16193

ENGINE ANALYZERS

Modular instrumentation system for real-time

measurements and control on reciprocating engines

[NASA-TP-1757] p 101 N51-11315

ENGINE CONTROL

Ft00 munivanable control synthesis program:

Evaluation of a multiveriebte control using a real-time

engine simulation

[NASA-TP-1056| p 4t N77-33169

Generation of linear dynamic models from a digital

nonlinear simulation

[NASA.TP-1388] p 2 N79-16796

Propulsion Controls, 1979 --- air breathing engine

control

[NASA-CP.2137| p 47 N81-120go

Space shuttle main engine controller

[NASA-TP-1932] p 178 N82-t1784

Digital Electronic Engine Control (DEEC) Flight

Evaluation in an F-15 Airplane

{NASA-CP-2295] p 52 N86-25342

ENGINE COOLANTS

Three-dimensional turbulent-mixing-length modeling for

discrete-hole coolant injection into a crossflow

[NASA-TP-2200] p t 11 N83-34232

Vortax-generating coolant-flow-passage des_Jn for

Increased film-cooling effectiveness and surface

cevorage

INASA-TP-2388] p 112 N85-12314

ENGINE DESIGN

Effect of fin passage length on optimzation of cylinder

head cooling fins

[NASA-TP-1054J p 104 N77-32432

SUBJECT INDEX

Cold-air pedormance of a tip turbine designed to drive

a lift fan, 3: Effect of simulated fan leakage on turbine

performance

[NASA-TP-ft09J p 7 N78-16001

Cold-sir performance of free-power turbine designed for

112-kilowatt automotive gas-turbine engine. 1 : Design

Stator-vane-chord setting angle of 35 deg

[NASA.TP-1007] p 42 N78-16053

Design and overall performance of four highly loaded.

high speed inlet stages for an advanced high-pressure-ratio

core compressor

[NASA-TP-1337] p 43 N75-33108

The rotary combustion engine: A candidate for general

aviation -- conferences

[NASA-CP-2067] p 44 N79-15961

Aeropropulsion 1979 --- conferences

[NASA.CP-2092] p 45 N50-10205

General Aviation Propulsion

[NASA-CP-2126] p 46 N80-22327

Design and cold-air test of single-stage uncooted turbine

with high work output

[NASA-TP-1680] p 46 N80-25337

Cold-air investigation of a 4 1/2 stage turbine with

stage-loading factor of 4.66 and high spec_c work output,

2: Stage group performance

|NASA-TP-1688] p 47 N80-25338

Conceptual model of turbulent flameholding for ecramlet

combustors

[NASA-TP-15431 p 47 N80-33409

Forward acoustic performance of a model turbofan

designed for a high specific flow (QF-14)

[NASA-TP-1968] p 158 N82-21036

Automated procedure for developing hybrid computer

simulations of turbofan engines Part 1: General

description

[NASA-TP-1851] p 179 N82.33020

F100 multivariable control synthes_s program. Computer

implementation of the F 100 muttiveriable control

aigoflthm

[NASA-TP-2231 ] p 51 N84-11171

Bibliography of Supersonic Cruise Research (SCR)

program from 1980 to 1983

[NASA-RP-1117] p 24 N84-27674

ENGINE FAILURE

Effects of visual and motion simulation cueing systems

on pilot performance during takeoffs with engine failures

[NASA-TP-1365} p 32 N79-14082

Effects of inlet distortion on a static pressure probe

rod,unfed on the engine hub in an F-15 airplane

[NASA-TP-241 t ] p 52 N85-22394

ENGINE INLETS

Theoretical study of VTOL tilt.nacelle axisymmetric inlet

geometries

[NASA-TP-1380] p 10 N79.14996

Experimental evaluation of a spinning.mode

acoustic-treatment design concept for aircraft inlets ---

suppression of YF-102 engine fan noise

[NASA-TP-1613] p 46 N80-21323

Experimental investigation of the radiation of sound from

an unflanged duct and a bellmouth, including the flow

effect

[NASA-TP-1697] p 157 N80-32188

Low.speed aerodynamic performance of

5O.8-centimeter-dlameter noise-suppressing inlets for the

Quiet, Clean, Shod-haul Experimental Engine (QCSEE) ---

Lewis 9- by 15-foot low speed wind tunnel tests

[NASA-TP-t178] p47 Nat-11037

Numencal analysis of the scramiet-iniet flow field by

using two-dimens_onal Navler-Stokes equations

[NASA-TP-1940] p 48 N82-13142

Preliminary tests of an advanced high-temperature

combustion system

[NASA-TP-2203] p 50 N83-33593

Theoretical and experimental engine-inlet flow fields for

tighter forebodies

{NASA-TP-2270] p 23 N84-17132

Experimental investigation of tangential blowing applied

to a subsonic V/STOL inlet

[NASA-TP-2297] p 23 N84-20493

Effect of underwing aft-mounted nacelles on the

longitudinal serodynarmc characteristics of a high-wing

transport airplane

[NASA-TP-2447| p 27 N86-20345

ENGINE MONITORING INSTRUMENTS

Modular instrumentation system for real-time

measurements and control on reciprocating engines

[NASA-TP-1757] p t01 N81-11315

Aircraft Engine Diagnostics

INASA-CP-2190] p48 N81-31196

Development of an instrument for real-time computation

of indicated mean effective pressure

[NASA-TP-2238] p 102 N84-16461

Advanced High Pressure O2/H2 Technology

(NASA-CP-2372] p 78 N85-26862
SUBJECT INDEX

ENGINE NOISE

Measurements and predictions of flyover and static noise

of a TF30 afferburning turbolan engine

INASA-TP-1372] p 43 N79-13046

Experimental investigation of the radiation of sound from

an unflanged duct and a bellmouth, including the flow

effect

[NASA-TP-1697} p 187 N80-32188

Noise suppression characteristics of peripherally

segmented duct liners

[NASA-TP-19041 p 188 N81-33946

Forward acoustic performance of a model turbofan

designed for a high specific flow (QF-14)

[NASA-TP-1968| p 188 N82-21036

Fluctuating pressures on fan blades of a turbofan engine:

Static and wind-tunnel investigations

{NASA-TP-19761 p 168 N82-21037

Airport/Community Noise

[NASA-CP-2241 ] p 188 N82-31070

Flight effects of fan noise

[NASA-CP-2242} p 169 N83-10883

Study of stator-vane fluctuating pressures in a turbofan

engine for static and flight tests

[NASA-TP-2217] p 189 N84-22363

ENGINE PARTS

Extension of similarity test procedures to cooled engine

components with insulating ceramic coatings

[NASA-TP-1615] p 108 N80-24577

Elastic-plastic finite-element analyses of thermally

cycled double-edge wedge specimens

{ NASA-TP-t 973 ] p 130 N92-20666

Advanced High Pressure O2/H2 Technology

{NASA-CP-2372J p 78 N95-26862

Turbine Engine Hot Section Technology (HOST)

{NASA-CP-2289| p 135 N86-11495

Aeronautical facilities catalogue. Volume 2: Airbreathing

propulsion and flight simulators

[NASA-RP-1133] p 60 N86-18328

ENGINE STARTERS

Reasons for low aerodynamic performance of

135-centimeter-tip-diameter aircraft engine starter

turbine

[NASA-TP-1810] p 48 N81-20076

ENGINE TESTS

Effect of slotted casing treatment with change in

Reynolds number index on performance of a jet engine

[NASA.TP-1058] p 41 N77-32154

Altitude calibration of an Ff 00, SiN P680063, turbofan

engine

[NASA-TP-t 228] p 42 N78-23095

Evaluation of a simplified gross thrust calculation

technique using two prototype F100 turbofan engines in

an altitude facility

[NASA-TP-1482] p 44 N79-26057

Aerodynamic performance of axial-flow fan stage

operated at nine inlet guide vane angles --- to be used

on vertical lift aircraft

[NASA-TP.1510] p 45 N79-31214

Static and transient performance of YF-t 02 engine with

up to 14 percent core airbleed for the quiet short-haul

research aircraft

[NASA-TP-1692] p 47 N80-26339

Aircraft Engine Diagnostics

NASA-CP-2fg0} p 48 N81-31196

Test-engine and inlet performance of an aircraft used

for investigating flight effects on fan noise

NASA-TP-2264] p 189 N84-21277

Study of stator-vane fluctuating pressures in a turbofan

engine for static and flight tests

NASA-TP-2217] p 189 N84-22363

integrated exhaust gas analysis system for aircraft

turbine engine component testing

NASA-TP-2424| p 116 N85-16100

Aeronautical facilities catalogue. Volume 2: Airbreathing

propulsion and flight simulators

NASA-RP-1133} p 60 N86-18328

ENGINEERING

Advances in engineering science, volume 3

NASA-CP-200f-VOL-3] p 98 N77-10305

ENTHALPY

A class of nonideal solutions. 1: Definition and

properties

[NASA-TP-f929J p 196 N63-23169

ENTRAINMENT

Viscous-inviscid calculations of jet entrainment effects

on the subsonic flow over nozzle afferbodies

[NASA-TP-1626] p 14 N60-22261

ENTRY GUIDANCE (STS)

Shuttle Performance: Lessons Learned, part 1

[NASA-CP-2283-PT-t ] p 69 N84-10115

Shuttle Performance: Lessons Learned, part 2

[NASA-CP-2293-PT-2] p 69 N84-10144

ENVIRONMENT EFFECTS

An assessment of the effect of supersonic aircraft

operations on the stratospheric ozone content

[NASA-RP-1026] p 159 N78-30774

Environmental analysis of the chemical release module

--- space shuffle payload

INASA-TP-1750J p 209 N61-13912

Two-dimensional model studies of the effect of

supersonic a=rcraft operations on the stratospheric ozone

content

INASA-RP-1064] p 149 N81-17622

Report of Workshop on Mount Saint Helena: Its

Atmospheric Effects and Potential Climatic impact

I NASA-SP-4581 p t 54 N62-32915

Atmospheric Effects and Potential Climatic Impact of

the 1980 Eruptions of Mount St. Helena

I NASA-CP-22401 p 136 N63-11534

Airborne measurements of launch vehicle effluent:

Launch of Space Shuttle (STS-1) on 12 April 1981

[NASA-TP-2O90] p 150 N83-16952

Procedure for estimating orbital debris risks

INASA-TP-2507J p 69 N65-33169

High Temperature Polymer Matrix Composites

I NASA-CP-2385] p 83 N86-11260

ENVIRONMENT MODELS

Advances in engineering science, volume 3

INASA-CP-200t-VOL-3] p 98 N77-10305

Understanding climate: A strategy for climate modeling

and predictability research, 1985-1995

[NASA-RP-1158_ p 166 N86-13866

ENVIRONMENT POLLUTION

Man's impact on the troposphere: Lectures in

tropospheric chemistry

{NASA-RP-1022} p 151 N79-10634

Analytic model for washout of HCI(g) from dispersing

rocket exhaust clouds

[NASA-TP-1601 I p 149 N81-24601

ENVIRONMENTAL CONTROL

Electric Flight Systems

[ NASA-CP-22091 p3 N82-t9134

Orbiting quarantine facility. The Antaeus report

[NASA-SP-454] p 66 N62-20225

ENVIRONMENTAL MONITORING

Significant initial results from the environmental

measurements experiment on ATS-6

[NASA-TP-1101] p 65 N78-15142

Investigation of effects of background water on upwelled

reflectance spectra and techniques for analysis of dilute

primary-treated sewage sludge

[NASA-TP-1446] p 168 N79-28864

Reporf of the NASA working group on tropospheric

program planning

[NASA-RP-t062} p 153 N61.23742

Applications systems verification and transfer project.

Volume 1: Operational applications of satellite snow cover

observations: Executive summary --- usefulness of satellite

snow-cover data for water yield prediction

[NASA-TP.1822] p 140 N62-20617

Applications systems verification and transfer project.

Volume 2: Operational applications of satellite snow-cover

observations and data-collection systems in the Arizona

test site

[NASA-TP-1823] p 140 N82-20618

Applications systems verification and transfer project.

Volume 6: Operational applications of satellite snow-cover

observations NOAA/NESS support study

[NASA-TP.1827] p 140 N82-20622

Proceedings of the National Conference on Energy

Resource Management. Volume 2: Applications

[E83-10336] p 142 N83-26176

Present state of knowledge of the upper atmosphere:

An assessment report; processes that control ozone end

other climatically important trace gases

[NASA-RP-1162j p 166 N86-25911

ENVIRONMENTAL QUALITY

Time-of-Day Corrections to Aircraft Noise Metrics

[NASA-CP-2136] p 187 N80-26150

ENVIRONMENTAL SURVEYS

Application of Remote Sensing to the Chesapeake Bey

Region Volume 2: Proceedings

{NASA-CP-O06-PT-2} p 138 N78-21526

Quantitative mapping by remote sensing of an ocean

acid.waste dump

[NASA-TP-1275J p t47 N78-33617

ENVIRONMENTAL TESTS

MARS 1414 recorder environmental tests

{NASA-TP-1709} p 115 N80-30716

Effects of environment on microhardness of magnesium

oxide

[NASA-TP-2002} p 95 N82-22366

EPOXY MATRIX COMPOSITES

Tough Composite Materials

[NASA-CP-2334] p 83 N85-12941

EPOXY RESINS

Moisture diffusion parameter characteristics for epoxy

composites and neat resins

{NASA-TP-14741 p 80 N79-29241

Tribological characteristics of a composite total-surfaca

hip replacement

{NASA-TP-16531 p 94 N82-16239

ERROR DETECTION CODES

Failure mechanics in low-velocity impacts on thin

composite plates

[NASA-TP-2152} p 62 N63-24562

EQUATIONS OF MOTION

Planar equations of roliout motion for an aircraft with

free or steerable landing gears

[NASA-TP-1984] p 35 N62-23244

Theoretical method for calculating relative joint geometry

of assembled robot arms

[NASA-TP-2155] p 182 N83-25438

Transition in Turbines

[NASA-CP-2386} p 113 N65-31433

Space station rotational equations of motion

{NASA-TP-2611 ] p 68 N85-34148

EQUIPMENT SPECIFICATIONS

An optical profiiometer for spatial characterization of

three-dimensional surfaces

INASA-TP-1012} p 113 N77-32458

Spacecraft transmitter reliability

INASA-CP-2159] p 76 N81-f6t 19

Handbook of sensor technical characteristics

I NASA-RP-1087 ] p 115 N82-29577

EREP

Skylab EREP investigations summary

INASA-SP-399} p 136 N79-17279

EROSION

Hydrogen film cooling of a smalt hydrogen-oxygen thrust

chamber and its effect on erosion rates of various ablative

materials

[NASA-TP-t098] p 76 N78-13124

Scanning-elect ton- microscope study of

normal-impingement erosion of ductile metals

[NASA-TP-1609} p 87 NS0-t6141

Effects of erodant particle shape and various heat

treatments on erosion resistance of plain carbon steel

{NASA-TP-1755] p 87 N81-162t0

Universal approach to analysis of cavitation and

liquid-impingement erosion data

[NASA-TP-2061] p 88 N83-15413

Morphology of an aluminum alloy eroded by a let of

angular particles impinging at normal incidence

[NASA-TP-2139] p 69 N83-24641

Time dependence of solid-particle impingement erosion

of an aluminum alloy

[NASA-TP.2169| p 8g N83-32908

Cavitation pitting and erosion of aluminum 6061-T6 in

mineral oil water

[NASA.TP-2146] p 123 N63-35400

Erosion of iron-chromium alloys by glass particles

[NASA-TP-2354] p 90 N84-28965

Empirical re{ations for cavitation and liquid impingement

erosion processes

[ NASA-TP-2339] p 90 N84-31349

Characterization of erosion of metallic matedals under

cavitation attack in a mineral oil

[NASA-TP-2368] p 124 N64o32825

High-temperature erosion of plasma-sprayed,

yftda.stabilized zirconia in a simulated turbine

environment

[NASA.TP-2406] p 96 N65.13045

ERROR ANALYSIS

Effects of errors on decoupled control systems

[NASA-TP-11841 p 53 N78-27138

Instrument error analysis as it applies to wind-tunnel

testing

[NASA-TP-1572] p 114 N80-13430

Aliased noise in radiometric measurements

[NASA-TP-1639] p 114 N80-22660

Pitfalls and guidelines for the numerical evaluation of

moderate-order system frequency response

[NASA-TP-1814] p 72 N61-25136

Design and analysis of a torsion braid pendulum

displacement transducer

[NASA-TP-1840] p 115 N8t-25352

Ozone Trend Detectability

[NASA-CP-2189] p 153 N82-10624

Establishment of a rotor model basis

[NASA-TP-2026] p 36 N62-29311

ERROR CORRECTING CODES

Fault tolerant computing: A preamble for assuring

viability of large computer systems

[NASA-TP-f0671 p 177 N77-33868

Correction factors for on-line microprobe analysis of

multietement alloy systems

[NASA-RP-IO06I p 66 N78-15236

A decoding procedure for the Reed-Solomon codes

[NASA-TP-1286] p 180 N78-30862

ERROR DETECTION CODES

Fault tolerant computing: A preamble for assuring

viability of large computer systems

[NASA-TP-f067] p 177 N77-33868

Concurrent error detecting codes for arithmetic

processors

[NASA-TP-1528] p 177 N79-30947

A-45
ERROR FUNCTIONS

Vahdation Methods Research for Fault-Tolerant Avionics

and Control Systems: Working Group Meeting, 2

{NASA-CP-2f30J p 176 N80-23008

High-density digital recording

[NASA-RP-1111J p 103 N86-14498

ERROR FUNCTIONS

Ozone Trend Detectability

[NASA.CP.2189} p 153 N82-10624

ERRORS

Results of the first complete stalie calibration ol the

RSRA rotor-_oad-measurement system

[NASA-TP-2327] p 37 N84-31111

Orifice-induced pressure error studies in Langley 7- by

10-foot high-speed tunnel

{NASA-TP-2545] p 27 N86-20347

The application to airfoils of a technique for reducing

orifice-induced pressure error at high Reynolds numbers

{NASA-TP-2537J p 27 N86-20351

Effects of model error on control of large flexible space

antenna with comparisons of decoupled and linear

quadratic regulator control procedures

[NASA-TP-2604} p 75 N86-30801

ESCAPE SYSTEMS

The 15th Aerospace Mechanisms Symposium

[NASA-CP-2181J p 130 N81-22388

Service life evaluation of rigid explosive transfer lines

[NASA-TP-2143J p 36 N83-31596

ESSA 7 SATELLITE

Analyses of earth radiation budget data from unrestricted

broadband radiometers on the ESSA 7 satellite

{NASA-TP-t4021 p 180 N79-22709

ESTERS

Analysis of a MIL-L-27502 lubricant from a gas-turbine

engine test by size-exclusion chromatography

[NASA-TP-2063] p 95 N83-18528

ESTIMATES

Estimation of attainable _eading-edge thrust for wings

at subsonic and supersonic speeds

{NASA-TP-15001 p 12 N80-10105

Procedure for estimating orbital debris risks

{ NASA-TP-2507} p 69 N85-33169

ESTIMATING

Effects of control inputs on the estimation of stabdity

and control parameters of a light airplane

[NASA-TP-1043] p 53 N78-13071

Convective rainfall estimation from digital GOES-1

infrared data

INASA-RP-t034] p 160 N79-31885

ESTUARIES

Chesapeake Bay Plume Study: Superflux 1980

{NASA-CP-2188} p 168 N82-10661

Measurements of spectral attenuation coefficients in the

lower Chesapeake Say

[NASA-TP-2130] p 168 N83-24133

Literature review of organic matter transport from

marshes

[E83-10352} p 142 N83-29750

ETHERS

Thermal and oxidative degradation studies of formulated

C-ethers by gel-permeation chromatography

[NASA-TP-19941 p 94 N82-21332

ETHYL ALCOHOL

Axial jet mixing of ethanol in cylindrical containers during

weightlessness

{NASA-TP-14871 p 97 N79-28350

EULER EQUATIONS OF MOTION

Surrogate-equation technique for simulation of steady

inv1⁄4scid flow

INASA-TP-1886} p 18 N81-31129

Comparison of two- and three-dimensional flow

computations with laser anemometer measurements in a

transonic compressor rotor

t NASA-TP-1931 ] p 22 N83-32774

A comparative study of the nonunlqueness problem of

the potential equation

[NASA-TP-2385J p 25 N85-15694

EUTECTIC ALLOYS

Wear of aluminum and hypoeutectic aluminum-silicon

alloys in boundary-lubricated pin-on disk sliding

|NASA-TP-1442J p 87 N79-21184

EUTECTICS

Feasibility study of tungsten as a diffusion barrier

between nickel-chromium-aluminum and Gamma/Gamma

prime - Delta eutectic alloys

[NASA-TP-11311 p86 N78-15230

EVALUATION

Evaluation of a computer-generated perspective lunne_

display for flight path following

INASA-TP-17361 p 39 N81-13958

An evaluation and comparison of verticat profile data

from the VISSR Atmosphenc Sounder (VAS)

{NASA-TP-24251 p t66 N85-16351

Fabrication and evaioation of superptastically

formed/weld-brazed corrugated compression panels with

beaded webs

INASA-TP-2512i p 90 N86-13406

A-46

Experimental evaluation of two turning vane designs for

high-speed corner of 0 t-acute modet of NASA Lewis

Research Center's proposed attitude wind tunnel

{NASA-TP-25701 p 60 N86-28101

EVAPORATION

Friction and hardness of gold films deposited by ion

plating and evaporation

{NASA-TP-2207] p 89 N83-34019

EVAPOTRANSPIRATION

Remote Sensing of Snow and Evapotranspiration

[NASA-CP-2363] p 143 N85-23223

EVOLUTION (DEVELOPMENT)

Fronts and frontogenesis as revealed by high time

resolution data

{NASA-RP-IO051 p 158 N77-30705

The Soviet-American Conference on Cosmochemistry

of the Moon and Planets, part 2

[NASA-SP-3?0-PT-2] p 203 N78-12958

Gamma Ray Astrophysics: New insight into the

universe

I NASA-SP-453 j p 204 N82-21118

The evolution o1 complex and higher organisms

INASA'SP-478] p 169 N85-32708

EXCHANGING

Global Biology Research Program: Biogeochemica_

Processes in Wetlands

[NASA-CP-2316t p 169 N84-30665

EXCITATION

Laboratory tank studies of a single species ol

phytoptankton using a remote sensing fluorosensor

{NASA-TP-t821 I p 139 N81-20492

Mean excitation energies for stopping powers in various

materials using local plasma oscillator strengths

I NASA-TP-2271 } p 210 N84-21485

EXHAUST DIFFUSERS

An experimental investigation of two large annular

diffusers with swirling and distorted inflow

[NASA-TP-16281 p 14 N80-17984

EXHAUST EMISSION

Analysis of effect of flameholder characteristics on lean,

premixed, partially vaporized fuel-air mixtures quality and

nitrogen oxides emissions

INASA-TP-1842] p 48 N81-24065

Effect of fuel-air-ratio nonuniformity on emissions of

nitrogen oxides

[NASA-TP-1798] p 48 N82-13143

Effect el flameholder pressure drop on emissions and

pedormance of premixed-prevaponzed combustors

[NASA-TP-2131 I p 50 N83-23309

Airborne measurements of launch vehicle effluent of

STS-2 launch on November 12, 1981 at Cape Canaveral,

Florida

[NASA-TP-2260] p 150 N84-18764

EXHAUST FLOW SIMULATION

Effect of a simulated engine jet blowing above an arrow

wing at Much 20

INASA-TP-t050] p 6 N78-10030

Effects of sidewall geometry on the installed

performance of nonaxisymmetric convergent-divergent

exhaust nozzles

[NASA-TP-1771 I p 18 N81-f5976

EXHAUST GASES

Aircraft Piston Engine Exhaust Emission Symposium

JNASA-CP-2005J p 41 N77-17081

Aircraft engine emissions --- conference

INASA-CP-202t ] p 41 N78-11063

Effects of entrained water and strong turbulence on

afferburning within solid rocket motor plumes

[NASA-TP-1111] p 147 N78-15596

Thermodynamic and chemical parameters of the

exhaust effluents from the HARPOON booster motor

[NASA-TP-1280} p 147 N78-28682

Effect of swider-mounted mixing venturi on emissions

of flame-tube combustor using jet A fuel

INASA-TP-13931 p 44 N79-14099

Effect of primary-zone equivalence ratio on pollutant

formahon

I NASA-TP-1463J p 44 N79-23086

Effect of degree of fuel vaporization upon emissions

for a premixed partially vaporized combustion system -

for gas turbine engines

{ NASA-TP-1582 j p46 N80-14125

Pollutant emissions from fiat-flame burners at high

pressures

INASA-TP-t673J p 85 N80-25392

Low-pressure performance of annular, high-pressure (40

aim) high-temperature (2460 K) combustion system

I NASA-TP-1713J p47 N80-32396

Performance tests of a gas blending system based on

mass-flow controllers

[NASA-TP-1896] p 97 N81-29246

Venturi nozzle effects on fuel drop size and nitrogen

oxide emissions

INASA-TP-20281 p 49 N82-31329

SUBJECT INDEX

Integrated exhaust gas analysis system for aircraft

turbine engine component testing

{NASA-TP-2424] p 116 N85-16100

EXHAUST NOZZLES

Experimental and analytical investigation of a

nonaxlsymmetric wedge nozzle at static conditions

{NASA-TP-1188} p 8 N78-26109

Fuselage and nozzle pressure distributions on a

1/12-scale F-15 propulsion model at transonic speeds ---

conducted in langley 16 foot transonic tunnet

INASA-TP-1521] p 13 N80-11036

Turbojet-exhaust-nozzle secondary-airflow pumping as

an exit control of an inlet-stability bypass system for a

Mach 2.5 axisymmetric mixed-compression inlet --- Lew*s

10- by 10-if supersonic wind tunnel test

{ NASA-TP- t 532} p46 N80-14124

Effects of sidewall geometry on the installed

performance of nonaxisymmetric convergent-divergent

exhaust nozzles

[NASA-TP-1771 } p 16 N81-15976

Static internal performance o! single expansion-ramp

nozzles with thrust vectoring and reversing

[NASA-TP-1962] p 19 N82-20156

Static internal performance characteristics ol two thrust

reverser concepts for axisymmetric nozzles

[NASA-TP-20251 p 20 N82-26235

Thrust performance of a variable-geometry, divergent

exhaust nozzle on a turbojel engine at attitude

{NASA-TP-2171 } p 50 N83-26839

FPuid shielding of high-velocity jet noise

{NASA-TP-22591 p 189 N84-15894

EXHAUST SYSTEMS

Static test-stand performance of the YF-102 turbofan

engine with several exhaust configurations for the Quiet

Short-Haul Research Aircraft (QSRA)

[NASA-TP-1556] p 45 N80-14121

EXISTENCE THEOREMS

Existence and uniqueness of solutions to a class of

nonlinear-operator-differential equations arising in

automated spaceship navigation

{NASA-TP-18601 p 70 N81-23182

EXOBIOLOGY

Life in the Universe

I NABA-CP-2156] p 175 N82-20884

The tst Symposium on Chemical Evolution and the

Origin and Evolution of Life

INASA-CP-22761 p 79 N83-24556

NASA Space Biology Program. Eighth annual

symposium's program and abstracts

[NASA-CP-2299J p 169 N84-18829

The cosmic history of the biogenic elements and

compounds

i NASA-SP-476J p 175 N85-28562

Search for the universal ancestors

INASA-SP-477] p 175 N85-32777

Aerospace Medicine and Biology: A Cumulative Index

to the 1985 Issues

[ NASA-SP-7011(280) j p 170 N86-23285

Second Symposium on Chemical Evolution and the

Origin of Life

[NASA-CP-2425J p 175 N86-26844

EXPANSION

Experimental perfect-gas study of expansion-lube flow

characteristics

{NASA-TP-1317J p 106 N79-14327

EXPERIMENT DESIGN

The use of nonhuman primates in space

[NASA-CP-005] p 169 N78-11663

The t3th Aerospace Mechanisms Symposium

INASA-CP-2081 ] p 128 N79-2253g

Space plasma physics active experiments

{NASA-CP-2165] p 212 N81-14944

Spacecraft Dynamics as Related to Laboratory

Experiments in Space --- conference

i NASA-CP-21991 p 72 N82-12t09

Finite-difference fluid dynamics computer mathematical

mode_s for the design and interpretation of experiments

for space fight --- atmospheric general circulation

experiment, convection in a float zone, and the

Bridgman-Stockbarger crystal growing system

r NASA-TP-2323 } p 112 N84-23852

Living and working _n space A history of Skyiab

INASA-SP-42081 p 63 N84-25737

EXPERIMENTATION

Experimental evaluation of two turning vane designs for

high-speed corner of 0 l-scale model of NASA Lewis

Research Center's proposed altitude wind lunnel

I NASA-TP-2570] p 60 N86-28101

EXPLORER SATELLITES

Meteoroid bumper experiment on Explorer 46

[NASA-TP-18791 p 72 N81-29155

The 1985 Get Away Special Expehmenter's

Symposium

I NASA-CP-2401 I p 63 N86-27297
SUBJECT INDEX FANS

EXPLOSIVES

Service life evaluation of rigid explosive transfer lines

INASA-TP-2143] p 36 N83-31596

EXPONENTIAL FUNCTIONS

Simulation study of the power of the

Kolmogoroff-Smirnoff and Z tests for the exponential

distribution

[NASA-TP-1311] p 183 N78-31854

EXPOSURE

Spectroscopic analysis of radiation-generated changes

in tensile properties of a potyetherimide film

[NASA-TP-2429] p 83 N85-25435

EXTENSIONS

Theoretical parametric study of the relative advantages

of winglets and wing-tip extensions

[NASA-TP-1020] p 5 N77-33112

EXTERNAL STORES

Effects of stores on longitudinal aerodynamic

characteristics of a fighter at supersonic speeds

[NASA-TP-1175} p 8 N78-22028

EXTERNAL TANKS

Preliminary vibration, acoustic, and shock design and

test criteria for components on the Lightweight External

Tank (LWT)

[NASA-RP-1074] p 71 N81-19218

Vibration, acoustic, and shock design and test criteria

for components on the Solid Rocket Boosters (SRB),

Lightweight External Tank (LWT), and Space Shuttle Main

Engines (SSME)

(NASA-RP-tt27J p 134 N85-10405

EXTERNALLY BLOWN FLAPS

Aeroacouslic performance of an externally blown flap

configuration with several flap noise suppression devices

[NASA-TP-1995] p 188 N82-24942

EXTINCTION

SAM 2 Measurements of the Polar Stratospheric

Aerosol, volume 2 April 1979 to October 1979

[NASA-RP-1088-VOL-2| p 153 N82-19734

SAM II measurements of the polar stratospheric aerosol

Volume 6: April to October 1981

INASA-RP-1141 ] p 155 N85-27422

SAM 2 measurements of the polar stratospheric aerosol,

volume 2

[NASA-RP-1164] p 157 N86-28562

SAM 2 measurements of the polar stratospheric aerosol,

volume 8

[NASA-RP-1165] p t57 N86-29428

EXTRAPOLATION

MEGA16 - Computer program for analysis and

extrapolation of stress-rupture data

{NASA-TP-1809J p 130 N81-23486

EXTRASOLAR PLANETS

An Assessment of Ground-Based Techniques for

Detecting Other Planetary Systems. Volume 2: Position

papers

[NASA-CP-2124-VOL-21 p 201 N80-25224

Project Orion: A design study of a system for detecting

extraselar planets

[NASA-SP-436] p 206 N80-27260

EXTRATERRESTRIAL LIFE

On the habitability of Mars: An approach to planetary

ecosynthesis

[NASA-SP-414] p t75 N77-12718

The search for extraterrestnal intelligence (SETI)

[NASA-SP-419] p 175 N78-18771

A bibliography on the search for extraterrestrial

intelligence

{NASA-RP-1021 ] p 199 N78-21019

Life in the Universe

[NASA-CP-2156] p 175 N82-20884

The 1st Symposium on Chemical Evolution and the

Origin and Evolution of Life

[NASA-CP-2276] p 79 N83-24556

EXTRATERRESTRIAL RADIATION

Spectroscopic analysis of radiation-generated changes

in tensile properties of a polyetherimide film

[NASA-TP-2429] p 83 N85-25435

Ninteenth International Cosmic Ray Conference

Conference program and author index

[NASA-CP-2376] p 210 N85-33901

Nineteenth International Cosmic Ray Conference

papers, General index, volume 10

[NASA-CP-2376-VOL-10J p 211 N88-28904

EXTRATERRESTRIAL RESOURCES

Summer Workshop on Near-Earlh Resources

[NASA-CP-2031 J p 205 N78-16973

EXTRAVEHICULAR ACTIVITY

The 15th Aerospace Mechanisms Symposium

[NASA-CP-218t I p 130 N8f-22388

EVA assembly of large space structure element

[NASA-TP-1872] p 62 N81-28180

EXTRAVEHICULAR MOBILITY UNITS

A mobile work station concept for mechanically aided

astronaut assembly of large space trusses

[NASA-TP-2108] p 74 N83-19806

Swing-arm beam erector (SABER) concept for single

astronaut assembly Of space structure

[NASA-TP-2379] p 75 N85-19015

EXTREMUM VALUES

Statistical analysis ol direct-strike lightning data (1980

to f 982)

[NASA-TP-22521 p 167 N86-24090

F

F-100 AIRCRAFT

Airflow and thrust calibration of an F100 engine, SIN

P680059, at selected flight conditions

[NASA-TP-1069] p 42 N78-21112

Altitude calibration of an Ft00, S/N P680063, turbofan

engine

[NASA-TP-t228J p 42 N78-23095

F-102 AIRCRAFT

Experimental evaluation of a spinning-mode

acoustic-treatment design concept for aircraft inlets ---

suppression of YF-t 02 engine fan noise

INASA-TP-1613] p 46 N80-21323

F-106 AIRCRAFT

Lightning attachment parlerns and flight conditions for

storm hazards, 1980

[NASA-TP-2087] p 30 N83-14077

F-111 AIRCRAFT

Flight-measured buffet characteristics of a supercritical

wing and a conventional wing on a variable-sweep

airplane

[NASA-TP-1244] p 8 N78-23056

Flight-determined stability and control derivatives for the

F-111 Tact research aircraft

INASA-TP-1350J p 54 N79-10068

Measurements and predictions of flyover and static noise

of a TF30 afterburning turbofan engine

{NASA-TP-1372] p 43 N79-13045

Flight comparison of the transonic agility of the F-111A

airplane and the F-1 f 1 supercritical wing airplane

[NASA-TP-13681 p 54 N79-13056

Application of a performance modeling technique to an

airplane with variable sweep wings

[NASA-TP-18551 p 35 N81-24048

F-15 AIRCRAFT

Development of systems and techniques for landing an

aircraft using onboard television

[NASA-TP-t 171 I p 32 N78-20114

Flight evaluation of a simplified gross thrust calculation

technique using an F100 turbofan engine in an F-15

airplane

{ NASA-TP-1782 } p 48 N81-15000

Effect of simulated in-flight thrust reversing on

vertical-tail loads of F-18 and F-15 airplane models ---

conducted in the Langley 16-foot transonic tunnel

INASA-TP-1890I p 18 N81-30086

In-flight transition measurement on a 10 deg cone at

Mach numbers from 0 5 to 2.0

[NASA-TP-1971} p 19 N82-26227

Effect of nozzle and vertical-tail variables on the

performance of a 3-surface F-15 modet at transonic Mach

numbers --- Langley 16 foot transonic tunnel

INASA'TP'20431 p 20 N82-32320

Effect of thrust reverser operation on the

lateral-directional characteristics of a three-surface F-15

model at transonic speeds

[NASA-TP-2234J p 22 N84-13165

Effects of inlet distortion on a static pressure probe

mounted on the engine hub in an F-15 airplane

[NASA-TP-2411 ] p 52 N85-22394

Digital Electronic Engine Control (DEEC) Flight

Evaluation in an F-t 5 Airplane

tNASA-CP'22981 p 52 N86-25342

F-1S AIRCRAFT

Effects of stores on longitudinal aerodynamic

characteristics of a fighter at supersonic speeds

[NASA-TP-1175] p 8 N78-22028

Simulator study of stalf/post-stall characteristics of a

fighter airplane with relaxed longitudinal static slabilii_ ---

F-16

{NASA-TP-15381 p 55 N80-14138

F-I 7 AIRCRAFT

Precision controllability of the Y F-17 airplane

{NASA-TP-1677 ] p 55 N80-23327

F-18 AIRCRAFT

Investigation of axisymmetric and nonaxisymmetric

nozzles installed on a 010 scale F-t8 prototype airplane

model --- wind tunnel tests

INASA-TP-t638J p 15 N80-24267

Effect of simulaled in-flight thrust reversing on

vertical-tail loads of F-18 and F-15 airplane models - -

conducted in the Langley 16-foot transonic tunnel

INASA-TP-18901 p 18 N81-30086

Aeropropulsive characteristics of Mech numbers up to

2.2 of axisymmetric and nonaxisymmetric nozzles installed

on an F-18 model

[NASA-TP-2044] p 20 N82-30291

F-8 AIRCRAFT

Pilot-model analysis and simulation study of effect of

control task desired control response

[NASA-TP-1140] p 53 N78-20143

FABRICATION

Design and fabrication of a low-specific-weight parabolic

dish solar concentrator

[NASA-TP-t152] p 75 N78-17145

Effects of fabrication and joining processes on

compressive strength of boron/aluminum and

borsic/aluminum structural panels

|NASA-TP-1121 I p 80 N78-20258

Lithium/sulfur dioxide cetl and battery safety

INASA-RP-1099| p 146 N83-14684

Fabrication and evaluation of brazed titanium-clad

borsic/aluminum skin-stringer panels

INASA-TP-1674] p 82 N83-28098

Fabrication and evaluation of superplastically

formed/weld-brazed corrugated compression panels with

beaded webs

[NASA-TP-2512] p 90 N86-13406

FACTORIAL DESIGN

Effect of lead-aircraft ground-speed on self-spacing

performance using a cockpit display of traffic information

INASA-TP-2194J p 40 N83-36028

FAILURE

Reliability bounds for fault-tolerant systems with

competing responses to component failures

[NASA-TP-2409] p 126 N85-23090

FAILURE ANALYSIS

An Assessment of Technology for Turbojet Engine Rotor

Failures

[NASA-CP-2017] p 41 N78-I0068

Lubrication and failure mechanisms of graphite fluoride

films

[NASA-TP-1197] p 91 N78-20337

Lubrication and failure mechanisms of molybdenum

disulfide films I: Effect of atmosphere

[NASA-TP-1343] p 92 N79-13158

Lubrication and failure mechanisms of molybdenum

disulfide films. 2: Effect of substrata roughness

[NASA-TP-1379} p 92 N79-t3159

A relation between semiempincal fracture analyses and

R-curves

[NASA-TP-1600] p 129 N80-15428

Method for estimating crack-extension resistance curve

from residual strength data

[NASA-TP-f753J p 129 N81-11417

Some effects of thermal-cycle-induced deformation in

rocket thrust chambers

[NASA-TP-1834] p 77 N81-20176

MEGA16 - Computer program for analysis and

extrapolation of stress-rupture data

INASA-TP-18091 p 130 N81-23486

Failure mechanics in low-velocity impacts on thin

composite plates

[NASA-TP-2152] p 82 N83-24562

Failure Analysis and Mechanisms of Failure of Fibrous

Composite Structures

INASA-CP'2278] p 82 N83-33957

Turbine Engine Hot Section Technology (HOST)

[NASA-CP-2289] p 135 N86-tt495

Surface fatigue tile and failure characteristics of EX-53,

CBS 1000M, and AlSl 9310 gear materials

[NASA-TP-2513] p 125 N86-12609

FAILURE MODES

Experimental data on single-bolt joints in quasi isotropic

graphite/poymide laminates

[NASA-TP-2015} p 81 N82-25325

Buckling and failure characteristics of graphite-pofyimide

shear panels

[NASA-TP-2153] p 82 N83-24561

FAN BLADES

Cold-air investigation of first stage of 4-1/2-stage, fan

drive turbine with average stage-loading factor of 466

{NASA-TP-1780] p 48 N81-16050

Incidence loss for fan turbine rotor blade in

two-dimensional cascade

{ NASA-TP-21881 p 50 N83-30431

Detailed flow measurements in casing boundary tayer

of 429-meter-per-second-tip-speed two-stage fan

I NASA-TP-20521 p 51 N84-28795

Fluctuating pressures on fan blades of a turbofan engine,

flight test investigation

I NASA-TP-23811 p 190 N85-19790

FANS

ACOuStic performance of two 1.83-meter-diameter fans

designed for a wind-tunnel dnve system

INASA-TP-1008] p 185 N77-30909

Performance of two-stage fan with larger dampers on

first-stage rotor

[ NASA-TP-t 3991 p 44 N79-23967

A-47
FAR INFRARED RADIATION SUBJECT INDEX

Performance of two-stage fan having low-aspect-ratio

first-stage rotor blading

{NASA-TP-1493[ p 45 N79-27143

FAR INFRARED RADIATION

Far infrared supplement: Catalog of infrared

observations

I NASA-RP-1119] p202 N84-265 t 9

Catalog of infrared observations ancluding: Bibliography

ot infrared astronomy and index of infrared source

positions

[ NASA-RP-t 118} p 202 N84-26520

FARADAY EFFECT

Propagation effects on satellite systems at frequencies

below 10 GHz, a handbook for satellite systems design,

1 st edit=on

[NASA-RP-1108i p 100 N84-13397

FAST FOURIER TRANSFORMATIONS

Geometric interpretations of the Discrete Fourier

Transform (DFT)

INASA-TP-23321 p t77 N84-24114

FASTENERS

The 161h Aerospace Mechanisms Symposium

[NASA-CP-2221 ] p 99 N82-23344

Theorelical basis for design of thermal-stress-free

fasteners

INASA-TP-22261 p 132 N84-13614

Welding, Bonding and Fastening, 1984

I NASA-CP 23871 p79 N86-11227

FATIGUE (MATERIALS)

Evaluation o! CBS 600 carburized stee_ as a gear

material

INASA-TP-1390] p 120 N79-14389

Comparisons of modified Vasco X-2 and AISI 9310 gear

steels

INASA-TP-1731 h p 122 N81-14322

Design of power-transmitting shifts

INASA-RP-1123] p 124 N84-27041

Structural Integnty and Durability of Reusable Space

Propulsion Systems

I NASA-CP-2361 ] p 78 N85-27941

Turbine Engine Hot Sect=on Technology (HOST)

iNASA-CP-2289) p 135 N86-11495

An update of the total-strain version of SRP

t NASA-TP-24991 p 90 N86-12295

Design of tract=on drives

{NASA-RP-11541 p 125 N66-13734

FATIGUE LIFE

influence of fretting on flexural fatigue of 304 stainless

steel and mild steel

INASA-TP-1193) p 66 N78-21269

Roiling-element fatigue life of AISI M-50 end t8-4-1

bells

{NASA-TP-1202J p 119 N78-21473

Effect of filtration on rolling-element-bearing life in

contaminated lubricant environment

INASA-TP-t272} p 119 N76-28457

Low-cycle fatigue of thermal-barrier coatings at 982 deg

C

{NASA-TP-1322} p 43 N79.13046

Effect of low-stiffness closeout overwrap on rocket

thrust-chamber life

{NASA-TP-14561 p 77 N79-23132

Life analysis of multirofler planetary traction drive

[NASA-TP-1710] p 122 N81-20423

Effect of shot peening on surface fatigue life of

carburized end hardened AISI 9310 spur gears

{NASA-TP-20471 p 122 N82-32736

Advanced Materials Technology

lNASA-CP-2251 ] p 79 N83-12147

Rolling-element fatigue life with traction fluids and

automatic transmission fluid in a high-speed rolling-contact

ng

{NASA-TP-2050] p t22 N83-13457

Roiling-element fatigue life of AMS 5900 balls

[NASA-TP-2080 ] p 122 N83-16758

Effect of carbide distribution on rolling-element fatigue

life of AMS 5749

{NASA-TP-2189] p 123 N83-33166

Effect of preforming adherends on static and fatigue

strength of bonded composite single-lap joints

INASA'TP'2324] p 133 N84-26053

Effect of lubricant extreme-pressure additives on surface

fatigue life ot AtSI 9310 spur gears

I NASA-TP-2408] p 124 N85-13234

Effect of speed and press fit on talngue life of

roller-bearing inner-race contact

[NASA-TP-2496] p 125 N85-31511

Joint design for improved fat_ue life of diffusion-bonded

box-stiffened panels

[NASA-TP-2480} p 135 N85-33537

Surface fatigue life and failure characteristics of EX-531

CBS 1000M, and AISI 9310 gear materials

[NASA-TP-2513} p 125 N86-12609

Thermal-fatigue and oxidation resistance of

cobalt-modified Udlmet 700 alloy

[NASA-TP-2591 j p 135 N86-28464

FATIGUE TESTS

Influence of fretting On flexural fatigue of 304 stainless

steel and mild steel

I NASA-TP-1193 } p 86 N78-21269

Characterization of wear debris generated in accelerated

rolling-element fatigue tests

INASA-TP-12031 p 119 N78-21470

Rolling-element fatigue life of AISI M-50 and 18-4-1

bails

INASA-TP-1202} p 119 N78-21473

Evaluation of high-contact-ratio spur gears with profile

modification

{NASA-TP-1456} p 120 N79-31604

Ferrographic analysis of wear debris from full-scale

bearing fatigue tests

{NASA-TP-t511] p 121 N79-31605

Creep and residual mechanical properties of cast

superatloys end oxide dispersion strengthened alloys

[NASA-TP-1781 ] p 87 N81-19273

Rolling-element fatigue life of AMS 5900 balls

INASA-TP-2080] p 122 N83-16756

Preliminary study of Ihermomechanical fatigue of

polycrystalline MAR-M 200

fNASA-TP-2280} p 89 N84-17350

Effect of five lubricants on life of AISI 9310 spur gears

{NASA-TP-2419} p 116 N85-16099

A method for developing design diagrams for ceramic

and glass materials using fatigue data

{NASA-RP-1174} p 126 N66-32763

FAULT TOLERANCE

Validation Methods Research for Fault-Tolerant Avionics

and Control Systems Sub-Working Group Meeting. CARE

3 peer review

INASA-CP-2167] p 176 N8t-15702

Production of Reliable Flight Crucial Software: Validation

Methods Research for Fault Tolerant Avionics and Control

Systems Sub-Working Group Meeting

INASA'CP'2222] p 179 N82-24645

Validation of a fault-tolerant clock synchronization

system

[NASA-TP-2346} p 180 N84-34198

Reliability bounds for fault-tolerant systems with

competing responses to component failures

[NASA-TP-2409J p 126 N85-23090

Hybrid routing technique for a fault-tolerant, integrated

information network

[NASA-TP-2S05] p 180 N86-27947

FEASIBILITY ANALYSIS

A feasibility study of ion implantation techniques for mass

spectrometer calibration

[NASA-TP-1185] p 114 N78-21431

Simulation of a cockpit-display concept for executing a

wake-vortex avoidance procedure

[NASA-TP-2300] p 40 N84-21542

Acoustic treatment of the NASA Langley 4- by 7-meter

tunnel: A feasibility study

[NASA-TP-2563] p 191 N86-31337

FEDERAL BUDGETS

Western Regional Remote Sensing Conference

Proceedings, 1981

[E82-10104| p 141 N82-22546

FEEDBACK

Total energy-rate feedback for automatic glide-slope

tracking during wind-sheer penetration

[NASA-TP-2412] p 58 N85-23801

FEEDBACK CONTROL

Eigenvalue/eigenveclor assignment using output

feedback

{NASA-TP-11181 p 160 N78-18823

Study of the use of e nonlinear, rate-limited filter on

pilot control signals

{NASA-TP-1147} p 53 N76-20142

Stability boundaries for systems with frequency-model

feedback and complacency filler

tNASA-TP-1744] p 184 N8t-10769

Decoupled control of a long flexible beam in orbit

[NASA-TP-17401 p 71 N81-13082

Pitfalls end guidelines for the numerice_ evaluation of

moderate-order system frequency response

{NASA-TP-1814] p 72 N81-25138

Reduced order feedback control equations for linear time

and frequency domain analysis

[NASA-TP-1818] p 72 N81-25140

An application of multivariable design techniques to the

control of the national transonic facility

[NASA-TP-1887] p 181 N81-29840

A method for obtaining reduced-order control laws for

high-order systems using optimization techniques

{NASA-TP.1876} p 181 N81-30851

Gain selection method and model for coupled propulsion

and airframe systems

[ NASA-TP-2067 ] p 57 N83-11139

Comparison of simulator fidelity model predictions with

in-simulator evaluation data

[NASA-TP-2106] p 36 N83-18715

NASA Aircraft Controls Research, 1983

[NASA-CP-22961 p 58 N84-20567

Decoupled control analysis of a large flexible space

antenna with linear quadratic regulator comparisons

[NASA-TP-22931 p 74 N84-23675

Regions of attraction and ultimale boundedness for

linear quadratic regulators with nonlinearities

INASA-TP-2322} p 181 N84-26538

FEEDFORWARD CONTROL

Application of the concept Of dynamic trim control tO

automatic landing of carrier aircraft --- utilizing digital

feedforeward control

INASA-TP-1512] p 55 N80-19126

FEMALES

Physiological responses of women to simulated

weightlessness: A review of the first female bed-rest

study

[NASA-SP*4301 p 170 N79-13686

FERRITES

FrictK:,n and wear of single-crystal and poiycrystalline

maganese-zioc ferrite in contact with various metals

INASA-TP-1059] p 91 N78-I0295

Anisotropic friction and wear of single-crystal

manganese-zinc ferrite in contact with itself

{NASA-TP-1339] p 120 N79-10425

X-ray photoe4ectron spectroscopy and friction studies

of nickekzinc and manganese-zinc ferrifes in contact with

metals

INASA-TP-21631 p 88 N83-23419

Humidity effects on adhesion ol nickel-zinc ferrite in

elastic contact with magnetic tape and itself

[NASA-TP-2449} p 96 N85-21359

FERROMAGNETISM

Characterization of wear debris generated in accelerated

rolling-element fatigue tests

INASA-TP-12031 p 119 N78-21470

Ferrographic analysis of wear particles from sliding

elastohydrodynamic experiments

{NASA-TP-12301 p 119 N78-22377

FERROUS METALS

Friction and surface chemistry of some ferrous-base

metallic glasses

[NASA-TP-1991 I p 88 N82-21301

FIBER COMPOSITES

Selected NASA research in composite Materials and

structures

INASA-CP-2142] p 80 N80-28436

Failure Analysis and Mechanisms of Failure of Fibrous

Composite Structures

[NASA-CP-2278} p 82 N83-33957

Fracture toughness of fibrous composite materials

[NASA-TP-23701 p 83 N85-11136

Tough Composite Materials

[NASA-CP-2334] p 83 N85-12941

integrated Composite Analyzer (ICAN): Users end

programmers manual

{NASA-TP-2515] p 83 N86-21614

FIBER ORIENTATION

Fracture toughness of fibrous composite matenels

[NASA-TP-2370] p 83 N85-11136

FIBER REINFORCED COMPOSITES

Effects of temperature, thermal exposure, and fatigue

on an alumina/aluminum composite

[NASA-TP-17951 p 81 N81-14001

Interface control end mechanical property improvements

in silicon oath;de/titanium composites

[NASA-TP-2066] p 81 N82-31451

NASA/aarcraff industry standard specification for

graphite fiber toughened thermeset resin composite

material

[NASA-RP-11421 p 63 N65-26923

Effect of low-velocity or ballistic impact damage on the

strength of thin composite and aluminum shear panels

[NASA-TP-2441 } p 83 N85-26924

FIELD EFFECT TRANSISTORS

High-voltage, high-power, solid-state remote power

controllers for aerospace applications

[NASA-TP-2437] p 78 N85-21263

Programmable, automated transistor test system

[NASA-TP-2554} p 103 N86-2t755

FIELD OF VIEW

Comparison of data mversaon techniques for remotely

sensed wide-angle observations of Earth emitted

radiation

[NASA-TP-1924} p 164 N82-13620

FIGHTER AIRCRAFT

Improvement of maneuver aerodynamics by sperwvise

blowing

[NASA-TP-t0651 p 7 N76-14997

Longitudinal aerodynamic characteristics at Mach 0.60

to 2.86 of a fighter configuration with strut braced w_ng

[ NASA-TP-1102 ] p7 N78-16000

Computer-automated Opponent for manned air-to-air

combat simulations

INASA-TP-15181 p 176 N79-33855

A-48
SUBJECT INDEX

Experiments in sensing transient rotational acceleration

cues on a flightsimulator

[NASA-TP-1537] p 33 N80-10193

Summary of low-speed longitudinal aerodynamics of two

powered close-coupled wing-canard fighter configurations

--° conducted in Langley C/STOL tunnel

[NASA-TP-1535] p t3 N80-12994

Effects of fuselage forebody geometry on low-speed

lateral-dirsctional characteristics of twin-tail fighter model

at high angles of attack

[NASA-TP.t592J p 13 N80-t3002

Control-system techniques for improved departure/spin

resistance for fighter aircraft

[NASA-TP-1689] p 2 N80-29244

Experimental study of wing leading-edge devices for

improved maneuver performance of a supercriticai

maneuvering fighter configuration --- Langley 7- by 10-ff

high speed tunnel tests

[NASA-TP-2125J p 21 N83-22162

Pressures measured in flight on the aft fuselage and

external nozzle of a twin-jet fighter

[NASA-TP-2017] p 21 N83-25665

Effects of varying podded nacelle-nozzle installations

on transonic aeropropulsive characteristics of a supersonic

fighter aircraft

[NASA-TP-2120] p 21 N83-26821

Sen,ice life evaluation of rigid explosive transfer lines

[NASA-TP-2143] p 36 N83-31596

Effect of thrust vectoring and wing maneuver devices

on transonic aeropropulsive characteristics of a supersonic

fighter

[NASA-TP-2119] p 22 NS4-t0025

Aircraft Electric Secondary Power

[NASA-CP-2282] p 50 N84-10055

Wave drag as the objective function in transonic fighter

wing optimization

[ NASA-TP-2265] p 23 N84-17127

Theoretical and experimental engine-inlet flow fields for

fighter forebodies

[NASAoTP-2270] p 23 N84-17132

Wind-tunnel free-flight investigation of a model of a

forward-swept-wing fighter configuration

[NASA-TP-2230] p 57 N84-t7184

Investigation of trailing-edge-flap, spanwise-blowing

concepts on an advanced fighter configuration

[NASA-TP-2250} p 23 N84-18164

Wing planform effects at supersonic speeds for an

advanced fighter configuration

[NASA-TP-2269] p 23 N84-20486

Aeropropulsive characteristics of

nonaxisymmetdc-nozzle thrust reversers at Msch numbers

from 0 to 1.20

[NASA-TP-2306] p 23 N84-24538

Effect of fuselage upwesh on the supersonic longitudinal

aerodynamic characteristics of 2 fighter configurations

[NASA-TP-2330] p 24 N84-27676

Low-speed stability and control wind*tunnel

investigations of effects of spanwise blowing on fighter

flight characteristics at high angles of attack --- Langely

12-ft low-speed tunnel and 30- by 60-ft tunnel

[NASA-TP-2431 ] p 26 N85-23708

Aerodynamic characteristics of a supersonic fighter

aircraft model at Msch 0.40 to 2.47

[NASA-TP-2580] p 28 N86.23561

FILAMENT WINCING

Identification and management of filameot-wound case

stiffness parameters

[NASA-TP-2117] p 81 N83-16400

FILE MAINTENANCE (COMPUTERS)

Office of Space Terrestrial Applications

(OSTA)/Applications Data Service (ADS) data systems

standerds

[NASA-CP-2196] p 65 N82-15095

FILLERS

Study of austenitic stainless steel welded wwth low alloy

steel filler metal --- tensile and impact strength tests

[NASA-TP-1460J p 87 N79.28288

FILM COOLING

Experimental flow coefficients of a full-coverage

film-cooled-vane chamber

[NASA.TP-1036J p 41 N77-32153

Hydrogen film cooling of a small hydrogen-ox'ygen thrust

chamber and its effect on erosion rates of various ablative

materials

[NASA-TP-1098] p 76 N78-13124

Effects of film injection angle on turbine vane cooling

[NASA-TP-1095J p 104 N78-13379

Effect of cooling-hole geometry on aerodynamic

performance of a film-cooled turbine vane tested with cold

air in a two-dimensional cascade

[NASA-TP-1136] p 8 N78.20080

Two-dimensional cold-air cascade study of a film-cooled

turbine stator blade. 4: Comparison of experimental and

analytical aerodynamic results for blade with 12 rows of

0.078-centimeter-(0.030-inch-) diameter holes having

streamwise ejection angles

[NASA-TP-1151 ] p 42 N78-20130

Two-dimensional cold-air cascade study of a film-cooled

turbine stater blade. 5: Comparison of experimental and

analytical aerodynamic results for blade with 12 rows of

O.038-centimeter.(O.Ot5 inch) diameter coolant holes

having streamwise ejection angles

INASA-TP-1204} p 42 N78-20133

Flow visualization of film cooling with spanwise injection

from a small array of holes and compound-angle injection

from a large array

{NASA-TP-t 195 J p42 N78-21113

FORTRAN program for calculating coolant flow and

metal temperatures of a lull-coverage-film-cooled vane or

blade

[NASA-TP-1259J p 43 N78-28099

Analysis of metal temperature and coolant flow with a

thermal-barrier coating on a full-coverage-film-cooled

turbine vane

[NASA-TP-1310] p 43 N78-31109

direct measurements and analysis of skin friction and

cooling downstream of multiple flush-slot injection into a

turbulent Mach 6 boundary layer

[NASA-TP-tt76] p 106 N78-33385

Ceramic coating effect on liner metal temperatures of

film-cooled annular combustor

[NASA-TP-1323] p 44 N7g-14098

Flow visualization of discrete.hole film cooling with

spanwise injection over a cylinder

I NASA-TP-1491] p 44 N79-27142

Influence of coolant tube curvature on film cooling

effectiveness as detected by infrared imagery

[NASA-TP-1546] p 45 N80-11087

Film-cooling effectiveness with developing coolant flow

through straight and curved tubular passages

[NASA-TP-2062] p lt0 N83-12360

Three-dimensional turbulent-mixing-length modeling for

diecrete-hole coolant injection into a crossftow

[NASA-TP-2200] p 111 N83-34232

Vortex-generating coolant-flow-passage design for

increased film-cooling effectiveness and surface

coverage

[NASA-TP-2388| p 112 N85-12314

FILM THICKNESS

Elastohydrodynamic lubrication of elliptical contacts for

materials of low elastic modulus. 2: Starved

coniunction

[NASA-TP-t273J p 119 N78-28458

Effect of geometry on hydrodynamic film thickness

{NASA-TP-1287] p 119 N78-30585

Minimum film thickness in elliptical contacts for different

regimes of fluid-film lubrication

[NASA-TP-1342] p 119 N78-33447

Comparison of predicted and measured

elastohydrodynamic film thickness in a 20-millimeter-bore

ball bearing

[NASA-TP-1542] p 121 N79-32552

Correlation of asperity contact-time fraction with

elastohydrodynamic film thickness in a 20-millimeter-bore

ball bearing

INASA-TP-1547] p 12t N79-33476

Film thickness measurement for spiral groove and

Rayleigh step lift pad self-acting face seals

[ NASA-TP-2058 ] p49 N83-11126

Elastohydrodynamic contacts. Effects of dents and

grooves on traction and local film thickness

[NASA-TP-2175] p 123 N83-28453

Dynamic behavior of sp_ral-groeve and Rayleigh-Step

self-scting face seals

[NASA-TP-2266] p 51 N84-t6181

Dynamic response of film thickness in spiral-groove face

seals

[NASA-TP-25441 p 52 N86-15313

FILTRATION

Effect of filtration on rolling-element-bearing life in

contaminated lubricant environment

[NASA-TP-12721 p 119 N78-28457

FINITE DIFFERENCE THEORY

Advances in engineering science, volume 4

[NASA-CP-2001-VOL-4] p 98 N77-10345

Finite-difference theory for sound propagation in a lined

duct with uniform flow using the wave envelope concept

[NASA-TP-1001 I p 185 N77-30908

Numerical study of transonic flow over oscillating airfoils

using the full potential equation

[NASA-TP-1120] p 8 N78-21055

Inverse boundary-layer theory and comparison with

experiment

[NASA-TP-t208J p 106 N78-32385

FINITE ELEMENT METHOD

A hybridized method for computing

high-Reynolds-number hypersonic flow about blunt

bodies

INASA.TP-14971 p 107 N7g-33441

Calculation of three-dimensional unsteady transonic

flows past helicopter blades

[NASA-TP-17211 p 15 N80-33356

A study of the sonic-boom characteristics of a blunt body

at a Mach number of 6

{NASA-TP-1787] p 3 N81-13915

Numerical solutions of the Navier-Stokes equations for

transonic aftsrbody flows

{NASA-TP-17841 p 16 N81-13919

Numerical grid generation techniques ---conference

[NASA-CP-2166} p 182 N81-14690

Numerical simulation of steady supersonic flow --- spatial

marching

{NASA-TP-t749} p 17 N81-22018

Temporal and spatial inconsistencies of time-split

finite-difference schemes

{NASA-TP.1790} p 182 N81-22754

Surrogate-equation technique for simulation of steady

inviscid flow

[NASA-TP-1866| p 18 N81-31129

Some observations on a new numerical method for

solving Navier-Stokes equations

[NASA-TP-1934] p 18 N82-11032

Numencal analysis of the scram|at-inlet flow field by

using two-dimensional Navier-Stokes equations

[NASA-TP-t940] p 48 N82-13142

Finite-difference fluid dynamics computer mathematical

models for the design end interpretation of experiments

for space flight --- atmospheric general circulation

experiment, convection in a float zone, and the

Bridgman-Stockberger crystal growing system

[NASA-TP-2323] p 112 N84-23852

Viscous-inviscid interaction method including wake

effects for three-dimensional wing-body configurations

[NASA-TP-t910] p 24 N84-27682

Interactive algebraic gnd-generation technique

{NASA-TP-2533] p 177 N86-23282

FINITE ELEMENT METHOD

Advances in engineering science, volume 4

[NASA-CP-200t-VOL-4] p 98 N77-10345

Sixth NASTRAN Users' Colloquium

[NASA-CP-2018] p 127 N78-12443

Evaluation of a hybrid, anisotropic, multilayered,

quadrilateral finite element

[NASA-TP-1236] p 127 N78-28482

Critical study of higher order numerical methods for

solving the boundary-layer equations

[NASA-TP-1302] p 106 N79-13305

A critical examination of stresses in an elastic single

lap joint

[NASA-TP-1507] p 128 N7g-31626

Analysis of surface cracks in finite plates under tension

or bending loads

[NASA-TP-1578] p 129 N80-13512

Nonlinear, three-dimensional finite-element analysis of

air*cooled gas turbine blades

[NASA-TP-1669] p 129 N80-22734

Eighth NASTRAN User's Colloquium

[NASA-CP-2131] p 129 N80-24648

Ninth NASTRAN Users' Colloquium

[NASA-CP-2151| p 129 N80-33782

Stress-concentration factors for finite orthotropic

laminates with a pin-loaded hole

[NASA-TP-1862] p 81 N81-24178

Elastic-plastic finite-element analyses of thermally

cycled double-edge wedge specimens

[NASA-TP-1973J p t30 N82-20566

Tenth NASTRAN User's Colloquium

[NASA-CP-2249] p 131 N83-12452

Reduction methods for nonlinear steady-state thermal

analysis

[NASA-TP.2098] p t 10 N83-20032

Tire Modeling

[NASA-CP-2264| p 131 N83-21391

Eleventh NASTRAN User's Colloquium

[NASA-CP-2284] p 132 N84-15590

The NASTRAN user's manual

[NASA-SP-222(06)] p 133 N84-21899

Nonlinear Structural Analysis

[NASA-CP-2297J p 133 N84-31688

Twelfth NASTRAN Users' Colloquium

[NASA-CP-2328J p 133 N84-32864

STARS: A general-purpose finite element computer

program for analysis of engineenng structures

{NASA-RP-1129| p 134 N85-11378

Local strain redistribution corrections for a simplified

inelastic analysis procedure based on an elastic

finite-element analysis

[NASA-TP-2421] p 134 N85-20396

Thirteenth NASTRAN Users' Colloquium

[NASA-CP-2373] p 134 N85-25863

A-49
FINS

Joint research effort on vibrations of twisted plates,

phase 1: Final results

INASA-RP-t150] p 135 N86-10579

Numerical Techniques in Acoustics

INASA-CP-2404] p 190 N86-12007

Fourteenth NASTRAN Users' Colloquium

{NASA-CP-2419] p 135 N86-25823

FINS

Low-speed wind.tunnel investigation of wing fins as

trailing-vortex-alleviation devices on a transport airplane

model

INASA-TP-1453J p 12 N79-24961

FIREBREAKS

Conference on F,re Resistant Materiels: A compilation

of presentations end pepers

[NASA-CP-2094] p 29 N79-31166

FIREPROOFING

Conference on Fire Resistant Materiels: A compilation

of presentations end papers

[NASA-CP-20g4] p 29 NTg-31166

FIRES

Conference on Fire Resistent Materials: A compilation

of presentafuons end papers

INASA.CP.20g4] p 29 N79.31166

Aslresement of Carbon Fiber Electrical Effects

[NASA-CP-2119] p 80 N80-19193

FISHES

Remote sensing of oceanic parameters during the

Skyleq/gemefish expenment

CNASA-RP-t012] p 187 N78.12644

FISSIONABLE MATERIALS

Direct nuclear-powered lasers

[NASA.TP.2091] p 1t8 N83-16738

FLAME HOLDERS

Conceptual model of turbulent flemeholding for scramjet

combustors

[ NASA-TP- 1543 ] p 47 N80-33409

Effect of flameholder pressure drop on emissions and

performance of premixed-preveporized combustors

[NASA.TP.2131] p 50 N83-23309

FLAME PROPAGATION

Conceptual model of turbulent fiemeholding for scramjet

combustors

[NASA-TP-1543 p 47 N80-33409

Modeling interface Motion Of Combusbon (MINE)C), A

computer code for two-dimensional, unsteady turbulent

combustion

[NASA-TP-2132 p 50 N83-32806

FLAMEOUT

Conceptual model of turbulent flamehotding for scremiet

combustors

INASA-TP-1543 p 47 N80-33409

FLAMES

lnvesfugation of light scattering as a technique for

detecting discrete soot particles in a luminous flame

[NASA-TP-1235 p 193 N78-27906

Effects of percentage of blockage and flameholder

downstream counterbores on lean combustion limits of

premixed, prevsporized propane-air mixture

[NASA-TP-2227 p 50 N83-34941

FLAMMABILITY

Conference on Fire Resistant Materials: A compilation

of presentations and papers

{NASA-CP-2094! p 29 N79-31166

FLAPPING HINGES

Effects of primary rotor parameters on flapping

dynamics

[NASA-TP-1431 p 55 N80-15138

FLAPS (CONTROL SURFACES)

Effects of wing leading-edge flap deflections on subsonic

longitudinal aerodynamic characteristics of a wing-fuselage

configuration with a 44 deg swept wing

[NASA-TP-1351 ] p 10 N79-13002

Large-scale wind-tunnel tests of inverting flaps on a

STOL ufility aircraft model

[NASA-TP-1696] p 34 N80-25318

Performance characteristics of axisymmetric

convergent-divergent exhaust nozzles with longitudinal

slots in the divergent

[NASA-TP-2013] p 19 N82-26231

Design and experimental results for a flapped

natural-laminar-flow airfoil for general aviation

applications

[NASA-TP-1865] p 21 N83-30386

FLAT PLATES

Two-dimenstonal transonic testing with splitler plates

{NASA-TP*1153] p 7 N78-t7999

Orifice-induced pressure error studies in Langley 7- by

10-foot high-speed tunnel

[NASA-TP-2545] p 27 N86-20347

FLAT SURFACES

Noise transmission through flat rectangular panels into

a closed cavity --- light aircraft noise

INASA-TP-1321] p 186 N79-14874

Local stability analysis for a planar shock wave

[ NASA.TP-2387] p 25 N85-12864

A-50

FLEXIBILITY

Decoupled control analysis of a large flexible space

antenna with linear quadratic regulator comparisons

[NASA-TP-2293] p 74 N84-23675

FLEXIBLE BODIES

Influence of oil-squeeze-film damping on steady-state

response of flexible rotor operating to supercritical

speeds

[NASA-TP-1094} p 41 N78.13064

Effects of model error on control of large flexible space

antenna with comparisons of decoupied and linear

quadratic regulator control procedures

[NASA-TP-2604] p 75 N86-30801

FLEXIBLE SPACECRAFT

Application of the LQG/LTR technique to robust

controller synthesis for a large flexible space antenna

[NASA.TP.2560] p 75 N86-30800

FLEXIBLE WINGS

An analytical technique for predicting the characteristics

of a flexible wing equipped with an active

flufter-auppreas_on system end comparison with

wind.tunnel data

[NASA-TP-1367] p 128 N79-17264

Flight measurements of surface pressures on a flexible

superorifical research wing

[NASA-TP-2501] p 27 N86-20350

FLEXING

Long-term thermal aging of 2 graphite.polyimide

composite materials

[NASA-TP-2369] p 83 N85-12094

FLIGHT ALTITUDE

Measurement of aircraft speed and altitude

[NASA-RP-1046] p 34 N80-24296

FLIGHT CHARACTERISTICS

Similitude requirements and scaling relationships as

applied to model testing

[NASA-TP-1435] p 33 N79-30176

Inclusion of unsteady aerodynamics in longitudinal

parameter estimation from flight data --- USe of vortices

and mathematical models for parametedzafuon from flight

characteristics

[NASA-TP-1536J p 13 Na0-12995

Flight tests of the total automatic flight control system

(-rafcos) concept on a DHC-6 Twin Otter aircraft

[NASA-TP-1513] p 55 N80-17081

Pseudosteady-state analysis of nonlinear aircraft

maneuvers

{NASA-TP-t7581 p 56 N81-13065

Advanced aerodynamics and active controls. Selected

NASA research

[NASA-CP-2172] p 3 N81-19001

Simulator study of flight characteristics of a large

twm-fusoiege cargo transport airplane during approach and

landing

[NASA-TP-2183] p 57 N84-12190

Space Shuttle separate-surface control-system study

INASA'TP-2340] p 58 N84-28801

Simulator study of flight characteristics of several large,

dissimilar, cargo transport airplanes during approach and

landing

[ NASA-TP-2357] p 58 N85-11002

Low-speed stability and control wind-tunnel

investigations of effects of spanwise blowing on fighter

flight characteristics at high angles of attack --- Lengely

12-tt low-speed tunnel and 30- by 60-It tunnel

[NASA-TP-2431) p 26 N85-23708

Ground-based and in-flight simulator studies of flight

charectensfucs of a twin-fuselage passenger transport

airplane during approach and landing

[NASA-TP-24511 p 58 N85-34144

Meteorological and Environmental Inputs to Aviation

Systems

[NASA-CP*2388J p 166 N86-11735

FLIGHT CONDITIONS

Sensitivity analysis of the space shuffle to ascent wind

profiles

[NASA-TP-t 988] p 69 N82-20236

FLIGHT CONTROL

Fourth NASA Inter-Center Control Systems

Conference

[NASA-CP-O071 p 212 N78-23010

Avionics and controls research and technology

[NASA-CP-2061 I p 1 N79-15898

Configuration management and automatic control of an

augmentor wing aircraft with vectored thrust

[ NASA-TP-12221 p 54 N79-17872

Science and Technology of Low Speed and Motorless

Flight. Third International Symposium

[L-12973J p 2 N79-27070

Description ol the VTOL Approach and Landing

Technology (VALT) CH-47 research system

[NASA-TP-1436] p 54 N79-29195

Validation Methods for Fault-Tolerant avionics and

control systems, working group meeting 1

[NASA-CP-21141 p 176 N80-12741

SUBJECT INDEX

Development and flight test results of an autothroftle

control system at Mech 3 cruise

[NASA-TP-1621] p 56 N80-26328

Evaluation of a computer-generated perspective tunnel

display for flight path following

[NASA.TP-1736] p 39 N81-13958

Val_3afuon Methods Research for Fault-Tolerant Avionics

and Control Systems Sub-Working Group Meeting. CARE

3 peer review

[NASA-CP.2167] p 176 N81-15702

The 1980 Aircraft Safety and Operating Problems, part

1

[NASA-CP-2170-PT-1J p 29 N81-1g035

An analytical study of the longitudinal response of

airplanes to positive wind shear

(NASA-TP-1765] p 56 N81-20082

Electric Flight Systems

[NASA-CP-2209] p 3 N82-fgf34

Gain selection method end model for coupled propulsion

end airframe systems

[NASA-TP-2067] p 57 N83-11139

Effect of lead-aircraft ground.speed on self-spacing

performance using a cockpit display of traffic information

[NASA-TP.2194] p 40 N83.36028

Controls, Displays, end Information Transfer for General

Aviation IFR Operations

(NASA-CP-2279] p 4 N84.t202g

NASA Aircraft Controls Research, t983

[NASA-CP.2296] p 58 N84-20567

Twentieth Annual Conference on Manual Control,

volume 2

(NASA.CP.2341-VOL-2] p 174 N85-14535

Effect of aerodynamic and angle-of-attack uncertainties

on the May 1979 entry flight control system of the Space

Shuttle from Mech 8 to 1.5

[NASA-TP-2365] p 69 N85.15778

Reference energy-altitude descent guidance: Simulator

evaluation --- aircraft descent and fuel conservation

[NASA-TP-2383] p 40 N85-16868

Space Shuttle Technical Conference, part 2

[NASA-CP-2342-PT-2] p 63 N85-16937

Advanced secondary power system for transport

aircraft

[NASA-TP-2463] p 52 N85-28944

Piloted simulation of an algorithm for onboard control

of bme-optimal intercept

(NASA-TP-2445] p 58 N85-28949

FLIGHT CREWS

Handbook on astronaut crew motion disturbances for

control system design --- in skylab

{NASA-RP-t025J p 7t N79-27237

Resource management on the flight deck ---

conferences

[NASA-CP-2120J p 29 N80-22283

Guidelines for line-oriented flight training, volume 2

[NASA-CP-2184-VOL-2] p 30 N82-13123

Summary Proceedings of a Wind Shear Workshop

[NASA-CP-2270] p 165 N83-25265

FLIGHT HAZARDS

An analytical study of the longitudinal response of

airplanes to posifuve wind shear

[ NASA-TP* 1765 j p 56 N81-20082

Meteorological and Environmental Inputs to Aviation

Systems

[NASA-CP-2388] p 166 N86-11735

FLIGHT INSTRUMENTS

A rotor-mounted digital instrumentation system for

helicopter blade flight research measurements

INASA-TP-f 146] p 38 N78-20128

A review of some head-up display formats --- tests on

sensing equipment for flights following partly visible terrain

close to the ground

INASA-TP-14991 p 38 N79-33201

Cognitive issues in head-up displays

[NASA-TP-1711] p 173 N81-13636

Shock response spectra variefuonet analysis for

pyrotechnic qualification testing of flight hardware

[NASA-TP-2315J p 74 N84-23676

FLIGHT LOAD RECORDERS

Comparison of concurrent strain gage- and pressure

transducer-measured flight loads on a lifting reentry vehicle

and correlation with wind tunnel predictions

{NASA-TP-1331 J p 10 N78-33053

FLIGHT MANAGEMENT SYSTEMS

Planning fuel-conservative descents in an airline

environmental using a smatl programmable calculator:

Algorithm development and flight test results

NASA-TP-2393J p 40 N85-26705

FLIGHT MECHANICS

Flight Mechanics/Estimation Theory Symposium --- with

application to autonomous navigation and attitude/orbit

detarminatJon

{NASA-CP-2082] p 64 N79-26082

Sixth Annual Flight Mechanics/Estimation Theory

Symposium

I NASA-CP-2205] p 62 N82-10064
SUBJECT INDEX FLIGHT TESTS

Flight Mechanics/Estimation Theory Symposium

[NASA-CP-2002] p 61 N78-76855

FLIGHT PATHS

Simulator evaluation of a flight-path-angle control system

for a transpod airplane with direct lift control

[NASA-TP-1116] p 53 N78.20139

Light airplane crash tests at three flight-path angles

[NASA-TP-1210] p 127 N78-26494

A review of some head-up display formats --- tests on

sensing equipment for flights following partly visible terrain

close to the ground

[NASA-TP-1499] p 38 N79-33201

Crash tests of four identical high-wing single-engine

airplanes

[NASA-TP-1699] p 35 N80-30296

Design cdtafla for fiightpath and airspeed control for

the approach and landing of STOL aircraft

[NASA-TP-1911 ] p 57 N82-20187

Analysis and Monte Carlo simulation of near-terminal

aircraft flight paths

[NASA-TP-1997] p 31 N82.23233

Minlmum-fuel, 3-dimensional flightpsth guidance of

transfer Jets

[NASA.TP-232fl] p 58 N84-32394

Planning fuel.conservative descents in an aidine

environmental using • small programmable calculator:

Algorithm development and flighl test results

[NASA-TP-2393] p 40 N85.26705

Slip-boundary equations for multicomponenl

nonequilibrlum airflow

[NASA-TP-2452] p 113 N86-14530

FLIGHT SAFETY

Proceedings of the 2nd Annual Workshop on

Meteorological and Environmental Inputs to Aviation

Systems

[NASA-CP-2057] p 159 N79.17413

Proceedings, Third Annual Workshop on Meteorological

end Environmental Inputs to Aviation Systems

[NASA-CP-2104] p 160 N60-14633

Proceedings: Fifth Annual Workshop on Meteorological

and Environmental Inputs to Aviation Systems

[NASA-CP-2192] p 3 N62-21139

Proceedings: Sixth Annual Workshop on Meteorological

and Environmental inputs to Aviation Systems

[NASA-CP-2274] p 4 N63-33827

Flight Training Technology for Regional/Commuter

Aidine Operations: Regional Airline Association/NASA

Workshop Proceedings

[NASA-CP-2348] p 30 N85-18009

FLIGHT SIMULATION

Simulated flight effects on noise characteristics of a fan

inlet with high throat Mech number

[NASA-TP-1199] p42 N78-20132

Pilot-model analysis and simulation study of effect of

control task desired control response

[NASA-TP-1140] p 53 N78-20143

Simulation study of the oscillatory longitudinal motion

of an airplane at the stall

[NASA-TP-1242] p 54 N78-30141

Simulation and flight evaluation of a head-up landing

aid for general aviation

[NASA-TP-1276] p 38 N78-31101

A pilot evaluation of two G-seat cueing schemes

[NASA*TP-1255] p 172 N78-31739

Development and validation of a piloted simulation of

a helicopter and external sling load

[NASA-TP-1265] p 32 N79-14083

Aidine pilot scan patterns during simulated tLS

approaches

[NASA.TP-1250] p 171 N79-19682

Effect of image tilt of a virtual image display on simulated

transport touchdown performance

[NASA-TP-1520] p 33 N79-33169

Experiments in sensing transient rotational acceleration

cues on s flight simulator

[NASA-TP-1537] p 33 N80-10193

Application of modified profile analysis to function testing

of simulated CTOL transport touchdown-performance

data

[NASA-TP-1541] p 33 N80-11069

Simulator study of stall/post-staU characteristics of a

fighter airplane with relaxed longitudinal static slability ---

F-16

[NASA-TP-1538] p 55 N80-14136

The effects of motion and g-seat cues on pilot simulator

performance of three piloting tasks

(NASA-TP-1601 ] p 34 N80-15069

An experimental evaluation of heed-up display formats

[NASA-TP-1550] p 39 N80-28349

A simulator study for the development and evaluation

of operating procedures on a supersonic cruise research

transport to minimize airport-community noise

[NASA-TP-1742] p 29 N81-12043

Head*up transition behavior of pilots with and without

head-up display in simulated low-visibility approaches

[NASA-TP-1720] p 173 N61-13635

Simulator study of conventional general aviation

instrument displays in path-following tasks with emphasis

on pilot-induced oscillations

[NASA-TP-1776J p 39 N61-14997

Guidelines for line-oriented flight training, volume 1

[NASA-CP-21841 p30 N81-30101

Longitudinal and tatersl static stability end control

characteristics of a 1/6-scale model of a remotely piloted

research vehicle with a supercriticsl wing

[NASA-TP-1360 p 57 N82-15075

Simulator study of vortex encounters by a twin.engine,

commercial, jet transport airplane

[NASA-TP-1966 p 57 N82-19225

Simulator study of a pictorial display for general aviation

instrument flight

[NASA-TP-1963 p 39 N82-20180

Sensitivity analysis of the space shuttle to ascent wind

profiles

[NASA.TP.1988 p 69 N82-20236

A conceptual framework for using Doppler radar

acquired atmospheric data for flight simulation

[NASA.TP.2192 p 36 N83-27977

Effects of motion base and g-seat cueing of simulator

pilot performance

[NASA-TP-2247 p 37 N84-18189

A spatial model of wind shear and turbulence for flight

simulation

[NASA-TP-2313 p 165 N84.24044

Effects of simulated flight on the structure and noise

of underexpsnded jets

[NASA-TP.2308 p 189 N84.25422

Adding computationslly efficient realism to Monte Carlo

turbulence simulation

[NASA-TP-2469 p t85 N85-28708

Aeronautical facilities catalogue Volume 2: Airbresthing

propulsion and flight simuIators

[ NASA-RP-t 133 p60 N86-18328

Theoretical three-and four-axle gimbai robot wrists

[NASA-TP-2564] p 18t N86-25168

FLIGHT SIMULATORS

Analysis and design of a refractive virtual image

system

[NASA-TP-t066] p 193 N78-12829

Simulator evaluation of a flight-path-angle control system

for a transport airplane with direct lift control

[NASA-TP-1116] p 53 N78-20139

Evaluation of several secondary tasks in the

determination of permissible time delays in simulator visual

and motion cues

[NASA-TP-1214] p 32 N78-30089

Simulator study ol the effect of visual-motion time delays

on pilot tracking performance with an audio side task

[NASA-TP-1216] p 32 N76-30090

Effect of image tilt of a virtual image display on simulated

transport touchdown performance

INASA-TP-I$20] p 33 N79-33189

Application of modified profile analysis to function testing

of the motion/no-motion issue in an aircraft

ground-handling simulation --- statistical analysis

procedure for man machine systems flight simulation

INASA-TP-1540J p 33 N80-13024

A general aviation simulator evaluation of a

rate-enhanced instrument landing system display

[NASA-TP-1960] p 39 N82-14085

Comparison of simulator fidelity model predictions with

in-simulator evaluation data

[NASA-TP-2106] p 36 N83-16715

Simulator study of flight characteristics of several large,

dissimilar, cargo transport airplanes during approach and

landing

[NASA-TP-2357] p 58 N85-11002

Reference energy-altilude descent guidance: Simulator

evaluation --- aircraft descent and fuel conservation

[NASA-TP-2383] p 40 N85-16868

FLIGHT TESTS

Light airplane crash tests at impact velocities of 13 and

27 m/sac

[NASA-TP-1042] p 29 N78-10034

Phugoid characteristics of a YF-12 airplane with

variable-geometry in_ets obtained in flight tests at • Mech

number of 29

INASA-TP-1107J p 52 N78-12100

Flight-test evaluation of two electronic display formats

for approach to landin 9 under instrument conditions

INASA-TP-10851 p 36 N78-13054

A flight evaluation of a trailing anemometer for low-speed

calibrations of airspeed systems On research aircraft

INASA-TP-1135] p 32 N78-18044

A rotor-mounted digital instrumentation system for

helicopter blade flight research measurements

[NASA-TP-1146] p 38 N78-20128

Flight evaluation of the transonic stability and control

characteristics of an airplane incorporating a supercritical

wing

[NASA-TP-11671 p 53 N78-20140

Results from flight and simulator studies of s Mech 3

cruise longitudinal autopilot

[NASA.TP-1160} p 53 N78.21160

A new dimension. Wallops Island flight test range: The

first fifteen years

[NASA-RP-t028] p 64 N79-20166

Important factors in the maximum likelihood analysis of

flight test maneuvers

[NASA-TP-145g} p 54 N79-22113

Flight investigation of piloting techniques and crosswind

limitations using • research type crosewind landing gear

[NASA-TP-1423] p 12 N79.23012

A unique facility for V/STOL aircraft hover testing ---

Langley Impact Dynamics Research Facility

{NASA-TP-1473] p 59 N79-2919g

A review of some heed-up display formats --- tests on

sensing equipment for flights follo_ng partly visible terrain

close to the ground

[NASA-TP-1499] p 38 N79.33201

Evaluation of a wind-tunnel gust response technique

including correlations with analytical and flight test

results

[ NASA.TP.t 501] p2 N80-11028

Wind.tunnel/flight correlation study of aerodynamic

characteristics of a large flexible supersonic cruise airplane

(XB.701) 2: Extrapolation of wlnd-tunnel data to full-scale

conditions

[NASA-TP-1515] p 13 N80-16032

Comparison of analytical end flight test identified

aerodynamic derivatives for a tandem-rotor transport

helicopter

[NASA.TP.1581] p 34 N80-17060

Wind-tunnel/flight correlation study of aerodynamic

characlshetics of a large flexible superson¢ cruise airplane

(XB-70-1). 3: A comparison between ohsractadstlcs

predicted from wind-tunnel measurements and those

measured in flight

[NASA.TP.1516] p 14 N80-17986

Measucement of the handling characteristics of two light

mrplanes

{NASA-TP-1636] p 56 N80-25345

Development and flight test results of an sutothrottle

control system at Mech 3 cruise

[NASA.TP-1621 ] p 56 N80-26328

Development and test results of a flight management

aigohthm for fuel conservative descents in a time-based

metered traffic environment

[NASA-TP-17171 p 39 N80-33404

User's manual for MMLE3, s general FORTRAN program

for maximum likelihood parameter estimation

[NASA-TP-1563] p 176 N81-12744

Comparison of Space Shuttle O¢oiter low-speed static

stability and control derivatives obtained from wind-tunnel

and approach and landing flight tests

[NASA-TP-1779] p 56 N81-13066

Assessment of ground effects on the propagation of

aircraff noise: The T-38A flight experiment

[NASA.TP-1747| p 187 N81-14788

Advanced aerodynamics and active controls. Selected

NASA research

[NASA-CP-2172] p 3 N81-19001

The 1980 Aircraft Safety and Operating Problems, part

2

[NASA-CP-2170*PT-2J p 29 N81-19056

Flight-test evaluation of STOL control and flight director

concepts in a powered-liff aircraft flying curved

decelerating approaches

[NASA.TP.1641 ] p 56 N81-19131

Subsonic tests of an all-flush-pressure-orifice air elate

system

INASA-TP-1671 | p 39 N81-26144

Flight test of a pure-tone acoustic source --- aircraft

noise

[NASA-TP-1898] p 188 N81-33945

Ruggedized minicomputer hardware and software

topics, 1961: Proceedings of the 4th ROLM MIL-SPEC

Computer User's Group Conference

[NASA-CP-2206] p 180 N82-14629

Wind-Tunnel/Flight Correlation, 1961

{NASA-CP-2225] p 19 N82-25196

Lightning attachment patterns and flight conditions for

storm hazards, 1980

[NASA-TP-2087] p 30 N83-14077

The application of parameter estimation to flight

measurements to obtain lateral-directionel stab_lity

denvatives of an augmented jet-flap STOL airplane

[NASA-TP-2033] p 57 N83-16350

Helical automatic approaches of helicopters with

microwave landing systems

[NASA-TP-2109] p 31 N83-18704

Motion/visual cueing requirements for vortex encounters

during simulated transport visual approach and landing

(NASA-TP-2136] p 36 N83-22192

A-51
FLIGHT TRAINING SUBJECT INDEX

A companson of two position estimate algorithms that

use ILS Iocetizer and DME information Simulation and

flight test results

I NASA-TP-228'I I p 31 N84-17165

Study of stator-vane fluctuating pressures in a turbofan

engine for static and flight tests

[NASA-TP-2217] p 189 N84-22363

KC- 135 Winglef Program Review

{NASA-CP-2211 J p 24 N84-27686

An experimental and theoretical investigation of

deposition patterns from an agncultural airplane

{NASA-TP-2348] p 25 N84-33379

Flight and wind-tunnel comparisons of the inlet-airframe

interaction of the F-t 5 airplane

{NASA-TP-23741 p 37 N85-12884

Planning fuel-conservative descents in an airline

environmental using a small programmable calculator:

Algorithm development and flight test results

{NASA-TP-23931 p 40 N85-26705

Digital Electronic Engine Control (DEEC) Flight

Evaluation in an F-15 Airplane

INASA'CP'2298} p 52 N86-25342

Supercritical wing technology: A report on flight

evaluations

[NASA-SP-301 j p 6 N77-85474

FLIGHT TRAINING

Resource management on the flight deck ---

conferences

{ NASA-CP-2120] p 29 N80-22283

Guidelines for line-oriented flight training, volume 2

[NASA-CP-2184-VOL-2} p 30 N82-13123

Summary Proceedings of a Wind Shear Workshop

[NASA-CP-2270} p 165 N83-25265

Flight Training Technology for Regional/Commuter

Airline Operations: Regional Airline Association/NASA

Workshop Proceedings

{NASA-CP-2348] p 30 N85-18009

FLOAT ZONES

Analytical and numerical studies of the thermocapillary

flow in a uniformly floating zone

{NASA-TP-2576} p 113 N86-23851

FLOORS

Survey of NASA research on crash dynamics

{NASA-TP-2298} p 133 N84-21901

Full-scale crash-test evaluation of two iced-limiting

subfloors for general aviation airframes

[NASA-TP-23801 p 134 N85-13267

FLORIDA

Aehat color infrared photography: Applications in

citriculture --- Florida

{NASA.RP-1067J p 139 N8t-21437

Application of a Gaussian multitayer diffusion model to

characterize dispersion of vertical HCi column density in

rocket exhaust clouds

[NASA-TP-1956} p 149 N82-14672

Airborne measurements of launch vehicle effluent of

STS-2 launch on November 12. 1981 at Cape Canaveral,

Florida

[NASA-TP-2260] p 150 N84-t8764

FLOW CHARACTERISTICS

Theoretical flow characteristics of inlets for tilting-nacelle

VTOL aircraff

[NASA-TP-t205] p 42 N78-21114

Experimental perfect-gas stud,/of expansion-tube flow

characteristics

[NASA-TP-1317} p 106 N79-14327

Characteristics of Mach 10 transitional and turbulent

boundary layers

{NASA-TP-1243] p 106 N79-14328

Design of high-perveance confined-flow guns for

periodic-permanent - magnet - f ocused tubes

{NASA-TP-1485] p 101 N79-27400

Description and calibration ot the Langley unitary plan

wind tunnel

{NASA-TP-1905} p 18 N82-12035

Flow in a torsionally oscillating filled cylinder

[NASA-TP-2115} p 110 N83-16674

Recent modifications and calibration of the Langley

low-turbulence pressure tunnel

[NASA-TP-23281 p 24 N84-27675

Vortex-generating coolant-flow-passage design for

increased film-cooling effectiveness and surface

coverage

{NASA-TP-2386} p 1t2 N85-t2314

Flow through very porous screens

[NASA-TP-2436} p 1t2 N85-20270

Transition in Turbines

[NASA-CP-2386] p 113 N65-31433

FLOW CHARTS

Programmers manual for MMLE3, a general FORTRAN

program for maximum likelihood parameter estimation

{NASA-TP-1690] p 176 N81-27613

FLOW COEFFICIENTS

Experimental flow coefficients of a full-coverage

film-cooled-vane chamber

[NASA-TP-t0351 p 41 N77-32153

FLOW DIRECTION INDICATORS

Miniature flow-direction and airspeed sensor for

airplanes and radio controlled models in spin studies

{NASA-TP-t467J p 38 N79-2306t

FLOW DISTORTION

Effect of rotor meridional velocity ratio on response to

inlet radial sod circumferential distortion

{NASA-TP-1278J p 45 N79-28177

An experimental investigation of two large annular

diffusers with swirling and distorted inflow

INASA-TP-1628I p t4 N80-17984

Computer analysis of flow perturbations generated by

placement of choke bumps in a wind tunnel

tNASA-TP-1892I p 18 N81-30088

Amplified crossflow disturbances in the laminar boundary

layer on swept wings with suction

INASA-TP-1902I p 109 N82-1139t

Supersonic jet noise generated by large scale

instabilities

iNASA-TP-2072J p 188 N82-34189

FLOW DISTRIBUTION

Inviscid, nonadiabatic flow fields over blunt, sonic corner

bodies for outer planet entry conditions by a method of

integral relations

(NASA-TP-1133i p 104 N76-18363

A distributed vortex method for computing the vortex

field of a missile

INASA-TP-1183] p 6 N78-25058

A correlation of mixing noise from coannular }eta with

inverted flow profiles

[NASA-TP-t301J p 187 N79-22849

Investigation of flow characteristics over missile bodies

at supersonic speeds

[NASA-TP-t579J p 13 N80-13001

Progress in turbulence modeling for complex flow fields

including effects of compressibility

[NASA-TP-t517] p 107 N80-20527

Aerodynamic performances of three fan stator designs

operating with rotor having tip speed of 337 meters per

second and pressure ratio of 1.54. Relation of analytical

code calculations to experimental performance

INASA-TP-1614] p 46 N80-21324

Investigation of the ftow field surrounding circular-arc

boattail nozzles at subsonic speeds

{NASA-TP-t633J p 14 N80-22262

An improved viscous characteristics analysis program

[NASA-TP-t289J p 108 N81-12356

The high-speed frontier Case histones of four NACA

programs, 1920- 1950

[ NASA-SP-445] p 3 N81-15969

Steady and nonsteedy supersonic turbulent afferbody

flow

{NASA-TP-1769} p 16 N81-16977

Numencal analysis of the scramlet-iniet ftow field by

using two-dimensional Navier-Stokes equations

[NASA-TP-1940] p 46 N62-13142

Simulator study of vortex encounters by a twin-engine,

commercial, jet transport airplane

[NASA-TP-1966] p 57 N82-19225

Effects of axisymmetric and normal air jet plumes and

solid plume on cylindrical afferbody pressure distributions

at Msch numbers from 1.65 to 2.50

I NASA-TP-2005 } p 19 N82-22215

Flow Visualization and Laser Velocimetry for Wind

Tunnels

{ NASA-CP-2243] p 116 N82-32663

Analytical and experimental investigation of stator

endwall contouring in a small axial-flow turbine. 1: Stator

performance

I NASA-TP-20231 p 49 N63-11 t 25

The aerodynamic performance of several flow control

devices for internal flow systems

{NASA-TP-1972I p 59 N93-17560

Theoretical and experimental engine-inlet flow fields for

fighter forebodies

I NASA-TP-2270 ] p23 N84-t 7132

Test-engine and inlet performance of an aircraft used

for investigating flight effects on fan noise

INASA-TP-2254} p 189 N84-21277

Magnetohydrodynamic power generation

[NASA-TP-2331 ] p 195 N84-25458

A new method for determining scousttcJiner admittance

in a rectangular duct with grazing flow from experimental

data

INASA-TP-2310} p 190 N84-27543

Fuselage and nozzle pressure distributions of a

1/12-scale F-15 propulsion model at transonic speeds

Effect of fuselage modifications and nozzle variables

INASA-TP-2333] p 24 N64-32354

Experimental trim drag values and flow-field

measurements for a wide-body transport model with

conventional and supercritical wings

[NASA-TP-2071] p 25 N85-10920

Wind Tunnel Wall Interference Assessment and

Correction, 1983

[NASA-CP-2319} p 25 N85-12011

Effect of two inner-ring oil-flow distribution schemes on

the operating characteristics of a 35 millimeter bore ball

bearing to 2.5 million DN

[NASA-TP-2404J p 124 N85-13233

Aerothermal tests of a 12.5 percent cone at Mach 6.7

for various Reynolds numbers, angles of attack and nose

shapes --- conducted in Langley 8-foot high temperature

tunnel

[ NASA-TP-2345} p 112 N85-17322

Flow through very porous screens

[NASA-TP-2436J p 1t2 N85-20270

Static and dynamic pressure measurements on a NACA

0012 airfoil in the Ames High Reynolds Number Facility

{NASA-TP-2465} p 26 N85-27823

Wind Tunnel Seeding Systems for Laser Velocimetets

[NASA-CP-2393J p 116 N86-11437

A method for determining acoustic-liner admittance in

ducts with sheared flow in two-cross-sectionel directions

{NASA-TP-2518J p 190 N86-13056

Mach 6 flow field surveys beneath the forebody of an

airbreathing missile

{NASA-TP-2491 } p 28 N86-23558

FLOW EQUATIONS

Temporal and spatial inconsistencies of time-split

finite-difference schemes

{NASA-TP-1790] p 182 N81-22754

Computer program for calculating full potential transonic,

quasi-three-dimension al flow through a rotating

turbomachinary blade row

{NASA-TP-2030I p 20 N82-28247

Breakdown of the conservative potential equation

[NASA-TP-25391 p 28 N86-20352

FLOW GEOMETRY

The Numerical Studies Program for the Atmospheric

General Circulation Experiment (AGCE) for Spacelab

Flights

{NASA-CP-2200] p 163 N82-12715

FLOW MEASUREMENT

TACT1, a computer program for the transient thermal

analysis of a cooled turbine blade or vane equipped with

a coolant insert. I Users manual

[NASA-TP-1271 } p 105 N76-26374

A laser vbiocimeter flow survey above a stalled wing

[NASA-TP-1266} p 10 N79-14019

In-flight transition measurement on a 10 dog cone at

Mach numbers from 05 to 2.0

[NASA-TP-1971 I p 19 N82-26227

Detailed flow measurements in casing boundary layer

of 42g-meter-per-second-tip-speed two-stage fan

{ NASA-TP-2052} p 51 N64-28795

Calibration of sonic valves for the laminar flow control,

leading-edge flight test

[NASA-TP-2423} p 26 N85-23707

FLOW RESISTANCE

A siphon method of determining resistivities of thin

heat-pipe wicks

{NASA-TP-t304} p 106 N79-10379

FLOW STABILITY

Performance of a vortex-controlled diffuser in an annular

swirl-can combustor at inlet Mach numbers up to 0.53

[NASA-TP-1452] p 44 N79-22099

A throat-bypass stability-bleed system using relief valves

to increase the transient stability of a mixed-compression

inlet --- YF-12 aircraff inlet tests in the Lewis 10 by 10 ff

supersonic wind tunnel

[NASA-TP-1083] p 45 N79-28176

The wave structures of the Lady model of baroclinic

instability

[NASA-TP-1546} p 160 N79-32796

Supersonic jet noise generated by large scale

instabilities

INASA-TP-2072} p 168 N82-34189

FLOW THEORY

Crossflow effects on steady and fluctuating pressures

on an ogive-cylinder cone-frustum model in supersonic

separated flow

[NASA-TP-1951 ] p 18 N82-13108

FLOW VELOCITY

Representation of turbulent shear stress by a product

of mean velocity differences

[NASA-TP-10291 p 104 N77-31441

Lubrication of optimized-design tapered-roller bearings

to 2.4 million DN

[NASA-TP-1714) p 121 N80-29734

Effect of hole geometry and Electric-Discharge

Machining (EDM) on airflow rates through small diameter

holes in turbine blade material

[NASA-TP-1716} p 47 N81-t2089

Evaluation of flow quality in two large NASA wind tunnels

at transonic speeds

[NASA-TP-17371 p 108 N81-13303

High-speed laser anemometer system for intrarotor ftow

mapping in turbomachinery

[NASA-TP-1663] p 115 N82-19521

Flow through aligned sequential orifice type inlets

[NASA-TP-1967] p 10g N62-20467

A-52
SUBJECT INDEX FORCE-FREE MAGNETIC FIELDS

Velocity gradient method for catulating velocities in an

axisymmetric annular duct

[NASA-TP-2029} p 20 N82-29270

A new method for determining acoustic-liner admittance

in a rectangular duct with grazing flow from expenmental

data

[NASA-TP-2310] p 190 N84-27543

Flow rates and pressure profiles for one to four axially

alined Borda inlets

[NASA-TP-2390) p 112 N85-14078

Flow rate and pressure profiles for 1 to 4 axially alined

orifice inlets

{NASA-TP-2460} p 112 N85-27165

FLOW VISUALIZATION

FlOW visualization of film cooling with spanwise injection

from a small array of holes and compound-angle injection

from s large array

{ NASA-TP-t 1 g5] p42 N78-21113

Holography through optically active windows

[NASA-TP-1414] p 114 N79-17195

Flow visualization of discrete-hole film cooling with

spanwise injection over a cylinder

INASA-TP-1491 ] p 44 N79-27142

Some flow phenomena associated with aligned,

sequential apertures with Borda-type inlets --- inlet

pressure and flow separation

[NASA-TP-1792} p 109 N81-24387

Effects of vortex flaps on the low-speed aerodynamic

characteristics of an arrow wing

INASA-TP-1914] p3 N82-11013

Fringe localization requirements for three-dimensional

flow visualization of shock waves in diffuse-illumination

double-pulse holographic interferometry

[NASA-TP-1868} p 115 N82-22481

Flow Visualization and Laser Velocimetry for Wind

Tunnels

[NASA-CP-2243] p 116 N82-32663

Natural laminar flow experiments on modern airplane

surfaces

[NASA-TP-2256] p 24 N84-26660

Lee-side flow over delta wings at supersonic speeds

[NASA-TP-2430] p 26 N85-2992f

New techniques for experimental generation of

two-dimensional blade-vortex interaction at low Reynolds

numbers

[NASA-TP-2551] p 191 N86-21280

Optical elements formed by compressed gases:

Analysis and potential applications

[NASA-TP-2555] p 194 N86-22390

FLUCTUATION THEORY

Low-frequency fluctuation spectra and associated

particle transport in the NASA Lewis bumpy-torus

plasma

[NASA-TP-1258] p 194 N78-30944

FLUID DYNAMICS

Evaluation of a vortax model of turbulent cavity flow

--- for computing noise generation of fluid flow

{NASA-TP-1505] p 187 N79-32057

The wave structures of the Eady model of baroctinic

instability

{NASA-TP-1548} p 160 N79-32796

Modeling of space vehicle propellant mixing --- cryogenic

propellants

[NASA-TP-2107] p 97 N83.16545

Finite-difference fluid dynamics computer mathematical

models for the design and interpretation of experiments

for space flight --- atmospheric general circulation

experiment, convection in a float zone, and the

Bridgman-Stockbarger crystal growing system

[NASA-TP-2323] p 112 N84-23852

Three-dimensional bsroclinic instability of a Hadley cell

for small Richardson number

[NASA-TP-24501 p 166 N85-20605

Second Workshop on Spacecraft Glow

[NASA-CP-2391] p 201 N86-13239

FLUID FILMS

Minimum film thickness in elliptical contacts for different

regimes of fluid-film lubrication

[NASA-TP-1342] p 119 N78-33447

FLUID FLOW

The effects of curvature and viscosity on baroclinic

instability: A two-layer model

[NASA-TP-1328] p 15g N78-32641

Compressible flow across narrow passages:

Comparison of theory and experiment for face seals

_NASA-TP-1346] p 120 N79-t0424

Numerical grid generation techniques ---conference

(NASA-CP.2166] p 182 N81-14690

Fundamental heat transfer research for gas turbine

engines

[NASA-CP-2178] p 48 N81-24063

GRtD30: Computer program for fast generation of

multilevel, three-dimensional boundary-conforming O-type

computational grids

[NASA-TP-t9201 p 18 N81-31128

Combustion Fundamentals Research

[NASA-CP-2309J p 51 N84-20525

A preliminary study of numerical simulation of

thermosolutsi convection of interest to crystal growth

INASA-TP-2394] p 112 N85-13175

FLUID INJECTION

FlOW visualization of film cooling with spanwise injection

from a small array of holes and compouod-angie injection

from a large array

INASA-TP-1195] p 42 N78-21113

Direct measurements and analysis of skin friction and

cooling downstream of multiple flush-slot infection into a

turbulent Mach 6 boundary layer

[NASA-TP-1176] p 106 N78-33385

Effect of steam addition on cycle performance of simple

and recuperated gas turbines

[NASA-TP-1440] p 144 N79-22626

FLUID JETS

Liquid jet impingement normsi to a disk in zero gravity

[NASA-TP-t017] p 104 N77-30413

Capillary and acceleration wave breakup of liquid jets

in axial-flow airstreams

[NASA-TP-1791 ] p 109 N81-t6417

FLUID MANAGEMENT

Liquid management in low gravity using baffled rotating

containers

[NASA-TP-2263] p 111 N84-15427

FLUID MECHANICS

Draining characteristics of hemispherically bottomed

cylinders in a low-gravity environment

[NASA-TP-1297] p 106 N78-31384

Spacecraft Dynamics as Related to Laboratory

Experiments in Space --- conference

[NASA-CP-2199] p 72 N82-12109

Mechanics of liquid helium in a partially filled rotating

dewar in low gravity with application to Gravity Probe-B

{NASA-TP-2124] p it0 N83-166.80

Comparison of two- and three-dimensional flow

computations with laser anemometer measurements in a

transonic compressor rotor

[NASA-TP-1931] p 22 N83-32774

Fluid surface behavior in low gravity, Center

discretionary fund no 83-21

{NASA-TP-2486] p 113 N85-282S0

Transition in Turbines

{NASA.CP-2386} p 113 N85-31433

FLUID POWER

Rotordynamic instability Problems in High-Performance

Turbomechinery

[NASA-CP-2338} p 124 N85-14116

FLUIDIZED BED PROCESSORS

Elastic-plastic finite-element analyses of thermally

cycled single-edge wedge specimens

[NASA-TP-f982] p 130 N82-20565

Development of a simplified optical technique for the

simultaneous measurement of particle size distribution and

velocity

[NASA.TP-2185J p 194 N83-27846

FLUORESCENCE

Laboratory tank studies of a single species of

phytopienkton using a remote sensing fluorosensor

[NASA-TP-1821} p 13g N81-20492

Oceanic Lidar

[NASA-CP-2194] p 168 N81.31801

FLUORIDES

Effect of thermal exposure on lubricating properties of

polyimide films end polyimide-bonded graphite fluoride

films

[NASA-TP-1125] p 91 N78-15277

FLUORINE COMPOUNDS

Chlorofluoromethanes and the stratosphere

[NASA-RP-t0f0] p 151 N77-31694

FLUOROSCOPY

Preliminary applications and evaluation results.

Lixiscope: Proceedings of the Lixiscope Conference

[ NASA.CP-2112 ] p 114 N80-12384

FLUTTER

An experimental and analytical investigation of proprotor

whirl flutter

[NASA.TP-1047] p 6 N78-12039

A method for: obtaining practical flutter-suppression

control laws using results of optimal control theory

[NASA-TP-1471] p t28 N79-28614

Application of two design methods for active flutter

suppression and wind.tunnel test results

[NASA-TP-1683} p 129 N80-22737

Flutter analysis of an airplane with multiple structural

nonlinearities in the control system

{NASA-TP-1620} p 55 N80-24324

Wind-tunnel experiments on divergence of

forward-swept wings

[NASA-TP-1685] p 34 N80-29287

Comparison of analytical and wind-tunnel results for

fiofter and gust response of a transport wing with active

controls

[NASA-TP-20t0] p 131 N82-26703

Formulation of blade-flutter spectral analyses in

stationary reference frame

[NASA-TP-2296] p 51 N84-20562

STABCAR: A program for finding characteristic root

systems having transcendental stability matrices

[NASA-TP-21651 p 179 N84-27461

KC-t 35 Winglet Program Review

[NASA-CP-2211 } p 24 N84-27686

FLUTTER ANALYSIS

Flutter Testing Techniques

[NASA-SP-415} p t N77-2t022

Development and application Of an optimization

procedure for flutter suppression using the aerodynamic

energy concept

[NASA-TP-1137] p 127 N78-18459

Analysis of preflutter and postflutter characteristics with

motion-matched aerodynamic forces

[NASA-TP-1232] p 127 N78-28481

An analytical technique for predicting the characteristics

of a flexible wing equipped with an active

flutter-suppression system and comparison with

wind-tunnel data

{NASA-TP-1367] p 128 N79-t7264

Classical aerodynamic theory

[NASA-RP-1050] p 13 N80-15033

Experimental and analytical transonic flutter

characteristics of a geared-elevator configuration

{NASA-TP-16661 p 34 N80-25321

Longitudinal and lateral static stability and control

characteristics of a 1/6-scale model of s remotely piloted

research vehicle with a supercritical wing

[NASA-TP-1360] p 57 N82-15075

Application of modal control to wing-flutter

suppression

[NASA-TP-1983] p 57 N82-24209

Generalization of the subsonic kernel function in the

s-plane, with applications to flutter analysis

[NASA-TP-2292] p 23 N84-20480

FLY BY WIRE CONTROL

Advanced aerodynamics and active controls Selected

NASA research

[NASA-CP-2172] p 3 N51-19001

FLYBY MISSIONS

Space missions to comets

[ NASA-CP-2089 } p 206 N80-11972

Voyage to Jupiter

[NASA-SP-439] p 206 N81-10910

Pioneer: First to Jupiter, Saturn, and beyond

[NASA-SP.446] p 206 N81-15925

FLYING PLATFORMS

Parametric study of microwave.powered high.sititude

airplane platforms designed for linear flight

[NASA-TP-lgla} p 35 N82-f 1050

FLYWHEELS

Integrated Flywheel Technology, 1983

[NASA-CP-2290J p 77 N84-12228

An Assessment of integrated Flywheel System

Technology

[NASA-CP-2346] p 78 N85-13850

FOAMS

Cryogenic foam insulation: Abstracted publications

[NASA-RP-t002] p 79 N78-11200

Evaluation of a low.density polyimide foam in a dynamic,

high temperature environment

[NASA-TP-t049] p 91 N78-12223

FOCUSING

Efficiency enhancement of dual.mode traveling wave

tubes at saturation and in the linear range by use of

sbent-beam refocusing and multistage depressed

collectors

[NASA-TP-1486] p 101 N79-28420

Experimentsi verification of the multistage depressed

collector design procedure for s high-perveencel

helix-type, traveling-wave tube --- in communications

satellites

{NASA°TP-2162} p 102 N83-25985

FOIL BEARINGS

Experimental evaluation of foil-supported resilient-pad

gas-lubricatecl thrust bearing

{NASA-TP-1030} p 118 N77-31502

FOLDING STRUCTURES

The 18th Aerospace Mechanisms Symposium

[NASA-CP-2311 ] p t33 N84-25078

FOOD PROCESSING

Food Service and Nutrition for the Space Station

[NASA-CP-2370] p 174 N85-24733

FORCE DISTRIBUTION

Flight and wind-tunnel comparisons of the inlet-airframe

interaction of the F-t 5 airplane

[NASA-TP-23741 p 37 N85-12884

A study of the cornering forces generated by aircraft

tires on a tilted, free-swiveling nose gear

[NASA-TP-2481] p 135 N86-11522

FORCE-FREE MAGNETIC FIELDS

Measurements of Solar Vector Magnetic Fields

[NASA-CP-2374] p 210 N85-29869

A-53
FOREBODIES SUBJECT INDEX

FOREBOOIES

A theoretical investigabon of forebody shapes designed

for natural laminar boundary-layer flow

[NASA-TP*1375] p 11 N79-15903

Effects of fuselage forebody geometry on tow-speed

lateral-directlonat characteristics of twin-tail fighter model

at high angles of attack

[NASA-TP-f592j p 13 N80.13002

A procedure for designing fotebodiea with constraints

on cross-section shape and axial area distribution

INASA-TP-1881] p 17 N81-26078

Aerodynamic characteristics of a sanes of bodies with

variations in nose camber

[NASA-TP-2206} p 22 N83-34904

Theoretical and experimental engine-inlet flow fields for

fighter forebodioa

{NASA-TP-2270} p 23 N84-17132

FORECASTING

Applications systems verification and transfer project,

Volume 3: Operational applications of satellite snow cover

observations in California

[NASA-TP-1824] p 140 N82.20619

Applications systems venfication and transfer project.

Volume 4: Operational applications of satellite snow cover

observations. Colorado Field Test Center

[NASA-TP-1825} p 140 N82-20620

Applications systems verification and transfer project.

Volume 5: Operational applications of satellite snow-cover

observations, northwest United States

[NASA-TP-1826] p 140 N82-20621

Applications systems verification and transfer project.

Volume 7: Cost/benefit analysis for the ASVT on

operational applications of satellite snow-cover

observations

[NASA-TP-1828} p t41 N82-20623

Applications systems verification and transfer project

Volume 8: Satellite snow mapping and runoff prediction

handbook

[NASA-TP-t829] p 141 N82-20624

FORESTS

Wildland inventory and resource modeling for Douglas

and Carson City Counties, Nevada, using LANDSAT and

digital terrain data

[E83-103021 p 142 N83-27293

FORGING

Characterization of large 2219 aluminum alloy hand

forgings for the space shuttle solid rocket booster

{NASA-TP-1383} p 87 N79-16950

FORMING TECHNIQUES

Fabrication end evaluation of superptastically

formed/weld-brazed corrugated compression panels with

beaded webs

{NASA-TP-25121 p 90 N86-13406

FORTRAN

User's guide to SFTRAN/1100

{NASA-TP-1200} p 178 N78-20806

Applicatton of special-purpose digital computers to

rotorcreft real-time simulation

[NASA-TP-1267} p 32 N78-27t13

An improved viscous characteristics analysis program

[NASA-TP-1289] p 108 N81-12356

User's manual for MMLE3. a general FORTRAN program

for maximum likelihood parameter estimation

{NASA-TP-1563] p 176 N81-12744

Programmer's manual for MMLE3, a general FORTRAN

program for maximum hkelihood parameter estimation

{NASA-TP-1690} p 176 N81-27813

STGSTK: A computer code for predicting multistage

axial flow compressor performance by s meenline stage

stacking method

{NASA-TP-2020J p 49 N82-25250

FORWARD SCAT'rERING

Particle sizing by measurement of forward-scattered light

at two angles

{NASA-TP-2156} p 50 N83-24509

FRAGTIONATION

Characterization of soil and postlaunch pad debris from

Cape Canaveral taunch complex end analysis of soil

_nteraction with aqueous HCt

INASA-TP-2076) p 150 N83-12595

FRACTURE MECHANICS

Advances in engineering science, volume 2

I NASA-CP-200t-VOL-2] p 98 N77-10265

Mechanical behavior and fracture characteristics of

off axis fiber composites, I: Experimental investigation

--- at the Lewis Research Center

1NASA-TP-1081 } p 79 N78-13138

A relation between semiempirical fracture analyses and

F:l-curves

I NASA-TP-1600} p t29 N80-15428

Experimental and analytical investigation of the fracture

processes of boron/aluminum laminates containing

notches

j NASA-TP-21871 p 82 N83-33956

Nonlinear Constitutive Relations for High Temperature

Applmatidns

[NASA-CP-2271] p 132 N83.34351

Metallurgical characterization of the fracture of several

high strength aluminum alloys

INASA-TP-t086] p 85 N84-11230

FRACTURE STRENGTH

Mechanical behavior end fracture characteristics of

off.axis fiber composites, 2: Theory and comparisons

{NASA-TP-1082] p 79 N78-16098

A relation between semiemplrical fracture analyses and

R-curves

[NASA-TP-1600} p 129 N80-15428

Fracture toughness of boron/aluminum laminates with

various proportions of 0 deg and plus or minus 45 deg

[NASA-TP-1707] p 81 N81-tllf5

Method for estimating crack-extension resistance curve

from residual strength data

{NASA-TP-1753] p 129 N81-11417

Fracture temperature and flaw growth in nitronic 40 at

cryogenic temperatures

{NASA-TP-2312] p 89 N84-23750

Fracture toughness of fibrous composite materials

I NASA-TP-2370J p 83 N85-11 t36

Tough Composite Materials

[NASA-CP-2334] p 83 N85-12941

FRACTURES (MATERIALS)

Anisotropic friction, deformation, and fracture of

single-crystal silicon carbide at room temperature

lNASA-TP-1525] p 93 N79-30380

Nonlinear Structural Analysis

[NASA-CP-2297J p 133 N84-31688

FRACTURING

Structural Integrity and Durability of Reusable Space

Propulsion Systems

[NASA-CP-2381] p 78 N85-27941

Surface fatigue life and failure characteristics of EX-53,

CBS 1000M, and AIS] 9310 gear matenals

[NASA-TP-2513] p 125 N86-12609

FRAGMENTATION

Atmospheric entry and fragmentation of dense

meteoroids

[NASA-TP-1333] p 205 N79-14978

An abrasion-ablation model description of galactic

heavy-ion fragmentation

{NASA-TP-23051 p 192 N84-22396

A T-matrix theory of galactic heavy-idn fragmentation

{NASA-TP-23631 p 193 N85-17690

FREE CONVECTION

Approximate analysis of thermal convection in a

crystal-growth cell for Spacetab 3

[NASA-TP-20161 p 62 N82-29335

FREE FLIGHT

The science and technology of low speed and motodess

flight, part 1

[NASA-CP-2085-PT-1 ] p 2 N79-23889

FREE FLOW

Wind-tunnel investigation at supersonic speeds of a

canard-controlled missile with fixed and free-roiling tail

fins

INASA-TP-1316} p 9 N78-32067

Evaluation of flow quality in two large NASA wind tunnels

at transonic speeds

{NASA-TP-1737} p 108 N81-13303

Experimental investigation of two nonaxisymmetric

wedge nozzles at free stream Mach numbers up to 1.20

[NASA-TP-2054J p 20 N82-32322

Performance test of laser velocimeter system for the

Langley 16-foot transonic tunnel

[NASA-TP-2502] p 118 N86-16563

FREE JETS

Liquid jet impingement normal to a disk in zero gravity

{NASA-TP-1017J p 104 N77-30413

A comparison of the noise produced by a small jet on

a moving vehicle with that in a free jet --- jet mixing

noise

{NASA-TP-1326} p 186 N79-14872

Stochastic analysis of spectral broadening by a free

turbulent shear layer

INASA-TP-1816} p 188 N8t-24854

Aeronautical facilities catalogue. Volume 2: Airbrealhing

propulsion and flight simulators

[NASA-RP-1133] p 60 N86-18328

FREEZING

Design of a blood-freezing system for leukemia

research

[NASA-TP-1165] p 169 N78-18673

FREQUENCIES

Guidelines for spaceborne microwave remote sensors

{NASA-RP-t0861 p 140 N82-19647

FREQUENCY ANALYZERS

Time and frequency domain analysis of sampled data

controllers via mixed operation equations

[NASA-TP-1817) p 72 N81-25139

Reduced order feedback control equations for linear time

and frequency domain analysis

{NASA.TP-1818] p 72 N8t.25140

FREQUENCY ASSIGNMENT

Guidelines for speceborne microwave remote sensors

(NASA-RP-f086} p 140 N82-19647

FREQUENCY MEASUREMENT

Measurements of the tonal component of cavity noise

and comparison with theory --- aircraft noise

[NASA-TP-1013} p 185 N78-12800

Applied Routh approximation

[NASA-TP-1231} p 98 N78-22257

FREQUENCY MODULATION

Carrier-intarference ratios for frequency sharing between

frequency-modulated

bend television systems

[NASA-TP-1264] p 69 N78-28159

FREQUENCY RESPONSE

Spatial.frequency response of the limb infrared monitor

of the stratosphere

[NASA-TP-1504] p 148 N79-29679

FREQUENCY STANDARDS

Proceedings of the 12th Annual Precise Time and Time

Interval (PTFt) Applications and Planning Meeting

[NASA-CP-2175] p 117 N81-27467

Proceedings of the 14th Annual Precise Time and Time

interval (PFFI) Applications Planning Meeting

[NASA-CP-2265] p 118 N83-35351

FRESNEL LENSES

An analytical and experimental investigation of a 1.8

by 3.7 meter Fresnel lens solar concentrator

[NASA-TP-1005} p 144 N77-30617

FREI"rING

influence of fretting on flexural fatigue of 304 stainless

steel and mild steel

[NASA-TP-1193J p86 N78-21269

Effect of humidity on fretting wear of several pure

metals

[NASA-TP-2403] p 90 N85-13006

FRICTION

Effect of carbon content on friction and wear of cast

irons

[NASA-TP-1052] p 85 N77-32286

Friction and wear of radiofrequency-sputtered bohdes,

silicides, and carbides

{NASA-TP-1156] p 91 N78-20338

Effect of oxygen and nitrogen interactions on friction

of single-crystal silicon carbide

[NASA-TP-1265J p 92 N78-28247

Effect of nitrogen-containing plasma on adherence,

friction, and wear of radiofrequency-sputtered titanium

carbide coatings

[NASA-TP-1377] p 92 N79-15184

Friction and wear characteristics of wire-brush skids

[NASA-TP-t495] p 33 N79-2917f

Changes in surface chemistry of silicon carbicle (0001)

surface with temperature and their effect on friction

[NASA-TP-1756} p 94 N8t-14079

Surface chemistry and friction behavior of the silicon

carbide (0001) surface at temperatures to 1500 dog C

[NASA-TP-1813] p 94 N81-19300

Tdbological properties at 25 C of seven polyimide films

bonded to 440 C high-temperature stainless steel

INASA-TP-1944] p 94 N82-19373

Fdction and wear of iron in corrosive metal

{NASA-TP-1985} p 88 N82-20291

Friction and surface chemistry of some ferrous-base

metallic glasses

[NASA-TP.1991} p 88 N82-21301

Tire tread temperatures during antiskid braking and

cornering on a dry runway

INASA-TP-2009] p 35 N82-24193

Frictional heating due to asperity interaction of

elastohydrodynamic line-contact surfaces

[NASA-TP-1882] p 122 N82-25514

X-ray photoeioctron spectroscopy and friction studies

of nickel-zinc end manganese-zinc tarrites in contact with

metals

{NASA-TP-21631 p88 N83-23419

Friction and wear behavior of aluminum and composite

airplane skins

[NASA-TP-2262J p 37 N84-f7175

Water-vapor effects on friction of magnetic tape in

contact with nickel-zinc ferrite

INASA-TP-2279} p 95 N84-18399

Triboiogy in the 80's Volume 1: Sessions 1 to 4

{NASA-CP-2300-VOL-1 ] p 124 N84-23891

Tribology in the 80's Volume 2: Sessions 5 - 8

[NASA-CP-2300-VOL-2] p 124 N84-25047

Erosion of iron-chromium alloys by glass particles

{NASA-TP-2354] p 90 N84-28965

Surface roughness effects in etastohydrodynamic

contacts

I NASA-TP-2488J p 125 N85-32329

A-54
SUBJECT INDEX GALACTIC STRUCTURE

FRICTION FACTOR

X-Ray photoelectron spectroscopy study of

radiofrequency-sputtered titanium, carbide, molybdenum

carbide, and titanium boride coatings and their friction

properties

[NASA-TP-1033] p 91 N77-33348

Surface chemistry, microstructure and friction properties

of some ferrous.base metallic glasses at temperatures to

750 C

[NASA-TP-2006] p 88 N82-22349

FRICTION MEASUREMENT

Friction characteristics of three 30 by t 1.5-14.5, type

8, aircraft tires with various tread groove patterns and

rubber compounds

[NASA-TP-t080] p 32 N78-13043

Some effects of composition on friction and wear of

graphite-fiber-reinforced polyimide liners in plain spherical

bearings

[NASA.TP.1229] p 119 N78-25433

Direct measurements and analysis of skin friction and

cooling downstream of multiple flush-slot injection into a

turbulent Mach 6 boundary layer

[NASA-TP-1176] p 106 N78-33385

Measurement of rolling friction by a damped oscillator

[NASA-TP-2257} p 123 N84-13577

Friction behavior of silicon in contact with titanium, nickel,

silver and copper

[NASA.TP.2362] p 96 N84-33590

FRICTION REDUCTION

Effect of oxygen, methyl meroaptan, and methyl chloride

on fdction behavior of copper-iron contacts

[NASA-TP-1309] p 86 N78-30206

Surface chemistry of iron sliding in air and nitrogen

lubricated with hexedecane and hexadecane containing

dibenzyl-dilsulfide

[NASA-TP-1545] p 79 N79-31346

Lubrication of machine elements

[NASA.RP-1126] p 124 N84-31640

Friction behavior of silicon in contact with titanium, nickel,

silver and copper

[NASA-TP-2362] p 96 N84-33590

FRONTS (METEOROLOGY)

Fronts and frontogenesis as revealed by high time

resolution data

[NASA-RP-1005} p 158 N77-30705

A comparative analysis of rawinsonde and NIMBUS 6

and TIROS N satellite profile data

[NASA-RP-t070] p 162 N81-t5640

Atmospheric structure determined from satellite data

[NASA-RP-10711 p 162 Nat-t6678

Current Scientific Issues in Large Scale Atmospheric

Dynamics

[NASA-CF-2410} p 167 N86-24082

FROST

Water vapor measurement system in global atmospheric

sampling program, appendix

[NASA-TP-2051 J p 150 N83-t3643

FRUSTUMS

Crossflow effects on steady and fluctuating pressures

on an ogive-cylinder cone-frustum model in supersonic

separated flow

[NASA-TP-1951 ] p 18 N82-13108

FUEL COMBUSTION

Computer program for obtaining thermodynamic and

transport properties of air and products of combustion of

ASTM-A-t fuel and air

[NASA-TP-lt60} p 97 N78-20351

Effect of swirler-mounted mixing venturi on emissions

of flame-tube combustor using jet A fuel

[NASA-TP-1393J p 44 N79-t4099

Premixed Prevaporized Combustor Technology Forum

[NASA-CP-20781 p 44 N79-24994

Aircraft Research and Technology for Future Fuels

[NASA-CP-2146} p 47 N80-29300

Effect of fuel-air-ratic nonuniformity on emissions of

nitrogen oxides

{NASA-TP-1796] p 48 N82-13143

Combustion gas properties I-ASTM jet A fuel and dry

air

{NASA-TP-2359] p 51 N85-10064

Ignition of mixtures of Sill sub 4. CH sub 41 O sub 2,

and Ar or N sub 2 behind reflected shock waves

{NASA-TP-2415J p 52 N85-22395

Fuel-rich catalytic combustion: A soot-free technique

for in situ hydrogen-like enrichment

{NASA-TP-2498J p 85 N85-31244

FUEL CONSUMPTION

Implications of fuel-efficient vehicles on ride quality and

passenger acceptance: Workshop proceedings

[NASA-CP-2096} p 199 N80-18990

Analysis of fuel-conservative curved decelerating

approach trajectories for powered-lift and CTOL jet

aircraft

[NASA-TP-1650] p 2 N80-19622

Development and test results of a flight management

algorithm for fuel conservative descents in a time-based

metered traffic environment

{NASA-TP-1717} p 39 N80-33404

Fuel economy in aviation

[NASA-SP-4621 p 36 N84-t5144

KC-135 Winglet Program Review

INASA-CP'221t ] p 24 N84-27686

Reference energy-altitude descent guidance: Simulator

evaluation --- aircraft descent and fuel conservation

{NASA-TP-2383] p 40 N85-16868

Planning fuel-conservative descents in an airline

environmental using a smelt programmable calculator:

Algorithm development and flight test results

[NASA-TP-2393] p 40 N85-26705

FUEL CONTAMINATION

Sound speed measurements in liquid oxygen-liquid

nitrogen mixtures

{NASA-TP-2464] p 98 N85-35307

FUEL INJECTION

Combustion of hydrogen in a two*dimensional duct with

step fuel injectors

[NASA-TP.f15g] p 42 N78-23093

Interaction between step fuel injectors on opposite walls

in a supersonic combustor model

[NASA-TP-1174] p 42 N78-23094

Reverse-flow combustor for small gas turbines with

pressure-atomizing fuel injectors

[NASA-TP-12601 p 43 N78-27130

Effect of swider.mounted mixing venturi on emissions

of flame-tube combustor using jet A fuel

[NASA-TP-1393] p 44 N79-14099

Low-pressure performance of annular, high-pressure (40

atm) high-temperature (2480 K) combustion system

[NASA-TP-1713] p 47 N80-32396

Capillary and acceleration wave breakup of liquid jets

in axial-flow airstreams

[NASA-TP-1791 } p 109 Nat-t6417

Effect of fuel injector type on performance and emissions

of reverse-flow combustor

[NASA-TP-1945] p 49 N82-15040

Effects of percentage of blockage and f_ameholder

downstream counterbores on lean combustion limits of

premixed, prevaporized propane-air mixture

[NASA-TP-2227] p 50 N83-34941

FUEL PRODUCTION

Aircraft Research and Technology for Future Fuels

[NASA-CP-2146] p 47 N80-29300

Effect of hydroprocessing severity on characteristics of

jet fuel from OSCO 2 and Paraho distillates

{ NASA-TP-17681 p 97 N81-24283

Assessment of Alternative Aircraft Fuels

[NASA-CP-2307] p 51 N84-23630

FUEL SPRAYS

Combustion Fundamentals Research

INASA-CP-23091 p 51 N84-20525

FUEL SYSTEMS

Aviation Gasolines and Future Alternatives

INASA-CP-2267] p 97 N83-22442

Assessment of Alternative Aircraft Fuels

[NASA'CP-2307] p 51 N64-23630

FUEL TESTS

Effect of hydroprocessing severity on characteristics of

jet fuel from OSCO 2 and Paraho distillates

[NASA-TP-f768] p 97 N81-24283

Rapid estimation of concentration of aromatic classes

in middistillate fuels by high-performance liquid

chromatography

[NASA-TP-2495] p 98 N85-31307

FUEL-AIR RATIO

Effect of degree of fuel vaporization upon emissions

for a premixed partially vaporized combustion system ---

for gas turbine engines

[ NASA-TP-15821 p46 N80-14125

Low-pressure performance of annular, high-pressure (40

atm) high-temperature (2480 K) combustion system

{ NASA-TP-1713 j p 47 N80-32396

Spectral flame radtance from a tubular-can combustor

I NASA-TP-17221 p 48 N8t-19121

Performance of semi-transportation-cooled liner in

high-temperature-rise combustors

I NASA-TP-1806J p 48 N61-2t077

Analysis of effect of flameholder characteristics on lean,

premixed, partially vaporized fuel-air mixtures quality and

nitrogen oxides emissions

[NASA-TP-16421 p 48 N81-24065

Effect of fuel-air-ratio nonuniformlty on emissions ot

nitrogen oxides

{NASA-TP-1798] p 48 N62-t3143

Combustion gas properties 2: Natural gas tuet and

dry air

[NASA-TP-2435] p 52 N85-21166

FUELS

Liquid hydrogen as a propulstoc fuel, 1945-1959

{ NASA-SP-4404 ] p 97 N79-16994

Group-type hydrocarbon standards for

high-performance liquid chromatographic analysis of

middistillate fuels

[NASA-TP-2317] p 97 N84-23774

FULL SCALE TESTS

Full-scale wind tunnel-investigation of the Advanced

Technology Light Twin-Engine airplane (ATLIT) --- Langley

full scale tunnel

[NASA-TP-t5gl ] p 14 N80-22266

FUNCTIONAL DESIGN SPECIFICATIONS

Large Deployable Reflector Science and Technology

Workshop. Volume 3: Systems and Technology

Assessment

[NASA-CP.2275.VOL.3} p 202 N84-32318

Vibration, acoustic, and shock design and test criteria

for components on the Solid Rocket Boosters (SRB),

Lightweight External Tank (LWT), and Space Shutlle Main

Engines (SSME)

[NASA-RP-1127] p 134 N85-10405

FUNCTIONS (MATHEMATICS)

A class of nonideal solutions. 2: Application to

experimental data

{NASA-TP-lg30] p 196 N83-23188

Convergence of Newton's method for a single real

equation

[NASA-TP-248g] p 183 N85-28656

FUSELAGES

A theoretical investigation of noise reduction through

the cylindrical fuselage of a twin-engine, propeller-driven

aircraft

[NASA-TP-1325] p 186 N79-1382t

Fuselage and nozzle pressure distributions on a

t/12-scale F-f 5 propulsion model at transonic speeds ---

conducted in langley 16 foot transonic tunnel

[NASA-TP-1521] p 13 N80-11036

Experimental study of noise reduction for an unstiffened

cylindrical model of an airplane fuselage

{NASA-TP-lg64] p 188 N82-14879

Crash tests of four low-wing twin-engine airplanes with

truss-reinforced fuselage structure

[NASA-TP-2070] p 131 N83-10442

The vibration characteristics of a coupled helicopter

rotor-fuselage by a finite element analysis

[NASA-TP-2118} p 36 N83-18714

Pressures measured in flight on the aft fuselage and

external nozzle of e twin-jet fighter

[NASA-TP-2017] p 21 N83-25665

Effect of fuselage upwash on the supersonic longitudinal

aerodynamic characteristics of 2 fighter configurations

[NASA-TP-2330] p 24 N84-27676

Fuselage and nozzle pressure distributions of a

1/12-scale F-15 propulsion model at transonic speeds

Effect of fuselage modifications and nozzle variables

INASA-TP-2333] p 24 N84-32354

Aerodynamic characteristics of a distinct wing-body

configuration at Mach 6: Experiment, theory, and the

hypersonic isolation principle

[NASA-TP-2467} p 27 N85-33107

Ground-based and in-flight simulator studies of flight

characteristics of a twin-fuselage passenger transport

airplane during approach and landing

{NASA-TP-2451 ] p 58 N85-34144

Aerodynamic characteristics of several current

helicopter tail boom cross sections including the effect

of spoilers

[NASA-TP-2506} p 27 N86-20349

G

GALACTIC COSMIC RAYS

Tables of nuclear cross sections for galactic cosmic rays:

Absorption cross sections

(NASA-RP-1134] p 193 N85-27665

Electromagnetic dissociation effects in galactic

heavy-ion fragmentation

[NASA-TP-2527] p 211 N86-21492

GALACTIC EVOI UTtON

Scientific research with the space Telescope:

International Astronomical Union Colloquium no 54 ---

conferences

{NASA-CP-211 t I p 200 N80-22130

GALACTIC RADIATION

An abrasion-ablation model description of galactic

heavy-ion fragmentation

{NASA-TP-2305] p 192 N84-22396

GALACTIC ROTATION

CoUisionless galaxy simulations

[NASA-RP-1037J p 201 N79-24921

GALACTIC STRUCTURE

The structure and content of the galaxy and galactic

gamma rays

INASA-CP-0021 p 199 N77-20977

Molecular clouds and galactic spiral structure

[ NASA-TP-22881 p 204 N84-20457

A-55
GALAXIES

GALAXIES

Advances in Ultraviolet Astronomy: Four Years of tUE

Research

I NASA-CP-22381 p20t N82-31163

Future of Ultraviolet Astronomy Based on Six Years of

IUE Research

tNASA-CP-2349] p 203 N85-20961

GALERKIN METHOD

Reduction methods for nonlinear steady-state thermal

analysis

[ NASA-TP-2098 ] p 110 N83-20032

GALILEAN SATELLITES

Voyage to Jupiter

[NASA-SP-4391 p 206 N81-10910

GALILEO PROBE

Twelfth Space Simulation Conference: Shuttle Plus One

A New View of Space

[NASA-CP-22291 p 73 N82-25291

GALILEO PROJECT

Galileo! Exploration of Jupiter's system

{ NASA-SP-4791 p 208 N86-11137

GALLIUM ARSENIDES

Analysis ol costs of gallium arsenide and silicon solar

arrays for space power applications

[ NASA-TP-1811 j p77 N81-20173

A simple model of space radiation damage in GaAs solar

cells

[NASA-TP-2242] p 192 N84-13978

Effect ot barrier height on friction behavior of the

semiconductors sihcon and gallium arsenide in contact with

pure metals

I NASA-TP-24051 p 96 N85-t 3044

GAME THEORY

A formulation and analysis of combat games

I NASA-TP-2487] p 185 N85-33745

GAMMA RAY ASTRONOMY

Gamma Ray Astrophysics: New insight into the

universe

I NASA-SP-453 ] p204 N82-2t118

Ninteenth International Cosmic Ray Conference OG

sessions, volume 1

I NASA-CP-2376-VOL-t I p 210 N85-33902

GAMMA RAYS

The structure and content of the galaxy and galactic

gamma rays

I NASA-CP-002t p 199 N77-20977

Ninteenth International Cosmic Ray Conference. OG

sessions, volume 1

I NASA-CP-2376-VOL-1 ] p 210 N85-33902

Nineteenth International Cosmic Ray Conference, HE

Sessions. volume 7

[NASA-CP-2376-VOL-7 ] p 21 t N85-35968

Nineteenth international Cosmic Ray Conference

Conference papers: Invited rapporteur, h_hlight,

miscellaneous, volume 9

1NASA-CP-2376-VOL-9 J p211 N86-31483

GAPS

Aerodynamic healing in gaps of thermal protection

system tile arrays in laminar and turbulent boundary

layers

INASA-TP-11871 p 105 N78-28373

Aerothermal environment in chordwise gaps between

split elevons at Mach 68

{NASA-TP-1783] p 109 N81-15237

Analysis of gap heating due 1o stepped tiles in the shuffle

thermal protection system

[NASA-TP-2209] p 74 N83-31713

GAS ANALYSIS

Integrated exhaust gas analysis system for a_rcraft

turbine engine component testing

[NASA-TP-24241 p 116 N85-16100

GAS BEARINGS

Operating characteristics of a cantilever-mounted

resilient-pad gas-lubricated thrust beanng

[NASA-TP-1438] p 120 N79-22518

Film thickness measurement for spiral groove and

Rayteigh step lift pad self-acting face seals

[NASA-TP-2058] p 49 N83-11126

C,estgn analysis of a self-acting spiral-groove ring seal

for counter-rotating shafts

[NASA-TP-2142] p 50 N83-25712

Dynamic behavior of spiral-groove and Rayleigh-Step

self-acting face seals

I NASA-TP-2266J p 51 N84-16181

Dynamic response of film thickness in spiral-groove lace

sea_s

INASA-TP-25441 p 52 N86-15313

GAS COMPOSITION

Review of Spectroscopic Data for Measurements 3f

Stratospheric Species

{NASA-CP-21361 p 192 N80-26125

Combustion gas properties I-ASTM jet A fuel and dry

air

I NASA-TP-2359 j p 51 N85-10064

Combustion gas properties Part 3: Hydrogen gas fuel

and dry air

[NASA-TP-24771 p 52 N85-31058

GAS DENSITY

Effect of vacuum processing on outgassing within an

orbiting molecular shield

[NASA-TP-1980J p 99 N82-19390

GAS DYNAMICS

Numerical Boundary Condition Procedures

{NASA-CP-2201 ] p 182 N81-33856

Mechanics of a gaseous film barner to lubricant wetting

of elastohydrodynamically lubricated conjunctions

{NASA-TP-25001 p 125 N85-32330

Optical elements formed by compressed gases:

Analysis and potential applications

[NASA-TP-2555] p 194 N86-22390

GAS EXPANSION

Performance of a short annular dump diffuser using

suction-stabilized vortices at inlet Macb numbers to 0.41

INASA-TP-1194} p 42 N78-20131

Effects of various assumptions on the calculated liquid

fraction in isentropic saturated equilibrium expansions

[NASA-TP-1682] p 108 N80-25615

GAS FLOW

Thermal stress analysis of ceramic gas-path seal

components for aircraft turbines

{NASA-TP-1437 ] p92 N79-21205

Simulation of ideal-gas flow by nitrogen and other

selected gases at cryogenic temperatures --- transonic flow

in cryogenic wind tunnels

INASA-TP-19011 p 109 N81-324t8

Pockels-effect cetl for gas-flow simulation

INASA-TP'20071 p 115 N82-23515

GCKP84-general chemical kinetics code for gas-phase

flow and batch processes including heat transfer effects

[ NASA-TP-23201 p 85 N84-32446

GAS INJECTION

Velocity field of a round jet in a cross flow for various

jet injection angles and velocity ratios --- Langley V/STOL

tunnel

INASA-TP-1506J p 107 N79-32500

GAS LASERS

A NASA high-power space-based laser research and

applications program

(NASA-SP-464] p 118 N83-27200

GAS LUBRICANTS

Experimental evaluation of foil-supported resilient-pad

gas-lubricated thrust bearing

{NASA-TP-10301 p 118 N77-31502

GAS MIXTURES

Critena for self-ignition of Supersonic hydrogen-air

mixtures

[NASA-TP-t457J p 45 N79-29192

Effect of degree of fuel vaporization upon emissions

lot a premlxed partially vapenzed combustion system ---

for gas turbine engines

[ NASA-TP-t 5821 p46 N80-14125

Combustion gas properlies Part 3: Hydrogen gas fuel

and dry air

[NASA-TP-24771 p 52 N85-31058

Measurement of viscosity of gaseous mixtures at

atmospheric pressure

{NASA-TP-25821 p 1t7 N86-24962

GAS PRESSURE

Low-pressure performance of annular, h_gh-pressure (40

atm) high-temperature (2480 K) combustion system

[NASA-TP-17131 p 47 N80-32396

GAS TEMPERATURE

Recovery and radiation corrections and time constants

of several sizes of shielded and unshielded therrnocouple

probes for measuring gas temperature

[NASA-TP-t099] p 113 N78-15463

GAS TURBINE ENGINES

Lean premixed/prevaporized combustion

[NASA-CP-2016] p 84 N77-33297

Experimental performance of a

13.65-centimeter-tip-diameter tandem-bladed sweptback

centrifugal compressor designed for a pressure ratio of 6

[NASA-TP-t091 ] p 6 N78-11002

Cold-air performance of free-power turbine designed for

lt2-kiiowatt automotive gas-turbine engine 1: Design

Stator-vane-chord setting angle of 35 deg

[NASA-TP-t007] p 42 N78-16053

Reverse-ffow combustor for small gas turbines with

pressure-atomizing fuel iniectors

INASA-TP-1260] p 43 N78-27130

Premixed Prevaporized Combustor Technology Forum

[NASA-CP-2078) p 44 N79-24994

Industry tests of NASA ceramic thermal barner coating

--- for gas turbine engine applications

[NASA-TP-1425] p 44 N79-25023

Effect of degree of fuel vaporization upon emissions

for a premixed partially vaporized combustion system ---

for gas turbine engines

I NASA-TP-1582] p 46 N80-14125

SUBJECT INDEX

Operating characteristics of high-speed, let-lubrioated

35-millimeter-bore ball bearing with a

single-out er-land-guided cage

[NASA-TP-16571 p 121 N80-21753

Extension of simdarity test procedures to cooled engine

components with insulating ceramic coatings

[NASA-TP-16151 p 108 N80-24577

Effect of hole geometry and Electnc-Discharge

Machining (EDM) on airflow rates through small diameter

holes in turbine blade material

[NASA-TP-17161 p 47 N81-12089

Fundamental heat transfer research for gas turbine

engines

[NASA-CP-2178] p 48 N81-24063

Effect of fuel injector type on performance and emissions

of reverse-flow combustor

[NASA-TP-19451 p 49 N82-15040

Multiroller traction drive speed reducer: Evaluation lor

automotive gas turbine engine

[NASA-TP-2027] p 122 N82-26678

Pedormance of a tandem-rotor/tandem-stator

conical-flow compressor designed for a pressure ratio of

3

[NASA-TP-2034] p 20 N83-11058

Analysis of a MIL-L-27502 lubricant from a gas-turbine

engine test by size-exclusion chromatography

[NASA-TP-2063J p 95 N83-16528

Particle sizing by measurement of forward-scattered light

at two angles

[NASA-TP-2156t p 50 N83-24509

Simplified method for nonlinear structural analysis

INASA-TP-2208] p t32 N83-34372

Combustion Fundamentals Research

INASA-CP-2309] p 51 N84-20825

Analysis of a topping-cycle, aircraft, gas-turbine-engine

system which uses cryogenic fuel

INASA-TP-2294] p 51 N84-21549

Overview of zirconia with respect to gas turbine

applications

lNASA-TP-2286] p 95 N84-21740

Assessment of Alternative Aircraft Fuels

I NASA-CP-2307] p 51 N84-23630

Nonlinear Structural Analysis

[NASA-CP-2297} p 133 N84-31688

High-temperature erosion of plasma-sprayed.

yttria-stabilized zirconia in a simulated turbine

environment

[NASA-TP-2406] p 96 N85-13045

Integrated exhaust gas analysis system for aircraft

turbine engine component testing

lNASA-TP-2424] p 116 N85-16100

Turbine Engine Hot Section Technology (HOST)

{NASA-CP-2289] p 135 N86-11495

Technology for Bey'ton-cycle powerplants using solar

and nuclear energy

[NASA-TP-25581 p 78 N86-21577

GAS TURBINES

Review and status of liquid-cooling technology for gas

turbines

{NASA-RP-1038J p 106 N7g-22427

Effect of steam adddion on cycle performance ol simple

and recuperated gas turbines

INASA-TP-1440} p 144 N79-22626

Fundamentals of Gas Turbine combustion

[ NASA-CP-2087 J p44 NTg-25016

Nonlinear, three-dimensional finite-element analysis of

air-cooled gas turbine blades

[NASA-TP-t66g] p 129 N80-22734

Gas turbine ceramic-coated-vane concept with

convection-cooled porous metal core

[NASA-TP-t942] p 48 N82-14090

Cornbustion Fundamentals Research

{NASA-CP-2268] p 50 N83-29208

GAS-LIOUID INTERACTIONS

Mechanics of a gaseous film barrier to lubricant wetting

of elastohydrodynamicatly lubricated conjunctions

[NASA-TP-2500] p 125 N85-32330

GAS-SOLID INTERACTIONS

Analys=s of the physical atomic forces between noble

gas atoms, alkali _ons and halogen ions

[NASA-TP-2568] p g0 N86-26413

GASDYNAMIC LASERS

Experimental evaluation of a pilot multinozzle-ducf

apparatus

[NASA-TP-1319J p 59 N79-16877

GASEOUS DIFFUSION

Purging of a tank-mounted multilayer insulation system

by gas diffusion

{ NASA-TP-1127 ] p65 N78-17127

Electrical enclosure hydrogen intrusion study --- purging

Cape Kennedy Launch Complex 39

[NASA-TP-1461 ] p 191 N79-25881

GASES

Combustion gas properties I-ASTM let A fuel and dry

air

{NASA-TP-23591 p 51 N85-10064

A-56
SUBJECTINDEX GERMANIUM

GASOLINE

Aviation Gasolines and Future Alternatives

[NASA-CP-2267} p 97 N83-22442

GEAR TEETH

Evaluation of high-contact-ratio spur gears with profile

modification

[NASA-TP-1458] p 120 N79-31604

Spur-gear-system efficiency at part and full load

[NASA-TP-1622} p 121 N80-17466

Effect of shot peening on surface fatigue life of

carbudzed and hardened AISI 9310 spur gears

{NASA-TP-2047] p 122 N82-32736

Surface fatigue life and failure characteristics of EX-53,

CBS 1000M, and AISI 9310 gear materials

[NASA-TP-2513] p 125 N86-t2609

GEARS

Evaluation of CBS 600 carburized steel as a gear

material

[NASA-TP-1390] p 120 N79-14389

Evaluation of high-contact-ratio spur gears with profile

modification

[NASA-TP-1458] p 120 N79-31604

Spur-gear-system efficiency at part and full load

[NASA-TP-1622] p 121 N80-17466

Comparisons of modified Vesco X-2 and AIS19310 gear

steels

[NASA-TP-1731] p 122 N81-14322

Effect of lubricant extreme-pressure additives on surface

fatigue life of AISI 9310 spur gears

[NASA-TP*2408] p 124 N85-13234

Effect of five lubricants on life of AISI 9310 spur gears

[NASA-TP-2419] p 116 N85-16099

A study of the cornering forces generated by aircraft

tires on a tilted, free-swiveling nose gear

[NASA-TP-2481 ] p 135 N86-11522

Surface fatigue life and failure characteristics of EX-53,

CBS 1000M, and AISI 9310 gear materials

[NASA-TP-2513] p 125 N86-12609

Gearing

[NASA-RP-1152] p 125 N86-14612

Testing of YUH.61A helicopter transmission in NASA

Lewis 2240-kW (3000.hp facility

[NASA-TP-2538] p 126 N86-24992

GEMINI PROJECT

On the Shoulders of Titans; A History of Project

Gemini

[NASA-SP-4203] p 61 N78-20151

GEMINI SPACECRAFT

On the Shoulders of Titans: A History of Project

Gemini

[NASA-SP-4203J p 61 N78-20151

GENERAL AVIATION AIRCRAFT

Ground distance covered during airborne horizontal

deceleration of an airplane

[NASA-TP-1157} p 32 N78-20115

Simulation and flight evaluation of a head-up landing

aid for general aviation

[NASA-TP-1276} p 38 N78-31101

Low-speed aerodynamic characteristics of a

16-percent-thick variable-geometry airfoil designed for

general aviation applications

[NASA-TP-1324] p t0 N79-14018

The rotary combustion engine: A candidate for general

aviation --- conferences

{NASA-CP-2067] p 44 N79-15961

Light airplane crash tests at three roll angles

{NASA-TP-1477J p 126 N80-10512

Light airplane crash tests at three pitch angles

[NASA-TP-1481] p 128 N80-11505

Exploratory study of the effects of wing-leading-edge

modifications on the stall/spin behavior of a light general

aviation airplane

[NASA-TP-15891 p 33 N80-13026

General Aviation Propulsion

[NASA-CP-2126] p 46 N80-22327

Measurement of the handling characteristics of two light

airplanes

[NASA-TP-1636} p 56 N80-25345

Low-speed aerodynamic characteristics of a 13 percent

thick medium speed airfoil designed for general aviation

applications

[NASA-TP-1498] p 16 N81-12015

Spin tests of a single-engine, high-wing light airplane

{NASA-TP-1927] p 35 N82-16068

Simulator study of a pictorial display for general aviation

instrument flight

[NASA-TP-1963] p 39 N82-20180

Effects of wing-leading-edge modifications on a

full-scale, low-wing general aviation airplane: Wind-tunnel

investigation of high-angle-of-attack aerodynamic

characteristics o-- conducted in Langley 30- by 60-foot

tunnel

{NASA-TP-2011 I p 4 N82-26217

Crash tests of four low-wing twin-engine airplanes with

truss-rainforced fuselage structure

[NASA-TP-2070} p 131 N83-10442

Low-speed aerodynamic characteristics of a

17-percent-thick medium speed airfoil designed for general

aviation applications

[NASA-TP-1786} p 20 N83-16290

Crash tests of three identical low-wing single-engine

airplane

INASA-TP-2190] p 30 N83-3492t

Natural laminar flow experiments on modern airplane

surfaces

INASA-TP-22561 p 24 N84-26660

Full-scale crash-test evaluation of two load-limiting

subfioors for general aviation aidrames

{NASA-TP-2380} p 134 N85-t3267

Wind-tunnel investigation of a full-scale

canard-configured general aviation airplane

{NASA-TP-2382} p 25 N85-19925

Quest for performance: The evolution of modern

aircraft

{NASA-SP-468] p 5 N85-32089

GENERATORS

Generation of pseudo-random numbers

[NASA-TP-2105] p 183 N83-16095

GENETICS

Search for the universal ancestors

[NASA-SP-477J p 175 N85-32777

GEOCHEMISTRY

Global Mega-Geomorphology

[NASA-CP-2312J p 137 N85-32357

GEOCHRONOLOGY

Global Mega-Geomorphology

{NASA-CP-2312} p 137 N85-32357

GEODESY

Application of space technology to crustal dynamics and

earthquake research

[NASA-TP-1464J p 152 N79-31864

Radio interferomefry: Techniques for Geodesy ---

conference

{NASA-CP-2115t p 139 N80-28798

Geodynamics

[NASA-CP-2325} p 137 N84-30475

Gaopotentisi Research Mission (GRM)

[NASA-CP-2390] p 155 N86-12852

GEODETIC SATELLITES

National geodetic satellite program, part 1

[NASA-SP-365-PT-1 ] p 151 N78-11545

National geodetic satellite program, part 2

[NASA.SP.365-PT-2] p 151 N78-tt552

GEODETIC SURVEYS

Planetary cartography in the next decade (1984 -

1994)

[NASA-SP-475] p 208 N85-22323

GEODYNAMICS

The NASA Geedynamics Program: An overview

{NASA-TP-2147} p 154 N84-10675

Geodynamics

{NASA-CP-2325} p 137 N84-30475

Geopotential Research Mission {GRM)

[NASA-CP-2390} p 155 N86-t2852

GEOGRAPHIC INFORMATION SYSTEMS

Second Eastern Regional Remote Sensing Applications

Conference

{E83-10189} p 141 N83-t9141

Proceedings of the National Conference on Energy

Resource Management. Volume 1: Techniques,

Procedures and Data Bases

[E83-10335] p 141 N83-26155

Proceedings of the National Conference on Energy

Resource Management. Volume 2: Applications

IE83-t0336] p 142 N83-26176

GEOGRAPHY

Astronautics and aeronautics, 1976. A chronology

INASA-SP-4021 } p 212 N84-25602

Global Biology Research Program: Biogeochemicat

Processes in Wefiands

INASA-CP-23161 p 169 N84-30665

The Multispectral Imaging Science Working Group

Volume 1: Executive summary

[E85-10001] p 142 N85-11404

The Multispectral Imaging Science Working Group.

Volume 2: Working group reports

[E85-100021 p 142 N85-11405

GEOLOGICAL SURVEYS

Discrimination of rock classes and alteration products

in southwestern Saudi Arabia with computer-enhanced

LANDSAT data

{NASA-TP-1327} p 136 N78-33499

Skytab explores the Earth

{ NASA-SP-380 } p 140 N82-12492

GEOLOGY

The 1st Symposium on Chemical Evolution and the

Origin and Evolution of Life

I NASA-CP-2276] p 79 N83-24556

The Multispectral Imaging Science Working Group

Volume 1: Executive summary

IE85-10001 ] p 142 N85-11404

The Multispectral Imaging Science Working Group.

Volume 2: Working group reports

[E85-10002] p 142 N85-11405

Global Mega-Geomorphology

{NASA-CP-2312} p 137 N85-32357

GEOMAGNETIC TAIL

Solar Terrestrial Physics: Present and Future

[NASA-RP-tt20] p 2(30 N84-34332

GEOMAGNETISM

Geodynamics

[NASA-CP-2325 J p 137 N84-30475

GEOMETRIC ACCURACY

LANDSAT-4 Science investigations Summary, including

December 1983 Workshop results, volume 2

{E84-10167} p 137 N84-30380

LANDSAT-4 Science Characterization Early Results.

Volume 3, part 2: Thematic Mapper (TM)

[E85-10069} p 143 N85-21724

GEOMETRY

Geometric relationships for homogenization in

single-phase binary alloy systems

[NASA-TP-t349] p 87 N79-13137

GRID30: Computer program for fast generation of

multilevel, three-dimensional boundary-conforming O-type

computational grids

[NASA-TP-1920] p 18 N81-31128

Theoretical method for calculating relative joint geometry

of assembled robot arms

[NASA-TP-2155] p 182 N83-25438

Rolling-element bearings

[NASA-RP-1105] p 123 N83-27214

Computer-Aided Geometry Modeling

[NASA-CP-2272] p 177 N84-22179

Planetary Data Workshop, part 2

[NASA-CP-2343-PT-2] p 208 N84-34376

Computational Geometry and Computer-Aided Design

[NASA-CP-2379] p 177 N85-28563

GEOMORPHOLOGY

Planetary geology in the 1980s

[NASA-SP-467} p 200 N85-23457

Global Mega-Geomorphology

[NASA-CP-2312] p 137 N85-32357

GEOPHYSICS

A geological basis for the exploration of the planets

[NASA-SP-417} p 204 N77.15961

Guntersville Workshop on Solar-Terrestrial Studies

[NASA-CP-2037] p 144 N78-19600

OGO program summary, supplement 1 -- updated

b_bliography for all OGO missions and scientific results

from OGO 5 and 6 missions

INASA-SP-760t-SUPPL-l} p 151 N79-13601

A coupled radiative-convective-photochemical model of

the stratosphere

[NASA-TP-1418] p 136 N79-22580

Application of space technology to crustal dynamics and

earthquake research

[NASA-TP-1464} p 152 N79-31864

Radio interferometry: Techniques for Geodesy ---

conference

{ NASA-CP-21151 p 139 N80-28798

Global Mega-Geomorphology

(NASA-CP-2312} p 137 N85-32357

GEOPOTENTIAL

Spaceborne Gravity Gradiometers

[NASA-CP-2305} p 136 N84-18716

Geodynamics

{NASA-CP'2325] p 137 N84-30475

Geopotential Research Mission (GRM)

INASA-CP-2390J p 155 N86-12852

GEOPOTENTIAL RESEARCH MISSION

Spaceborne Gravity Gradiometers

INASA-CP-2305] p 136 N84-18716

Geopotenfial Research Mission (GRM)

[NASA-CP-2390} p 155 N86-12852

GEOS 3 SATELLITE

Pralaunch testing of the GEOS-3 laser reflector array

{NASA-TP-tf38] p 117 N78-16354

Remote sensing of Gulf Stream using GEOS-3 radar

altimeter

{NASA-TP-1209J p 167 N78-21737

NASA Wallops Flight Center GEOS-3 altimeter data

processing report

[NASA-RP-f066] p 139 N81-11438

GEOSYNCHRONOUS ORBITS

Synchronous Energy Technology

[NASA-CP-2154} p 77 N80-33465

Design guidelines for assessing and controlling

spacecraft charging effects

[NASA-TP-2361] p 74 N84-33452

GERIATRICS

Space Gerontology

[NASA-CP-2248] p 170 N83-16018

GERMANIUM

Growth of high-quality thin-film Ge single crystals by

plasma-enhanced chemical vapor deposition

{NASA-TP-25321 p 100 N86-20586

A-57
GERONTOLOGY SUBJECT INDEX

GERONTOLOGY

Splice Gerontology

[NASA-CP.2248} p 170 N83-16018

GET AWAY SPECIALS (STS)

Get away special experimenter's symposium

[ NASA-CP-2324 } p63 N84.27758

The 1985 Get Away Special Experimenter's

Symposium

[NASA.CP-2401 } p63 N86-27297

GIBBS FREE ENERGY

Volume-energy parameters and turb,ulent-flow density

fluctuations

[NASA-TP-1585} p 107 N80-f7398

Simplified free-energy calculation for ion-induced

heteromolecular nucleation

{NASA.TP.2039] p 150 N82.28839

A class of nonideal solutions. 2: Application to

experimental data

[NASA-TP-t930] p 196 N83-23188

GIMBALS

Effect of several geometric parameters on the static

internal performance of three nonaxisymmetric nozzle

concepts

[NASA-TP-1468] p 12 N79-26022

Theoretical three-and four-axis gimbal robot wrists

[NASA-TP-2564} p 181 N86-25168

GLASS

Time dependence of solid-particle impingement erosion

of an aluminum alloy

{NASA-TP-2169] p 89 N83-32908

A method for developing design diagrams for ceramic

and glass materials using fatigue data

(NASA.RP.f 174] p 126 N86-32763

GLASS FIBERS

A study of resonant-cavity and fiberglass-filled parallel

baffles as duct silencers --- for wtnd tunnels

[NASA-TP-lg70] p 188 N82-24052

GLAUBER THEORY

Optical-model abrasion cross sections for high-energy

heaw ions

[NASA-TP-1893] p 192 N81-27899

GLIDE LANDINGS

Flight-teat of the glide-slope track and flare-control laws

for an automatic landing system/or a powered-lift STOL

sirptane

[NASA-TP.2128} p 57 N84.13198

GLIDE PATHS

Simulation of a cockpit-display concept for executing a

wake-vortex avoidance procedure

[NASA-TP-2300] p 40 N84-21542

A cockpit-display concept for executing a multiple

glide-slope approach for wake.vortex avoidance

[NASA-TP-2386} p 40 N85.16869

Total energy-rate feedback for automatic glide.slope

tracking during wind-shear penetration

[NASA-TP-2412] p 58 N85-23801

GLIDERS

Science and Technology of Low Speed and Motodess

Flight, Third International Symposium

[L-12973] p 2 N79-27070

GLIDING

The science and technology of low speed and motor'tess

flight, pert 1

[NASA-CP-2085-PT-1} p 2 N79-23889

GLOBAL AIR SAMPLING PROGRAM

Ozone measurement system for NASA global air

sampling program

[NASA-TP-1451 } p 148 N79-22654

Carbon monoxide measurement in the giobsi

atmospheric sampling program

[NASA-TP-t526J p 148 N79-31841

Analysis of atmospheric ozone levels at commercial

airplane cruise altitudes in winter and spring, 1976 - 1977

--- Global Atmospheric Sampling Program

{NASA-TP-1807} p 163 N81-21685

Cloud-encounter and particle-concentration variabilities

from GASP data

fNASA-TP-1886} p 164 N82-15677

Water vapor measurement system in global atmospheric

sampling program, appendix

{NASA-TP-205t ] p 150 N83-13643

Climatology of ozone at altitudes from 19.000 at 59.000

feet based on combined GASP and ozonesonde data

{NASA-TP-2303} p 166 N84-31865

GLOBAL ATMOSPHERIC RESEARCH PROGRAM

Condensetion-nuctsi (Aitken Particle) measurement

system used in NASA global atmospheric sampling

program

[NASA-TP-1415} p 148 N79-18479

Globat Scale Atmospheric Processes Research Program

Review

[NASA-CP-2344] p 166 N85-14360

GLOBAL POSITIONING SYSTEM

Proceedings of the Thirteenth Annual Precise Time and

Time Interval (PTTI) Applications and Planning Meeting

INASA-CP-2220] p 118 N82-20494

GODOARD TRAJECTORY DETERMINATION SYSTEM

Fifth Annual Flight Mechanics/Estimation Theory

Symposium

{NASA-CP-2152] p 64 N81-11070

GOES SATELLITES

Convective rainfall estimation from digital GOES-1

infrared data

[NASA-RP-1034] p 160 N79-31885

GOLD

Morphology of gold and copper ion-plated coatings

[NASA-TP-'I262] p 86 N78-26199

Friction and hardness of gold films deposited by ion

plating and evaporation

[NASA-TP-2207] p 89 N83-34019

GOLD COATINGS

Adhesion between potymers and evaporated gold and

nickel films

[NASA-TP-2360} p 96 N84-31379

GOVERNMENT/INDUSTRY RELATIONS

Second Symposium on Space Industrialization --- space

commercialization

[ NASA-CP-2313 J p63 N85-11011

GRADIENTS

Location of noise sources using a phase-slope

method

{NASA-TP-2505] p 191 N86-16041

GRAIN BOUNDARIES

Long-time creep behavior of the tantalum alloy Astar

811C --- as a function of stress, temperature, and gram

size

[NASA-TP-1691J p 87 N80-32489

GRAINS (FOOD)

Controlled Ecological Life Support System First

Principal Investigators Meeting

{NASA-CP-2247} p 174 N83-30016

GRAND TOURS

Voyager to Jupiter and Saturn

[NASA-SP-420] p 205 N77-29046

GRANULAR MATERIALS

Ferrographic analysis of wear particles from sliding

elsstohydrodynemic experiments

[NASA-TP-1230} p 119 N78-22377

GRAPHIC ARTS

Technical communication: Perspectives for the eighties,

part 1. Proceedings of the technical communications

sessions at the 32nd Annual Meeting of the Conference

on College Composition and Communication

INASA-CP-2203-PT-1 ] p 197 N82-14960

GRAPHITE

Effect of thermal exposure on iubricatiog properties of

polyimide films and polyimide-bonded graphite fluoride

films

[NASA-TP-1125} p 91 N78-15277

Some effects of composition on friction and wear of

graphite-fiber-reinforced polyimide liners in plain spherical

bearings

[NASA-TP-1229J p 119 N78-25433

Lubricating and wear mechanisms for a hemisphere

sliding on polyimide-bonded graphite fluoride film

[NASA-TP-1524J p 93 N79-30381

Lubrication and wear mechanisms of polyimide-bonded

graphite fluonde films subjected to tow contact stress

[NASA-TP-1584] p 93 N80-17220

Beam impingement angle effects on secondary electron

emission characteristics of textured pyrolytic graphite

[NASA-TP-2285] p 95 N84-18400

NASA/aircraft industry standard specification for

graphite fiber toughened thermoset resin composite

material

{NASA-RP-1142] p 83 N85-26923

Verification of computer-aided designs of traveling-wave

tubes utilizing novel dynamic refocusers and graphite

electrodes for the multistage depressed collector

[NASA-TP-2524} p 103 N86-13643

Secondary-electron-emission losses in multistage

depressed collectors and traveling-wave-tube efficiency

improvements with carbon collector electrode surfaces

[NASA-TP-2622} p 103 N86-32629

GRAPHITE-EPOXY COMPOSITES

Mechanical behavior and fracture characteristics of

off-axis fiber composites. 1: Experimental inveshgation

--- at the Lewis Research Center

I NASA-TP-1081J p7g N78-13138

Mechanical behavior and fracture characteristics of

off-axis fiber composites 2: Theory and comparisons

I NASA-TP-1082] p 79 N78-16098

Carbon Fiber Risk Analysis --- conference

[NASA-CP-2074] p 80 N79-22196

Exploratory investigation of two resin-matrix composites

subjected to arc-tunnel heating

{NASA-TP-14291 p 80 N79-23141

Moisture diffusion parameter characteristics for epoxy

composites and neat resins

[NASA-TP-14741 p 80 N79-29241

Electron end proton absorption calculations for a

graphite/epoxy composite model --- large space

structures

[NASA-TP-t568J p 93 N80-11226

Stress analysis and buckling of J-stiffened

graphite-epoxy panel

[NASA-TP-1607] p 129 N80-18427

Selected NASA research in compo_te Materials and

structures

INASA'CP'2142} p 80 N80-28436

A new look at numerical analyses of free-edge stresses

in composite laminates

{NASA-TP-1751] p 130 N81-13373

Design detail verification tests for a lightly loaded

open-corrugation graphite-epoxy cylinder

INASA-TP-1981 ] p 130 N82-20567

Buckling test of a 3-meter-diameter corrugated

graphite-epoxy ring-stiffened cylinder

{NASA-TP-20321 p 131 N82-28665

Standard tests for toughened resin composites, revised

edition

{NASA-RP-1092-REVI p 82 N83-31730

Galvamc coupling between D6AC steel, 6061-T6

aluminum, Inconel 7t8 and graphite-epoxy composite

material: Corrosion occurrence and prevention

[NASA-TP-2236J p 89 N84-13263

Friction and wear behavior of aluminum and compo_ta

airplane skins

[NASA-TP-2262J p 37 N84-17175

Fracture toughness of fibrous composite materials

{NASA-TP-2370J p 83 N85-11136

Effect of low-velocity or ballistic impact damage on the

strength of thin composite and aluminum shear panels

{NASA-TP-2441] p 83 N85-26924

Abrasion behavior of aluminum and composite skin

coupons, stiffened skins and stiffened panels

representative of transport airplane structures

{NASA-TP-2520] p 38 N86-13316

Strength of graphite/epoxy bolted wing.skin splice

specimens subjected to outdoor exposure under constant

load and yearly fatigue loading

[NASA.TP-2542] p 83 N86-20508

GRAPHITE-POLYIMIDE COMPOSITES

Tests of grsphite/polyimide sandwich panels in un_lxial

edgewise compression

INASA-TP-1785} p 81 N81-16129

Effects of static tensile load on the thermal expansion

of Gr/PI composite material

[NASA-TP-1867] p 81 N81-24179

Experimental data on single-bolt joints in quasi isotropic

graphite/polyimide laminates

[NASA-TP-2015] p 81 N82-25325

Buckling and failure characteristics of graphita-polyimide

shear panels

[ NASA-TP-2153] p 82 N83-24561

Long-term thermal aging of 2 graphite-potyimide

composite materials

[NASA-TP-2369] p 83 N85-12094

GRAPHS (CHARTS)

MARS t414 recorder environmental tests

{NASA-TP-1709] p 115 N80.30718

A modified T-value method for selection of strain gages

for measuring loads on a low aspect ratio wing

[NASA-TP-1748] p 35 N81-1206,6

Charts for determining potential minimum sonic-boom

overprassures for supersonic cruise aircraft

[NASA-TP-1820] p 17 N81-21016

GRAVIRECEPTORS

The Regulatory Functions of Calcium and the Potential

Role of Calcium m Mediating Gravitational Responses in

Cells and Tissues

[NASA-CP-2286] p 169 N84.11720

NASA Space Biology Program. Eighth annual

symposium's program and abstracts

INASA-CP-2299] p 169 N84-18829

GRAVITATION

Fluid surface behavior in tow gravity Center

discretionary lund no. 83-21

I NASA-TP-24861 p t f 3 N85-28260

GRAVITATION THEORY

Forced and natural convection in laminar-iet diffusion

flames --- normal-gravity, inverted-gravity and zero-gravity

flames

[NASA-TP-1841} p 109 N81-24388

GRAVITATIONAL EFFECTS

Draining characteristics of hemispherically bottomed

cylinders in a low-gravity environment

(NASA-TP-1297J p 106 N78-31384

Barociinic instability with vanable gravity: A perturbation

analysis

{NASA-TP-15861 p 136 N80-15445

NASA Space Biology Program: gth Annual

Symposium

I NASA-CP-2336] p 169 N85-26054

Microgravity Polymers

[NASA-CP-23921 p 96 N86-28194

A-58
SUBJECT INDEX HEAT RADIATORS

GRAVITATIONAL FIELDS

APOlto*Soyuz test project. Volume 1: Astronomy, earth

atmosphere end gravity field, life sciences, and materials

processing

[NASA-SP-412} p 60 N78-17088

The evolution of complex and higher organisms

[NASA-SP-478] p 169 N85-32708

Geopotential Research Mission (GRM)

. [NASA-CP-2390] p 155 N86-12852

GRAVITY GRADIOMETERS

Spaceborne Gravity Gradiometers

[NASA-CP-2305] p 136 N84-18716

GRAVITY PROBE B

Mechanics of liquid helium in a partially filled rotating

dewar in low gravity with application to Gravity Probe-B

[NASA-TP-2124J p 110 N83-16680

GRAVITY WAVES

Currant Scientific Issues in Large Scale Atmospheric

Dynamics

[NASA-CP-2410} p 167 N86-24082

GRAZING FLOW

A new method for determining acoustic-liner admittance

in a rectangular duct wtth grazing flow from experimental

data

[NASA-TP-2310] p ,190 N84-27543

A method for determining acoustic-liner admittance in

ducts with sheared flow in two-cross-sectional directions

[NASA-TP-2518] p ,190 N86-13056

GREEN'S FUNCTIONS

Noise transmission loss of a rectangular plate in an

infinite baffle

[NASA-TP-2398] p ,190 N85-22109

A cracked orthotropic sheet stiffened by a semi-infinite

orthotropic sheet

[NASA-TP-2455] p 134 N85-32339

GREENE&NO

North Atlantic Deep Water Formation

[NASA-CP-2367] p 169 N85-26028

GRIDS

Semianalytic modeling of aerodynamic shapes

[NASA-TP-2413] p 25 N85-2'1120

GROOVES

Design analysis of a self-acting spiral-groove ring seal

for counter-rotating shafts

[NASA-TP-2142] p 50 N83-25712

Elastobydrodynamic contacts. Effects of dents end

grooves on traction and local film thickness

[NASA-TP-2175J p 123 N83-28453

Dynamic response of film thickness in spiral-groove face

seals

[NASA-TP-2544] p 52 N86-153,13

GROUND BASED CONTROL

NASA ground-based and space-based laser ranging

systems

[NASA-TP-,It49] p 113 N78-17360

Handbook of sensor technical charactenstics

[NASA-RP-1087] p 115 N82-29577

Simulation studies of time-control procedures for the

advanced air traffic control system

[NASA-TP-2493] p 30 N85-32101

GROUND EFFECT (AERODYNAMICS)

Prediction of ground effects on aircraft noise

[NASA-TP-1104] p ,186 N78-t7823

Theoretical and experimental investigation of

ground-induced effects for e low-aspect-ratio highly swept

arrow-wing configuration

[NASA-TP-t508J p 54 N79-31223

Assessment of ground effects on the propagation of

aircraff noise: The T-38A flight experiment

[NASA*TP-,1747] p t87 N81-14788

An experimental and theoretical investigation of thick

wings at various sweep angles in and out of ground

effect

[NASA-TP-2068) p 20 N83-I0016

GROUND SPEED

Temperature distribution in an aircraft tire at low ground

speeds

[NASA-TP-2195] p 132 N83-33217

GROUND TRUTH

Procedures for gathering ground truth information for

a supervised approach to a computer-implemented land

cover classification of LANDSAT-acquired mul,lispec,lral

scanner data

[NASA-RP-1015} p 137 N78-15549

Field Study for Remote Sensing: An instructor's

manual

[NASA-CP-2'I55] p 136 N8'I-32564

VAS demonstration: (VISSR Atmospheric Sounder)

description

[NASA-RP-1151} p 166 N86-13867

GROUND-AIR-GROUND COMMUNICATION

Information transfer problems in the aviation system

[NASA-TP-1875) p 30 N81-31162

GROWTH

Growth of high-quality thin-film Ge single crystals by

plasma-enhanced chemical vapor deposition

[NASA-TP-2532] p 100 N86-20586

GUIDANCE (MOTION)

Automated rendezvous and docking: A parametric

study

[NASA-TP-2314] p 74 N84-23677

GUIDANCE SENSORS

A stochastic model for photon noise induced by charged

particles in multiplier phototubes of the space telescope

fine guidance sensors

INASA-TP-2337t p 193 N84-26398

GUIDE VANES

Aerodynamic performance of axial-flow fan stage

Operated at nine inlet guide vane angles --- to be used

on vertical lift aircraft

[NASA-TP-1510] p 45 N7g-312,14

GULF STREAM

Remote sensing of Gulf Stream using GEOS-3 radar

altimeter

[NASA-TP-1209] p ,167 N78-21737

GUST LOADS

An analysis of the gust-induced overspeed trends of

helicopter rotors

(NASA-TP-12131 p 8 N78-28056

Evaluation of a wind-tunnel gust response technique

including correlations with analytical and flight test

results

[ NASA-TP-1501 ] p 2 N80-11028

Comparison of analytical and wind-tunnel results for

flutter end gust response of a transport wing with active

controls

(NASA-TP-20t01 p 131 N82-26703

GUSTS

Development and application of an optimization

procedure for flutter suppression using the aerodynamic

energy concept

[NASA-TP-11371 p 127 N78-18459

NASA/MSFC FY-83 Atmospheric Research Review

[NASA-CP-2288] p ,165 N83-36587

H

HABITABILITY

On the habitability of Mars; An approach to planetary

ecosynthesis

[NASA-SP-414] p 175 N77-12718

HABITATS

Space settlements: A design study

[NASA-SP-413] p 60 N77.2,1106

Wildland inventory and resource modeling for Douglas

end Carson City Counties, Nevada, using LANDSAT and

digital terrain data

[E83.10302] p 142 N83-27293

HALITES

Analysis of the physical atomic forces between noble

gas atoms, alkali ions and halogen ions

[NASA.TP.2568] p 90 N86-264,13

HAMILTONIAN FUNCTIONS

Algorithm for fixed-range optimal trajectories

[NASA-TP-,1565] p 30 N60-28329

HAND (ANATOMY)

Theoretical three-and four-axis gimbal robot wrists

[NASA-TP-2564] p t81 N86-25168

HANDBOOKS

Anthropometric source book. Volume 2: A handbook

of enthropometric data

(NASA-RP-1024-VOL-2] p 172 N79-1371,1

Engineering handbook on the atmospheric

environmental guidelines for use in wind turbine generator

development

[NASA-TP-1359J p t59 N79-14679

Propagation effects handbook for satellite systems

design: A summary of propagation impairments on 10

to 100 GHz satellite links with techniques for system

design

{NASA-RP-,1082] p 100 N82-15270

Applications systems verification and transfer project.

Volume 8: Satellite snow mapping and runoff prediction

handbook

[NASA-TP-1829] p 141 N82-20624

HARDENING (MATERIALS)

Ni,lnding of titanium and titanium: 8 percent aluminum,

1 percent molybdenum, 1 percent vanadium alloy with an

ion-beam source

INASA-TP-2149] p 89 N83-24640

HARDNESS

Friction end hardness ol gold films deposited by ion

plating and evaporation

{NASA-TP-2207} p 89 N83-34019

Erosion of iron-chromium alloys by glass particles

[NASA-TP-2354] p 90 N84-28965

HARDNESS TESTS

Long-term hot-hardness characteristics of five

through-hardened bearing steels

[NASA-TP-t341] p 87 N78-33196

Comparisons of modified Vasco X-2 and AISI 9310 gear

steels

[NASA-TP-1731 ] p 122 N81-,14322

Effects of environment on microhardness of magnesium

oxide

[NASA-TP-2002] p 95 N82-22366

HARMONIC FUNCTIONS

Tenth NASTRAN User's Colloquium

[NASA-CP-2249] p 131 N83-12452

HARMONIC MOTION

Harmonic well mallet densities and Pauli correlation

effects in heavy-,on collisions

[NASA-TP-2003] p 192 N82-23003

HARPOON MISSILE

Thermodynamic and chemical parameters of the

exhaust effluents from the HARPOON booster motor

[NASA-TP-1280] p 147 N78-28682

HAWAII

Volcanic features of Hawaii. A basis for comparison

with Mars

[NASA-SP-403] p 152 N80-23912

HEAD-UP DISPLAYS

Simulation and flight evaluation of a head-up landing

aid for general aviation

[NASA-TP-1276] p 38 N78-31101

A review of some head-up display formats --- tests on

sensing equipment for flights following partly visible terrain

close to the ground

[NASA-TP-1499] p 38 N79-33201

An experimental evaluation of head-up display formats

[ NASA-TP-,1550] p 39 N80-28349

Head-up transi,l_on behavior of pilots wi,lh and without

head-up display in simulated low-visibility approaches

[NASA-TP-f720] p 173 N8,1-t3635

Cognitive issues in head-up displays

[ NASA-TP-17tl ] p 173 N81-13636

Magnitude of visual accommodation to a head-up

display

[NASA.TP-1796] p 173 N8,1-,17711

An Operational evaluation of head up displays for civil

transport operations. NASA/FAA phase 3 report

[NASA-TP-18,15] p 40 N82-3338,1

HEALTH

Space Physiology and Medicine

[NASA-SP-447] p ,170 N63-25349

HEALTH PHYSICS

Human exposure in low Earth orbit

[NASA-TP-2344] p 174 N84-29479

HEAD

The star splitters: The high energy astronomy

observatories

[NASA-SP-466] p 202 N84-22516

HEAD 1

HEAD Science Symposium

[NASA-CP-21131 p 200 N60-14977

HEAO 2

HEAD Science Symposium

[NASA-CP-2113] p 200 N80-14977

HEAT BALANCE

Evaluation of a bulk calorimeter and heat balance for

determination of supersonic combustor efficiency

[NASA-TP-1739] p 48 N81-13058

HEAT CAPACITY MAPPING MISSION

The Heat Capacity Mapping Mission (HCMM)

anthology

[E84-10051] p 142 N84-14563

HEAT OF COMBUSTION

New method for determining heats of combustion of

gaseous hydrocarbons

( NASA-TP-2531 ] p 117 N86-20753

HEAT OF SOLUTION

A class of nonidesl solutions, 1: Definition and

properties

[NASA-TP-19291 p 196 N83-23189

HEAT PIPES

A siphon method of determining resistivities of thin

heat-pipe wicks

INASA-TP-1304] p ,106 N79-10379

Aerothermal tests of a heat-pipe-cooled leading edge

at Mach 7 --- hypersonic heat transfer for space shuttle

orbiters

[NASA-TP-1320) p 195 N79-13901

Transient shutdown analysis of low-temperature thermal

diodes

[NASA-TP-1369J p 106 N79-,16287

Description and orbit data of variable-conductance

heat-pipe system for the communications technology

satellite

[NASA-TP-,1465] p 107 N79-305,16

HEAT RADIATORS

Space Station Technology, 1983

[NASA-CP-2293] p 67 N84-18277

A-59
HEAT RESISTANT ALLOYS SUBJECT INDEX

HEAT RESISTANT ALLOYS

Erosion/corrosion of turbine airfoil materials in the

high-velocity effluent of a pressurized fluidized coal

combustor

INASA-TP-12741 p86 N78-28225

Thermal-conductwity measurements of

tungsten-fiber-reinforced superelloy composites using a

thermal-conductivity comparator

lNASA-TP-1445] p 80 N79-28234

Creep and residual mechanical properties of cast

superalloys and oxide dispersion strengthened alloys

[ NASA-TP-f 781J p 87 N81-19273

Aerodynamic heating on the corrugated surlace of a

10.2 dee hell-angle blunted cone at Mach 6.7

[NASA-TP-1928] p 109 N82-13383

Preliminary study of thermomechanical fatigue of

polycrystelline MAR-M 200

{ NASA-TP-22801 p 89 N84-17350

Analy,_s of thermoelectric properties of

high-temperature complex alloys of nickel-base, iron-base

and cobalt-base groups

[ NASA-TP-2278 J p 89 N84-18370

Effects of alloy compo,_tion on cyclic flame hot-cor rosion

atlack of cast nickel-base superalloys at 900 dee C

|NASA-TP-2338] p 89 N84-26783

Chemical mechanisms and reaction rates for the

initiation of hot corrosion of IN-738

[ NASA-TP-2319] p 90 N84-28958

Oxidation and emittance of superalloys in heat shield

applications

[NASA-TP-2578] p 90 N86-26412

Thermal-fatigue and oxidation resistance of

cobalt-modified Udimet 700 alloy

[ NASA-TP-2591 ] p 135 N86-28464

HEAT SHIELDING

Evaluation of a low-density poiyimide foam in a dynamic,

high temperature environment

[NASA-TP-t049J p 91 N78-12223

Recovery and radiation correcPons and time constants

of several sizes of shielded and unshielded thermocouple

probes for measuring gas temperature

{NASA-TP-1099] p 113 N78-15463

Aerodynamic heating in gaps of thermal protecbon

system tile arrays in laminar and turbulent boundary

layers

INASA-TP-ft87] p 105 N78-28373

Stud.'es of implicit and explictt solution techniques in

trans,'ent thermal analysis of structures

JNASA-TP-2038J p 110 N82-31646

Flightwelght radiantly and actively cooled panel:

Thermal and structural performance

[NASA-TP-2074J p 131 N83-11513

Effect of strain isolator pad modulus on inplane strain

in Shuttle Orbiter thermal protection system tiles

[NASA-TP-2141J p 132 N83-33216

Electroless-plating technique for fabricating thin.wail

convective heat-transfer models

INASA-TP-2349] p 1t2 N84-31561

Experimental aerodynamic heating to simulated space

shuttle tiles in laminar and turbulent boundary layers with

vanabte flow angles at a nominal Mach number of 7

[NASA-TP-2307] p 1t3 N85-34351

Oxidat_n and emittance of superelloys in heat shield

applications

[NASA-TP-2578] p 90 N86-26412

HEAT STORAGE

Thermal Energy Storage: Fourth Annual Review

Meeting

[NASA-CP-2125] p 145 N80-22788

NEAT TRANSFER

Advances in engineering science, volume 4

[NASA-CP-200f-VOL-4] p 98 N77-10345

Effects of film injection angle on turbine vane cooling

[NASA-TP-1095J p 104 N78-13379

FORTRAN program for calculating coolant flow and

metal temperatures of a full-coverage-film-cooled vane or

blade

t NASA-TP-1259] p 43 N78-28099

Analysis of metal temperature and coolant flow with a

thermal-barrier coating on a full-coverage-film-cooled

turbine vane

INASA-TP-1310] p 43 N78-31109

Thermal characteristics of the 12-gigahertz. 200-watt

output stage tube for the communications technology

satellite

[NASA-TP-1344] p 69 N78-33137

Pressure end thermal distributions on wings and adjacent

surfaces induced by elevon deflections at Math 6

{NASA-TP-1356] p t06 N79-20344

Review and status of liquid-cooling technology for gas

turbines

[NASA-RP-1038] p 106 N79-22427

Comparison of predicted and experimental performance

of large-bore roller bearing operating to 3 0 million DN

[NASA-TP-15991 p 121 Na0-t5410

Prediction method for two-dimensional aerodynamic

losses of cooled vanes using integral boundary-layer

parameters

INASA-TP-16231 p 14 N80-17030

Extension of similarity test procedures to cooled engine

components with insulating ceramic coatings

[NASA-TP-16151 p 108 N80-24577

Wind-tunnel measurements and comparison w=th flight

of the boundary layer and heat transfer on a hollow cylinder

at Mach 3

INASA-TP-17891 p 16 N81-14975

Fundamental heat transfer research for gas turbine

engines

INASA-CP-2178J p 48 N81.24063

Gas turbine ceramic-coated-vane concept with

convection-cooled porous metal core

[NASA-TP-19421 p 48 N82-14090

Computational Aspects of Heat Transfer in Structures

[NASA-CP-2216] p 109 N82-23473

Studies of impticit and explicit solution techniques in

transient thermal analysis of structures

tNASA-TP-2038] p 1t0 N82-31646

Effects of flow separation and cove leakage on pressure

and heat-transfer distributions along a wing-cove-elevon

configuration at Mach 6.9 --- Langley 8-ft high temperature

tunnel test

[NASA.TP.2127J p 111 N83-28378

The wedge hot-film anemometer in supersonic flow

[ NASA-TP-21341 p 189 N83-30164

Expenmental and theoretical deposition rates from

salt-saeded combustion gases of a Mach 0.3 burner rig

NASA-TP-22251 p 111 N84-19741

Review and status of heat-transfer technology for

internal passages of air-cooled turbine blades

NASA-TP-22321 p 1 f 1 N84-21828

Hybrid perlurbation/Bubnov-Galerkin technique for

nonlinear thermal analysis

NASA-TP-2145J p 1 f 1 N84-22907

Electroless-plating technique for fabricating thin-wall

convective heat-transfer models

NASA-TP-2349] p 1t2 N84-31561

GCKP84-general chemical kinetics code for gas-phase

flow and batch processes including heat transfer effects

NASA-TP-23201 p 85 N84-32446

Experimental and predicted heating distributions for

biconics at incidence nn air at Math 10

NASA-TP-2334] p 112 N85-12313

Transition in Turbines

I NASA-CP-2386 ] p 113 N85-31433

HEAT TRANSFER COEFFICIENTS

Method for calculating convective heat-transfer

coefficients over turbine vane surfaces

[NASA-TP-f134J p 104 N78-17338

Configuration heating for s hypersonic research airplane

concept having a 70 deg swept double-delta wing

{ NASA-TP-1143 J p 105 N78-23389

In-flight boundary-layer measurements on a hollow

cylinder at a Math number of 3.0

lNASA-TP-17641 p 108 N81-12361

Influence of thermal boundary conditions on heat

transfer from a cylinder in cross flow

[NASA-TP-1894] p 109 N81-29384

HEAT TRANSMISSION

Turbine Engine Hot Section Technology (HOST)

[NASA-CP-2289] p 135 N86-11495

HEAT TREATMENT

Effects of erodant particle shape and various heat

treatments on erosion resistance of plain carbon steel

[NASA-TP-1755] p 87 N81-16210

Metallurgical characterization of the fracture of several

high strength aluminum alloys

[NASA-TP-1086] p 85 N84-11230

HEATING

Pressure and heating-rate distributions on a corrugated

surface in a supersonic turbulent boundary tayer

l NASA-TP-1024 ] p f 11 N84-10504

The Origin of Nonradiative Heating/Momentum in Hot

Stars

[NASA-CP-2358] p 200 N85-17755

HEAVY IONS

Optical-model abrasion cross sections for high-energy

heavy ions

INASA-TP-1893] p 192 N81-27899

Harmonic well matter densities and Pauli correlation

effects in heavy-ion collisions

INASA-TP-2003] p 192 N82-23003

Heavy-ion total and absorption cross sections above

25 MeV/nucleon

INASA-TP-2138] p 192 N83-23140

Heavy ion transporl in the straight ahead

approximation

INASA-TP-2178] p 210 N83-29169

An abrasion-ablation model description of galactic

heavy-ion fragmentation

I NASA-TP-2305i p 192 N84-22396

A T-matrix theory of galacbc heavy-ion fragmentabon

[NASA-TP-2363J p 193 N85-t7690

Tables of nuclear cross sections for galactic cosmic rays:

Absorption cross sections

{NASA-RP-11341 p 193 N85-27665

Electromagnetic dissociation effects in galactic

heavy-ion fragmentation

lNASA-TP-25271 p 211 N86-21492

Cross section calculations for subthreshold pion

production in peripheral heavy-ion collisions

[NASA-TP-26001 p 193 N86*30485

HEAVY LIFT HELICOPTERS

Vehicle concepts and technology requirements for

buoyant heavy-lift systems

[NASA-TP-19211 p 35 N81-31185

HELICOPTER CONTROL

Navigation, guidance, and control for helicopter

automatic landings

[ NASA-TP-1649] p 55 N80-23326

Helicopter Handling Qualities

INASA-CP-2219] p 30 N82-23208

HELICOPTER DESIGN

Calculation of three-dimensional unsteady transonic

flows past helicopter blades

[NASA-TP-f721 I p 15 N80-33356

Experimental investigation of a 10-percent-thick

helicopter rotor aidoil section designed with a viscous

transonic analysis code

{NASA-TP-18641 p 2t N83-30389

Two-dimensional aerodynamic charactenstics of an

airfoil designed for two

[NASA-TP-1965] p 24 N84-27694

Two-dimensional aerodynamic characteristics of three

rotorcraft airfoils at Math numbers from 0.35 to 0.90

[NASA-TP-2000] p 24 N84-28743

Rotorcraft Dynamics 1984

[NASA-CP-2400] p 38 N86-15280

HELICOPTER PERFORMANCE

Processing of on-boerd recorded data for quick enelysls

of aircraft performance --- rotor systems research

aircraft

[NASA-RP-1043] p 33 N79-33191

Effects of primary rotor parameters on flapping

dynamics

[NASA-TP-1431 ] p 55 N80-15138

Wind-tunnel evaluation of a 2f-percent-scale powered

model of a prototype advanced scout helicopter

[NASA-TP-24201 p 26 N85-28923

Rotorcrafl Dynamics 1984

I NASA-CP-2400] p 38 N86-15280

HELICOPTER TAIL ROTORS

Aerodynamic characteristics of several current

helicopter tail boom cross sections including the effect

of spoilers

[NASA-TP-2506J p 27 N86-20349

HELICOPTER WAKES

Development and validation of a combined rotor

fuselage induced flow field computational method ---

Langley V/STOL tunnel

[NASA-TP-16561 p 15 N80-25296

HELICOPTERS

An analysis of the gust-induced overspeed trends of

helicopter rotors

I NASA-TP-12131 p8 N78-28056

Helicopter Acoustics

[NASA-CP-2052-PT-lJ p 186 N78-32816

Helicopter Acoustics, part 2 --- conferences

[NASA-CP-2052-PT-2] p 186 N79-10843

Design and analysis of an active jet control system for

helicopter sling loads

(NASA-TP-1397] p 54 N79-15970

Effect of noise spectra and a listening task upon

passenger annoyance in a helicopter interior noise

environment

INASA-TP-1590J p 171 N80-13769

Eveluabon of helicopter noise due to b blade-vortex

interaction for five tip configurations --- conducted in the

Langley V/STOL tunnel

INASA-TP-1608] p 187 N80-14840

Aerodynamic characteristics of three helicopter rot_

airfoil sections at Reynolds number from model scale to

full scale at Mach numbers from 035 to 0.90 --- conducted

bn Langley 6 by 28 inch transonic tunnel

[NASA-TP-1701 ] p 15 N80-32333

Subjective field study of response to impulsive hal*copter

noise

[NASA-TP-1833] p 187 N81-21873

Kinematic properties of the helicopter dn coordinated

turns

INASA-TP-1773] p 35 N81-22039

Effects of repetition rate and impulsiveness of simulated

helicopter rotor noise on annoyance

[NASA-TP-1969J p 150 N82-19707

Self-tuning regulators for multicychc control of helicopter

vibration

[NASA-TP-19961 p 57 N82-20188

A-60
SUBJECT INDEX HOLE DISTRIBUTION (MECHANICS)

Helical automatic approaches of helicopters with

microwave _anding systems

INASA-TP-2109] p 31 N83-18704

The vibration characteristics of a coupled helicopter

rotor-fuselage by a finite element analysis

[NASA-TP-2118] p 36 N83-18714

Evaluation of ride quality prediction methods for

helicopter interior noise and vibration environments

{NASA-TP-2261 i p 172 N84-20155

Rotorcraft noise

{NASA-CP-22341 p 190 N84-29662

Transonic flow analysis for rotors. Part 1:

Three-dimensional quasi-steady, full-potential calculation

[NASA-TP-2375-PT-1 I p 25 N85-10914

Technical Workshop: Advanced Helicopter Cockpit

Design

{NASA-CP-2351 J p 31 N85-14806

Compressible, unsteady lifting-surface theory for a

helicopter rotor in forward flight

{NASA-TP-25031 p 27 N86-18289

Testing of YUH-61A helicopter transmission in NASA

Lewis 2240-kW (3000-hp facility

[NASA-TP-2538] p 126 N86-24992

Acoustic treatment of the NASA Langley 4- by 7-meter

tunnel: A feasibility study

INASA-TP-2563] p 191 N86-31337

HEUOSPHERE

Ninteenth International Cosmic Ray Conference. SH

sessions, volume 4

[NASA-CP-2376-VOL-4 ] p 210 N85-34729

Nineteenth International Cosmic Ray Conference. SH

sessions, volume 5

{NASA-CP-2376-VOL-5 ] p 211 N85-34991

HELIUM

Purging of a tank-mounted mu_tilayer insufation system

by gas diffusion

[NASA-TP-1127} p 65 N78-17127

Comparison of two computer programs by predicting

turbulent mixing of helium in a ducted supersonic

airstream

INASA-TP-1166] p 105 N78-22333

Thermal performance of gaseous-helium-purged

tank-mounted multilayer insulation system during

ground-hold and space-hold thermal cycling and exposure

to water vapor

{NASA-TP-1114 ] p65 N78-28150

Experimental perfect-gas study ol expansion-tube flow

characteristics

{NASA-TP-1317] p 106 N79-14327

Measured and predicted shock shapes and aerodynamic

coefficients for blunted cones at incidence in helium at

Mach 20.3

[NASA-TP-t395J p 106 N79-20345

Pressures, forces, moments and shock shapes for a

geometrically matched sphere-cone and hyperboloid at

Math 20.3 in helium --- 22-inch aerodynamics leg of the

Langley hypersonic helium tunnel facility

INASA-TP-2100] p 110 N83-16675

HELIUM ISOTOPES

Direct nuclear-powered lasers

[NASA-TP-2091 ) p 118 N83-16738

HEMATOLOGY

Design of a blood-freezing system for leukemia

research

[NASA-TP-11651 p 169 N78-18673

HETERODYNING

DIAL with heterodyne detection including speckle noise:

Aircraft/shuttle measurements of O3, H20, and NH3 with

pulsed tunable CO2 lasers

{NASA-TP-17251 p 115 N80-30717

Comparative performance of HgCdTe photodiodes for

heterodyne application

[NASA-TP-17451 p 101 N80-33683

Atmospheric solar absorption measurements in the 9

to 11 mu m region using a diode laser heterodyne

spectrometer

{NASA-TP-1726) p 153 N80-33998

HIGH ALTITUDE

High altitude perspective --- cost-reimbursable services

using NASA U-2 aircraft

[NASA-SP-4271 p 138 N78-31508

Wind study for high altitude platform design

[NASA-RP-t0441 p 160 N80-12661

HIGH ALTITUDE ENVIRONMENTS

Slip-boundary equations for multicomponent

nonequilibrium airflow

{NASA-TP-24521 p 113 N86-14530

HIGH ASPECT RATIO

Low-speed tests of a high-aspect-ratio,

superchtical-wing transport model equipped with a high-lift

flap system in the Langley 4- by 7-meter and Ames 12-foot

pressure tunnels

{NASA-TP-20971 p 26 N85-31010

Static investigation of circular-to-rectangular transition

ducts for high-aspect-ratio nonaxisymmetric nozzles

{NASA-TP-2534] p 52 N86-22576

HIGH ENERGY INTERACTIONS

Nineteenth International Cosmic Ray Conference. HE

Sessions, volume 6

[NASA-CP-2376-VOL-61 p 211 N85-35848

Nineteenth International Cosmic Ray Conference. HE

Sessions, volume 7

[NASA-CP-2376-VOL-7 ] p 211 N85-35968

HIGH ENERGY PROPELLANTS

Current evaluation of the tnpropellant concept

{NASA-TP-2602] p 78 N86-28124

HIGH FREQUENCIES

Recovery of pyroshock data from distorted acceleration

records

[ NASA-TP-2494 } p 75 N85-31141

HIGH PASS FILTERS

Sample data effects of high-pass filters

[NASA-TP-1797] p 35 N81-16040

HIGH PRESSURE

Performance of two-stage fan with larger dampers on

first-stage rotor

[NASA-TP-1399I p 44 N79-23967

Pollutant emissions from flat-flame burners at high

pressures

[NASA-TP-t673] p 85 N80-25392

Design guide for hfgh pressure oxygen systems

[NASA-RP-1113] p 99 N83-32990

HIGH PRESSURE OXYGEN

Mechanical impact tests of materials in oxygen effects

of contamination --- Teflon, stainless steel, and

aluminum

{NASA-TP-1571 ) p 97 N80-21551

HIGH RESOLUTION

Development of a procedure to model high-resolution

wind profiles from smoothed or low-frequency data

I NASA-TP-1071 ] p 158 N78-11642

Sequential high-resolution wind profile measurements

[NASA-TP-'I354} p 159 N79o14680

High Resolution Infrared Spectroscopy Techniques for

Upper Atmospheric Measurements

{ NASA-CP-21341 p 152 N80-27866

HIGH SPEED

An analysis of the gust-induced overspeed trends ot

helicopter rotors

[NASA-TP-1213] p 8 N78-28056

Comparison of predicted and expenmental performance

of large-bore roller bearing operating to 3.0 million DN

[NASA-TP-1599} p 121 N80-15410

A numencal technique for calculation of the noise of

high-speed propellers with advanced blade geometry

[NASA-TP-t662] p 187 N80-27161

Lubrication of optimized-design tapered-roller bearings

to 2.4 million DN

INASA-TP-1714] p 121 N80-29734

Effect of cage design on characteristics of

hig h-speed-jet-lubricat ed 35-millimeter-bore ball bearing ---

turbojet engines

[NASA-TP-1732} p 121 N80.33749

Effect of two inner-ring oil-flow distribution schemes on

the operating characteristics of a 35 millimeter bore ball

bearing to 2.5 million DN

[NASA-TP-2404] p 124 N85-13233

The algorithms for rational spiine interpolation of

surfaces

{NASA-TP-2536J p 183 N86-18060

HIGH STRENGTH STEELS

Microstructure and mechanical properties of quenched

and tempered 300M steel

lNASA-TP-1288J p 127 N78-30610

HIGH TEMPERATURE

Tdbotogical properties at 25 C of seven polyimide films

bonded to 440 C high-temperature stainless steel

INASA-TP-1944] p 94 N82-19373

Proposed fast-response oxygen monitoring and control

system for the Langley 8-foot high-temperature tunnel

INASA-TP-2218} p 116 N84-11460

Turbine Engine Hot Section Technology {HOST)

{NASA-CP-2289} p 135 N86-11495

HIGH TEMPERATURE GASES

Fluid shielding of high-velocity jet noise

[NASA-TP-22591 p 189 N84-15894

Local Interstellar Medium. International Astronomical

Union Colloquium No. 81

[NASA-CP-2345} p 204 N85-15539

HIGH TEMPERATURE LUBRICANTS

Steady-state boundary lubrication with formulated

C-ethers to 260 C

INASA-TP-1812j p 94 N81-21193

Analysis of a MIL-L-27502 lubricant from a gas-turbine

engine test by size-exclusion chromatography

INASA-TP-2063] p 95 N83-16528

HIGH TEMPERATURE RESEARCH

Analysis of thermoelectric properties of

high-temperature complex alloys of nickel-base, iron-base

and cobalt-base groups

[NASA-TP-22781 p 89 N84-18370

HIGH TEMPERATURE TESTS

Elevated-temperature application of the IITRI

compression test fixture for graphite/polyimide filamentary

composites

{NASA-TP-1496} p 80 N79-32277

Nonlinear Constitutive Relations for High Temperature

Application, 1984

{NASA-CP-23691 p 134 N85-31530

HIGH VOLTAGES

Optically isolated logarithmic nanoammeter capable of

floating to 5 kilovolts

{NASA-TP-1527] p 101 N79-32467

Radiating dipole model of interference induced in

spacecraft circuitry by surface discharges

iNASA-TP-2240} p 74 N84-16247

Circuit transients due to negative bias arcs on a

high-voltage solar array in low Earth orbit

[NASA-TP-2407} p 75 N85-14858

Spacecraft Environmental interactions Technology,

1983

{NASA-CP-2359] p 75 N85-22470

HILSCH TUBES

Influence of coolant tube curvature on film cooting

effectiveness as detected by infrared imagery

[NASA-TP-1546] p 45 N80-11087

HISTOGRAMS

Analytical techniques of pilot scanning behavior and their

application

[NASA-TP-2525] p 172 N86-27920

HISTORIES

Essays on the History of Rocketry and Astronautics:

Proceedings of the Third through the Sixth History

Symposia of the international Academy of Astronautics,

volume 1

INASA-CP-2014-VOL-t I p 211 N77-33030

Essays on the History of Rocketry and Astronautics:

Proceedings of the Third through the Sixth History

Symposia of the International Academy of Astronautics,

volume 2

INASA-CP-2014-VOL-2} p 212 N77-33048

Lunar impact: A history of Proiect Ranger

[NASA-SP-4210} p 65 N78-15149

On the Shoulders of Titans: A History of Project

Gemini

JNASA-SP-4203] p 61 N78-20151

Skylab: A chronology

{ NASA-SP-4011 } p 61 N78-25115

The Apollo spacecraft: A chronology volume 4, 21

Janua_ 1966 - 13 July 1974

INASA-SP'40og-voL-4} p 98 N80-20437

Beyond the atmosphere: Early years of space

science

I NASA-SP-4211 ] p 200 N81-20962

Wind Tunnels of NASA

[NASA-SP-440} p 59 N81-32153

Orders of magnitude: A history of NACA and NASA,

1915 - 1980

[NASA-SP-44031 p 196 N82-14955

Meteorological satellites: Past, present, and future

{NASA°CP-22271 p 164 N82-24781

Living and working in space. A history of Skylab

{NASA-SP-42081 p 63 N84-25737

On the frontier: Flight research at Dryden 1946-1981

{NASA-SP-4303J p 4 N85-17934

Model research; The National Advisory Committee for

Aeronautics, 1915-1958, volume 1

I NASA-SP-4103-VOL-1} p 4 N85-23683

Model research, the National Advisory Committee for

Aeronautics, 1915-1958, volume 2

[NASA-SP-4103-VOL-2} p 4 N85-23684

Quest for performance: The evolution of modern

aircraft

[NASA-SP-468] p 5 N85-32089

A spacefaring people: Perspectives on early

spaceflight

{NASA-SP-4405] p 212 N85-35142

Searching the horizon; A history of Ames Research

Center, 1940-1976

INASA-SP-4304] p 213 N86-16185

Astronautics and aeronautics, 1977: A chronology

I NASA-SP-4022 ] p 213 N86-31524

HOLE DISTRIBUTION (ELECTRONICS)

Effect of hole geometry and Electric-Discharge

Machining (EDM) on atrftow rates through small diameter

holes in turbine blade material

{NASA-TP-1716] p 47 N81-12089

HOLE DISTRIBUTION (MECHANICS)

Effect of cooling-hole geometry on aerodynamic

performance of a film-cooled turbine vane tested with cold

air in a two-dimensional cascade

{NASA-TP-1136] p 8 N78.20080

A-61
HOLE GEOMETRY (MECHANICS)

HOLE GEOMETRY (MECHANICS)

Evaluation of multilayer printed wiring boards by

metallographic techniques: An illustrated guide to the

preparation and inspection of plated-through bole test

coupons based on the requirements of MiI-P-55110D

INASA-RP-1161J p 126 N86-26639

HOLES (ELECTRON DEFICIENCIES)

Symmetry cons*derations in the scattering of identical

composite bodies

INASA-TP-2548] p 193 N88-23388

HOLLOW CATHODES

Effect of anode-cathode geometry on pedormance of

the HIP-1 hot ion plasma --- magnetic mirrors

INASA-TP-1201] p 194 N78-21922

HOLOGRAPHIC INTERFEROMETRY

Fringe Iocalizahon requirements for three-dimensional

flow visualization of shock waves in diffuse-illumination

double-pulse holographic interterometry

[NASA-TP-1868] p 115 N82-22481

HOLOGRAPHY

Optical and holographic storage properties of F3, Cu.

and Mg-doped tithium niobate

[ NASA-TP- 11441 p 193 N78-20948

Holography through optically active windows

[NASA-TP-1414} p 114 N7g-17195

Simulated electronic heterodyne recording and

processing of pulsed-laser holograms

[NASA.TP-1444] p 114 N79-21329

HOMOGENEITY

A cracked orthotropic sheet stiffened by a semHnfinite

orthotropic sheet

I NASA-TP-2455} p t34 N85-32339

HOMOGENIZING

Geometric relationships for homogenization in

single-phase binary alloy systems

I NASA-TP-1349 ] p87 N79-13137

Effect of concentration dependence of the diffusion

coefficient on homogenization kinetics in multiphase binary

alloy systems

I NASA-TP-1281 j p 87 N79-13138

HONEYCOMB STRUCTURES

Comparison of experimental and theoretical turbulence

reduction characteristics Ior screens, honeycomb, and

honeycomb*screen combinations

INASA-TP-1958/ p 19 N82-14055

Fabrication and evaluation of brazed titanium-clad

borsic/aluminum skin-stringer panels

! NASA-TP-1674 } p 82 N83-28098

HONEYWELL COMPUTERS

Interactive debug program for evaluation and

modification of assembly-language software

NASA-TP-1441 ] p 178 N79-21796

HOOP COLUMN ANTENNAS

Apphcahon of the LQG/LTR technique to robust

controller synthesis for a large flexible space antenna

NASA-TP=2560] p 75 N86-30800

Effects of model error on control of large flexible space

antenna with comparisons of decoup_ed and _mear

quadratic regulator control procedures

NASA-TP-2604 I p 75 N86-30801

HORIZONTAL FLIGHT

Parametric study of m=crowave-powered high-altitude

a_rplane platforms designed for linear flight

NASA-TP-19181 p 35 N82-11050

HORIZONTAL TAIL SURFACES

Expenmental and analytical transonic f_utter

characteristics of a geared-elevator configurahon

NASA-TP-1666! p 34 N80-25321

Longitudinal aerodynamE characteristics of an elliptical

body with a horizontal tail at Mach numbers from 2 3 to

4 63

NASA-TP 2024 ; p 19 N82-26232

Expenmental trim drag values and flow-held

measurements for a wide-body transport model with

convenhona_ and supercritical wings

NASA-TP-2071 J p 25 N85-10920

HOT CORROSION

Effects of alloy composition on cyclic Ilame hot-corrosion

attack ol cast n_ckel-base superatioys at 900 deg C

NASA-TP-2338 ! p 89 N84-26763

Chem=cal mechamsms and reaction rates for the

_mhatlon ol hot corrosion of IN-738

INASA-TP 2319J p 90 N84-28958

Pocketing mechanics of SRM nozzte liner

tNASA-TP-2577] p 135 N86-23974

HOT STARS

The Origin of Nonradiative Heating/Momentum in Hot

Stars

[ NASA-CP-23581 p 200 N85-t 7755

HOT-FILM ANEMOMETERS

Pressure probe and hot-film probe rsponses to acoustic

excitation in mean flow

I NASA TP 258t I p 19t N86-27043

HOUSINGS

Identification and management of filament-wound case

stiffness parameters

INASA-TP-2117} p 81 N83-16400

HOVERING

A unique facility for WSTOL aircraft hover testing ---

Langley Impact Dynamics Research Facility

[NASA-TP-1473] p 59 N79-29199

The vibration chsracteristE:s of a coupled helicopter

rotor-fuselage by a finite element analysis

I NASA-TP-2118J p36 N83-18714

Aerodynamic characteristics of several current

helicopter tail boom cross sections indudiog the effect

of spoilers

INASA'TP'2506] p 27 N86o20349

HUDDLE SPACE TELESCOPE

Scientific research with the space Telescope:

international Astronomical Union Colloquium no. 54 ---

conferences

I NASA-CP-2111 } p 200 N80-22130

System analysis approach to deriving design criteria

(loads) for Space Shuttle and its payloads Volume 1:

General statement of approach

INASA-TP-1949] p 66 N82-14203

The Space Telescope Observatory. Special session of

Commission 44, IAU 181h General Assembly

NASA-CP-2244] p 202 N82-33296

Algorithm for astronomical, extended source,

signal-to-noise radio calculations

NASA-TP-2396] p 202 N85-12833

Algorithm for astronomical, point source, signal to noise

ratio calculations

NASA-TP-2397] p 202 N85-t2634

Local Interstellar Medium International Astronomical

Union Colloquium No. 61

NASA-CP-2345] p 204 N85-15539

Graphical techniques to assist in pointing and control

studies of orbiting spacecraft

NASA-TP-2575] p 63 N86-21559

Technology for large space systems: A bibliography with

indexes (supplement 14)

NASA-SP-7046(14)} p 63 N86-28104

HUMAN FACTORS ENGINEERING

Advances in engineering science, volume 4

NASA-CP-200t-VOL-4] p 98 N77-10345

Space settlements: A design study

I NASA-SP-413] p 60 N77-21106

Effect of vibration duration on human discomfort ---

passenger comfort and random vibration

INASA-TP-1283] p 171 N78-32717

Anthropometric source book Volume 1 : Anthropometry

for designers

iNASA-RP-1024 I p t72 N79-1t734

Models of human operators in vision dependent tasks

I NASA-CP-2103] p 171 N79-33838

Some human factors issues in the development and

evaluation of cockpit alerting and warning systems

I NASA-RP-1055] p 173 N80-15821

Simulator study of the effect of control-system time

detays on the occurrence of pilot-induced oscillations and

on pilot tracking performance with a space-shuttle-orbiter

configuration

INASA-TP-15881 p 34 N80-21317

Head-up transibon behavior of pilots during simulated

low-visibility approaches

INASA-TP-1616} p 173 N80-26039

An experimental evaluation of head-up display formats

I NASA-TP-15501 p 39 N80-28349

Annoyance due to multiple airplane noise exposure

I NASA-TP-17061 p 149 N60-29946

Head-up transition behavior of pilots with and without

head-up display in simulated low-visibility approaches

{NASA-TP-17201 p 173 N61-13635

Magnitude of visual accommodation to a head-up

display

INASA-TP-17961 p 173 N81-17711

The t 960 Aircraft Safety and Operating Problems, part

2

t NASA-CP-2170-PT-21 p29 N81-19056

Human Factors Considerations =n System Design

l NASA-CP-2246 } p 173 N83-18238

Effect of low-frequency tones and

turbulent-boundary-layer noise on annoyance

I NASA-TP-2202] p 172 N83-34579

Twentieth Annual Conference on Manual Control,

volume I

INASA-CP-2341-VOL-tl p 174 N85-t4487

Twentieth Annual Conference on Manual Control,

votume 2

INASA-CP-2341-VOL-2} p 174 N85-t4535

Technical Workshop: Advanced Helicopter Cockpit

Design

I NASA-CP-2351 ] p 31 N85-14806

Living aloft: Human requirements for extended

spaceflight

I NASA-SP-4831 p 174 N85 32772

SUBJECT INDEX

Space Station Workstation Technology Workshop

Report

[NASA-CP-2414] p 70 N86-23620

Baseline experiments in teteoperator control

{NASA-TP-25471 p 174 N86-26836

Analytical techniques of pilot scanaing behavior and their

application

[NASA-TP-25251 p 172 N86-27920

Twenty-First Annual Conference on Manual Control

{NASA-CP-2428} p 174 N88-32976

HUMAN PERFORMANCE

Information transfer problems in the aviation system

{NASA-TP-1875] p 30 N61-31162

Human exposure in low Earth orbit

[NASA-TP-2344] p 174 N64-29479

Twenty-First Annual Conference on Manual Control

[NASA-CP-24281 p 174 N86-32976

HUMAN REACTIONS

Proceedings and findings of the 1976 Workshop on Ride

Quality --- passenger acceptance of transportation

systems

[NASA-CP-20061 p 172 N77-27710

The 14th Annual Conference on Manual Control --- digital

simulation of human operator dynamics

[ NASA-CP-20601 p 173 N79-15588

Discomfort criteria for single-axis vibratK:.ns

INASA-TP-1422] p 171 N79-23662

Effect of noise spectra and a listening task upon

passenger annoyance in a helicopter interior noise

environment

{NASA-TP-1590] p 171 N80-13769

Annoyance due to mutttple airplane noise exposure

INASA-TP-1706] p 149 N80-28946

Effects of activity interference on annoyance due to

aircraft noise

INASA-TP-1938] p 149 N82-12654

A user-oriented and computerized model lot estimating

vehicle ride quality

INASA-TP-22991 p 172 N84-22162

Physiological, Psychological, and Social Effects of

Noise

I NASA-RP-1115 j p t 74 N84-29465

HUMAN TOLERANCES

Effect of vibration duration on human discomfort ---

passenger comfort and random vibration

INASA-TP-1283J p 171 N78-32717

Variability of annoyance response due to aircraft noise

iNASA-TP-1335] p 186 N79-18687

Human discomfort response to noise combined with

vertical vibration

INASA-TP-1374} p 171 N79-22761

Discomfort criteria for single-axis vibrations

INASA-TP-1422] p 171 N79-23662

Laboratory study of annoyance to combined airplane

and road-traftic noise

[NASA-TP-1478} p 148 N79-32743

Effects of sound level fluctuations on annoyance caused

by aircraft-flyover noise

I NASA-TP-15761 p 187 N80-13880

The physiological basis for spacecraft environmental

limits

INASA-RP-t045} p 170 N80-15788

HUMAN WASTES

Man's impact on the troposphere: Lectures in

tropospheric chemistry

INASA-RP-1022] p 151 N79-10634

HUMIDITY

Atmospheric aerosols: Their Optical Properties and

Effects

I NASA-CP-2004 ] p 151 N77-15563

Water-vapor etlects on friction of magnetic tape in

contact with nickel-zinc ferrite

I NASA-TP-22791 p 95 N84-18399

Low-frequency sound absorption measurements in air

INASA-RP-11281 p 190 N85-11789

Effect of humidity on fretting wear Of several pure

metals

[NASA-TP-2403] p 90 N65-13006

Humidity effects on adhesion of nickeFzinc fernte in

elastic contact with magnetic tape and itself

I NASA-TP-24491 p96 N85-21359

HUMIDITY MEASUREMENT

Comparisons between Nimbus 6 satellite and

rawinsonde soundings for several geographical areas

INASA-RP-t0731 p 163 N81-16679

HYBRID CIRCUITS

Proceedings of the 1977 NASA/ISHM Microelectronics

Conference

INASA-CP-20271 p 101 N76-16266

HYBRID COMPUTERS

Development and verification of real-time, hybrid

computer simulation of F100-PW-100(3) turbofan engine

t NASA-TP-t034 ] p4t N77-31154

A-62
SUBJECT INDEX HYPERSONIC FLOW

HYDRAULIC CONTROL

Experimental investigation of active loads control for

aircraft landing gear

[NASA-TP-2042J p 36 N82-31321

HYDRAULIC EQUIPMENT

Single-stage electrohydraulic servosystem for actuating

on airflow valve with frequencies to 500 hertz

[NASA-TP-16781 p 56 N80-2936g

HYDRAULIC TEST TUNNELS

Water-tunnel and analytical investigation of the effect

of strake design variables on strake vorlex breakdown

characteristics

NASA-TP-1676} p 15 N80-28304

HYDRAZINES

Tnpie point determinations of monomethylhydrazine and

nitrogen tetroxide, 2.2 percent by weight nitric oxide

NASA-RP-1013] p 96 N78-13234

HYDROCARBON COMBUSTION

Thermodynamic and transpod combustion properties of

hydrocarbons with air. Part 1: Properties in SI units

NASA-TP-1906] p 195 N82-32186

Thermodynamic and transport combustion properties of

hydrocarbons with air, Part 2: Compositions corresponding

to Kelvin temperature schedules in part 1

NASA-TP-1907] p 195 N82.32187

Thermodynamic and transport combustion properties of

hydrocarbons with air. Part 3: Properties in US customary

units

NASA-TP-1908] p 195 N82-32t88

Thermodynamic and transport combustion properties of

hydrocarbons with air. Part 4: Compositions corresponding

to Rankine temperature schedules in part 3

NASA-TP-1909J p 195 N82-32189

HYDROCARBON FUELS

Jet aircraft hydrocarbon fuels technology

[NASA'CP-2033] p 97 N78-19325

Spectral flame radiance from a tubular-can combustor

[NASA-TP-1722] p 48 N81-19121

Recent trends in aviation turbine fuel properties

[NASA-TP-2056] p 97 N83-1 t340

Combustion gas propertie& 2: Natural gas fuel and

dry air

[NASA-TP-2435] p 52 N85-21168

Fuel-rich catalytic combustion: A soot-free technique

for in situ hydrogen-like enrichment

[NASA-TP-2498J p 85 N85-31244

Rapid estimation of concentration of aromatic classes

in middistillate fuels by high-performance liquid

chromatography

{NASA-TP-2495j p 98 N85-31307

HYDROCARBONS

Chemical kinetic models for combustion of hydrocarbons

and formation of nitric oxide

[NASA-TP-1794] p 85 N81-14017

Homogeneous reactions o1 hydrocarbons, silane, and

chlorosilanes in radiofrequency plasmas at low

pressures

{NASA-TP-2301 ] p 79 N84-20643

Group-type hydrocarbon standards for

high-performance liquid chromatographic analysis of

middistillate fuels

[NASA-TP-2317] p 97 N84-23774

HYDROCHLORIC ACID

Enhanced hydrophilicity of chlobded aluminum oxide

particulates

[ NASA-TP-13121 p84 N79-12178

Characterization of soil and posttaunch pad debris from

Cape Canaveral taunch complex and analysis of sod

interaction with aqueous HCI

iNASA-TP-20761 p 150 N83-12595

HYDRODYNAMICS

Effect of geometry on hydrodynamic film thickness

[NASA-TP-1287] p 119 N78-30585

Self-acting lift-pad geometry for circumferential seals:

A noncontacting concept --- performance tests on

hydrodynamic seals

[NASA-TP-15831 p 12t N80-14403

Classical aerodynamic theory

[NASA-RP-10501 p 13 N80-15033

Combustion Fundamentals Research

[ NASA-CP-22681 p 50 N83-29208

Dynamic behavior of spiral-groove and Rayleigh-Step

self-acting face seals

[NASA-TP-22661 p 51 N84-16181

Rotordynamic instability Problems in High-Performance

Turbomachinery

(NASA-CP-23381 p 124 N85-14116

Mechanics of a gaseous film barrier to lubricant wetting

of elastohydrodynamically lubricated coniunctions

I NASA-TP-25001 p 125 N85-32330

HYDROELASTICITY

Hydroelastic vibration analysis of partially liquid-filled

shells using a series representation ot the liquid

I NASA-TP-15581 p 129 N80-19563

HYDROGEN

Combustion of hydrogen in a two-dimensional duct with

step fuel injectors

{NASA-TP-1159] p 42 N78-23093

Electrical enclosure hydrogen intrusion study --- purging

Cape Kennedy Launch Complex 39

INASA-TP-1461 ] p 191 N79-25861

Criteria for self-ignition of supersonic hydrogen-air

mixtures

INASA-TP-1457] p 45 N79-29192

Effect of vacuum processing on oufgassieg within an

orbiting molecular shield

[NASA-TP-1980] p 99 N82-19390

Vibrational-Rotational Spectroscopy for Planetary

Atmospheres, volume 2

[NASA-CP-2223-VOL-2] p 207 N82-26134

Ignition of SiH4-H2-O2-N2 behind reflected shock

waves

[NASA-TP-2114] p 50 N83-18727

HYDROGEN CHLORIDES

A gas fitter correlation monitor for CO, CH4, and HCI

[NASA-TP-1113] p 113 N78-13408

Adsorption and chemical reaction of gaseous mixtures

of hydrogen chloride and water on aluminum oxide and

application to solid-propellant rocket exhaust clouds

[NASA-TP-1105] p 84 N78-22188

Analytic model for washout of HCI(g) from dispersing

rocket exhaust clouds

[NASA-TP-1801] p 149 N81-24601

Application of a Gaussian multilayer diffusion model to

characterize dispersion of vertical HCI column density in

rocket exhaust clouds

[NASA-TP-1956] p 149 N82-14672

Effects of environment on microhardness of magnesium

oxide

[NASA-TP-20O2] p 95 N82-22366

Airborne measurements of launch vehicle effluent:

Launch of Space Shuttle (STS-1) on 12 Aprit 1981

[NASA-TP-2090I p 150 N83-16952

HYDROGEN EMBRITTLEMENT

An electrochemical method for determining hydrogen

concentrations in mefats and some applicalions

INASA-TP-21131 p 88 N83-16491

HYDROGEN FUELS

Liquid hydrogen as a propulsion fuel, 1945-1959

INASA-SP-44041 p 97 N79-16994

Chemical kinetic analysis of hydrogen-air ignition and

reaction times

INASA-TP-18561 p 85 N81-27223

Aerodynamic characteristics, including effect of body

shape, of a Mach 6 aircraft concept

[NASA-TP-22351 p 22 N84-13164

Analysis of a topping-cycle, aircraft, gas-turbine-engine

system which uses cryogenic fuet

[ NASA-TP-22941 p 51 N84-21549

Combustion gas properties Part 3: Hydrogen gas fuel

and dry air

{ NASA-TP-24771 p 52 N85-31058

HYDROGEN MASERS

Proceedings of the 12th Annua_ Precise Time and Time

Interval (PTTI) Applications and Planning Meeting

[NASA-CP-21751 p 117 N81-27467

Proceedings of the Thirteenth Annual Precise Time and

Time Interval (PTTI) Applications and Ptanning Meeting

[NASA-CP-2220 j p 118 N82-20494

Proceedings of the 14th Annual Precise Time and Time

Interval (PTTI) Applications Planning Meeting

[NASA-CP-22651 p 118 N83-35351

HYDROGEN OXYGEN ENGINES

Hydrogen film cooling of a small hydrogen-oxygen thrust

chamber and its effect on erosion rates of various ablative

materials

{NASA-TP-t0981 p 76 N78q3124

Advanced High Pressure O2/H2 Technology

[NASA-CP-23721 p 78 N85-26862

HYDROGEN PEROXIDE

Description of an expenmental (hydrogen peroxide)

rocket system and its use in measuring aileron and rudder

effectiveness of a light airplane

I NASA-TP-16471 p 55 N80-22358

HYDROGENATION

Enhanced hydrophihclty of chiorided aluminum oxide

particulates

INASA-TP-13121 p 84 N79-12178

Effect of hydroprocessing severit,/on characteristics of

let fuel from OSCO 2 and Paraho distillates

INASA-TP-1768} p 97 N81-24283

HYDROLOGY

Operationa_ Applications of Satellite Snowcover

Observations

IE80-101671 p 139 N80-25742

Microwave remote sensing of snowpack properties

[NASA-CP-2153] p 139 N81-19511

The Multispectral Imaging Science Working Group

Volume 1 Executive summary

[E85-100011 p 142 N85-11404

The Multispectral Imaging Science Working Group

Volume 2: Working group reports

[E85-10002] p 142 N85-11405

HYDROLOGY MODELS

Applications systems verification and transfer project.

Volume 6: Operational applications of satellite snow-cover

observations NOAA/NESS support study

INASA-TP-1827] p 140 N82-20622

Remote Sensing of Snow and Evapotranspiration

[NASA-CP-2363] p 143 N85-23223

HYDROLYSIS

Development of silane-hydrolysate binder for

UV-resistant thermal control coatings

[NASA-TP-1900] p 94 N81-31365

HYGROSCOPICITY

Moisture diffusion parameter characteristics for epoxy

composites and neat resins

[NASA-TP-1474] p 80 N79-29241

HYPERBOLAS

Pressures, forces, moments and shock shapes for a

geometrically matched sphere-cone and hyperboloid at

Mach 20.3 in helium --- 22-inch aerodynamics leg of the

Langley hypersonic helium tunnel facility

[NASA-TP-2100] p 110 N83-16675

HYPERGOLIC ROCKET PROPELLANTS

Proceedings of the NASA/Florida Institute of

Technology Environmental Engineering Conference on

Nitrogen Tetroxide --- with emphasis on space shuttle

t'NASA-CP-20491 p 136 N79-20424

HYPERSONIC AIRCRAFT

Aerodynamic characteristics at Mach numbers from 0.33

to 1 20 of a wing-body design concept for a hypersonic

research airplane

{NASA-TP-1044] p 6 N78-12038

Aerodynamic characteristics at Mach number 0.2 of a

wing-body concept for a hypersonic research airplane

[NASA-TP-t 189] p 8 N78-25059

Aerodynamic characteristics at Mach 6 of a wing-body

concept for a hypersonic research airplane

[NASA-TP-1249] p 8 N78-30055

Aerodynamic characteristics of a hypersonic research

airplane concept having a 70 deg swept double-delta wing

at Mach number 0.2

[NASA-TP-1252] p 9 N78-31045

Recent Advances in Structures for Hypersonic Flight,

part 1 --- conferences

[NASA-CP-2065-PT-1 ) p 128 N79-21422

The use of compuTer-generated color graphic images

for transient thermal analysis --- for hypersonic aircraft

[NASA-TP-1455] p 107 N79-30518

Aerodynamic characteristics of a hypersonic research

airplane concept having a 70 dog swept double-delta wing

at Mach numbers from 0 80 to 120, with summary of data

from 020 to 6.0 --- Langley 8-fl transonic wind tunnel

INASA-TP-1552J p 13 N80-12064

Aerothermal performance of radiatively and actively

cooled panel at Mach 66

[NASA-TP-1595] p 107 N80-13402

Loading tests of a wing structure for a hypersonic

aircraft

[NASA-TP-1596] p 34 N80-15068

Flightweight radiantly and actively cooled panel:

Thermal and structural performance

INASA-TP-2074J p 131 N83-11513

Wall-temperature effects on the aerodynamics of a

hydrogen-fueled transport concept in Mach 8 blowdown

and shock tunnels

I NASA-TP-2159] p 21 N83-30391

Aerodynamic characteristics, including effecl of body

shape, of a Mach 6 aircraft concept

INASA-TPo22351 p 22 N84-13164

Aerodynamic characteristics of a distinct wing-body

configuration at Mach 6: Expenment, theory, and the

hypersonic isolation principle

INASA TP-24671 p 27 N85-33107

HYPERSONIC FLIGHT

Recenl Advances in Structures for Hypersonic Flight,

part 2

INASA-CP-2065-PT-21 p 128 N79-21435

HYPERSONIC FLOW

A hybridized method for computing

high-Reynolds-number hypersonic flow about blunt

bodies

[NASA-TP-1497} p 107 N79-33441

Determination of the

hypersonic continuum/rarefied-flow drag coefficient of the

Viking lander capsule 1 aeroshell from flight data

[NASA-TP-1793] p 3 N81-14961

Experimental and predicted heating distributions for

biconics at incidence in air at Mach 10

INASA-TP-2334J p 112 N85-12313

Laminar heat-transfer distributions on biconics at

incidence in hypersonic-hyperveIocity flows

INASA-TP-2213] p 112 N85-16065

A-63
HYPERSONIC HEAT TRANSFER SUBJECT INDEX

Experimental aerodynamic heating to simulated space

shuttle tiles in laminar and turbulent boundary layers with

variable flow angles at a nominal Mach number of 7

[NASA-TP-2307 } p 113 N85-34351

HYPERSONIC HEAT TRANSFER

Aerothermal tests of a heat-pipe-cooled leading edge

at Mach 7 --- hypersonic heat transfer for space shuttle

orbiters

{NASA-TP-13201 p 195 N79-13901

HYPERSONIC SPEED

Mach 6 flow field surveys beneath the forebody of an

airbreathmg missile

I NASA-TP-2491 I p 28 N86-23558

HYPERSONIC VEHICLES

Configuration heating for a hypersonic research airplane

concept having a 70 deg swept double-delta wing

I NASA-TP-t 1431 p 105 N78-23389

HYPERSONIC WIND TUNNELS

Aerodynamic characteristics at Mach 6 of a wiog-body

concept for a hypersonic research airplane

INASA-TP-t249_ p 9 N78-30055

Aeronautical facilities catalogue Volume 1: Wind

tunnels

INASA-RP-1132} p60 N85-1899t

HYPERSONICS

Application of supersonic linear theory and hypersonic

impact methods to three nonslender hypersonic airplane

concepts at Mach numbers from 1_10 to 2.86

INASA-TP-1539] p 13 N80-12065

Measured and predicted shock shapes and aerodynamic

coefficients for blunted cones at incidence in air at Mach

5.9

INASA-TP.t652J p 108 N80-23600

HYPERTHERMIA

Hyperthermia as an Antineoplastic Treatment Modality

INASA-CP-205t ] p 170 N79.t0728

HYPERVELOCITY FLOW

Laminar heat-transfer distributions on biconics at

incidence in hypersonic-hypervetocity flows

INASA-TP-2213] p 112 N85-16065

HYPERVELOCITY tMPACT

Orbital Debris

[NASA-CP-2360] p 63 N85-21188

HYPERVELOCITY LAUNCHERS

Rail accelerators for Space transportation: An

experimental investigation

{NASA-TP-2571 J p 78 N86-28123

HYSTERESIS

Results ot the first complete static calibration of the

RSRA rotor-load-measurement system

[ NASA-TP-2327 ] p37 N84-31111

I

ICE

Cloud-encounter and particle-concentration variabilities

from GASP data

[NASA-TP-1886] p 164 N82-15677

Radiometer requirements for Earth-observation systems

using large space antennas

{NASA-RP-tlOt] p 116 N83-28410

North Atlantic Deep Water Formation

{NASA-CP-2367 } p 169 N85-26028

tCE FORMATION

Aircraft icing

( NASA-CP-2086 } p 12 N79-23912

Ice crystal growth in a dynamic thermal diffusion

chamber

{NASA-TP-1651 1 p 162 N80-23934

tCE MAPPING

The rote ot satellite altimetry in climate stud0es

[NASA-TP-f5701 p 161 N80-16676

Antartlc sea ice, 1973 1976: Satelhte

passive-microwave observations

{NASA-SP-4591 p 168 N84-10718

ICE NUCLEI

The Third International Cloud Condensation Nuclei

Workshop -- conference

[ NASA-CP-2212 } p 115 N82-15383

IDEAL GAS

Simulation of ideal-gas flow by nitrogen and other

selected gases at cryogenic temperatures --- transonic flow

in cryogenic wind tunnels

[NASA-TP-1901 } p 109 N81-32418

GCKP84-general chemical kinetics code for gas-phase

flow and batch processes including heat transfer effects

[NASA-TP-23201 p 85 N84-32446

IGNITION

Chemical kinetic analysis of hydrogen-air ignition and

reaction times

[ NASA-TP-18561 p 85 N81-27223

Ignitfon of SiH4-H2-O2-N2 behind reflected shock

waves

{ NASA-TP-21141 p50 N83-18727

A chemical kinettc mixture tor the ignition of

silane/hydrogen mixtures

INASA-TP-2129] p 85 N83-19825

Preliminary tests of an advanced high-temperature

combustion system

{NASA-TP-22031 p 50 N83-33893

Ignition of mixtures of Sill sub 4, CH sub 4, O sub 2,

and Ar or N sub 2 behind reflected shock waves

[NASA-TP-24151 p 52 N85-22395

IGNITION LIMITS

Criteria for self.ignition of supersonic hydrogen-air

mixtures

[NASA-TP-1457] p 45 N79-29192

ILLUMINATING

Illumination from space with orbiting solar-reflector

spacecraft

[NASA-TP-2065J p 74 N82-3342t

IMAGE ANALYSIS

Proceedings of the National Conference on Energy

Resource Management. Volume 1: Techniques,

Procedures and Data Bases

{E83-10335] p 141 N83-26155

Trends in Ptanetary Data Analysis Executive summary

of the Planetary Data Workshop

{NASA-CP*2333} p 208 N84-34363

The Multispectral imaging Science Working Group.

Volume 1: Executive summary

{E85-10001J p 142 N85-11404

The Multispectral Imaging Science Working Group

Volume 2: Working group reports

{E85-10002] p 142 N85-11405

IMAGE CONVERTERS

Effect of image tilt of a virlual image display on simulated

transport touchdown performance

[NASA-TP-1520J p 33 N79-33189

IMAGE INTENSIFIERS

Analysis and design of a refractive virtual image

system

{NASA-TP-1066} p 193 N78-12829

IMAGE PROCESSING

Synthetic aperture radar/LANDSAT MSS image

registration

{NASA-RP-1039] p 139 N80-16405

Conference of Remote Sensing Educators

(CORSE-78)

{NASA-CP-2102I p 212 N80-20003

Computerized video densitometry method for rapid

analysis of infrared photographic images --- temperature

distribution across a turbine blade

INASA-TP-1686} p 114 N80-25635

Operational Applications of Satellite Snowcover

Observations

IE80-t0167} p 139 N80-25742

High speed lookup table approach to rsdiometric

calibration of multispeetral image data

INASA-TP-1741} p 76 N80-33463

Digital processing of remotely sensed images

[NASA-SP-431 ] p 139 N81-20489

A design approach to real-time formatting of high speed

multispeetral image data

[NASA-TP-1870} p 178 N81-25690

The LANDSAT tutorial workbook: Basics of satellite

remote sensing

[E83-1000t ] p 141 N83-10458

Automated rendezvous and docking: A parametric

study

[NASA-TP-2314} p 74 N84-23677

LANDSAT-4 Sc,'ence Investigations Summary, including

December 1983 Workshop results, volume 1

{E84-101661 p 137 N84-30359

LANDSAT-4 Science Investigations Summary, including

December 1983 Workshop results, volume 2

[E84-10167} p 137 N84-30380

Planetary Data Workshop, part 2

{NASA-CP-2343-PT-2] p 208 N84-34376

Conclusion of Viking Lander Imaging Investigation:

P,'cture catalog of experiment data record

[ NASA-RP-1137 } p 208 N85-21099

LANDSAT-4 Science Characterization Early Resutts

Volume 4: Applications --- agriculture, sorts land use.

geology, hydrology, wetlands, water quality, biomass

identification, and snow mapping

{E85-10070} p 143 N85-23186

LANDSAT-4 and LANDSAT-5 multispectral scanner

coherent noise characterization and removal

{NASA-TP-2595} p 143 N86-31945

IMAGE RECONSTRUCTION

Aliased noise in radiometric measurements

JNASA-TP-1639 } p 114 N80-22660

Viking lander imaging _nvestigation during extended and

continuation automatic missions. Volume 1: Lander 1

picture catalog of expenment data record

INASA-RP-1068} p 206 N81-25012

Viking lander imaging investigation during extended and

continuation automatic missions Volume 2: Lander 2

picture catalog ol experiment data record

[NASAoRP-1068-VOL-2J p 207 N82-16028

IMAGE RESOLUTION

Atiased noise in radiometric measurements

[ NASA-TP-16391 p t 14 N80-22660

The Multispectral _maging Science Working Group

Volume 3: Appendices

[E83-t0351 J p 142 N83-28506

The Multispectral Imaging Science Working Group.

Volume 1: Executive summary

{E85-100011 p 142 N85-11404

The Multispectral Imaging Science Working Group,

Volume 2: Working group reports

[ES5-10002] p 142 N85-11405

LANDSAT-4 Science Characterization Early Results

Volume 3, part 2: Thematic Mapper (TM}

[E85-100691 p 143 N85-21724

IMAGE TUBES

Analysis and design of a refractive virtual image

system

[NASA-TP-t0661 p 193 N78-12829

IMAGERY

Eulusmap: An international land resources map utilizing

satellite imagery

[NASA-TP-t371 I p 138 N79-13475

IMAGES

Educator's guide for Mission to Earth: LANDSAT views

the world

[NASA-SP-360} p 138 N80-10537

IMAGING TECHNIQUES

Performance analysis of grazing incidence imaging

systems --- X ray telescope aberrations

{NASA-TP-1088J p 193 N78-11812

Viking Lander imaging investigation: Picture catalog of

pnmary mission experiment data record

{ NASA-RP-tO07} p 205 N78-20042

Holography through optically active windows

{NASA+TP*1414} p 114 N79-17195

The use of computer-generated color graphic images

tot transient thermal analysis --- for hypersonic aircraft

[NASA-TP-1455} p 107 N79-30518

The time-space relationship of the data point (Pixets)

of the thematic mapper and multispectral scanner or the

myth of simultaneit'/

[NASA-TP-1715} p 76 N80-28424

Effects of magnification and visual accommodation on

aimpoint estimation in simulated landings with real and

virtual image displays

INASA-TP-1635] p 171 N80-34099

Spatial frequency response of an optical heterodyne

receiver

{NASA-TP-1763} p 194 N81-13739

Digital processing of remotely sensed images

{NASA-SP-431] p 139 N81-20489

Application of information theory to the design of

line-scan imaging systems

INASA-TP-1897] p 115 N81-33452

Western Regional Remote Sensing Conference

Proceedings, 1981

[E82-10104] p 141 N82-22546

The Multispectral Imaging Science Working Group.

Volume 3: Appendices

[E83-10351] p 142 N83-28506

LANDSAT-4 Science tnvestigabons Summary, including

December 1983 Workshop results, volume 2

{E84-10167] p 137 N84-30380

An image compression survey and algorithm switching

based on scene activity

{NASA-TP-2458J p 27 N85-33106

IMPACT DAMAGE

Scanning-electron-microscope study of

normal-impingement erosion of ductile metals

{NASA-TP-f609J p 87 N80-16141

Crash tests of four identical high-wing single-engine

airplanes

[NASA-TP-1699} p 35 N80-30296

Solid spherical glass particle impingement studies of

plastic materials

I NASA-TP-2161 I p 95 N83-24695

Orbital Debris

I NASA-CP-23601 p 63 N85-21188

IMPACT LOADS

Analytical investigation of the landing dynamics ot a large

airplane with a load-control system in the main landing

gear

[NASA-TP-1555] p 33 N80-13025

Orbiter landing loads math model description and

correlation with ALT flight data

lNASA-RP-f056] p 71 N80-16091

Impact data from a transport aircraft during a controlled

impact demonstration

{NASA-TP-2589] p 38 N86-30721

A-64
SUBJECT INDEX INFRARED SCANNERS

IMPACT RESISTANCE

Effects of erodant particle shape and various heat

treatments on erosion resistance of plain carbon steel

[NASA-TP-1755] p 87 N81-16210

Correlation and assessment of structural airplane crash

data with flight parameters at impact

[NASA-TP-2083] p 131 N83-14521

IMPACT STRENGTH

Study of austenitic stainless steel welded with low alloy

steel filter metal --- tensile and impact strength tests

{NASA-TP-1460] p 87 N79-28288

Research in structural and solid mechanics, 1982

[NASA-CP-2245] p 131 N82-33739

Tough Composite Materials

[NASA-CP-2334] p 83 N85-12941

Effect of low-velocity or ballistic impact damage on the

strength of thin composite and aluminum shear panels

[NASA-TP-2441] p 83 N85-26924

IMPACT TESTS

Light airplane crash tests at three flight-path angles

[NASA-TP-1210] p 127 N78-26494

Light airplane crash tests at three roll angles

[NASA-TP-1477] p 128 N80-10512

Light airplane crash tests at three pitch angles

[NASA-TP-1481] p 128 N80-11505

Mechanical impact tests of materials in oxygen effects

of contamination --- Teflon, stainless steel, and

aluminum

[NASA-TP-1571 I p 97 N80-21551

Crash tests of four identical high-wmg singio-engine

airplanes

[NASA-TP-1699] p 35 N80-30296

Crash tests of four low-wing twin-engine airplanes with

truss-reinforced fuselage structure

[NASA-TP-2070] p 131 N83-10442

Correlation and assessment of structural airplane crash

data with flight parameters at impact

[NASA-TP-20831 p 131 N83-14521

Failure mechanics in low-velocity impacts on thin

composite plates

[NASA-TP-2152J p 82 N83-24562

Full-scale crash-test evaluation of two load-limiting

subfloors for general aviation airframes

[NASA-TP-2380] p 134 N85-13267

Full-Scale Transport controlled Impact Demonstration

[NASA-CP*2395] p 135 N86-21933

Impact data from a transport aircraft during a controlled

impact demonstration

[NASA-TP-2589] p 38 N86-30721

IMPACT TOLERANCES

Light airplane crash tests at impact velocities of 13 and

27 m/sec

[NASA-TP-1042] p 29 N78-10034

IMPEDANCE PROBES

A method for determining acoustic-liner admittance in

ducts with sheared flow in two-cross-sectional directions

[NASA-TP-2518J p 190 N86-13056

IMPINGEMENT

TACT 1: A computer program for the transient thermal

analysis of a cooled turbine blade or vane equipped with

a coolant insert. 2 Programmers manual

[NASA-TP-1391 ] p 106 N79-18288

UnNersal approach to analysis of cavitation and

liquid-impingement erosion data

[NASA-TP-2061} p 88 N83-15413

Solid spherical glass particle impingement studies of

plastic materials

[NASA-TP-2161 ] p 95 N83-24695

Experimental aerodynamic heating to simulated space

shuttle tiles in laminar and turbulent boundary layers with

variable flow angles at e nominal Mach number of 7

(NASA-TP-23071 p 113 N85-34351

Textured carbon on copper: A novel surface with

extremely low secondary electron emission

characteristics

[NASA-TP-2543 j p 96 N86-15394

IN-FUGHT MONITORING

Determinabon of stability and control parameters of a

light airplane from flight data using two estimation methods

--- equation error and maximum likelihood methods

[NASA-TP-130,6] p 11 N79-20071

Processing of on-board recorded data for quick analysis

of aircraft performance --- rotor systems research

aircraft

[NASA-RP-1043J p 33 N79-33191

Flight-measured afterbody pressure coefficients from an

airplane having twin side-by-side jet engines for Mach

numbers from 06 to 1 6

[NASA-TP-1549J p 13 N80-11035

Flight evaluation of a simplified gross thrust calculation

technique using an F100 turbofan engine in an F-15

airplane

[NASA-TP-1782} p 48 N81-15000

In-flight transition measurement on a 10 deg cone at

Maeh numbers from 05 to 20

[NASA-TP-1971 ] p 19 N82-26227

INCIDENCE

Performance analysis of grazing incidence imaging

systems --- X ray telescope aberrations

[NASA-TP-1088i p 193 N78-11812

Incidence loss for fan turbine rotor blade in

two-dimensional cascade

[NASA-TP-21881 p50 N83-30431

INCIDENT RADIATION

Performance analysis of grazing incidence imaging

systems --- X ray telescope aberrations

[NASA-TP-1088J p 193 N78-11812

INCOMPRESSIBLE FLOW

Approximate indicial lift function for tapered, swept wings

in incompressible flow

iNASA-TP-1241 J p 9 N78-30054

Classical aerodynamic theory

[NASA-RP-1050] p 13 N80-15033

Velocity-split Navier-Stokes solution procedure for

incompressible high Reynolds number external flows

[NASA-TP-16551 p 108 N80-21702

Mean-flow and turbulence measurements in the vicinity

of the trailing edge of an NACA (63 sub 1)-012 airfoil

[NASA-TP-1845) p 109 N81-23410

Analysis of gap heating due to stepped tiles in the shuttle

thermal protection system

[NASA-TP-2209J p 74 N83-31713

INCOMPRESSIBLE FLUIDS

Damping in tapered annular seals for an incompressible

fluid

[NASA-TP-1646J p 121 N80-19495

INCONEL (TRADEMARK)

Galvanic coupling between D6AC steel, 6061-T6

aluminum, Inconel 718 and graphite-epoxy composite

material: Corrosion occurrence and prevention

[NASA-TP-2236J p 89 N84-13263

A mechanical property and stress corrosion evaluation

of VIM-ESR.VAR work strengthened and direct double

"aged Ineonel 718 bar material

[NASA-TP-2634] p 68 N86-30753

INDENTATION

Occurrence of spherical ceramic debris in indentation

and sliding contact

[NASA-TP.2048) p 95 N82-32491

INDEPENDENT VARIABLES

The mechanics of atmospheric systems derived through

vertical and honzontal analysis of parametric data

(NASA-TP-1072] p 158 N78-t564t

INDEXES (DOCUMENTATION)

NASA Thesaurus supplement: A 3-part cumulative

supplement to the 1982 edition of the NASA Thesaurus

[NASA-SP-7051(SUPPL-2)] p 198 N85-12785

Ninteenth International Cosmic Ray Conference.

Conference program and author index

4NASA-CP-2;.76] p 210 N85-33901

NASA thesaurus. Volume 1: Hierarchical listing

[NASA-SP-7053-VOL-1 ] p 198 N86-20168

NASA thesaurus. Volume 2: Access vocabulary

[NASA-SP-7053-VOL-2] p 198 N86-20169

Nineteenth International Cosmic Ray Conference

papers. General index, volume 10

INASA-CP-2376-VOL-101 p 211 N86-28904

INDIAN OCEAN

Satellite-derived global oceanic raintall atlas (1973 and

1974)

[NASA-SP-4t0] p 157 N77-19709

INDUCTION HEATING

A mechanical property and stress corrosion evaluation

of V]M-ESR-VAR work strengthened and direct double

aged Inconel 718 bar material

[NASA-TP-2634] p 68 N86-30753

INDUCTION MOTORS

Energy saving concepts relating to induction

generators

[NASA-TP-1719] p 146 N82-32859

INDUSTRIAL WASTES

Laboratory measurements of radiance and reflectance

spectra of a dilute biosolid industnal waste product

[NASA-TP-1401 ] p 148 N79-17360

Spectral measurements of ocean-dumped wastes tested

in the marine upwelled spectral signature laboratory

[NASA-TP-14801 p 168 N79-31890

INELASTIC STRESS

Materials constitutive models for nonlinear analysis of

thermally cycled structures

[NASA-TP-2055J p 131 N83-12449

Development of a simplified procedure for cyclic

structural analysis

[NASA*TP-2243} p 133 N84-20878

Nonlinear Structural Analysis

(NASA-CP-2297J p 133 N84-31688

Local strain redistribution corrections for a simplified

inelastic analysis procedure based on an elastic

finite-eioment analysis

[NASA-TP-2421 i p 134 N85-20396

INFORMATION DISSEMINATION

NASA publications guide

INASA-SP-7047J p 197 N83-32671

INFORMATION MANAGEMENT

Human Factors Considerations in System Design

[ NASA-CP-2246] p 173 N83-18238

INFORMATION RETRIEVAL

NASA Administrative Data Base Management

Systems

I NASA-CP-22541 p 197 N83-18559

NASA Thesaurus supplement: A 3-part cumulative

supplement to the 1982 edition of the NASA Thesaurus

[NASA-SP-7051(SUPPL-2)] p t98 N85-12785

NASA thesaurus. Volume 1 : Hierarchical listing

[NASA-SP-7053-VOL-1 ] p 198 N86-20168

NASA thesaurus. Volume 2: Access vocabulary

[NASA-SP-7053-VOL-2] p 198 N86-20169

INFORMATION SYSTEMS

Western Regional Remote Sensing Conference

Proceedings, 1981

{E82-10104] p 141 N82-22546

NASA Administrative Data Base Management

Systems

I NASA-CP-2254] p 197 N83-18559

Optical Information Processing for Aerospace

Applications 2

[NASA-CP-2302"_ p 194 N84-22402

Hybrid routing technique for a fault-tolerant, integrated

information network

[NASA-TP-2605] p 180 N86-27947

Proceedings of the Second Pilot Climate Data System

Workshop

[NASA-CP-2430] p 137 N86-29282

INFORMATION THEORY

Application of information theory to the design of

line-scan imaging systems

[NASA-TP-1897] p 115 N81-33452

INFRARED ASTRONOMY

Large Deployable Reflector Science and Technology

Workshop. Volume 2: Scientific Rationale and Technology

Requirements

INASA-CP-2275-VOL-2] p 202 N83-27939

Far infrared supplement: Catalog of infrared

observations

INASA-RP-1119] p202 N84-26519

Catalog of infrared observations including: Bibliography

of infrared astronomy and index of infrared source

positions

[NASA-RP-1118] p 202 N84-26520

Large Deployable Reflector Science and Technology

Workshop. Volume 3: Systems and Technology

Assessment

[NASA-CP-2275-VOL-3J p 202 N84-32318

Airborne Astronomy Symposium. A symposium

commemorating the tenth anniversary of operations of the

Kuiper Airborne Observatory

I NASA-CP-2353] p 202 N85-17848

INFRARED DETECTORS

Heterodyne systems and technology, part 1 ---

conferences

[NASA°CP-2138-PT-1 I p 117 N80-29652

INFRARED FILTERS

A gas filter correlation monitor for CO, CH4, and HCl

[NASA-TP-1113] p 1t3 N78-13408

INFRARED IMAGERY

Influence of coolant tube curvature on film cooling

effectiveness as detected by infrared imagery

[ NASA-TP-1546] p45 N80-11087

Aerial color infrared photography: Applications in

citriculture --- Florida

INASA-RP-1067] p 139 N8t-21437

The Heat Capacity Mapping Mission (HCMM)

anthology

[E84-10051 ] p 142 N84-14563

INFRARED PHOTOGRAPHY

Computerized video densitometry method for rapid

analysis of infrared photographic images --- temperature

distribution across a turbine blade

[NASA-TP-1686] p 114 N80-25635

INFRARED RADIATION

Large Deployable Reflector Science and Technology

Workshop. Volume 3: Systems and Technology

Assessment

[NASA-CP-2275-VOL-31 p 202 N84-32318

INFRARED RADIOMETERS

Analyses of earth radiation budget data from unrestricted

broadband radiometers on the ESSA 7 satellite

{NASA-TP-1402} p 160 N79-22709

Vibrational-Rotational Spectroscopy For Planetary

Atmospheres, volume 1

[NASA-CP-2223-VOL-1] p 207 N82-25043

INFRARED SCANNERS

Some physical and thermodynamic properties of rocket

exhaust clouds measured with infrared scanners

{NASA-TP-10411 p 147 N78-11520

A-65
INFRARED SPECTRA SUBJECT INDEX

Spatial-frequency response of the limb infrared monitor

of the stratosphere

[NASA-TP-1504] p 148 N79-29679

INFRARED SPECTRA

Proceedings of the Large Deployable Reflector Science

and Technology Workshop Volume 1: Executive

Summary

[NASA.CP.2275-VOL-1} p 202 N84-28709

INFRARED SPECTROSCOPY

High Resolution Infrared Spectroscopy Techniques for

Upper Atmospheric Measurements

INASA-CP-2134} p 152 N80-27866

Heterodyne Systems and Technology, part 2

[NASA-CP-2138.PT-2J p 117 N80-29672

INFRARED TRACKING

Atmospheric solar absorption measurements in the 9

to 1 I mum region using a diode laser heterodyne

spectrometer

{ NASA-TP-1726J p 153 NS0-3399S

INJECTORS

Experimental and analylical study of nitric oxide

formation during combustion of propane in a jet-stirred

combustor

[NASA-TP-1181J p 84 N78-23172

Feasibility study of LITVC for shuttle SRB

[NASA-TP-lg12] p 77 N81-33231

INLET AIRFRAME CONFIGURATIONS

Flight and wind-tunnel compansons of the inlet-airframe

interaction of the F-15 airplane

{NASA-TP-2374] p 37 N85-12884

Performance and surge limits of a TF30-P-3 turbofan

engine/axisymmetnc mixed-compression inlet propulsion

system at Mach 2 5

[NASA-TP-2461 } p 52 N85-25261

INLET FLOW

Effects of temperature transients at fan inlet of a turbofan

engine

INASA-TP-1031 j p 41 N77-31153

Effect of design changes on aerodynamic end acoustic

performance ol translating-centerbody sonic inlets

[NASA-TP-1132} p 7 N78-17998

Simulated flight effects on noise characteristics of a fan

inlet with high throat Mach number

I NASA-TP-t 199 } p 42 N78-20132

Theoretical flow characteristics of inlets for tilting-nacelle

VTOL aircraft

{ NASA-TP-1205 J p42 N78-21114

Theoretical study of VTOL tilt-nacelle axisymmetric inlet

geometries

[NASA-TP-f380J p 10 N79-14996

Effect of rotor mendional velocity ratio on response to

inlet radial and circumferential distortion

{NASA-TP-12781 p 45 N79-28177

Numerical analysis ol the scramjet-inlet flow field by

using two-dimensional Navier-Stokes equations

NASA-TP-1940} p 48 NB2-13142

Theoretical and experimental engine-inlet flow fields for

fighter forebodies

NASA-TP-2270} p 23 N84-17132

Flow rates and pressure profiles for one to four axially

alined Borda inlets

I NASA-TP-2390} p 112 N65-14078

Effects of inlet distortion on a static pressure probe

mounted on the engine hub in an F-15 airplane

NASA-TP-24t 1 ] p 52 N85-22394

Flow rate and pressure profiles for 1 to 4 axialty alined

orifice inlets

tNASA-TP-2460J p 112 N85-27165

INLET PRESSURE

Some flow phenomena associated with aligned,

sequential apertures with Borda-type inlets --- inlet

pressure and flow separation

{NASA-TP-17921 p 109 N81-24387

Flow rates and pressure profiles for one to four axially

alined Borda inlets

[NASA-TP-2390] p 112 N85-14078

INLET TEMPERATURE

Low-pressure performance of annular, high-pressure (40

atm) h_gh-temperature (2480 K) combustion system

[NASA-TP-1713] p 47 N80-32396

INORGANIC COATINGS

Control of volume resistivity in inorganic organic

separators

[NASA-TP-1439] p 84 N79-22246

INORGANIC COMPOUNDS

Improved, low cost _norganic-organic separators for

rechargesble silver-zinc batteries

{NASA-TP-1476J p 84 N79-25181

INPUT/OUTPUT ROUTINES

Effects of control inputs on the estimation of stability

and control parameters of a light airplane

{NASA-TP-10431 p 53 N78-13071

INSECTS

Radar, Insect Population Ecology, and Pest

Management

{NASA-CP-2070] p 169 N79-19592

INSOLATION

Earth Radiation Science Seminars

INASA-CP-22391 p 210 N82-33320

INSPECTION

Procedures for precsp visual inspection

[NASA-RP-1122} p 103 N85-13156

INSTITUTIONS

Model research: The National Advisory Committee for

Aeronautics, 1915-1958, volume 1

[NASA-SP-4103-VOL-1 I p 4 N85-23683

Model research, the National Advisory Committee for

Aeronautics, 1915-1958, volume 2

[NASA-SP-4103-VOL-2] p 4 N85-23684

INSTRUMENT APPROACH

Simulation study of traffic-sensor noise effects on

utilization of traffic situation display for self-spacing task

[NASA-TP-2082} p 40 N83-18723

INSTRUMENT ERRORS

Total ozone measurement: Intercompadson of

prototype New Zealand filter instrument and Dobson

spectrophotometer

[NASA-TP-1277] p 114 N78-28412

instrument error analysis as it applies to wind-tunnel

testing

[NASA-TP-1572] p 114 N80-13430

Simulation study of traffic-sensor noise effects on

utilization of traffic situation display for self-spacing task

{NASA-TP-2082} p 40 N83-18723

INSTRUMENT FLIGHT RULES

Controls, Displays, and Information Transfer for General

Aviation IFR Operations

INASA-CP'22791 p 4 N84-12029

INSTRUMENT LANDING SYSTEMS

Flight-test evaluation of two electronic display formats

for approach to tending under instrument conditions

INASA-TP-10851 p 38 N78-13054

Development of systems and techniques for landing an

aircraft using onboard television

t NASA-TP-t 171 j p32 N78-20114

Airline pilot scan patterns during simulated ILS

approaches

[NASA-TP-1250} p 171 N79-19682

Flight-test evaluation Of STOL control and flight director

concepts in a powered-lift aircraft flying curved

decelerating approaches

[NASA-TP-1641 J p 56 N61-19131

Simulator evaluation of separation of display parameters

m path-following tasks

[NASA-TP-19151 p 39 N8t-33203

A general aviation simulator evaluation of a

rate-enhanced instrument landing system display

{NASA-TP-19601 p 39 N82-14085

Simulator study of a pictorial display for general aviation

instrument flight

INASA-TP-1963] p 39 N82-20180

A comparison of two position estimate algorithms that

use ILS Iocalizer and DME information Simulation and

flight test results

[NASA-TP-2281 ] p 31 N64-17165

INSTRUMENT ORIENTATION

Effects of curved approach paths and advanced displays

on pilot scan patterns

{NASA-TP-1846] p 171 N81-23791

INSULATED STRUCTURES

Approximation methods for combined thermal/structural

design

{ NASA-TP-1428 ] p 128 N7g-25427

INSULATION

Effective thermal conductivity determination for

low-density insulating materials

(NASA-TP-1155] p 105 N78-18364

INTAKE SYSTEMS

Phugcid characteristics of s YF-12 airplane with

variable-geometry inlets obtained in flight tests at a Mach

number of 2.9

[NASA-TP-1107} p 52 N78-12100

A small gas inlet system for orbital mass-spectrometer

calibrations

{NASA-TP-11701 p 114 N78-21430

Pedormance with and without inlet radial distortion of

a transonic fan stage designed for reduced loading in the

tip region

[NASA-TP-1294] p 9 N78-30057

Design and overall performance of four highly loaded,

high speed inlet stages for an advanced high-pressure-ratio

core compressor

[NASA-TP-1337] p 43 N78-33108

Application of coherence in fan noise studies

[NASA-TP-1630] p 187 N80-18882

Performance of single-stage axial-flow transonic

compressor with rotor and stator aspect ratios of 1.63

and 1.78, respectively, and with design pressure ratio of

t 82

[NASA-TP-19741 p 49 N82-19222

Flight effects Of fan noise

l NASA-CP-2242 i p 18g N83-10883

Flow rates and pressure profiles for one to four axially

alined Borda inlets

[ NASA-TP-2390} p 112 N85-14078

Performance and surge limits of a TF30-P-3 turbofan

engine/axisymmetnc mixed-compression inlet propulsion

system at Mech 2.5

{NASA-TP-2461] p 52 N85-25261

INTEGRAL EQUATIONS

Noise transmission loss of a rectangular plate m an

infinite baffle

i NASA-TP-2398] p 190 N85-22109

A cracked orthotropic sheet stiffened by a semi-infinite

orlhotropic sheet

{NASA-TP-2456 p 134 N85-32339

INTEGRAL TRANSFORMATIONS

Geometric interpretations ol the Discrete Fourier

Transform (DFT)

NASA-TP-2332 p 177 N84-24114

INTEGRALS

An integral representation of the generalized

Euler-Mascheroni constants

NASA-TP-2456 p 177 N85-23305

INTEGRATED CIRCUITS

The PR2D (Place, Route in 2-Dimensions) automatic

layout computer program handbook

NASA-RP-t029 p 179 N81-12760

INTEGRATED ENERGY SYSTEMS

An Assessment of Integrated Flywheel System

TechnolOgy

NASA-CP-2346 p 78 N85-13850

INTEGRATED OPTICS

Optical Information Processing for Aerospace

Applications

NASA-CP-2207 p 194 N82-15894

INTERACTIVE CONTROL

Interactive design and analysis of future large spacecraft

concepts

NASA-TP-1937 p 72 N82-14276

AESOP: An interactive computer program for the design

of linear quadratic regulators and Kalman filters

[NASA-TP-2221 I p 181 N84-16843

MINDS: A microcomputer interactive data system for

8086-based controllers

{NASA-TP-2378} p 179 N85-17576

INTERATOMIC FORCES

Analysis of the physical atomic forces between noble

gas atoms, alkali ions and halogen ions

{NASA-TP-2568] p 90 N86-26413

INTERFACIAL ENERGY

Friction and metal transfer for single-crystal silicon

carbide in contact with various metals in vacuum

[NASA-TP-1191 I p 91 N78-21294

INTERFAClAL TENSION

Float Zone Workshop

[ NASA-CP-2179 } p62 N81-tg144

Hertzian contact in two and three dimensions

[NASA-TP-2473] p 125 N85-32331

INTERFERENCE

Effects of conversation interference on annoyance due

to aircraft noise

[NASA-TP-1712] p 149 N80-29911

INTERFEROMETERS

Project Orion: A design study of a system for detecting

extrasotar planets

INASA-SP-436] p 206 N80-27260

Large-aperture interferometer using local reference

beam

INASA=TP-2060} p 194 N83-13979

Optical elements formed by compressed gases:

Analysis and potential applications

{NASA-TP-2555t p 194 N86-22390

INTERFEROMETRY

Radio interferometry: Techniques for Geodesy ---

conference

{NASA-CP-2115 } p 139 N80-28798

INTERMODULATION

Computer modeling of multiple-channel input signals and

intermodulation losses caused by nonlinear traveling wave

tube amplifiers

{NASA-TP-1999] p 102 N82-25441

INTERMOLECULAR FORCES

Analysis of the physical atomic forces between noble

gas atoms, alkali ions and halogen ions

{ NASA-TP-2568 } p 90 N86-26413

INTERNAL COMBUSTION ENGINES

Development of an instrument for real-time computation

of indicated mean effective pressure

[NASA-TP-2238] p 102 N64-16461

Modeling the internal combustion engine

{NASA-RP-10941 p 182 N85-19733

INTERNAL COMPRESSION INLETS

Low-speed performance Of an axisymmetric,

mixed-compression, superson*c inlet with auxiliary inlets

tNASA-TP-25571 p 52 N86-24694

A-66
SUBJECT INDEX JET AIRCRAFT

INTERNAL FRICTION

Instability in Rotating Machinery

[NASA-CP-2409] p 126 N86-30160

INTERNATIONAL COOPERATION

Apol_o-Soyuz test project Volume 1: Astronomy, earth

atmosphere and gravity field, life sciences, and materials

processing

[NASA-SP-412] p 60 N78-17088

The partnership: A history of the Apollo-Soyuz test

project

I NASA-SP-42091 p 61 N79-10074

Significant NASA inventions available for licensing in

foreign countries

[NASA-SP-7038(08)] p 198 N86-26243

INTERPLANETARY DUST

Interrelationships among Circumstellar, Interstellar and

Interplanetary Dust

[NASA-CP-2403] p 201 N86-23493

INTERPLANETARY FLIGHT

Far travelers: The exploring machines

[NASA-SP-4801 p 63 N85-33126

INTERPLANETARY MAGNETIC FIELDS

Significant initial results from the environmental

measurements experiment on ATS-6

[NASA-TP-1101 ] p 65 N78-15142

Solar Terrestrial Physics: Present and Future

[NASA-RP-1120] p 200 N54-34332

INTERPLANETARY MEDIUM

Solar Terrestrial Physics: Present and Future

[ NASA-RP-11201 p 200 N84-34332

Ninteenth International Cosmic Ray Conference SH

sessions, volume 4

[NASA-CP-2376-VOL-41 p 210 N85-34729

INTERPLANETARY SPACECRAFT

The Saturn System

[NASA-CP-2068} p 205 N79-16758

Pioneer: First to Jupiter, Saturn, and beyond

[NASA-SP-446) p 206 N81-15925

Far travelers: The exptonng machines

[NASA-SP-480J p 63 N55-33126

INTERPROCESSOR COMMUNICATION

Joint University Program for Air Transportation

Research, 1981

INASA-CP-2224J p 3 N82-26199

INTERSECTIONS

Intersection of three-dimensional geometric surfaces

[NASA-TP-2454} p 177 N85-31839

INTERSTELLAR GAS

The structure and content of the galaxy and galactic

gamma rays

[NASA-CP-O02] p 199 N77-20977

INTERSTELLAR MATTER

Advances in Ultraviolet Astronomy: Four Years of IUE

Research

[NASA-CP-22381 p 201 N82-31163

Local Interstellar Medium {nternational Astronomical

Union Colloquium No. 81

[NASA-CP-2345) p 204 N85-15539

Future of Ultraviolet Astronomy Based on Six Years of

IUE Research

[NASA-CP-2349] p 203 N85-20961

Interrelationships among Circumsteltar, Interstellar and

Interplanetary Dust

[NASA-CP-2403] p 201 N86-23493

INVERSIONS

Inversion Methods in Atmospheric Remote Sounding

[NASA-CP-004] p 151 N78-12586

INVESTIGATION

Skylab EREP investigations summary

[ NASA-SP-399] p 136 N79-17279

INVISGID FLOW

inviscid, nonadiabatic flow fields over blunt, sonic corner

bodies for outer planet entry conditions by a method of

integral relations

[NASA-TP-11331 p 104 N78-18353

Solution of axisymmetric and two-dimensional inviscid

flow over blunt bodies by the method of lines

[NASA-TP-1154] p 105 N78-22332

Application of a numerically generated orthogonal

coordinate system to the solution of inviscid axisymmetric

supersonic flow over blunt bodies

[NASA-TP-t619] p 14 N50-19031

Viscous-inviscid calculations of jet entrainment effects

on the subsonic flow over nozzte afterbodies

[NASA-TP-1626] p 14 N80-22261

Surrogate-equation technique for simulation of steady

inviscid flow

[NASA-TP-18661 p 18 N81-31129

Calculation of inviscld flow over shuttle-like vehicles at

high angles of attack and comparisons with experimental

data

[NASA-TP-2103] p 110 N83-24808

Viscous-inviscid interaction method including wake

effects for three-dimensional wing-body configurations

( NASA-TP-1910 ] p24 N84-27682

A comparative study of the nonuniqueness problem of

the potential equation

[NASA-TP-2385] p 25 N85-15694

IODINE

Disposal of radioactive iodine in space

[NASA-TP-1313] p t72 N78-31740

IODINE LASERS

Solar-simulator-pumped atomic iodine laser kinetics

[NASA-TP-2182] p 118 N83-32044

Threshold kinetics of a solar-simulator-pumped iodine

laser

[NASA-TP-224tJ p 118 N84-17575

ION BEAMS

Nitriding of titanium and titanium: 8 percent aluminum.

1 percent molybdenum, I percent vanadium alloy with an

ion-beam source

[NASA-TP-21491 p 89 N83-24640

ION DENSITY (CONCENTRATION)

Harmonic well matter densities and Pauli correlation

effects in heavy-ion collisions

[NASA-TP-2003I p 192 N82-23003

ION DISTRIBUTION

Significant initial results from the enwronmental

measurements experiment on ATS-6

[ NASA-TP-1101 } p65 N78-15142

ION EXCHANGE MEMBRANE ELECTROLYTES

Three methods for in situ cross-linking of polyvinyl

alcohol films for application as ion-conducting membranes

in potassium hydroxide electrolyte --- battery separators

INASA-TP-1407] p 78 N79-21128

ION IMPLANTATION

A feasibility study of ion implantation techniques for mass

spectrometer calibration

INASA-TP-1185] p 114 N78-21431

Friction wear and auger analysis of iron implanted with

1 5-MeV nitrogen ions

[NASA-TP-1989] p 88 N82-21300

ION PLATING

Friction and hardness of gold films deposited by ion

plating and evaporation

[NASA-TP-2207] p 89 N83-34019

ION TEMPERATURE

Effect of anode-cathode geometry on performance of

the HIP-1 hot ion plasma --- magnetic mirrors

[NASA-TP-1201 ] p 194 N78-21922

IONIC COLLISIONS

Harmonic well matter densities and Pauli correlation

effects in heavy-ion collisions

[NASA-TP-2003] p 192 N82-23003

IONIC MOBILITY

Ion confinement and transport in a toroidai plasma with

externally imposed radial electric fields

[NASA-TP-14111 p 195 N79-19867

IONIZING RADIATION

Experimental study of cluster formation in binary mixture

of H20 and H2SO4 vapors in the presence of an ionizing

radiation source

[NASA-TP-17351 p 149 N81-11565

IONS

Calculation of composition distribution of ultrafine

ion-H20-H2SO4 clusters using a modified binary ion

nucleation theory

[NASA-TP-2031 ] p 150 N82-27867

IRON

Effect of carbon content on friction and wear of cast

irons

[NASA-TP-1052] p 85 N77-32286

Fnction and wear of selected metals and alloys in sliding

contact with AISI 440 C stainless steel in liquid methane

and in liquid natural gas

[NASA-TP-1150] p 119 N78-20512

Effects of thermomeohanical processing on strength and

toughness of iron - 12-percent-nickel - reactive metal alloys

at -196 C

[NASA-TP-1308} p 86 N78-31213

Friction end transfer of copper, silver, and gold to iron

in the presence of various adsorbed surface films

[NASA-TP-1392] p 120 N79-14386

Surface chemistry of iron sliding in air and nitrogen

lubricated with hexadecane and hexadecane containing

dibenzyl-dilsulfide

[NASA-TP-t545J p 79 N79-31346

Adhesion and friction of iron-base binary alloys in contact

with silicon carbide in vacuum

[NASA-TP-1604] p 87 N80-t5234

Surface chemistry and wear behavior of single-crystal

silicon carbide sliding against iron at temperatures to 1500

C in vacuum

{NASA-TP-19471 p 94 N52-19374

Friction and wear of iron in corrosive metal

I NASA-TP-19851 p88 N82-20291

Friction wear and auger analysis of iron implanted with

1.5-MeV nitrogen ions

INASA-TP-t989J p 88 N82-21300

Friction and wear of iron in sulfuric acid

INASA-TP-22891 p 59 N84-21716

IRON ALLOYS

Friction and wear characteristics of iron-chromium alloys

in contact with themselves and silicon carbide

INASA-TP-1387J p 120 N79-14387

Friction and wear with a single-crystal abrasive grit of

silicon carbide in contact with iron base binary alloys in

oil: Effects of alloying element and its content

[NASA-TP-1394] p 120 N79-17227

Friction and wear of iron-base binary alloys in sliding

contact with silicon carbide in vacuum

[NASA-TP-16121 p 93 N80-22494

Analysis of thermoelectric properlies of

high-temperature complex alloys of nickel-base, iron-base

and cobalt-base groups

(NASA-TP-2278] p 89 N84-18370

Erosion of iron-chromium alloys by glass particles

[NASA-TP-2354) p 90 N84-28965

Effects of chromium and aluminum on mechanical end

oxidation properties of iron-nickel-base superalloys based

on CG-27

[NASA-TP-2443] p 90 N85-21323

IRRADIANCE

User's guide for the Solar Backscattered Ultraviolet

(SBUV) and the Total Ozone Mapping Spectrometer

(TOMS) RUT-S end RUT-T data sets: October 31, 1978

to November 1, 1980

(NASA-RP-t1121 p 165 N83-28828

Solar Irradiance Variations on Active Region Time

Scales

JNASA-CP-2310] p 209 N84-27635

IRRADIATION

Evaluation of materials for high performance solar

arrays

JNASA-TP-1220] p 92 N78-22233

Effect of sterilization irradiation on friction and wear of

utt rahigh-molecular-weight polyethylene

[NASA-TP.1462] p 92 N79-23216

ISOTHERMAL PROCESSES

Effect of geometry on hydrodynamic film thickness

[ NASA-TP-1287 ] p 119 N78-30585

Low-pressure performance of annular, high-pressure (40

atm) high-temperature (2480 K) combustion system

[NASA-TP-1713] p 47 N80-32396

Elastohydrodynamic lubrication of rectangular contacts

[NASA-TP-2111] p 123 N83-16759

ISOTOPES

Ninteenth International Cosmic Ray Conference. OG

sessions, volume 2

[NASA-CP-2376-VOL-21 p 210 N85-34006

ISOTROPIC TURBULENCE

A spatial model of wind shear and turbulence for flight

simulation

[NASA-TP-2313] p 185 N84.24044

ITERATION

Computation of transonic boattail flow with separation

{NASA-TP-t0701 p 7 N78-13017

ITERATIVE SOLUTION

Surrogate-equation technique for simulation of steady

inviscid flow

[NASA-TP-1866] p 18 N81-31129

Solution of the symmetric eigenproblem AX=lambde

BX by delayed division

[NASA-TP-2514] p 135 N86.20857

Solution of elliptic partial differential equations by fast

Poisson solvers using a local relaxation factor, 1 : One*step

method

INASA-TP-2529] p 183 N86-28861

IUE

The Universe at Ultraviolet Wavelengths: The first two

years of International Ultraviolet Explorer

[ NASA-CP-2171 ] p 203 N81-25893

Advances in Ultraviolet Astronomy: Four Years of IUE

Research

[NASA-CP-2238] p 201 N82-31163

Future of Ultraviolet Astronomy Based on Six Years of

IUE Research

[NASA-CP-2349J p 203 N85-20961

international Ultraviolet Explorer Atlas of O-typespectra

from 1200 to 1900 angstrom

[ NASA-RP-1155] p 204 N86-25307

J

JET AIRCRAFT

Jet aircraft hydrocarbon fuels technology

[ NASA-CP-2033 ] p 97 N78-19325

Effect of winglets on a first-generation iet transport wing.

5: Stability characteristics of a full-span wing with a

generalized fuselage at high subsonic speeds

I NASA-TP-t 163] p 8 N78-20081

Minimum-fuel. 3-dimensional flightpath guidance of

transfer jets

[NASA-TP-2326 j p 58 N84-32394

A-67
JET AIRCRAFT NOISE SUBJECT INDEX

Installation effects of long-duct pylon-mounted nacelles

on a twm-iet transport model with swept supercritical

wing

INASA'TP'2457] p 27 N86-20346

JET AIRCRAFT NOISE

A companson Of the noise produced by a small jet on

a moving vehicle with that in a free jet --- jet mixing

no_se

[NASA-TP-t3261 p 186 N79-14872

A correlation of mixing noise from coannular jets with

inverted flow profiles

[NASA-TP-1301 J p 187 N79-22849

Experimental evaluation of a spinning-mode

acoustic-treatment design concept for aircraft inlets ---

suppressJon of YF-t02 engine fan noise

[NASA-TP-16131 p 46 N80-21323

A new theory for ral_d calculation of the ground pattern

of the incident sound intensity produced by a maneuvering

jet airplane

{ NASA-TP-t7331 p 15 N80-32334

A simulator study for the development and evaluation

of operating procedures on a supersonic cruise research

transport to minimize airport-community noise

[NASA-TP-17421 p 29 N81-12043

Computer program to predict aircraft noise levels

[NASA-TP-t9131 p 188 N81-33947

Forward acoustic performance of a model turbofan

designed for a high specific flow (QF-14)

[NASA-TP-19681 p 188 N82-2t036

Aeroacoustic performance of an externally blown flap

configuration with several flap noise suppression devices

{NASA-TP-t9951 p 188 N82-24942

Airport/Community Noise

[NASA-CP-2241 J p 188 N82-3t070

Empirical source noise prediction method with

application to subsonic coaxial jet mixing noise

[NASA-TP-2084] p 189 N83-16149

Investigation of jet-installation noise sources under statLc

conditions

[NASA-TP-2181 I p 189 N83-33684

Residents' annoyance responses to aircraft noise

events

[NASA-TP-2t2t I p 189 N83-34713

Fluid shielding of high-velocity jet noise

[NASA-TP-22591 p 189 N84-15894

Effects of simulated flight on the structure and noise

of underexpanded jets

[NASA-TP-2308] p 189 N84-25422

JET CONTROL

Design and analysis of an active jet control system for

helicopter sling loads

[ NASA-TP-13971 p54 N79-t5970

JET ENGINE FUELS

Jet aircraft hydrocarbon fuels technology

( NASA-CP-2033 ] p97 N78-t 9325

Aircraft Research and Technology for Future Fuels

[NASA-CP-2146] p 47 N80-29300

Effect of hydroprocessing severity on characteristics of

let fuel from OSCO 2 and Paraho distillates

[NASA-TP-t768] p 97 N81-24283

Recent trends in aviatidn turbine fuel properties

[NASA-TP-2056] p 97 N83-11340

Assessment of Alternative Aircraft Fuels

[NASA-CP-2307] p 5t N84-23630

Combustion gas properties I-ASTM jet A fuel and dry

air

INASA-TP-2359] p 51 N85-10064

JET ENGINES

Effect of slotted casing treatment with change dn

Reynolds number index on performance ol a jet engine

[NASA-TP-1058] p 41 N77-32154

Fluctuating loads measured on an over-the-wing

supersonic )el model

[NASA-TP-t3661 p 186 N79-16641

Aircraft Electric Secondary Power

[NASA-CP-22821 p 50 N84-10055

JET EXHAUST

Lean premixed/prevaporized combustion

[NASA-CP-2016J p 84 N77-33297

Effect of s s,mulated engine jet blowing above an arrow

wing at Mech 2.0

INASA-TP-1050] p 6 N78-10030

Induced velocity field of a jet in a crossflow

INASA-TP-1087] p 105 N78-26392

Flight-measured afterbody pressure coefficients from an

airplane having twin side-by-side jet engines for Mach

numbers from 0,6 to 1.6

[NASA-TP-1549| p 13 N80-tt035

Viscous-inviscid calculations of iet entrainment effects

on the subsonic flow over nozzle afferbodies

[NASA-TP-t626] p 14 N80-22261

Investigation of the flow field surrounding circular-arc

boattail nozzles at subsonic Speeds

[ NASA-TP-1633 J p 14 N80-22262

Effects ol sidewall geometry on the installed

performance of nonaxisymmetnc convergent-divergent

exhaust nozzles

INASA-TP-t7711 p 16 N81-15976

Investigation of jet-installation norse sources under static

conditions

[NASA-TP-2181 I p 189 N83-33684

Thrust-induced effects on subsonic longitudinal

aerodynamic characteristics of a

vectored-engine-over-wing configuration

[ NASA-TP-22281 p22 N84-13163

Fluid shielding of high-velocity jet noise

[NASA-TP-2259J p 189 N84-t5894

JET FLAPS

The application of parameter estimation to flight

measurements to obtain lateral-directional stability

derivatives of an augmented jet-flap STOL airplane

INASA-TP-20331 p 57 N83-16350

JET FLOW

A comparison of the noise produced by a small jet on

a moving vehicle with that in a free jet --- jet mixing

noise

[NASA-TP-1326] p 186 N79-14872

Forced and natural convection in laminar-jet diffuston

flames --- normal-gravity, inverted-gravity and zero-gravity

flames

[NASA-TP-1841] p 109 N81-24388

JET IMPINGEMENT

Liquid iet impingement normal to a dnsk in zero gravity

INASA-TP-IOtT] p 104 N77-30413

Mean velocity, turbulence intensity, and scale in a

subsonic turbulent jet impinging normal to a large flat

plate

{NASA-TP-1037] p 104 N77-3243t

Fluctuating sudace pressure and acoustic radiation for

subsonic normal jet impingement

INASA-TP-1361 ] p 186 N79-19813

Computer program for generating input for analysis of

impingement-cooled, axial-flow turbine blade

{NASA-TP-1603] p 107 N80-t5361

Morphology of an aluminum alloy eroded by a jet of

angular particles impinging at normal incidence

[NASA-TP-2139] p 89 N83-24641

Time dependence of solid-particle impingement erosion

of an aluminum alloy

INASA-TP-2169] p 89 N83*3290B

Empirical relations for cavitation and liquid impingement

erosion processes

[NASA-TP-2339] p 90 N84-31349

JET MIXING FLOW

A comparison of the noise produced by a small jet on

a moving vehicle with thai in a free jet --- jet mixing

noise

[NASA-TP-1326] p 186 N79-14872

A correlation of mixing noise from coannular jets with

inverted flow profiles

INASA-TP-1301J p 187 N7g-22849

Empirical source noise prediction method with

application to subsonic coaxial jet mixing noise

[NASA-TP-2084] p 189 N83-16149

Modeling of space vehicle propellant mixing --- cryogenic

propellants

{NASA-TP-2t07] p 97 N83-16545

Effects of simulated flight on the structure and noise

of underexpanded jets

[NASA-TP-2308] p 189 N84-25422

JET STREAMS (METEOROLOGY)

Power spectral measurements of clear-air turbulence

to long wavelengths for altitudes up to 14,000 meters

{NASA-TP-1979] p 164 N82-24790

JET THRUST

Comparison of calculated and attitude.facility-measured

thrust and airflow of two prototype El00 turbofan

engines

[ NASA-TP- 13731 p 43 N79- t 3044

Ehght evaluation of a simplified gross thrust calculation

technique using an Pt00 turbofan engine in an F-15

airplane

[NASA-TP-1782] p 48 N8t-15000

Experimental investigation of leading-edge thrust at

supersonic speeds

[NASA-TP-2204J p 22 N83-34905

JOINTS (ANATOMY)

Modified Denavit-Hartenberg parameters for better

location of joint axis systems in robot arms

(NASA-TP-25851 p 183 N86-27963

JOINTS (JUNCTIONS)

Experimental data on single-bolt joints in quasi isotropic

graphite/polyim_de laminates

[NASA-TP-2015] p 81 N82-25325

Theoretical basis for design ol thermal-stress-lree

fasteners

lNASA-TP-2226] p 132 N84-13614

Translational control of a graphically simulated robot arm

by kinematic rate equallons that overcome elbow joint

singularity

[ NASA-TP-23761 p 181 N85-15446

JUPITER (PLANET)

Pioneer odyssey

{ NASA-SP-349] p 205 N77-28055

Voyager to Jupiter and Saturn

t NASA-SP-4201 p 205 N77-29046

Voyage to Jupiter

tNASA-SP-439j p 206 Nat-t09t0

JUPITER ATMOSPHERE

Vibrational-Rotational Spectroscopy For Planetary

Atmospheres, volume 1

INASA-CP-2223-VOL-1 J p 207 N82-25043

Galileo: Exploration of Jupiter's system

I NASA-SP-479 j p208 N86-11137

JUPITER PROBES

Jupiter probe charging study

INASA-TP-t2631 p 70 N79-15149

Pioneer: First to Jupiter, Saturn, and beyond

[ NASA-SP-4461 p206 N8t-15925

K

KALMAN FILTERS

Development and evaluation of a Kalman-lilter algorithm

for terminal area navigation using sensors of moderate

accuracy

[NASA-TP-2035] p 31 N83-29193

AESOP: An interactive computer program for thedesign

of linear quadratic regulators and Kalman filters

tNASA-TP-2221] p 181 N84-16843

KANSAS

A comparative statistical study of long-term agroclimatic

conditions alfecting the growth of US winter wheat:

Distributions of regional monthly average precipitation on

the Great Plains and the state of Maryland and the effect

of agroclimatic conditions on yield in the state of Kansas

[NASA-TP-1724I p 163 N81-22658

KERNEL FUNCTIONS

Generalization of the subsonic kernel function in the

s-plane, with applncations to flutter analysis

lNASA-TP-2292] p 23 N84-20480

KEROSENE

Full-Scale Transport controlled Impact Demonstration

[NASA-CP-2395] p 135 N86-21933

KEVLAR (TRADEMARK)

Effect of low-velocity or ballistic impact damage on the

strength of thin composite and aluminum shear panels

[NASA-TP-2441 I p 83 N85-26924

KINEMATIC EQUATIONS

Kinematic properties of the helicopter in coordinated

turns

[ NASA-TP-17731 p35 N81-22039

Kinematic control of robot with degenerate wrist

I NASA-TP-2341 j p 181 N84-28539

Translational control of a graphically simulated robot arm

by kinematic rate equations that overcome elbow joint

singutanty

[NASA-TP-23761 p 181 N85-15446

Kinematic rate control of simulated robot hand at or

near wrist singulartty

(NASA-TP-2440] p 181 N85-27575

KINEMATICS

Rolling-element bearings

[NASA-RP-tl051 p 123 N83-27214

Nonlinear equabons for dynamics of pretwisted beams

undergoing small strains and targe rotations

[NASA-TP-2470] p 134 N85-27258

KINETIC ENERGY

Application of a two-dimensional parabolic computer

program to prediction of turbulent reacting flows

{ NASA-TP-t 169 j p 105 N78-20463

Fhght evaluation of a simple tolat energy-rate system

with potential wind-shear application

[NASA-TP-1854] p 39 N81-24058

Analytical and experimental investigation of stator

endwall contouring in a small axia;-flow turbine. 1: Stator

performance

(NASA-TP-2023J p 49 N83-11125

KINETIC FRICTION

Wear, friction, and temperature characterislics of an

aircraft tire undergoing braking and cornering

[NASA-TP-1569J p 29 N80-13013

KINETICS

Effect of concentration dependence of the diffusion

coefficient on homogenization kinetics in mulliphase binary

alloy systems

I NASA-TP-1281 I p 87 N79-13138

Solar-simulator-pumped atomic iodine laser kinetics

INASA-TP-21821 p 118 N83-32044

A-68
SUBJECT INDEX LANDSAT 4

KIRCHHOFF LAW OF RADIATION

An experimental evaluation of the application of the

Kirchhoff formulation for sound radiation from an oscillating

airfoil

[NASA-TP-10481 p 186 N78-12801

KLYSTRONS

Three-dimensional relativistic field-electron interaction

in a multicavity high-power klystron. 1: Basic theory

[NASA-TP-1992] p 102 N82-22439

Three-dimensional relativistic field-electron interaction

in a multicavity high-power klystron. Part 2: Working

Equations

[NASA-TP-2008) p 102 N82-23397

KNUDSEN FLOW

Potytetrafiuoroethylene transfer film studied with X-ray

photoelectron spectroscopy

[NASA-TP-1728] p 93 N81.11214

KOLMOGOROFF-SMIRNOFF TEST

Simulation study of the power of the

Kolmogoroff-Smirnoff and Z tests for the exponential

distribution

[NASA-TP-131t] p 183 N78-31854

L

LAGEOS (SATELLITE)

Prelaunch testing of the laser geodynamic satellite

(LAGEOS)

{NASA-TP-t062] p 69 N7B-10200

LAKE ERIE

Coordinated aircraft and ship surveys for determining

impact o1 river inputs on great lakes waters. Remote

sensing results

[NASA-TP-1694) p 149 N80-27832

LAKE MICHIGAN

Coordinated aircraft and ship surveys for determining

impact of river inputs on great lakes waters. Remote

sensing results

[NASA-TP-1694] p 149 N80-27832

LAKE ONTARIO

Coordinated aircraft and ship surveys for determining

impact of river inputs on great lakes waters. Remote

sensing results

[NASA-TP-1694) p 149 N80-27832

LAKE SUPERIOR

Coordinated aircraft and ship surveys for determining

impact of river inputs on great lakes waters. Remote

sensing results

[NASA-TP-t694] p 149 N80-27832

LAKES

Laboratory measurements of physical, chemical, and

optical characteristics of Lake Chicot sediment waters

[NASA-TP-t941 J p 140 N82-13468

LAMINAR BOUNDARY LAYER

A theoretical investigation of forebody shapes designed

for natural laminar boundary-layer flow

[NASA-TP-1375] p 1t N79-t5903

A theoretical analysis of simulated transonic boundary

layers in cryogenic-nitrogen wind tunnels

[NASA-TP-1631 ] p 59 N80-19131

Amplified orossfiow disturbances in the laminar boundary

layer on swept wings with suction

[NASA-TP-1902] p 109 N82-11391

Natural laminar flow experiments on modern airplane

surfaces

[NASA-TP-2256} p 24 N84-26660

Aerodynamic design of the contoured wind-tunnel liner

for the NASA supercritical, laminar-flow-control,

swept-wing experiment

[NASA-TP-2335 J p 24 N84-33377

Aerothermal tests of a 12.5 percent cone at Mach 6.7

for various Reynolds numbers, angles of attack and nose

shapes --- conducted in Langley 8-foot high temperature

tunnel

[NASA-TP-2345| p 112 N85-t7322

LAMINAR FLOW

Survey and bibliography on attainment of laminar flow

control in air using pressure gradient and suction, volume

1

[NASA-RP-1035] p 107 N79-33438

Status of linear boundary-layer stability and the e to the

nth method, with emphasis on swept-wing applications

INASA-TP-1645] p 108 N80-22633

Forced and natural convection in laminar-jet diffusion

flames --- normal-gravity, inverted-gravity and zero-gravity

flames

[NASA-TP-1841 ] p t09 N81-24388

Design and experimental results for a flapped

natural-laminar-flow airfoil for general aviation

applications

{NASA-TP-1865] p 21 N83-30386

Natural laminar flow experiments on modern airplane

surfaces

[NASA-TP-22561 p 24 N84-26660

Recent modifications and calibration of the Langley

tow-turbulence pressure tunnel

[NASA-TP-2328J p 24 N84-27675

Flight-measured laminar boundary-layer transition

phenomena including stability theory analysis

I NASA-TP-24f 7 ] p25 N85-2t 118

Calibration of sonic valves for the laminar flow control,

leading-edge flight test

(NASA-TP-2423] p 26 N85-23707

Nacellepylon/wing integration on a transport model

with a natural laminar flow nacelle

[NASA-TP-2439} p 26 N85-29924

Measurement of viscosity of gaseous mixtures at

atmospheric pressure

[NASA-TP-2582] p t 17 N86-24962

LAMINAR FLOW AIRFOILS

Design and experimental results for a

natural-laminar-flow airfoil for general aviation

applications

[NASA-TP-186fl p 17 NSf-24022

Laminar Flow Control. The Research and Technology

Studies 1981

(NASA-CP-2218J p 19 N82-20149

LAMINAR HEAT TRANSFER

Effects of mass addition on blunt-body boundary-layer

transition and heat transfer

[NASA-TP-1139] p 104 N78-f6326

Calculation of laminar heating rates on

three-dimensional configurations using the axisymmetric

analogue

INASA-TP-1698] p 108 N80-33719

Laminar heat-transfer distributions on bioonics at

incidence in hypersonic-hypervelocity flows

INASA-TP-2213] p 112 N65-t6065

LAMINATES

Evaluation of a hybrid, anisotropic, multilayered,

quadrilateral finite element

INASA-TP-t236] p 127 N78-28482

Fracture toughness of boron/aluminum laminates with

various proportions of O deg and plus or minus 45 dog

[NASA-TP-1707] p 81 N81-flt15

Stress-concentration factors for finite orthotropic

laminates with a pin-loeded hole

[NASA-TP-f862] p 81 N81-24178

An improved transverse shear deformation theory for

laminated antisofropic plates

IrNASA-TP-1903} p 130 N82-f1488

Standard tests for toughened resin composites, revised

edition

[NASA-RP-1092-REV] p 82 N83-31730

Experimental and analytical investigation of the fracture

processes of boron/aluminum laminates containing

notches

[NASA-TP-21B7] p 82 N83-33956

Nonlinear Structural Analysis

[NASA-CP-22971 p 133 N84-31688

Fracture toughness of fibrous composite materials

lNASA-TP-2370J p 83 N85-t1136

Tough Composite Materials

[NASA-CP-23341 p 83 N85-12941

Evaluation of multilayer printed wiring boards by

metallographio techniques: An illustrated guide to the

preparation and inspection of plated-through hole test

coupons based on the requirements of MiI-P-55110D

[ NASA-RP-1161 I p 126 N86-26639

LAND

Eulusmap: An international land resources map utilizing

satellite imagery

{NASA-TP-1371) p 13B N79-13475

LAND USE

Proceedings of the National Conference on Energy

Resource Management. Volume 2: Applications

[E83-10336] p 142 N83-26176

Wildland inventory and resource modeling for Douglas

and Carson City Counties. Nevada, using LANDSAT and

digital terrain data

[E83-10302] p 142 N83-27293

LANDFORMS

Global Mega-Geomorphology

[NASA-CP-23121 p 137 N85-32357

LANDING

Ground-based and in-flight simulator studies of

low-speed handling characteristics of two supersonic

cruise transport concepts

I NASA-TP-t 240 J p32 N78-27111

A simulator study for the development and evaluation

of operating procedures on a supersonic cruise research

transport to minimize airport-community noise

|NASA-TP-17421 p 29 N81-12043

Ground-based and in-flight simulator studies of flight

characteristics of a twin-fuselage passenger transport

airplane during approach and landing

INASA-TP-2451 ] p 58 N85-34144

LANDING AIDS

Simulation and flight evaluation of a head-up landing

aid for general aviation

[NASA-TP-t276J p 38 N78*3t 101

LANDING GEAR

Microstructure and mechanical properties of quenched

and tempered 300M steel

INASA-TP-1288] p 127 N78-30610

Flight investigation of piloting techniques and crosswind

limitations using a research type crosswind landing gear

[NASA-TP-f423J p 12 N79-23012

Analytical investigation of the landing dynamics of a large

airplane with a load-control system in the main landing

gear

[NASA-TP-1555} p 33 NSO-f3025

Cornering characteristics of the nose-gear tire of the

space shuttle orbiter

[NASA-TP-1917] p 130 N82-10430

Planar equabons of rollout motion for an aircraft with

free or steerable landing gears

[NASA-TP-1984] p 35 N82-23244

Experimental investigation of active loads control for

aircraft landing gear

|NASA-TP-2042] p 36 N82-31321

Validation of an Active Gear, Flexible Aircraft Take-off

and Landing analysis (AGFATL)

[NASA-TP-2353] p 37 N84-32378

LANDING LOADS

Ground distance covered duhng airborne horizontal

deceleration of an airplane

[NASA-TP-1157] p 32 N78-20115

LANDING SIMULATION

Effect of image tilt of a virtual image display on simulated

transport touchdown pedorrnance

[NASA-TP-f520] p 33 N79-33189

Effects of magnification and visual accommodation on

aimpoint estimation in simulated landings with real and

virtual image displays

[NASA-TP-1635] p 171 N80-34099

Evaluation of g seat augmentation of fixed.base/moving

base simulation for transport landings under two visually

imposed runway width conditions

[NASA-TP-2135J p 36 N83-22191

LANDING SITES

Viking site selection and certdication

[NASA-SP-429] p 207 N81-25992

LANDING SPEED

Ground distance covered dunng airborne bonzontal

deceleration of an airplane

[NASA-TP-1157] p 32 N78-20115

LANDSAT SATELLITES

Procedures for gathering ground truth information for

a superwsed approach to a computer-implemented land

cover classification of LANDSAT-acquired multispectral

scanner data

[NASA-RP-1015] p 137 N78-15549

The use of LANDSAT digital data and

computer-implemented techniques for an agricultural

application

[NASA-RP-10f6J p 138 N78-21568

Discrimination of rock classes and alteration products

in southwestern Saudi Arabia with computer-enhanced

LANDSAT data

[NASA-TP-1327] p 136 N78-33499

Educator's guide for Mission to Earth: LANDSAT views

the world

[NASA-SP-360J p 138 N80-10537

The LANDSAT tutorial workbook: Basics of satellite

remote sensing

[E83-I0001] p 141 N83-10458

LANDSAT 4

LANDSAT-4 Science Investigations Summary, including

December 1983 Workshop results, volume 1

[E84-10166} p t37 N84-30359

LANDSAT-4 Science Investigations Summary, including

December 1963 Workshop results, volume 2

[E84-t0167} p 137 N84-303B0

LANDSAT-4 Science Characterization Early Results.

Volume 1: Muitispectral Scanner (MSS)

[E85-10067} p 143 N85-20496

LANDSAT-4 Science Characterization Early Results.

Volume 2, part 1: Thematic Mapper (TM)

{E85-t0068] p 143 N85-20508

LANDSAT-4 Science Characterization Early Results.

Volume 3. part 2: Thematic Mapper (TM)

[E85-100691 p 143 N85-21724

LANDSAT-4 Science Characterization Early Results

Volume 4: Applications --- agriculture, soils land use,

geology, hydrology, wetlands, water quality, biomass

identification, and snow mapping

[E85-f0070] p 143 N85-23186

LANDSAT-4 and LANDSAT-5 muftispectral scanner

coherent noise characterization and removal

lNASA-TP-2595] p 143 N86-31945

A-69
LANDSAT5 SUBJECT INDEX

LANDSAT 5

LANDSAT-4 and LANDSAT-5 multtspectrat scanner

coherent no_se characterization and removal

[NASA-TP-2595] p 143 N86-31945

LANGUAGE PROGRAMMING

INFORM: An interactive data collection and display

program with debugging capability

INASA-TP-1424] p 177 N80-16742

LAP JOINTS

A critical examination of stresses in an eIastic single

lap joint

{NASA-TP-t507J p 128 N79-31626

Effect of preforming adhetends on static and fatigue

strength Of bonded composite single-tap joints

[NASA-TP-2324] p 133 N84-26053

LARGE SPACE STRUCTURES

Large Space Systems Technology, volume 1

[NASA-CP-2035-VOL-t } p 65 N79-10078

Large Space Systems Technology, volume 2

[NASA-CP-2035-VOL-2] p 66 N79-t0097

Load concentration due to missing members in planar

faces of a large space truss

[NASA-TP-15221 p 128 N79-33500

Electron and proton absorption calculations for a

graphite/epoxy composite modei --- large space

structures

{NASA-TP-1568] p 93 N80-11226

Large Space Systems Technology. 1979 --- antenna and

space platform systems conference

{NASA-CP-2118} p 66 N80-19145

Large Space Systems/Low-Thrust Propulsion

Technology

[NASA-CP-2144} p 77 N80-31449

Decoupted control of a long flexible beam in orbit

{NASA-TP-1740} p 71 N81-13082

Large space systems technology, t 960, volume 1

{NASA-CP-2168} p 66 N81-19164

The 1980 Large space systems technology Volume

2: Base technology

INASA-CP-2168-VOL-2} p 66 N81-19196

The 15th Aerospace Mechanisms Sympostum

iNASA-CP-2181 } p 130 N81-22388

EVA assembly of large space structure element

INASA-TP-1872} p 62 N81-26160

Structural dynamics and control of large space structures

---conference

INASA-CP-2187} p 66 N81-26166

Interactive design and analysis of future large spacecraft

concepts

INASA-TP-1937J p 72 N82-14276

The m*crowave radiometer spacecraft: A design study

[NASA-RP-t0791 p 73 N82-16153

Large space systems technology, 1981 ---

conferences

INASA-CP-2215-PT-f J p 66 N82-18275

Large Space Systems Technology part 2, 1981

INASA-CP-2215-PT-2] p 66 N82-19257

The 161h Aerospace Mechanisms Symposium

NASA-CP-2221 I p 99 N82-23344

Computabonal Aspects of Heat Transfer in Structures

{NASA-CP-22161 p 109 N82-23473

Vibrabon studies of a lightweight three-sided membrane

suitable for space application

[NASA-TP-2095] p t31 N83-16785

Modeling, Analysis. and Optimization Issues for Large

Space Structures

l NASA-CP-22581 p 66 N83-18819

A mobile work station concept for mechanically aided

astronaut assembly of large space trusses

[NASA-TP-21081 p 74 N83-19806

Structural Dynamics and Control of Large Space

Structures, 1982

INASA-CP-22661 p 67 N83-22256

Large Space Antenna Systems Technology, pad 1

i NASA-CP-2269-PT-1 ] p 67 N83-26853

Large Space Antenna Systems Technology, pad 2

[NASA-CP-2269-PT-21 p 67 N83-26879

Radiometer requirements for Earth-observation systems

using large space antennas

INASA-RP-11011 p 116 N83-28410

Vibration characteristics of a deployable

controllable-geometry truss boom

INASA-TP-2160] p 132 N83-28491

STEP Experiment Requirements

INASA-CP-2294} p 67 N84-17211

Decoupled control analysis of a large flexible space

antenna with linear quadratic regulator compansons

INASA-TP-2293] p 74 N84-23675

The 18th Aerospace Mechanisms Symposium

lNASA-CP-23111 p 133 N84-25078

Regions of attraction and uihmate boundedness for

linear quadratic regulators with nonlinearities

INASA-TP 23221 p 181 N84-28538

Large Deployable Reflector Science and Technology

Workshop Volume 3: Systems and Technology

Assessment

INASA-CP-2275-VOL-3] p 202 N84-32318

Swing-arm beam erector (SABER) concept for single

astronaut assembly of space structure

[NASA-TP-2379} p 75 N85-19015

Large Space Antenna Systems Technology, 1984

INASA-CP-2368-PT-1 I p 67 N85-23813

Large Space Antenna Systems Technology, 1984

[NASA-CP-2368-PT-2] p 68 N85-23840

Submitlimeter local oscillators for spaceborne

heterodyne applications

[NASA-RP-1147] p 76 N85-30005

Space station rotational equations of motion

[NASA-TP-2511 ] p 68 N85-34148

Problems experienced and envisioned for dynamical

physical systems

[NASA-TP-2508] p 68 N86.'11215

Decoupted and iinear quadratic regulator control of a

large, flexible space antenna with an observer in the control

loop

{NASA-TP-2484] p 75 N86-'16250

Technology for large space systems: A bibliography with

indexes (supplement 14)

{NASA-SP-7046(14)] p 63 N86.28104

Application of the LQG/LTR technique to robust

controller synthesis for a large flexible apace antenna

[NASA-TP-2560] p 75 N86-30800

Effects of mode{ error on control of large flexible apace

antenna with comparisons of decoupled and linear

quadratic regulator control procedures

[NASA-TP-26041 p 75 N66-30801

LASER ANEMOMETERS

High-speed laser anemometer system for intrarotor flow

mapping in turbomachinery

{NASA-TP-16631 p 115 N82-19521

Laser anemometer measurements in an annular

cascade of core turbine vanes and comparison with

theory

I NASA-TP-20181 p 20 N82-26234

Development of a simplified optical technique for the

simultaneous measurement of particle size distribution and

velocity

{NASA-TP-21851 p 194 N83-27846

LASER ANNEALING

Space Photovoltatc Research and Technology 1980.

High Efficiency, Radiation Damage and Blanket

Technology

INASA-CP-2169J p 145 N81-17531

LASER APPLICATIONS

Laser Doppler Velocimetry Workshop

I NASA-CP-2084 ] p 117 N79-22455

First Scientific Working Group Meeting of Airborne

Doppler Lidar Wind Vetocity Measurement Program

INASA-CP-2161 I p 162 N81-10637

Oceanic Lidar

INASA-CP-2194] p 168 N81-31801

Comparative analyses of space-to-space central power

stations

I NASA-TP-1955J p66 N82-14202

Space Laser Power Transmission System Studies ---

conferences

[NASA-CP-2214 I p 117 N82-16578

A NASA high-power space-based laser research and

applications program

[NASA-SP-4641 p 118 N83-27200

LASER DOPPLER VELOCIMETERS

Correlation of laser velocimeter measurements over a

wing with results of two prediction techniques --- in the

Langley V/STOL tunnel

[NASA-TP-1168] p 105 N78-21410

A laser velocimeter flow survey above a stalled wing

INASA-TP-12661 p 10 N79-14019

Laser Doppler Velocimetry Workshop

I NASA-CP-2084 ] p 117 N79-22455

A Scanning laser-vetocimeter technique for measuring

two-dimensional wake-vortex velocity distributions ---

Langley Vortex Research Facility

{NASA-TP-1661 I p 114 N80-24594

Exploratory Meeting on Airborne Doppler Lidar Wind

Velocity Measurements

[NASA-CP-21401 p 162 N80-26999

Flow Visuahzation and Laser Vefocimetry for Wind

tunnels

l NASA-CP-22431 p 116 N82-32663

Wind Tunnel Seeding Systems for Laser Velocimeters

INASA-CP-2393] p 116 N86-11437

Performance test of laser veloclmeler system for the

Langley 16-foot transonic tunnel

I NASA-TP-2502 } p t 18 N86-16563

LASER OUTPUTS

Atmospheric effects on CO2 laser propagation

INASA-TP-13571 p 152 N79-13607

Threshold kinetics of a solar-simulator-pumped _dine

laser

{NASA-TP-2241J p 116 N84-17575

A blackbody-pumped CO2-N2 transfer laser

{NASA-TP-2347J p 118 N84-31617

LASER PROPULSION

A NASA high-power space-based laser research and

applications program

[NASA-SP-464] p 118 N83-27200

LASER PUMPING

Direct nuclear-powered lasers

[NASA-TP-2091 I p 118 N83-16738

A NASA high-power space-based laser research and

applications program

[ NASA-SP-464 ] p 118 N83-27200

Solar-simulator-pumped atomic iodine laser kinetics

[NASA-TP-2182J p 118 N83-32044

Threshold kinetics of a solar-simulator-pumped iodine

laser

[NASA-TP-2241] p 118 N84-17575

Intensity and absorbed.power distribution in a cylindrical

solar-pumped dye laser

[NASA-TP-2321 } p 118 N84-23878

A blackbody-pumped CO2-N2 transfer laser

[NASA-TP-2347] p 1t8 N84-31617

LASER RANGE FINDERS

Prelaunch testing of the laser gaodynamic satellite

(LAGEOS)

{NASA.TP.t062] p 69 N78-10200

A comparative study of optimum and suboptimum

direct-detectlon laser ranging receivers

{NASA-TP-13151 p 117 N78-31413

LASER RANGER/TRACKER

NASA ground.based and space-based laser ranging

systems

{NASA-TP-f'I49] p 113 N78-17360

LASER SPECTROSCOPY

Comparative performance of HgCdTe photodiodes for

heterodyne application

[NASA-TP-17451 p 101 N80-33683

Atmospheric solar absorption measurements in the 9

10 11 mu m region using a diode laser heterodyne

spectrometer

[ NASA-TP-1726} p t 53 N80-33998

Vibrational-Rotational Spectroscopy For Planetary

Atmospheres, volume t

{ NASA-CP-2223-VOL-1 } p 207 N82-25043

LATCHES

Release mechanism lor releasing and reattaching

experiments on the Space Shuttle

INASA-TP-1702J p 121 N80-27694

The 161h Aerospace Mechanisms Symposium

{NASA-CP-2221 } p 99 N82-23344

LATE STARS

The Origin of Nonradiative Heating/Momentum in Hot

Stars

I NASA-CP-2358 J p 200 N85-t7755

LATERAL CONTROL

Wind-tunnel investigation at Mach numbers from 1.90

to 2.86 of a canard-controlled missile with ram-air-let

spoiler roll control --- in the Langley Unitary Plan Wind

Tunnel

[NASA-TP-11241 p 7 N78-20079

An experimental wind-tunnel investigation of a

ram-air-spoiler roll-control device on a forward-control

missile at supersonic speeds

[NASA-TP-1353] p 11 N79-17809

Simulator study of conventional general aviation

instrument displays in path-following tasks with emphasis

on pilot-induced OScillations

INASA-TP-1776] p 39 N61-14997

Simulator evaluation of separation of display parameters

in path-following tasks

{NASA-TP-19151 p 39 N8t-33203

Retative control effectiveness technique with application

to airplane control coordination

{NASA-TP-24161 p 37 N85-23753

LATERAL STABILITY

Entry dynamics of space shuttle orbiter with

lateral-directional stability and control uncertainties at

supersonic and hypersonic speeds

] NASA-TP-1011 ] p70 N76-13119

Leading-edge deflection opttmization for a highly swepl

arrow wing configuration

[NASA-TP-17771 p 16 N81-14974

Expenmental and theoretical supersonic

lateral-directional stability characteristics of a simplified

wing-body configuration with a series of vertical-tail

arrangements

INASA-TP-1878] p 17 N81-29095

The applicahon of parameter estimation to flight

measurements to obtain lateral-directional stability

derivatives of an augmented iet-flap STOL airplane

[ NASA-TP-20331 p 57 N83-16350

A-70
SUBJECT INDEX

Modal analysis of a nonuniform string with end mass

and variable tension

[NASA-TP-2198) p 87 N83-32826

LA'I-£1CES (MATHEMATICS)

Adaptive identification and control of structural dynamics

systems using recursive lattice filters

[NASA-TP-2371 ] p 75 N85-31142

LAUNCH VEHICLE CONFIGURATIONS

Stages to Saturn: A technological history of the

Apollo/Saturn launch vehicles

[NASA-SP-4206] p 72 N81-29154

LAUNCH VEHICLES

Parametric study of ascent performance of a vertically

launched hydrogen-fueled single-stage reusable

transport

[NASA-TP-t045] p 65 N78-10188

Effect of propulsion system characteristics on ascent

performance of dual-fueled single-stage earth-to-orbit

transports

[NASA-TP-1115] p65 N78-13109

Near-field sonic-boom pressure signatures for the space

shuttle launch and orbiter vehicles at Mach 6

[NASA-TP-1405] p68 N79-21119

Second Symposium on Space Industrialization --- space

commercialization

[NASA-CP-2313] p63 N85-11011

LAUNCHING PADS

Characterization of soil and postlaunch pad debris from

Cape Canaveral launch complex and analysis of soil

interaction with aqueous HCI

[NASA-TP-2076] p 150 N83-12595

LAW (JURISPRUDENCE)

Second Symposium on Space Industrialization --- space

commercialization

[NASA-CP-2313] p83 N85-11011

LAY-UP

Fracture toughness of fibrous composite materials

[NASA-TP-23701 p 83 N85-11136

LEADING EDGE FLAPS

Laminar Flow Control. The Research and Technology

Studies 1981

[NASA-CP-2218] p 19 N82-20149

Experimental study of wing leading-edge devices for

improved maneuver performance of a supercritical

maneuvering fighter configuration --- Langley 7- by 10-ft

high speed tunnel tests

[NASA-TP-2125] p 21 N83-22162

Aerodynamic characteristics of a distinct wing-body

configuration at Mach 6: Experiment, theory, and the

hypersonic isolation principle

[NASA-TP-2467] p 27 N85-33107

LEADING EDGE SLATS

Low-speed aerodynamic performance of an

aspect-ratio-10 supercritical-wing transport model

equipped with a full-span slat and part-span and full-span

double.slotted flaps

[NASA-TP-1805] p 21 N83-30390

Low-speed tests of a high-aspect-ratio,

supercritical-wing transport model equipped with a high-lift

flap system in the Langley 4- by 7-meter and Ames 12-foot

pressure tunnels

[NASA-TP-2097] p 26 N85-31010

LEADING EDGE SWEEP

Supersonic wings with significant leading-edge thrust at

cruise

[NASA-TP-1632] p 14 N80-21279

LEADING EDGES

Estimation of leading-edge thrust for supersonic wings

of arbitrary planform

[NASA-TP-1270] p 9 N78-3305t

Effects of wing leading-edge flap deflections on subsonic

longitudinal aerodynamic charactenstics of a wing-fuselage

configuration with a 44 deg swept wing

lNASA-TP-1351 ] p 10 N79-13002

Aerothermal tests of a heat-pipe-cooled leading edge

at Mach 7 --- hypersonic heat transfer for space shuffle

orbiters

[NASA-TP-1320] p 195 N79-13901

Effects of wing leading-edge deflection on tow-speed

aerodynamic characfenstics of a low-aspect-ratio highly

swept arrow-wing configuration --- wind tunnel tests

[NASA-TP-1434] p 12 N79-26020

Estimation of attainable leading-edge thrust for wings

at subsonic and supersonic speeds

[NASA-TP-1500J p 12 N80-10105

Exploratory study of the effects of wing-leading-edge

modifications on the stall/spin behavior of a light general

aviation airplane

[NASA-TP-t589J p 33 N80-13026

Leading-edge deflection optimization for a highly swept

arrow wing configuration

[NASA-TP-1777] p 16 N81-14974

Design and experimental results for a

natural-laminar-flow airfod for general aviation

applications

[NASA-TP-t861 ] p 17 N81-24022

Effects of wing-leading-edge modifications on a

full*scale, low-wing general aviation airplane: Wind-tunnel

investigation of high-angle-of-attack aerodynamic

characteristics --- conducted in Langley 30- by 60-foot

tunnel

[NASA-TP-2011] p 4 N82-26217

Wind-tunnel investigation of leading-edge thrust on

arrow wings in supersonic flow

[NASA-TP-2167J p 21 N83-31577

Experimental investigation of leading-edge thrust at

supersonic speeds

[NASA-TP-2204] p 22 N83-34905

Lee-side flow over delta wings at supersonic speeds

[NASA-TP-24301 p 26 N85-29921

LEAKAGE

Compressible flow across narrow passages:

Comparison of theory and experiment for face seals

[NASA-TP-1348] p 120 N79-10424

Thermal stress anatysis of ceramic gas-path seal

components for aircraft turbines

[NASA-TP-1437] p 92 N79-21205

LEAR JET AIRCRAFT

Ozone concentration in the cabin of a Gates Learjet

measured simultaneously with atmospheric ozone

concentrations

[NASA-TP-1340] p 148 N78-33618

LEARNING THEORY

Technical communication: Perspectives for the eighties,

part 1. Proceedings of the technical communications

sessions at the 32nd Annual Meeting of the Conference

on College Composition and Communication

[NASA-CP-2203-PT-1 ] p 197 N82-14960

LEAST SQUARES METHOD

An analytical technique for approximating unsteady

aerodynamics in the time domain

[NASA-TP-1738] p t30 N81-11422

A class of nonideal solutions. 2: Application to

experimental data

INASA-TP-19301 p 186 N83-23188

Rational-spline approximation with automatic tension

adjustment

[NASA-TP-2366] p 182 N84-34204

Adaptive identification and control of structural dynamics

systems using recursive lattice filters

[NASA-TP-23711 p 75 N85-31142

LECTURES

Man's impact on the troposphere: Lectures in

tropospheric chemistry

[NASA-RP-t022] p 151 N79-10834

LENS DESIGN

Analysis and design of a refractive virtuat =mage

system

{NASA-TP-f0661 p 193 N78-12829

LENSES

Large-aperture interferometer using local reference

beam

[NASA-TP-2060] p 194 N83-13979

Optical elements formed by compressed gases:

Analysis and potential applications

[NASA-TP-25551 p 194 N86-22390

LEUKEMIAS

Design of a blood-freezing system for leukemia

research

[NASA-TP-1165} p 169 N78-18673

MBRATIONAL MOTION

Motion about the stable Iibration points in the linearized,

restricted three-body problem

I NASA-RP-1065 j p 203 Nat-11970

LIFE (DURABILITY)

The 1983 Goddard Space Plight Center Battery

Workshop

[NASA-CP-2331 j p 103 N84-33668

LIFE CYCLE COSTS

Life test of a nickel cadmium battery with a

protection/reconditioning circuit

[NASA-TP-18731 p 77 N81-24167

LIFE SCIENCES

Search for the universal ancestors

[NASA-SP-477] p 175 N85-32777

LIFE SUPPORT SYSTEMS

Human Neurological Development: Past, Present and

Future

INASA-CP-2063] p 212 N79-15887

Space resources and space settlements

[NASA-SP-428] p 62 N79-32225

Controlled Ecological Life Support System: Use of

Higher Plants

[NASA-CP-223t} p 173 N82-24834

Controlled Ecological Life Support System: Research

and Development Guidelines

[NASA-CP-22321 p 173 N82-24835

Controlled Ecological Life Support System First

Principal Investigators Meeting

[NASA-CP-22471 p 174 N83-30016

Space Station Technology, 1983

[NASA-CP-22931 p67 N84-18277

LIGHT AIRCRAFT

Controlled Ecological Life Support System. Life Support

Systems in Space Travel

I NASA-CP-2378J p 174 N85-29531

LIFT

Simulator evaluation of a flight-path-angle control system

for a transport airplane wifh direct lift control

[NASA-TP-1116) p 53 N78-20139

Approximate indicial lift function for tapered, swept wings

in incompressible flow

[NASA-TP-1241 ] p 9 N78-30054

Experimental and theoretical aerodynamic

characteristics of two hypersonic cruise aircraft concepts

at Mach numbers of 2.96. 396, and 463

[NASA-TP-1767] p 16 N81-12021

Design and experimental results for a

natural-laminar-flow airfoil for general aviation

applications

[NASA-TP-1861] p 17 N81-24022

Design analysis of a self-acting spiral-groove ring seal

for counter-rotating shafts

[NASA-TP-2142J p 50 N83-25712

Airfoil interaction with impinging vortex

[NASA-TP-2273] p 23 N84-18159

LIFT AUGMENTATION

Powered-Lift Aerodynamics and Acoustics ---

conferences

[NASA-SP-406] p 8 N78-24046

Large-scale wind-tunnel tests of inverting flaps on a

STOL utility aircraft model

[NASA-TP-1696J p 34 N80-25318

LIFT DEVICES

Analysis of preflutter and posfflutter characteristics with

motion-matched aerodynamic forces

[NASA-TP-1232] p 127 N78-28481

Compressible, unsteady lifting-surface theory for a

helicopter rotor in forward flight

[NASA-TP-2503] p 27 N86-18289

LIFT DRAG RATIO

Longitudinal aerodynamic characteristics of an elliptical

body with a horizontal tail at Mach numbers from 2.3 to

4.63

[NASA-TP-2024] p 19 N82-26232

LIFT FANS

Cold-air performance of a tip turbine designed to drive

a lift fan

[NASA.TP-11261 p 7 N78-14998

Cold-air performance of a tip turbine designed to drive

a lift fan. 3: Effect of simulated fan leakage on turbine

performance

[NASA-TP-t t09] p 7 N78-16001

Study of the application of an implicit model-following

flight controller to lift-fan VTOL aircraft

[NASA-TP-1040] p 53 N78-16063

Aerodynamic performance of 1.38-pressure-ratio,

variable-pitch fan stage

[ NASA-TP-15021 p45 N79-3t213

Aerodynamic performance of axial-flow fan stage

operated at nine inlet guide vane angles --- to be used

on vertical lift aircraft

[NASA-TP-1510] p 45 N79-31214

LIFTING REENTRY VEHICLES

Comparison of concurrent strain gage- and pressure

transducer-measured flight loads on a lifting reentry vehicle

and correlation with wind tunnel predictions

[NASA-TP-1331] p t0 N78-33053

LIFTING ROTORS

Compressible, unsteady lifting-surface theory for a

helicopter rotor in forward flight

[NASA-TP-2503] p 27 N86-18289

LIGHT (VISIBLE RADIATION)

Introduction to the theory of atmosphehc radiative

transfer

[NASA-RP-1156} p 157 N86-27839

LIGHT AIRCRAFT

Spin-tunnel investigation of the spinning characteristics

of typic, el single-engine general aviation airplane designs.

2: Low-wing model A; tail parachute diameter and canopy

distance for emergency spin recovery

[NASA-TP-1076] p 6 N78-12040

Effects of control inputs on the estimation of stability

and control parameters of a fight airplane

[NASA-TP-1043] p 53 N78-13071

Noise transmission through flat rectangular panels into

a closed cavity --- light aircraft noise

INASA-TP-1321 ] p 186 N79-14874

Determination of stability and control parameters of a

light airplane from flight data using two estimation methods

--- equation error and maximum likelihood methods

INASA-TP-t308) p It N79-20071

Light airplane crash tests at three pitch angles

[NASA-TP-t481 I p 128 N80-11505

Exploratory study of the effects of wing-leading-edge

modifications on the stall/spin behavior of a light general

aviation airplane

[NASA-TP-1589] p 33 N80-13026

A-71
LIGHT SCATTERING

Description of an experimental (hydrogen peroxide)

rocket system and its use in measuring aileron and rudder

effectiveness of a hght airplane

[NASA-TP-1647] p, 55 N80-22358

LIGHT SCATTERING

Investigation of light scattering as a technique for

detecting discrete soot particles in s luminous flame

INASA-TP-t235J p 193 N78-27906

Particle sizing by measurement of foPNard-scattered light

a! two angles

{NASA-TP-2156] p 50 N83-24509

Airborne measurements of launch vehicle effluent of

STS-2 launch on November 12, t 981 at Cape Canaveral,

Florida

fNASA-TP-22601 p 150 N84-18764

Single scattering from nonsphericai Chebyshev

particles: A compendium of calculations

[NASA-RP-1 t57j p, 194 N86-17140

LIGHT TRANSMISSION

Measurements of spectral attenuation coefficients in the

lower Chesapeake Bay

[NASA-TP-2130] p 168 N83-24133

LIGHTNING

Lightning protection of aircraft

[ NASA-RP-t008 ] p29 N78-11024

RF radiation produced by intracloud lightning

discharges

INASA-TP-t454] p 160 N79-22708

Proceedings: Workshop on the Need for Lightning

Observations from Space

INASA-CP-2095] p, 162 N79-30869

Lightning Technology: Proceedings of a technical

symposium

[NASA-CP-2128] p 161 N80-21927

Rate statistics for radio noise from lightning

INASA-TP-1665] p 161 N80-23933

Advanced aerodynamics and active controls. Selected

NASA research

{NASA-CP-2172] p 3 N81-tg00t

Lightning attachment patterns and flight conditions for

storm hazards, 1980

( NASA-TP-20871 p 30 N83-14077

NASA/MSFC FY-83 Atmosp,hehc Processes Research

Review

[NASA-CP-2281 ] p, 165 N83-33494

NASA/MSFC FY-84 Atmosphenc Processes Research

Review

{NASA-CP-23291 p 166 N84.34829

International Aerospace and Ground Conference on

Lightning and Static Electricity 1984 technical papers.

Supplement

{NASA-CP-2356] p 166 N85-16343

Statistical analysis of direct-strike lightning data (1980

to 1982)

{ NASA-TP-22521 p 167 N86-24090

LIMB DARKENING

Solar Irradience Variations on Active Region Time

Scales

[NASA-CP-2310] p 209 N84-27635

LINE SPECTRA

An emission-line survey of the Milky Way

[NASA-SP-434] p 201 N60-11966

Atlas of absorption lines from 0 to 17 900 cm(-t)

[NASA-RP-10841 p, 192 N82-15853

Vibrational-Rotational Spectroscopy for Planetary

Atmospheres, volume 2

{NASA-CP-2223-VOL-2] p 207 N82-26134

LINEAR SYSTEMS

ORACLS: A system for tinear-quadratic-Gaussian

Control taw design

{NASA-TP-1106} p 181 N78-22809

Nonlinear optimization with linear constraints using s

projection method

[NASA-TP-2086] p 184 N83-10876

A method to stabilize linear systems using e_genvalua

gradient information

INASA-TP-2479] p 181 N66-13946

LINEARITY

Effect of fuselage up,wash on the supersonic Iongitudinai

aerodynamic characteristics of 2 fighter configurations

[NASA-TP-2330] p 24 N84-27676

Oecoupled and linear quadrabc regulator control of a

large, flexible space antenna with an Observer in the control

loop

[NASA-TP-2484( p 75 N86-16250

LINEARIZATION

A microprocessor-based table lookup approach for

magnetic bearing lineerization

[NASA-TP-t838J p 101 N81-22281

LINES (GEOMETRY)

A general solution to the hidden-line problem --- to

graphically represent aerodynamic stability derivatives

[NASA-RP-tO85J p 176 N82-21907

A-72

LININGS

Performance of semi-transportation-cooled liner in

high-temperature-rise combustors

[NASA-TP-1806J p 48 N81-21077

Noise suppression characteristics of peripherally

segmented duct liners

[NASA-TP-lg04J p 188 N81-33946

Circumferentially segmented duct lines optimized for

axisymmetnc and standing wave sources --- reducing noise

from turbofan engines galerkin method acoustic

attenuation

[NASA-TP-20751 p 188 N82-34190

A method for determining ecousbc-liner admittance in

ducts with sheared flow in two-cross-sectional directions

{NASA-TP-2518] p 190 N86-13056

LIQUID ATOMIZATION

Capillary and acceleration wave breakup' of liquid jets

in _(iel-flow sirsfreams

[NASA-TP-1791] p 109 N81-16417

LIQUID CHROMATOGRAPHY

Thermal and oxidative degradation studies of formulated

C-ethers by gel-permeation chromatography

[NASA-TP-1994] p 94 N82-21332

Group-type hydrocarbon standards for

high-performance liquid chromatographic analysis of

middistillate fuels

INASA-TP-2317J p 97 N84-23774

Rapid estimation of concentration of aromatic classes

in middistiUate fuels by high-performance liquid

chromatography

{NASA-TP-24951 p 96 N85-31307

LIQUID COOLING

Effect of coolant flow ejection on aerodynamic

performance of low-aspect-ratio vanes. 2: Performance

with coolant flow ejection at temperature ratios up to 2

[NASA-TP-1057] p 6 N78-11008

Review and status of liquid-cooling technology for gas

turbines

[NASA-RP-1038) p 106 N79-22427

LIQUID FILLED SHELLS

Experimental studies of effects of tilt and structural

asymmetry on vibration characteristics of thin-wall circular

cylinders partly filled with liquid

[NASA-TP-1211 I p 127 N78-28480

Hydroelastic vibration analysis of partially liquid-filled

shells using a series representation of the liquid

irNASA-TP-1558] p 129 N80.19563

Flow in a torsionally oscillating filled cylinder

INASA-TP-21151 p, 110 N83-16674

Liquid management in low gravity using baffled rotating

containers

I NASA-TP-2263] p 11t N84-15427

LIQUID FUELS

Experimental design of an interlaboratory study for trace

metat analysis of liquid fluids --- for aerospace vehicles

[NASA-TP-2148J p 85 N83-24575

LIQUID HELIUM

Mechanics of liquid helium in a partially filled rotating

dewar in low gravity with application to Gravity Probe-B

{NASA-TP-2124] p, 110 N63-16680

LIQUID HYDROGEN

Vapor ingestion in Centaur liquid-hydrogen tank

[NASA-TP-10611 p 104 N77-33444

Liquid hydrogen as a propulsion fuel, 1945-1959

INASA-SP-4404] p 97 N79-16994

Analysis of a topping-cycle, aircraft, gas-turbine-engine

system which uses cryogenic fuel

[ NASA-TP-2294 ] p, 51 N84-21549

LIQUID INJECTION

Feasibility study of LITVC for shuttle SRB

[NASA-TP-1912] p 77 N81-33231

LIQUID METALS

Magnetohydrodynamic power generation

[NASA-TP-2331 ] p, 195 N84-25456

LIQUID NITROGEN

Depressurization and two-phase flow of water containing

high levels of dissolved nitrogen gas

[NASA-TP-1839] p 109 N81-28389

Sound speed measurements in liquid oxygen-liquid

nitrogen mixtures

[NASA-TP-2464] p 98 N85-35307

Dynamic measurement of total temperature, pressure

end velocity in the Langley O.3-meter transonic cryogenic

tunnel

[NASA-TP-2584} p 60 N86-24709

LIQUID OXYGEN

Comp,erison of analysis and experiment for self-acting

seals for liquid-oxygen turbopumps

[NASA-TP-1443] p, 120 N79-22519

Sound speed measurements in liquid oxygen-liquid

nitrogen mixtures

[NASA-TP-2464] p 98 N85-35307

LIQUID PROPELLANT ROCKET ENGINES

Stages to Saturn: A technological history of the

Apollo/Saturn launch vehicles

{NASA-SP-4206] p 72 N81-29154

SUBJECT INDEX

Sound speed measurements in liquid oxygen-liquid

nitrogen mixtures

lNASA-TP-2464] p 98 N85-35307

LIQUID ROCKET PROPELLANTS

Axial jet mixing of ethanol in cyiindncal containers during

weightlessness

INASA-TP-1487J p g7 N79-28350

Current evaluation of the tripropellant concept

[NASA-TP-2602J p 76 N86-28124

LIQUID-GAS MIXTURES

WETAIR: A computer code for calculating

thermodynamic and transport properties of air-water

mixtures

(NASA-TP-14661 p 178 N79-23688

LIQUIDS

On the tidal oscillations of the liquid core of the earth

{NASA-TP-1223} p 151 N78-21691

LITHIUM NIOBATES

Optical and holographic storage properties of F3, Cu,

and Mg-doped lithium niobate

[ NASA-TP-11441 p 193 N78-20948

LITHIUM SULFUR BATrERIES

The 1981 Goddard Space Flight Center Battery

Workshop

{NASA-CP-22171 p 102 N82-20402

Lithium/sulfur dioxide cell and battery safety

INASA-RP-lOg9] p 146 N83-14684

The 1962 Goddard Space Flight Center Battery

Workshop

[NASA-CP-2263} p 102 N83-35230

The 1983 Goddard Space Flight Center Batlery

Workshop

[NASA-CP-2331] p 103 N84-33668

LOAD DISTRIBUTION (FORCES)

A modified T-value method for selection of strain gages

for measuring loads on a low aspect ratio wing

I NASA-TP-1748] p 35 N81-12066

Rolling-element bearings

[NASA-RP-1105] p 123 N83-27214

LOAD TESTS

Loading tests of a wing structure for s hypersonic

aircraft

[NASA-TP-1596] p, 34 N80-15068

Design detail verification tests for a lightly loaded

open-corrugation graphite-epoxy cylinder

[ NASA-TP-1981 ] p 130 N82-20567

Instability in Rotating Machinery

[NASA-CP-2409J p 126 N86-301E0

LOADS (FORCES)

Geussian step-pressure loading of rigid viscoptastic

plates

INASA-TP-1123] p 127 N78-20536

Fluctuating loads measured on an over-the-wing

supersonic jet model

INASA-TP-1366] p 186 N79-16641

Load concentration due to missing members in planar

faces of a large space truss

[NASA-TP-15221 p 128 N79-33500

Dynamic behavior of a beam drag-force anemometer

[NASA-TP-1687J p, 114 N80-24595

Cold-air investigation of a 4 1/2 stage turbine with

stage-loading factor of 466 and high specific work output.

2: Stage group performance

lNASA-TP-1688} p 47 N80-25338

Method for estimating crack-extension resistance curve

from residual strength data

[NASA-TP-1753] p 129 N81-11417

Cold-air investigation of first stage of 4-1/2-stage, fan

drive turbine with average stage-loading factor of 4.66

INASA-TP-t780] p 48 N81-16050

System analysis approach to deriving design criteria

(Loads) for Space Shuttle and its payloads. Volume 2:

Typical examples

[NASA-TP-1950j p 66 N82-15106

An assessment of the capability to calculate tilting

prop,-rotor aircraft performance, loads and stability

[NASA-TP-2291 ] p 37 N84-19333

Shock response spectra variational analysis for

pyrotechnic qualification testing of flight hardware

{NASA-TP-23151 p 74 N84-23676

Application of the ONERA model of dynamic stall

{NASA-TP-23991 p 25 N85-12862

Structural integrity and Durability of Reusable Space

Propulsion Systems

I NASA-CP-2381 I p 78 N85-27941

Surface fatigue life and failure characteristics ot EX-53,

CBS 1000M, and AISI 9310 gear materials

[NASA-TP-2513] p 125 N86-12609

LOFTING

Semianalyttc modehng of aerodynamic shapes

{NASA-TP-24131 p 25 N85-21120

LOGARITHMS

Status of linear boundary-layer stability and the e to the

nth method, with emphasis on swept-wing applications

{NASA-TP-16451 p 108 N80-22633
SUBJECT INDEX LUBRICANTS

LOKI ROCKET VEHICLE

Results of the August 1977 Soviet and American

meterological rocketsonde intercompadson held at

Wallops Island, Virginia

(NASA-RP-1053] p 161 N80-16682

LONG DURATION EXPOSURE FACILITY

Long Duration Exposure Facility (LDEF). Mission 1

Experiments

{NASA-SP-473J p 67 N84-24632

LONG DURATION SPACE FLIGHT

Living aloft: Human requirements for extended

spaceflight

[NASA-SP-463] p 174 N85-32772

LONG TERM EFFECTS

Long-term hot-hardness characteristics of five

through-hardened bearing steels

{NASA-TP-1341 ] p 87 N78-33196

Large Space Antenna Systems Technology, part 1

[NASA-CP-2269-PT-lJ p 67 N83-26653

Long-term thermal aging of 2 graphite-polyimide

composite materials

{NASA-TP-2369} p 83 N85-12094

LONG WAVE RADIATION

Parameter estimation applied to Nimbus 6 wide-angle

Iongwave radiation measurements

INASA-TP-1307} p 159 N79-13644

Deconvolution and analysis of wide-angle iongwave

radiation data from Nimbus 6 Earth radiation budget

experiment for the first year

[NASA-TP-1746] p 162 N8t-13593

El Nino and outgoing Iongwave radiation: An atlas of

Nimbus-7 Earth radiation budget observations

{NASA-RP-1163] p 157 N86-29425

LONGITUDINAL CONTROL

Phugoid characteristics of a YF-12 airplane with

variable-geometry inlets obtained in flight tests at a Mach

number of 2.9

[ NASA-TP-f 1071 p52 N78-12100

Results from flight and simulator studies of a Mach 3

cruise longitudinal autopilot

[ NASA-TP-11801 p 53 N78-21160

Effects of errors on decoupled control systems

{ NASA-TP-1164 } p 53 N78-27138

Theoretical study of the effect of wind velocity gradients

on longitudinal stability and control in climbing and level

flight

INASA-TP-1332] p 54 N79-14110

Fixed-base simulation study of decoupled longitudinal

controls during approach and landing of a medium jet

transport in the presence of wind shear

[NASA-TP-1519] p 55 N79-33218

Total energy-rate feedback for automatic glide-slope

tracking during wind-shear penetration

[NASA-TP-24121 p 58 N86-23801

LONGITUDINAL STABILITY

Entry dynamics of space shuttle orbiter with longitudinal

stability and control uncertainties at supersonic and

hypersonic speeds

[NASA-TP-1084] p 70 N77-33259

Effects of deflected thrust on the longitudinal

aerodynamic characteristics of a close-coupled

wing-canard configuration --- in the Langley V/STOL

tunnel

[NASA-TP-1090J p 6 N76-13014

Longitudinal aerodynamic characteristics at Mach 0.60

to 2.66 of a fighter configuration with strut braced wing

J"NASA-TP-1102 } p 7 N78-16000

Effects of stores on longitudinal aerodynamic

characteristics of a fighter at supersonic speeds

[NASA-TP-1175} p 8 N78-22026

Simulation study of the oscillatory longitudinal motion

of an airplane at the stall

[NASA-TP-1242} p 54 N78-30141

Theoretical study of the effect of wind velocity gradients

on longitudinal stability and control in climbing and level

f,ight

{NASA-TP-1332] p 54 N79-14110

Effects of relaxed static longitudinal stability on a

single-stage-to-orbit vehicle design

[ NASA-TP-15941 p55 N80-13052

Simulator study of stall/post-stall characteristics of a

fighter airplane with relaxed longitudinal static stability ---

F-16

[NASA-TP-t538J p 55 N80-14136

Effect o! nozzle and vertical-tail variables on the

performance of a 3-surface F-15 model at transonic Mach

numbers --- Langley 16 foot transonic tunnel

INASA-TP'2043] p 20 N82-32320

An experimental and theoretical investigation of thick

wings at various sweep angles in and out of ground

effect

(NASA-TP-2066] p 20 N63-10016

LORAN C

Joint University Program for Air Transportation

Research, 1980

[NASA-CP-21761 p 3 N81-21999

Joint University Program for Air Transportation

Research, 1981

INASA-CP-2224] p 3 N82-26199

Joint University Program for Air Transportation

Research, 1982

[ NASA-CP-2285 ] p 4 N84-11099

LOSSES

Thermal analysis of a planetary transmission with

spherical roller bearings operating after complete loss of

oil

[NASA-TP-2367} p 124 N84-32824

LOUDNESS

Overall loudness of steady sounds according to theory

and experiment

IrNASA-RP-1001 ] p 171 N79-25753

LOW ASPECT RATIO

Performance of two-stage fan having low-aspect-ratio

first-stage rotor blading

[NASA-TP-1493} p 45 N79-27143

Performance of single-stage axial-flow transonic

compressor with rotor and stator aspect ratios of 1.19

and 1.26 respectively, and with design pressure ratio of

2.05

[NASA-TP-1659] p 46 N80-21325

LOW ASPECT RATIO WINGS

Effects of wing leading-edge deflection on low-speed

aerodynamic characteristics of a low-aspect-ratio highly

swept arrow-wing configuration --- wind tunnel tests

[NASA-TP-14341 p 12 N79-26020

LOW DENSITY MATERIALS

Effective thermal conductivity determination for

low-density insulating materials

[NASA-TP-1155] p 105 N78-18364

LOW DENSITY RESEARCH

Potytetrafluoroethylene transfer film studied with X-ray

photoelectron spectroscopy

[NASA-TP-1726} p 93 N81-11214

Slip-boundary equations for multicomponent

nonequilibbum airflow

[NASA-TP-2462} p 113 N86-14530

LOW FREQUENCIES

Effect of low-frequency tones and

turbulent-boundary-layer noise on annoyance

[NASA-TP-2202] p 172 N83-34579

LOW GRAVITY MANUFACTURING

Float Zone Workshop

[NASA-CP-2179] p 62 N81-19144

Avenues and incentives for commercial use of a

low-gravity environment

[ NASA-TP-19251 p 94 N81-33292

Fundamentals of Alloy Solidification Applied to Industrial

Processes

{NASA-CP-2337] p 90 N84-34569

LOW LEVEL TURBULENCE

Adding computationally efficient realism to Monte Carlo

turbulence simulation

[NASA-TP-2469J p 165 N85-26708

LOW PASS FILTERS

Stability boundaries for systems with frequency-model

feedback and complacency filter

[NASA-TP-1744] p 184 N81-10789

LANDSAT-4 and LANDSAT-5 multispectral scanner

coherent noise characterization and removal

[NASA-TP-2695} p 143 N86-31945

LOW REYNOLDS NUMBER

Aerodynamic characteristics of a distinct wing-body

configuration at Mach 6: Experiment, theory, and the

hypersonic isolation principle

[NASA-TP-2467} p 27 N85-33107

Slip-boundary equations for multicomponent

nonequilibrium airflow

[NASA-TP-2452} p 113 N66-14530

LOW SPEED

A flight evaluation of a trailing anemometer for low-speed

calibrations of airspeed systems on research aircraft

{NASA-TP-1135] p 32 N78-t8044

Low-speed aerodynamic characteristics of a

16-percent-thick variable-geometry airfoil designed for

general aviation applications

INASA-TP-13241 p 10 N79-14018

The science and technology of low speed and motorless

flight, part 1

INASA-CP-2085-PT-1} p 2 N79-23889

Science and Technology of Low Speed and Motorless

Flight. Third International Symposium

I L-12973] p 2 N79-27070

Low-speed aerodynamic performance of a

high-aspect-ratio supercrdical-wing transport model

equipped with full-span slat and part-span double-slotted

flaps

{NASA-TP-1580} p 19 N82-15015

Low-speed aerodynamic characteristics of a

17-percent-thick medium speed airfoil designed for general

aviation applications

(NASA-TP-1786J p 20 N83-16290

Failure mechanics in low-velocity impacts on thin

composite plates

[NASA-TP-2152] p 62 N83-24562

Temperature distribution in an aircraft tire at low ground

speeds

{ NASA-TP-2195 } p 132 N83-33217

Drag of two-dimensional small-amplitude symmetric and

asymmetric wavy walls in turbulent boundary layers

INASA-TP-2316] p 112 N84-25944

Low-speed performance of an axisymmetnc,

mixed-compression, supersonic inlet with auxiliary inlets

[NASA.TP-2557] p 52 N86-24694

LOW SPEED STABILITY

Ground-based and in.flight simulator studies of

low-speed handling characteristics of two supersonic

cruise transport concepts

[NASA-TP-1240] p 32 N78-27111

Effects of wing leading-edge deflection on low-speed

aerodynamic characteristics of a low-aspect-ratio highly

swept arrow-wing configuration --- wind tunnel tests

[NASA-TP-1434] p 12 N79-26020

Summary o1 low-speed longitudinal aerodynamics of two

powered close-coupled wing-canard fighter configurations

--- conducted in Langley C/STOL tunnel

[NASA-TP-1535} p 13 N80-12994

Effects of vortex flaps on the low-speed aerodynamic

characteristics of an arrow wing

{NASA-TP-1914] p 3 N82-11013

Wind-tunnel results for a modified 17-percent-thick

low-speed airfoil sect,on

{NASA-TP-t919} p 18 N82-11033

Application of the ONERA model of dynamic stall

[NASA-TP-23991 p 25 N85-12862

Low-speed stability and control wind.tunnel

investigations of effects of spanwise blowing on fighter

flight characteristics at high angles of attack --- Langely

12-ft low-speed tunnel and 30- by 60-ft tunnel

I NASA-TP-2431 I p 26 N85-23708

Low-speed tests of a high-aspect-ratio,

supercdtical-wing transport model equipped with a high-lift

flap system in the Langley 4- by 7-meter and Ames f2-foot

pressure tunnels

INASA-TP-2097] p 26 N85-31010

LOW SPEED WIND TUNNELS

Low-speed wind-tunnel parametric investigation of flight

spoilers as trailing-vortex-elleviation devices on a transport

aircraft model

{NASA-TP-1419} p 11 N79-22038

Effects of fuselage forebody geometry on low-speed

lateral-directional characteristics of twin-tail fighter model

at high angles of attack

[NASA-TP-1592] p 13 N80-13002

Recent modifications and calibration of the Langley

low-turbulence pressure tunnel

{NASA-TP-2328} p 24 N84-27675

LOW TEMPERATURE TESTS

Fracture temperature and flaw growth in nitronic 40 at

cryogenic temperatures

{ NASA-TP-2312 J p 89 N84-23750

LOW THRUST PROPULSION

Large Space Systems/Low-Thrust Propulsion

Technology

INASA-CP-2144} p 77 N80-31448

LOW TURBULENCE

Recent modifications and calibration of the Langley

low-turbulence pressure tunnel

[NASA-TP-2328] p 24 N84-27675

LOW VISIBILITY

Head-up transition behavior of pilots during simulated

low-visibility approaches

{NASA-TP-1616} p 173 N80-26039

LOW WING AIRCRAFT

Spin-tunnel investigation of the spinning characteristics

of typical single-engine general aviation sirp_ane designs.

1 Low-wing model A: Effects of tail configurations

{NASA-TP-1009} p 5 N77-33111

LUBRICANT TESTS

Evaluation and auger analysis of a

zinc-dielkyl-dithiophosphate antiwear additive in several

diester lubricants

INASA-TP-1544] p 93 N79-32359

LUBRICANTS

Effect of thermal exposure on lubricating properties of

polyimide films and potyimide-bonded graphite fluoride

films

[NASA-TP-1125] p91 N78-15277

Elastohydrodynamic lubrication of elliptical contacts for

materials of tow elastic modulus. 2: Starved

conjunction

{NASA-TP-1273] p 119 N78-28458

Lubrication and failure mechanisms of molybdenum

disulfide films. 1: Effect of atmosphere

[NASA-TP-1343} p 92 N79-13158

Lubrication and failure mechanisms of molybdenum

disulfide films. 2: Effect of substrata roughness

{NASA-TP-1379] p 92 N79-13159

A-73
LUBRICATING OILS SUBJECT INDEX

Thermal and oxidative degradation studies of formulated

C-ethers by get-permeation chromatography

{NASA-TP-lg941 p 94 N82-21332

Rolling-element fatigue life with traction fluids and

automatic transmission fluid in a high-speed rolling-contact

ng

[NASA-TP-2050] p 122 N83-13457

Mechanism of lubrication by fricresylphosphata (TCP)

[NASA-TP-2053} p 85 N83-18863

Regression analysis of traction characteristics of traction

fluids

[NASA-TP-2154] p 123 N83-24862

Comparison of predicted and experimental thermal

performance of angular-contact ball bearings

[NASAoTP-2275J p 123 N84-18654

Simulation of lubricating behavior of a thioether liquid

lubricant by an electrochemical method

{NASA-TP-2316J p 95 N84-23764

Operating characteristics of a t_eeopiece-mner-ring

large-bore roller beahng to speeds of 3 million DN

[NASA-TP-2355] p 124 N84-29226

Effect of lubricant extreme-pressure additives on surface

fatigue life of AISI 9310 spur gears

[NASA-TP-2408] p 124 N85-13234

Effect of five iubhcants on life of AISI 9310 spur gears

{NASA-TP-2419] p 116 N85-1E099

LUBRICATING OILS

Tnbology in the 80's Volume 2: Sessions 5 - 8

{NASA-CP-2300-VOL-2] p 124 N84-25047

Effect of two inner-ring oil-flow distribution schemes on

the operating characteristics of a 35 millimeter bore ball

bearing to 2.5 million DN

[NASA-TP-2404J p 124 N85-13233

LUBRICATION

Statistical model for asperity-contact time traction in

elastohydrodynamlc lubrication

[NASA-TP-1130} p 119 N78-t8429

Lubrication and failure mechanisms of graphite fluoride

films

[ NASA-TP-t 197 j p91 N78-20337

Minimum film thickness in elliptical contacts for different

regimes of fluid-film tubncation

[NASA-TP-1342] p 119 N78-33447

Auger spectroscopy analysis of lubrication with zinc

dialkyldrihtophosphate of several metal combinations in

sliding contact

[NASA-TP-1489] p 92 N79-27308

Lubricating and wear mechanisms for a hemisphere

sliding on polyimide-bended graphite fluoride film

{ NASA-TP-1524 ] p93 N79-30381

Comparison of predicted and measured

elastohydrodynamic film thickness in a 20-millimeter-bore

ball bearing

{NASA-TP-t 5421 p 121 N79-32552

Correlation of asperity contact-time fraction with

elastohydrodynamlc film thickness in a 20-millimeter-bore

ball bearing

l NASA-TP-1547 } p 121 N79-33476

Lul_ication and wear mechanisms of potyimide-bonded

graphite fluoride films subjected to tow contact stress

INASA-TP-t5841 p 93 N80-17220

Operating characteristics of high-speed, jet-lubricated

35-millimeter-bore ball bearing with a

s_ngte-oute r-la nd -guld ed cage

tNASA-TP-t6571 p 121 N80-21753

Lubrication of optimized-design tapered-roller bearings

to 2.4 million DN

INASA-TP-1714} p 121 N80-29734

Effect of cage design on characteristics of

high-speed-jet-lubricated 35-millimeter-bore ball beanng ---

turboiet engines

INASA-TP-1732J p 121 N80-33749

Performance of jet- and inner-ring-lubncatad 35

millimeter bo_e bail bearings operating to 2.5 million DN

INASA-TP-1808I p 122 N8t-19458

Frictional heating due to aspenty interaction of

elestohydrodynamtc line-contact surfaces

INASA-TP-1882} p 122 N82-25514

Elestohydrodynam¢ lubrication of rectangular contacts

INASA-TP-2t 11] pt23 N83-16759

Mechanism of lubrication by tricresylphosphate (TCP)

INASA-TP-2274} p 123 N84-18653

Surface roughness effects in elastohydrodynamic

contacts

[NASA-TP-2488] p t25 N85-32329

Mechanics of a gaseous film barrier to lubricant wetting

of etastohydrodynamically lubricated conjunctions

[NASA-TP-2500} p 125 N85-32330

Design of traction drives

[NASA-RP-t154] p 125 N86-13734

LUBRICATION SYSTEMS

Predicted and experimental performance of

jet-lubricated 120-millimeter-bore ball bearings operating

to 25 million DN

[NASA-TP-tt96] p 119 N78-20513

Comparison of predicted and experimental performance

of large-bore roller bearing operating to 3.0 million DN

[NASA-TP-1599} p 121 N80-15410

LUMINOSITY

Second Workshop on Spacecraft Glow

[NASA-CP-23911 p 201 N86-13239

LUNAR COMPOSITION

The Soviet-Amerioan Conference on Cosmochemistry

of the Moon and Planets, part 1

[NASA-SP-37O-PT-11 p 203 N78-12925

LUNAR CRATERS

NASA catalogue of lunar nomenclature

[NASA-RP*1097J p 207 N83-12031

LUNAR EVOLUTION

The Soviet-American Conference on Cosmochemistry

of the Moon and Planets, part 1

{NASA-SP-370-PT-1} p 203 N78-12925

LUNAR EXPLORATION

Lunar impact: A history of Project Ranger

[NASA-SP-4210] p 65 N78-15149

ALSEP termination report

[NASA-RP-1036] p 199 N79-22979

The Apollo spacecraft: A chronology volume 4, 21

January 1966 - 13 July 1974

[NASA-SP-4009.VOL-4} p 98 N80-20437

LUNAR GEOLOGY

Handbook of lunar materials

[NASA-RP-1057] p 206 N80-16009

LUNAR MARIA

Apollo over the moon: A view from orbit

{NASA-SP-362} p 61 N78-21174

LUNAR PHOTOGRAPHY

Apollo over the moon: A view from orbit

[NASA-SP-362J p 61 N78-21174

LUNAR PROBES

Lunar impact: A history of Proiect Ranger

INASA-SP-4210} p 65 N78*15149

LUNAR ROCKS

Lunar sample studies --- breccias basalts, and

anorthosites

[NASA-SP-418J p 204 N77-27053

The Soviet-American Conference on Cosmochemistry

of the Moon and Planets, pad 1

[NASA-SP-370-PT-1 I p 203 N78-12925

LUNAR SOIL

Summer Workshop on Near-Earth Resources

[NASA-CP-2031 } p 205 N78-16973

LUNAR SURFACE

ALSEP termination report

INASA-RP-f036J p 199 N79-22979

NASA catalogue of lunar nomenclature

I NASA-RP-10971 p207 N83-1203f

M

MACH HUMBER

Aerodynamic characteristics at Mach numbers from 0.33

to 1.20 of a wing-body design concept for a hypersonic

research airplane

I NASA-TP-t044 } p6 N78-12038

Simulated flight effects on noise characteristics of a fan

inlet with high throat Mach number

I NASA-TP-t 19g] p 42 N78-20132

Results from flight and simulator studies of a Mach 3

cruise longitudinal autoptlot

] NASA-TP-1180 j p 53 N78-21160

Wake-shock interaction at s Mach number of 6

INASA-TP-1103J p 105 N78-22331

Characteristics of Mach t0 transitional and turbulent

boundary layers

I NASA-TP-1243} p 106 N79-14328

Flight-measured afferbody pressure coefficients from an

airplane having twin side-by-side jet engines for Mach

numbers from 0.6 to 1.6

INASA-TP-15491 p 13 N80-11035

Application of supersomc linear theory and hypersonic

impact methods to three nonslender hypersonic airplane

concepts at Mach numbers from 1.10 to 2.86

[NASA-TP-1539] p 13 N80-12065

Development and flight test results of an autothrottle

control system at Mach 3 cruise

{NASA-TP-1621 ] p 56 N80-26328

A fan pressure ratio correlation in terms of Mach number

and Reynolds number for the Langley 0.3 meter transonic

cryogenic tunnel

[NASA-TP-17521 p 16 N81-10005

In-flight boundary-layer measurements on a hollow

cylinder at a Mach number of 3.0

INASA-TP-1764J p 108 N81-12361

A study of the sonic-boom characteristics of a blunt body

at a Mach number of 6

[NASA-TP-1787} p 3 N8t-13915

Descnption and calibration of the Langley unitary plan

wind tunnel

[NASA-TP-1905) p 18 N82-12035

Experimental and analytical investigation of

axisymmetric supersonic cruise nozzle geometry at Mach

numbers from 060 to 1 30

{NASA.TP-f9531 p 19 N82-14052

Effects of axisymmetric and normal air jet plumes and

solid plume on cylindrical afferbody pressure distributions

at Mach numbers from 1.65 to 250

{NASA-TP-2005] p 19 N82-22215

In-flight transition measurement on a 10 dog cone at

Math numbers from 0.5 to 2.0

[NASA-TP-1971 I p 19 N82-26227

Aeropropulsive characteristics of Mach numbers up to

2.2 of axisymmetric and nonaxisymmetric nozzles installed

on an F-18 model

{NASA'TP-2044J p 20 N82-30291

Experimental investigation of two nonaxisymmetnc

wedge nozzles at free stream Mach numbers up to 1.20

[NASA-TP-2054} p 20 N82-32322

Studies of sidewall boundary layer in the Langley 0.3

meter transomc cryogenic tunnel with and wtthout

suction

[NASA'TP-2096 J p t 10 N83-20031

Comparison of two- and three-dimensional flow

computations with laser anemometer measurements in a

transonic compressor rotor

[NASA-TP-1931] p 22 N83-32774

Free-stream noise and transition measurements on a

cone in a Mech 35 pilot tow-disturbance tunnel

[NASA-TP-2180} p 111 N83-34229

Aerodynamic charactenstics, including effect of body

shape, of a Mech 6 aircraft concept

{NASA-TP-22351 p 22 N84-13164

Correlations of supersonic boundary-layer transition on

cones including effects of large axial variations in

wind-tunnel noise

[NASA-TP-22291 p 111 N84-17534

Mach 6 flow field surveys beneath the forebody of an

airbreathing missile

I NASA-TP-2491 ] p 28 N86-23558

MACHINING

Effect of hole geometry and Eiectnc-Discharge

Machining (EDM) on airflow rates through small diameter

holes in turbine blade material

I NASA-TP-1716} p47 N81-12089

MAGNESIUM OXIDES

Effects of oxide additions and temperature on

sinterability of milled silicon nitride

{NASA-TP-16441 p 93 N80-2t532

Influence of mineral oil and additives on mierohardness

and surface chemistry of magnesium oxide (001) surface

{NASA-TP-19861 p 94 N82-20316

Effects of environment on microhardness of magnesium

oxide

[NASA-TP-2002] p 95 N82-22366

influence ot corrosive solutions on microhardness and

chemistry of magnesium oxide/001/ surfaces

[NASA-TP-204O] p 122 N82-31691

MAGNETIC AMPLIFIERS

Three*dimensional relativistic field-electron interaction

in a multicavity high-power klystron Part 2: Working

Equations

INASA-TP-20081 p 102 N82-23397

MAGNETIC CONTROL

Effects of cable geometry and aircraft attitude on the

accuracy of a magnetic leader cable system for aircraft

guidance during rollout and turnoff

INASA-TP-1978] p 31 N82-22239

MAGNETIC FIELD CONFIGURATIONS

Solar Wind Five

INASA-CP-22801 p 209 N84-13067

MAGNETIC FIELDS

Lightning protection of aircraft

I NASA-RP- 1008 _ p29 N78-11024

Design of h_gh-perveance confined-f_ow guns for

penodic-permanent-magnet-focused tubes

[NASA-TP-14851 p 101 N79-27400

Three-dimensional relativistic field-electron interaction

in a multicavity high-power ktystron. 1: Basic theory

{NASA-TP-1992i p 102 N82-22439

Magnetohydrodynamic power generation

{NASA-TP-2331 I p 195 N84-25458

Solar Terrestrial Physics: Present and Future

{ NASA-RP-1120 } p 200 N84-34332

Geopotential Research Mission (GRM)

[NASA-CP-2390] p 155 N86-12852

MAGNETIC FLUX

Analysis and simulation of a magnetic bearing

suspension system for a laboratory model annular

momentum control device

INASA-TP-1799} p 99 N81-20311

Solar Terrestrial Physics: Present and Future

[NASA-RP-112OJ p 200 N84-34332

Measurements of Solar Vector Magnetic Fields

[NASA-CP-23741 p 210 N85-29869

A-74
SUBJECT INDEX MARINE ENVIRONMENTS

MAGNETIC MIRRORS

Effect of anode-cathode geometry on performance of

the HIP-1 hot ion plasma --- magnetic mirrors

[NASA-TP-12013 p 194 N78-21922

MAGNETIC MONOPOLES

Nineteenth International Cosmic Ray Conference. HE

sessions, volume 8

[NASA-CP-2376-VOL-81 p 211 N85-36066

MAGNETIC RECOROING

Magnetic Tape Recording for the Eighties

[NASA-RP-1075] p 116 N82-29579

MAGNETIC STARS

The A-stars: Problems and perspectives. Monograph

series on nonthermal phenomena in stellar atmospheres

[NASA-SP-463] p 204 N83-32693

MAGNETIC STORAGE

A decoding procedure for the Reed-Solomon codes

[NASA-TP-1286] p 180 N78-30882

MAGNETIC STORMS

Development and design of three monitoring instruments

for spacecraft charging

{NASA-TP-1800} p 76 N81-31282

Solar Terrestrial Physics: Present and Future

[NASA-RP-1120J p 200 N84-34332

MAGNETIC SUSPENSION

Analysis and simulation of a magnetic bearing

suspension system for a laboratory model annular

momentum control device

[NASA.TP-1799] p 99 N81-20311

A microprocessor-based table lookup approach for

magnetic bearing linearization

{NASA.TP.1838] p 101 N81-22281

MAGNETIC TAPES

Friction and morphology of magnetic tapes in sliding

contact with nickel-zinc ferrite

{NASA-TP-2267} p 95 N84-16334

Water-vapor effects on friction of magnetic tape in

contact with nickel-zinc fertile

INASA-TP-2279} p 95 N84-18399

Humidity effects on adhesion of nickel-zinc ferrite in

elastic contact with magnetic tape and itself

INASA-TP-2449} p 96 N85-21359

Airborne Lidar measurements of aerosols, mixed layer

heights, and ozone during the 1980 PE PE/N EROS summer

field experiment

[NASA-RP-1143} p 150 N86-16748

MAGNETOHYDRODYNAMIC FLOW

The aerodynamics of bodies in a rarefied ionized gas

with applications 1o spacecraft environmental dynamics

{NASA-TP-1933] p 72 N82-15116

MAGNETOHYDRODYNAMIC STABILITY

Fluctuation spectra in the NASA Lewis bumpy-torus

plasma

[NASA-TP-1257] p 194 N78-26927

MAGNETOHYDRODYNAMIC TURBULENCE

Solar Wind Five

[NASA-CP-2280L p 209 N84-13067

Solar Terrestrial Physics: Present and Future

[NASA-RP-1120] p 200 N84-34332

MAGNETOHYDRODYNAMIC WAVES

Solar Terrestrial Physics: Present and Future

[NASA-RP-1120] p 200 N84-34332

MAGNETOHYDRODYNAMICS

Magnetohydrodynamic power generation

[NASA-TP-2331 ] p 195 N84-25458

Solar Terrestrial Physics: Present and Future

{NASA-RP-1120] p 200 N84-34332

MAGNETOPAUSE

Solar Terresfnal Physics: Present and Future

[NASA-RP-1120} p 200 N84-34332

MAGNETOSPHERE

The Saturn System

[NASA-CP-2068} p 205 N79-16758

Uranus and Neptune

[NASA-CP-2330] p 208 N85-11927

MAINTENANCE

Standardization. cerlification, maintenance, and

dissemination of large scale engineering software

systems

{NASA-CP-2015J p 178 N77-33876

Aircraft Engine Diagnostics

iNASA-CP-2190} p 48 N81-31196

MAN ENVIRONMENT INTERACTIONS

Proceedings of the First Annual Meteorological and

Environmental Inputs to Aviation Systems Workshop

[NASA-CP-20281 p 158 N78-19711

The stratosphere: Present and future

[NASA-RP-1049} p 161 N80-14641

MAN MACHINE SYSTEMS

Anthropometric source book. Volume 1: Anthropometry

for designers

{NASA-RP-1024] p 172 N7g-t1734

The 14th Annual Conference on Manual Control --- digital

simulation of human operator dynamics

{NASA-CP-20601 p 173 N79-f5588

Models of human operators in vision dependent tasks

I NASA-CP-21031 p 171 N7g-33838

Application of modified profile analysis to function testing

of the motion/no-motion issue in an aircraft

ground-handling simulation --- statistical analysis

procedure for man machine systems flight simulation

[NASA-TP-1540] p 33 N80-13024

Head-up transition behavior of pilots during simulated

low-visibility approaches

[NASA-TP-1618] p 173 N80-26039

Space Station Technology, 1983

[NASA-CP-2293] p 67 N84-18277

Twentieth Annual Conference on Manual Control,

volume 1

[NASA-CP-2341-VOL-I ] p 174 N85-14487

Twentieth Annual Conference on Manual Control,

volume 2

[NASA-CP-2341-VOL-2} p 174 N85-14535

Technical Workshop: Advanced Helicopter Cockpit

Design

[NASA-CP-2351] p 31 N85-14806

Space Station Workstation Technology Workshop

Report

{NASA-CP-2414J p 70 N86-23620

Baseline experiments in teleoperator control

[NASA-TP-2547] p 174 N86-26836

Twent,/-Firsf Annual Conference on Manual Control

[NASA-CP-2428] p 174 N86-32976

MANAGEMENT

Flight Training Technology for Regional/Commuter

Airline Operations: Regional Airline Association/NASA

Workshop Proceedings

INASA-CP'2348] p 30 N85-18009

Management: A bibliography for NASA Managers

[NASA-SP-7500(20)} p 196 N86-27108

MANAGEMENT INFORMATION SYSTEMS

NASA Administrative Data Base Management Systems_

1983

[NASA-CP-23041 p 198 N84-21403

NASA Administrative Data Base Management Systems,

1984

{NASA-CP-2323J p 198 N84-33266

MANAGEMENT METHODS

Managing NASA in the Apollo era

{NASA-SP-4102] p 196 N83-18551

Management: A bibliography for NASA Managers

[NASA-SP-7500(20) I p 196 N86-27108

MANAGEMENT PLANNING

Managing NASA in the Apollo era

{NASA-SP-4102} p 196 N83-18551

The management of research institutions: A look at

government laboratories

{NASA-SP-481 } p 196 N85-16665

MANAGEMENT SYSTEMS

Management system, organizational climate and

performance relationships

[NASA-TP-14171 p 196 N79-19912

MANEUVERABILITY

Precision controllability of the YF-17 airplane

I NASA-TP-1677 J p 55 N80-23327

Theory for computing the size and shape of a region

of influence associated with a maneuvenng vehicle

I NASA-TP*1648 j p 15 N80-24261

A computer technique for detailed analysis of mission

radius and maneuverability characteristics of fighter

aircraft

I NASA-TP-1837 } p 17 N81-20026

Helicopter Handling Qualities

I NASA-CP-2219J p 30 N82-23208

Experimental study of wing leading-edge devices for

improved maneuver performance of a supercritical

maneuvering fighter configuration --- Langley 7- by 10-ft

high speed tunnel tests

INASA-TP-2125} p 21 N83-22162

Effect of thrust vecloring and wing maneuver devices

on transonic aeropropulsive characteristics of a supersonic

fighter

[NASA-TP-2119] p 22 N84-10025

Aerodynamic design for improved manueverability by

use of three-dimensional transonic theory

[NASA-TP-2282] p 23 N84-18161

MANEUVERS

Translationa_ control of a graphically simulated robot arm

by kinematic rate equations that overcome elbow joint

singularity

[NASA-TP-2376] p 181 N85-15446

MANGANESE

X-ray photoelectron spectroscopy and friction studies

of nickel-zinc and manganese-zinc ferrites in contact with

metals

{NASA-TP-21631 p88 N83-23419

MANGANESE ALLOYS

Anisotropic friction and wear of single-crystal

manganese-zinc ferrite in contact with itself

[NASA-TP-1339} p 120 N79-10425

MANGANESE COMPOUNDS

Performance of alkaline battery cells used in emergency

Iocator transmitters

[NASA-TP-22771 p 103 N84-20759

MANIPULATORS

Translational control of a graphically simulated robot arm

by kinematic rate equations that overcome elbow joint

singularity

[NASA-TP-2376} p 181 N85-15446

Kinematic rate control of simulated robot hand at or

near wrist singularity

{NASA-TP-2440} p 181 N85-27575

Theoretical three-and four-axis gimbal robot wrists

[NASA-TP-2564] p 181 N86-25168

Baseline experiments in teleoperator control

[NASA-TP-2547] p 174 N86-26836

Modified Denavit-Hartenberg parameters for better

location of joint axis systems in robot arms

[NASA-TP-2585] p 183 N86-27953

MANNED ORBITAL RESEARCH LABORATORIES

Skytab, classroom in space

{ NASA-SP-401 } p 65 N77-29189

MANNED SPACE FLIGHT

The Apollo spacecraft: A chronology volume 4, 21

January 1966 - 13 July 1974

[NASA-SP-400g-VOL-4] p 96 N80.20437

Orders of magnitude: A history of NACA and NASA,

1915 - 1980

[NASA-SP-4403J p 196 N82-14955

Space Physiology and Medicine

[NASA-SP-447] p 170 N83-25349

Living aloft: Human requirements for extended

spaceflight

INASA-SP-483} p 174 N85-32772

The human factor: Biomedicine in the manned space

program to 1980

[NASA-SP-42131 p 170 N86-21097

MANNED SPACECRAFT

Chariots for Apollo: A history of manned lunar

spacecraft

[NASA-SP-42051 p 62 N79-28203

MANUAL CONTROL

The f 4th Annual Conference on Manual Control --- digital

simulation of human operator dynamics

{NASA-CP-2060] p 173 N79-15588

Flight-test evaluation of STOL control end flight director

concepts in a powered-litt aircraft flying curved

decelerating approaches

[NASA-TP-1641] p 56 N81-19131

Twentieth Annual Conference on Manual Control,

volume 1

{NASA-CP-2341-VOL-1 } p 174 N85-14487

Twentieth Annual Conference on Manual Control,

volume 2

{NASA-CP-2341-VOL-2} p 174 N85-14535

Twenty-First Annual Conference on Manual Control

[NASA-CP-2428J p 174 N86-32976

MANUALS

Programmer's manual for MMLE3, a general FORTRAN

program for maximum likelihood parameter estimation

{NASA-TP-16g0] p 176 N81-27813

MAPPING

Quantitative mapping by remote sensing of an ocean

acid-waste dump

[NASA-TP-1275] p 147 N78-33617

Sea-surface temperature and salinity mapping from

remote microwave radiometric measurements of

brightness temperature

INASA-TP-1077} p t68 N79-28863

Demonstration of wetland vegetation mapping in Florida

from computer-processed satellite and aircraft

multispectral scanner data

[NASA-TP-1553] p 139 N80-15535

User's guide for the Total-Ozone Mapping Spectrometer

(TOMS) instrument first year ozone T data set

{NASA-RP-1096] p 164 N82-28880

Description of data on the Nimbus 7 LIMS map archive

tape: Temperature and geopotential height

INASA-TP-2553] p 167 N86-25924

MAPS

Eulusmap: An international land resources map utilizing

satellite imagery

{NASA-TP-1371] p 138 N79-13475

Procedure for extraction of disparate data from maps

into computerized data bases

[NASA-RP-1048] p 177 N79-33858

Atlas of Mars: The 1:5000000 map series

{NASA-SP-438] p 206 N80-16998

Voyager 1 and 2 atlas of six Saturnian Satellites

INASA-SP-474} p 208 N84-35242

MARINE ENVIRONMENTS

Remote Sensing and Problems of the Hydrosphere

iNASA-CP-2109] p 168 N80-12718

A-75
MARINE METEOROLOGY SUBJECT INDEX

MARINE METEOROLOGY

Satellite-derived global oceamc rainfall atlas (I 973 and

1974)

INASA-SP-4101 p 157 N77-19709

The rote of satellite altimetry in climate studies

[NASA-TP-1570] p 161 N80-16676

MARINER SPACE PROBES

On Mars: Exploration of the red planet, 1958 - 1978

[ NASA-SP-42121 p 208 N84-35248

MARINER 10 SPACE PROBE

The voyage of Manner 10: Missions to Venus and

Mercury

[ NASA-SP-4241 p 6t N78-27146

Atlas of Mercury --- Mariner 10 mission

[NASA-SP-423] p 205 N78-30025

MARKETING

Significant NASA inventions available for licensing in

foreign countries

[NASA-SP-7038(08)] p 198 N86-26243

MARKING

Marking parts to aid robot vision

[NASA-TP-18191 p 176 Nat-21775

MARKOV CHAINS

Reliability bounds for fault-tolerant systems with

competing responses to component failures

[NASA-TP-2409J p 126 N85-23090

MARKOV PROCESSES

Optimal regulation m systems with stochastic time

sampling

[NASA-TP-f7431 p 184 N81-12812

MARS (PLANET)

On the habitability of Mars: An approach to planetary

ecosynthesis

[NASA-SP-414] p 175 N77-12718

Second International Colloquium on Mars: Abstracts

for a colloquium --- bibliography

[NASA-CP-2072] p 205 N79-16757

Viking orbiter views of Mars

[NASA-SP-441 ] p 200 N81-11966

On Mars: Exploration of the red planet, 1958 - 1978

[NASA-SP-4212] p 208 N84-35248

The geology ol the terrestnal planets

[ NASA-SP-469] p 200 N85-18888

Conclusion of Viking Lander Imaging Investigation:

Picture catalog of experiment data record

[NASA-RP-t137] p 208 N85-21099

MARS ATMOSPHERE

Viking 1: early results --- Mars atmosphere and surface

examinations

[ NASA-SP-408 ] p 70 N76-28296

Vibrational-Rotational Spectroscopy For Planetary

Atmospheres, volume t

[NASA-CP-2223-VOL-f ] p 207 N82-25043

MARS LANDING

Viking site select:on and certification

[NASA-SP-429| p 207 N81-25992

MARS PHOTOGRAPHS

The Martian landscape --- Viking Mars mission and

photographs

[NASA-SP-425] p 205 N79-t2984

Images of Mars: The Viking extended mission

[ NASA-SP-444 ] p 206 N80-26239

Viking orbiter views of Mars

[ NASA-SP-441 ] p 200 N81-11966

Viking lander imaging investigation dunng extended end

continuation automatic missions. Volume t: Lander f

10_cture catalog of axpenment data record

[NASA-RP-t068] p 206 N81-25012

Viking lander imaging investigation during extended and

continuation automatic missions. Volume 2: Lander 2

pccture catalog of experiment data record

[NASA-RP-1068-VOL-21 p 207 N82-t6028

A Catalog of Selected Viking Orbiter Images

[NASA-RP-1093 ] p 207 N83.25636

Conclusion of Viking Lander Imaging Investigation:

Picture catalog of expenment data record

|NASA-RP-1137] p 208 N85-21099

MARS SURFACE

The Martian landscape --- Viking Mars mission and

photographs

[NASA-SP-425] p 205 N79-12984

Atlas of Mars: The 1:5000000 map series

[NASA-SP-438J p 206 N80.t6998

Volcanic features of Hawaii A basis for comparison

with Mars

[NASA-SP-403] p 152 N80-23912

Conclusion of Viking Lander Imaging Investigation:

Fhcture catalog of axpenment data record

[NASA-RP-1137] p 208 N85-21099

MARS SURFACE SAMPLES

Viking 1 : early results *-- Mars atmosphere and surface

examinations

[NASA-SP-408] p 70 N76-28296

Orbiting quarantine facility. The Antaeus report

[ NASA.SP-454 ] p 66 N82-20225

MARSHLANDS

Literature review of organic matter transpod from

marshes

{E83-10352} p 142 N83-29750

MARYLAND

A comparative statist:cal study of long-term agroclimatic

conditions affecting the growth of US winter wheat:

Distnbutions of regional monthly average precipitation on

the Great Plains and the state of Maryland and the effect

of sgroclimatic conditions on yield in the state of Kansas

[NASA-TP-17241 p 163 N81-22658

MASS FLOW

Design and cold-air test of single-stage uncooled turbine

with high work output

[NASA-TP-1680J p 46 N80-25337

MASS FLOW RATE

Performance tests of a gas blending system based on

mess-flow controllers

[NASA-TP-1896J p 97 N81-29246

Calibration of sonic valves for the laminar flow control.

leading-edge flight test

[NASA-TP-24231 p 26 N85-23707

MASS RATIOS

Effect of oxygen-nitrogen ratio on sinterability of

Sialons

[NASA-TP-1382J p 92 N79-21204

MASS SPECTROMETERS

A small gas inlet system for orbital mass-spectrometer

calibrations

[NASA-TP-ftT0] p 114 N78-21430

A feasibility study of ion implantation techniques for mass

spectrometer calibration

INASA-TP-11851 p 114 N78-21431

MASS TRANSFER

Effects of mess addition on blunt-body boundary-layer

transition and heat transfer

INASA-TP-t139] p 104 N78-16326

Experimental and theoretical deposition rates from

salt-seeded combustion gases of a Mech 0.3 burner rig

[NASA-TP-2225] p 111 N84-19741

MATERIALS HANDLING

Design and analysis of an active jet control system for

helicopter sling loads

{NASA-TP-13971 p 54 N79-15970

Orbiting quarantine facility The Antaeus report

[NASA-SP-454 J p 66 N82-20225

MATERIALS SCIENCE

Materials processing in space: Early experiments

{ NASA-SP-443 J p62 N81-16075

Optical Information Processing for Aerospace

Applications 2

[NASA-CP-2302| p t94 N84-22402

TriboIogy in the 80's Volume 2: Sessions 5 - 8

[ NASA-CP-2300-VOL-2J p 124 N84-25047

MATHEMATICAL LOGIC

Overall loudness of steady sounds according to theory

and experiment

[NASA-RP-10Ol ] p t7t N79-25753

MATHEMATICAL MODELS

Evaluation of a laboratory test model annular momentum

control device

[NASA-TP-1142] p 98 N78-18252

Procedures for generation and reduction of linear models

of a turbofan engine

[NASA-TP-1261 } p 184 N78-30896

Development and validation of a piloted simulation of

a helicopter and external sling load

[NASA-TP-f285] p 32 N79-t4083

Simulated electronic heterodyne recording and

processing of pulsed-laser holograms

INASA-TP-1444) p 114 N79-21329

The NASA-AMES Research Center stratospheric

aerosol model, 1, Physical processes and computational

analogs

[NASA-TP-f362] p t60 N79-21721

Computer formulations of aircraft models for simulation

studies

INASA-TP-1470] p 2 N79-23008

Evaluation of a vortex model of turbulent cavity flow

--- for computing noise generation of fluid flow

INASA-TP-1505J p t87 N79-32057

A summation and inhibition model of annoyance

response to multiple community noise sources

INASA-TP-147gl p 148 N79-32744

Inclusion of unsteady aerodynamics in longitudinal

parameter estimation from flight data --- use of vortices

and mathematical models for parameterization from flight

characteristics

[NASA-TP-1536J p 13 N80-12995

Mathematical Modeling of Diverse Phenomena

JNASA-SP-437] p 182 N80-f3839

Progress in turbulence modeling for complex flow fields

mctuding effects of compressibility

JNASA-TP-1517) p 107 N80-20527

Lightning Technology: Proceedings of a technical

symposium

[NASA-CP-2128] p 161 N80-21927

CAS2D: FORTRAN program for nonrotating

blade-to-blade, steady, potential transonic cascade flows

[ NASA-TP-t7051 p 15 N80-27284

Aerothermal analysis of a wing-elevon cove with variable

leakage

INASA-TP-1703 ] p 108 N80-32692

Research in nonlinear structural and solid mechanics

[NASA-CP-2147] p 129 N80-32756

An analytical technique for approximating unsteady

aerodynamics in the time domain

[NASA-TP-1738] p 130 N81-11422

Sample data effects of high-pass filters

{NASA-TP-1797] p 35 N81-16040

Analytic model for washout of HCI(g) from dispersing

rocket exhaust clouds

INASA-TP-ta01J p 149 N81-2460f

The theory and practice of estimating the accuracy of

dynamic flight-determined coefficients

[NASA-RP-10771 p 183 N81-27865

Surrogate-equation technique for simulation of steady

inviscid flow

[NASA-TP-18661 p 18 N81-31129

An algorithm for minimum-cost set-point ordering in a

cryogenic wind tunnel

[NASA-TP-19231 p 59 N82-11090

Computational Aspects of Heat Transfer in Structures

[NASA-CP-2216} p 109 N82-23473

Computer modeling of multiple-channel input signals and

intermodulation losses caused by nonlinear traveling wave

tube amplifiers

tNASA-TP-19991 p 102 N82-25441

Establishment of a rotor model basis

{NASA-TP-20261 p 36 N82-29311

Modeling, Analysis, and Optimization Issues for Large

Space Structures

[ NASA-CP-22581 p66 N83-18819

Stochastic differential equations and turbulent

dispersion

[NASA-RP-lt031 p 110 N83-22546

Theoretical method for calculating relative joint geometry

of assembled robot arms

[NASA-TP-2155} p 182 N83-25438

Literature review of organic matter transport from

marshes

[E83-t0352_ p 142 N83-29750

Computer-Aided Geometry Modeling

[ NASA-CP-2272 J p 177 N84-22179

Finite-difference fluid dynamics computer mathematical

models for the design and interpretation of experiments

for space flight --- atmospheric general circulation

experiment, convection in a float zone, and the

Br_dgman-Stockbarger crystal growing system

I NASA-TP-2323] p 112 N84-23852

Empirical relations for cavitation and liqu_ impingement

erosion processes

[ NASA-TP-2339] p90 Na.4-3f 349

A preliminary study of numerical simulation of

thermosolutal convection of interest to crystal growth

[NASA-TP-2394] p 112 N85-13175

A critical evaluation of various turbulence models as

applied to internal fluid flows

[NASA-TP-2474J p 112 N85-25757

A formulation and analysis of combat games

[NASA-TP-2487] p 185 N85-33745

Symmetry considerations in the scattering of identical

composite bodies

NASA-TP-2548J p 193 N86-23388

Numerical modeling of physcal vapor transport in a

vertical cylindrical ampoule, with and without gravity

lNASA'TP'2620J p 96 N86-29040

Effects of model error on control of large flexible space

antenna with comparisons of decoupled and linear

quadrat¢ regulator control procedures

[NASA-TP-2604J p 75 N88-30801

MATRICES (MATHEMATICS)

DYGABCD: A program for calculating linear A, B, C,

and D matrices from a nonlinear dynamic engine

simulation

{NASA-TP-f 295 ] p43 N78-33110

M ultlgrid Methods

INASA-CP-2202| p 182 N81-33879

Vector-algebra approach tO extract Denavit-Hartenberg

parameters of assembled robot arms

{NASA-TP-219t J p 182 N83-34661

STABCAR: A program for finding charactenstic roof

systems having transcendental stability matrices

[NASA-TP-2165] p 179 N84-27461

MATRIX MATERIALS

Interface control and mechanical property imwovements

in silicon carbide/titanium composites

[NASA-TP-2066] p 81 N82-31451

Advanced Matenals Technology

[NASA-CP-2251] p 79 N83-12147

A-76
SUBJECTINDEX METALSURFACES

High Temperature Polymer Matrix Composites

[ NASA-CP-2385 ] p83 N86-11260

MATRIX THEORY

A T-matrix theory of galactic heavy-ion fragmentation

[NASA-TP-2363] p 193 N85-17690

MAXIMUM LIKELIHOOD ESTIMATES

Determination of stability and control parameters of a

light airplane from flight data using two estimation methods

--- equation error and maximum likelihood methods

[NASA-TP-13061 p 11 N7g-20071

Important factors in the maximum likelihood analysis of

flight test maneuvers

{NASA-TP-1459J p 54 N79-22113

Maximum likelihood method for estimating airplane

stability and control parameters from flight data in

frequency domain

[NASA-TP-1637] p 55 N80-24323

User's manual for MMLE3, a general FORTRAN program

for maximum likelihood parameter estimation

[NASA-TP-1563] p 176 N81-12744

Programmer's manual for MMLE3, a general FORTRAN

program for maximum likelihood parameter estimation

[NASA-TP-1690} p 176 N81-27813

The theory and practice of estimating the accuracy of

dynamic flight-determined coefficients

(NASA-RP-1077] p 183 N81-27865

An algorithm for maximum likelihood estimation using

an efficient method for approximating sensitivities

[NASA-TP-2311 ) p 58 N84-28717

Identification of dynamic systems, theory and

formulation

INASA-RP-1138] p 185 N85-19784

MEAN FREE PATH

Polytetrafluoroethylene transfer film studied with X-ray

photoelectron spectroscopy

[NASA-TP-1728] p 93 N81-11214

MEASURING INSTRUMENTS

NASA Workshop on Solar-Terrestrial Studies from a

Manned Space Station

(NASA-CP-2024] p 136 N77-3254g

Total ozone measurement: Intercomparison of

prototype New Zealand filter instrument and Dobson

spectrophotometer

[NASA-TP-12771 p 114 N78-28412

Condensation-nuclei (Aitken Particle) measurement

system used in NASA global atmospheric sampling

program

[NASA-TP-1415] p 148 N79-18479

Carbon monoxide measurement in the global

atmospheric sampling program

[NASA-TP-1526] p 148 N7g-31841

Lightning Technology: Proceedings of a technical

symposium

[NASA-CP-2128] p 161 Na0-21927

Ozone climatology series. Volume 1: Atlas of total

ozone, April 1970- December 1976

[NASA-RP-1098] p 154 N83-16992

Assessment of Techniques for Measuring Tropospheric

H sub x O sub y

[NASA-CP-2332] p 155 N85-14336

MECHANICAL DEVICES

The 12th Aerospace Mechanisms Symposium

[NASA-CP-2080] p 120 N79-21352

The 13th Aerospace Mechanisms Symposium

[NASA-CP-2081 ] p 128 N79-22539

Lubrication of machine elements

[NASA-RP-1126] p 124 N84-31640

Swing-arm beam erector (SABER) concept for single

• astronaut assembly of space structure

[NASA-TP-2379] p 75 N85-1g015

MECHANICAL DRIVES

Wind Turbine Structural Dynamics

[NASA-CP-2034J p 144 N75-t9616

Performance of a Nasvytis multiroiler traction drive

[NASA-TP-1378) p 120 N79-t3369

The rotary combustion engine: A candidate for general

aviation --- conferences

[NASA-CP-2067J p 44 N79-t5961

Traction drive performance prediction for the Johnson

and Tevaarwerk traction model

[NASA-TP-t530] p 121 N79-33475

Release mechanism for releasing and reattaching

experiments on the Space Shuttle

[NASA-TP-1702 p 121 N80-27694

Life analysis of multiroiler planetary traction drive

INASA-TP-1710 p 122 N81-20423

The 15th Aerospace Mechanisms Symposium

[NASA-CP-2181 p 130 N81-22368

Ninteenth Aerospace Mechanisms Symposium

[NASA-CP-2371 p 134 N85-33512

Design of traction drives

[NASA-RP-1154 p 125 N86-13734

Gearing

[NASA-RP-1152 p 125 N86-14612

MECHANICAL ENGINEERING

Engineering handbook on the atmospheric

environmental guidelines for use in wind turbine generator

development

(NASA-TP-1359] p 159 N79-14679

The 12th Aerospace Mechanisms Symposium

[NASA-CP-2080] p 120 N79-21352

Proceedings of the 14th Aerospace Mechanisms

Symposium

[NASA-CP-2127] p 99 N80-23495

Research in nonlinear structural and solid mechanics

[NASA-CP-2147-SUPPL] p 130 N82-11489

Space shuttle main engine controller

(NASA-TP-1932] p 178 N82-11784

MECHANICAL PROPERTIES

Mechanical behavior and fracture characteristics of

off-axis fiber composites. 2: Theory and comparisons

[NASA-TP-1082] p 79 N78-16098

Microstructure and mechanical properties of quenched

and tempered 300M steel

[NASA-TP-1288] p 127 N78-306t0

Handbook of lunar materials

[NASA-RP-1057] p 206 N80-16009

Mechanical property characterization of

Borsic/aluminum laminates at room and elevated

temperatures

[NASA-TP-1761 p 81 N8t-16130

Creep and residual mechanical properties of cast

superalloys and oxide dispersion strengthened alloys

[NASA-TP-1781 p 87 N81-19273

Static and yawed-rolling mechanical properties of two

type 7 aircraft tires

[NASA-TP-1863 p 130 N81-24471

Design and analysis of a torsion braid pendulum

displacement transducer

[NASA-TP-1840 p 115 N81-25352

Effect of Yttria additives on properties of

pressureless-sintered silicon nitride

(NASA-TP-189g p 94 N81-31366

Rotordynamic Instability Problems in High-Performance

Turbomechiner

{NASA-CP-2250 p 122 N83-15629

Overview of zirconia with respect to gas turbine

applications

[NASA-TP-2286 p 95 N84°21740

Microstructure and orientation effects on properties of

discontinuous silicon carbide/aluminum composites

[NASA-TP-2302 p 79 N84-26749

Engineering and design properties of thallium-doped

sodium iodide and selected properties of sodium-doped

cesium iodide

[NASA-RP-113t] p 99 N84-33613

Effects of chromium and aluminum on mechanical and

oxidation properties of iron-nickel-base superalloys based

on CG-27

[NASA-TP-2443] p 90 N85-21323

A mechanical property and stress corrosion evaluation

of VIM-ESR-VAR work strengthened and direCt double

aged Inconel 718 bar material

[NASA-TP-2634] p 68 N86-30753

MECHANICAL SHOCK

Recovery of pyroshock data from distorted acceleration

records

[NASA-TP-2494] p 75 N85-3t 141

MEDICAL EQUIPMENT

Design of a blood-freezing system for leukemia

research

[NASA-TP-1165] p 169 N78-18673

MELTING

The Snowmelt-Runoff Model (SRM) user's manual

[NASA-RP-1100] p 141 N83-23660

MELTS (CRYSTAL GROWTH)

Float Zone Workshop

[NASA-CP-2226] p 62 N82-26330

MEMBRANES

Vibration studies of a lightweight three-sided membrane

suitable for space application

[NASA-TP-2095] p 131 N83-16785

Structural efficiency studies of corrugated compression

panels with curved caps and beaded webs

[NASA-TP-2272] p 132 N84-18675

MERCURY (PLANET)

The voyage of Mariner 10: Missions to Venus and

Mercury

{ NASA-SP-424 ] p61 N78-27146

Atlas of Mercury --- Mariner 10 mission

{NASA-SP-423] p 205 N78-30025

The geology of the terrestrial planets

[NASA-SP-46gJ p 200 N85-18888

MERIDIONAL FLOW

Effect of rotor meridional velocity ratio on response to

inlet radial and circumferential distortion

[NASA-TP-1278] p 45 N79-28177

MEROMORFHIC FUNCTIONS

The generalized Euler-Mascheroni constants

[ NASA-TP-2264 J p 185 N84-15880

MESH

Numerical grid generation techniques ---conference

INASA-CP-2166} p 182 N81-14690

MESOSCALE PHENOMENA

NASA/MSFC FY-83 Atmospheric Processes Research

Review

INASA-CP-2281J p 165 N83-33494

NASA/MSFC FY-84 Atmospheric Processes Research

Review

[NASA-CP-2329I p 166 N84-34829

MESOSPHERE

Abstracts of papers presented at the Eleventh

International Laser Radar Conference

[NASA-CP-2228] p t 15 N82-27706

METABOLISM

NASA Space Biology Program. Eighth annual

symposium's program and abstracts

[NASA-CP-2299] p 169 N84-18829

NASA Space Biology Program: 9th Annual

Symposium

[NASA-CP-2336] p 169 N85-26054

METAL BONDING

Further industrial tests of ceramic thermal barrier

coatings

[NASA-TP-2057] p 49 N83-10045

METAL COATINGS

X-ray photoelectron spectroscopy study of

radiofrequency-sputtered refractory compound steel

interfaces

[NASA-TP-1161 ] p 91 N78-20336

METAL COMPOUNDS

Friction and wear of single-crystal and polycrystalline

maganese-zinc ferrite in contact with various metals

[NASA-TP-1059] p 91 N78-10295

Emiffance and absorptance of NASA ceramic thermal

barrier coating system --- for turbine cooling

[NASA-TP-1190] p43 N78-26148

METAL CRYSTALS

Charectenzation of erosion of metallic materials under

cavitation attack in a mineral oil

[NASA-TP-2368] p 124 N84-32825

METAL FATIGUE

Preliminary study of thermomechanical fatigue of

polycrystatline MAR-M 200

[NASA.TP-2280] p 89 N84-17350

METAL FILMS

Friction and hardness of gold films deposited by ion

plating and evaporation

[NASA-TP-2207] p 89 N83-3401g

Adhesion between polymers and evaporated gold and

nickel films

[NASA-TP-2360] p 96 N84-31379

METAL MATRIX COMPOSITES

Effects of temperature, thermal exposure, and fatigue

on an alumina/aluminum composite

[NASA-TP-1795] p 81 N81-14001

Long-term thermal degradation and alloying constituent

effects on five boron/aluminum composites

[NASA-TP-1977] p 81 N82-22317

A study of production of misibility gap alloys with

controlled structures

[NASA-TP-2144] p 195 N63-21991

Compression panel studies for supersonic cruise

vehicles

[NASA-TP-1617] p 82 N83-28099

Fabrication and evaluation of brazed titanium-clad

Borsic/aluminum compression panels

[NASA-TP-1573] p 82 N83-28100

Experimental and analytical investigation of the fracture

processes of boron/aluminum laminates containing

notches

[NASA-TP-2187] p 82 N53-33956

Microstructure and orientation effects on properties of

discontinuous silicon carbide/aluminum composites

[NASA-TP-2302} p 79 N84-2674g

METAL OXIDE SEMICONDUCTORS

Ionized dopant concentrations at the heavily doped

surface of a silicon solar cell

[NASA-TP-1347] p 195 N79-13886

The PR2D (Place, Route in 2-Dimensions) automatic

layout computer program handbook

[NASA-RP-10291 p 179 N8t-12760

METAL PROPELLANTS

Current evaluation of the tripropellant concept

{NASA-TP-26021 p 78 N86-28124

METAL SURFACES

Transfer of molybdenum disulfide to venous metals

[NASA-TP-1019J p 98 N77-30296

Friction and wear of metals with a single-crystal abrasive

grit of silicon carbide: Effect of shear strength of metal

[NASA-TP-1293J p 92 N78-30238

Friction and transfer of copper, silver, and gold to iron

in the presence of various adsorbed surface films

[NASA-TP-1392J p 120 N79-14386

A-77
METAL WORKING SUBJECT INDEX

Effects of erodant particle shape and various heat

treatments on erosion resistance of plain carbon steel

INASA-TP-17551 p 87 N81-16210

Gas turbine ceramic-coated-vane concept with

convection-cooled porous metal core

[NASA-TP-1942] p 48 N82-14090

Friction and wear of iron m corrosive metal

{ NASA-TP-19851 p 88 N82-20291

Mechanism Of fubncation by tricresylphosphate {TCP)

INASA-TP-2053} p 85 N83-18863

Friction and wear of nickel in sulfuric acid

[NASA-TP-2290} p 89 N84-21721

Empirical relations for cavitation and liquid impingement

erosion processes

[NASA-TP-2339] p 90 N84-31349

METAL WORKING

Materials processing in space: Early experiments

[NASA-SP-443} p 62 N81-16075

METAL-METAL BONDING

Tribology in the 80's Volume 1: Sessions 1 to 4

[NASA-CP-2300-VOL-1 } p 124 N84-23891

Welding, Bonding and Fastening, 1984

{NASA-CP-23871 p 79 N86-11227

METAL-WATER REACTIONS

Cavitation pitting and erosion of aluminum 6061-T6 in

mineral oil water

{NASA-TP-2146J p 123 N83-35400

METALLIC GLASSES

Friction and surface chemistry of some ferrous-base

metallic glasses

[NASA-TP.1991 ] p 88 N82-21301

Surface chemistry, microstructure and friction properties

of some ferrous-base metallic glasses at temperatures to

750 C

[NASA-TP-2006] p 68 N82-22349

Sliding induced crystallization of metallic glass

[ NASA-TP-2140 J p88 N83-21110

METALS

Measurement techniques for trace metals in coal-plant

effluents: A brief review

[NASA-RP-10471 p 148 N79-33611

Correlation of ideal and actual shear strengths of metals

with their friction properties

{NASA-TP-1891 t p 94 N81-27282

Relationship between the ideal tensile strength and the

friction properties of metals in contact with nonmetals and

themselves

INASA-TP-1883] p 94 N81-33293

Fundamentals of Alloy Solidification Applied to industrial

Processes

I NASA-CP-2337] p 90 N64-34589

Effecl of humidity on fretting wear of several pure

metals

INASA-TP-2403] p 90 N85-13006

Effect of barrier height on friction behavior of the

semiconductors silicon and gallium arsenide in contact with

pure metals

[NASA-TP-2405 ] p96 N85-13044

Monte Carlo lattice models for adsorbed polymer

conformation

[ NASA-TP-24531 p 195 N85-24961

Current evaluation of the trlpropellant concept

[NASA-TP-2602J p 78 N86-28124

METEOROID HAZARDS

Meteoroid bumper experiment on Explorer 46

[NASA-TP-18791 p 72 N81-29155

METEOROID PROTECTION

Meteoroid bumper experiment on Explorer 46

{NASA-TP-18791 p 72 N81-29155

METEOROIDS

Atmospheric entry and tragmentation of dense

meteoroids

INASA-TP-1333} p 205 N79-14978

Space Station Planetology Experiments (SSPEX)

INASA-CP-2424] p 201 N86-27136

METEOROLOGICAL BALLOONS

STRATCOM 8 Data Workshop and supplement

I NASA-CP-2043] p 136 N79-23461

METEOROLOGICAL CHARTS

Satellite-derived global oceanic rainfall atlas (1973 and

t974)

[NASA-SP-410] p 157 N77-19709

Synopbc analyses, 5-, 2-, and 0 4-millibar surfaces for

July 1974 through June 1976

[ NASA-RP-t 023 ] p 158 N76-28746

METEOROLOGICAL FLIGHT

First Scientific Working Group Meeting ot Airborne

Doppler Lidar Wind Velocity Measurement Program

INASA CP-2161 I p 162 N81-I0637

METEOROLOGICAL INSTRUMENTS

VAS demonstration: (VISSR Atmospheric Sounder)

description

INASA-RP 11511 p 166 N86-13867

METEOROLOGICAL PARAMETERS

Results of the August 1977 Soviet and American

meterological rocketsonde intercomparison held at

Wallops Island, Virginia

{NASA-RP-1053] p 161 N80-16682

Proceedings: Fourth Annual Workshop on

Meteorological and Environmental Inputs to Aviation

systems

(NASA-CP-2139] p 162 N81-14555

Comparisons between Nimbus 6 satellite and

rawinsonde soundings for several geographical areas

INASA-RP-1073} p 163 N81-16679

Cloud-encounter and particle-concentration variabilities

from GASP data

[NASA-TP-1886} p 164 N82-15677

NASA/MSFC FY-81 Atmospheric Processes Research

Review

[ NASA-CP-2204 I p 164 N82-16660

Guidelines for spaceborne microwave remote sensors

{NASA-RP-t0861 p 140 N82-19647

Meteorological satellites: Past, present, and future

{NASA-CP-2227} p 164 N82-24781

Abstracts of papers presented at the Eleventh

International Laser Radar Conference

[NASA-CP-2228] p 115 N82-27706

NASA/MSFC FY-82 atmospheric processes research

review

{NASA-CP-2259] p t65 N83-19391

Proceedings: Sixth Annual Workshop on Meteorological

and Environmental inputs to Aviation Systems

{NASA-CP-2274] p 4 N83-33827

Meteorologicat and Environmental Inputs to Aviation

Systems

I NASA-CP-2388 ] p 166 N86-11735

Compendium of meteorology scientific issues of 1950

still outstanding

[NASA-RP-1167] p 156 N86-25900

METEOROLOGICAL SATELLITES

Synoptic analyses. 5-, 2-, 1-, and 0 4-millibar surfaces

for July 1976 through June 1977

[NASA-RP-t0321 p 159 N79-19569

Meteorological satellites: Past, present, and future

[NASA-CP-2227] p 164 N62-24781

The Conception. Growlh, Accomplishments and Future

of Meteorological Satellites

[NASA-CP-2257] p 164 N63-14825

METEOROLOGICAL SERVICES

Proceedings: Fifth Annuat Workshop on Meteorological

and Environmental inputs to Aviation Systems

INASA-CP-2192] p 3 N82-21139

Meteorological and Environmental Inputs to Aviation

Systems

I NASA-CP-2388] p 166 N86-11735

METEOROLOGY

Proceedings of the 2rid Annual Workshop on

Meteorological and Environmental Inputs to Aviation

Systems

[ NASA-CP-20571 p 159 N79-17413

Proceedings, Third Annual Workshop on Meteorological

and Environmental inputs to Aviation Systems

INASA-CP-2104} p 160 N80-14633

The stratosphere: Present and future

{NASA-RP-10491 p 161 N80-14641

Goddard Laboratory for Atmospheric Science, collected

reprints 1975-1979, volume 1

[NASA-TP-1768-VOL-1 ] p 163 N81-21666

Proceedings: Fifth Annual Workshop on Meteorological

and Environmental Inpuls to Aviation Systems

{NASA-CP-2192} p 3 N82-21139

NASA/MSFC FY-83 Atmospheric Research Review

[NASA-CP-22881 p t65 N83-36587

VAS demonstration: (VISSR Atmospheric Sounder)

descnption

{NASA-RP-1151] p 166 N86-13667

Compendium of meteorology scientific issues of 1950

still outstanding

I NASA-RP-t 167 ] p 156 N86-25900

METHANE

Chtorofluoromethanes and the stratosphere

INASA-RP-1010] p 151 N77-31694

A gas filter correlation monitor for CO, CH4, and HCI

[NASA-TP-1113j p 113 N78-13408

A high-pressure premixed flat-flame burner for chemical

process studies .-- of pollutant formation in hydrocarbon

flames

{NASA-TP-13181 p 84 N79-14177

Vibrational-Rotational Spectroscopy for Planetary

Atmospheres, volume 2

{NASA-CP-2223.VOL.2] p 207 N82-26134

Ignition of mixtures of Sill sub 4, CH sub 4, O sub 2,

and Ar or N sub 2 behind reflected shock waves

I NASA-TP-2415] p 52 N85-22395

METHYL ALCOHOL

Catalytic decomposition of methanol for onboard

hydrogen generation

I NASA-TP-1247 ! p 97 N78-25236

METHYL CHLORIDE

Effect el oxygen, methyl mercaptan, and methyl chloride

on friction behavior of copper-iron contacts

INASA-TP-1309] p 86 N78-30206

METROLOGY

NASA Metrology and Calibration, 1980

[ NASA-CP-21741 p 115 N81-23432

MICROCOMPUTERS

Joint University Program for Air Transportation

Research, 1982

[ NASA-CP-22851 p 4 N84-11099

MINDS: A microcomputer interactive data system for

8086-based controllers

[NASA-TP-2378] p 179 N85-17576

MICRODENSITOMETERS

Computerized video densitometry method for rapid

analysis of infrared photographic images -- temperature

distribution across a turbine blade

[NASA-TP-1686} p 114 N80-25635

Astronomical Microdensitometry Conference

[NASA-CP-2317} p 116 N84-28020

MICROELECTRONICS

Proceedings of the 1977 NASA/ISHM Microetectronics

Conference

[NASA-CP-2027} p 101 N76-16266

Procedures for precap visual inspection

[NASAoRP-1122} p 103 N85-13156

MICROHARDNESS

Influence of mineral oil and additives on microhardness

and surface chemistry of magnesium oxide (O01) surface

INASA-TP-1986} p 94 N82-20316

Effects of environment on microhardness of magnesium

oxide

INASA-TP-2002] p 95 N82-22366

Influence of corrosive solutions on microhardness and

chemistry of magnesium oxide /001/ surfaces

[NASA-TP-2O40] p 122 N82-31691

MICROMILLIAMMETERS

Optically isolated logarithmic nanoammeter capable of

floating to 5 kilovolts

{NASA-TP-1527] p 101 N79-32467

MICROPHONES

Investigation of effects of microphone position and

orientation on near-ground noise measurements

I NASA-TP-20041 p 189 N84-10913

Location of noise sources using a phase-slope

method

(NASA-TP-2505J p 191 N66-16041

MICROPROCESSORS

Concept report: Microprocessor control of electrical

power system

I NASA-TP-1016] p 100 N77-30367

High speed lookup table approach to radiometric

calibration of multispectral image data

[NASA-TP-1741] p 76 N80-33463

Aerospace Applications of Microprocessors

INASA-CP-2158J . p 177 N81-11644

A microprocessor-based table lookup approach for

magnetic bearing linearization

[NASA-TP-1836] p 101 N81-22281

A design approach to real-time formatting of high speed

multispectral image data

[ NASA-TP-1570 ] p 178 N81-25690

Ruggedized minicomputer hardware and software

topics, 1981: Proceedings of the 4th ROLM MIL-SPEC

Computer User's Group Conference

[NASA-CP-2206j p 180 N62-14629

Joint University Program for Air Transportation

Research, 1981

I NASA-CP-2224 ] p 3 N82-26199

MICROPROGRAMMING

Aerospace Applications of Microprocessors

INASA-CP-2158] p 177 N81-11644

MICROSTRIP TRANSMISSION LINES

Analysis of rectangular microstrip antennas

[NASA-TP-2276} p 100 N84-20735

MICROSTRUCTURE

Microstructure and mechanical properties of quenched

and tempered 30OM steel

[NASA-TP-1288] p 127 N78-30610

Surface chemistry, microstructure and friction properties

of some ferrous-base metallic glasses at temperatures to

750 C

[NASA-TP-2006] p 88 N82-22349

MetallurgJcal characterization ot the lracture of several

high strength aluminum alloys

1NASA-TP-10861 p 85 N84-11230

Microstructure and orientation effects on properties of

discontinuous silicon carbidealuminum composites

INASA-TP-23021 p 79 N84-26749

MICROWAVE AMPLIFIERS

Secondary electron-emission properties ol conducting

surfaces with application to multistage depressed

collectors for microwave amplifiers

[NASA-TP- 10971 p86 N78-11230

A-78
SUBJECTINDEX MOLECULAR GASES

Seam impingement angle effects on secondary electron

emission characteristics of textured pyrolytic graphite

[NASA-TP-22851 p 95 N84-18400

Secondary electron emission characteristics of

ion-textured copper and high-purity isotropic graphite

surfaces

{NASA-TP-2342} p 95 N84-28989

Textured carbon on copper: A novel surface with

extremely low secondary electron emission

characteristics

[NASA-TP-2543} p 96 N86-15394

MICROWAVE ANTENNAS

Radiometer requirements for Earth-observation systems

using large space antennas

[NASA-RP-1101} p 116 N83-28410

MICROWAVE EMISSION

Microwave emission from polar firn

INASA-TP-1212J p 151 N78-21890

Antartic sea ice, 1973 - 1976: Satellite

passive-microwave observations

[NASA-SP-459] p 168 N84-10718

Remote Sensing of Snow and Evapotranspiration

[NASA-CP-2363] p 143 N85-23223

MICROWAVE EQUIPMENT

Sea-surface temperature and salinity mapping from

remote microwave radiometbc measurements of

brightness temperature

[NASA-TP-t077] p 168 N79-28863

MICROWAVE FREQUENCIES

Dielectric constants of soils at microwave

frequencies-2

[NASA-TP-1238] p 138 N78-23538

MICROWAVE IMAGERY

Active Microwave Users Workshop Report

iNASA-CP-2030] p 138 N78-21562

MICROWAVE LANDING SYSTEMS

Experimental determination of position-estimate

accuracy using back-azimuth signals from a microwave

landing system

[NASA-TP-1574] p 30 N80-13020

Evaluation of Microwave Landing System (MLS) effect

on the delivery performance of a fixed-path metering and

spacing system

lNASA-TP-1844] p 31 N81-29111

Helical automatic approaches of helicopters with

microwave landing systems

INASA-TP-2109] p 31 N83-18704

MICROWAVE RADIOMETERS

Preliminary results of passive microwave snow

experiment during February and March 1978

[NASA-TP-1408} p 152 N79-19519

Microwave remote sensing of snowpack properties

[NASA-CP-2153] p 139 N81-19511

The microwave radiometer spacecraft: A design study

[NASA-RP-1079] p 73 N82-16153

Development of UHF radiometer

[NASA-TP-2504] p 103 N86-20678

MICROWAVE SENSORS

Goddard Laboratory for Atmospheric Sciences,

collected reprints 1978 - 1979, volume 2

[NASA-TP-1788-VOL-2] p 163 N81-21693

Guidelines for spaceborne microwave remote sensors

[NASA-RP-1086] p 140 N82-19647

MICROWAVE TRANSMISSION

Solar Power Satellite Microwave Transmission and

Reception

[NASA-CP-2141 ] p 145 N81-16533

Satellite power system: Concept development and

evaluation program. Volume 3: Power transmission and

reception Technical summary and assessment

INASA-RP-1076] p 145 N8t-27622

Parametric study of microwave-powered high-altitude

airplane platforms designed for linear flight

[NASA-TP-19181 p 35 N82-11050

MICROWAVE TUBES

Three-axis electron-beam test facility

[NASA-TP-1836] p 101 N81-20359

MICROWAVES

Estimation of snow temperature and mean crystal radius

from remote multispectrat passive microwave

measurements

INASA-TP-1251 j p 151 N78-26677

Propagation effects handbook for satellite systems

design. A summary of propagation impairments on 10

to 100 GHz satellite links with techniques for system

design

[NASA-RP-1082(03)} p 100 N83-29491

MIDL&TITUDE ATMOSPHERE

Middle atmosphere electrodynamlcs: Report of the

workshop on the Role of the Electrodynamies of the Middle

Atmosphere on Solar Terrestrial Coupling

{NASA-CP-2090] p 152 N79-25608

MILITARY OPERATIONS

Service life evaluation of rigid explosive transfer _ines

{NASA-TP-21431 p36 N83-31596

MILITARY TECHNOLOGY

Essays on the History of Reckelry and Astronautics:

Proceedings of the Third through the Sixth History

Symposia of the International Academy of Astronautics,

volume 1

[NASA-CP-2014-VOL-1 t p 211 N77-33030

MILKY WAY GALAXY

An emission-line survey of the Milky Way

[NASA-SP-4341 p 201 N80-11966

Airborne Astronomy Symposium A symposium

commemorating the tenth anniversary of operations of the

Kuiper Airborne Observatory

[NASA-CP-2353] p 202 N85-17848

MILLIMETER WAVES

Topics in the optimization of millimeter-wave mcxers

{NASA-TP*22871 p 103 N84-20758

MINERAL OILS

Effectiveness of various organometallics as antiwear

additives in mineral oil

{NASA-TP-10961 p 91 N78-12222

Characterization of wear debris generated in accelerated

rolling-element fatigue tests

INASA-TP-12031 p 119 N78-21470

Influence of mineral oil and additives on microhardness

and surface chemistry of magnesium oxide (001) surface

[NASA-TP-1986) p 94 N82-20316

Cavitation pitting and erosion of aluminum 6061-T6 in

mineral oil water

[NASA-TP-21461 p 123 N83-35400

Characterization of erosion of metallic materials under

cavitation attack in a mineral oil

[NASA-TP-23681 p 124 N84-32825

MINES (EXCAVATIONS)

Proceedings of the National Conference on Energy

Resource Management. Volume 2: Applications

[E83-103361 p 142 N83-26176

MIRRORS

Illumination from space wilh orbiting solar-reflector

spacecraft

[NASA-TP-20651 p 74 N82-33421

MISSILE BODIES

A distributed vortex method for computing the vortex

field of a missile

[NASA-TP-lt83 ] p8 N78-25058

Investigation of flow characteristics over missile bodies

at supersonic speeds

[NASA-TP-1579] p 13 N80-13001

MISSILE CONFIGURATIONS

Wind-tunnel investigation at Mach numbers from 1.90

to 2.86 of a canard-controlled missile with ram-air-jet

spoiler roll control --- in the Langley Unitary Plan Wind

Tunnel

[NASA-TP-t 124 ] p7 N78-20079

An analytical procedure for computing smooth

transitions between two specified cross sections with

applications to blended wing body configuration

{NASA-TP-2012] p 19 N82-25193

Effect of tail-fin span on stability and control

characteristics of a Canard-controlled missile at supersonic

Mech numbers

{NASA-TP-2157] p 21 N83-27959

MISSILE CONTROL

Stability and control characteristics of a monoplanar

elliptic missile model at Mach numbers from f 60 to 2.86

INASA-TP-1352] p 11 N79-17808

MISSILE DESIGN

An analytical procedure for computing smooth

transitions between two specified cross sections with

applications to blended wing body configuration

[NASA-TP-2012J p 19 N82-25193

MISSILES

Mach 6 flow field surveys beneath the forebody of an

airbreathing missile

[NASA-TP-2491 J p 28 N86-23558

MISSION PLANNING

Asteroids: An Exploration Assessment

[NASA-CP-2053] p 205 N78-29007

Large Space Systems Technology, volume 1

[NASA-CP-2035-VOL-1 } p 65 N79-10078

The Martian landscape --- Viking Mars mission and

photographs

[NASA-SP-425] p 205 N79-12984

The Saturn System

[NASA-CP-2068] p 205 N79-16758

Chariots for Apollo: A history of manned lunar

spacecraft

[ NASA-SP-42051 p 62 N79-28203

Space resources and space settlements

[NASA-SP-428] p 62 N79-32225

Study of the Solar Cycle Irom Space

I NASA-CP-2098 } p 209 N80-17944

Viking '75 spacecraft design and test summary Volume

1: Lander design

INASA-RP 1027 VOL-1J p 71 N81-10100

A computer technique for detailed analysts of mtsslon

radius and maneuverability characteristics of fighter

aircraft

INASA-TP-1837] p 17 N81-20026

Atmospheric constraint statistics for the Space Shuttte

mission planning

[ NASA-TP-2069] p 69 N82-33417

On Mars: Exploration of the red planet, 1958 - 1978

[ NASA-SP-4212} p 208 N84-35248

Galileo: Exploration of Jupiter's system

[ NASA-SP-4791 p208 N86-11137

MIXERS

Topics in the optimization of millimeter-wave mixers

[NASA-TP-2287] p 103 N84-20758

MIXING

Axia_ jet mixing of ethanol in cylindrical containers during

weightlessness

{NASA-TP-14871 p 97 N79-28350

Performance tests of a gas blending system based on

mass-flow controllers

{NASA-TP-1896] p 97 N81-29246

Flow in a torsionally OScillating filled cylinder

{NASA-TP-2115] p 110 N83-16674

North Atlantic Deep Water Formation

{NASA-CP-23671 p 169 N85-26028

MIXING LENGTH FLOW THEORY

Three-dimensional turbulent-mixing-length modeling for

discrete-hole coolant injection into a crossflow

[NASA-TP-2200} p 1t 1 N83-34232

Hot-flow tests of a series of 10-percent-scale turbofan

forced mixing nozzles

[NASA-TP-2268} p 111 N84-17525

MIXTURES

Ignition of SiH4-H2-O2-N2 behind reflected shock

waves

{NASA-TP-2114} p 50 N83-18727

Effects of percentage of blockage and flameholder

downstream counterbores on lean combustion limits of

premixed, prevaporized propane-air mixture

[NASA-TP-2227} p 50 N83-34941

MODAL RESPONSE

Decoupled control of a long flexible beam m orbit

{NASA-TP-1740] p 71 N81-13082

Analytical study of acoustic response of a

semireverberant enclosure with application to active noise

control

{NASA-TP-2472] p 191 N86-16040

MODELS

Development of a procedure to model high-resolution

wind profiles from smoothed or low-frequency data

[NASA-TP-1071 ] p 158 N78-11642

Site selection and directional models of deserts used

for ERBE validation targets

[NASA-TP-2540} p 167 N86-23160

MODES (STANDING WAVES)

Interaction of a turbulent-jet noise source with transverse

modes in a rectangular duct

INASA-TP-1248] p 1 N78-25049

MODULATION TRANSFER FUNCTION

Spatial frequency response of an optical heterodyne

receiver

INASA-TP-1763} p 194 N81-13739

Application of information theory to the design of

line-scan imaging systems

INASA-TP-18971 p 116 N81-33452

MOISTURE

An evaluation and comparison of vertical profile data

from the VISSR Atmospheric Sounder (VAS)

[NASA-TP-2425} p 166 N85-t6351

MOISTURE CONTENT

Soil Moisture Workshop

[NASA-CP-2073} p 138 N79-16329

Moisture diffusion parameter characteristics for epoxy

composites and neat resins

[NASA-TP-14741 p 80 N79-29241

Moisture determination in composite materials using

positron iifetime techniques

[NASA-TP-1681 j p 80 N80-27428

Water vapor measurement system in global atmospheric

sampling program, appendix

{NASA-TP-2051] p 150 N83-13643

MOISTURE METERS

Soil Moisture Workshop

{NASA-CP-2073] p 138 N79-16329

MOLECULAR BIOLOGY

The cosmic history of the btogenic etements and

compounds

{ NASA-SP-476] p 175 N85-28562

MOLECULAR CLOUDS

Molecular clouds and galactic spiral slructure

{ NASA-TP.22881 p 204 N84-20457

MOLECULAR GASES

Atlas of absorption lines from 0 to 17 900 cm(-1)

INASA-RP-t084] p 192 N82-15853

A-79
MOLECULAR INTERACTIONS SUBJECT INDEX

MOLECULAR INTERACTIONS

Expenmental study of cluster formation in binary mixture

of H20 and H2SO4 vapors in the presence of an ionizing

radiation source

fNASA-TP-1735] p 149 N81-11565

MOLECULAR RELAXATION

Low-frequency sound absorption measurements an air

INASA-RP-1128} p 190 N85-11789

MOLECULAR SHIELDS

Effect of vacuum processing on outgassmg within an

orbiting molecular shield

[NASA-TP-19801 p 99 N82-19390

MOLECULAR SPECTRA

Molecules of significance in planetary aeronomy

[NASA-RP-t030) p 199 N79-22980

Vlbrahonal-Rotational Spectroscopy For Planetary

Atmospheres, volume 1

(NASA-CP-2223-VOL-t ] p 207 N82-25043

MOLECULAR SPECTROSCOPY

Review of Spectroscopic Data for Measurements of

Stratosphenc Species

{NASA-CP-2136) p 192 N80-26125

Review o! spectroscopic parameters for upper

atmospheric measurements

lNASA-CP-2396} p 192 N86-13064

MOLECULAR WEIGHT

Friction and wear of polyethylene oxide polymer having

a range of molecular weights

/ NASA-TP-11291 p91 N78-15278

Effect of sliding speed and contact stress on tribological

properties ot ultra-high-molecular-weighl polyethylene

I NASA-TP-20591 p 95 N83-14269

Ultra-high molecular weight silphenylene-silexane

potymers

(NASA-TP-2295p p g5 N84-19564

Formulation/cure technology for ultrahigh molecular

weight silphenyfene-siloxane polymers

INASA-TP-2476} p 96 N85-26990

MOLYBDENUM DISULFIDES

Transfer of molybdenum disulfide to various metals

I NASA-TP-10191 p 98 N77-30296

Lubrication and failure mechanisms of molybdenum

disulfide films. 1: Effect of atmosphere

INASA-TP-1343} p 92 N79-13158

Lubrication and failure mechanisms Of molybdenum

disulfide films. 2: Effect of substrate roughness

INASA-TP-13791 p 92 N79-13159

MOMENTS

Experimental trim drag values and flow-field

measurements for a wide-body transport model with

conventional and supercrntical wings

lNASA-TP-2071 ] p 25 N85-t0920

MOMENTUM

The Origin of Nonradiative Heating/Momenlum in Hot

Stars

[ NASA-CP-23581 p 200 N85-17755

MOMENTUM TRANSFER

A m_croprocessor-based table lookup approach for

magnetic bearing linearization

{NASA-TP-1838] p 101 NB1-22281

A stochastic model for particle impingements on orbiting

spacecraft

INASA TP 2550] p 184 N86-19095

MONITORS

Proposed fast-response oxygen monitoring and control

system for the Langley 8-foot high-temperature tunnel

{NASA-TP-2218] p 116 N84-11460

MONTE CARLO METHOD

Generation of pseudo-random numbers

INASA-TP-2105] p 183 N83-16095

An efficient algorithm for generating random number

pairs drawn from a blvariate normal distribution

[ NASA-TP-2173 ] p 184 N83-27679

Monte Carlo lattice models for adsorbed polymer

conformation

[ NASA-TP-24531 p 195 N85-24961

Adding computationally efficient realism to Monte Carlo

turbulence simulation

[NASA-TP-2469J p 185 N85-28708

MOON

The Soviet-American Conference on Cosmochemistry

of the Moon and Planets. parl 2

j NASA-SP-370-PT-21 p 203 N78-12958

Handbook of lunar materials

INASA-RP-t0571 p 206 N80-16009

The geology of the terrestrial planets

[ NASA-SP-469 } p200 N85-18888

MORPHOLOGY

Morphology of an aluminum alloy eroded by a jet of

angular particles impinging at normal incidence

[NASA-TP-2139} p 89 N83-24641

MOSAICS

Atlas of Mars: The 1:5000000 map series

[NASA-SP-438] p 206 N80-t6998

A Catalog of Selected Viking Orbiter Images

{NASA-RP-10931 p 207 N83-25636

MOTION PERCEPTION

Simulator study of the effect of visual-motion time delays

on pilot tracking performance with an audio side task

{NASA-TP-1216J p 32 N78-30090

Experiments in sensing transient rotational acceleration

cues on a flight simulator

{NASA-TP-1537] p 33 N80-10193

MOTION SIMULATORS

Effects of visual and motion simulation cueing systems

on pilot performance during takeoffs with engine failures

[NASA-TP-1365] p 32 N79-14082

Application of modified profile analysis to function testing

of the motion/no-motion issue in an aircraft

ground-handling simulation --- statistical analysis

procedure for man machine systems flight simulation

INASA-TP-1540] p 33 N80-13024

The effects of motion and g-seal cues on pilot simulator

performance of three piloting tasks

INASA-TP-160t } p 34 N80-15069

Sample data effects of high-pass filters

INASA-TP-1797] p 35 N81-16040

Evaluation of g seat augmentation of fised-base/moving

base simulation for transport landings under two visually

imposed runway width conditions

INASA-TP-2135} p 36 N83-22191

Effects of motion base and g-seat cueing of simulator

pilot performance

[NASA-TP-2247] p 37 N84-18189

MOTOR VEHICLES

Summary report: Workshop on Vehicle Ride Quality

{NASA-CP-2013} p 172 N78-11705

MOUNTAINS

Operational Applications of Satellite Snowcover

Observations

[E80-101671 p 139 N80-25742

MOUNTING

investigation of effects of microphone position end

orientation on near-ground noise measurements

{NASA-TP-20041 p 189 N84-10913

MULTILAYER INSULATION

Purging of a tank-mounted multilayer insulation system

by gas diffusion

[ NASA-TP-t 127 J p65 N78-17127

Thermal performance of gaseous-helium-purged

tank-mounted multilayer insulation system during

ground-hold and space-hold thermal cycling and exposure

to water vapor

{ NASA-TP-11 f41 p65 N78-28150

MULTIPLIERS

Topics in the optimization of millimeter-wave mixers

INASA-TP-2287} p 103 N84-20758

MULTIPROCESSING (COMPUTERS)

Operating system for a real-time multiprocessor

propulsion system simulator User's manual

INASA-TP-2426] p 180 N85-17596

ReabTime Multiprocesser Programming Language

(RTMPL) user's manual

[NASA-TP-24221 p 179 N85-28610

MULTISPECTRAL BAND SCANNERS

Quantitative analysis of aircraft muttispectral-scanner

data and mapping of water-quality parameters in the James

River in Virginia

JNASA-TP-t021 ] p 147 N78-13628

Procedures for gathering ground truth information for

a supervised approach to a computer-implemented land

cover classification of LANOSAT-ecquired multispectral

scanner data

(NASA-RP-1015J p 137 N78-15549

Preliminary resulls of passive microwave snow

experiment during February and March 1978

[NASA-TP-t4081 p 152 N79-19519

Determination of noise equivalent reflectance for a

multispectral scanner: A scanner sensitivity study

{NASA-TP-1575} p 114 N80-12399

Demonstration of wetland vegetation mapping in Florida

from computer-processed satellite and aircraft

multispectral scanner data

INASA-TP-1553] p 139 N80-15535

The time-space relationshap of the data point (Pixels)

of the thematic mapper and multispectral scanner or the

myth of simultaneity

{NASA-TP-1715] p 76 N80-28424

LANDSAT-4 Science Characterization Early Results.

Volume 1: Multispectral Scanner (MSS)

[E85-10067} p 143 N85-20496

LANDSAT-4 and LANDSAT-5 multispectral scanner

coherent noise characterization and removal

JNASA-TP-2595] p 143 N86-31945

MULTISPECTRAL PHOTOGRAPHY

Eulusmap: An international land resources map utilizing

satellite imagery

INASA-TP-1371] p 138 N79-13475

Synthebc aperture radarfLANDSAT MSS image

regustration

INASA-RP-1039] p 139 N80-16405

High speed lookup table approach to radiometric

calibration of multispectral image data

INASA-TP-1741 ] p 76 N80-33463

The Multispectral Imaging Science Working Group.

Volume 3: Appendices

[E83-10351 } p 142 N83-28506

The Multispectral Imaging Science Working Group.

Volume 1; Executive summary

[E85-10001] p 142 N85-t1404

The Multispectral Imaging Science Working Group

Volume 2: Working group reports

IE85-10002] p 142 N85-11405

MULTISTAGE ROCKET VEHICLES

Stages to Saturn: A technological history ol the

Apollo/Saturn launch vehicles

[NASA-SP-4206] p 72 N81-29154

MUONS

Nineteenth International Cosmic Ray Conference HE

sessions, volume 8

[ NASA-CP-2376-VOL-8 ] p 21 t N85-36066

N

NACELLES

Effect of slotted casing treatment with change in

Reynolds number index on performance of a jet engine

{NASA-TP-1058 ] p41 N77-32154

Theoretical flow characteristics of inlets for titling-nacelle

VTOL aircraft

{NASA-TP-t 205 ] p42 N78-21114

Theoretical study of VTOL tilt-nacelle axisymmetric inlet

geometries

[NASA-TP-13801 p 10 N79-14996

Experimental and theoretical aerodynamic

characteristics of two hypersonic cruise aircraft concepts

at Mach numbers of 2.96, 3.96, and 4.63

[NASA-TP-17671 p 16 N81-12021

Effects of varying podded nacelle-nozzle installations

on transonic aeropropulsive characteristics of a supersonic

fighter aircraft

[NASA-TP-2120J p 21 N83-26821

An experimental investigation of nacelle-pylon

installation on an unswept wing at subsonic and transonic

speeds

{NASA-TP*22461 p 23 N84-18162

Aerodynamic characteristics of a high-wing transport

configuration with a over-the-wing nacelle-pylon

arraogemenl

INASA-TP-2497] p 27 N86-16193

Effect of underwiog aft-mounted nacelles on the

longitudinal aerodynamic characlenstics of a high-wing

transport airplane

INASA-TP-2447] p 27 N86-20345

Installation effects of long-duct pylon-mounted nacelles

on a twin-jet transport model with swept supercritical

wing

[NASA-TP-24571 p 27 N86o20346

NAMING

Origins of NASA names

|NASA-SP-4402} p 21t N77-16981

NAP-OF-THE-EARTH NAVIGATION

Helicopter Handling Qualities

[NASA-CP-22191 p 30 N82-23208

NASA PROGRAMS

Origins of NASA names

[NASA-SP-4402} p 211 N77-16981

Aircraft Safety and Operating Problems --- conference

[NASA-SP-4f6} p 28 N77-18081

Voyager to Jupiter and Saturn

[NASA-SP-420] p 205 N77-29046

Skylab, classroom in space

INASA-SP-401 I p 65 N77-29189

Bibfiography of Supersonic CruiSe Aircraft Research

(SCAR)

{NASA-RP-10031 p 197 N78-12895

Astronaulics and aeronautics, 1974: A chronology

INASA-SP-40"19_ p 212 N78-12997

Gunlersville Workshop On Solar-Terrestrial Studies

[NASA-CP-20371 p 144 N78-19600

High altitude perspective --- cost-reimbursable services

using NASA U-2 aircraft

INASA-SP-4271 p 138 N78-31508

YF-12 experiments symposium, volume 1

[NASA-CP-2054-VOL-1 I p 9 N78-32055

The partnership: A history of the Apotlo-Soyuz test

project

[NASA-SP-4209] p 61 N79-10074

OGO program summary, supptemenl 1 --- updated

bibliography for atl OGO missions and sctentihc results

from OGO 5 and 6 missions

{NASA-SP-7601-SUPPL-t } p 151 N79-13601

Fourth National Aeronautics and Space Administration

Weather and Climate Program Science Review

{NASA-CP-2076} p 159 N79-20633

A-80
SUBJECT INDEX NICKEL HYDROGEN BAI"FERIES

Ozone Contamination in Aircraft Cabins

[NASA-CP-2066] p 29 N79-21021

NASF transposition network: A computing network for

unscrambling p-ordered vectors

{NASA-TP-1426] p 180 N79-21822

Onset of condensation effects with an NACA 0012-64

airfoil tested in the Langley 0.3-meter transonic cryogenic

tunnel

[NASA-TP-1385] p 12 N79-22043

Important factors in the maximum likelihood analysis of

flight test maneuvers

[NASA-TP-1459] p 54 N79-22113

NASA JSC water monitor system: City of Houston field

demonstration

|NASA-RP-1041] p 198 N79-28062

Summary of the NASA/MSFC FY-79 Severe Storm and

Local Weather research review --- cloud physics,

atmospheric electricity, and mesescale/storm dynamics

reserach

[NASA-CP-2f05] p 160 N79-33722

An evaluation of the NASA Tech House, including live-in

test results, volume 1

[NASA-TP-1564] p 145 N80-11559

Quiet powered-lift propulsion

[NASA.CP-2077| p 46 N80-15127

NASA/MSFC FY-80 Atmospheric Processes Research

Review

[NASA-CP-2145J p 153 N80-28965

Astronautics and Aeronautics. 1975. A chronology

[NASA-SP-4020] p 212 N81-16973

The 1980 Aircraft Safety and Operating Problems, pad

t

[NASA-CP-2170-PT-1] p 29 N81-19035

Beyond the atmosphere: Early years of space

science

[NASA-SP-421f ] p 200 N81-20962

Goddard Laboratory for Atmospheric Science, collected

reprints f978-f979, volume 1

[NASA-TP-1788-VOL-11 p 163 N81-21686

Goddard LaboratoP/ for Atmospheric Sciences,

collected reprints 1978 - 1979, volume 2

[NASA-TP-1788-VOL-2) p 163 N81-21693

Orders of magnitude: A history of NACA and NASA,

1915 - 1980

[NASA.SP-4403] p 196 N82-14955

Managing NASA in the Apo;;o era

[NASA-SP-4102] p 196 N83-18851

Small transport aircraft technology

[NASA-SP-460] p 36 N83-20931

Pioneer Venus

[NASA.SP-461J p 207 N83-30340

NASA publications guide

[NASA-SP-7047] p 197 N83-32671

Records of achievement: NASA special publications

[NASA-SP-470J p 197 N83-33792

The NASA Geodynamics Program: An overview

[NASA-TP-2147] p 154 N84-10675

STEP Experiment Requirements

[NASA-CP-2294] p 67 N84-17211

NASA Administrative Data Base Management Systems,

1983

[NASA-CP-2304] p 198 N84-21403

The star splitters: The high energy astronomy

>bservatodes

NASA.SP-466] p 202 N84-22516

NASA Administrative Data Base Management Systems,

1984

NASA-CP-2323] p 198 N84-33266

A spaoefaring people: Perspectives on early

spaceflight

NASA-SP-4405] p 212 N85-35142

Significant NASA inventions available for licensing in

foreign countries

NASA-SP-7038(08) I p 198 N86-26243

NASA patent abstracts bibliography: A continuing

bibliography. Section 1: Abstracts

NASA-SP-7039(29)-SECT-1J p 198 N86-28788

NASA Patent Abstracts Bibliography A continuing

bibliography. Section 2: Indexes (Supplement 29)

NASA-SP-7039(29)-SECT-2] p 198 N86-28789

The MSFC/UAH Data Management Symposium

[NASA-CP-2040] p 177 N78-74659

NASTRAN

Sixth NASTRAN Users' Colloquium

=[NASA-CP-2019,1 p 127 NTB-t2443

Seventh NASTRAN User's Colloquium

[NASA-CP-2062] p 127 N78-32466

Guide to a condensed form of NASTRAN

[NASA-RP-1019] p 178 N78-33791

Eighth NASTRAN User's Colloquium

[NASA-CP-2131] p 129 N80-24648

Ninth NASTRAN Users' Colloquium

[NASA..CP-2151] p 129 N80-33782

Tenth NASTRAN User's Colloquium

[NASA-CP-2249] p 131 N83-12452

The NASTRAN theoretical manual

[NASA-SP-221(06)] p 132 N84-18677

The NASTRAN user's manual

|NASA-SP-222(06) l p 133 N84-21899

Twelfth NASTRAN Users' Colloquium

[NASA-CP-2328] p 133 N84-32864

Thirteenth NASTRAN Users' Colloquium

[NASA-CP-2373} p t34 N85-25863

Fourteenth NASTRAN Users' Colloquium

INASA-CP-24191 p 135 N86-25823

The NASTRAN demonstration problem manuaJ, level

17.5

I NASA-SP-224(05) j p 130 N81-71592

The NASTRAN programmers manual, level 175

[ NASA-SP-223(05) j p 130 N81-71594

NATtON_I,L OCEANIC SATELUTE SYSTEM

NOSS altimeter algorithm specifications

[NASA-RP-1083] p 168 N82-16683

NATURAL GAS

Combustion gas properties, 2: Natural gas fuel and

dry air

[NASA-TP-2435] p 52 N85-21168

New method for determining heats of combustion of

gaseous hydrocarbons

[NASA-TP-2531 I p I f7 N86-20753

Measurement of viscosity of gaseous mixtures at

atmospheric pressure

{ NASA-TP-28821 p 117 N86-24962

NATURAL SATELLITES

The Saturn System

[NASA-CP-2068J p 205 N79-16758

NAVIER-STOKES EQUATION

Foreb_y and afterbody solutions of the Navier-Stokes

equations for supersonic flow over blunt bodies in a

generalized orthogonal coordinate system

INASA-TP-10751 p 104 N78-18362

A numerical solution of the Navier-Stokes equations for

chemically nonequilibrium, merged stagnation shock layers

on spheres and two-dimensional cylinders in air

[NASA-TP-1227] p 105 N78-23390

Velocity-split Navier-Stokes solution procedure for

incompressible high Reynolds number external flows

INASA-TP-1655J p 108 N80-21702

Numerical SOlUtions of the Navier-Stokes equations for

transonic afterbody flows

INASA-TP-1784] p 16 N81-13919

Numerical simulation of steady supersonic flow --- spat_aJ

marching

I NASA-TP-1749 ] p 17 N81-22018

Multignd Methods

INASA-CP-2202_ p 182 1"481-33879

Some observations on a new numerical method for

solving Navier-Stokes equations

INASA-TP-19341 p 18 N82-11032

Numedcal analysis of the scramjet-inlef flow field by

using two-dimensional Navier-Stokes equations

[NASA-TP-1940] p 48 N82-13142

NAVIGATION

Space Shuttle Technical Conference, part 2

{NASA-CP-2342-PT-2] p 63 N85-16937

NAVIGATION AIDS

Experimental determination of position-estimate

accuracy using back-azimuth signals from a microwave

landing system

INASA-TP-f5741 p 30 N80-13020

Navigation, guidance, and control for helicopter

automatic landings

INASA-TP-16491 p 55 N80-23326

Joint University Program for Air Transportation

Research, 1980

(NASA-CP-2176] p 3 N81-21999

NAVIGATION SATELLITES

Proceedings of the Thirteenth Annual Precise Time and

Time Interval (PTrl) Applications and Planning Meeting

[ NASA-CP-2220] p 118 N82-20494

NEAR INFRARED RADIATION

Laboratory measurements of physical, chemical, and

optical characteristics of Lake Chicof sediment waters

[NASA-TP-t941 ] p 148 N82-f3468

Introduction to the theory of atmospheric radiative

transfer

[NASA-RP-1156] p 157 N86-27839

NEAR WAKES

Mean-flow al'_d turbulence measurements in the vicinity

of the trailing edge of an NACA (63 sub 1)-012 airfoil

]NASA-TP-1845] p 109 N81-23410

NEBULAE

An emission-line survey of the Milky Way

[ NASA-SP-434 ] p201 N80-11966

Future ol Ultraviolet Astronomy Based on Six Years of

IUE Research

[NASA-CP-2349] p 203 N85-2096t

NEGATIVE CONDUCTANCE

Circuit transients due to negative bias arcs on a

high-voltage solar array in low Earth orbit

[NASA-TP-2407] p 75 N85-14858

NEPHANALYSIS

A new NASA/MSFC mission analysis global cloud cover

data base

lNASA-TP-2448] p 186 N85-21878

NEPTUNE (PLANET)

Uranus and Neptune

{NASA-CP-2330J p 208 N85-11927

NETWORK CONTROL

Concept for a power system controller for large space

electrical power systems

[NASA-TP-1939J p 77 N82-11109

NEUROLOGY

Human Neurological Development: Past, Present and

Future

[NASA-CP-2063] p 212 N79-15887

NEUTRINOS

Nineteenth International Cosmic Ray Conference HE

sessions, volume 8

JNASA-CP-2376-VOL-8J p 211 N85-36066

NEUTRON SOURCES

Direct nuclear-powered lasers

[NASA-TP-20gt I p 1t8 N83-t6738

NEVADA

Wildland inventory and resource modeling tot Douglas

and Carson City Counties, Nevada, using LANDSAT and

digital terrain data

[E83-103021 p 142 N83-27293

NEWTON THEORY

Research in nonlinear structural and solid mechanics

[NASA-CP-2147J p 129 N80-32756

NICKEL

Friction and wear of selected metals and alloys in sliding

contact with AISI 440 C stainless steel in liquid methane

and in liquid natural gas

[NASA-TP-1150] p 119 N78-20512

Effects of thermomechanical processing on strength and

toughness of iron - 12-percent-nickel - reactive metal alloys

af -196 C

I NASA-TP-1308 J p86 N78-31213

X-ray photoelectron spectroscopy and friction studies

of nickel-zinc and manganese-zinc ferrites in contact with

metals

[NASA-TP-2163J p 88 N83-23419

Friction and wear of nickel in sulfuric acid

l NASA-TP-2290 J p 89 N84-21721

Humidity effects on adhesion of nickel-zinc ferrde in

elastic contact with magnetic tape and itself

[NASA-TP-2449J p 96 N85-21359

An update of the total-strain version of SRP

_ NASA- TP-2499 _ p 9'3 N86- f 2295

NICKEL ALLOYS

Feasibility study of tungsten as a diffusion barrier

between nickel-chromium-aluminum and Gamma/Gamma

prime - Delta eutectic alloys

[NASA-TP-f 131 | p86 N78-15230

Friction and morphology of magnetic tapes in siiding

contact with nickel-zinc ferrite

[NASA-TP-2267] p 95 N84-16334

Analysis of thermoelectric properties of

high-temperature complex alloys of nickel-base, iron-base

and cobalt-base groups

[NASA-TP-2278] p 89 N84-f8370

Water-vapor effects on friction of magnetic tape in

contact with nickel-zinc ferrite

INASA-TP-2279] p 95 N84-18399

Effects of alloy composition on cyclic flame hot-corrosion

attack of cast nickel-base superalloys at 900 deg C

[NASA-TP-2338] p 89 N84-26783

Chemical mechanisms and reaction rates for the

initiation of hot corrosion of IN-738

{NASA-TP-2319] p 90 N84-28958

Thermal-fatigue and oxidation resistance of

cobalt-modified Udimet 700 alloy

[NASA-TP-2591 } p 135 N86-28464

NICKEL CADMIUM BATTERIES

Sealed.cell nickel-cadmium battery applications

manual

INASA-RP-1052] p 77 N80-16095

Life test of a nickel cadmium battery with a

protection/reconditioning circuit

INASA-TP-1873J p 77 N81-24167

The 1981 Goddard Space Flight Center Battery

Workshop

[ NASA-CP-2217 ] p 102 N82-20402

The 1984 Goddard ._oace F_jht Center Battery

Workshop

INASA-CP-2382} p 103 N85-31371

NICKEL COATINGS

Adhesion between polymers and evaporated gold and

nickel films

[NASA-TP-2360J p 96 N84-31379

NICKEL HYDROGEN BATTERIES

The 1981 Godqard Space Flight Center Battery

Workshop

[NASA-CP-2217] p 102 N82-20402

A-81
NIGHT FLIGHTS (AIRCRAFT)

The 1982 God(lard SPace Flight Center Battery

Workshop

[ NASA-CP-22631 p 102 N83-35230

The 1984 Goddard Space Flight Center Battery

Workshop

{NASA-CP-2382t p 103 N85-31371

NIGHT FLIGHTS (AIRCRAFT)

Helicopter Handling Qualities

[NASA-CP-2219] p 30 N82-23208

NIMBUS PROJECT

The Conception, Growth, Accomplishments and Future

of Meteorological Satellites

[NASA-CP-2257] p 164 N83-14825

NIMBUS 8 SATELLITE

Parameter estimation applied to Nimbus 6 wide-angle

Iongwave radiation measurements

INASA-TP-t307} p 159 N79-13644

Determination of wind from NIMBUS 6 satellita sounding

data

[NASA-RP-1072] p 162 N81-15639

A comparat_'e analysis of rawmsonde and NIMBUS 8

and TIROS N satellite profile data

[NASA-RP-1070] p 162 N81.15640

Atmospheric structure determined from satellite data

[NASA-RP-10711 p 162 N8'1-16678

Comparisons between Nimbus 6 satellite and

rawinsoode soundings for several geographical areas

INASA-RP-f073] p 163 N81-16679

Nimbus 6 Random Access Measurement System

applications experiments

INASA-SP-457} p 165 N83-14835

NIMBUS 7 SATELLITE

User's guide for the Solar Backscattered Ultraviolet

(SBUV) instrument first year ozone-S data set

{NASA-RP-1095] p 164 N82-29826

Description of data on the Nimbus 7 LIMS map archive

tape: Temperature end geopetentiel height

I NASA-TP-25531 p 167 N86-25924

El Nino and outgoing Iongwave radiabon: An atlas of

Nimbus-7 Earth radiation budget observations

I NASA-RP-t 163 } p 157 N86-29425

NIOBIUM ALLOYS

Long-time creep behavior of the niobium alloy C-103

I NASA-TP-17271 p 87 N80-33555

NITRATES

Sulfate and nitrate collected by filter sampling near the

tropopause

{NASA-TP-1567J p t49 N80-t4581

NITRIC OXIDE

Effect of nitric oxide on photochemical ozone formation

in mixtures of air w_th molecular chtonne and with

Irichlorofluoromethane

( NASA-TP-1192 J p 84 N78-20281

Experimental and analytical study of nitric oxide

formation during combustion of propane in a jet-stirred

combustor

I NASA-TP-1181 j p 84 N78-23172

Chemical kinetic models for combustion of hydrocarbons

and formation of nitric oxide

[NASA TP 1794] p 85 N81-14017

Proceedings of s Workshop on Assessment of

Techniques for Measuring Tropospheric N sub x O sub y

INASA-CP-22921 p 154 N84-13706

NITRIDING

Nitriding of titanium and titanium: 8 percent aluminum,

1 percent molybdenum. I percent vanadium alloy with an

ion-beam source

[NASA-TP-21491 p 89 N83-24640

NITROGEN

Effect of oxygen and nitrogen interactions on friction

of single-crystal silicon carbide

t NASA-TP-1265 ] p 92 N78-28247

Effect of nitrogen-containing plasma On adherence,

fricbon, and wear of rsdiofrequency-spuftered titanium

carbide coatings

ENASA-TP 1377J p92 N79-15184

Effect of oxygen-nitrogen ratio on sinterability of

S=alons

[ NASA-TP-t 3821 p92 N79-21204

Surface chemistry of iron sliding in air and nitrogen

lubricated with hexadecane and hexadecsne containing

dibenzyt-ditsulfide

[NASA-TP-15451 p 79 N79-31346

Thermodynamic properties of nitrogen gas derived from

measurements of sound speed --- for cryogenic wind

tunnels

I NASA-RP-1051 J p 97 N80-14257

A theoretical analysJs of simulated transonic boundary

layers in cryogenic-nitrogen wind tunnels

[NASA-TP-1631 } p 59 N80-19131

Effecls of various assumptions on the calculated liquid

fraction in isentropic saturated equilibrium expansions

{NASA-TP-1682] p 108 N80-25615

A-82

Experimental study of cluster formation in binary mixture

of H20 end H2SO4 vapors in the presence of an ionizing

radiation source

{NASA-TP-1735] p 149 N81-11565

Simulation of ideal-gas flow by nitrogen and other

selected gases at cryogenic temperatures --- transonic flow

in cryogenic wind tunnels

[NASA-TP-1901} p 109 N81-32418

Nitnding of titanium and titanium: 8 percent aluminum,

1 percent molybdenum, 1 percent vanadium alloy with an

ion-beam source

[NASA-TP-2149] p 89 N83-24640

NITROGEN DIOXIDE

Nitrogen dioxide vapor penetration of chlorobutyl rubber

SCAPE under operational conditions

[NASA-TP-t605] p 85 N80-161t8

Carbon-catalyzed oxidation of SO2 by NO2 and air

{NASA-TP-2014} p 85 N82-22330

SAGE aerosol measurements Volume 1; February 21,

1979 to December 31, 1979

[NASA-RP-1144} p 155 N86-11700

SAGE Aerosol Measurements. Volume 2: 1 January -

31 December 1980

[NASA-RP-1149] p 156 N86-23088

NITROGEN IONS

Friction wear and auger enatysis of iron implanted with

1 5-MeV nitrogen ions

[NASA-TP-19891 p 88 N82-21300

NITROGEN LASERS

A blackbody-pumped CO2-N2 transfer laser

[NASA-TP-2347] p 118 N84o31617

NITROGEN OXIDES

Nitric oxide production in the stratosphere within the

Space Shuttle's solid rocket motor plumes

[NASA-TP-1305] p 68 N78-33135

Effect of pressure on structure and NO sub X formation

in CO-SIr diffusion flames

{NASA-TP-1448] p 84 N80-13191

The stratcom 8 effort --- stratospheric photochemistry

(NASA-TP-1640] p 16t N80-22924

Analysis of effect of flameholder characteristics on lean,

premixed, partially vaporized fuel-sir mixtures quality and

nitrogen oxides emissions

{NASA-TP-1842] p 48 N81-24065

Effect of fuel-sir-ratio nonuniformity on emissions of

nitrogen oxides

INASA-TP-1798] p 48 N82-13143

Venturi nozzle effects on fuel drop size and nitrogen

oxide emissions

{NASA-TP-2028] p 49 N82-31329

Expanded operational capabilities of the Langley Mach

7 Scramjet test facility

[NASA.TP-2"I86] p 60 N83-36039

NITROGEN TETROXIDE

Triple point determinations of monomethylhydrazine and

nitrogen tetroxide, 22 percent by weight nitric oxide

[NASA-RP-10131 p 96 N78-13234

Proceedings of the NASA/Florida institute of

Technology Environmental Engineering Conference on

Nitrogen Tetroxide --- with emphasis on space shuttle

INASA-CP-20491 p 136 N79-20424

NOBLE METALS

Friction and transfer of copper, silver, and gold 1o iron

in the presence of various adsorbed surface films

[NASA-TP-13921 p 120 N79-14386

NOISE (SOUND)

Interaction of a turbulent-jet noise source with transverse

modes in a rectangular duct

[NASA-TP-1248] p 1 N78-25049

Overall loudness of steady sounds according to theory

and experiment

INASA-RP-1001 ] p 171 N79-25753

Free-stream noise and transition measurements on a

cone in a Mach 3.5 p,lot low-disturbance tunnel

{NASA-TP-2180} p 111 N83-34229

Physiological, Psychological, and Social Effects of

Noise

[NASA-RP-1115J p 174 N84-29465

Numerical Techniques in Acoustics

{NASA-CP-2404] p 190 N86-12007

ExperimentaI study of the effects ol installation on

singteand counter-rotation propeller noise

[NASA-TP-2541 ] p 191 N86-26162

NOISE GENERATORS

Measurements of the tonal component of cavity noise

and comparison with lheory --- aircraft noise

INASA-TP-10131 p 185 N78-12800

Investigation of jet-installation noise sources under static

conditions

[NASA-TP-2181 I p 189 N83-33684

Location of no_se sources umng a phase-slope

method

{NASA-TP-2505] p 191 N86-t6041

SUBJEC T INDEX

NOISE INTENSITY

Acoustic performance of two 1.83-meter-diameter fans

designed for a wind-tunnel drive system

[NASA-TP-1008} p 185 N77-30909

Statistical comparisons of aircraft flyover noise

adjustment procedures for different weather conditions

[NASA-TP-1430} p 187 N79-24773

Effects of sound level fluctuations on annoyance caused

by aircraft-flyover noise

[NASA-TF-1576] p 187 N80-13880

NOISE MEASUREMENT

Measurements and predictions of flyover and static noise

of • TF30 afterbuming turbofan engine

[NASA-TP-1372] p 43 N79-13045

Effects of road traffic background noise on judgments

of individual airplane noises

[NASA.TP-1433} p 148 N79-28796

Evaluation ol a vortex model of turbulent cavity flow

--- for computing noise generation of fluid flow

[NASA-TP-1505] p 187 N79-32057

Landing approach airframe noise measurements and

analysis

[NASA-TP-1602] p 2 N80-15028

Aliased noise in radiometric measurements

{NASA-TP-1639] p 114 N80-22660

Noise reduction in a Mach 5 wind tunnel with •

rectangular rod-wall sound shield

[ NASA-TP-f 672l p 108 N80-26622

Time-of-Day Corrections to Aircraft Noise Metrics

[NASA-CP-2135] p 187 N80-28150

A new theory for rap0d calculation of the ground pattern

of the incident sound intensity produced by e maneuvering

jet airplane

I NASA-TP-1733} p 15 N80-32334

Flight test of a pure-tone acoustic source --- aircraft

noise

NASA-TP-1898} p 188 N81-33945

Experimental study of noise reduction for an unstiffened

cylindrical model of an airplane fuselage

NASA-TP-1964} p 188 N82-14879

Fluctuating pressures on fan blades of s turbofan engine:

Static and wind-tunnel investigations

NASA-TP-19761 p 188 N82-21037

Residents' annoyance responses to aircraft noise

events

NASA-TP-2121 } p 189 N83-34713

Investigation of effects of microphone position and

orientation on near-ground noise measurements

NASA-TP-2004] p 189 N84-10913

Simplified combustion noise theory yielding a prediot_on

of fluctuating pressure level

NASA-TP-2237] p 189 N84-19049

Physiological, Psychological, and Social Effects of

Noise

NASA-RP-t 1 t 51 p 174 N84-29465

Analysis of noise measured from a propeller in a wake

{ NASA-TP-23581 p 190 N85-11788

Experimental study of the effects of installation on

singleand counter-rotation propeller noise

INASA-TP-2541 j p 191 N86-26162

NOISE POLLUTION

Laboratory study of annoyance to combined airplane

and road-traffic noise

[NASA-TP-t478J p 148 N79-32743

A summation and inhibition model of annoyance

response to multiple community noise sources

[NASA-TP-14791 p 148 N79-32744

Annoyance due to multiple airplane noise exposure

{NASA-TP-1706J p 149 N80-28946

A new theory for rapid calculation of the ground pattern

of the incident sound intensity produced by a maneuvering

jet airplane

[NASA-TP-17331 p 15 N80-32334

Effects of activity interference on annoyance due to

aircraft noise

[NASA-TP-19381 p 149 N82-12654

Airport/Community Noise

{NASA-CP-2241 ] p 188 N82-31070

Physiological, Psychological, and Social Effects of

Noise

{NASA-RP-1115] p 174 N84-29465

NOISE PREDICTION

Numerical Techniques in Acoustics

[NASA-CP-24041 p 190 N86-12007

NOISE PREDICTION (AIRCRAFT)

A numencal technique for calculation ol the noise of

high-speed propellers with advanced blade geometry

tNASA-TP-16621 p 187 N80-27161

Time-of-Day Corrections to Aircraft Noise Metrics

[NASA-CP-2135] p 187 N80-28150

Subjective field study of response to impulsive helicopter

noise

INASA-TP-1833} p 187 N81-21873

Airframe noise of a small model transport aircraft and

scaling effects --- Boeing 747

[NASA-TP-1858i p 188 N81-22832
SUBJECT INDEX NONUNIFORM FLOW

Computer program to predict aircraft noise levels

INASA-TP-19131 p 188 N81-33947

Noise and economic characteristics of an advanced

blended supersonic transport concept

[NASA-TP-2073] p 4 N82-31294

Empirical source noise prediction method with

application to subsonic coaxial jet mixing noise

[NASA-TP-2084} p 189 N83-16149

NOISE PROPAGATION

Noise transmission through plates into an enclosure

{NASA-TP-1173] p 186 N78-23877

Noise transmission through flat rectangular panels into

a closed cavity --- light aircraft noise

{NASA-TP-1321 } p 186 N79-14874

Theoretical prediction of nonlinear propagation effects

on noise signatures generated by subsonic or supersonic

propeller or rotor-blade tips

{NASA-TP-1660] p 14 N80-22265

Experimental investigation of the radiation of sound from

an unflanged duct and a belimouth, including the flow

effect

[NASA-TP-16971 p 187 N80-32188

Assessment of ground effects on the propagation of

aircraft noise: The T-38A flight expebment

[NASA-TP-1747} p 187 N81-14788

Flight test of a pure-tone acoustic source --- aircraft

noise

[NASA-TP-1898] p 188 N81-33945

Noise transmission loss of a rectangular plate in an

infinite baffle

lNASA-TP-2398} p 190 N85-22109

Analytical study of acoustic response of a

semireverberant enclosure with application to active noise

control

{NASA-TP-2472} p 191 N86-16040

Consideration of some factors affecting low-frequency

fuselage noise transmission for propeller aircraft

{NASA-TP-2552J p 191 N86-24393

NOISE REDUCTION

Aerodynamic and directional acoustic performance of

a scoop inlet

[NASA-TP-1028} p 41 N77-31152

Optimal guidance and control for investigating aircraft

noise-impact reduction

[NASA-TP-1237| p 53 N78-23t00

A theoretical investigation of noise reduction through

the cylindrical fuselage of a twin-engine, propeller-driven

aircraft

[NASA-TP-13251 p 186 N79-13821

Sonic-boom minimization with nose-bluntness

relaxation

INASA-TP-1348J p 10 N79-15000

A summation and inhibition model of annoyance

response to multiple community noise sources

{NASA-TP-t4791 p 148 N79-32744

A closed-form solution for noise contours

[ NASA-TP-t 4321 p 187 N80-11869

Evaluation of helicopter noise due to b blade-vortex

interaction for five tip configurations --- conducted in the

Langley V/STOL tunnel

{NASA-TP-t608] p 187 N80=14840

Evaluation of approximate methods for the prediction

of noise shielding by airframe components

[ NASA-TP-1004 ] p46 N80-15129

Experimental evaluation of a spinning-mode

acoustic-treatment design concept for aircraft inlets ---

suppression of YF-t02 engine fan noise

[ NASA-TP-1613 } p46 N80-21323

Forward acoustic performance of a shock-swallowing

high-tip-speed fan (QF-13)

{NASA-TP-16681 p 187 N80-23100

Noise reduction in a Mach 5 wind tunne} with a

rectangular rcd-wall sound shield

[NASA-TP-t672] p 108 N80-26622

Low-speed aerodynamic performance of

50,8-centimeter-diameter no_se-suppressing inlets for the

Quiet, Clean, Short-haul Experimental Engine (QCSEE) ---

Lewis 9- by 15-foot low speed wind tunnel tests

{NASA-TP-1178] p 47 N81-11037

A simulator study for the development and evaluation

of operating procedures on a supersonic cruise research

transport to minimize airport-community noise

INASA-TP-1742] p 29 N81-12043

The 1980 Aircraft Safety and Operating Problems, part

2

{NASA-CP-2170-PT-2] p 29 N81-19056

Noise suppression characteristics of peripherally

segmented duct liners

[NASA-TP-1904} p 188 N81-33946

Experimental study of noise reduction for an unstiffened

cylindrical model of an airplane fuselage

{NASA-TP-1964} p 188 N82-t4879

Forward acoustic performance of a model turbofan

designed for a high specific flow (QF-14)

[NASA-TP-1968} p 188 N82-21036

Aeroecoustic performance of an externally blown flap

configuration with several flap noise suppression devices

[NASA-TP-tggs] p 168 N82-24942

Airport/Community Noise

[NASA-CP-2241 } p 188 N82-31070

Circumferential]y segmented duct lines optimized for

axisymmetric and standing wave sources --- reducing noise

from turbofan engines galerkin method acoustic

attenuation

[NASA-TP-2075] p 188 N82-34190

Flight effects of fan noise

[NASA-CP-2242] p 189 N83-10883

Empirical source noise prediction method with

application to subsonic coaxial jet mixing noise

[NASA-TP-2084] p 189 N83-16149

Fluid shielding of high-velocity jet noise

[NASA-TP-2259] p 189 N84-15894

Physiological, Psychological, and Social Effects of

Noise

[NASA-RP-tt15] p 174 N84-29465

Rotorcraff noise

[NASA-CP-2234} p 190 N84-29662

Effects of propeller rotation direction on airplane interior

noise levels

[NASA-TP-2444] p 190 N85-30767

Analytical study of acoustic response of a

semireverberant enclosure with application to active noise

control

[NASA-TP-2472} p 191 N86-16040

NOISE SPECTRA

A comparison of the noise produced by a small jet on

a moving vehicle with that in a free jet --- jet mixing

noise

[NASA-TP-1326J p 186 N79-14872

Statistical comparisons of aircraft flyover noise

adiustment procedures for different weather conditions

[NASA-TP-1430} p 187 N79-24773

Proton-induced noise in digicons

[NASA-TP-t852} p 76 N81-31281

Consideration of some factors affecting low-frequency

fuselage noise transmission for propeller aircraft

[NASA-TP-2552} p 191 N86-24393

NOISE THRESHOLD

Variability of annoyance response due to aircraft noise

[NASA-TP-13351 p 186 N79-18687

NOISE TOLERANCE

Effects of duration and other noise characteristics on

the annoyance caused by aircraft-flyover noise

[NASA-TP-1386] p 186 N79-20832

Human discomfort response to noise combined with

vertical vibration

[NASA-TP-1374] p 171 N79-22761

Laboratory study of annoyance to combined airplane

and read-traffic noise

[NASA-TP-1478] p 148 N79-32743

Effect of noise spectra and a listening task upon

passenger annoyance in a helicopter interior noise

environment

INASA-TP-1590} p 171 N80-13769

Time-of-Day Corrections to Aircraft Noise Metrics

INASA-CP'2135 ] p 187 N80-28150

Effects of conversation interference on annoyance due

to aircraft noise

INASA-TP-1712] p 149 N80-29911

Effects of repetition rate and impulsiveness of simulated

helicopter rotor noise on annoyance

INASA-TP-1969] p 150 N82-19707

NOMENCLATURES

NASA catalogue of lunar nomenclature

[NASA-RP-10971 p 207 N83-12031

NONDESTRUCTIVE TESTS

Structural Integrity and Durability of Reusable Space

Propulsion Systems

{NASA-CP-2381 I p 78 N85-27941

Analytical Ultrasonics in Materials Research and

Testing

{NASA-CP-2383] p 126 N86-22962

NONEQUILIBRIUM CONDITIONS

A numerical solution of the Navier-Stokes equations for

chemically nonequilibrium, merged stagnation shock layers

on spheres and two-dimensional cylinders in air

{NASA-TP-t227t p 105 N78-23390

NONEQUILIBRIUM FLOW

Slip-boundary equations for multicomponent

nonequilibrium airflow

{NASA-TP-2452 ] p t 13 N86-14530

NONFLAMMABLE MATERIALS

Conference on Fire Resistant Materials: A compilation

of presentations and papers

{NASA-CP-2094] p 29 N79.3t166

NONLINEAR EQUATIONS

Theoretical prediction of nonlinear propagation effects

on noise signatures generated by subsonic or supersonic

propeller or rotor-blade tips

{ NASA-TP-16601 p 14 N80-22265

Pseudosteady-state analysis of nonlinear aircraft

maneuvers

INASA-TP-1758} p 56 N81-t3065

Existence and uniqueness of solutions to a class of

nonlinear-operator-differential equations arising in

automated spaceship navigation

{NASA-TP-1860] p 70 N81-23182

Research in structural and solid mechanics, 1982

{NASA.CP-2245] p 131 N82-33739

Reduction methods for nonlinear steady-state thermal

analysis

[NASA-TP-2098] p 110 N83.20032

Local strain redistribution corrections for a simplified

inelastic analysis procedure based on an elastic

finite-element analysis

[NASA-TP-2421] p 134 N85-20396

Convergence of Newton's method for a single real

equation

[NASA-TP-2489} p 183 N85-28656

NONLINEAR FEEDBACK

Regions of attraction and ultimate boundednese for

linear quadratic regulators with nonlinearities

{NASA-TP-2322} p 181 N84-28538

NONLINEAR FILTERS

Study of the use of a nonlinear, rate-limited filter on

pilot control signals

[NASA-TP-1147} p 53 N78.20142

NONLINEAR PROGRAMMING

Use of constrained optimization in the conceptual design

of a medium-range subsonic transport

{NASA-TP-1762} p 35 N81-16039

A method for obtaining reduced-order control laws for

high-order systems using optimization techniques

[NASA-TP.1876} p 181 N81-30851

Nonlinear optimization with linear constraints using a

projection method

[NASA-TP-2086] p 184 N83-10876

NONLINEAR SYSTEMS

A nonlinear trajectory command generator for a digital

flight-control system

[NASA-TP-1221] p 54 N79-13057

Predicting dynamic performance limits for servosystems

with saturating nonlinearities

[NASA-TP-1488] p 54 N79-28186

On the nonlinear deformation geometry of

Euler-Bernoulli beams --- rotary wings

INASA-TP-1566} p 129 Neo-20619

Research in nonlinear structural and solid mechanics

INASA-CP-2147] p 129 N80-32756

Solution of complex nonlinear problems by a generalized

application of the method of base and comparison

solutions with applications to aerodynamics problems

[NASA-TP-1857] p 17 Net-22019

Global differential geometry: An introduction for control

engineers

INASA-RP-1091] p t76 N82-29904

Nonlinear optimization with linear constraints using a

proiection method

INASA-TP-2086J p 164 N83-10876

Hybnd perturbation/Bubnov-GaJerkin technique for

nonlinear thermal analysis

INASA-TP-2145} p 111 N84-22907

Regions of attraction and ultimate boundedness for

linear quadratic regulators with nonlinearities

INASA-TP-2322} p 181 N84-28538

Nonlinear Structural Analysis

[NASA-CP-2297] p 133 N84-31688

A methodology for airplane parameter estimation and

confidence interval determination in nonlinear estimation

problems

[NASA-RP-t 153} p 56 N86-22579

NONLINEARITY

Flutter analysis of an airplane with multiple structural

nonlinearities in the control system

INASA-TP'1620} p 55 N80-24324

Estimation of wing nonlinear aerodynamic

characteristics at supersonic speeds

[NASA-TP-1718} p 15 N81-10004

A solution procedure for behavior of thick plates On a

nonlinear foundation and postbuckling behavior of long

plates

[NASA-TP-2174) p 132 N83-34373

Development of a simplified procedure for cyclic

structural analysis

INASA-TP-2243} p 133 N84-20878

Nonlinear Constitutive Relations for High Temperature

Application, 1984

|NASA-CP-2369] p 134 N85-31530

NONPOINT SOURCES

Algorithm for astronomical, extended source.

signal-to-noise radio calr.Jlations

[NASA-TP-2396] p 202 N85-12833

NONUNIFORM FLOW

Effect of fuel-air-ratio nonuniformity on emissions of

nitrogen oxides

INASA-TP-1798t p 48 N82-13143

A-83
NONUNIFORMITY SUBJECT INDEX

NONUNIFORMITY

Rainbow Schtieren

[NASA-TP-2t66] p 116 N83-33126

Single scattering from nonspherical Chebyshev

particles: A compendium of calculations

{NASA-RP-11571 p 194 N66-17140

NORMAL DENSITY FUNCTIONS

Gaussian step-pressure loading of rigid viscoplastic

plates

I NASA-TP-1123 ] p t 27 N78-20536

NORTHERN HEMISPHERE

A new NASA/MSFC mission analysis global cloud Cover

data base

I NASA-TP-2448} p 166 N65-21878

NOSE CONES

Sonic-boom minimization wifh nose-bluntness

relaxation

INASA-TP-t348] p 10 N79-15000

Measured and predicted shock shapes and aerodynamic

coefficients for blunted cones at incidence in air at Math

59

{NASA-TP-t6521 p 108 N80-23600

In-flight transition measurement on a 10 dog cone at

Mach numbers from 05 to 20

ENASA-TP-19711 p 19 N82-26227

Laminar heat-transfer distributions on biconics at

incidence in hypersonic-hypervetoclty flows

{NASA-TP-22131 p 112 N85-16065

NOSE FINS

Effects of spanwlse blowing on the surface pressure

distnbutidn and vortex-lift characteristics of a trapezoidal

wing-strake configuration

INASA-TP-1290} p 11 N79-16803

Water-tunnel and analytical investigation of the effect

of strake design variables on strake vortex breakdown

characteristics

INASA-TP-1676] p 15 N80-28304

Experimental and analytical study of the longitudinal

aerodynamic characteristics of analytically and empincally

designed Strake-wing configuratlons at subcrifical

speeds

I NASA-TP-1603} p 17 N8t-25040

NOSE TIPS

Comparison of predicted and experimental real-gas

pressure distributions on space shuttle orbiter nose for

shuttle entry air data system

{NASA-TP-1627] p 14 N60-21280

Cornering characteristics of the nose-gear tire of the

space shuttle orbiter

{NASA-TP-1917] p 130 N82-t0430

NOSE WHEELS

A study of the cornering forces generated by aircraft

tires on a tilted, free-swiveling nose gear

{NASA-TP-2481 I p 135 N86-11522

NOZZLE DESIGN

Investigation of the flow field surrounding circular-arc

boattail nozzles at subsonic speeds

[NASA-TP-16331 p 14 N80-22262

Investigation of convergent-dwergent nozzles applicable

to reduced-power supersonic cruise aircraft

{NASA-TP-t7661 p 16 Nat-14972

Effects of sidewall geometry on the installed

performance of nonaxisymmetric convergent-divergent

exhaust nozzles

{NASA-TP-1771} p 16 N81-15976

Experimental and analytical investigation of

axisymmetric supersonic cruise nozzle geometry at Math

numbers from 0.60 to 130

[NASA-TP-1953} p tg N82-14052

Effects of varying podded nacelle-nozzle idstatlations

on transonic aeropropulslve characteristfcs of a supersonic

fighter aircraft

{NASA-TP-2t201 p 21 N63-26821

Effect of thrust reverser operation on the

lateral-directional characteristics of a three-surface F-15

model st transonic speeds

INASA-TP-2234] p 22 N64-13165

Star 48 solid rocket motor nozzle analyses and

instrumented firings

[NASA-TP-2572] p 68 N86-20460

NOZZLE EFFICIENCY

The effect of throat contouring on two-dimensional

converging-diverging nozzles at statid conditions

[NASA-TP-1704} p 15 N60-29250

NOZZLE FLOW

Mean velocity, turbulence intensity, and scale in a

subsonic turbulent jet impmg_ng normal to a large flat

plate

[NASA-TP-t037} p t04 N77-32431

Workshop on Thrust Augmenting Ejectors

tNASA-CP-20931 p 13 N80-10107

Fuselage and nozzle pressure distributions on a

1 / 12.scale F- 15 propulsion model at transonic speeds ---

conducted in langley 16 foot transonic tunnel

{NASA-TP-1521] p 13 N60-1t036

Investigation of axisymmetric and nonaxisymmetric

nozzles installed on a 0,10 scale F-18 prototype airplane

model --- wind tunnel tests

i NASA-TP-1636 ] p 15 N80-24267

Static internal performance of single expansion-ramp

nozzles with thrust vectoring and reversing

INASA-TP-1962J p 19 N82-20156

Ventun nozzle effects on fuel drop size and nitrogen

oxide emissions

INASA'TP'2028} p 49 N82-31329

Expenmental investigation of two nonaxisymmetric

wedge nozzles at free stream Mach numbers up to 1.20

I NASA-TP-2054J p 20 N62-32322

Pressures measured in flight on the aft fuselage and

external nozzle of a twin-jet fighter

[NASA-TP-2017] p 21 N83-25665

Aeropropulsive characteristics of

nonaxisymmetrie-nozzle thrust reversers at Mach numbers

from 0 to 1.20

[NASA-TP-2306] p 23 N84-24538

Local stability analysis for a planar shock wave

INASA-TP-2387] p 25 N85-12864

Static internal performance of a two-dimensional

convergent nozzle with thrust-vectoring capability up to

60 deg

{NASA-TP-2391 ] p 25 N65-18951

NOZZLE GEOMETRY

Static performance of five twin-engine nonaxisymmetric

nozzles with vectoring and reversing capability

{NASA-TP-1224J p 9 N78-28057

Experimental evaluation of a pilot multinozzle-duct

apparatus

[NASA-TP-1319J p 59 N79-16877

Static test-stand performance of the YF-t02 turbofan

engine with several exhaust configurations for fhe Quiet

Short-Haul Research Aircraft (QSRA)

[NASA-TP-1556} p 45 N60-14121

Investigation of axisymmetric and nonaxisymmetric

nozzles installed on a 0.10 scale F-18 prototype airplane

model --- wind tunnel tests

J NASA-TP-1636 j p 15 N60-24267

Effects of sidewall geometry on the installed

performance of nonaxisymmetric convergent-divergent

exhaust nozzles

JNASA-TP-177t] p 16 N81-15976

Experimental and analytical investigation of

axisymmetric supersonic cruise nozzle geometry at Mach

numbers from 0.60 to 1.30

[NASA-TP-1953] p 19 N82-t4052

Static internal pedormanee of single expansion-ramp

nozzles with thrust vectoring and reversing

[NASA-TP-t962] p 19 N82-20156

Performance characteristics of axisymmetnc

convergent-divergent exhaust nozzles with longitudinal

slots in the divergent

{NASA-TP-20131 p 19 N82-26231

Aeropropulsive characteristics of Mach numbers up to

2.2 of axisymmetric and nonaxisymmetric nozzles installed

on an F-18 model

{NASA-TP-2044J p 20 N62-30291

Effect of nozzle and vertical-tail variables on the

performance of a 3-surtace F-t 5 model at transonic Mach

numbers --- Langley 16 foot transonic tunnel

{NASA-TP-2043] p 20 N82-32320

Experimental investigation of two nonaxisymmetric

wedge nozzles at free stream Mash numbers up to 1.20

INASA-TP-20541 p 20 N62-32322

Perfect bell nozzle parametric and optimization curves

[NASA-RP-1104} p 77 N83-24549

Pressures measured in flight on the aft fuselage and

external nozzle of a twin-jet fighter

{NASA-TP-20t7I p 21 N83-25665

Effect of empennage location on twin-engine

afferbody-nozzle aerodynamic characteristics at Math

Numbers from 0.6 to 1.2 --- wind tunnel tests

INASA-TP-21161 p 21 N83-25666

Static internal performance including thrust vectoring

and reversing of two-dimensional convergent-divergent

nozzles

[NASA-TP-2253] p 23 N84-18165

Aeropropulsive characteristics of

nonaxisymmetric-nozzle thrust reversers at Mach numbers

from 0 to 1.20

[NASA-TP-23061 p 23 N84-24538

Fuselage and nozzle pressure distributions of a

t/12-scale F-15 propulsion model at transonic speeds

Effect of fuselage modifications and nozzle variables

[NASA-TP-23331 p 24 N64-32354

Static internal performance of a single-engine

onaxisymmefrid-nozzte vaned-thrust-reverser design with

thrust modulation capabilities

{NASA-TP-2519) p 27 N86-20348

Static investigation of two STOL nozzle concepts with

pitch thrust-vectoring capability

[NASA-TP-25591 p 28 N86-23559

Static internal pertormance of a thrust vectonng and

reversing two-dimensional convergent-divergent nozzle

with an aft flap

[NASA-TP-25491 p 28 N86-23560

NOZZLE INSERTS

Pocketing mechanics of SRM nozzle liner

[NASA-TP-2577] p 135 N86-23974

NOZZLE THRUST COEFFICIENTS

Aeropropulsive characteristics of twin

single-expansion-ramp vectoring nozzles installed with

forward-swept wings and canards --- transonic tunnel

tests

I NASA-TP-21331 p20 N83-22161

Stalid internal performance of a two-dimensional

convergent nozzle with thrust-vectoring capability up to

60 deg

{NASA-TP-239f ] p 25 N85-18951

Static investigation of two STOL nozzle concepts with

pitch thrust-vectoring capability

[NASA-TP-25591 p 28 N86-23559

NOZZLE WALLS

Effects of sidewall geometry on the installed

performance of nonaxisymmetric convergent-divergent

exhaust nozzles

{NASA-TP-1771 I p 16 N81-15976

NOZZLES

Effects of twin-vertical-tail parameters on twin-engine

afferbody/nozzle aerodynamic characteristics --- Langley

16-ff transonic tunnel tests

[NASA-TP-21581 p 21 N63-24478

NUCLEAR FISSION

Direct nuclear-powered lasers

{NASA-TP-2091 J p tt6 N83-16738

NUCLEAR INTERACTIONS

Heavy-ion total and absorption cross sections above

25 MeV/nucleon

lNASA-TP-2138] p 192 N83-23140

An abrasion-ablation model description of galactic

heavy-ion fragmentation

INASA-TP-2305] p 192 N84-22396

Nineteenth International Cosmic Ray Conference, OG

sessions, volume 3

INASA-CP'2376-VOL-3] p 2t I N65-34662

NUCLEAR PROPULSION

Technology for Bayton-cycle powerpiants using solar

and nuclear energy

INASA'TP-2558] p 78 N86-21577

NUCLEAR PUMPED LASERS

Nuclear-Pumped Lasers --- efficient conversion of

energy liberated in nuclear reactions to coherent

radiation

[NASA-CP-21071 p 117 N80-13438

NUCLEAR REACTIONS

Nuclear-Pumped Lasers --- efficient conversion of

energy liberated in nuclear reactions to coherent

radiation

[NASA-CP-2107] p 117 N80-13438

Tables of nuclear cross sections for galactic cosmic rays:

Absorption cross sections

{ NASA-RP-1134 _ p 193 N85-27665

NUCLEATION

The Soviet-American Conference on Cosmochemistry

of the Moon and Planets, part 2

{NASA-SP-370-PT-2} p 203 N76-12958

Ice crystat growth in a dynamic thermal diffusion

chamber

I NASA-TP-1651 j p 162 N80-23934

The Third International Cloud Condensation Nuclei

Workshop --- conference

INASA-CP-22121 p 116 N82-15383

Calculation of composition distribution ol ultrafine

ion-H20-H2SO4 clusters using a modified binary ion

nucleation theory

INASA-TP-2031] p 150 N82-27867

Simplified free-energy calculation for ion-induced

heteromolecular nucleation

{NASA-TP-2039J p 150 N82-28839

NUCLEI (NUCLEAR PHYSICS)

Ninteenth Internationa_ Cosmic Ray Conference OG

SeSsions. volume 2

{NASA-CP-2376-VOL-2} p 210 N85-34006

Nineteenth International Cosmic Ray Conference. HE

Sessions, volume 6

{NASA-CP-2376-VOL-eJ p 211 N85-35848

Cross section calculations for subthreshold pion

production in peripheral heavy-ion collisions

INASA-TP-2600} p 193 N86-30485

NUCLEON-NUCLEON INTERACTIONS

Second quantization techniques in the scattering of

nonidentical composite bodies

[ NASA-TP-2522} p 193 N66-21297

NUCLEON-NUCLEON SCAI"I"ERING

Heavy-ion total and absorption cross sections above

25 MeV/nucleon

[NASA-TP-2138] p 192 N83-23140

A-84
SUBJECT INDEX OPTICAL HETERODYNING

NUMERICAL ANALYSIS

Future Computer Requirements for Computational

Aerodynamics

[NASA-CP-2032] p 176 N78-19778

A simplified method for calculating the atmospheric

heating rate by absorption of solar radiation in the

stratosphere end mesosphere

[NASA-TP-1398] p 159 N79-16493

A characterization of the real zeros of a particular

transcendental function

[NASA-TP-1420] p 185 N79-18679

Approximation concepts for numerical airfoil

optimization

[NASA-TP-1370] p 1t N79-18915

A critical examination of stresses in an elastic single

lap joint

[NASA-TP-1507) p 128 N79-31626

Measured and predicted shock shapes and aerodynamic

coefficients for blunted cones at incidence in air at Mech

5.9

[NASA-TP-1652] p 108 N80-23600

Flutter analysis of an airplane with multiple structural

nonlinearities in the control system

[NASA-TP-1620] p 55 N80-24324

Calculation of three-dimensional unsteady transonic

flows past helicopter blades

[NASA-TP-1721] p 15 N80-33356

A new look at numerical analyses of free-edge stresses

in composite laminates

[NASA-TP-1751 ] p 130 N81-13373

Pitfalls and guidelines for the numerical evaluation of

moderate-order system frequency response

[NASA-TP-1814] p 72 N81-25138

Time and frequency domain analysis of sampled data

controllers via mixed operation equations

[NASA-TP-1817] p 72 N81-25139

Reduced order feedback control equations for linear time

and frequency domain analysis

{NASA-TP-1818] p 72 N81-25140

Multigrid Methods

[NASA-CP-22021 p 182 N81-33879

Comparison of numerical techniques for integration of

stiff ordinary differential equations arising in combustion

chemistry

|NASA-TP-2372} p 51 N85-10065

NUMERICAL CONTROL

Digital Electronic Engine Control (DEEC) Flight

Evaluation in an F.15 Airplane

[NASA-CP-2298] p 52 N86-25342

NUMERICAL FLOW VISUALIZATION

Future Computer Requirements for Computational

Aerodynamics

[NASA-CP-2032] p 176 N78-19778

Aerodynamic performances of three fan atator designs

operating with rotor having tip speed of 337 meters per

second end pressure ratio of 154. Relation of analytical

code calculations to exponmental performance

[NASA-TP-1614] p 46 N80-21324

WIND: Computer program for calculation of three

dimensional potertfial compressible flow about wind turbine

rotor blades

[NASA-TP-1729J p 15 N80-33357

Steady and nonsteady supersonic turbulent atterbody

flow

[NASA-TP-1769] p 16 N81-16977

Numerical Boundary Condition Procedures

[NASA-CP-2201] p 182 N81-33856

NUMERICAL INTEGRATION

Stability of numerical integration techniques for transient

rotor dynamics

[NASA-TP-t092] p 119 N78-10474

Direct integration of transient rotor dynamics

[NASA-TP-1597] p 46 N80-15128

NUMERICAL STABILITY

Stability of numerical integration techniques for transient

rotor dynamics

[NASA-TP-1092] p 119 N78-10474

NUTATION

An active nutation damper for spacecraft

[NASA-TP-1108] p 65 N78-15143

NUTATION DAMPERS

An active nutation damper for spacecraft

[NASA-TP-1108] p 65 N78-15143

NUTRITION

Food Service and Nutrition for the Space Station

[NASA-CP-2370] p 174 N85-24733

0

O RING SEALS

Damping in tapered annular seals for an incompressible

fluid

[NASA-TP-t646J p 121 N80-19495

O STARS

International Ultraviolet Explorer Atlas of O-typespectra

from 1200 to 1900 angstrom

[NASA-RP-1155 ] p204 N86-25307

OCCULTATION

The Pinhole/Occulter Facility

[ NASA-TP.2168] p 209 N83.25646

Solar Flares and Coronal Physics Using P/OF as a

Research Tool

[NASA-CP-2421 ] p 210 N86-24614

OCEAN COLOR SCANNER

Ocean color algorithm for remote sensing of

chlorophyll

[NASA-TP*2164] p 142 N83-26201

Characteristic vector analysis of inflection ratio spectra:

New technique for analysis of OCean color data

[NASA-TP-2428] p 143 N85-23237

OCEAN CURRENTS

Frontiers of Remote Sensing of the Oceans and

Troposphere from Air and Space Platforms

[NASA-CP-2303] p 142 N84-27262

OCEAN DYNAMICS

Characteristic vector analysis of inflection ratio spectra:

New technique for analysis of ocean color data

[NASA-TP-2428] p 143 N85-23237

OCEAN SURFACE

Quantitative mapping by remote sensing of an ocean

acid-waste dump

[NASA-TP-1275] p 147 N78-33617

Sea-surface temperature and salinity mapping from

remote microwave radiometric measurements of

brightness temperature

[NASA-TP-t077] p 168 N79-28863

NASA Wallops Flight Center GEOS-3 altimeter data

processing report

[NASA-RP-f066J p 139 N81-11438

OCEAN TEMPERATURE

North Atlantic Deep Water Formation

[NASA-CP-2367] p 169 N85-26028

OCEANOGRAPHIC PARAMETERS

Remote sensing of oceanic parameters during the

Skylab/gemefish experiment

[NASA-RP-1012J p 167 N78-12644

Oceanic Lider

[NASA-CP-21941 p 168 N81-31801

Ocean color algorithm for remote sensing of

chlorophyll

[NASA-TP-21641 p 142 N83-26201

OCEANOGRAPHY

The role of satellite altimetry in climate studies

(NASA-TP-1570J p 161 N80-16676

Godderd Laboratory for Atmospheric Sciences,

collected reprints 1978 - 1979, volume 2

[NASA-TP-1788-VOL-2] p 163 N81-21693

Measurements of spectral attenuation coefficients in the

lower Chesapeake Bay

[NASA-TP-2130J p 168 N83-24133

Understanding climate: A strategy for climate modeling

and predictability research, 1985-1995

[NASA-RP-1158] p 166 N86-13866

OCEANS

Laboratory measurements of radiance and reflectance

spectra of dilute secondary-treated sewage sludge

[NASA-TP-1089] p t47 N78-12555

Frontiers of Remote Sensing of the Oceans and

Troposphere from Air and Space Platforms

[NASA-CP-2303] p 142 N84-27262

Global Mega-Geomorphology

[NASA-CP-2312] p 137 N85-32357

Development of UHF radiometer

[NASA-TP-2504] p 103 N86-20678

OCULOMETERS

Analytical techniques of pilot scanning behavior and their

application

[NASA-TP-2525] p 172 N86-27920

OGIVES

Crossflow effects on steady and fluctuating pressures

on an ogive-cylinder cone-frustum model in supersonic

separated flow

[NASA-TP-1951J p 18 N82-13108

OGO

OGO program summary, supplement 1 --- updated

bibliography for all OGO missions and scientific results

from OGO 5 and 6 missions

[NASA-SP-7601-SUPPL-1 ] p 151 N79-13601

OIL ADDITIVES

Auger spectroscopy analysis of lubrication with zinc

dialkyldithiophosphate of several metal combinations in

sliding contact

[NASA-TP-1489} p 92 N79-27308

OILS

Thermal analysis of a planetary transmission with

spherical roller bearings operating after complete loss of

oil

[NASA-TP-2367] p t24 N84-32824

OMNIDIRECTIONAL ANTENNAS

Diversity techniques for omnidirectional telemetry

coverage of the HiMAT research vehicle

[NASA-TP-1830] p 39 N81-20074

ON-LINE PROGRAMMING

Correction factors for on-line microprobe analysis of

muttielement alloy systems

[NASA-RP-1006] p 86 N78.15236

ON-LINE SYSTEMS

NASA Administrative Data Base Management Systems,

1983

[NASA-CP-2304J p 198 N84-21403

NASA Administrative Data Base Management Systems,

1984

[NASA-CP-2323] p 198 N84-33266

New method for determining heats of combustion of

gaseous hydrocarbons

[NASA-TP-2531] p 117 N86-20753

Proceedings of the Second Pilot Climate Data System

Workshop

[NASA-CP-2430] p 137 N86-29282

ONBOARD DATA PROCESSING

High speed lookup table approach to radiornetric

calibration of multispectral image data

[NASA-TP-1741] p 76 N80-33463

A design approach to real-time formatting Of high speed

multispectral image data

[NASA.TP-1870] p 178 N81.25690

Ruggedized minicomputer hardware and software

top=cs, 1981: Proceedings of the 4th ROLM MIL-SPEC

Computer User's Group Conference

{NASA-CP-220E, J p 180 N82-14829

Piloted simulation of an algorithm for onpoard control

of time-optimal intercept

[NASA-TP-2445} p 58 N85-28949

ONBOARD EQUIPMENT

Development of the reentry flight dynamics simulator

for evaluation of space shuttle orbiter entry systems

[NASA-TP-1700] p 71 N80-32429

OPENINGS

An approximate buckling analysis for rectangular

orthotropic plates with centrally located cutouts

[NASA-TP-2528] p 135 N86-20856

OPERATING TEMPERATURE

Turbine Engine Hot Section Technology (HOST)

[NASA-CP-2289] p 135 N86-11495

OPERATIONAL PROBLEMS

The 1980 Aircraft Safety and Operating Problems, part

1

|NASA-CP-2170-PT-t ] p 29 N81-19035

OPERATIONS RESEARCH

Automated decision making and problem solving.

Volume 2: Conference presentations

[NASA-CP-2180-VOL-2] p 184 N81-29902

Automated Decision Making and Problem Solving.

Volume 1: Executive Summary

[NASA-CP.2180-VOL-t ] p 184 N81-30889

OPERATOR PERFORMANCE

The 14th Annual Conference on Manual Control --- digital

simulation of human operator dynamics

[NASA-CP-2060J p 173 N79-15588

Models of human operators in vision dependent tasks

[NASA-CP-2103) p 171 N79-33838

OPTICAL ACTIVITY

Holography through optically active windows

[NASA-TP-1414J p 114 N79-17195

OPTICAL DATA PROCESSING

Optical and holographic storage properties of F3, Cu,

and Mg-doped lithium niobste

[NASA-TP-t 144 ] p 193 N78-20948

Optical Information Processing for Aerospace

Applications

[NASA-CP-2207] p 194 N82-15894

Optical Information Processing for Aerospace

Applications 2

JNASA-CP-2302] p 194 N84-22402

OPTICAL DENSITY

SAM 2 measurements of the polar stratospheric aerosol,

volume 5

[NASA-RP-1140] p 155 N85-25970

SAM 2 measurements of the polar stratospheric aerosol,

volume 2

INASA-RP-1164] p 157 N86-28562

SAM 2 measurements of the polar stratosphenc aerosol,

volume 8

[NASA-RP-1165] p 157 N86-29428

OPTICAL EQUIPMENT

Design and analysis of a torsion braid pendulum

displacement transducer

[NASA-TP-1840] p 115 N81-25352

OPTICAL HETERODYNING

Simulated electronic heterodyne recording and

processing of pulsed-laser holograms

[NASA-TP-1444] p 114 N79-21329

A-85
OPTICAL MEASUREMENT SUBJECT INDEX

Heterodyne systems end technology, part 1 ---

conferences

{NASA-CP-2138-PT-1 } p 117 N80.29652

Heterodyne Systems end Technology, part 2

[NASA-CP.2138-PT-2] p 117 N80-29672

Spatial frequency response of an optical heterodyne

recewer

{NASA-TP-1763] p 194 N81-13739

Excess noise in tunable diode lasers

[NASA-TP-fg35] p 117 N82-12431

OPTICAL MEASUREMENT

Astronomical M_crodensitometry Conference

{NASA-CP-2317} p 116 N84-28020

OPTICAL MEASURING INSTRUMENTS

An optical profitometer for spatial characterization of

three-dimensional suffices

{NASA-TP-1012} p 113 N77-32458

Investigation of light scattering as a technique for

detecting discrete soot particles in • luminous flame

[NASA-TP-1235} p 193 N78-27906

Optically isolated logarithmic nanoemmeter capable of

floating to 5 kilovolts

INASA-TP-1527J p 101 N79.32467

Preliminary applications and evaluation results.

Lixiscope: Proceedings of the Lixiecope Conference

[NASA-CP-2112] p 114 N80-12384

Development of e simplified optical technique for the

simultaneous measurement of particle size distribution end

velocity

[NASA-TP-2185] p 194 N83-27846

OPTICAL PROPERTIES

Atmospheric aerosols: Their Optical Properties and

Effects

tNASA-CP-2004] p 151 N77-15563

Atmospheric aerosols: Their Optical Properties end

Effects (supplement)

{ NASA-CP-2004-SUPPL ] p t 51 N77-15564

Laboratory measurements of physical, chemical, end

optical characteristics of Lake Chioot sediment waters

{NASA-TP-1941 ] p 140 N82-t3468

OPTICAL RADAR

A comparative study of optimum and suboptimum

direct-detection laser ranging receNers

[NASA-TP-1315] p 117 N78-31413

Lider beckscettering measurements of background

stratospheric aerosols

{ NASA-TP-1381 ) p 152 N79-17388

Shuttle atmospheric Iidar research program

{NASA-SP-433] p 117 N80-11414

Exploratory Meeting on Airborne Doppler Lidar Wind

Velocity Measurements

4 NASA-CP-2140] p 162 NS0-2699g

NASA/MSFC FY-80 Atmosphenc Processes Research

Review

INASA-CP-2145} p t53 N80-289,65

DIAL with heterodyne detection including speckle noise:

Aircraft/shuttle measurements of 03, H20, end NH3 with

pulsed tunable CO2 lasers

iNASA-TP-1725} p 115 N80-30717

Oceanic Lidar

INASA-CP-2194] p 168 N81-31801

Abstracts of papers presented at the Eleventh

international Laser Radar Conference

iNASA-CP-2228] p 115 N82-27706

NASA/MSFC FY-84 Atmospheric Processes Research

Review

I NASA-CP-2329] p 166 N84-34829

Airborne lidar measurements of El Chichon stratosphehc

aerosols, October 1982 to November 1982

[NASA-RP-1136} p 155 N85-19550

Airborne lidar measurements of El Chichon stratospheric

aerosols

[NASA-RP-1148] p 155 N86-13850

Airborne Lidar measurements of aerosols, mixed layer

heights, and ozone during the 1980 PEPE/NEROS summer

field experiment

[NASA-RP-1143] p 150 N86-f6748

Airborne lider measurements of El Chichon stretoshperic

aerosols

INASA-RP-1166] p 186 N86-27835

OPTICAL REFLECTION

A tutorial solution to scattering of radiation in a thin

atmosphere bounded below by a diffusely reflecting,

absorbing surface

I NASA-TP-2077 ] p 154 N82-33918

OPTICAL SCANNERS

Astronomical Microdensitometry Conference

[NASA-CP-2317] p 116 N84-28020

OPTICAL TRACKING

Free Drifting Buoys

iNASA-CP-20031 p 167 N77-16675

OPTICAL TRANSFER FUNCTION

Spahal frequency response of an optical heterodyne

receiver

[NASA-TP-1763] p 194 N81-t3739

OPTICAL WAVEGUIDES

Optical Information Processing for Aerospace

Applications

[NASA-CP-2207} p 194 N82-15894

OPTICS

Performance analysis of grazing incidence imaging

systems --- X ray telescope aberrations

[NASA-TP-f088] p 193 N78-11812

OPTIMAL CONTROL

ORACLS: A system for linear-quadratic-Gaussian

control law design

[NASA-TP-1106} p 181 N78-22809

Generation of linear dynamic models from • digital

nonlinear simulation

[NASA-TP-1388} p 2 N79-t6796

Approximation concepts for numerical airfoil

optimization

{NASA-TP-1370} p 11 N79-18915

A method for obtaining practical flutter-suppression

control laws using results of optimal control theory

[NASA-TP-1471 ] p 128 N79-28614

Application of two design methods for active flutter

suppression and wind-tunnel test results

[NASA-TP-1653] p 129 N80-22737

Realizable optimal control for a remotely piloted research

vehicle --- stabdity augmentation

{NASA-TP-1654] p t81 N80-25039

An application of multivariable design techniques to the

control of the national transonic facility

INASA-TP-1887} p 181 N81-29840

An algorithm for minimum-cost set-point ordering in a

cryogenic wind tunnel

INASA-TP-1923] p 59 N82-11090

Modeling, Analysis, and Optimization Issues for Large

Space Structures

[NASA-CP-2258J p 66 N83-t8819

Decoupled control anatysis of a large flexible space

antenna with linear quadratic regulator comparisons

[NASA-TP-2293} p 74 N84-23675

Regions of attraction and ultimate boundedness for

linear quadratic regulators with nonlinearities

[NASA-TP-2322] p 181 N84-28538

Total energy-rate feedback for automatic glide-slope

tracking during wind-shear penetration

[NASA-TP-24121 p 58 N85-23801

OPTIMIZATION

An integrated computer procedure for sizing composite

airframe structures

[NASA-TP-1300J p 178 N79-17580

Wind-tunnel investigation of the validity of a

sonic-boom-minimization concept --- Langley Unitary Plan

Wind Tunnel tests for supersonic transport design

[NASA-TP-t421 } p 12 N80-10102

Economic evaluation of flying-qualities design criteria for

a transport configured with relaxed stebc stability

[NASA-TP-1760] p 56 N81-13968

Use Of constrained optimization in the conceptual design

of a medium-range subsonic transport

[NASA-TP-1762} p 35 N81-16039

A method for obtaining reduced-order control laws for

high-order systems using optimization techniques

[NASA-TP-1876] p t8t N81-30851

Circumferentially segmented duct lines optimized for

axisymmetric and standing wave sources --- reducing noise

from turbofan engines gaterkin method acoustic

attenuation

[NASA-TP-20751 p 188 N82-34190

Nonlinear optimization with linear constraints using a

projection method

[NASA-TP-2086] p 184 N83-10876

An algonthm for maximum likelihood estimation using

an efficient method for approximating sensitivities

[ NASA-TP-2311 ] p 58 N84-25717

Reduction method for thermal analysis of complex

aerospace structures

[NASA-TP-2373J p 112 N85-16066

Identification of dynamic systems, theory and

formulation

{NASA-RP-t138J p 185 N85-19784

Relative control effectiveness technique with application

to airplane control coordination

[NASA-TP-2416} p 37 N85-23753

A method to stabilize linear systems using eigenvalue

gradient information

[NASA-TP-2479J p 181 N86-13946

A methodology for airplane parameter estimation and

confidence interval determination in nonlinear estimation

problems

{ NASA-RP-1153 ] p 58 N86-22579

ORBIT CALCULATION

An introduction to orbit dynamics and its application 1o

satellite-based earth monitoring systems

I NASA-RP-10091 p64 N78-12113

Flight Mechanics/Estimation Theory Symposium

INASA-CP-21231 p 64 N80-28389

Fifth Annual Flighl Mechanics/Estimation Theory

Symposium

[NASA-CP-2152} p 64 N81-11070

Flight Mechanics/Estimation Theory Symposium

{NASA-CP-2002] p 61 N78-76855

ORBIT DECAY

Orbital Debris

[NASA-CP-2360] p 63 N85-21188

ORBIT TRANSFER VEHICLES

Performance requirements analysis for payload delivery

from • space station

[NASA-RP-f 110] p67 N83-32828

OTV Propulsion Issues

[NASA-CP-2347} p 67 N85-16989

Orbital Debris

{NASA-CP-2360] p 63 N85-21188

ORBITAL ASSEMBLY

Large Space Systems Technology, volume 1

[NASA-CP-2035-VOL-1} p 65 N79-10078

Large Space Systems Technology, 1979 --- antenna and

space platform systems conference

[NASA.CP.2t 18} p66 N80-19145

The 1980 Large space systems technology. Volume

2: Base technology

[NASA-CP-2168-VOL-2] p 66 N81-19196

EVA assembly of large space structure element

[NASA-TP-1872} p 62 N81-26160

Performance requirements analysis for payload delivery

from a space station

[NASA-RP-11 t0} p67 N83-32828

Swing-arm beam erector (SABER) concept for single

astronaut assembly of space structure

[NASA-TP-2379] p 7.5 N85-t9015

ORBITAL LAUNCHING

Performance requirements analysis for payload delivery

from a space station

[NASA-RP-t110} p 67 N83-32828

ORBITAL MECHANICS

Flight Mechanics/Estimation Theory Symposium

[NASA-CP-2050] p 64 N79-14121

Flight Mechanics/Estimation Theory Symposium --- with

application 10 autonomous navigation and attitude/odmt

determination

[NASA-CP-2082] p 64 N79-26082

Flight Mechanics/Estimation Theory Symposium

fNASA-CP-2123] p 64 N80-28389

Sixth Annual Flight Mechanics/Estimation Theory

Symposium

[NASA-CP-2205] p 62 N82-10064

Radiometer requirements for Earth-observation systems

using large space antennas

INASA-RP-1101} p t16 N83-28410

Orbital Debris

[NASA-CP-2360} p 63 N85-21188

ORBITAL POSITION ESTIMATION

Flight Mechanics/Estimation Theory Symposium

[NASA-CP-2050} p 64 N79-1412t

Flight Mechanics/Estimation Theory Symposium --- with

application to autonomous navigation and attitude/orbit

determination

{NASA-CP-2082] p 64 N79-26082

Flight Mechanics/Estimation Theory Symposium

[NASA-CP-2123] p 64 N80-28389

Sixth Annual Flight Mechanics/Estimation Theory

Symposium

[NASA-CP-2205] p 62 N82-10064

Flight Mechanics/Estimation Theory Symposium

[NASA-CP-2002] p 61 N78-76855

ORBITAL SERVICING

Applications of Tethers in Space, volume 1

{NASA-CP-2364J p 125 N85-20339

Orbital Debris

[NASA-CP-2360] p 63 N85-21188

Solar Terrestrial Observatory Space Station Workshop

Report

[NASA-CP-2411} p 76 N86-19349

ORBITAL SPACE STATIONS

Interactive design and analysis of future large spacecraft

concepts

{NASA-TP-1937] p 72 N82-14276

Space Station Software Issues

I NASA-CP-23611 p 179 N85-20689

Space Station Planetology Experiments (SSPEX)

INASA-CP-2424] p 201 N86-27t36

ORCHARDS

Aerial color infrared photography: Applications in

citnculture --- Flonda

INASA-RP-1067] p 139 N81-21437

ORGANIC COMPOUNDS

Control of volume resistivity in Inorganqc organic

separators

[NASA-TP-1439J p 84 N79-22246

Improved, low cost inorganic-organic separators for

rechargeabie silver-zinc baffenes

[NASA-TP-1476J p 84 N79-25181

A-86
SUBJECT INDEX

ORGANIC MATERIALS

Literature review of organic matter transport from

marshes

[E83-10352] p 142 N83-29750

ORGANIC SULFUR COMPOUNDS

Solubility, stability, and electrochemical studies of

sulfur-sulfide solutions in organic solvents

[NASA-TP-f245] p 144 N76-26624

ORGANIZATIONS

Model research: The National Advisory Committee for

Aeronautics, 1915-1958, volume 1

[NASA-SP-4103.VOL-t ] p 4 N85-23683

Model research, the National Advisory Committee for

Aeronautics, 1915-1958, volume 2

[NASA-SP-4103-VOL-2] p 4 N85-23684

ORGANOMETALLIC COMPOUNDS

Effectiveness of various organometallics as ant!wear

additives in mineral oil

[NASA-TP-1096] p 91 N78-12222

ORIFICE FLOW

Use of nose cap and fuselage pressure orifices for

determination of air data for space shuttle orbiter below

supersonic speeds

[NASA-TP-1643] p 39 N80-32389

Oepresaurization and two-phase flow of water containing

high levels of dissolved nitrogen gas

[NASA-TP-1839] p 109 N81-28389

Flow through aligned sequential orifice type inlets

[NASA.TP.1967] p 109 N82.20467

Flow rate and pressure profiles for 1 to 4 axially alined

orifice inlets

[NASA-TP-2460] p 1t2 N85-27165

ORIFICES

Wind tunnet investigation of an all flush orifice air data

system for a large subsonic aircraft --- conducted in a

Langley 8 foot transonic pressure tunnel

[NASA-TP-t642] p 38 N80-23304

Subsonic tests of an all-flush-pressure-orifice air data

system

[NASA-TP-1871] p 39 N81-26144

Flow rate and pressure profiles for 1 to 4 axially alined

orifice inlets

[NASA-TP-2460} p 112 N85-27165

Orifice-induced pressure error studies in Langley 7- by

10-foot high-speed tunnel

[NASA-TP-2545] p 27 N86-20347

The application to airfoils of a technique for reducing

orifice-induced pressure error at high Reynolds numbers

[NASA-TP-2537J p 27 N86-20351

OROGRAPHY

Current Scientific Issues in Large Scale Atmospheric

Dynamics

[NASA-CP-2410] p 167 N86-24082

ORTNOGONALITY

Application of a numerically generated orthogonal

coordinate system to the solution of inviscid axisymmetric

supersonic flow over blunt bodies

[NASA-TP-1619] p 14 N80-19031

ORTHOTROPIC PLATES

Stress-concentration factors for finite orthotropic

laminates with a circular hole and uniaxial loading

[NASA-TP-1469J p 80 N79-23140

A cracked orthotropic sheet stiffened by a semi-infinite

orthotropic sheet

[NASA-TP-2455] p 134 N85-32339

An approximate buckling analysis for rectangular

orthotropic plates with centrally located cutouts

[NASA-TP-25281 p 135 N86-20856

ORTHOTROPISM

Stress-concentration factors for finite orthotropic

laminates with a pin-loaded hole

[NASA-TP-1862] p 81 N81-24178

OSCILLATION DAMPERS

Off-design correlation for losses due to part-span

dampers on transonic rotors

[NASA-TP-1693] p 47 N80-28352

Measurement of rolling friction by a. damped oscillator

[NASA-TP-2257] p 123 N84-13577

OSCILLATIONS

Phugoid characteristics of a YF-12 airplane with

variable-geometry inlets obtained in flight tests at a Mach

number of 2.9

[NASA-TP-1107J p 52 N78-12100

Simulator study of conventional general aviation

instrument displays in path-following tasks with emphasis

on pilot-induced oscillations

[NASA-TP-1776] p 39 N81-14997

influence of display and control compatibility on

pilot-induced oscillations

[NASA-TP-t936J p 172 N82-14804

Flow in a torsionally oscillating filled cylinder

[NASA-TP-2115] p 110 N83-16674

El Nino and outgoing Iongwave radiation: An atlas of

Nimbus-7 Earth radiation budget obse_ations

[NASA-RP-1163] p 157 N86-29425

OSCILLATORS

Submitlimeter local oscillators for spaceborne

heterodyne applications

[NASA-RP-t147] p 76 N85-30005

OUTER PLANETS EXPLORERS

Voyager to Jupiter and Saturn

[NASA-SP-420] p 205 N77-29046

OUTGASSING

Evaluation of materials for high performance solar

arrays

[NASA.TP-122OJ p 92 N78-22233

Outgassing data for spacecraft materials

[NASA-RP-1061 ] p 80 N80-30441

Effect of vacuum processing on outgassing within an

orbiting molecular shield

[NASA-TP-1980J p 99 N82-19390

Outgassing data for selecting spacecraft materials

[NASA-RP-1124] p 82 N84-26751

OUTLET FLOW

Contoured tank outlets for draining of cylindrical tanks

in idw-gravity environment --- Lewis Research Center Zero

Gravity Facility

[NASA.TP.1492] p 107 N79-29467

OVERFRESSURE

Wind-tunnel investigation of the validity of a

sonic-boom-minimization concept --- Langley Unitary Plan

Wind Tunnel tests for supersonic transport design

[NASA-TP.1421] p 12 N80-10102

Charts for determining potential minimum sonic-boom

overpressures for supersonic cruise aircraft

[NASA-TP-1820] p 17 Nat-2t016

OXIDATION

Chemical kinetic modeling of benzene and toluene

oxidation behind shock waves

[NASA-TP-1472J p 84 N79.28259

Thermal and oxidative degradation studies of formulated

C.ethers by get-permeation chromatography

{NASA-TP-1994] p 94 N82-21332

Carbon-catalyzed oxidation of SO2 by NO2 and air

I NASA-TP-2014J p 85 N82-22330

Effects of chromium and aluminum on mechanical and

oxidation properties of iron-nickel-base superalloys based

on CG-27

[NASA-TP-2443] p 90 N85-21323

Fuel-rich catalytic combustion: A soot-free technique

for in situ hydrogen-like enrichment

[NASA-TP-2498] p 85 N85-31244

Oxidation and emittance of superalloys in heat shield

applications

J NASA-TP-2578 j p 90 N86-26412

Thermal-fatigue and oxidation resistance of

cobaR-modified Udimet 700 alloy

[NASA-TP-2591 ] p 135 N86-28464

OXIDATION RESISTANCE

Modules of rupture and oxidation resistance of

$1255AI0.600 72N3 52 sialon

INASA-TP-14901 p 93 N79-27309

OXIDE FILMS

Oxidation and emittance of superalloys in heat shield

applications

[NASA-TP-25781 p 90 N86-26412

OXIDES

Friction and wear of polyethylene oxide polymer having

a range of molecular weights

{NASA-TP-1129] p 91 N78-15278

OXYGEN

Thermodynamic and related properties of oxygen from

the triple point to 300 K at pressures to 1000 bar

INASA-RP-10t 11 p84 N78-t611g

Effect of oxygen and nitrogen interactions on fdction

of single-crysta_ silicon carbide

|NASA-TP-1265J p 92 N78-28247

Effect of oxygen, methyi mercaptan, and methyl chloride

on friction behavior of copper-iron contacts

[NASA-TP-1309J p 86 N78-30206

Effect of oxygen-nitrogen ratio on sinterability of

Siatons

[NASA-TP-1382J p 92 N79-2t204

Surface chemistry of iron sliding in air and nitrogen

lubricated with hexadecane and hexadecane containing

dibenzyl-dilsulfide

INASA-TP-1545] p 79 N79-31346

ignition of SiH4-H2-O2-N2 behind reflected shock

waves

INASA-TP-2114] p 50 N93-18727

Transport properties of oxygen

[NASA-RP-1102] p 110 N83-24800

Proposed fast-response oxygen monitoring and control

system for lhe Langley 8-foot high-temperature tunnel

INASA-TP-22181 p 116 N84-11460

OXYGEN SUPPLY EQUIPMENT

Design guide for high pressure oxygen systems

[ NASA-RP-11131 p 99 N83-32990

OZONE

Chlorofluoromethanes and the stratosphere

[NASA-RP-t010] p 151 N77-31694

OZONOSPHERE

Effect of trichlorofluoromathane and molecular chlorine

on ozone formation by simulated solar radiation

[NASA-TP-1093] p 84 N78-12167

Effect of nitric oxide on photochemical ozone formation

in mixtures of air with molecular chlorine and with

tdchlorofluoromethane

[NASA-TP-t 192] p 84 N78-20281

An evaluation of in situ Ozone sensor performance during

a cold frontal passage

[NASA-TP-1239] p 158 N78-27706

An assessment of the effect of supersonic aircraft

operations on the stratospheric ozone content

[NASA-RP.1026] p 159 N78-30774

Ozone Contamination in Aircraft Cabins

[NASA-CP.2066] p 29 N79.21021

Ozone measurement system for NASA global air

sampling program

[NASA-TP-1451 ] p 148 N79-22654

Procedures for estimating the frequency of commercial

airline flights encountering high cabin ozone levels

[NASA-TP.1560] p 2g N79.33171

The stratosphere: Present and future

[NASA-RP-1049] p 181 N80-14641

The stratcom 8 effort --- stratospheric photochemistry

[NASA-TP-1640] p 161 N80-22924

DIAL with heterodyna detection including speckle noise:

Aircraft/ahu_e measurements of 03, H20, and NH3 with

pulsed tunable CO2 lasers

[NASA-TP-1725] p 115 N80-30717

Two-dimensional model studies of the effect of

supersonic aircraft operations on the stratosphenc ozone

content

{NASA-RP-1064] p 149 N51-17622

SAM 2 measurements of the polar stratospheric aerosol,

volume 1: October to April 1979

[NASA-RP-1081] p 153 N82-13592

User's guide for the Total-Ozone Mapping Spectrometer

(TOMS) instrument first year ozone T data set

[NASA.RP-1096] p 164 N82-28880

Ozone climatology series, Volume 1: Atlas of total

ozone, April 1970- December 1976

[NASA-RP-1098] p 154 N83-16992

User's guide for the Solar Beckscaffered Ultraviolet

(SBUV) and the Total Ozone Mapping Spectrometer

(TOMS) RUT-S and RUT.T data sets: October 31, 1978

to November 1, 1980

[NASA-RP-1112] p 165 N83-28828

User's guide for SBUV/TOMS ozone derivative

products

[NASA-RP-1116] p 165 N84-16720

Climatology of ozone at altitudes from 19,000 at 59,000

feet based on combined GASP and ozonesonde data

[NASA-TP-2303] p 166 N84-31865

Ozone Correlative Measurements Workshop

{NASA-CP-2362] p 137 N85-23112

SAGE aerosol measurements Volume 1: February 21,

1979 to December 31, 1979

[NASA-RP-1144] p 155 N86-11700

Airborne Lidar measurements of aerosols, mixed layer

heights, and ozone during the 1980 PEPE/NEROS summer

field experiment

[NASA-RP-1143] p t50 N86-16748

SAGE Aerosol Measurements, Volume 2:1 January

31 December 1980

INASA-RP-1149] p 156 N86-23088

Present state of knowledge of the upper atmosphere:

An assessment report; processes that controt ozone and

other climatically important trace gases

[NASA-RP-1162] p 156 N86-25911

OZONE FLUORIDE

Effect of trichlorofluoromethane and molecular chlorine

on ozone formation by simulated solar radiation

[NASA-TP-1093] p 84 N78-12167

OZONOMETRY

Total ozone measurement: Intercomparison of

prototype New Zealand filter instrument and Dobson

spectropbotometer

INASA-TP-t277] p 114 N78-28412

Ozone concentration in the cabin of a Gates Leaflet

measured simultaneously with atmospheric ozone

concentrations

[NASA-TP-1340] p 148 N78-33618

Analysis of atmospheric ozone levels at commercial

airplane cruise altitudes in winter and spring, 1976 - 1977

--- Global Atmospheric Sampling Program

[NASA-TP-1807] p t63 N81-21685

User's guide for the Solar Backscaffered Ultraviolet

(SBUV) instrument first year ozone-S data set

[NASA-RP-1095] p 164 N82-29826

OZONOSPHERE

Ozone Trend Detectability

[NASA-CP-2189J p 153 N82-10624

A-87
P-531 HELICOPTER

P

P-531 HELICOPTER

Wind-tunnel evaluation of • 21-percent-scale powered

model of a prototype advanced scout helicopter

[NASA-TP.2420] p 26 N85-28923

PACIFIC OCEAN

Satellite-derived global oceanic rainfall atlas (1973 and

1974)

INASA.SP.410] p 157 N77-19709

PAD

Effect of strain isolator pad modulus on inplane strain

in Shuttle Orbiter thermal protection system tiles

INASA-TP-21411 p 132 N83-33216

PADE APPROXIMATION

An analytical technique for approximating unsleedy

aerodynamics in the time domain

{NASA-TP-1738t p 130 Nat-It422

PALEONTOLOGY

Global Mega-Geomorphoiogy

INASA.CP.2312] p 137 N85-32357

PANEL METHOD (FLUID DYNAMICS)

Development end validation of a combined rotor

fuselage induced flow field computational method ---

Langley V/STOL tunnel

[NASA-TP-16561 p 15 N80-25296

PANELS

Effects of fabrication and joining processes on

compressive strength of boron/aluminum and

borsic/aluminum structural panels

(NASA-TP-1121 ] p 80 N78-20256

Noise transmission toss of aircraft panels using acoustic

intensity methods

[NASA-TP-2046] p 188 N82-31069

Flightweight radiantly and actively cooled panel:

Thermal and structural performance

INASA.TP.2074] p 131 N83-tt513

A new measurement method for separating airborne and

structureborne noise radiated by aircraft type panels

[NASA-TP-2079] p 189 N83-11838

Buckling and failure characteristics of graphite-polyimide

shear panels

[NASA-TP-21531 p 82 N83-24561

Fabrication and evaluation of cold/formed/weldbrazed

beta-titanium skin-stiffened compression panels

[NASA-TP-2201 ] p 89 N83-35100

Buckling loads of stiffened panels subjected to combined

longitudinal compression and shear: Results obtained with

PASCO, EAL, and STAGS computer programs

[NASA-TP-22151 p 132 N84-16585

Structural efficiency studies of corrugated compress_n

panels with curved caps and beaded webs

INASA-TP-2272J p 132 N84-18675

Long-term thermal aging of 2 graphite-polyfmide

composite materiels

[NASA-TP-2369) p 83 N85-12094

Joint design for improved fatigue life of diffuscon-bonded

box-stiffened panels

INASA-TP-24801 p 135 N85-33537

Abrasion behavior of aluminum and composite skin

COupons, stiffened skins and stiffened panels

representative of transport sirpisne structures

[NASA-TP-2520] p 38 N86-133t6

Fabrication and evaluation of superplastically

formed/weld-brazed corrugated compression panels with

beaded webs

[NASA-TP-25121 p 90 N86-13406

PARABOLIC DIFFERENTIAL EQUATIONS

Application of • two-dimensional parabolic computer

program to prediction of turbulent reacting flows

[NASA-TP-t169J p 105 N78-20463

Critical study of higher order numerical methods for

SOlving the boundary-layer equations

NASA-TP-1302] p 106 N79-13305

PARABOLIC REFLECTORS

Design and fabrication of a tow-specific-weight parabolic

dish solar concentrator

NASA-TP-1152] p 75 N78-17145

PARABOLOID MIRRORS

Large-aperture interferometer using local reference

beam

NASA-TP-20601 p 194 N83-13979

PARAFFINS

A desKJn handbook for phase change thermal control

and energy storage devices -- selected paraffins

NASA-TP-t0741 p 104 N78-15434

PARALLEL PROCESSING (COMPUTERS)

Parallel, Asynchronous Execuhve (PAX): System

concepts, facilities, and architecture

NASA-TP-21791 p 180 N83-28921

PARAMETER IDENTIFICATION

User's manual for MMLE3, a general FORTRAN program

for maximum likelihood parameter estimation

NASA-TP-t563J p 176 N81-12744

Parametric study of microwave-powered high-attitude

airplane platforms designed for linear flight

INASA-TP-1918] p 35 N82-t1050

Analysis end Monte Carlo simulation of near-terminal

aircraft flight paths

INASA-TP-19971 p 31 N82-23233

The applicat_n of parameter estimation to flight

measurements to obtain lateral-directional stability

derivatives of an augmented jet-flap STOL airplane

[NASA-TP-2033J p 57 N83-16350

An algorithm for maximum likelihood estimation using

an efficient method for approximating sensitivities

INASA-TP-2311 J p 58 N84-25717

Identification of dynamic systems, theory and

formulation

INASA-RP-1138} p 185 N85-19784

A methodology for airplane parameter estimation and

confidence interval determination in nonl4near estimation

problems

[ NASA-RP-1153] p 58 N86-22579

PARAMETERIZATION

Effects of control inputs on the estimation of stability

and control parameters of a light airplane

[NASA-TP-10431 p 53 N78-13071

Parameter estimation applied to Nimbus 6 w=de-angle

Iongwave radiation measurements

[NASA-TP-1307] p 159 N79-13644

Similrlude requirements and scaling relationships as

apphed to model testing

I NASA-TP-1435 J p33 N79-30176

Inclusion of unsleady aerodynamics in longitudinal

parameter estimation from flight data --- use of vortices

and mathematical models for parameterization from flight

characteristics

[NASA-TP-1536) p 13 N80-12995

Economic evaluation of flying-qualities design criteria for

a transport configured with relaxed static stability

INASA-TP-17601 p 56 N81-13968

PARTIAL DIFFERENTIAL EQUATIONS

Numerical grid generation techniques ---conference

(NASA-CP-2166] p 182 N81-14690

Multigrid Methods

[ NASA-CP-22021 p 182 N81-33879

Solution of si]iptic partial differential equations by fast

Poisson solvers using a local relaxation factor. 1 : One-step

method

I NASA-TP-2529 ] p 183 N86-28661

PARTICLE ACCELERATION

Solar Terrestrial Physics: Present and Future

(NASA-RP-1120 ] p 200 N84-34332

Ninteenth International Cosmic Ray Conference, SH

sessions, volume 4

{NASA-CP-2376-VOL-4] p 210 N85-34729

Nineteenth International Cosmic Ray Conference. OG

sessions, volume 3

[NASA-CP-2376-VOL-3_ p 211 N85-34862

PARTICLE COLLISIONS

Tables of nuclear cross sections for galactic cosmic rays:

Absorption cross sections

[NASA-RP-1134] p 193 N85-27665

Cross section calculations for subthreshold pion

production in peripheral heavy-ion collisions

I NASA-TP-2600] p 193 N86-30485

PARTICLE DENSITY (CONCENTRATION)

Cloud-encounter and particle-concentration variabilities

from GASP data

[NASA-TP-t8861 p 164 N82-15677

Wind Tunnel Seeding Systems for Laser Velocimeters

[NASA-CP-2393J p 116 N86-11437

PARTICLE INTERACTIONS

Spacecraff Charging Technology, t 978

[NASA-CP-2071 ] p 71 N79-24001

Nineteenth International Cosmic Ray Conference HE

Sessions, volume 6

INASA-CP-2376-VOL-61 p 2tl N85-35848

PARTICLE LADEN JETS

Morphology of an aluminum alloy eroded by a jet of

angular parbcles impinging at normal incidence

lNASA-TP-21391 p 89 N83-24641

PARTICLE MOTION

Three-dimensional relativistic fioId-electron interaction

in a mutticavity high-power klystron 1: Basic theory

INASA-TP-1992] p 102 N82-22439

PARTICLE PRODUCTION

Nineteenth International Cosmic Ray Conference HE

Sessions, volume 6

l NASA-CP-2376-VOL-6] p 211 N85-35848

PARTICLE SIZE DISTRIBUTION

The Third International Cloud Condensation Nuclei

Workshop --- conference

[NASA-CP-2212} p 115 N82-15383

Particle sizing by measurement of forward-scattered light

at two angles

[NASA-TP-21561 p 50 N83-24509

SUBJECT INDEX

Development of a simplified optical technique for the

simultaneous measurement of particle size distribution and

velocity

[NASA-TP-2185] p 194 N83-27846

Wind Tunnel Seeding Systems for Laser Veiocimeters

INASA-CP-23931 p 116 N86-11437

Performance test of laser veiocimeter system for the

Langley 16-Ioot transonic tunnel

[NASA-TP-25021 p 118 N86-16563

Single scattering from nonsphencal Chebyshev

particles: A compendium of calculations

INASA-RP-1157] p 194 N86-17140

PARTICLE TRAJECTORIES

A stochastic model for particle impingements on orbiting

spacecraft

(NASA-TP-2550] p 184 N86-t9095

PARTICLES

Space Station Planetology Experiments (SSPEX)

[NASA-CP-2424] p 201 N86-27136

PARTICULATE SAMPLING

Fuel-rich catalytic combustion: A soot-free technique

for in situ hydrogen-like enrichment

[NASA-TP-2498] p 85 N85-31244

PARTICULATES

Enhanced hydrophilicity of chlonded aluminum oxide

particulates

{ NASA-TP-13121 p84 N79-12178

PASSAGEWAYS

Film-cooling effectiveness with developing coolant flow

through straight and curved tubular passages

[ NASA-TP-2062 ] p 110 N83-12360

Review and status of heat-transfer technology for

internal passages of sir-cooled turbine blades

I NASA-TP-2232 j p 111 N84-21828

Vortex-generating coolant-flow-passage design for

increased film-cooling effectiveness and surface

coverage

[NASA-TP-23881 p 112 N85-12314

PASSENGER AIRCRAFT

Implications of fuel-efficient vehicles on ride quality and

passenger acceptance: Workshop proceedings

INASA-CP-2096J p 199 N80-18990

Small transport aircraft technology

[NASA-SP-4601 p 36 N83-20931

PASSENGERS

Effect of vibration duration on human discomfort ---

passenger comfort and random vibration

INASA-TP-1283] p 171 N78-32717

PATENT POLICY

Significant NASA inventions available for licensing in

foreign countries

{NASA-SP-7038(08) J p 198 N86-26243

NASA patent abstracts bibliography: A continuing

bibliography Section 1: Abstracts

[NASA-SP-7039(29)-SECT-t ] p 198 N86-28788

NASA Patent Abstracts Bibliography A continuing

bibliography Section 2: Indexes (Supplement 29)

[NASA-SP-7039(29)-SECT-2] p 198 N86-28789

PATTERN RECOGNITION

Marking parts to aid robot vision

{NASA-TP-1819] p 176 N81-21775

PATTERN REGISTRATION

Synthetic aperture rsdar/LANDSAT MSS image

registration

INASA-RP-'I039] p 139 N80-16405

PAULI EXCLUSION PRINCIPLE

Harmonic well matter densities and Pauli correlation

effects in heavy-ion collisions

[NASA-TP-2O03I p 192 N82-23003

PAYLOAD DELIVERY (STS)

Performance requirements analysis for payload clelivery

from a space station

{ NASA-RP-1110J p67 N83-32828

PAYLOAD DEPLOYMENT A RETRIEVAL SYSTEM

The 16th Aerospace Mechanisms Symposium

[NASA-CP-2221 ] p 99 N82-23344

PAYLOAD MASS RATIO

Parametric study of variation in cargo-airplane

pedormence related to progression from current to

spanloader designs

INASA-TP-1625] p 34 N80-21318

PAYLOAD TRANSFER

The 18th Aerospace Mechanisms Symposium

[NASA-CP-2311 I p 133 N84-25078

PAYLOADS

Government/Industry Workshop on Payload Loads

Technology

[NASA-CP-20751 p 62 N79-20162

Get away special experimenter's symposium

[NASA-CP-23241 p 63 N84-27758

PENDULUMS

Design and analysis of a torsion braid pendulum

displacement transducer

lNASA-TP-1840] p 115 N81-25352

A-88
SUBJECTINDEX

PENETRATION

Results of analyses performed on basalt adjacent to

penetrators emplaced into volcanic rock at Amboy,

California, April 1976

[NASA-TP-1026] p 199 N77-33003

PERCEPTION

Twentieth Annual Conference on Manual Control,

volume 1

[NASA-CP-2341-VOL-1 J p 174 N85-14487

PERFORATED PLATES

Expehmental flow coefficients of a full-coverage

film-cooled-vane chamber

[NASA-TP-t036] p 41 N77-32153

Evaluation of multilayer printed wiring boards by

metallographic techniques: An illustrated guide to the

preparation and inspection of plated-through hole test

coupons based on the requirements of MiI-P-55110D

[NASA-RP-t 161 I p 126 N86-26639

PERFORMANCE

Cold air performance of a

12.766-centimeter-tip-diameter axial-flow cooled turbine.

2: Effect of air ejection on turbine performance

[NASA-TP-1018] p 5 N77-30089

PERFORMANCE PREDICTION

An analytical technique for predicting the characteristics

of a flexible wing equipped with an active

flutter-suppression system and comparison with

wind-tunnel data

[NASA-TP-1367J p 128 N79-17264

Analytical prediction with multidimensional computer

programs and experimental verification of the

performance, at a variety of operating conditions, of two

traveling wave tubes with depressed collectors

[NASA-TP-1449] p 101 N79-22375

Traction drive performance prediction for the Johnson

and Tevaarwerk traction model

[NASA-TP-1530] p 121 N79-33475

Comparison of predicted and experimental performance

of large-bore roller bearing operating to 3.0 million DN

[NASA-TP-t599J p 121 N80-15410

Measured and predicted shock shapes and aerodynamic

coefficients for blunted cones at incidence in air at Mach

5.9

[NASA-TP-1652] p 108 N80-23600

Experimental performance and analysis of

15.04-centimeter-tip-diameter, radial-inflow turbine with

work factor of 1.126 and thick blading

[NASA-TP-1730] p 47 N80-33410

Parametric study of microwave-powered high-altitude

airplane platforms designed for linear flight

[NASA-TP-1918] p 35 N82-11050

Automated rendezvous and docking: A parametric

study

[NASA-TP-2314] p 74 N84-23677

Operating characteristics of a three-piece-inner-ring

large-bore roller bearing to speeds of 3 million DN

[NASA-TP-2355] p 124 N84-29226

PERFORMANCE TESTS

Experimental evaluation of foil-supported resilient-pad

gas-lubncated thrust bearing

INASA-TP-t030] p 118 N77-31502

Experimental performance of a

13.65-centimeter-tip-diameter tandem-bladed sweptback

centrifugal compressor designed for a pressure ratio of 6

[NASA-TP-1091 ] p 8 N78-11002

Cold-air performance of a tip turbine designed to drive

a lift fan. 3: Effect of simulated fan leakage on turbine

performance

[NASA-TP-1109J p 7 N78-16001

Performance of a short annular dump diffuser using

suction-stabilized vortices at inlet Mach numbers to 0.41

(NASA-TP-11941 p42 N78-20131

, A pilot evaluation of two G-seat cueing schemes

[NASA-TP-1255] p 172 N78-31739

Aerodynamic performance of axial-flow fan stage

operated at nine inlet guide vane angles --- to be used

on vertical lift aircraft

[NASA-TP-1510J p 45 N79-31214

Effects of diffusion factor, aspect ratio and solidity on

overall performance of 14 compressor middle stages ---

the effects of varying both diffusion through the rotor and

compressor blades and blade aspect ratio

[NASA-TP-1523_ p 45 N79-33210

Self-acting lift-pad geometry for circumferential seals:

A noncontacting concept --- performance tests on

hydrodynamic seals

INASA-TP-1583] p 121 N60-14403

Investigation of convergent-divergent nozzles applicable

to reduced-power supersonic cruise aircraft

INASA-TP-17661 p 16 N81-14972

Performance of jet- and inner-ring-lubricated 35

millimeter bore ball bearings operating to 2.5 million DN

INASA-TP-1808] p 122 N81-19458

Performance tests of a gas blending system based on

mass-flow controllers

INASA-TP-1896J p 97 N81-29246

Effect of fuel injector type on performance and emissions

of reverse-flow combustor

JNASA-TP-1945] p 49 N82-15040

Group-type hydrocarbon standards for

high-performance liquid chromatographic analysis of

middistiltate fuels

[NASA-TP-2317] p 97 N84-23774

The 18th Aerospace Mechanisms Symposium

I NASA-CP-2311 J p 133 N84-25078

Astronomical Microdensitometry Conference

[NASA-CP-2317] p 116 N84-28020

Programmable, automated transistor test system

[NASA-TP-2554} p 103 N86-21755

PERIODIC VARIATIONS

Ozone Trend Detectability

INASA-CP-2189] p 153 N82-10624

Variations of the Solar Constant --- conference

[NASA-CP-21911 p 209 N82-17014

North Atlantic Deep Water Formation

{NASA-CP-2367J p 169 N85-26028

Nineteenth International Cosmic Ray Conference. SH

sessions, volume 5

{NASA-CP-2376-VOL-5] p 211 N85-34991

PERIPHERAL VISION

Peripheral Vision Horizon Display (PVHD)

[NASA-CP-23061 p 40 N85-10044

PERMEATING

Nitrogen dioxide vapor penetration of chlorobutyf rubber

SCAPE under operational conditions

{NASA-TP-16051 p85 N80-16118

PERMITTIVITY

Dielectric constants of soils at microwave

freduencies-2

[NASA-TP-1238] p 138 N78-23538

PERSONNEL MANAGEMENT

Resource management on the flight deck ---

conferences

[ NASA-CP-2120 ] p29 N80-22283

PERTURBATION

Hybrid perfurbation/Elubnov-Galerkin technique for

nonlinear thermal analysis

[NASA-TP-2145] p 111 N84-22907

Three-dimensional baroclinic instability of a Hadley cell

for small Richardson number

(NASA-TP-2450J p 166 N85-20605

PERTURBATION THEORY

Baroclinic instability with variable gravity: A perturbation

analysis

[NASA-TP-1586] p 136 N80-15445

Status of linear boundary-layer stability and the e to the

nth method, with emphasis on swept-wing applications

(NASA-TP-1645] p 108 N80-22633

Rapid estimation of frequency response functions by

close-range photogrammetry

[NASA-TP-2471] p 116 N86-12579

PERVEANCE

Experimental verification of the multistage depressed

collector design procedure for a high-perveance,

hefix-type, traveling-wave tube --- in communications

satellites

(NASA-TP-21621 p 102 N83-25985

PETROGRAPHY

Lunar sample studies --- breccias basalts, and

anorthosites

JNASA-SP-418] p 204 N77-27053

PETROLEUM PRODUCTS

Assessment of Alternative Aircraft Fuels

[NASA-CP-2307] p 51 N84-23830

PETROLOGY

Results of analyses performed on basalt adjacent to

penetrators emplaced into volcanic rock at Amboy,

California, April 1976

[NASA-TP-1026] p 199 N77-33003

Space Station Planetology Experiments (SSPEX)

[NASA-CP-2424] p 201 N86-27136

PHASE TRANSFORMATIONS

A design handbook for phase change thermal control

and energy storage devices --- selected paraffins

INASA-TP-1074] p 104 N78-15434

Metallurgical characterization of the fracture of several

high strength aluminum alloys

[NASA-TP-10861 p 85 N84-11230

Overview of zirconia with respect to gas turbine

applications

[NASA-TP-22861 p 95 N84-21740

PHASED ARRAYS

Large Space Antenna Systems Technology, part 1

[NASA-CP-2269-PT-I ] p 67 N83-26853

PHILOSOPHY

The Impact of Science on Society

INASA-SP-482] p t96 N85-24994

PHOBOS

Images of Mars: The Viking extended mission

I NASA-SP-4441 p 206 N80-26239

PHOTOMAPPING

Phobos: Close encounter imaging from the Viking

Orbiters

[NASA-RP-t 109) p 207 N84-32330

PHOSPHATES

Mechanism of lubrication by tricresylphosphate (TCP)

[NASA-TP-2053] p 85 N83-18863

Mechanism of lubrication by tricresylphosphate (TCP)

[NASA-TP-2274] p 123 N84-18653

PHOTOCHEMICAL REACTIONS

Effect of nitric oxide on photochemical ozone formation

in mixlures of air with molecular chlorine and with

trichlorofluoromet bane

{NASA-TP-1192] p 84 N78-20281

The stratosphere: Present and future

INASA-RP-1049] p 181 N80-14641

The stratcom 8 effort --- stratospheric photochemistry

[NASA-TP-1640] p 161 N80-22924

A diagnostic model for studying daytime urban air quality

trends

[NASA-TP-1843J p 149 N81-22587

Solar-simulator-pumped atomic iodine laser kinetics

[NASA-TP-2182] p 118 N83-32044

PHOTODIODES

Comparative performance of HgCdTe photodiodes for

heterodyne application

[NASA-TP-1745} p 101 N80-33683

Excess noise in tunable diode lasers

[NASA-TP-1935] p 117 N82-12431

PHOTOELASTIC ANALYSIS

An optical profitometer for spatial characterization of

three-dimensional surfaces

[NASA-TP-1012| p 113 N77-32458

PHOTOE LECTROCHEMISTRY

Semiconductor photoelectrochemistry

[NASA-TPo2088] p 146 N83-18024

PHOTOELECTRON SPECTROSCOPY

Surface chemistry and friction behavior of the ._licon

carbide (0001) surface at temperatures to 1500 deg C

[NASA-TP-1813J p 94 N81-19300

PNOTOGEOLOGY

Volcanic features of Hawaii, A basis for comparison

with Mars

{NASA-SP-403J p 152 N80-23912

Skytab explores the Earth

[NASA-SP-380] p 140 N82-12492

PHOTOGRAMMETRY

Conference of Remote Sensing Educators

(CORSE-78)

[NASA-CP-2102] p 212 N80-20003

Rap_d estimation of frequency response functions by

close-range photogrsmmetry

[NASA-TP-2471] p 116 N86-12579

Earth resources: A continuing bibliography with indexes,

issue 50

[NASA-SP-7041(50)J p t43 N86-31940

PHOTOGRAPHIC EQUIPMENT

Apollo over the moon: A view from orbit

[NASA-SP-362] p 61 N78-21174

PHOTOGRAPHS

Viking Lander imaging investigation: Picture catalog of

primary mission experiment data record

[NASA-RP-1007] p 205 N78-20042

PHOTOINTERPRETATION

Aehal color infrared photography: Applications in

citriculture --- Florida

[NASA-RP-1067] p 139 N81-21437

Field Study for Remote Sensing: An instructor's

manual

[NASA-CP-2155] p 136 N81-32564

Skylab explores the Earth

[NASA-SP-380] p 140 N82-12492

Applications systems verification and transfer project.

Volume 8: Satellite snow mapping and runoff prediction

handbook

[NASA-TP-1829] p 141 N82-20624

The Heat Capacity Mapping Mission (HCMM)

anthology

JE84-10051 l p 142 N84-14563

PHOTOIONIZATION

Thermosphere Dynamics Workshop, volume 2

[NASA-CP-2389] p 137 N86-29301

PHOTOMAPPING

Atlas of Mars: The 1:5000000 map series

INASA-SP-438] p 206 N80-16998

Applications systems verification and transfer project.

Volume 1 : Operational applications of satellite snow cover

observations: Executive summary *-- usefulness of satellite

snow-cover data for water yield prediction

[NASA-TP-1822] p 140 N82-20617

Applications systems verification and transfer project.

Votume 2: Operational applications of satellite snow-cover

observations and data-collection systems in the Arizona

test site

[NASA-TP-1823] p 140 N82-20618

A-89
PHOTOMAPS

Applications systems vehfication and transfer proiect.

Volume 6: Operational applications of satellite snow-cover

observations NOAA/NESS support study

[NASA-TP-1827} p f40 N82-20622

Voyager 1 and 2 atlas of six Saturnian satellites

[NASA.SP.474] p 208 N84-35242

PHOTOMAPS

Atlas of Mercury --- Manner 10 mission

[NASA-SP-423] p 205 N78-30025

PHOTOMETRY

Proceedings of the Workshop on Improvements to

Photometry

[NASA-CP-2350} p 203 N85-17892

Planetary cartography in the next decade (1984 -

1994 )

{NASA-SP-475] p 208 N85-22323

PHOTOMICROGRAPHY

Sliding induced crystallization of metallic glass

{ NASA-TP-2140] p88 N83-21110

PHOTOSENSITIVITY

Determination of noise equivalent reflectance for a

multispectral scanner: A scanner sensitivity study

[NASA-TP-1575] p 114 N80-12399

PHOTOSPHERE

Measurements of Solar Vector Magnebc F_etds

[NASA-CP-2374} p 210 N85-29869

PHOTOVOLTAIC CELLS

Terrestrial photovoltaic measurements, 2

INASA-CP-2010] p 136 N77-30521

Space Photovoltaic Research and Technology 1982:

High Effic=ency, Radiation Damage, and Blanket

Technology

[NASA.CP.22561 p 146 N83.15806

Space Photovolta_c Research and Technology 1985:

High Efficiency, Space Environment, and Array

Technology

[NASA-CP-2408] p 146 N86-17839

PHYSICAL CHEMISTRY

A class of nonldeal solutions 1: Definition and

properties

[NASA-TP-tg29J p 196 N83-23189

PHYSICS AND CHEMISTRY EXPERIMENT IN SPACE

Spacecraft Dynamics as Related to Laboratory

Experiments in Space --- conference

[NASA-CP-2199J p 72 N82-12109

PHYSIOLOGICAL EFFECTS

The physiological basis for spacecraft environmental

limits

INASA-RP-1045] p 170 N80-15788

PHYSIOLOGICAL FACTORS

Multiple-event airplane noise annoyance

[NASA-TP-2101 ] p t50 N83-16951

PHYSIOLOGICAL RESPONSES

Biomedical results from Skylsb

[NASA-SP-377} p 169 N77-33780

Physiological responses of women to simulated

weightlessness: A review of the first female bed-rest

study

[NASA-SP-430] p 170 N79-13686

The Regulatory Functions of Calcium and the Potential

Role of Calcium in Mediating Gravitational Responses in

Cells and Tissues

[NASA-CP-2286} p 169 N84-11720

A user-oriented and computerized model for estimating

vehicle ride quality

[NASA-TP-2299} p 172 N84-22162

PHYTOPLANKTON

Laboratory tank studies of a single species of

phytoplsnkton using a remote sensing fluorosensor

{NASA-TP-1821} p 139 N81-20492

Visible sbeorbance spectra: A basis for in situ and

passrve remote sensing of phytoplsnkton concentration

and community composition

[NASA-TP-2094} p 168 N83-lg411

PIGMENTS

Formulation of electrically conductive thermal-control

coatings

INASA.TP-1218] p 78 N78-21216

PILOT PERFORMANCE

Analytical study of ride smoothing benefits of control

system configurations Optimized lot pilot handling

qualities

INASA.TP-1148] p 53 N78-18076

Study of the use of a nonlinear, rate-limited filter on

pilot control s_gnais

[NASA-TP-1147J p 53 N78-20t42

Pilot-model analysis and simulation study of effect of

control task desired control response

{NASA-TP-lt40J p 53 N78-20143

Simulator study of the effect of visual-motion time delays

on pilot tracking performance with an audio side task

{NASA-TP-12161 p 32 N78-30090

Effects of visual and motion simulation cueing systems

on pilot performance during takeoffs with engine lailures

[NASA-TP-13651 p 32 N7g-14082

Development and validation of s piloted simulation of

• helicopter and external sling toad

[NASA-TP-1285] p 32 N79-14083

Flight investigation of piloting techniques and crosswind

limitations using a research type crosswind landing gear

[NASA-TP-1423} p 12 N79-23012

Application of modified profile analysis to function testing

of simulated CTOL transport touchdown-performance

data

[NASA-TP-1541 J p 33 N80-11069

The effects of motion and g-seat cues on pilot simulator

performance of three piloting tasks

[NASA-TP-1EOl ] p 34 N80-15069

Resource management on the flight deck ---

conferences

[NASA-CP-2120} p 29 N80-22283

Head-up transition behavior of pilots during simulated

low-visibility approaches

{NASA-TP-1618} p 173 N80-26039

Simulation comparison of a decoupled longitudinal

control system and a velocity vector control wheel steering

system during landings in wind shear

[NASA-TP-1734] p 56 N81-12109

Head-up transition behavior of pilots with and without

head-up display in simulated tow-visibility approaches

INASA-TP-1720] p 173 N81-13635

Cognitive issues in head-up displays

[NASA-TP-1711} p 173 N81-13636

Evaluation of s computer-generated perspective tunnel

display for flight path following

NASA-TP-1736} p 39 N81-13958

Simulator study of conventional general aviation

instrument displays in path-following tasks with emphasis

on pilot-induced oscillations

NASA-TP-1776} p 39 N81-14997

EffectS of curved approach paths and advanced displays

on pilot scan patterns

NASA-TP-18461 p 171 N81-23791

Simulabon study of traffic-sensor noise effects on

utilization of traffic situation display for self-spacing task

NASA-TP-20821 p 40 N83-18723

Effects of motion base and g-seat cueing of simulator

pilot performance

NASA-TP-2247} p 37 N84-18189

Twentieth Annual Conference on Manual Control,

volume 2

NASA-CP-2341-VOL-2] p 174 N85-14535

Analytical techniques of pilot scanning behavior and their

appbcaticn

NASA-TP-2525] p 172 N86-27920

PILOT PLANTS

Stability boundaries for systems with frequency-model

feedback and complacency filter

{NASA-TP-1744] p 184 N81-10789

PILOT SELECTION

Resource management on the flight deck ---

conferences

[NASA-CP-2120} p 29 N80-22283

PILOT TRAINING

Guidelines for line-oriented flight training, volume 1

{NASA-CP-2184} p 30 N81-30101

Comparison of simulator fidelity model predictions with

in-simulator evaluation data

[NASA-TP-2106J p 36 N83-16715

Controls, Displays, and Information Transfer for General

Aviation IFR Operations

I NASA-CP-2279} p 4 N84-12029

Flight Training Technology for Regional/Commuter

Airline Operations: Regional Airline Association/NASA

Workshop Proceedings

[NASA-CP-2348] p 30 N85-18009

Analytical techniques of pilot scanning behavior and their

application

[NASA.TP-2525] p 172 N86-27920

PILOTLESS AIRCRAFT

Controls, Displays, and information Transfer lor General

Aviation IFR Operations

[NASA-CP-2279] p 4 N84-12029

PINHOLES

The Pinhole/Occulter Facility

INASA-TP-2168] p 209 N83-25646

Solar Flares and Coronal Physics Using P/OF as a

Research Tool

[NASA-CP-2421 I p 210 N86-24614

PINS

Water-vapor effects on friction of magnetic tape =n

contact with nickel-zinc fernte

INASA-TP-22791 p 95 N84-18399

PIONEER PROJECT

Voyage to Jupiter

INASA-SP-439] p 206 N81-10910

Pioneer: First to Jupiter, Saturn, and beyond

INASA-SP-446] p 206 N8t-15925

PIONEER VENUS SPACECRAFT

Pioneer Venus

l NASA-SP-461 ] p 207 N83-30340

SUBJECT INDEX

PIONEER 10 SPACE PROBE

Pioneer odyssey

fNASA-SP-349] p 205 N77-28055

PIONEER 11 SPACE PROBE

Pioneer odyssey

[NASA-SP-349] p 205 N77-28055

PIONS

Cross section calculations for subthreshold p*on

production in peripheral heavy-ton collisions

[NASA-TP-2600] p 193 N86-30485

PISTON ENGINES

Aircraft Piston Engine Exhaust Emission Symposium

[NASA-CP-2005] p 41 N77-17081

Modular instrumentation system for reaL-time

measurements and control on reciprocating engines

INASA-TP-1757} p 101 N81-11315

PITCHING MOMENTS

Kinematic properties of the helicopter in coordinated

turns

I NASA-TP-1773 J p 35 N81-22039

Airfoil interaction with impinging vortex

[NASA-TP-2273 ] p 23 N84-16159

PITTING

Cavitation pitting and erosion of aluminum 6061-T6 in

mineral oil water

[NASA-TP-2146J p 123 N83-35400

PLANE STRAIN

A cracked orthotropic sheet stiffened by a semi-infinite

orthotropic sheet

INASA-TP-2455] p 134 N85-3233g

PLANE WAVES

Consideration of some factors affecting low-frequency

fuselage noise transmission for propeller aircraft

I NASA-TP-2552J p 191 N86-24393

PLANETARY ATMOSPHERES

Molecules of significance in planetary aeronomy

tNASA-RP-t030J p 199 N7g-22980

Vibrational-Rotational Spectroscopy For Planetary

Atmospheres, volume 1

{NASA-CP-2223-VOL-1 I p 207 N82-25043

Vibrational-Rotational Spectroscopy for Planetary

Atmospheres, volume 2

[NASA-CP-2223-VOL-2] p 207 N82-26134

PLANETARY COMPOSITION

The Soviet-American Conference on Cosmochemistry

of the Moon and Planets, part "1

[NASA-SP-370-PT-1 ] p 203 N78-12925

PLANETARY ENVIRONMENTS

The 1st Symposium on Chemical Evolution and the

Origin and Evolution of Life

I NASA-CP-22761 p 79 N83-24556

PLANETARY EVOLUTION

Evolution of the solar system

I NASA-SP-345] p 203 N77-12959

Asteroids: An Exploration Assessment

I NASA-CP-2053} p 205 N78-29007

An assessment of ground-based techniques for

detecting other planetary systems. Volume 1: An overview

--- workshop conclusions

[NASA-CP-2124-VOL-1 I p 201 N80-18997

The geology of the terrestrial planets

{NASA-SP-4691 p 200 N85-18888

Planetary geology in the lg80s

[NASA-SP-467| p 200 N85-23457

Second Symposium on Chemical Evolution and the

Origin of Life

[NASA-CP-2425J p 175 N86-26844

PLANETARY GEOLOGY

The geology of the terrestrial planets

[NASA-SP-469] p 200 N85-18888

Planetary geology in the 1980s

[NASA-SP-467J p 200 N85-23457

PLANETARY GRAVITATION

Spaceborne Gravity Gradiometers

JNASA-CP-2305] p 136 N84-18716

PLANETARY MAPPING

Atlas of Mercury --- Mariner 10 mission

{NASA-SP-4231 p 205 N78-30025

A Catalog of Selected Viking Orbiter Images

{NASA-RP-1093J p 207 N83-25636

Planetary cartography in the next decade (1964 -

1994)

{NASA-SP-4751 p 206 N85-22323

PLANETARY QUARANTINE

Orbiting quaranlme facility. The Antaeus report

I NASA-SP-454I p 66 N82-20225

PLANETARY RINGS

Uranus and Neptune

INASA-CP-2330} p 208 N85-11927

PLANETARY SURFACES

The voyage of Mariner 10: Missions to Venus and

Mercury

INASA-SP-424J p 61 N78-27146

Atlas of Mercury --- Manner t0 mission

INASA-SP-423 j p 205 N78-30025

A-90
SUBJECT INDEX POLLUTION MONITORING

Planetary geology in the 1980s

[NASA-SP-467] p 200 N55-23457

PLANETARY WAVES

Global Scale Atmospheric Processes Research Program

Review

[NASA-CP-2344] p 166 N85-14360

Current Scientific Issues in Large Scale Atmospheric

Dynamics

[NASA-CP-24101 p 167 N86-24082

PLANETOLOGY

Second Internalional Colloquium on Mars: Abstracts

for a colloquium --- bibliography

[NASA-CP-2072] p 205 N79-16757

Trends in Planetary Data Analysis. Executive summary

of the Planetary Data Workshop

[NASA-CP-2333] p 208 N84-34363

Space Station Planetology Experiments (SSPEX)

{NASA-CP-2424] p 201 N86-27136

PLANETS

The Soviet-American Conference on Cosmochemistry

of the Moon and Planets, part 2

[NASA-SP-370-PT-2] p 203 N78-12958

Advances in Ultraviolet Astronomy: Four Years of IUE

Research

[NASA-CP-22381 p 201 N82-31163

Planetary Data Workshop, part 1

[NASA-CP*2343-PT-1] p 208 N84-34366

PLANKTON

Laboratory tank studies of a single species of

phytoptankton using a remote sensing fluorosensor

{NASA-TP-1821 I p t39 N81-20492

Visible absorbance spectra: A basis for in situ and

passive remote sensing of phytoplankton concentration

and community composition

[NASA-TP-2094J p 168 N83-19411

PLANT STRESS

Aerial color infrared photography: Applications in

citdculture -*- Florida

[NASA-RP-1067J p 139 N81-21437

PLANTS (BOTANY)

Controlled Ecological Life Support System: Use of

Higher Plants

{NASA-CP-2231 ) p 173 N82-24834

Controlled Ecological Life Support System: Research

and Development Guidelines

[NASA-CP-2232J p 173 N82-24835

Controlled ecological life support system - biological

problems

[NASA-CP-2233] p 173 N82-24836

NASA Space Biology Program. Eighth annual

symposium's program and abstracts

[NASA-CP-22991 p 169 N84-15829

NASA Space Biology Program: 9th Annual

Symposium

[NASA-CP-2336] p 169 N85-26054

PLASMA CONTROL

Ion confinement and transport in a toroidal plasma with

exlernally imposed radiaI electric fields

[NASA-TP-1411] p 195 N79-19867

PLASMA DIAGNOSTICS

Fluctuation spectra in the NASA Lewis bumpy-torus

plasma

INASA-TP-12571 p 194 N78-26927

Low-frequency fluctuation spectra and associated

particle transport in the NASA Lewis bumpy-torus

plasma

[NASA-TP-1258] p 194 N75-30944

Applications of Tethers in Space, volume 2

[NASA-CP-2365] p 125 N85-20361

PLASMA DIFFUSION

Fluctuation spectra in the NASA Lewis bumpy-torus

plasma

[NASA-TP-1257] p 194 N78-26927

Low-frequency fluctuation spectra and associated

particle transport in the NASA Lewis bumpy-torus

plasma

[NASA-TP-1258] p 194 N78-30944

PLASMA ELECTRODES

Effect of anode-cathode geometry on performance of

the HIP-1 hol ion plasma --- magnetic mirrors

[NASA-TP-1201 ] p 194 N78-21922

PLASMA INTERACTIONS

Spacecraft Charging Technology, 1978

[NASA-CP-2071 ] p 71 N79-24001

Spacecraft Charging Technology, 1980

[NASA-CP-2182] p 72 N82-14213

The aerodynamics of bodies in a rarefied ionized gas

with applications to spacecraft environmental dynamics

{NASA-TP-1933] p 72 N52-15116

Spacecraft Environmental Interactions Technology,

1983

fNASA-CP-2359] p 75 N85-22470

PLASMA JETS

Temperature distributions of a cesium-seeded

hydrogen-oxygen supersonic free iet

[ NASA-TP-1162 ] p 194 N75-20959

Reinforced carbon-carbon oxidation behavior in

convective and radistive environments

[NASA-TP-1284] p 106 N75-30555

Homogeneous reactions of hydrocarbons, silane, and

chlorosilanes in radiofrequency plasmas at tow

pressures

[NASA-TP-2301J p 79 N84-20643

PLASMA OSCILLATIONS

Mean excitation energies for stopping powers in various

materials using local plasma oscillator strengths

[NASA-TP-2271] p 210 N84-21485

PLASMA PHYSICS

Second Workshop on Spacecraft Glow

[NASA-CP-2391] p 201 N86-13239

PLASMA PROPULSION

Rail accelerators for space transportation: An

experimental investigation

INASA-TP-2571 ] p 78 N86-28123

PLASMA SPRAYING

Friction and wear of several compressor gas-path seal

movements

[NASA-TP-1128] p 86 N78-15229

Plasma-sprayed coatings for lubrication of a titanium

alloy in air at 430 deg C

[NASA-TP-15091 p 93 N79-29327

Preliminary study of methods for providing thermal shock

resistance to plasma-sprayed ceramic gas-path seals

[NASA-TP-1561 ] p 93 N80-23453

Effect of aluminum phosphate additions on composition

of three-component plasma-sprayed solid lubricant

[NASA-TP-1990] p 88 N82-21298

Further industrial tests of ceramic thermal barrier

coatings

[NASA-TP-2057] p 49 N83-10045

High-temperature erosion of plasma-sprayed,

yttria-stabilized zirconia in a simulated turbine

environment

[NASA-TP-2406J p 96 N85-13045

PLASMAS (PHYSICS)

Space plasma physics active experiments

[NASA-CP-2165] p 212 N8t-14944

Growth of high-quality thin-film Ge single crystals by

plasma-enhanced chemical vapor deposition

[NASA-TP-25321 p 1(3'0 N86-20586

PLASTIC DEFORMATION

Anisotropic friction, deformation, and fracture of

single-crystal silicon carbide at room temperature

[NASA-TP-1525] p 93 N79-30380

Plastic deformation at surface during unlubricated

sliding

(NASA-TP-2536] p 122 N53-11498

PLASTIC PROPERTIES

Elastic-plastic finale-element analyses of thermally

cycled double-edge wedge specimens

[NASA-TP-1973] p 130 N82-20566

PLATES (STRUCTURAL MEMBERS)

Evaluation of a hybrid, anisotropic, multilayered,

quadrilateral finite element

[NASA-TP-1236] p 127 N78-28482

Failure mechanics in low-velocity impacts on thin

composite plates

[NASA.TP-2152] p 82 N83-24562

A solution procedure for behavior of thick plates on a

nonlinear foundation and postbuckting behavior of long

plates

{NASA-TP.2174] p 132 N83-34373

PLATFORMS

The 1980 Large space systems technology. Volume

2: Base technology

[NASA-CP-2168-VOL-2] p 66 N81-19196

STEP Experiment Requirements

[ NASA-CP-2294 ] p 67 N54-17211

PLATING

Electroless-plating technique for fabricating thin-wall

convective heat-transfer models

[NASA-TP-2349] p 1 f2 N84-31561

PLENUM CHAMBERS

A theory for predicting boundary impedance and

resonance frequencies of slotted-walt wind tunnels,

including plenum effects

[NASA-TP-1880] p 17 N81-29096

PLOTTING

A general solution to the hidden-line problem --- to

graphically represent aerodynamic stabilitydenvatives

[NASA-RP-1085J p 176 N82-21907

PLUMES

An ultraviolet video technique for visualization of stack

plumes end for measuring sulfur dioxide concentration and

effluent velocity

[NASA-TP-10141 p 147 N77-32622

Space shuttle afterbody aerodynamics/plume simulation

data summary

[NASA-TP-1384J p 11 N79-17510

Numerical solutions of the Navier-Stokes equations for

transonic affed3ody flows

[NASA-TP-1784] p 16 N51-13919

Effects of axisymmetric and normal air jet plumes and

solid plume on cylindrical afferbody pressure distributions

at Mach numbers from 1.65 to 2.50

[NASA-TP-2005] p 19 N82-22215

Investigation of solid plume simulation criteria to produce

flight plume effects on multibody configuration in wind

tunnel tests

[NASA-TP-2569] p 28 N86-21507

PLY ORIENTATION

INHYD: Computer code for intraply hybrid composite

design. A users manual

[NASA-TP*2239] p 82 N84-13224

POGO EFFECTS

Space shuttle active-pogo-suppresaor control design

using linear quadratic regulator techniques

[NASA-TP-1217J p 101 N79-14309

POINT SOURCES

Algorithm for astronomical, point source, signal to noise

ratio calculations

[NASA-TP-2397] p 202 N85-12834

Ninteenth International Cosmic Ray Conference OG

sessions, volume 1

[NASA-CP-2376-VOL-1 ] p 210 N85-33902

POINTING CONTROL SYSTEMS

Graphical techniques to assist in pointing and control

studies of orbiting spacecraft

[NASA-TP-25751 p 63 N86-21559

POLAR CAPS

Microwave emission from polar firn

[NASA-TP-1212] p 151 N78-21690

The role of satellite altimetry in climate studies

[NASA-TP-15701 p 161 N80-16676

POLAR METEOROLOGY

Proceedings of a Workshop on Polar Stratospheric

Clouds: Their Rote in Atmospheric Processes

[NASA-CP-23181 p 154 N84-32952

SAM 2 measurements of the polar stratospheric aerosol.

volume 8

[NASA-RP-1165] p 157 N86-29428

POLAR REGIONS

SAM 2 measurements of the polar stratospheric aerosol.

Volume 3: October 1979 to April 1980

{NASA-RP-1106J p 154 N83-27520

SAM 2 measurements of the polar stratospheric aerosol

Volume 4: April 1980 1o October 1980

[NASA-RP*1107] p t54 N83-28796

SAM 2 measurements of the polar stratospheric aerosol,

volume 5

INASA-RP-1140] p 155 N85-25970

POLARIZATION {WAVES)

Efficiency enhancement of octave-bandwidth traveling

wave tubes by use of multistage depressed collectors

[NASA-TP-1416] p 101 N79-17139

POLICIES

Second Symposium on Space Industrialization --- space

commercialization

(NASA-CP-2313] p 63 N85-11011

POLLUTION CONTROL

Lean premixed/prevaporized combustion

[NASA-CP-2016} p 84 N77-33297

Aircraft engine emissions --- conference

[NASA-CP-2021] p 41 N78-t 1063

POLLUTION MONITORING

A gas filter correlation monitor for CO, CH4, and HCI

[NASA-TP-1113] p 113 N78-13408

Description and field test of an in _tu coliform monitoring

system

{NASA-TP-1334] p 148 N79-14591

Lidar backscattering measurements of background

stratospheric aerosols

[NASA-TP-1381 ] p 152 N79-17388

Condensation-nuclei (Aitken Particle) measurement

system used in NASA global atmospheric sampling

program

[NASA-TP-1415] p 148 N79-18479

NASA JSC water monitor system: City of Houston field

demonstration

[NASA-RP-1041] p 198 N79-28062

Carbon monoxide measurement in the global

atmospheric sampling program

[NASA-TP-1526] p 148 N79-31841

Measurement techniques for trace metals in coal-plant

effluents: A bnef review

[NASA-RP-t047) p 148 N79-33611

Coordinated aircraft and ship surveys for determining

impact of river inputs on great lakes waters Remote

sensing results

[NASA-TP-16941 p 149 N80-27832

A diagnostic model for studying daytime urban air quality

trends

[NASA-TP-1843} p 149 N81-22557

Water vapor measurement system in global atmospheric

sampling program, appendix

[NASA-TP-205t ] p 150 N83-13643

A-91
POLYCARBONATES SUBJECT INDEX

POLYCARBONATES

Solid spherical glass particle impingement studies of

plastic materials

INASA-TP-21611 p 95 N83-24695

POLYCRYSTALS

Friction and wear of single-crystal and polycrystalline

maganese-zinc fernte in contact with various metals

INASA-TP-1059] p 91 N78-10295

POLYETHYLENES

Fnction and wear of polyethylene oxide polymer having

a range of molecular weights

[ NASA-TP-1129 ] p91 N78-15278

Effect of sterilization irradiation on fnction and wear of

ultrahigh-molecular-weight polyethylene

[NASA-TP-1462] p 92 N79-23216

Effect of sliding speed and contact stress on tfibological

properties of ultra-high-molecular-weight polyethylene

I NASA-TP-20591 p 95 N83-14269

Adhesion between polymers and evaporated gold and

nickel films

INASA-TP-2360J p 96 N84-31379

POLYIMIDE RESINS

Evsiuetion of a low-density polyimide foam in a dynamic,

high temperature environment

I NASA-TP-t049J p 91 N78-12223

Graphite/Polyimide Composites --- conference on

Composites for Advanced Space Transportation

Systems

INASA-CP-2079] p 80 N79-30297

POLYIMIDES

Effect of thermal exposure on lubricating properties of

poly*mide films and polyimide-bonded graphite fluoride

films

[NASA-TP-11251 p 91 N78-15277

Some effects of composition on friction and wear of

grapNte-fiber-rsinforced potyimide liners in plain spherical

bearings

{NASA-TP-12291 p 119 N78-25433

Graphite/Polyimide Composites --- conference on

Composites for Advanced Space Transportation

Systems

INASA'CP-20791 p 80 N79-30297

Elevated-temperature apphcation of the IITRI

compression test fixture for graphite/potyimide filamentary

composites

[ NASA-TP-1496 } p80 N79-32277

Lubncation and wear mechanisms of polyimide-bor,x:led

graphite fluoride films subtected to low contact stress

I NASA-TP-1584 ] p93 N80-17220

Triboiogical properties at 25 C of seven potyimide films

bonded to 440 C high-temperature stainless steel

I NASA-TP-1944] p 94 N82-19373

Spectroscopic analys_s of radiation-generated changes

in tensile properties of a polyetherimide film

I NASA-TP-24291 p 83 N85-25435

POLYMER CHEMISTRY

Ultra-high molecular weight silphenylene-siloxane

polymers

{NASA-TP-22951 p 95 N84-19564

Microgravity Polymers

[NASA-CP-2392] p 96 N86-28194

POLYMER MATRIX COMPOSITES

Graphite/Polyimide Composites --- conference on

Composites lor Advanced Space Transportation

Systems

[NASA-CP-20791 p 80 N79-30297

Selected NASA research in composite Materials and

structures

INASA-CP-2142] p 80 N80-28436

Tough Composite Materials

I NASA-CP-2334 ] p 83 N85-12941

POLYMER PHYSICS

Ultra-high molecular weight sitphenylene-siloxane

polymers

I NASA-TP*2295} p 95 N84-19564

Microgravity Polymers

{ NASA-CP-2392_ p 96 N86-28194

POLYMERIC FILMS

Three methods for in situ cross-linking of potyvinyl

alcohol films for application as ion-conducting membranes

m potassium hydroxide electrolyte --- battery separators

[NASA-TP-1407] p 78 N79-21128

Lubrication and wear mechanisms of polyimide-bonded

graphite fluoride films subjected 1o low contact stress

I NASA-TP- 1584 ] p 93 N80-17220

Tribological properties at 25 C of seven pelyimide films

bonded to 440 C high-temperature stainless steel

[ NASA-TP-1944 } p94 N82-19373

Monte Carto latlice models for adsorbed polymer

conformation

I NASA-TP-2453 } p 195 N85-24961

POLYMERIZATION

Ultra-high molecular weight sdphenylene-siloxane

polymers

[ NASA-TP+22951 p 95 N84-19564

Formulation/cure technology for ultrahigh molecular

weight silphenylene-siioxane polymers

{NASA-TP-2476J p 96 N85-26990

POLYMETHYL METHACRYLATE

Solid spherical glass particle impingement studies of

plastic materials

{NASA.TP-2161 I p 95 N83-24695

POLYPHENYL ETHER

Steady-state boundary lubrication with formMated

C ethers to 260 C

[NASA-TP-1812] p 94 N81-21193

POLYTETRAFLUOROETHYLENE

Polytetrafluoroethylene transfer film studied with X-ray

photoelectron spectroscopy

I NASA-TP-1728 ] p93 N81-11214

Solid spherical glass particle impingement studies of

plastic materials

INASA-TP-2161 ] p 95 N83-24695

POLYVINYL ALCOHOL

Three methods for in situ cross-linking of pefyvinyl

alcohol films for application as ion-conducting membranes

in potassium hydroxide electrolyte --- battery separators

[NASA-TP-14071 p 78 N79-21128

POPULATIONS

Radar, Insect Population Ecology, and Pest

Management

NASAoCP-2070J p 169 N79-19592

Visible absorbance spectra: A bas_s for in situ and

passive remote sensing of phytoplankton concentration

and community composition

; NASA-TP-2094 ] p 168 N83-194 t 1

POROUS MATERIALS

Gas turbine ceramic-coated-vane concept with

convection-cooled porous metal core

NASA-TP-1942} p 48 N82-14090

PORTABLE EQUIPMENT

Preliminary applications and evaluation results.

Lixiscope: Proceedings of the Lixiscobe Conference

NASA-CP-21121 p 114 N80-t2384

POSITION (LOCATION)

Proceedings of the Workshop on an Electromagnetic

Positioning System in Space

NASA-CP-2069] p 61 N79-13069

Experimental determination of position-estimate

accuracy using back-azimuth signals from a microwave

landing system

NASA-TP-15741 p 30 N80-13020

Investigation of effects of microphone position and

orientation on near-ground noise measurements

INASA-TP-2004] p 189 N84-10913

Location of noise sources using a phase-slope

method

{ NASA-TP-25051 p 191 N86-16041

POSITIONING DEVICES (MACHINERY)

Release mechanism for releasing and reattaching

experiments on the Space Shuttle

[NASA-TP-t7021 p 121 N80-27694

POSITRONS

Moisture determination in composite materials using

positron lifetime techniques

[NASA-TP-1681 ] p 80 N80-27428

POSTMISSION ANALYSIS (SPACECRAFT)

ATS-6 engineering performance report

Volume:Program and systems summaries: Mechanical end

thermal details

INASA'RP'1080"VOL-1 } p 73 N82-16147

ATS-6 engineering performance report Volume 2: Orb, t

and attitude controls

INASA-RP-1080-VOL-2} p 73 N82-16148

ATS-6 engineering performance report. Volume 3:

Telecommunications and power

l NASA-RP-1080-VOL-3 ] p 73 N92-16149

ATS-6 engineering performance report. Volume 4:

Television experiments

{NASA-RP-t080-VOL-4 I p 73 N82-16150

ATS-6 engineering performance report. Volume 5:

Propagation experiments

INASA-RP-1080-VOL-51 p 73 N82-16151

ATS-6 engineering performance report. Volume 6:

Scientific experiments

INASA-RP-IO60-VOL-61 p 73 N82-16152

POTASSIUM HYDROXIDES

Three methods for in situ cross-linking of polyvinyl

alcohol films for application as ion-conducting membranes

m potassium hydroxide electrolyte --- battery separators

(NASA-TP-1407] p 78 N79-21128

POTENTIAL ENERGY

Flight evaluation of a simple total energy-rate system

with potential wind-shear application

[NASA-TP-1654] p 39 N81-24058

A potential-energy scaling model to simulate the initial

stages of thin-film growth

INASA-TP-2'_02} p 88 N83-18895

POTENTIAL FLOW

Computer program for calculating full potential transonic,

quasi-three-dimensional flow through a rotating

turbomachinery blade row

INASA-TP'2030} p 20 N82-28247

Test-engine and inlet performance of an aircraft used

for investigating flight effects on fan noise

[NASA-TP-22541 p 189 N94-21277

Breakdown of the conservative potential equation

{NASA-TP-25391 p 28 N86-20352

POTENTIAL THEORY

A comparative study of the nonuniqueness problem of

the potential equation

[NASA-TP-2385} p 25 N85-15694

POTENTIOMETERS (INSTRUMENTS)

Development and des_ln of three monitoring instruments

for spacecraft charging

INASA-TP.1800} p 76 N81-31282

POWDER METALLURGY

Effect of aluminum phosphate additions on compes_tion

of three-component plasma-sprayed solid lubricant

[NASA-TP-1990} p 88 N82-21298

Advanced Materials Technology

lNASA-CP-2251J p 79 N83-12147

POWER CONDITIONING

An Assessment of Integrated Flywheel System

Technology

INASA-CP-2346} p 78 N85-13850

POWER EFFICIENCY

Synchronous Energy Technology

[NASA-CP-2154J p 77 N80-33465

Comparative analyses of space-to-space central power

stations

t NASA-TP-1955] p6'6 N82-14202

POWER MODULES (STS)

Concept for a power system controller for large space

electrical power systems

INASA-TP-1939] p 77 N82-11109

POWER SERIES

The generalized Euler-Mascheroni constants

INASA-TP-2264} p 185 N84-15880

Introduction to time series analysis

[NASA-RP-11451 p 191 N86-24391

POWER SPECTRA

Stochastic analysis of spectral broadening by a free

turbulent shear layer

[NASA-TP-1816} p 188 N81-24854

Application of a computerized vibroacoustic data bank

for random vibration criteria development

{NASA-TP-19981 p 73 N82-20238

Power spectral measurements of clear-air turbulence

to long wavelengths for altitudes up 1o 14,000 meters

{NASA-TP-19791 p 164 N82-24790

Geometric interpretations of the Discrete Fourier

Transform (DFT)

tNASA-TP-2332] p 177 N84-24114

Introduction to time series analysis

[NASA-RP-1145] p 19t N86-24391

POWER SUPPLY CIRCUITS

Sealed-cell nickel-cadmium battery applications

manual

I NASA-RP-1052} p 77 N80-16095

High-voltage, high-power, solid-state remote power

controllers for aerospace applications

[NASA-TP-2437} p 78 N85-21263

POWER TRANSMISSION

Design of power-transmitting shifts

INASA-RP-1123} p 124 N84-27041

POWER TRANSMISSION (LASERS)

Space Laser Power Transmission System Studies ---

conferences

INASA-CP-2214] p t17 N92-18576

POWERED LIFT AIRCRAFT

Powered-Lift Aerodynamics and Acoustics ---

conferences

I NASA-SP-406] p 8 N78-24046

Configuration management and automatic control of an

augmentor wing aircraft with vectored thrust

i NASA-TP-1222] p 54 N79-17872

Workshop on Thrust Augmenting Ejectors

INASA-CP-20931 p 13 N80-10107

Quiet powered-lift propulsion

{NASA-CP-2077] p 46 N80-15127

Analysis of fuel-conservative curved decelerating

approach trajectories for powered-lift and CTOL let

aircraft

I NASA-TP-16501 p2 N80-19022

Flight-test of the glide-slope track and flare-control laws

for an automatic landing system for a powered-lift STOL

airplane

INASA-TP-21281 p 57 N84-13198

A-92
SUBJECT INDEX PRESSURE RATIO

PRECIPITATION (METEOROLOGY)

A comparative statistical study of long-term agreclimatic

conditions affecting the growth of US winter wheat:

Distributions of regional monthly average precipitation on

the Great Plains and the state of Maryland and the effect

of agroclimatic conditions on yield in the state of Kansas

[NASA-TP-1724] p 163 N81-22658

NASA/MSFC FY-84 Atmospheric Processes Research

Review

{NASA-CP-23291 p 166 N84-34829

PRECISION

Proceedings of the Workshop on improvements to

Photometry

[NASA-CP-23501 p 203 N85-t7892

PREDICTION ANALYSIS TECHNIQUES

Simplified sonic-boom prediction --- using aerodynamic

configuration charts and calculators or slide rules

{NASA-TP-t122] p 7 N78-20078

Predicted and experimental performance of

jet-lubricated 120-millimeter-bore ball bearings operating

to 2,5 million DN

[NASA-TP-1196} p 119 N78-20513

Correlation of laser velocimeter measurements over a

wing with results of two prediction techniques --- in the

Langley V/STOL lunnel

{NASA-TP-1168) p 105 N78-21410

Analysis of preflutter and postflutter characteristics with

motion-matched aerodynamic forces

INASA-TP-1232J p 127 N78-28481

Convective rainfall estimation from digital GOES-t

infrared data

[NASA-RP-10341 p 160 N79-31885

Estimation of attainable leading-edge thrust for wings

at subsonic and supersonic speeds

INASA-TP-1500J p 12 N80-10105

Prediction method for two-dimensional aerodynamic

losses of cooled vanes using integral boundary-layer

parameters

[NASA-TP-16231 p 14 N80-17030

Analysis of uncertainties in turbine metal temperature

predictions

{NASA-TP-1593] p 46 N80-21326

Off-design correlation for losses due to part-span

dampers on transonic rotors

[NASA-TP-1693] p 47 N80-28352

Wind-tunnel experiments on divergence of

forward-swept wings

{NASA-TP-16851 p34 N80-29287

Theoretical and experimental engine-inlet flow fields for

fighter forebodies

{ NASA-TP-22701 p 23 N84-17132

Evaluation of ride quality prediction methods for

helicopter interior noise and vibration environments

[NASA-TP-2261 I p 172 N84-20155

Triboiogy in the 80's, Volume 1: Sessions 1 to 4

[NASA-CP-2300-VOL-1 I p 124 N84-238gf

Rotorcraft noise

INASA'CP'2234] p lg0 N84-29662

An update of the total-strain version of SRP

INASA-TP-24991 p 90 N86-12295

Understanding climate: A strategy for climate modeling

end predictability research, 1985-1995

[NASA-RP-1158] p 166 N86-13866

An approximate buckling analysis for rectangular

orthotropic plates with centrally located cutouts

[NASA-TP-2528] p 135 N86-20856

PREDICTIONS

Theoretical and experimental investigation of supersonic

aerodynamic characteristics of a twin-fuselage concept

{NASA-TP-2184 ] p 22 N83-32776

PREFORMS

Effect of preforming adherends on static and fatigue

_trength of bonded composite single-lap joints

[NASA-TP-23241 p t33 N84-26053

PRELAUNCH TESTS

Prelaunch testing of the laser geodynamie satellite

(LAGEOS)

{ NASA-TP-10621 p 69 N78-10200

Moonport: A history of Apollo launch facilities and

operations

INASA-SP-4204] p 64 N79-12127

PREMIXED FLAMES

Lean premixed/prevaporlzed combustion

[NASA-CP-2016] p 84 N77-33297

A high-pressure premixed fiat-flame burner for chemical

process studies --- of poltutant formation in hydrocarbon

flames

[NASA-TP-1318 ] p84 N79-14177

Premixed Prevaporized Combustor Technology Forum

JNASA-CP-2078] p 44 N79-24994

Effect of flameholder pressure drop on emissions and

pertormance of premixed-prevaporized combustors

{NASA-TP-2131 } p 50 N83-23309

PREMIXING

Effect of fuel-air-ratio nonuniformity on emissions of

nitrogen oxides

[NASA-TP-1798i p 48 N82-13143

Combustion Fundamentals Research

[NASA-CP-22681 p 50 N83-29208

PRESSURE

Thermodynamic and related properties of oxygen from

the triple point to 300 K at pressures to 1000 bar

{ NASA-RP-1011 ] p84 N78-t6119

Fluctuating surface pressure and acoustic radiation for

subsonic normal jet impingement

{NASA-TP-1361 } p 188 N79-19813

PRESSURE DISTRIBUTION

A study of the sonic-boom characteristics of a blunt body

at a Mach number of 4.14

{NASA-TP-f015] p 1 N77.32072

Geussian step-pressure loading ol rigid viscoplastic

plates

I NASA-TP-1123 j p 127 N78-20536

Reverse-flow combustor for small gas turbines with

pressure-atomizing fuel injectors

[NASA-TP-1260] p 43 N78-27130

Elastohydrodynamic lubrication of elliptical contacts for

materials of low elastic modulus, 2: Starved

conjunction

[NASA-TP-1273] p 119 N78-28458

Design and overall performance of four highly loaded,

high speed inlet stages for an advanced high-pressure-ratio

core compressor

[NASA-TP-1337] p 43 N78-33108

Aerodynamic performance of a 1.35-pressure-ratio

axial-flow fan stage

[NASA-TP-1299] p 10 N79-10022

Effects of spanwise blowing on the surface pressure

distribution and vortex-liff cheractenstics of a trapezoidal

wing-strake configuration

[NASA-TP-12901 p 11 N79-16803

A modification to lioearized theory for prediction of

pressure ioadings on lifting surfaces at high supersonic

Math numbers and large angles of attack

[NASA-TP-1406] p 11 N79-17806

Pressure and thermal distributions on wings and adjacent

surfaces induced by elevoh deflections at Mach 6

[NASA-TP-1356] p 106 N79-20344

Fuselage and nozzle pressure distributions on a

1/12-scale F-f 5 propulsion model at transonic speeds ---

conducted in langley 16 foot transonic tunnel

INASA-TP-1521} p 13 N80-11036

A procedure for designing forebodies with constraints

on cross-section shape and axial area distribution

INASA-TP-1881 J p 17 N81-26078

Subsonic tests of an all-flush-pressure-orifice air data

system

INASA-TP-1871} p 39 N81-26144

Effects of axisymmetric and normal air jet plumes and

solid plume on cylindrical afterbody pressure distributions

at Mach numbers from 1.65 to 2.50

{NASA-TP-2005} p 19 N82-22215

Pressures, forces, moments and shock shapes for a

geometrically matched sphere-cone and hyperboloid at

Mech 20.3 in helium --- 22-inch aerodynamics leg of the

Langley hypersonic helium tunnel facility

[NASA-TP-2t00] p 1t0 N83-16675

The aerodynamic performance of several flow control

devices for internal flow systems

[NASA-TP-1972] p 59 N83-17560

Effects of flow separation and cove leakage on pressure

and heat-transfer distributions along a wing-cove-elevon

configuration at Mach 6.9 --- Langley 8-ft high temperature

tunnel test

{NASA-TP-21271 p 111 N83-28378

Pressure and heating-rate distributions on a corrugated

surface in a supersonic turbulent boundary layer

[NASA-TP-10241 p 111 N84-10504

Fuselage and nozzle pressure distributions of a

1/12-scale F-15 propulsion model at transonic speeds.

Effect of fuselage modifications and nozzle variables

I NASA-TP-2333 J p 24 N84-32354

Transonic flow analysis for rotors. Parl 1:

Three-dimensional quasi-steady, full-potential calculation

INASA-TP-2375-PT-1 } p 25 N85-10914

Flight and wind-tunnel comparisons of the inlet-airframe

interaction of the F-t 5 airplane

[NASA-TP-2374] p 37 N85-12884

Flow rate and pressure profiles for I to 4 axially alined

orifice inlets

[NASA-TP-2460J p 112 N85-27165

PRESSURE EFFECTS

Effect of pressure on structure and NO sub X formation

in CO-air diffusion flames

[NASA-TP-1448] p 84 N80-13191

PRESSURE GRADIENTS

Survey and bibliography on attainment of laminar flow

control in air using pressure gradient and suction, volume

1

[NASA-RP-1035] p 107 N79-33438

Use of nose cap and fuselage pressure orifices for

determination of air data for space shuttle orbiter below

supersonic speeds

{NASA-TP-1643] p 39 N80-32389

Crossfiow effects on steady and fluctuating pressures

on an ogive-cylinder cone-frustum model in supersonic

separated flow

[NASA-TP-1951 I p 18 N82-13108

Analytical and experimental investigation of stator

endwall countouring in a small axial-flow turbine

INASA-TP-2309J p 51 N84-32388

PRESSURE MEASUREMENT

Experimental performance of a

13.65-centimeter-tip-diameter tandem-bladed sweptback

centrifugal compressor designed for a pressure ratio of 6

INASA-TP-1091 ] p 6 N78-11002

Experimental and analytical investigation of a

nonaxisymmetric wedge nozzle st static conditions

[ NASA-TP-1188] p8 N78-26109

TACT1, a computer program for the transient thermal

analysis of s cooled turbine blade or vane equipped with

a coolant insert. 1. Users manual

[NASA-TP-1271 ] p 105 N78-28374

Fluctuating loads measured on an over-the-wing

supersonic jet model

{NASA-TP-1366} p 186 N79-16641

Aerodynamic performance of 1.38-pressure-ratio,

variable-pitch fan stage

[NASA-TP-1502} p 45 N79-31213

Wind tunnel investigation of an all flush orifice air data

system for a large subsonic aircraft --- conducted in a

Langley 8 foot transonic pressure tunnel

[NASA-TP-1642} p 38 N80-23304

Flow through aligned sequential orifice type inlets

{NASA-TP-1967] p 109 N82-20467

Pressures measured in flight on the aft fuselage and

external nozzle of a twin-jet fighter

{NASA-TP-20171 p 21 N83-25665

Hot-flow tests of a series of 10-percent-scale turbofan

forced mixing nozzles

[ NASA-TP-2268 ] p 111 N84-17525

Simplified combustion noise theory yielding a prediction

of fluctuating pressure level

[NASA-TP-2237J p t89 N84-19049

Lubrication of machine elements

{NASA-RP-1126J p 124 N84-31640

Orifice-induced pressure error studies in Langley 7- by

10-foot high-speed tunnel

[NASA-TP-25451 p 27 N86-20347

Flight measurements of surface pressures on a flexible

supercritical research wing

[NASA-TP-2501 } p 27 N86-20350

Dynamic measurement of total temperature, pressure

and velocity in the Langley 0 3-meter transonic cryogenic

tunnel

{NASA-TP-2584] p 60 N86-24709

PRESSURE OSCILLATIONS

Evaluation of flow quality in two large NASA wind tunnels

at transonic speeds

[NASA-TP-1737] p 108 N81-13303

Study of stator-vane fluctuating pressures in a turbofan

engine for static end flight tests

{NASA-TP-2217} p 189 N84-22363

Pressure probe and hot-film probe rsponses to acoustic

excitation in mean flow

{NASA-TP-2581] p 191 N86-27043

PRESSURE PULSES

Effects of repetition rate and impulsiveness of simulated

helicopter rotor noise on annoyance

{NASA-TP-1969] p 150 N82-19707

PRESSURE RATIO

Performance of single-stage axial-flow transonic

compressor with rotor and stator aspect ratios of 1.63

and 1.78, respectively, and with design pressure ratio of

1,82

INASA-TP-lg74} p 49 N82-19222

Performance of single-stage axial-flow transonic

compressor with rotor and stator aspect ratios of 163

and 1,77, respectively, and with design pressure ratio of

2.05

INASA-TP-2001 t p 49 N82-22269

Performance of a tandem-rotor/tandem-stator

conical-flow compressor designed for a pressure ratio of

3

{NASA-TP-2034 } p 20 N83-11058

Static internal performance including thrust vectoring

and reversing of two-dimensional convergent-divergent

nozzles

INASA-TP-2253] p 23 N84-18165

A-93
PRESSURE REDUCTION SUBJECT INDEX

CahbratiOn of sonic valves for the laminar flow control

leading-edge flight teat

{NASA-TP-24231 p 26 N85-23707

PRESSURE REDUCTION

Depressurizat,'on and two-phase flow of water contaming

high levels of dissolved nitrogen gas

INASA-TP-1839t p 109 N81-28389

Effect of flameholder pressure drop on emissions and

performance of premixed-prevaporized combustors

[NASA-TP-213f j p 50 N83-23309

PRESSURE REGULATORS

Applied Routh approximation

[NASA-TP-1231 ] p 98 N78-22257

PRESSURE SENSORS

A rotor-mounted digital instrumentation system for

helicopter blade flight research measurements

[NASA-TP-11461 p 38 N78-20128

Comparison of concurrent strain gage- and pressure

transducer-measured flight loads on s lifting reentry vehicle

and correlation with wind tunnel predictions

{NASA-TP-1331 1 p 10 N78-33053

Pressure probe and hot-film probe rsponses to acoustic

excitation in mean flow

INASA-TP-25811 p 191 N86-27043

PRESSURE VESSELS

Development of in situ stiffness properties for shuft_e

booster filament wound case

[NASA-TP-2377J p 83 N84.33521

PREVAPORIZATION

Effect of flameholder pressure drop on emissions and

performance of premixed-prevaporized combustors

I NASA-TP-2131 ] p 50 N83-23309

PRIMATES

The use of nonhuman primates in space

INASA-CP-005] p 169 N78-11663

PRIMERS (COATINGS)

An electrochemical study of the corrosion behavior of

primer costed 22 t 9-T87 aluminum

TNASA-TP-2459] p 90 N85-22662

The variation of corrosion potential with time for coated

metal surfaces

[NASA-TP-2636! p 91 N86-30837

PRINTED CIRCUITS

Evaluation of multitayer printed wiring boards by

meta_lographic techniques: An illustrated guide to the

preparation and inspection of plated4hrough hole test

coupons baaed on the requirements of MiI-P-55110D

{NASA-RP-1161 I p 126 N86-26639

PROBABILITY DENSITY FUNCTIONS

Analysis of random signal combinations for spacecraft

pointing stability

INASA-TP-2216I p 184 N83-33631

PROBABILITY DISTRIBUTION FUNCTIONS

Compu(er simulalion of random variables and vectors

with arbitrary probabdlty dialribuhon laws

INASA-TP-18591 p 183 N81-23838

Sp_ine methods for approximating quantile functions and

generating random samptes

JNASA-TP-23891 p 184 N85-16565

PROBABILITY THEORY

identification of dynamE systems, theory and

formulation

INASA-RP-11381 p 185 N85-19784

A formulatron and analysis of combat games

[NASA-TP-24871 p 185 N85-33745

PROBLEM SOLVING

Numerical grid generation techniques ---conference

{NASA-CP2166] p 182 N81-14690

Automated decision making and problem so_ving

Volume 2 Conference presentations

I NASA-CP-2180 VOL 2[ p 184 N81-29902

Automated Decision Making and Problem Solving

Volume f; Execulive Summary

[NASA-CP-2180 VOL I t p 184 N81-30889

The NASTRAN lheorefica_ manual

[NASA.SP.221(06)] p 132 N84-18677

The NASTRAN users manua_

[NASA-SP 222(06)1 p 133 N84-2t899

Research in Slruclures and Dynamic& 1984

INASA-CP-23351 p 134 N85 10377

Inlerachve algebraic grid-generation technique

INASA TP-25331 p 177 N86-23282

The NASTRAN demonstration problem manual, level

t75

INASA-SP-224(05)J p 130 N81-71592

PRODUCT DEVELOPMENT

Tropospheric Passive Remote Sensing

INASA-CP-223(I p 115 N82-26637

PRODUCTION MANAGEMENT

IPAD integrated Programs for Aerospace vehicle

Design

[NASA-CP-2143] p 179 N83-171t5

PROFILE METHOD (FORECASTING)

Application of modified profile analysis to function testing

of simulated CTOL transport touchdown-performance

data

lNASA-TP-1541 j p 33 N80-11069

PROFILOMETERS

An optical profilometer for spatial characterization of

three-dimensional surfaces

lNASA-TP-1012] p 113 N77-32458

PROGRAM VERIFICATION (COMPUTERS)

Production of Reliable Flight Crucial Software: Validation

Methods Research for Fault Tolerant Avionics and Control

Systems Sub-Working Group Meeting

{NASA-CP-22221 p 179 N82-24845

PROGRAMMING LANGUAGES

User's guide for SFTRAN/360

[NASA-TP-t006I p 178 N78-10746

Tools for Embedded Computing Systems Software

[NASA-CP-2064] p 178 N79-13736

PROGRAMS

NASA/MSFC FY-81 Atmospheric Processes Research

Review

{NASA-CP.2204} p 164 N82.16660

PROJECT MANAGEMENT

Astronautics and aeronautics, 1974: A chronology

{NASA-SP-4019] p 212 N78-12997

A critical review of the life sciences project management

at Ames Research Center for the Spaoelab Mission

development test 3

INASA-TP-1364/ p 196 N79-16709

IPAD: Integrated Programs for Aerospace-vehicle

Design

INASA-CP-2143] p 179 N83-17115

Living and working in space A history of Skylab

INASA'SP-42081 p 63 N84-25737

The management of research institutions: A look at

government laboratories

[NASA-SP-481J p 196 N85-16665

Space Station Software Issues

[NASA-CP-2361 I p t 79 N85-20689

Space Station Software Recommendations

INASA-CP-23941 p 180 N86-23314

Supercrihcal wing technology: A report on flight

evaluations

I NASA-SP-301 I p 6 N77-85474

PROJECT SETI

The search for extraterrestrial intelligence (SETI)

{NASA-SP-419] p 175 N78-18771

A bibliography on the search for extraterrestrial

intelligence

INASA-RP-1021 I p 199 N78-21019

SETI science working group report

tNASA-TP-22441 p 175 N84-22178

Second Symposium on Chemical Evolution and the

Ongin of Life

{NASA-CP-24251 p 175 N86-26844

PROJECTILES

Symmetry considerations in the scattering of identical

composite bodies

[NASA-TP-2548 J p 193 N86-23388

PROJECTIVE GEOMETRY

Nonlinear optimization with linear constraints using a

projecbon method

INASA-TP-20861 p 184 N83-10876

PROPAGATION MODES

The wave structures of the Eady model of baroclinic

inslability

{ NASA TP 15481 p 160 N79-32796

Theoretical prediction of nonhnear propagation effects

on no_se signatures generated by subsonic or supersonic

propeller or rotor-blade tips

[NASA-TP-1660] p 14 N80-22265

ATS-6 engineenng performance reporl Volume 5

Propagation experiments

INASA-RP-1080-VOL-5] p 73 N82-16151

PROPANE

Effects of percentage el blockage and flameholder

downstream ceunlerborea on lean combustion limits of

premlxed, prevaporized propane-air mixture

[NASA-TP-2227 j p 50 N83-34941

PROPELLANT TANKS

Purging of a tank-mounted multilayer insulation system

by gas diffusion

[NASA-TP-t 127 I p 65 N78-17127

Contoured tank outlets for draining of cylindrical tanks

in low-gravity environment Lewis Research Center Zero

Grawty Facility

[NASA-TP-1492] p 107 N79-29467

Hydroelaatic vibration analysis of partially liquid-filled

shetls using a series representation of the liquid

INASA-TP-1558i p 129 N80-19563

PROPELLER BLADES

An experimental and analytical investigation of proprotor

whirl flutter

INASA-TP-1047J p 6 N78-12039

A numerical technique for calculation of the noise of

high-speed propellers with advanced blade geometry

[NASA-TP-16621 p 187 N80-27161

The high-speed frontier Case histories of four NACA

programs, 1920- 1950

[NASA-SP-445} p 3 N81-15969

Optimization and performance calculation of

dual-rotation propellers

INASA-TP-19481 p 3 N82-14049

The compressible aerodynamics of rotating blades

based on an acoustic formulation

{NASA-TP-2197] p 189 N84-13923

Annoyance caused by propeller airplane flyover noise

{ NASA-TP-23561 p 190 N84-32124

Effects of propeller rotation direction on airplane interior

noise levels

[NASA-TP-2444} p 190 N85-30767

PROPELLER DRIVE

A theoretical investigation of noise reduction through

the cyiir'K;Irical fuselage of a twin-engine, propeller-driven

aircraft

[NASA-TP-1325] p 186 N79-1382t

PROPELLER EFFICIENCY

Subsonic aircraft: Evolution and the matching of size

to performance

[NASA-RP-10601 p 2 N80-29245

PROPELLER SLIPSTREAMS

Experimental study of the effects of installation on

singleand counter-rotation propeller noise

{NASA-TP-2541 ] p 191 N86-26162

PROPELLERS

Advanced aerodynamics Selected NASA research

INASA-CP-2208] p 4 N84-27660

Analysis of noise measured from a propeller in a wake

I NASA-TP-2358 ] p 190 N85-11788

Direotivib/and trends of noise generated by a propeller

in a wake

INASA-TP-2609] p 191 N86-31341

PROPULSION

Liquid hydrogen as a propulsion fuel, 1945-1959

INASA-SP-4404J p 97 N79-16994

Bibliography of Supersonic Cruise Research (SCR)

program from 1977 to mid-1980

[NASA-RP-1063J p 16 N81-14973

PROPULSION SYSTEM CONFIGURATIONS

Effect of propulsion system charactenstios on ascent

performance of dual-fueled single-stage earth-to-orbit

transports

INASA-TP-11151 p 65 N78-13109

General Aviation Propulsion

INASA-CP-21261 p 46 N80-22327

Large Space Systems/Low-Thrust Propulsion

Technology

INASA-CP-2144j p 77 N80-31449

Thrust-induced effects on subsonic longitudinal

aerodynamic characteristics of a

veclored-engine-over -wing configuration

{NASA-TP-22281 p 22 N84-13163

Effect of thrust reverser operation on the

_ateral-direclional characteristics of a three-surface F-15

model at transonic speeds

I NASA-TP-22341 p 22 N84-13165

OTV Propulsion Issues

INASA-CP-23471 p 67 N85-16989

Rail accelerators for space transportation: An

experimental investigation

I NASA-TP-2571 } p 78 N86-28123

PROPULSION SYSTEM PERFORMANCE

Parametric study of ascent performance of a vertically

launched hydrogen-fueled single-stage reusable

transport

INASA-TP-f045] p 65 N78-10186

Airflow and thrust calibrahon of an E100 engine, S/N

P680059, at selected flight conddions

INASA-TP-10691 p 42 N78-21112

Aeropropulsion 1979 --- conferences

{NASA-CP-2092} p 45 N80-10205

Dynamic response el a Mach 25 axisymmetric inlet and

turbojet engine with a poppet-value controlled inlet stability

bypass system when Sublected to internal and external

airflow transients

INASA-TP-1531 I p 45 N80-14123

Propulsion Controls, 1979 --- air breathing engine

control

INASACP-2137J p47 N81 12090

Impacl for the 80's: Proceedings el a Conference on

Selected Technology for Business and Industry

INASA-CP-21491 p 212 N81-12978

Gain selection method and model for coupled propulsion

and airframe systems

I NASA-TP-2067 t p57 N83-11139

Effects of varying podded nacelle-nozz_e installations

on transonic aeropropulsive characteristics of a supersonic

fighter aircraft

INASA-TP-21201 p 2! N83-26821

A-94
SUBJECT INDEX

Space Shuttle Technical Conference, part 2

[NASA.CP.2342-PT.2] p 63 N85-16937

Performance and surge limits of a TF30.P.3 turbofan

engtne/axisymmetric mixed-compression inlet propulsion

system at Mach 2.5

[NASA-TP-2461] p 52 N85-2526t

PROPULSIVE EFFICIENCY

Subsonic aircraft: Evolution and the matching of size

to performance

[NASA-RP.1060] p 2 N80.29245

PROTECTIVE CLOTHING

Nitrogen dioxide vapor penetration of chlorobutyl rubber

SCAPE under operational conditions

[NASA-TP.t805] p 85 N80.16118

PROTECTIVE COATINGS

Ceramic coating effect on liner metal temperatures of

film-cooled annular combustor

[NASA-TP-1323] p 44 N79-t4098

Development of silane.hydrolysate binder for

UV-reaistsnt thermal control coatings

[NASA-TP-1900] p 94 N81-31365

Thermal and aerothermal performance of a titanium

muffiwall thermal protection system

[NASA-TP-1961] p 72 N82-14277

Effect of aluminum phosphate additions on composition

of three-component plasma-sprayed solid lubricant

[NASA-TP-1990] p 88 N82-21298

Turbine Engine Hot Section Technology (HOST)

[NASA-CP-2289] p 135 N86-11495

Thermal-fatigue and oxidation resistance of

cobalt-modified Udimet 700 alloy

[NASA-TP-2591 ] p 135 N86-28464

The variation of corrosion potential with time for coated

metal surfaces

[NASA-TP-2636] p 9t N86-30837

PROTECTORS

Flow through very porous screens

[NASA-TP-2436] p 112 N85-20270

PROTON IRRADIATION

Proton-induced noise in digicons

[NASA-TP-t852] p 76 N81-31281

PROTOTYPES

A numencal simulation of three-dimensional flow in an

adaptive wall wind tunnel

[NASA-TP-2351] p 24 N84-28750

PROVING

Validation of a fault-tolerant clock synchronization

system

[NASA-TP-2346J p 180 N84-34198

Peer Review of a Formal VerificationDesign Proof

Methodology

[NASA-CP-2377 J p 179 N85-28609

Baseline experiments in teleoperator control

[NASA-TP-25471 p 174 N86-26836

PSEUDORANDOM SEQUENCES

Generation of pseudo-random numbers

(NASA-TP-21051 p 183 N83-16095

PSYCHOACOUSTICS

Effects of duration and other noise characteristics on

the annoyance caused by aircraft-flyover noise

[NASA-TP-13861 p 186 N79-20832

Effects of road traffic background noise on judgments

of individual airplane noises

[NASA-TP-t433] p 148 N79-28796

Effects of sound level fluctuations on annoyance caused

by aircraft-flyover noise

fNASA-TP-t576J p 187 N80-13880

Subjective field study of response to impulsive helicopter

noise

[NASA-TP-1833J p 187 N81-21873

Effects of activity interference on annoyance due to

aircraft noise

[NASA-TP-1938] p 149 N82-12654

Multiple-event airplane noise annoyance

[NASA-TP-2101J p 150 N83-t6951

Annoyance caused by propeller airplane flyover noise

(NASA-TP-2356] p 190 N84-32124

PSYCHOLOGICAL EFFECTS

Effects of duration and other noise characteristics on

the annoyance caused by aircraft-flyover noise

[NASA-TP-1386} p 186 N79-20832

Multiple-event airplane noise annoyance

[NASA-TP-21011 p 150 N83-t6951

PSYCHOLOGICAL FACTORS

Management system, organizational climate and

performance relationships

[NASA-TP-1417) p 196 N79-tggt2

Living aloft: Human requirements for extended

spaceflight

[NASA-SP-483] p 174 N85.32772

PSYCHOPHYSIOLOGY

The window of visibility: A psychological theory of fidelity

in time-sampled visual motion displays

[NASA-TP-2211 J p 172 N83-33538

PUBLIC HEALTH

Report of the NASA working group on tropospheric

program planning

INASA-RP.1062] p 153 N81-23742

PULSE CODE MODULATION

High-density digital recording

[NASA-RP-ltft] p 103 N86-14498

PULSE RATE

Effects of repetition rate and impulsiveness of simulated

helicopter rotor noise on annoyance

[NASA-TP-t969] p 150 N82-19707

PULSED LASERS

Prelaunch testing of the GEOS-3 laser reflector array

INASA-TP-1138] p 117 N78-16354

Simulated electronic haterodyne recording and

processing of pulsed-laser holograms

[NASA-TP.1444] p 114 N79-21329

PURGING

Purging of a tank-mounted multilayer insulation system

by gas diffusion

[NASA-TP-1127] p 65 N78-17127

Water-vapor pressure control in a volume

[NASA-TP-1172] p 147 N78-20654

Electrical enclosure hydrogen intrusion study --- purging

Cape Kennedy Launch Complex 39

[NASA-TP-1461 ] p 191 N79-25861

PYLON MOUNTING

Aerodynamic characteristics of a high-wing transport

configuration with a over-the-wing nacelle-pylon

arrangement

[ NASA'TP-24971 p27 N86-16193

PYLONS

Nacelle/pylon/wing integration on a transport model

with a natural laminar flow nacelle

INASA-TP'2439] p 26 N85-29924

Experimental study of the effects of installation on

singleand counter-rotation propeller noise

lNASA-TP-2541 ] p 191 N86-26162

PYROLYSIS

Fuel-rich catalytic combustion: A soot-free technique

for in situ hydrogen-like enrichment

[NASA-TP-2498J p 85 N85-31244

PYROLYTIC GRAPHITE

Secondary electron emission characteristics of

ion-textured copper and high-purity isotropic graphde

surfaces

[ NASA-TP-2342] p 95 N84-28989

PYROTECHNICS

Shock response spectra variational analysis for

pyrotechnic qualification testing of flight hardware

INASA-TP-2315] p 74 N84-23676

Q

QUADRATIC EQUATIONS

ORACLS: A system for linear-quadratic-Gaussian

control law design

[NASA-TP-ltO6; p 181 N78-22809

Decoupled and Iinear quadratic regulator control of a

large, fiexibie space antenna with an observer in the controt

loop

[NASA-TP-24841 p 75 N86-t6250

QUALITY CONTROL

Summary report: Workshop on Vehicle Ride Quality

[NASA-CP-20131 p 172 N78-11705

Spacecraft transmitter reliability

{NASA-CP-2t5g] p 76 N8t-16119

NASA Metrology and Cs;ibration, 1980

INASA-CP-2174] p 115 N81-23432

High Temperature Polymer Matrix Composites

I NASA-CP-2385] p 83 N86-t t260

Evaluation of multitayer printed wiring boards by

metallographic techniques: An illustrated guide to the

preparation and inspection of plated-through hole test

coupons based on the requirements of MiI-P-55110D

[NASA-RP-t 161J p 126 N86-26639

QUANTILES

Spline methods for approximating quantile functions and

generating random samples

[NASA-TP-2389J p 184 N85-16565

Statistical analysis of direct-strike lightning data (1980

to 1982)

INASA-TP-22521 p 167 N86-24090

QUANTITATIVE ANALYSIS

Quantitative analysis of aircraft mudispectral-scanner

data and mapping of water-quality parameters in the James

River in Virginia

[NASA-TP-t021 ] p 147 N78-t3628

Quantitative mapping by remote sensing of an ocean

acid-waste dump

[NASA-TP-12751 p 147 N78-33617

Rapid estimation of concentration of aromatic classes

in middistillate fuels by high-performance liquid

chromatography

[NASA-TP-2495J p 98 N85-31307

RADIANT COOLING

QUANTUM EFFICIENCY

Comparative performance of HgCdTe photodiodes for

heterodyne application

fNASA-TP-1745] p 101 N80-33683

QUANTUM MECHANICS

An abrasion-ablation model description of galactic

heavy-ion fragmentation

[NASA.TP.2305] p 192 N84.22396

QUARTZ

Characterization of soil and postlaunch pad debris from

Cape Canaveral launch complex and analysis of soil

Interaction with aqueous HCI

[NASA-TP-2076] p 150 N83-t2595

QUASARS

Advances in Ultraviolet Astronomy: Four Years of IUE

Research

[ NASA-CP.2238] p201 N82-3t 163

QUENCHING (COOLING)

Microstructure and mechanical properties of quenched

and tempered 300M steel

[NASA-TP.1288] p 127 N78.30610

QUIET ENGINE PROGRAM

Static test-stand performance of the YF-102 turbofan

engine with several exhaust configurations for the Quiet

Shorf-Haul Research Aircraft (QSRA)

[NASA-TP-1556] p 45 N80-14121

Quiet powered.lift propulsion

(NASA-CP-2077] p 46 N80-15127

Low-speed aerodynamic performance of

50.8-centimeter-diameter noise-suppressing inlets for the

Quiet, Clean, Short-haul Experimental Engine (QCSEE) ---

Lewis 9- by 15-foot low speed wind tunnel tests

INASA-TP-11781 p 47 N81-11037

R

Population

RADAR

Radar, Insect Ecology. and Pest

Management

[NASA-CP-2070] p 169 N79-19592

RADAR IMAGERY

Synthetic aperture radar/LANDSAT MSS image

registration

[NASA-RP*1039] p t39 N80-16405

RADAR MEASUREMENT

NASA Wallops Flight Center GEOS-3 altimeter data

processing reporl

INASA-RP-t066] p 139 N81-11438

Airborne ]idar measurements of El Chichon stratospheric

aerosols, October t 982 to November 1982

{NASA-RP-1136] p t55 N85-19550

RADAR TRACKING

Precision positional data of general aviation air traffic

in terminal air space

[NASA-RP-t020] p 1 N78-2,5048

RADIAL DISTRIBUTION

Low-frequency fluctuation spectra and associated

particle transport in the NASA Lewis bumpy*torus

plasma

[NASA-TP-1258] p 194 N78-30944

RADIAL FLOW

Computer code for off-design performance analysis of

radial-inflow turbines with rotor blade sweep

[NASA-TP-2199] p 50 N83-32807

RADIANCE

Laboratory measurements of radiance and reflectance

spectra of dilute primary-treated sewage sludge

[NASA-TP-1038] p 147 N78-12554

Laboratory measurements of upwelled radiance and

reflectance spectra of Catvert, Ball, Jordan. and Feldspar

soil sedimer.ts

INASA-TP-1039] p t67 N78-12645

Laboratory measurements of radiance and reflectance

spectra of a dilute biosotid industrial waste product

[NASA-TP-1401 ] p 148 N79-17360

Spectral flame radiance from a tubular-can combustor

INASA-TP-1722] p 48 N81-t9121

Laboratory upwelled radiance and reflectance spectra

of Kerr reservoir sediment waters

{NASA-TP-t 9931 p 150 N82-21774

User's guide for the Solar Backscattered Ultraviolet

(SBUV) and the Total Ozone Mapping Spectrometer

(TOMS) RUT-S and RUT-T data sets: October 31, 1978

to November 1. 1980

{NASA-RP-11121 p 165 N83-28828

Antartic sea ice, 1973 1976: Satellite

passive-microwave observations

INASA-SP-459] p 168 N84-10718

Site selection and directional models of deserts used

for ERBE validation targets

{NASA-TP-25401 p 167 N86-23160

RADIANT COOLING

Ftightweight radiantly and actively cooled panel:

Thermal and structural performance

[NASA-TP-2074] p 131 N83-11513

A-95
RADIANT FLUX DENSITY

RADIANT FLUX DENSITY

Simulation study of s geometric shape factor technique

for estimating earth-emitted radiant flux densities from

wide-field-of-view radiation measurements

ENASA-TP-1629} p 161 N80-20986

Comparison ol clata inversion techniques for remotely

sensed wide-angle observations of Earth emitted

radiation

{NASA-TP-1924J p 164 N82-13620

RADIANT HEATING

Reinforced carbon-carbon oxidation behavior m

convective and radiative environments

[NASA-TP-1284] p 106 N78-30555

RADIATION ABSORPTION

A simplified method for calculating the atmospheric

heating rate by absorption ol solar radiation in the

stratosphere and mesosphere

INASA-TP-t398t p 159 N79-16493

Electron and proton absorption calculations for a

graph*te/epoxy composite model --- large space

structures

[ NASA-TP- 1568 ] p 93 N80-11226

RADIATION BELTS

Proton-induced noise m digicons

[NASA-TP-1852] p 76 N81-31281

RADIATION DAMAGE

Solar Cell High Efficiency and Radiation Damage

LNASA-CP-2020J p 144 N78-13527

Annealing of radiation damage in 01- and

2-ohm-centimeter Silicon solar cells

INASA-TP-15591 p 145 N79-33572

Space Photovoltaic Research and Technology 1980

High Efficiency, Radiation Damage and Blanket

Technology

INASA-CP-21691 p 145 N81-17531

Computer program for pulsed thermocouples with

corrections for radiation effects

INASA TP 18951 p 179 N81-33838

A simple model of space radiation damage in GBAs solar

celts

{NASA-TP-2242] p 192 N84-13978

Space Photovoitaic Research and Technology 1983.

High Efficiency, Radiation Damage. and Blankel

Technology

ENASA-CP-2314] p 146 N84-29307

RADIATION DISTRIBUTION

Simulation studies of wide and medium field of view

earth radiation data analysis

INASA-TP-11821 p 158 N78-23679

RADIATION DOSAGE

Human expOsure in low Earth orbit

INASA-TP-2344 } p 174 N84-29479

RADIATION EFFECTS

NASA Workshop on Solar-Terrestrial Studies from a

Manned Space Station

{NASA-CP-20241 p t36 N77-32549

Human exposure in low Earth orbit

[NASA-TP-2344] p 174 N84-29479

Spectroscopic analysis of radiation-generated changes

in tensile properties o( a potyethenmide film

[NASA-TP-2429} p 83 N85-25435

RADIATION MEASUREMENT

Significant initial results from the environmental

measurements experiment on ATS-6

[NASA-TP-t 101 } p 65 N78-15142

Parameter estimation applied to Nimbus 6 wide-angle

Iongwave radiation measurements

[NASA-TP-13071 p 159 N79-13644

Earth Radiation Budget Science, 1978 --- conferences

[NASA-CP-21001 p 160 N79-32797

Simulation study of a geometnc shape factor technique

for estimating earth-emitted radiant flux densities from

w_de-tield-of-view radiation measurements

[NASA-TP-16291 p t61 N80-20986

Surface radiation budget for climate applications

[NASA-RP-ff69} p 167 N86-28574

RADIATION PYROMETERS

Surface pyrometry in presence of radiation from other

sources with application to turbine blade temperature

measurement

[NASA-TP-1754} p 47 N81-11039

RADIATION SHIELDING

Human exposure in low Earth orbit

[NASA-TP-2344} p 174 N84-29479

Electromagnetic dissociation effects in galactic

heavy-ion fragmentation

[NASA-TP-2527 ] p 211 N86-21492

RADIATION THERAPY

Hyperthermia as an Antineoplastic Treatment Modali_

[NASAoCP-2051 I p 170 N79-t0728

RADIATION TOLERANCE

Solar Cell High Efficiency and Radiation Damage,

1979

INASA-CP-20971 p 144 N79-32640

RADIATIVE HEAT TRANSFER

Earth Radiation Budget Science, 1978 --- conferences

[NASA-CP-2100] p 160 N79-32797

RADIATIVE TRANSFER

An asymptotic expansion approach to the inverse

radiative transfer problem --- to infer concentration profiles

of the atmosphere from measurements made onboard a

satellite

INASA-TP-'I587] p 152 N80-13730

A tutorial solution to scattering of radiation in a thin

atmosphere bounded below by a diffusely reflecting,

absorbing surface

[NASA-TP-2077} p 154 N82-33918

Comparative accuracy of the Albedo, transmission and

absorption for selected radiative transfer approximations

[NASA-RP-11601 p 156 N86-22022

Present state of knowledge of the upper atmosphere:

An assessment report; processes that control ozone and

other climatically important trace gases

[NASA-RP-1162] p 156 N86-25911

introduction to the theory of atmospheric radiative

transfer

INASA-RP-1156} p 157 N86-27839

Surface radiation budget for climate applications

[NASA-RP-1169] p 167 N86-28574

RADIO ALTIMETERS

NASA Wallops Flight Center GEOS-3 altimeter data

processing report

{NASA-RP-1066] p 139 N81-11438

NOSS altimeter algonfhm specifications

[NASA-RP-f083] p 168 N82-16683

RADIO ASTRONOMY

Recognition of compact astrophysical objects

[NASA-SP-4211 p 201 N77-34063

An assessment of ground-based techniques for

detecting other planetary systems Volume 1 : An overview

--- workshop conclusions

[NASA-CP-2124-VOL-t I p 201 N80-18997

SETI science working group report

I NASA-TP-2244] p 175 N84-22178

RADIO CONTROL

Miniature flow-direction and airspeed sensor for

airplanes and radio controlled models in spin studies

[NASA-TP-1467] p 38 N79-23081

RADIO FREOUENCY DISCHARGE

RF radiation produced by inlrscloud lightning

discharges

(NASA-TP-14541 p 160 N79-22708

Analytical prediction and experimental verification of

performance at vanous operating conditions of a

dual*mode traveling wave tube with multistage depressed

collectors

lNASA-TP-1831 ] p 102 N81-28352

Three-dimensional relativistic field-electron interaction

in a multicavity high-power klystron Part 2: Working

Equations

[NASA-TP-2008} p 102 N82+23397

RADIO FREQUENCY HEATING

Hyperfhermia as an Antineoplastic Treatment Modality

|NASA-CP-2051] p 170 N79-f0728

RADIO FREOUENCY INTERFERENCE

Rate statistics for radio noise from lightning

[NASA-TP-1665] p 161 N80-23933

RADIO NAVIGATION

ATS-6 engineering performance report Volume 5:

Propagation experiments

[NASA-RP-10B0-VOL-51 p 73 N82-16151

RADIO TRACKING

Free Drifting Buoys

[NASA.CP-2003] p 167 N77-16675

RADIO TRANSMISSION

Radio-wave propagation for space communications

systems

[NASA-TP-1770] p 70 N81-18082

RADIOACTIVE WASTES

Nuclear waste disposal in space

INASA-TP-1225] p 144 N78.23571

Disposal of radioactive iodine in space

INASA-TP-1313] p 172 N78-31740

RADIOCHEMISTRY

Assessment of Techniques for Measuring Troposphenc

H sub x 0 sub y

{NASA-CP-2332} p 155 N85-t4336

RADIOMETERS

Estimation of soow temperature and mean crystal radius

from remote muttispectral passive microwave

measuremenls

[NASA-TP-1251 J p 151 N78-26677

Sea-surface temperature and salinity mapping from

remote microwave radiometric measurements of

brightness temperature

[NASA-TP-f077] p 168 N79-28863

Flight Technology Improvement --- spaceborne optical

radtometric instruments, atlitude control, and

electromechanieaf and power subsystems

[NASA-CP-2101 } p 75 N80-13152

SUBJECT INDEX

Simulation study of a geometric shape factor technique

for estimating earth-emitted radiant flux densities from

wide-field-of-view radiation measurements

[NASA-TP-1629] p 161 N80-20986

Aliased noise in rad_ometric measurements

INASA-TP-16391 p 114 N80-22860

High speed lookup table approach to radiometr,'c

calibration of multispeotral image data

INASA-TP-1741 ] p 76 N80-33463

Earth Radiation Science Seminars

INASA-CP-2239} p 210 N82-33320

RADIOMETRIC CORRECTION

LANDSAT-4 Science Investigations Summary, including

December 1983 Workshop results, volume 1

{E84-10166} p 137 N84-30359

LANDSAT-4 Science Investigations Summary, including

December 1983 Workshop results, volume 2

[E84-101671 p 137 N84-30380

RADIOMETRIC RESOLUTION

LANDSAT-4 Science Investigations Summary, including

December 1983 Workshop results, volume 2

IE84-10167J p 137 N84-30380

LANDSAT-4 Science Characterization Early Results.

Volume 3, part 2: Thematic Mapper (TM)

IE85-10069] p 143 N85-21724

RADIOSONDES

Wind-weighting for sounding rockets with a telemetry

system

[NASA-TP-2438J p 70 N85-21246

RAILGUN ACCELERATORS

Rail accelerators for space transportation: An

experimental investigation

{NASA-TP-2571 ] p 78 N86-28123

RAIN

Satellite-derived global oceanic rainfall atlas (1973 and

1974)

iNASA-SP-410] p 157 N77-19709

Convective rainfall estimation from digital GOES-f

infrared data

{NASA-RP-1034J p 160 N79-31885

Propagation effects handbook for satellite systems

design. A summary of propagation impairments on 10

1o t00 GHz satellite links with techniques for system

design

{NASA-RP-1082(03)J p 100 N83-29491

RAINBOWS

Rainbow Schlieren

[NASA-TP-2166] p 116 N83-33f26

RAMJET MISSILES

An experimental wind-tunnel investigation of a

ram-air-spoiler roll-control device on a forward-control

missile at supersonic speeds

INASA-TP-1353] p 11 N79-17809

RAMP FUNCTIONS

Rapid estimation of frequency response functions by

close-range photogrammetry

[NASA-TP-2471 ) p 116 N86-12579

RANDOM ACCESS

Nimbus 6 Random Access Measurement System

applications expenments

[NASA-SP-457] p 165 N83-14835

RANDOM ACCESS MEMORY

NASF transposition network: A computing network for

unscrambling p-ordered vectors

{NASA-TP-1426] p 180 N79-21822

RANDOM NUMBERS

Generation of pseudo-random numbers

{NASA-TP-2105] p 183 N83-16095

An efficient algorithm for generating random number

pairs drawn from a bivanate normal distnbution

[NASA-TP-2173] p 184 N83-27679

RANDOM SAMPLING

Spline methods for approximating quantile functions and

generating random samples

[NASA.TP-2389] p 184 N85-16565

RANDOM SIGNALS

Analysis of random signal combinations for spacecraft

pointing stability

[NASA-TP-2216] p 184 N83-33631

RANDOM VARIABLES

Computer simulation of random variables and vectors

with arbitrary probability distribution laws

INASA-TP-1859] p 183 N81-23838

Analysis of random signet combinations for spacecraft

pointing stability

[NASA-TP-2216] p 184 N83-33631

RANDOM VIBRATION

Effect of vibration duration on human discomfort ---

passenger comfort and random vibration

{NASA-TP-1283} p 171 N78-32717

Application of s computerized vibroacoustic data bank

for random vibration criteria development

[NASA-TP-19981 p 73 N82-20238

A-96
SUBJECTINDEX REFRIGERATORS

RANDOM WALK

Monte Carlo lattice models for adsorbed polymer

conformation

INASA-TP-2453] p 195 N85-24961

RANGE ERRORS

Simulation study of traffic-sensor noise effects on

utilization of traffic situation display for self-spacing task

[NASA-TP-2082] p 40 N83-18723

RANGER PROJECT

Lunar impact: A history of Project Ranger

{NASA-SP-4210] p 65 N78-15149

RANGES (FACILITIES)

A new dimension. Wallops Island flight test range: The

first fifteen years

[NASA-RP-1028J p 64 N79-20166

RANKINE-HUGONIOT RELATION

Local stability analysis for a planar shock wave

{NASA-TP-2387] p 25 N85-12864

RARE GASES

Analysis of the physical atomic forces between noble

gas atoms, alkali ions and halogen ions

[ NASA-TP-2568} p 90 N86-26413

RAREFIED GAS DYNAMICS

The aerodynamics of bodies in a rarefied ionized gas

with applications to spacecraft environmental dynamics

INASA-TP-1933] p 72 N82-15116

RAWlNSONDES

Development of a procedure to model high-resolution

wind profiles from smoothed or low-frequency data

[NASA-TP-1071 ] p 158 N78-11642

Determination of wind from NIMBUS 6 satellite sounding

data

{NASAoRP-1072] p 162 N81-15639

A comparative analysis of rawinsonde and NIMBUS 6

and TIROS N satellite profile data

{NASA-RP-t070} p 162 N81-15640

Comparisons between Nimbus 6 satellite and

rawinsonde soundings for several geographical areas

[NASA-RP-1073] p 163 N81-16679

An evaluation and comparison of vertical profile data

from the VISSR Atmospheric Sounder (VAS)

[NASA-TP-2425] p 166 N85-16351

RAYLEtGH SCATTERING

Estimation of snow temperature and mean crystal rsdius

from remote multispectral passive microwave

measurements

[NASA-TP-1251J p 151 N78-26677

REACTION KINETICS

Chemical kinetic modeling of benzene and toluene

oxidation behind shock waves

[NASA-TP-1472| p 84 N79-2825g

Chemical kinetic models for combustion of hydrocarbons

and formation of nitric oxide

{NASA-TP-1794] p 85 N81-14017

Chemical kinetic analysis of hydrogen-air ignition and

reaction times

[NASA-TP-1856] p 85 N81-27223

Ignition of SiH4-H2-O2-N2 behind reflected shock

waves

[NASA-TP-2114} p 50 N83-18727

A chemical kinetic mixture for the ignition of

silane/hydrogen mixtures

{NASA-TP-2129] p 85 N83-19825

Rate processes in gas phase

{NASA-RP-1090] p 192 N83-27809

Combustion Fundamentals Research

[NASA-CP-2268] p 50 N83-29208

Nonlinear Constitutive Relations for High Temperature

Applications

[NASA-CP-2271 } p 132 N83-34351

Threshold kinetics of a solar-simulator-pumped iodine

laser

. INASA-TP-2241 ] p 118 N84-17575

Chemical mechanisms and reaction rates for the

initiation of hot corrosion of IN-738

{NASA-TP-2319] p 90 N84-28958

GCKP84-general chemical kinetics code for gas-phase

flow and batch processes including heat transfer effects

INASA-TP-2320] p 85 N84-32446

Comparison of numerical techniques for integration ot

stiff ordinary differential equations arising in combustion

chemistry

[NASA-TP-2372J p 51 N85-t0065

Ignition of mixtures of Sill sub 4, CH sub 4, O sub 2,

and Ar or N sub 2 behind reflected shock waves

{NASA-TP-2415J p 52 N85-22395

Physical and numerical sources of computational

inefficiency in integration of chemical kinetic rate

equations: Etiology, treatment and prognosis

[NASA-TP-2590] p 183 N86-28662

REAL GASES

Simulation of ideal-gas flow by nitrogen and other

selected gases at cryogenic temperatures --- transonic flow

in cryogenic wind tunnels

{NASA-TP-1901 } p 109 N81-32418

REAL TIME OPERATION

Flutter Testin, I Techniques

(NASA-SP-415 p 1 N77-21022

Concept report: Microprocessor control of electrical

power system

INASA-TP-1016 p 100 N77-30367

Development and verification of real-time, hybrid

computer simulation of F100-PW-100(3) turbofan engine

[NASA-TP-1034 p 41 N77-31154

A descgn approach to real-time formatting of high speed

multispectral image data

[NASA-TP-1870 p 178 N81-25690

Comparison of simulator fidelity model predictions with

in-simulator evaluation data

{NASA-TP-2106 p 36 N83-18715

Development of an instrument for real-time computation

of indicated mean effective pressure

INASA-TP-2238 p 102 N84-16461

Operating system for a real-time multiprocessor

propulsion system simulator. Users manual

I NASA-TP-2426 p 180 N65-17596

Real-Time Multiprocessor Programming Language

(RTMPL) user's manual

[NASA-TP-2422 p 179 N65-28610

Analytical techniques of pilot scanning behavior and their

application

{NASA-TP-2525 p 172 N86-27920

Hybrid routing technique for a fault-tolerant, integrated

information network

{NASA-TP-2605 p 180 N86-27947

REAL VARIABLES

A characterization of the real zeros of a particular

transcendental function

[NASA-TP-1420} p 185 N79-18679

REAI-FACHED FLOW

Inverse boundary-layer theory and comparison with

experiment

[NASA-TP-1208] p 106 N78-32385

RECEIVERS

A comparative study of optimum and suboptimum

direct-detection laser ranging receivers

{NASA-TP-13151 p 117 N78-31413

RECEPTION DIVERSITY

Diversity techniques for omnidirectional telemetry

coverage of the HiMAT research vehicle

{NASA-TP-18301 p 39 N81-20074

RECOVERY PARACHUTES

Spin-tunnel investigation of the spinning characteristics

of typical single-engine general aviation airplane designs.

2: Low-wing model A; tail parachute diameter and canopy

distance for emergency spin recovery

INASA-TP-1076] p 6 N78-12040

RECTANGLES

Etastohydr_. tynamic lubrication of rectangular contacts

INASA-TP-2111} p 123 N83-16759

RECTANGULAR PANELS

Noise transmission through flat rectangular panels into

a closed cavity --- light aircraft noise

{NASA-TP-1321 } p 186 N79-14874

Noise transmission loss of a rectangular plate in an

infinite baffle

[NASA-TP-23981 p t90 N85-22109

RECTENNAS

Solar Power Satellite Microwave Transmission and

Reception

[NASA-CP-21411 p 145 N81-16533

Satellite power system: Concept development and

evaluation program Volume 3: Power transmission and

reception. Technical summary and assessment

INASA-RP-1076} p t45 N81-27622

REDUCED GRAVITY

Optical observations of unidirectional solidification in

microgravity

[NASA-TP-21101 p 88 N83-16492

Liquid management in low gravity using baffled rotating

containers

{NASA-TP-2263 } p 111 N84-15427

Second Symposium on Space Industrialization --- space

commercialization

[NASA-CP-2313J p 63 N85-11011

Fluid surface behavior in low gravity. Center

discretionary fund no, 83-21

I NASA-TP-2486} p 113 N85-28260

The 1985 Get Away Special Experimenter's

Symposium

I NASA-CP-2401 } p 63 N86-27297

Applications of Tethers in Space: Workshop

proceedings, volume 2

INASA-CP-2422-VOL-2} p 126 N66-27644

Microgravity Polymers

(NASA-CP-23921 p 96 N86-28194

Numerical modeling of physical vapor transport in a

vertical cylindrical ampoule, with and without gravity

[NASA-TP-26201 p 96 N86-29040

REENTRY EFFECTS

Comparison of predicted and experimental real-gas

pressure distributions on space shuttle orbiter nose for

shuttle entry air data system

[NASA-TP-1627} p 14 N80-21280

Aerothermal analysis of a wing-elevon cove with vadable

leakage

{NASA-TP-1703] p 108 N80.32692

Computational Aspects of Heat Transfer in Structures

[NASA-CP-22161 p 109 N82-23473

Correlation of predicted and measured sonic boom

characteristics from the reentry of STS-t od0iter

[NASA-TP-24751 p 190 N85-29694

REENTRY GUIDANCE

Analysis of space shuttle orbiter entry dynamics from

Mach 10 to Mach 2.5 wdh the November 1976 flight control

system

INASA-TP-1667J p 71 N80-29417

Development of the reentry flight dynamics simulator"

for evaluation of space shuttle orbiter entry systems

INASA-TP-1700} p 71 N80-32429

REENTRY PHYSICS

Aerothermal environment in chordwise gaps between

split elevons at Mach 6.8

{NASA-TP-1783] p 109 N81-15237

REENTRY SHIELDING

Preliminary design procedure for insulated structures

subjected to transient heating

[NASA-TP-1534] p 128 N80.12438

Performance of a Haynes 188 metallic standoff thermal

protection system at Mach 7

[NASA-TP-t802} p 72 N81-21116

Oxidation and emittance of superalioys in heat shield

applications

[NASA-TP-2578] p 90 N86-26412

REFERENCE ATMOSPHERES

The 1976 standard atmosphere above 86-km altitude:

Recommendations of task group 2 to COESA

[NASA-SP-398] p 157 N77-10755

REFLECTANCE

Laboratory measurements of radiance and reflectance

spectra of dilute primary-treated sewage sludge

[NASA-TP-1038] p 147 N78.12554

Laboratory measurements of upwalled radiance and

reflectance spectra of Calvert, Ball. Jordan, and Feldspar

soil sediments

[NASA-TP-tO39] p 167 N78-12645

Laboratory measurements of radiance and reflectance

spectra of a dilute biosolid industhat waste product

{NASA-TP-1401 } p 148 N79-t7360

Investigation of effects of background water on upwelled

reflectance spectra and techniques for analysis of dilute

primary-treated sewage sludge

[NASA-TP-t4461 p 168 N79-28864

Spectral reflectances of natural targets for use in remote

sensing studies

[NASA-RP-1139} p 143 N85o30450

REFLECTORS

Prelaunch testing of the GEOS-3 laser reflector array

[NASA-TP-1138] p 117 N78-16354

The 15th Aerospace Mechanisms Symposium

[NASA-CP-2181 I p 130 N81°22388

Vibration studies of a lightweight three.sided membrane

suitable for space application

{NASA-TP-2095] p 131 N83-16785

Large Deployable Reflector Science and Technology

Workshop. Volume 2: Scientific Rationale and Technology

Requirements

[NASA-CP-2275-VOL-21 p 202 N83-27939

Large Deployable Reflector Science and Technology

Workshop. Volume 3: Systems and Technology

Assessment

INASA'CP'2276"VOL'31 p 202 N84-32318

Submillimeter local oscillators for spaceborne

heterodyne applications

{NASA-RP-1147J p 76 N85-30005

REFRACTIVITY

Pockels-effect cell for gas-flow simulation

{NASA-TP-2007i p 115 N82-23515

Rainbow Schlieren

{NASA-TP-2166] p 116 N83-33126

Group-type hydrocarbon standards for

high-performance liquid chromatographic analysis of

middistillate fuels

INASA-TP-23171 p 97 N84-23774

REFRACTORY MATERIALS

X-ray photoelectron spectroscopy study of

rediofrequency-sputtered refractory compound steel

interfaces

{NASA-TP-1161 ] p 91 N78-20336

REFRIGERATORS

Refrigeration for Cryogenic Sensors

{NASA-CP-22871 p 99 N84-15327

A-97
REGENERATION (ENGINEERING) SUBJECT INDEX

REGENERATION (ENGINEERING)

New features and appiicat_ons of PRESTO, a computer

code for the performance of regenerative, superheated

steam turbine cycles

[NASA-TP-1954] p 145 N82-16477

REGRESSION ANALYSIS

Determination of stability and control parameters of a

light airplane from flight data using two estimation methods

--- equation error and maximum likelihood methods

{NASA-TP-1306} p 11 N79-20071

Determination of airplane model structure from flight data

by using modified stepwlse regression

[NASA-TP-1916] p 56 N82-10041

Regression analysis of traction characteristics of traction

fluids

(NASA-TP-2154} p 123 N83-24862

A comparatwe look at sunspot cycles

[NASA-TP-2325} p 209 N84-24520

Ozone Correlative Measurements Workshop

{NASA-CP-2362J p 137 N85-23112

REGULATIONS

Significant NASA inventions available for licensing in

foreign countries

{NASA-SP-7038(08)] p 198 N86-26243

REGULATORS

AESOP: An interactive computer program for the design

of linear quadratic regulators and Kalman filters

[NASA-TP-2221] p 181 N84-16843

REINFORCEMENT (STRUCTURES)

Crash tests of four low-wing twin-engine airplanes with

truss-reinforced fuselage structure

[NASA.TP-2070] p 131 N83-10442

REINFORCEMENT RINGS

Buckling test ot a 3-meter-diameter corrugated

graphite-epoxy ring-stiffened cylinder

ENASA-TP'2032] p 131 N82-28665

REINFORCING FIBERS

Some effects of composition on fhction and wear of

graphite-fiber-reinforced polyimide liners in plain spherical

bearings

INASA-TP-1229I p 119 N78-25433

Thermal-conductivEty measurements of

tungsten-fiber-reinforced superalloy composites using a

thermal-conductivity comparator

INASA-TP-1445) p 80 N79-28234

RELATIVISTIC ELECTRON BEAMS

Three-dimensional relativistic field-electron interaction

in a multicavity high-power klystron Part 2: Working

Equations

i NASA-TP-2008 j p 102 N82-23397

RELATIVISTIC PARTICLES

Three-dimensional relativistic field-electron interaction

m a multicavit_ high-power klystron. 1: Basic theory

[NASA-TP-1992J p 102 N82-22439

RELAXATION (MECHANICS)

Research in structural and solid mechanics, 1982

INASA-CP-2245} p 131 N82-33739

RELEASING

Release mechanism for releasing and reattaching

experiments On the Space Shuttle

INASA-TP-17021 p 121 N80-27694

RELIABILITY

Validation of a fsult-lo_erant ctock synchronization

system

[ NASA-TP-23461 p 180 N84-34198

RELIABILITY ANALYSIS

Validation Methods Research for Fault-Tolerant Avionics

and Control Systems Sub-Working Group Meeting, CARE

3 peer rev=ew

iNASA-CP-2167J p 176 N81-15702

MEGA16 - Computer program for analysis and

extrapolation of stress-rupture data

{NASA-TP-18091 p 130 N81-23486

RELIABILITY ENGINEERING

Systems reliability issues for future aircraft

[NASA-CP-O03] p 175 N77-22808

Proceedings of the 12th Annual Precise Time and Time

Interval (PTTI) Appl=cations and Planning Meeting

{NASA-CP-21751 p 117 N81-27467

Aircraft Engine Diagnostics

[ NASA-CP-21901 p48 N81-31196

Productton of Reliable Flight Crucial Software: Validation

Methods Research for Fault Tolerant Avionics and Control

Systems Sub-Working Group Meeting

[NASA-CP-22221 p 179 N82-24845

Restructursbte Controls

INASA-CP-2277] p 57 N83-33896

REMOTE CONTROL

Release mechanism for releasing and reattaching

experiments on the Space Shuttle

INASA-TP-1702] p 121 N80-27694

REMOTE HANDLING

Theoretical method for calculating relative joint geometry

of assembled robot arms

I NASA-TP-21551 p t82 N83-25438

Theoretical three-and four-axis gimbal robot wrists

INASA-TP-2564} p 181 N86-25168

REMOTE MANIPULATOR SYSTEM

The 16th Aerospace Mechanisms Symposium

INASA-CP-2221 ] p 99 N82-23344

REMOTE SENSING

Determination of wind from NIMBUS 6 satellite sounding

data

[NASA-RP-1072} p 162 N81-15639

A comparative analysis of rswinsonde and NIMBUS 6

and TIROS N satellite profile data

INASA-RP-1070] p 162 N81-15640

Microwave remote sensing of snowpack properties

INASA-CP-2153] p 139 N81-195tl

Digital processing of remotely sensed images

I NASA-SP-431 } p 139 N81-20489

Proton-induced noise in digicons

{NASA-TP-1852] p 76 N61-31281

Field Study for Remote Sensing: An instructor's

manual

INASA-CP-2155J p 136 N81-32564

Chesapeake Bay Ptume Study: Superbux 1980

{NASA-CP-2188} p 168 N82-10661

SAGE measurements of the stratospheric aerosol

dispersion and loading from the Soufriere Volcano

[NASA-TP-1922) p 153 N82-t2687

Laboratory measurements of physical, chemical, and

optical characteristics of Lake Chicot sediment waters

[NASA-TP-1941} p 140 N82-13468

SAM 2 measurements of the polar stratospheric aerosol,

volume 1: October to April 1979

{NASA-RP-10811 p t53 N82-13592

Guidelines for spacebome microwave remote sensors

{NASA-RP-1086] p 140 N82-19647

Twelfth Space Simulation Conference: Shuttle Plus One

A New View of Space

[NASA-CP-2229] p 73 N82-25291

Abstracts of papers presented al the Eleventh

Intematlonal Laser Radar Conference

{NASA-CP-2228} p 115 N82-27706

The LANDSAT tutorial workbook: Basics of satellite

remote sensing

[E83-10001 } p 141 N83-10458

CORSE-81: The 1981 Conference on Remote Sensing

Education

{E83-10179} p 141 N83-17942

Second Eastern Regional Remote Sensing Applications

Conference

{E83-t0199} p 141 N83-19141

Eastern Regional Remote Sensing Applications

Conference

[E83-10201J p 141 N83-21419

The Snowmelt-Runoff Model (SRM) user's manual

[NASA-RP-11001 p 141 N83-23660

Ocean color algorithm for remote sensing of

chlorophyll

[NASA-TP-2164] p 142 N83-26201

Frontiers of Remote Sensing of the Oceans and

Troposphere from Air and Space Platforms

[NASA-CP-2303J p 142 N84-27262

Second Symposium on Space _ndustrialization --- space

commercialization

{NASA-CP-2313 J p63 N85-11011

Global Scale Atmospheric Processes Research Program

Review

{NASA-CP-2344] p 166 N85-14360

Remote Sensing of Snow and Evapotranspiration

{NASA-CP-2363} p 143 N85-23223

Characteristic vector analysis of inflection ratio spectra:

New technique for analysis of ocean color data

INASA-TP-2428] p 143 N85-23237

SAM 2 measurements of the polar stratospheric aerosol,

volume 5

{NASA-RP-1140J p 155 N85-25970

SAM II measurements of the polar stratospheric aerosol

Volume 6: April to October 1981

[NASA-RP-1141] p 155 N85-27422

Spectral reflectances of natural targets for use in remote

sensing studies

[NASA-RP-1139] p 143 N85-30450

Potential spin-offs of the carbon dioxide observational

platform system (CO-OPS) for remote sensing

opportunities

[NASA-TP-2510] p 68 N85-34t49

Review of spectroscopic parameters for upper

atmospheric measurements

[NASA-CP-23961 p 192 N86-13064

VAS demonstration: (VISSR Atmospheric Sounder)

description

[NASA-RP-1151] p 166 N86-13867

Development of UHF radiometer

[NASA-TP-2504] p 103 N86-20678

SAM 2 measurements of the polar stratospheric aerosol,

volume 2

[NASA-RP-1164] p 157 N86-28562

Earth resources: A continuing bibliography with indexes_

issue 50

[NASA-SP-7041(50)J p 143 N86-31940

REMOTE SENSORS

Laboratory measurements of radiance and reflectance

spectra of dilute secondary-treated sewage sludge

[NASA-TP-1089] p 147 N78-12555

Inversion Methods in Atmospheric Remote Sounding

[NASA-CP-004] p 151 N78-12586

Remote sensing of oceanic parameters during the

Skylab/gamefish experiment

[NASA-RP-1012] p 167 N78-12644

Application of Remote Sensing to the Chesapeake Bay

Region Volume 2: Proceedings

I NASA-CP-006-PT-2 } p 138 N78-21526

Active Microwave Users Workshop Report

INASA-CP-2030] p 138 N78-21562

Remote sensing of Gulf Stream using GEOS-3 radar

altimeter

{NASA-TP-1209 } p 167 N78-21737

Application of Remote Sensing to the Chesapeake Bay

Region. Volume 1: Executive summary

{NASA-CP-OOG-PT-1 } p t38 N78-23537

High altitude perspective --- cost-reimbursable services

using NASA U-2 aircraft

{NASA-SP-427] p 138 N78-31508

Quantitatrve mapping by remote sensing of an ocean

acid-waste dump

{NASA-TP-1275} p 147 N78-33617

Preliminary results of SAn soil moisture experiment,

November 1975

{NASA-TP-14041 p 152 N79-16473

Miniature flow-direction and airspeed sensor for

airplanes and radio controlled models in spin studies

INASA-TP-14671 p 38 N79-23081

Investigatton of effects of background water on upwelted

reflectance spectra and techniques for analysis of dilute

primary-treated sewage sludge

[NASA-TP-14461 p 168 N79-28864

Proceedings: Workshop on the Need for Lightning

Observations from Space

{NASA-CP-2095} p 152 N79-30869

Spectral measurements of ocean-dumped wastes tasted

in the marine upwelled spectral signature laboratory

{NASA-TP-1480] p 168 N79-31890

Remote Sensing and Problems of the Hydrosphere

{NASA-CP-2109} p 168 N80-12718

Orbit dynamics and geographical coverage capabilities

of satellite-based solar occultation experiments for global

monitoring of stratospheric constituents

{NASA-TP-t606J p 64 N80-19142

Remote Sensing and Problems of the Hydrosphere A

Focus for Future Research --- conferences

[NASA-CP-2132] p 168 N80-23956

Tropospheric Passive Remote Sensing

[NASA-CP-2237) p 115 N82-26637

Handbook of sensor technical characteristics

[NASA-RP-t087] p 115 N82-29577

LANDSAT-4 Science Characterization Early Results.

Volume 2, part 1: Themattc Mapper (TM)

[E85-10068] p 143 N85-20508

REMOTELY PILOTED VEHICLES

Development of systems and techniques for landing an

aircraft using onboard television

[NASA-TP-t 1711 p32 N78-20114

Realizable optimal control for a remotely piloted research

vehicle --- stability augmentation

{NASA-TP-1654] p 181 N80-25039

Diversity techniques for omnidirectional telemetry

coverage of the HiMAT research vehicle

[NASA-TP-1830] p 39 N81-20074

Parametric study of microwave-powered high-altitude

airplane platforms designed for linear flight

INASA-TP-1918 ] p35 N82-11050

Full-Scale Transport controlled Impact Demonstration

[NASA-CP-2395} p 135 N86-21933

RENE 41

improved adherence of sputtered titanium carbide

coatings on nickel- and titanium-base alloys

[NASA-TP-14501 p 78 N79-22194

REPORT GENERATORS

GEMPAK: An arbitrary aircraft geometry generator

[NASA-TP-1022i p 32 N78-16042

REPORTS

The Apolto-Soyuz Test Proiect: Medical report

[NASA-SP-411] p 170 N77-30738

Proceedings of the First Annual Meteorological and

Environmental Inputs to Aviation Systems Workshop

[NASA-CP-2028} p 158 N78-19711

NASA guidelines on report literature

[NASA-SP-7200] p 197 N79-13914

NASA publications guide

[NASA-SP-7047] p 197 N83-32671

A-98
SUBJECT INDEX RIGID STRUCTURES

RESEARCH

Proceedings of the 2nd Annual Workshop on

Meteorological and Environmental Inputs to Aviation

Systems

INASA-CP-2057} p 159 N79-17413

Computer Science Research at Langley

[NASA-CP-2236} p 176 N82-26996

Bibliography of Supersonic Cruise Research (SCR)

program from 1980 to 1983

[ NASA-RP-1117 ] p 24 N84-27674

Energy efficient transport technology: Program summary

and bibliography

[NASA-RP-ft35} p 37 N85-33116

RESEARCH AIRCRAFT

A flight evaluation of a trailing anemometer for low-speed

calibrations of airspeed systems on research aircraft

[NASA-TP-1135} p 32 N78-18044

Aerodynamic characteristics of a hypersonic research

airplane concept having a 70 deg swept double-delta wing

at Mach number 0.2

{NASA-TP-1252] p 9 N78-31045

YF-12 experiments symposium, volume 1

{NASA-CP-2054-VOL-1 J p 9 N78-32055

Performance evaluation method for dissimilar aircraft

designs --- using the square of the wing span for

nondimensional comparisons of aerodynamic

characteristics

[NASA.RP-t042] p 2 N79-30139

Small transport aircraft technology

[NASA-SP-460] p 36 N83-20931

RESEARCH AND DEVELOPMENT

Aircraft Safety and Operating Problems -- conference

[NASA-SP-416J p 28 N77-18081

Design of a blood-freezing system for leukemia

research

NASA-TP-1165] p 189 N78-18873

Fundamental heat transfer research for gas turbine

engines

NASA-CP-2178 J p 48 N81-24063

Joint University Program for Air Transportation

Research, 1982

NASA-CP-2285] p 4 N84-11099

The management of research institutions: A look at

iovernment laboratories

NASA-SP-481 ] p 196 N85-16665

RESEARCH FACILITIES

High Reynolds Number Research

NASA-CP-20091 p 59 N77-27139

Proceedings of workshops to define engineering

requiremenls for a space vacuum research facility

NASA-CP-2091 I p 62 N79-26076

A unique facility for V/STOL aircraft hover testing ---

Langley Impact Dynamics Research Facility

NASA-TP-1473] p 59 N79-29199

The management of research institutions: A look at

government laboratories

{NASA-SP-481 j p 196 N85-16665

Searching the horizon: A history of Ames Research

Center, 1940-1976

{NASA-SP-4304] p 213 N86-16185

RESEARCH MANAGEMENT

A NASA high-power space-based laser research and

applications program

[NASA-SP-464] p 118 N83-27200

Proceedings of a Workshop on Research Needs in

Heterogeneous Tropospheric Chemistry

iNASA-CP-2320] p 137 N84-28131

RESEARCH PROJECTS

Viking 1: early results --- Mars atmosphere and surface

examinations

[NASA-SP-4081 p 70 N76-28296

RESERVOIRS

Laboratory upwelled radiance and reflectance spectra

of Kerr reservoir sediment waters

[NASA-TP-1993} p 150 N82-21774

RESIDUAL STRENGTH

Strength of graphite/epoxy bolted wing-skin splice

specimens subjected to outdoor exposure under constant

load and yeady fatigue loading

INASA-TP-2542} p 83 N86-20508

RESIDUAL STRESS

Effect of shot peening on surface fatigue life of

carburized and hardened AISI 9310 spur gears

[NASA-TP-2047t p 122 N82-32736

RESILIENCE

Tire stiffness and damping determined from static and

free-vibration tests --- aircraft tires

{NASA-TP-1671 ] p 29 N80-27302

RESIN MATRIX COMPOSITES

Tough Composite Materials

{NASA-CP-23341 p 83 N85-12941

NASA/aircraft industry standard specification for

graphite fiber toughened thermoset resin composite

material

{ NASA-RP-11421 p 83 N85-26923

RESISTANCE

Flow through very porous screens

{NASA-TP-24361 p t12 N85-20270

RESOLUTION

Deconvolution and analysis of wide-angle Iongwave

radiation data from Nimbus 6 Earth radiation budget

experiment for the first year

[NASA-TP-1746} p 162 N81-13593

RESONANT FREQUENCIES

A theory for predicting boundary impedance and

resonance frequencies of slotted-wall wind tunnels,

including plenum effects

[NASA-TP-1880] p 17 N81-29096

Analysis of rectangular microstrip antennas

[NASA-TP-2276] p fO0 N84-20735

RESONATORS

Proceedings of the 14th Annual Precise Time and Time

Interval (PTTt) Applications Planning Meeting

[NASA-CP-2265] p 118 N83-35351

RESOURCES MANAGEMENT

Summer Workshop on Near-Earth Resources

[NASA-CP-2031 ] p 205 N78-18973

Operational Applications of Satellite Snowcover

Observations

[E80-10167] p 139 N80-25742

Western Regional Remote Sensing Conference

Proceedings. 1979

[NASA-CP-2148] p 139 N81-21440

Guidelines for line-oriented flight training, volume 1

{NASA-CP-21841 p 30 N81-30101

Applications systems verification and transfer project.

Volume 1: Operational applications of satellite snow cover

observations: Executive summary --- usefulness of satellite

snow-cover data for water yield prediction

[NASA-TP-1822] p 140 N82-20617

Applications systems verification and transfer project,

Volume 2: Operational applications of satellite snow-cover

observations and data-collection systems in the Arizona

test site

INASA-TP-1823} p 140 N82-20618

Applications systems verification and transfer project.

Volume 6: Operational applications of satellite snow-cover

observations NOAA/NESS support study

[NASA-TP-1827} p 140 N82-20622

Second Eastern Regional Remote Sensing Applications

Conference

[E83-t0189} p 141 N83-1914t

Eastern Regional Remote Sensing Applications

Conference

{E83-10201 ] p 141 N83-21419

Proceedings of the National Conference on Energy

Resource Management. Volume 1: Techniques,

Procedures and Data Bases

[E83-103351 p 141 N83-26155

Proceedings of the National Conference on Energy

Resource Management. Volume 2: Applications

{E83-10336} p 142 N83-26176

RETARDING

A method for determining acoustic-liner admittance in

ducts with sheared flow in two-cross-sectional directions

[NASA-TP-2518] p 190 N86-13056

RETRACTABLE EQUIPMENT

Large Space Systems Technology, 1979 --- antenna and

space platform systems conference

[NASA-CP-2118] p 66 N80-19145

REUSABLE HEAT SHIELDING

Expenmental aerodynamic heating to simulated space

shuttle tiles in laminar and turbulent boundary layers with

vadabie flow angles at a nominal Mach number of 7

{NASA-TP-2307} p 113 N85-34351

REUSABLE ROCKET ENGINES

Structural Integrity and Durability of Reusable Space

Propulsion Systems

[NASA-CP-2381} p 78 N85-27941

REUSABLE SPACECRAFT

The 1 lth Space Simulation Conference

[NASA-CP-21501 p 99 N81-14138

REVERBERATION

Analytical study of acoustic response of a

samireverberant enclosure with application to active noise

control

[NASA-TP-2472} p 191 N86-16040

REVERSED FLOW

Reverse-flow combustor for small gas turbines with

pressure-atomizing fuel injectors

[NASA-TP-1260] p 43 N78-27130

REVISIONS

Recent modifications and calibration of the Langley

iow-turbuionce pressure tunnel

[NASA-TP-2328] p 24 N84-27675

REYNOLDS NUMBER

High Reynolds Number Research

[NASA-CP-2009J p 59 N77-27139

Effect of slotted casing treatment with change in

Reynolds number index on performance of a jet engine

I NASA-TP-10581 p41 N77-32154

Application of shock tubes to transonic aidoil testing

at high Reynolds numbers

INASA-TP-1268i p 10 N79-12013

A hybridized method for computing

high-Reynolds-number hypersonic flow about blunt

bodies

INASA-TP-14971 p 107 N79-33441

Effect of Reynolds number on stability characteristics

of a cruciform wing-body

[NASA-TP-16831 p 15 N80-27283

Aerodynamic characteristics of three helicopter rotor

airfoil sections at Reynolds number from model scale to

full scale at Mach numbers from 0.35 to 090 --- conducted

in Langley 6 by 28 inch transonic tunnel

{NASA-TP-1701} p 15 N80-32333

A fan pressure ratio correlation in terms of Mach number

and Reynolds number for the Langley 0.3 meter transonic

cryogenic tunnel

{NASA-TP-1752} p 16 N81-10005

Wind-tunnel measurements and companson with flight

of the boundary layer and heat transfer on a hollow cylinder

at Mach 3

IrNASA-TP-1789J p 16 N81-14975

High Reynolds number research - 1980

JNASA-CP-2183] p 18 N81-31130

Gortler vortices and transition in wall boundary layers

of two Mach 5 nozzles

[NASA-TP-1869} p 109 N81-31509

Force and moment, flow-visualization, and

boundary-layer tests on a shuttle orbiter model at Math

6

(NASA-TP-1952] p 18 N82-13t06

Supersonic jet noise generated by large scale

instabilities

{NASA-TP-2072} p 188 N82-34189

Studies of sidewall boundary layer in the Langley 0.3

meter transonic cryogenic tunnel with and without

suction

{NASA-TP-2096} p 110 N83-20031

Low-speed tests of a high-aspect-ratio,

supercdtical-wing transport model equipped with a high-lift

flap system in the Langley 4- by 7-rneter end Ames 12-foot

pressure tunnels

{NASA-TP-20971 p 26 N85-31010

Mach 6 flow field surveys beneath the forebody of an

airbreathing missile

I NASA-TP-2491] p 28 N86-23558

REYNOLDS STRESS

Mean-flow and turbulence measurements in the vicinity

of the trailing edge of an NACA (63 sub 1)-012 airfoil

[NASA-TP-1845} p 109 N8t-23410

RHEOLOGY

Traction dnve performance prodiotion for the Johnson

and Tevaa;'werk traction model

{NASA-TP-1530] p 121 N79-33475

Tribology in the 80's. Volume 1: Sessions 1 to 4

[NASA-CP-2300-VOL-1] p 124 N84-23891

RICHARDSON NUMBER

Three-dimensional beroclinic instability of a Hadley cell

for small Richardson number

[NASA-TP-245OJ p 166 N85-20605

RIDING QUALITY

Proceedings and findings of the 1976 Workshop on Ride

Quality --- passenger acceptance of transportation

systems

[NASA-CP-2006J p 172 N77-27710

An investigation of r_e quality rating scales

[NASA-TP-1064} p 171 N78-11696

Analytical study of ride smoothing benefits of control

system configurations optimized for I_tot handling

qualities

{NASA-TP-1148} p53 N78-18076

Human discomfort response to noise combined with

vertical vibratton

{NASA-TP-1374] p 171 N79-22761

Implications of fuel,efficient vehicles on ride quality and

passenger acceptance: Workshop proceedings

[NASA-CP-2096] p 199 N80-18990

Evaluation of ride quality prediction methods for

helicopter interior noise and vibration environments

I NASA-TP-2261 } p 172 N84-20155

A user-oriented and computerized model for estimating

vehicle ride quality

[NASA-TP-2299} p 172 N84-22162

RIGID ROTORS

Effects of primary rotor parameters on flapping

dynamics

I NASA-TP-1431 I p 55 N80-15138

RIGID STRUCTURES

Stress analysis and buckling of J-stiffened

graphite-epoxy panel

{NASA-TP-16071 p 129 N80-f8427

Compression panel studies for supersonic cruise

vehicles

I NASA-TP-16171 p 82 N83-28099

A-99
RISK SUBJECT INDEX

Fabrication and evaluation of brazed titanium-clad

Borssc/eluminum compression panels

{NASA_TP-1573] p 82 N83-28100

Joint design for improved fatigue life of diffusion-bonded

box-stiffened panels

[NASA-TP-2480] p 135 N85-33537

Decoupled end linear quadratic regulator control of a

large, flexible space antenna with an observer in the control

loop

[NASA-TP-2484J p 75 N86-16250

RISK

Carbon Fiber Risk Analysis --- conference

{ NASA-CP-2074] p 80 N79-22196

Risk to the public from carbon fibers released in civil

aircraft accidents

{ NASA-SP-448 ] p81 N81-18096

Procedure for estimating orbital debris risks

{ NASA-TP-2507 ] p69 N85-33169

RIVER BASINS

Operational Applications of Satellite Snowcover

Observations

[E80-10167] p 139 N80-25742

RIVERS

Quantitative analysis of aircraft multisbectral-scanner

data and maplmng of water-quality parameters in the James

River in Virginia

[NASA-TP-1021] p 147 N78-13628

ROBOTICS

Kinematic control of robot with degenerate wnst

INASA-TP-2341 } p 181 N84-28539

Modified Denavit-Hartenberg parameters for better

location of joint axis systems in robot arms

INASA-TP-25851 p 183 N86-27953

ROBOTS

Marking parts to aid robot vision

[NASA-TP-1819] p 176 N81-21775

Advanced Automation for Space Missions

[NASA-CP-2255J p 76 N83-t5348

Theoretical method for calculating relative joint geometry

of assembled robot arms

[NASA-TP-2155] p 182 N83-25438

Vector-algebra approach to extract Denavit-Hartenberg

parameters of assembled robot arms

[NASA-TP-2191 J p 182 N83-34661

Translational control of a graphically simulated robot arm

by kinematic rate equations that overcome elbow joint

singularity

|NASA-TP-23761 p 181 N85-15446

Kinematic rate control of simulated robot hand at or

near wrist singularity

[NASA-TP-2440J p 181 N85-27575

Theoretical three-and four-axis gimbal robot wrists

[NASA-TP-25641 p 181 N86-25168

ROCKET ENGINE CASES

Development o1 in situ stiffness properties for shuttle

booster filament wound case

[NASA-TP-2377] p 83 N84-33521

ROCKET ENGINE DESIGN

Essays on the History of Rocketry and Astronautics:

Proceedings of the Third through the Sixth History

Symposia of the international Academy of Astronautics,

volume 2

[NASA-CP-2014-VOL-21 p 212 N77-33048

ROCKET ENGINES

Applied Routh approximation

INASA-TP-1231 ) p 98 N78-22257

Description of an experimental (hydrogen peroxide)

rocket system and its use in measunng aderon and rudder

effectiveness of a light airplane

[NASA-TP-1647} p 55 N80-22358

ROCKET EXHAUST

Research in the use of etectrets in measuring effluents

from rocket exhaust of the space shuttle (64 percent

scaled model) and Viking I launch

INASA-TP-1073J p 147 N78-11517

Some physical and thermodynamic properties of rocket

exhaust clouds measured with infrared scanners

[NASA-TP-1041 ] p 147 N78-11520

Effects of entrained water and strong turbulence on

afferburning within solid rocket motor plumes

_NASA-TP-1111 ] p 147 N78-15596

Proceedings of Shuttle Environmental Effects Program

Review -- conferences

{NASA-CP-2110J p 149 N80-15649

Analytic model for washout of HCI(g) from dispersing

rocket exhaust clouds

[NASA-TP-1801 ] p 149 N81-24601

Application of a Gaussian multilayer diffusion model to

characterize dispersion of vert;cal HCI column density in

rocket exhaust clouds

INASA-TP-1956] p 149 N82-14672

Charactebzat=on of soil and postlaunch pad debris from

Cape Canaveral launch complex and analysis of soil

interaction with aqueous HCf

{NASA-TP-20761 p 150 N83-12595

Airborne measurements of launch vehicle effluent:

Launch of Space Shuttle (STS-1) on 12 April 1981

JNASA-TP-2090I p 150 N83-16952

Space shuttle exhaust c=oud properties

[NASA-TP-2258J p 154 N84-14606

ROCKET FLIGHT

Essays on the History of Rocketry and Astronautics:

Proceedings of the Third through the Sixth History

Symposia of the International Academy of Astronautics,

volume 1

INASA-CP-2014-VOL-1 I p 211 N77-33030

ROCKET LININGS

Effect of low-stiffness closeout overwrap on rocket

thrust-chamber life

[ NASA-TP-f 456 j p77 N79-23132

ROCKET NOSE CONES

Measured and predicted shock shapes and aerodynamic

coefficients for blunted cones at incidence in helium at

Mach 20.3

INASA-TP-13951 p 106 N79-20345

ROCKET NOZZLES

Star 48 solid rocker motor nozzle analyses and

instrumented firings

[NASA-TP-2572} p 68 N86-20460

ROCKET OXIDIZERS

Proceedings of the NASA/Florida Institute of

Technology Environmental Engineering Conference on

Nitrogen Tetroxide --- with emphasis on space shuttle

/NASA-CP-2049] p 136 N79-20424

ROCKET PROPELLANTS

Essays on the History of Rocketry and Astronautics:

Proceedings of the Third through the Sixth History

Symposia of the International Academy of Astronautics,

volume 2

[NASA-CP-2014-VOL-21 p 212 N77-33048

ROCKET SOUNDING

Wind study for high altitude platform design

[NASA-RP-10441 p 160 N80-12661

Results of the August 1977 Soviet and American

meterological rocketsonde infercomparison held at

Wallops Island, Virginia

tNASA-RP-1053] p 161 N80-16682

Goddard Laboratory for Atmospheric Science, collected

reprints 1978-1979. volume 1

[NASA-TP-1788-VOL-1] p 163 N81-21686

ROCKET THRUST

Parametric study of ascent performance of a vertically

launched hydrogen-fueled single-stage reusable

transport

[NASA-TP-1045] p 65 N78-10186

ROCKS

Results of analyses performed on basalt adjacent to

penetrators emplaced into volcanic rock at Amboy,

California, April 1976

JNASA-TP- 10261 p 199 N77-33003

Discrimination of rock classes and alteration products

in southwestern Saudi Arab*a with computer-enhanced

LANDSAT data

I NASA-TP-13271 p 136 N78-33499

ROLL

Experiments in sensing transient rotational acceleration

cues on a flight simulator

{NASA-TP-15371 p 33 Na0-10193

Light airplane crash tests at three roll angles

{NASA-TP-14771 p 128 N80-10512

Kinematic properties of the helicopter in coordinated

turns

I NASA-TP-17731 p 35 N81-22039

Planar equations of rolloul motion for an aircraft with

free or steerable landing gears

INASA-TP-19841 p 35 N82-23244

ROLLER BEARINGS

Effect of filtration on rolling-element-bearing life in

contaminated lubricant environment

fNASA'TP'1272 ] p 119 N78-28457

Operating charactehstics of a large-bore roller bearing

to speeds of 3 times 10 to the 6th power DN

tNASA-TP-t4131 p 120 N79-18323

Comparison of predicted and experimental performance

ot large-bore roller bearing operating to 3,0 million DN

[NASA-TP-1599J p 121 N80-15410

Lubrication of optimized-design tapered-roller bearings

to 24 million DN

[ NASA-TP-1714 ] p 121 N80-29734

Effect of cage design on characteristics of

high-speed-jet-lubricated 35-mdlimeter bore ball bearing ---

turboiet engines

[NASA-TP-17321 p 121 N80-33749

Life analysis of multirolter planetary traction drive

[NASA-TP-17101 p 122 N81-20423

Advanced Power Transmission Technology

INASA-CP-22101 p 123 N83-20119

Rolling-element bearings

INASA-RP-1105] p 123 N83-27214

Effect of carbide distribution on rolling-element fatigue

life of AMS 5749

I NASA-TP-21891 p 123 N83-33166

Operating characteristics of a three-piece-inner-ring

large-bore roller bearing to speeds ol 3 million DN

[NASA-TP-2355 J p 124 N84-29226

Thermal analysis of a planetary transmission with

spherical roller bearings operating after complete loss of

oil

INASA-TP-2367} p 124 N84-32824

Effect of two inner-ring oil-flow distribution schemes on

the operating characteristics of a 35 millimeter bore ball

bearing to 2.5 million DN

[NASA-TP-2404] p 124 N85-13233

Effect of speed and press fit on fatigue life of

roller-beanng inner-race contact

INASA-TP-2496] p 125 N85-31511

ROLLING CONTACT LOADS

Operating characteristics of a large-bore roller bearing

to speeds of 3 times 10 to the 6th power DN

INASA-TP-f413J p 120 N79-18323

Spur-gear-system efficiency at part and full load

{NASA-TP-t622] p 121 N80-t7466

Rolling-element fatigue life with traction fluids and

automatic transmission fluid in a high-speed rolling-contact

rig

[NASA-TP-2050I p 122 N83-13457

Measurement of rolling friction by a damped oscillator

{NASA-TP-22571 p 123 N84-13577

Effect of speed and press fit on fatigue life of

roller-beanng inner-race contact

INASA-TP-24961 p 125 N85-31511

Surface fatigue life and failure characteristics of EX-53,

CBS 1000M, and AISt 9310 gear materials

[NASA-TP-2513] p 125 N86-12609

ROLLING MOMENTS

Wake Vortex Minimization

[NASA-SP-4091 p 6 N78-12017

Static and yawed-rolling mechanical properties of two

type 7 aircraft tires

INASA-TP-1863] p 130 N81-24471

ROOTS OF EQUATIONS

Convergence of Newlon's method for a single real

equation

J NASA-TP-2489J p 183 N85-28656

ROTARY STABILITY

Rotordynamic Instability Problems in high-performance

turbomachinery

JNASA-CP-21331 p 121 N80-29706

Effects of different rub models on simulated rotor

dynamics

[NASA-TP-2220] p 123 N84-17590

Instability in Rotating Machinery

{ NASA-CP-2409] p 126 N86-30160

ROTARY WING AIRCRAFT

Rotorcraft Dynamics 1984

{NASA-CP-2400] p 38 N86-15280

ROTARY WINGS

Wind-tunnel tests of wide-chord teetering rotors with and

without outboard flapping hinges

INASA-TP-10461 p 31 N78-11053

A rotor-mounted digital instrumentation system for

helicopter blade flight research measurements

[NASA-TP-11461 p 38 N78-20128

An analysis of the gust-induced overspeed trends of

helicopter rotors

[NASA-TP-12131 p 8 N78-28056

Experimental investigation ol effects of blade tip

geometry on loads and performance for an articulated rotor

system

[NASA-TP-1303] p 33 N79-15938

Experimental investigation of three helicopter rotor

airfoils designed analytically --- m the Langley 6 by 19

inch and 6 by 28 inch transonic wind tunnels

{NASA-TP-f396J p 11 N79-22037

Effects of pnmary rotor parameters on flapping

dynamics

[NASA-TP-14311 p 55 N80-15138

On the nonlinear deformation geometry of

Euter-Bernoulli beams --- rotary wings

[NASA-TP-1566J p 129 N80-20619

Wind-tunnel investigation of the effects of blade tip

geometry on the interaction of torsional loads and

performance for an articulated helicopter rotor

{NASA-TP-19261 p 18 N82-13107

Effects of repetition rate and impulsiveness ol simulated

helicopter rotor noise on annoyance

tNASA-TP-1969] p 150 N82-19707

The vibration characteristics of a coupled helicopter

rotor-fuselage by a finite element analysis

I NASA-TP-2118 ] p36 N83-18714

Experimental _nvestigat=on of a 10-percent-thick

helicopter rotor airfoil sechon designed with a viscous

transonic analysis code

[NASA-TP-1864 I p 2t N83-30389

A-100
SUBJECT INDEX SAGE SATELLITE

Two-dimensional aerodynamic characteristics of an

airfoil designed for two

(NASA-TP-1965] p 24 N84.27694

Transonic flow analysis for rotors. Part 1:

Three-dimensional quasi-steady, full-potential calculation

[NASA-TP-2375-PT-t ] p 25 N85-10914

ROTATING BODIES

On the nonlinear deformation geometry of

Euler-Bernoulli beams --- rotary wings

[NASA-TP-1566] p 129 N80-20619

The compressible aerodynamics of rotating blades

based on an acoustic formulation

[NASA-TP-2197] p 189 N84-13923

Nonlinear equations for dynamics of pretwistad beams

undergoing small strains and large rotabons

[NASA-TP-2470] p 134 N85-27258

ROTATING CYLINDERS

Liquid management in low gravity using baffled rotating

containers

[NASA-TP-2263] p 111 N84-15427

ROTATING FLUIDS

Mechanics of liquid helium in a partially filled rotating

dewar in low gravity with application to Gravity Probe-B

[NASA-TP-2124] p 110 N83-16680

ROTATING SHAFTS

Stability of numerical integrat,,on techniques for transient

rotor dynamics

[NASA-TP-1092J p 119 N78-10474

Direct integration of transient rotor dynamics

[NASA-TP-1597] p 46 N80-15128

Oes=gn of power-transmitling shifts

[NASA-RP-1123] p 124 N84-27041

ROTATION

An experimental and analytical investigation of proprotor

whirl flutter

[NASA-TP-1047] p 6 N78-12039

Decoupled control analysis of a large flexible space

antenna with linear quadratic regulator comparisons

|NASA-TP-22931 p 74 N84-23675

Mixed models and recugion techniques for

large-rotation, nonlinear analysis of shells of revolution with

application to tires

[NASA-TP-23431 p 133 N84-34773

ROTOR AERODYNAMICS

Wind-tunnel tests of wide-chord teetering rotors with and

without outboard flapping hinges

[ NASA-TP-10461 p31 N78-11053

Effect of casing treatment on performance of a two-stage

high-pressure-ratio fan

[NASA-TP-1409] p 44 N79-16852

Experimental investigation of three helicopter rotor

airfoils designed analytically --- in the Langley 6 by 19

inch and 6 by 28 inch transonic wind tunnels

[NASA-TP-1396 ] p 11 N79-22037

Effect of rotor meridional velocity ratio on response to

inlet radial end circumferential distortion

[NASA-TP-1278] p 45 N79-28177

Performance of two-stage fan with a first-stage rotor

redesigned to account for the presence of a part-span

damper

[NASA-TP-1483] p 45 N79-30191

Effects of primary rotor parameters on flapping

dynamics

[NASA-TP-1431] p 55 N80-15138

Aerodynamic performances of three fan stator designs

operating with rotor having tip speed of 337 meters per

second end pressure ratio of 154. 1: Experimental

performance

[NASA-TP-1610] p 46 N90-17071

Aerodynamic performances of three fan stator designs

operating with rotor having tip speed of 337 meters per

second and pressure ratio of 1.54. Relation of analytical

code calculations to experimental performance

[NASA-TP-1614J p 46 N80-21324

Performance of single-stage axial-flow transonic

compressor with rotor and stator aspect ratios of 1.19

and 1.26 respectively, and with design pressure ratio of

2.05

[NASA-TP-1659] p 46 N80-21325

Forward acoustic performance of a shock-swallowing

high-tip-speed fan (QF-13)

[NASA-TP-1668] p 187 N80-23100

Development and validation of a combined rotor

fuselage induced flow field computational method ---

Langley V/STOL tunnel

[NASA-TP-1656] p 15 N80-25296

Calculation of three-dimensional unsteady transonic

flows past helicopter blades

[NASA-TP-1721] p 15 N80-33356

Wind-tunnel investigation of the effects of blade tip

geometry on the interaction of torsional loads and

performance for an articulated helicopter rotor

[NASA-TP-1926] p 18 N82-t3107

Wind turbine dynamics

[NASA-CP-2185] p 146 N82-23684

Establishment of a rotor model basis

[NASA-TP-2026] p 36 N82-29311

Incidence loss for fan turbine rotor blade in

two-dimensional cascade

{NASA-TP.2198] p 50 N83-30431

The compressible aerodynamics of rotating blades

based on an acoustic formulabon

[NASA-TP-2197] p 189 N84-13923

Effects of different rub models on simulated rotor

dynamics

{NASA-TP-2220} p 123 N84-17590

Study of stator-vane fluctuating pressures in a turbofan

engine for static and flight tests

[NASA-TP-2217] p 189 N84-22363

Rotordynemic instability Problems in High-Performance

Turbomachinery

INASA-CP-23381 p 124 N85-14116

Passive eddy-current damping as a means of vibration

control in cryogenic turbomachinery

[NASA-TP-2562} p 68 N86-24722

ROTOR BLADES

Rotor tip clearance effects on overall and blade-element

performance of axial-flow transonic fan stage

{NASA-TP-2049] p 49 N82-33389

ROTOR BLADES ("FURBOMACHINERY)

In-place recalibration technique applied to a

capacitance-type system for measuring rotor blade tip

clearance

[NASA-TP-1110] p 42 N78-22101

Performance with and without inlet radial distortion of

e transonic fan stage designed for reduced loading in the

tip region

I NASA-TP-t2941 p 9 N78-30057

Effect of casing treatment on performance of a two-stage

high-pressure-ratio fan

{NASA-TP-14091 p 44 N79-16852

Performance of two-stage fan having low-aspect-ratio

first-stage rotor biading

|NASA-TP-1493] p 45 N79-27143

Performance of two.stage fan with a first-stage rotor

redesigned to account for the presence of a part-span

damper

I NASA-TP-1483 ] p45 N79-30191

Aerodynamic performance of 1.38-pressure-ratio.

variable.pitch fan stage

JNASA-TP-15021 p 45 N79-31213

Off-design correlation for losses due to part-span

dampers on transonic rotors

I NASA-TP-1693] p 47 N80-28352

Performance of single-stage axial-flow transonic

compressor with rotor and stetor aspect ratios of 1.63

and 1.77, respectively, and with design pressure ratio of

2.05

[NASA-TP-2001] p 49 N82-22269

Establishment of a rotor model basis

[NASA-TP-2026] p 36 N82-29311

Large Horizontal-Axis Wind Turbines

[NASA.CP-2230] p 146 N83-19231

Computer code for off-design performance analysis of

radial-inflow turbines with rotor blade sweep

[NASA-TP-2199] p 50 N83-32807

Effects of different rub models on simulated rotor

dynamics

[NASA-TP-2220] p 123 N84-17590

Two-dimensional aerodynamic characteristics of three

rotorcraft airfoils et Mach numbers from 0.35 to 0.90

[NASA-TP-2000] p 24 N84-28743

ROTOR SPEED

Damping seals for turbomacbinery

[NASA-TP-1987] p 49 N82-20183

ROTOR SYSTEMS RESEARCH AIRCRAFT

Processing of on-board recorded data for quick analysis

of aircraft performance --- rotor systems research

aircraft

{NASA-RP-f043J p 33 N79-3319t

Results of the first complete static calibration of the

RSRA rotor-load-measurement system

[NASA-TP-2327] p 37 N84-31111

ROTORCRAFT AIRCRAFT

Application of special.purpose digital computers to

rotorcraft real-time simulation

[NASA-TP-1267] p 32 N78-27113

A formulation of rotor-airframe coupling for design

analysis of vibrations of helicopter airframes

[NASA-RP-t089] p 133 N84-33832

ROTORS

An Assessment of Technology for Turbojet Engine Rotor

Failures

[NASA-CP-2017] p 41 N79-10068

Stability of numerical integration techniques for trens_nt

rotor dynamics

[NASA.TP.1092] p 119 N79-10474

Influence of oil-squeeze-film damping on steady-state

response of flexible rotor operating to supercritical

speeds

[NASA-TP-1094] p 41 N78-13064

Direct integration of transient rotor dynamics

[NASA-TP-1597] p 46 N80-15128

GRID30: Computer program for fast generation of

multilevel, three-dimensional boundary-conforming O-type

computational grids

[NASA-TP-1920] p 18 N81-31128

Performance of a tandem-rotor/tandem-stator

conical-flow compressor designed for a pressure ratio of

3

[NASA-TP-2034] p 20 N83-11058

Rotordynamic Instability Problems in High-Performance

Turbomachinery

[NASA.CP-2250| p 122 N83-15629

Aerodynamic effect of a honeycomb rotor tip shroud

on a 50.8-centimeter-tip-diameter core turbine

[NASA-TP-2112] p 49 N83-t7547

ROUGHNESS

Effects of roughness size on the position of

boundary-layer transition and on the aerodynamic

characteristics of a 55 deg. swept delta wing at supersonic

speeds

[NASA-TP-1027] p 7 N78-13016

RUBBER

Friction characteristics of three 30 by 11.5-14.5, type

8, aircraft tires with various tread groove patterns and

rubber compounds

[NASA-TP-1080} p 32 N78-13043

Nitrogen dioxide vapor penetration of chlorobutyl rubber

SCAPE under operational conditions

[NASA-TP-1805] p 85 N80-t6118

RUDDERS

Description of an experimental (hydrogen peroxide)

rocket system and its use in measuring aileron and rudder

effectiveness of e light airplane

[NASA-TP-1647] p 55 N80-22358

Effect of thrust reverser operation on the

laterat<lirectional characteristics of a three-surface F-15

model at transonic speeds

|NASA-TP-2234J p 22 N84-13165

RUNWAY CONDITIONS

Behawor of aircraft ant|skid braking systems on dry and

wet runway surfaces: Hydromechanically controlled

system

[NASA-TP-1877J p 35 N81-30112

RUNWAYS

Effects of landing approach methods and separation

intervals on single runway landing capacity

[NASA-TP-1112] p29 N78-t 3029

Behavior of aircraft antiskid braking systems on dry and

wet runway surfaces. A slip-veiocity-conVolted,

pressure-bias-modulated system

[NASA-TP-1051] p 33 N80-12084

Evaluation of g seat augmentation of fixeq*bese/moving

base simulation for transport landings under two visually

imposed runway width conditions

[NASA-TP-2135) p 36 N83-22191

Abrasion behavior" of aluminum and composite skin

coupons, stiffened skins and stiffened panels

representative of transport airplane structures

[NASA-TP-2520] p 38 N88-13316

S

SAFETY

Lithium/sulfur dioxide cell and battery safety

[NASA-RP-1099] p 146 N83-14684

The 1982 Goddard Space Flight Center Battery

Workshop

[NASA-CP-2263] p 102 N83-35230

Controls, Displays, and Information Transfer for General

Aviation IFR Operations

|NASA-CP-2279} p 4 N84-12029

SAFETY FACTORS

The 1980 Goddard Space Flight Center Battery

Workshop

[NASA.CP.2177] p 145 N81-21493

Proceedings: Sixth Annual Workshop on Meteorological

end Environmental Inputs to Aviation Systems

[NASA-CP-2274] p 4 N83-33827

SAGE SATELLITE

SAGE measurements of the stratospheric aerosol

dispersion and loading from the Soufriere Volcano

[NASA-TP.t922] p 153 N82-12687

SAM 2 measurements of the polar stratospheric aerosol

volume 1: October to April 1979

[NASA-RP-1081] p 153 N82-13592

SAGE aerosol measurements. Volume 1: February 21,

1979 to December 31, 1979

[NASA-RP-1144] p 155 N88-11700

SAGE Aerosol Measurements Volume 2:1 January31 December 1980

[NASA-RP-t149] p 156 N86-23088

A-101
SALINITY SUBJECT INDEX

IL&UNIT3t

Sea-surface temperature and salinity moPl_ng from

remote microwave radtometdc measurements of

I_ghtheM temperature

[NASA-TP-1077] p 168 N7g-28863

Radiometer requirements for Earth-observation systems

using large space antenr_s

[NASA-RP-1101] p 116 N83-28410

North Atlantic Deep Water Formation

[NASA-CP-2367] p 169 N85.26028

Development of UHF radiometer

[NASA-TP-2504] p 103 N86-20678

SAMPLES

Lunar sample studies -.. bceccies pasalts, end

anorthoottes

[NASA-SP-418] p 204 N77-27053

8AMPUNG

Description and field test of an in situ coliform monitoring

system

[NASA.TP-1334] p 146 N7g-14591

Airborne measurements of launch vehicle effluent of

STS.2 launch on November t 2, 198 t at Cape Canaveral,

Rodda

[NASA-TP-2200] p 150 N84-18764

Airborne lidar measurements of El Chichon stratoshperic

aerosols

[NASA-RP-1166] p 156 N86-27835

LS, N FRANCISCO BAY (CA)

Planning for airport access: An analysis of the San

Francisco Bay area

[NASA-CP-2044] p 198 N79-10942

SANDWICH STRUCTURES

Buckling and structural efficiency of sandwich-blade

stiffened composite compression panels

{NASA-TP-1269] p 127 N78-32492

Elastic constants for superplastically

formed/diffusion-bonded corrugated sandwich core

[NASA-TP-1562] p 129 N80-23677

Tests of graphite/polyimide sandwich panels in uniaxial

edgewise compression

[NASA-TP-1785] p 81 N81-16129

SATELLITE ANTENNAS

Large Space Antenna Systems Technology, 1964

[NASA.CP.2368-PT-1] p 67 N85-23813

SATELLITE AI"rlTUDE CONTROL

Flight Mechanics/Estimation Theory Symposium

[NASA-CP-2050] p 64 N79-14121

Two-impulse reonentation of asymmetric spacecraft

[NASA-TP-1554] p 64 N80-13135

Flight Technology Improvement --- spaceborne optical

radiometric instruments, attitude control, and

electromechanical and power subsystems

INASA-CP-2101] p 75 N60-13152

ATS-6 engineering performance report. Volume 2: Orbit

and attitude controls

INASA-RP-t080-VOL-2] p 73 N62-16146

SATELLITE CONFIGURATIONS

Aerothermet analysis of a wing-elevon cove with variable

leakage

[NASA-TP-t703J p 108 N80-32692

ATSo6 engineering performance report.

Volume:Program and systems summaries: Mechanical and

thermal details

[NASA-RP-1080-VOL-1 } p 73 N62-16147

The microwave radiometer spacecraft: A design study

[NASA-RP-t079] p 73 N82-t6153

SATELLITE CONTROL

ATS-6 engineering performance report, Volume 3:

Telecommunications and power

[NASA-RP-1080-VOL-3} p 73 N82-16149

SATELLITE DESIGN

ATS-6 engineering performance report.

Volume:Program and systems summaries: Mechanical and

thermal details

[NASA-RP-t080-VOL-t J p 73 N82-16147

Large Deployable Reflector Science and Technology

Workshop Volume 3: Systems and Technology

Assessment

[ NASA-CP-2275-VOL-31 p 202 N84-32318

SATELLITE IMAGERY

LANOSAT-4 Science Investigations Summary, including

December 1983 Workshop results+ volume 1

[E84-101661 p 137 N84-30359

The Multispectral Imaging Science Working Group

Volume 1: Executive summary

{E65-100011 p 142 N85-11404

The Multispectral Imaging Science Working Group,

Volume 2: Working group reports

IE85-t0002J p 142 N85-11405

LANDSAT-4 Science Characterization Early Results.

Volume 1: Multispectral Scanner (MSS)

{E85-t00.67J p 143 N85-20496

LANDSAT-4 Science Characterizs*Jon Early Results.

Volume 2, part 1: Thematic Mapper (TM)

(E85-100681 p 143 N85-20508

LANDSAT-4 Science Characterization Early Results.

Volume 3, part 2: Thematic Mapper ('I'M)

[E85-10069] p 143 N85-21724

LANDSAT-4 Science Cher_'tedzation Early Results.

Volume 4: Applications --- agriculture, =oils land usa,

geology, hydrology, wetlands, water quality, btomass

identification, and snow reaping

[E85-t0070] p 143 N85-23186

SATELLITE OOaERVATION

Proceedings: Workshop on the Need for Lightning

Observations from Space

[NASA-CP-2095) p 152 N79-30869

Earth Radiation Budget Science, 1978 --- conferences

[NASA-CP-2100] p 160 N79-32797

The time-apace relationship of the date point (Plxels)

of the thematic mapper and multispectrel =m._nner or the

myth of simultaneity

[NASA-TP-1715] p 76 N80.28424

Atmosphenc structure determined from satellite data

[NASA-RP-1071] p 162 N81.16,678

Meteorological satellites: Past, present, and future

[NASA-CP-2227] p 164 N82-24781

The Conception, Growth, Accomplishments and Future

of Meteorological Satellites

[NASA-CPo2257] p 164 N83-t4825

Frontiers of Remote Sensing of the Oceans and

Troposphere from Air and Space Platforms

[NASA.CP-2303] p 142 N84.27262

Earth resources: A continuing bibliography with indexes,

issue 50

[NASA-SP-7041(50)] p 143 N66-31940

SATELLITE ORBITS

Flight Mechanics/Estimation Theory Symposium

[NASA-CP-2050] p 64 N79-14121

Flight Mechanics/Estimation Theory Symposium --- with

application to autonomous navigation and attitude/orbit

determination

[NASA-CP-2082] p 64 N79-26082

Orbit dynamics and geographical coverage capabilities

of satellite-based solar occultation experiments for global

monitoring of stratosphenc constituents

[NASA-TP-1606] p 64 N80-19142

Flight Mechanics/Estimation Theory Symposium

(NASA-CP-2123] p 64 N60-28389

Fifth Annual Flight Mechanics/Estimation Theory

Symposium

[NASA-CP-2152] p 64 N61-11070

ATS-6 engineering performance report. Volume 2: Orbit

and attitude controls

{NASA-RP-t080-VOL-2J p 73 N82-16148

SATELLITE POWER TRANSMISSION (TO EARTH)

Solar Power Satellite Microwave Transmission and

Reception

[NASA-CP-2141 } p 145 N8t-16533

Satellite power system: Concept development and

evaluation program Volume 3: Power transmission and

reception. Technical summary and assessment

[NASA-RP-1076] p 145 N61-27622

Space Laser Power Transmission System Studies ---

conferences

[NASA-CP-2214] p 117 N62-18678

SATELLITE SOLAR ENERGY CONVERSION

Analysis of costs of gallium arsenide and silicon solar

arrays for space power applications

lNASA_TP-1811J p 77 N61-20173

SATELLITE SOLAR POWER STATIONS

AIAA/MSFC Symposium on Space Industrialization:

Proceedings

[NASA-CP-2026] p 60 N78-18088

SATELLITE SOUNDING

VAS Demonstration Sounding Workshop: The

Proceedings of a satellite sounding workshop

[NASA-CP-2157} p 163 N81-19709

Goddard Laboratory for Atmospheric Science, collected

reprints 1976-1979, volume t

[NASA-TP-1768-VOL-1 ] p 163 N81-21686

Goddard Laboratory for Atmospheric Sciences,

collected reprints 1978 - 1979, volume 2

INASA-TP-1788-VOL-2] p 163 N81-21693

SATELLITE SURFACES

Phobos: Close encounter imaging from the Viking

Orbiters

INASA-RP-t 109j p 207 N84-32330

Voyager I and 2 atlas of six Saturnian satellites

INASA-SP-474] p 208 N84-35242

SATELLITE TELEVISION

ATS-6 engineering performance report. Volume 4:

Television experiments

(NASA-RP-1080-VOL-4I p 73 N82-16150

SATELLITE TRACKING

National geodetic satellite program, part 1

(NASA-SP-365-PT-1 I p 15t N78-t1545

National geodetic satellite program, part 2

[NASA-SP-365-PT-2] p 151 N78-11552

Orbital Debris

I NASA-CP-2360J p 63 N85-21188

SATELLITE TRANS, Mtl_ION

Thermal anomalies of the transmitter experiment

package on the communications technology satellite

[NASA-TP-1410] p 69 N7g-21120

Rsdio-wsve propagation for apace communications

systems

[NASA-TP-1770] p 70 N61-18082

Propagation effects handbook for satellite systems

design: A summary of propagation impairments on 10

to 100 GHz satellite links with techniques for system

design

[NASA-RP-1062] p 100 N62-15270

ATS-8 engineering performance report. Volume 5:

Propagation experiments

[NASA-RP-t080oVOL.5] p 73 N62-16151

SATELLITE-BORNE INSTRUMENTS

An introduction to orbit dynamics and its application to

satellite-based earth monitoring systems

[NASA-RP.1009] p 64 N78-t2113

Active Microwave Users Workshop Report

[NASA-CP-2030] p 138 N78-21562

Proceedings: Workshop on the Need for Lightning

Observations from Space

[NASA-CP-2095] p 152 N79-30869

VAS Demonstration Sounding Workshop: The

Proceedings of a satellite sounding workshop

[NASA-CP-2157] p 163 N81-19709

Guidelines for spaceborne microwave remote sensors

[NASA-RP-1086] p 140 N82-19647

Handbook of sensor technical characteristics

[NASA-RP-t087] p 115 N82-29677

Spaceborne Gravity Gradiometers

[NASA-CP-23051 p 136 N64-18716

SATELLITE-BORNE PHOTOGRAPHY

NASA ground-based and space-based laser ranging

systems

[NASA-TP-1149] p 113 N78°17360

Apollo-Soyuz test proiect. Volume 2: Earth observations

and photography

INASA-SP-412-VOL-2] p 138 N80-10536

Voyager 1 and 2 atlas of six Saturnian satellites

[NASA-SP-474] p 208 N84-35242

SATURN (PLANET)

Voyager to Jupiter and Saturn

[NASA-SP-420] p 205 N77-29046

Pioneer: First to Jupiter, Saturn, and beyond

{NASA-SP-446] p 206 N81-15925

Voyages to Saturn

{NASA'SP'451J p 207 N82-26152

SATURN ATMOSPHERE

The Saturn System

{NASA-CP-2068] p 205 N79-16758

SATURN PROJECT

The Saturn System

{ NASA-CP-2068] p 205 N79-16758

Stages to Saturn: A technological history of the

Apollo/Saturn launch vehicles

INASA-SP-42061 p 72 N61-29154

Voyager 1 and 2 atlas of six Saturnian satellites

INASA-SP-474] p 208 N84.35242

SATURN RINGS

The Saturn System

INASA-CP-2068] p 205 N79-16758

SATURN SATELLITES

Voyages to Saturn

[NASA-SP-451 ] p 207 N82-26152

Voyager 1 and 2 atlas of six Saturnian satellites

[NASA-SP-4741 p 206 N84-35242

SAUOI ARABIA

Oiscrimination of rock classes and alteration products

in southwestern Saudi Arabia with computer-enhanced

LANDSAT data

INASA-TP-1327| p 136 N78-33499

SCALE EFFECT

Airframe noise of a small model transport aircraft and

scaling effects --- Boeing 747

I NASA-TP-18581 p 188 N81-22832

SCALE MODELS

Effect of winglets on a first-generation jet transport wing.

4: Stability characteristics for a full-span model at Much

0.30

JNASA-TP-t 119} p7 N78-17997

Effect of design changes on aerodynamic and acoustic

performance of translating-centerbody sonic inlets

[NASA-TP-1132] p 7 N76-17996

Applied Routh approximation

[NASA-TP-t231 ] p 98 N76-22257

A wind-tunnel study of the applicability of far-field

sonic-boom theory to the space shuttle orbiter

[NASA-TP-1186] p 8 N76-25061

Similitude requirements and scaling relationships as

applied to model testing

{NASA-TP-14351 p 33 N79-30176

A-102
SUBJECT INDEX

Water.tunnel and analytical investigation of the effect

of strake design variables on streke vortex breakdown

characteristics

[NASA.TP.1676] p 15 N80-28304

Wind-tunnel evaluation of a 21-percent-scale powered

model of • prototype advanced scout helicopter

[NASA-TP-_2420] p 26 N85-28923

SCALING LAWS

A fan pressure ratio correlation in terms of Mach number

and Reynolds number for the Langley 0.3 meter transonic

cryogenic tunnel

[NASA-TP-1752] p 16 N81-10005

A potential-energy scaling model to simulate the initial

stages of thin-film growth

[NASA-TP-2102] p 88 N83-t8895

SCANNERS

A Scanning laser-velocimeter technique for measuring

two-dimensional wake-vortex velocity distributions ---

Langley Vortex Research Facility

[NASA-TP-t661 ] p 114 N80-24594

SCANNING

Effects of curved approach paths and advanced displays

on pilot scan patterns

[NASA-TP-1646] p 171 N81-23791

SCATTERING

Wind Tunnel Seeding Systems for Laser Vetocimeters

[NASA-CP-2393) p 116 N86-11437

SCATTERING CROSS SECTIONS

Optical.model abrasion cross sections for high-energy

heavy ions

[NASA-TP.1893] p 192 N81-27899

Airborne Lidar measurements of aerosols, mixed layer

heights, end ozone during the 1980 PEPE/NEROS summer

field experiment

[NASA.RP-1143] p 150 N86-t6748

SCENE ANALYSIS

An image compression survey and algorithm switching

based on scene activity

[NASA-TP-2458] p 27 N85-33106

SCHEDULING

Simulation studies of time-control procedures for the

advanced air traffic control system

[NASA-TP-2493] p 30 N95-32101

SCHLIEREN PHOTOGRAPHY

Rainbow Schlieren

[NASA-TP-2166] p 116 N83-33126

Optical elements formed by compressed gases:

Analysis and potential applications

[NASA-TP-2555] p 194 N86-22390

SCNOTI"KY DIODES

Terrestrial photovoltaic measurements, 2

[NASA-CP-20t0] p 136 N77-30521

Topics in the optimization of millimeter-wave mixers

[NASA-TP-2287} p 103 N84-20758

Effect of barrier height on friction behavior of the

semiconductors silicon end gallium arsenide in contact with

pure metals

[NASA-TP-2405] p 96 N85-13044

SCIENCE

Engineering and Scientific Data Management

[NASA-CP-2058] p 178 N78-33776

The Impact of Science on Society

[NASA.SP-482] p 196 N85-24994

SCOOPS

Aerodynamic and directional acoustic performance of

e scoop inlet

[NASA-TP-t028] p 41 N77-31152

SEA ICE

The role of satellite altimetry in climate studies

[NASA-TP-1570] p 161 N80-16676

Antartic sea ice, 1973 - 1976: Satellite

pesslve-microweve observations

[NASA-SP-459] p 168 N84-10718

Frontiers of Remote Sensing of the Oceans and

Troposphere from Air and Space Platforms

[NASA-CP-2303] p 142 N84-27262

SEA ROUGHNESS

Radiometer requirements for Earth-observation systems

using large space antennas

[NASA-RP-1101] p 116 N83-28410

SEA STATES

NASA Wallops Flight Center GEOS-3 altimeter data

processing report

[NASA-RP-1066] p 139 N81-t 1438

SEALS (STOPPERS)

Friction and wear of several compressor gas-path seal

movements

[ NASA-TP-f 128] p86 N78-15229

Compressible flow across narrow passages:

Comparison of theory and experiment for face seals

[NASA-TP-1346] p 120 N79-10424

Comparison of analysis and experiment for self-acting

seals for liquid-oxygen turbopumps

[NASA-TP-1443] p 120 N79-22519

Self-acting lift-pad geometry for circumferential seals:

A noncontacting concept --- performance tests on

hydrodynamic seals

[NASA-TP-t583} p 121 N80-14403

Damping seals for turbomschinery

[NASA-TP-1987] p 49 N82-20183

Flow through aligned sequential orifice type inlets

[NASA-TP-t967] p 109 N82-20467

Film thickness measurement for spiral groove and

Rayie0gh step lift pad setf-actiog face seals

[NASA-TP-2058] p 4g N83-11t26

Design analysis of a self-acting spiral-groove ring seal

for counter-rotating shafts

[NASA-TPo2142] p 50 N83-25712

Dynamic behavior of spiral-groove and Rayleigh-Step

self-acting face seals

{NASA.TP-22661 p 51 N84-16181

High-temperature erosion of plasma-sprayed,

yttria-stabilized zirconia in a simulated turbine

environment

[NASA-TP-2406] p 96 N85-13045

Dynamic response of film thickness in spiral-groove face

seals

[NASA-TP-2544] p 52 N86-15313

SEARCH PROFILES

The search for extraterrestrial intelligence (SETI)

[NASA-SP-41g] p 175 N78-18771

SEASAT 1

The role of satellite altimetry in climate studies

[NASA-TP-1570] p 181 N80-16676

SEATS

Evaluation of g seat augmentation of fixed-base/moving

base simulation for transporl landings under two visually

imposed runway width conditions

[NASA-TP-2135] p 36 N83-22191

Effects of motion base and g-seat cueing of simulator

pilot performance

[NASA-TP-2247] p 37 N84-18189

Survey of NASA research on crash dynamics

[NASA-TP-2298] p 133 N84-21901

SECONDARY EMISSION

Beam impingement angle effects on secondary electron

emission characteristics of textured pyrolytic graphite

[NASA-TP-2265] p 95 N84-18400

Secondary electron emission characteristics of

ion-textured copper and high-purity isotropic graphite

SUrfaces

[NASA-TP-2342} p 95 N84-28989

Textured carbon on copper: A novel surface with

extremely low secondary electron emission

characteristics

[NASA-TP-2543] p 98 N86-15394

Secondary-electron-emission losses in multistage

depressed collectors and traveling-wave-tube efficiency

improvements with carbon collector electrode surfaces

[NASA-TP-2622] p 103 N86-32629

SEDIMENT TRANSPORT

Literature review of organic matter transport from

marshes

[E83-10352] p 142 N83-29750

SEDIMENTS

Laboratory measurements of upwelled radiance and

reflectance spectra of Calvert, Ball, Jordan, and Feldspar

soil sediments

[NASA-TP-1039] p 167 N78-12645

Laboratory and field measurements of upwetied radiance

and reflectance spectra of suspended James River

sediments near Hopewell, Virginia

[NASA-TP-1292] p 147 N78-33616

Laboratory upwetted radiance and reflectance spectra

of Kerr reservoir sediment waters

[NASA-TP-1993] p 150 N82-21774

SELF ADAPTIVE CONTROL SYSTEMS

Structural dynamics and control of large space structures

--- conference

[NASA-CP-2187] p 66 N81-26166

Self-tuning regulators for multicyclic control of helicopter

vibration

[NASA-TP-19961 p 57 N82-20188

SELF LUBRICATING MATERIALS

Plasma-sprayed coatings for lubrication of a titanium

alloy in air at 430 deg C

[NASA-TP-1509] p 93 N79-29327

SELF LUBRICATION

Effect of aluminum phosphate additions on composition

of three-component plasma.sprayed solid lubricant

[NASA-TP-1990] p 88 N82-21298

SELF REPAIRING DEVICES

Restructurabie Controls

[NASA_P-22771 p 57 N83-33896

SEMICONDUCTOR DEVICES

Heterodyne Systems and Technology, part 2

[NASA-CP-2138-PT-21 p 117 N80-29672

SEMICONDUCTOR JUNCTIONS

Solar Cell High Efficiency and Radiation Damage

[NASA-CP-2020} p 144 N78-13527

SERIES EXPANSION

A simple model of space radiation damage in GaAs solar

cells

INASA-TP-2242J p 192 N84-13978

SEMICONDUCTOR LASERS

Excess noise in tunable diode lasers

[NASA-TP-1935] p 117 N82-12431

SEMICONDUCTORS (MATERIALS)

Space Photovoltaic Research and Technology 1980,

High Efficiency, Radiation Damage and Blanket

Technology

[NASA-CP-2169] p 145 N8t-17531

Semiconductor photoelectrochemistry

[NASA-TP-2088] p 146 N83-18024

Friction behavior of silicon in contact with titanium, nickel,

silver and copper

[NASA-TP-2362 p 96 N84-33590

Effect of barrier height on friction behavior of the

semiconductors silicon and gallium arsenide in contact with

pure metals

[NASA-TP-2405 p 96 N85-13044

SENSITIVITY

An algorithm for maximum likelihood estimation using

an efficient method for approximating sensitivities

[NASA-TP-2311 p 58 N84-25717

SENSORIMOTOR PERFORMANCE

Effects of curved approach paths and advanced displays

on pilot scan patterns

[NASA-TP-1846 p 171 N81-23791

SENSORS

Evaluabon of a total energy-rate sensor on a transport

airplane

[NASA-TP-2212 p 40 N84-12164

SENSORY PERCEPTION

Effects of curved approach paths and advanced displays

on pilot scan patterns

[NASA-TP-t846 p 171 N61-23791

SEPARATED FLOW

Computation of transonic boattsil flow with separation

[NASA-TP-1070] p 7 N76-13017

Turbulent-flow separation criteria for overexpanded

supersonic nozzles

[NASA-TP-1207] p 105 N78-30554

Inverse boundary-layer theory and comparison with

experiment

[NASA-TP-1208] p 106 N78-32385

investigation of flow characteristics over missile bodies

at supersonic speeds

[NASA-TP-1579J p 13 N80-13001

Some flow phenomena associated with aligned,

sequential apertures with Borda-type inlets --- inlet

pressure and flow separation

[NASA-TP-1792] p 109 N81-24387

Crossflow effects on steady and fluctuating pressures

on an ogive-cylinder cone-frustum model in supersonic

separated flow

[NASA-TP-1951] p 18 N82-13106

Flow through aligned sequential orifice type inlets

[NASA-TP-1967] p 109 N82-20467

Effects of flow separation and cove leakage on pressure

and heat-transfer distributions along a wing-cove-eievon

configuration at Mach 6.9 --- Langley 8*ff high temperature

tunnel test

[NASA-TP-2127} p 111 N83-26378

SEPARATORS

Three methods for in situ cross-linking of polyvinyl

alcohol films for application as ion-conducting membranes

in potassium hydroxide electrolyte --- battery separators

[NASA-TP-1407] p 78 N79-21128

Control of volume resistivity in inorganic organic

separators

[NASA-TP-14391 p 84 N79-22246

Improved, low cost inorganic-organic separators for

rechargeabio silver-zinc batteries

[NASA-TP-t476] p 84 N79-25181

Rolling-element bearings

[NASA-RP-1105] p 123 N83-27214

SEQUENTIAL ANALYSIS

Sequential high-resolution wind profile measurements

[NASA-TP-1354] p 159 N79-14680

SERIES (MATHEMATICS)

Hydroelastic vibration analysis of partially liquid-filled

shells using a series representation of the liquid

[NASA-TP-1558] p 129 N80-19563

An integral representation of the generalized

Euier-Mascheroni constants

[NASA-TP-2456] p 177 N85-23305

SERIES EXPANSION

The generalized Euler-Mascheroni constants

[NASA-TP-2264] p 185 N84-15880

Mixed models and recugion techniques for

large-rotation, nonlinear analysis of shells ot revolution with

application to tires

[NASA-TP-2343J p 133 N84-34773

A-103
SERVICE LIFE

SERVICE LiFE

Materials constitutive models for nonlinear analysis of

thermally cycled structures

[NASA-TP-2055] p 131 N83-12449

Service life evaluation of rigid exptosNe transfer lines

[NASA-TP-2143] p 36 N83-31596

A method for developing design diagrams for ceramic

and glass materials using fatigue data

[NASA-RP-1174] p 128 N86-32763

SERVICES

Proceedings of the First Annual Meteorological and

Environmental Inputs to Aviation Systems Workshop

[NASA.CP.2028] p 158 N78.19711

SERVOMECHANISMS

Predicting dynamic performance limits for servosystems

with saturating nonlinearities

(NASA.TP-1488] p 54 N79-28186

Single.stage electrohydreulic servosystam for actuating

on airflow vane with frequencies to 500 hertz

[NASA.TP.1678] p 56 N80-29369

Simulator study of pilot-aircraft.display system response

obtained with a three-dimensional.box pictorial display

[NASA-TP-2122] p 40 N84-13182

SEWAGE TREATMENT

Laboratory measurements of radiance and reflectance

spectra of dilute pnmary-treated sewage sludge

[NASA-TP-1038] p 147 N78-12554

SHAFTS (MACHINE ELEMENTS)

Rolling-element fatigue life of AISI M-50 and 18-4-1

balls

{NASA-TP.1202] p 119 N78-2t473

Operating characteristics of high-speed, jet-lubricated

35-miUimeter-bore ball bearing with a

single-outer-land-guided cage

INASA-TP-1657] p 121 N80-21753

Effect of cage design on characteristics of

high-speed-jet-lubricated 35-millimetarobore ball boating ---

turbojet engines

{NASA-TP-1732} p 121 N80-33749

Design of power-transmitting shifts

[NASA-RP-1123] p 124 N84-27041

SHAKERS

Lewis Research Center spin rig and its use in vibration

analysis of rotating systems

[NASA-TP-2304] p 51 N84-24578

SHALE OIL

Effect of hydroprocessing severity on chatectatJstics of

jet fuel from OSCO 2 and Pareho distillates

[NASA-TP-1768] p 97 N81-24283

SHAPE CONTROL

Large Space Systems Technology, part 2, 198t

[NASA.CP-2215-PT-2] p 66 N82-19257

SHAPES

A theoretical investigation of forebody shapes designed

for natural laminar boundary-layer flow

[NASA-TP-1375] p 11 N79-t5903

Effects of erodant particle shape and various heat

treatments on erosion resistance of plain carbon steel

[NASA-TP-t755J p 87 N81-16210

A procedure for designing forebodies with constraints

on cross-section shape and axial area distribution

[NASA-TP-1881} p 17 N81-26078

Medal analysis of a nonuniform string with end mass

and vanabte tension

[NASA-TP-21981 p 67 N83-32826

Computer-Aided Geometry Modeling

INASA-CP-2272] p 177 N84-22179

Sem_anelytic modeling of aerodynamic shapes

[NASA-TP-2413] p 25 N85-21120

Fluid surface behavior in low gravity, Center

discretionary fund no. 83-21

[NASA-TP-2486] p 113 N85-28260

SHEAR FLOW

The disturbance flow field produced by an evolving

vortex

[NASA-TP-2245] p 111 N84-13500

A method for determining acoustic-liner admittance in

ducts with sheared flow in two-cross-sectional directions

[NASA-TPo2518] p 190 N86-13056

Motion end interaction of decaying trailing vortices in

spanwise shear wind

[NASA-TP-2599J p 5 N86-29762

SHEAR LAYERS

Stochastic enalys_s of spectral broadening by a free

turbulent shear layer

[NASA-TP-1816] p t88 N81-24884

Supersonic jet no,se generated by large scale

instabilities

[NASA-TP-2072] p 188 N82-34189

SHEAR STRENGTH

Friction and wear of metals with _ single-crystal 8braswe

grit of silicon carbide: Effect of shear strength of metal

[NASA-TP-1293] p 92 N78-30238

Correlation of ideal and actual shear strengths of metals

with their friction properties

[NASA-TP-1891 ] p 94 N81-27282

A-104

Experimental data on single-bolt joints in quasi isotropic

graphite/polyimide laminates

[NASA-TP-2015] p 81 N82-25325

SHEAR 8TRESS

Representation of turbulent shear stress by a product

of mean velocity differences

[NASA-TPot028] p 104 N77-3144t

An improved tranaverae shear deformation theory for

laminated enttsotropic plates

[NASA-TP.tg03] p 130 N82-11488

Buckllng loads of stiffened panels subjected to combined

longitudinal compression and shear, Results obtained with

PASCO, EAL, and STAGS computer programs

[NASA.TP.2215] p 132 N84-16585

A cracked orthotro_ic sheet stiffened by a semi.infinite

orthotropic sheet

[NASA-TP-2455] p 134 N85.32339

SHELLS (STRUCTURAL FORMS)

Nonlinear Structural Analysis

[NASA-CP-22971 p 133 N84.3t688

Mixed models and recugidn techniques for

large-rotation, nonlinear analysis of shells of revolution with

application to tires

[NASA.TP.2343] p 133 N84-34773

Joint research effort on vibrations of twisted plates,

phase t: Final results

INASA-RP-11501 p 135 N86-10579

SHIELDING

Fluid shielding of high-velocity jet noise

NASA-TP-2258} p 189 N84-15894

SHOCK ABSORBERS

Effect of underwing aft-mounted nacelles on the

longitudinal aerodynamic characteristics of a high-wing

transport airplane

NASA-TP-2447] p 27 N8B-20345

SHOCK LAYERS

A numerical SOlution of the Nevier-Stokes equations for

chemically nonequilibrium, merged stagnation shock layers

on spheres and two-dimensional cylinders in air

NASA-TP-t227J p t05 N78-23390

Aerothatmal tests of a 12.5 percent cone at Mach 6.7

for various Reynolds numbers, angles of attack and nose

shapes --- conducted in Langley 8-foot high temperature

tunnel

NASA-TP.2345] p 112 N85-17322

SHOCK LOADS

Preliminary vibration, acoustic, and shock design and

test criteria for components on the Lightweight External

Tank (LWT)

NASA-RP-1074] p 71 N81-19218

SHOCK RESISTANCE

Measured and predicted shock shapes and aerodynamic

coefficients for blunted cones at incidence in helium at

Mech 20.3

NASA-TP-1395] p 106 N79-20345

Preliminary study of methods for providing thermal shock

resistance to plasma-sprayed ceramic gas-path seals

[NASA-TP-1561 J p 93 N80-23453

SHOCK SPECTRA

Shock response spectra variational analysis for

pyrotechnic qualification testing of flight hardware

{NASA-TP-2315] p 74 N84-23676

Recovery of pyroshock data from distorted acceleration

records

[NASA-TP-2494] p 75 N85-31141

SHOCK TESTS

Shock response spectra variational analysis for

pyrotechnic qualification testing of flight hardware

INASA-TP-2315] p 74 N84-23676

Vibration, acoustic, and shock design and test criteria

for components on the Solid Rocket Boosters (SRS),

Lightweight Extatnat Tank (LWT), and Space Shuttle Main

Engines (SSME)

[NASA-RP-11271 p t34 N85-10405

SHOCK TUBES

Applicabon of shock tubes to transonic airtoil testing

at high Reynolds numbers

[NASA-TP-1268] p 10 N79-12013

SHOCK WAVE A'I'rENUATION

Forward acoustic performance of a shock-swallowing

high-tip-speed fan (QF.13)

[NASA-TP.1668] p t87 N80-23100

SHOCK WAVE CONTROL

Turbojet-exhaust-nozzle secondary-airflow pumping as

an exit control of an inlet-stability bypass system for a

Mech 2.5 axisymmetric mixed-compression inlet --- Lewis

10- by 10-fl. supersonic wind tunnel test

[NASA-TP.1532] p 48 N80-14124

SHOCK WAVE INTERACTION

Wake-shock interaction at a Mech number of 6

[NASA-TP-f103J p 105 N78-2233t

Sonic-boom wave-front shapes and curvatures

associated with maneuvering flight

{NASA-TP-t6tt] p 13 N80-14045

SUBJECT INDEX

SHOCK WAVES

Chemica_ kinetic medeiing of benzene and toluene

oxidation behind shock waves

[NASA-TP-1472] p 84 N78-28259

Measured and predicted shock shapes and aerodynamic

coefficients for blunted cones at incidence in sir at Mech

5,9

[NASA-TP-t652] p 108 N80-23600

SAGE measurements of the stratospheric aerosol

dispersion and loading from the Soufriere Volcano

[NASA.TP.1922] p 153 N82-12687

Fringe localization requirements for three.dimensional

flow visualization of shock waves in diffuse-illumination

double-pulse holographic interferometry

[NASA-TP-1868] p 115 N82-22481

ignition of SiH4-H2-O2-N2 behind reflected shock

waves

[NASA-TP-2114] p50 N83-18727

An analysis of shock coalescence including

three-dimensional effects with application to sonic boom

extrapolation

{NASA-TP-2214] p 111 N84-22906

Solar Terrestrial Physics: Present and Future

[NASA-RP-1120] p 200 N84-34332

Local stability analysis for a planar shock wave

[NASA-TP-2387J p 25 N85-12864

A comparative study of the nonuniqueness problem of

the potential equation

(NASA-TP-2385] p 25 N85-15694

Ignition of mixtures of Sill sub 4, CH sub 4, O sub 2,

and Ar or N sub 2 behind reflected shock waves

[NASA-TP-2415J p 52 N85-22395

SHORT HAUL AIRCRAFT

Static test-stand performance of the YF-tO2 turbofan

engine with several exhaust configurations for the Quiet

Short-Haul Research Aircraft (QSRA)

[NASA-TP-1556] p 45 N80-t4121

Static and transient performance of YF-102 engine with

up to t4 percent core airbleed for the quiet short-haul

research aircraft

[ NASA-TP-1692] p47 N80-25339

Low-speed aerodynamic performance of

50.8-centimeter-diameter noise-suppressing inlets for the

Quiet, Clean, Short-haul Experimental Engine (QCSEE) ---

Lewis 9- by 15-fool low speed wind tunnel tests

I NASA-TP-t 178 J p47 N81-11037

SHORT TAKEOFF AIRCRAFT

A flight investigation of the stability, control, and handling

qualities of an augmented jet flap STOL airplane

{NASA-TP-1254J p 53 N78-26151

Effects of errors on decoupled control systems

INASA-TP-1184] p 53 N78-27138

Experimental study of acoustic loads on an

upper-surface-blown STOL airplane configuration ---

Langley full-scale wind tunnel tests

INASA-TP-1577J p 187 N80-13879

Evaluation of approximate methods for the prediction

ot noise shielding by airframe components

[NASA-TP-tOO4] p 46 N80-15129

Flight tests of the total automatic flight control system

{Tafcos) concept on a DHC-6 Twin Otter aircraft

{NASA-TP-15131 p 55 N80-17081

Large-scale wind-tunnel tests of inverting flaps on a

STOL utility aircraft model

{NASA-TP-16g61 p 34 N80-25318

Flight evatuat,'on of stabilization and command

augmentation system concepts and cockpit disptays dunng

approach and landing of powered-lift STOL aircraft

INASA-TP-1551 ] p 56 N81-tt044

Flight-test evaluation of STOL control and flight director

concepts in a powered-lift aircraft flying curved

decelerating approaches

[NASA-TP-1641J p 56 N81-19131

Design criteria for flightpath and airspeed control for

the approach and landing of STOL aircraft

[NASA-TP-1911 ] p 57 N82-20187

The application of parameter estimation to flight

measurements to obtain laterel-directionel stability

derivatives of an augmented jet-flap STOL airplane

{NASA-TP-20331 p 57 N83-16350

Thrust-induced effects on subsonic longitudinal

aerodynam,c charactenstics of a

vectored-engine-over-wing configuration

[NASA-TP-2228] p 22 N84-13163

Flight-test of the glide-slope track and flare-control laws

for an automatic landing system for a powered-lift STOL

a_rplane

[NASA-TP-2128] p 57 N84-t3198

Static investigation of two STOL nozzle concepts with

pitch thrust-vectoring capability

{NASA-TP-2559J p 28 N86-23559

SHOT PEENING

Effect of shot peening on surface fatigue life of

carburized and hardened AISI 9310 spur gears

{NASA-TP-2047] p 122 N82-32736
SUBJECT INDEX

SHOULDERS

Modified Denavit-Hartenberg parameters for better

location of joint axis systems in robot arms

[NASA-TP-2585] p 183 N86-27953

SHROUDED TURBINES

Aerodynamic effect of a honeycomb rotor tip shroud

on a 50 8-centimeter-tip-diameter core turbine

[NASA-TP-21121 p 49 N83-17547

SIDESLIP

Kinematic properties of the helicopter in coordinated

turns

[NASA-TP-1773] p 35 N81-22039

SIGNAL DISTORTION

Computer modeling of multiple-channel input signals and

intermodulation losses caused by nonlinear traveling wave

tube amplifiers

[NASA-TP-1999] p 102 N82-25441

Recovery of pyroshock data from distorted acceleration

records

[NASA-TP-2494] p 75 N85-31141

An image compression survey and algorithm switching

based on scene activity

[NASA-TP-2458] p 27 N85-33106

SIGNAL GENERATORS

Optical Information Processing for Aerospace

Applications 2

[NASA-CP-2302] p 194 N84-22402

SIGNAL PROCESSING

Application of coherence in fan noise studies

[NASA-TP-1630] p 187 N80-18882

Nimbus 6 Random Access Measurement System

applications experiments

[NASA-SP-4571 p 165 N83-14835

SETI science working group report

(NASA-TP-2244] p 175 N84-22178

Adaptive identification and control of structural dynamics

systems using recursive lattice filters

[NASA-TP-2371 ] p 75 N85-31142

SIGNAL TO NOISE RATIOS

Excess noise in tunable diode lasers

[NASA-TP-1935) p 117 N82-12431

Algorithm for astronomical, extended source_

signal-to-noise radio calculations

[NASA-TP-2396] p 202 N85-12833

Algorithm for astronomical, point source, signal to noise

ratio calculations

[NASA-TP-2397] p 202 N85-12834

SIGNATURE ANALYSIS

A study of the sonic-boom characteristics of a blunt body

at a Math number of 6

[NASA-TP-1787] p 3 N81-13915

SIGNATURES

Near-field sonic-boom pressure signatures for the space

shuttle launch and orbiter vehicles at Mach 6

[NASA-TP-1405 J p68 N79-21119

SILANES

Development of silane-hydrolysate binder for

UV-resistant thermal control coatings

[NASA-TP-1900J p 94 N81-31365

Ignition of SiH4-H2-O2-N2 behind reflected shock

waves

[NASA-TP-2114J p 50 N83-18727

A chemical kinetic mixture for the ignition of

silane/hydrogen mixtures

[NASA-TP-2129] p 65 N93-t9825

Homogeneous reactions of hydrocarbons, silane, and

chloresitanes in radiofrequency plasmas at low

pressures

[NASA-TP-2301] p 79 N84-20643

Ignition of mixtures of Sill sub 4, CH sub 4, O sub 2,

and Ar or N sub 2 behind reflected shock waves

(NASA-TP-2415] p 52 N85-22395

SILENCERS

A study of resonant-cavity and fiberglass-filled parallel

baffles as duct silencers --- for wind tunnels

[NASA-TP-1970] p 188 N82-24052

SlLICIDES

Friction and wear of radiofrequency-sputtered borides,

silicides, and carbides

[NASA-TP-tt56] p 91 N78-20338

SILICON

Pressureless sintered Sialons with low amounts of

sintering aid

[NASA-TP-1246] p 92 N78-25215

Wear of aluminum and hypoeutectic aluminum-silicon

alloys in boundary-lubricated pin-on disk sliding

[NASA-TP-1442] p 87 N79-21184

Space Photovottaic Research and Technology 1980.

High Efficiency, Radiation Damage and Blanket

Technology

[NASA-CP-2169] p 145 N81-17531

Analysis of costs of gallium arsenide and silicon solar

arrays for space power applications

[NASA-TP-1811J p 77 N81-20173

Effect of barrier height on friction behavior of the

semiconductors silicon and gallium arsenide in contact with

pure metals

[NASA-TP-2405] p 96 N85-13044

SILICON CARBIDES

Friction and wear behavior of single-crystal silicon

carbide in contact with titanium

INASA-TP-10351 p 91 N77-32312

Friction and deformation behavior of single-crystal

silicon carbide

[NASA-TP-1053] p 91 N77-33350

Friction and metal transfer for single-crystal silicon

carbide in contact with various metals in vacuum

IrNASA-TP-1191 ] p 91 N78-21294

Wear of single-crystal silicon carbide in contact with

vanous metals in vacuum

[NASA-TP-1198J p 92 N78-21295

Effect of oxygen and nitrogen interactions on friction

of single-crystal silicon carbide

[NASA-TP-1265J p 92 N78-28247

Friction and wear of metals with a single-crystal abrasive

grit of silicon carbide: Effect of shear strength of metal

[NASA-TP-1293] p 92 N78-30238

Friction and wear with a single-crystal abrasive grit of

silicon carbide in contact with iron base binary alloys in

oil: Effects of alloying element and its content

[NASA-TP-1394] p 120 N79-17227

Anisotropic friction, deformation, and fracture of

single-crystal silicon carbide at room temperature

[NASA-TP-1525] p 93 N79-30380

Adhesion and friction of iron-base binary alloys in contact

with silicon carbide in vacuum

{NASA-TP-1604] p 87 N90-15234

Wear particles of single-crystal silicon carbide in

vacuum

_NASA-TP-1624 I p 93 N80-18178

Friction and wear of iron-base binary alloys in sliding

contact with silicon carbide in vacuum

[NASA-TP-16121 p 93 N80-22494

Changes in surface chemistry of silicon carbide (0001)

surface with temperature and their effect on friction

[NASA-TP-1756] p 94 N81-14079

Surface chemistry end friction behavior of the silicon

carbide (0001) surface at temperatures to 1500 deg (3

[NASA-TP-1813] p 94 N81-19300

Surface chemistry and wear behavior of single-crystal

silicon carbide sliding against iron at temperatures to 1500

C in vacuum

[NASA-TP-19471 p 94 N82-19374

Interface control and mechanical property improvements

in silicon carbide/titanium composites

[NASA-TP-2066] p 61 N82-31451

Occurrence of spherical ceramic debris in indentation

and sliding contact

[NASA-TP-2048] p 95 N82-32491

Micrestructure and orientation effects on properties of

discontinuous si(icon carbide/aluminum composites

[NASA-TP-23021 p 79 N84-26749

SILICON COMPOUNDS

Effect of oxygen-nitrogen ratio on sinterability of

Sialons

[NASA-TP-1382] p 92 N79-21204

Modules of rupture and oxidation resistance of

S12.56AIO GOO 72N352 sialon

[NASAoTP-1490] p 93 N79-27309

SILICON NITRIDES

Effects of oxide additions and temperature on

sinterabitity of milled silicon nitride

[NASA-TP-1644] p 93 N90-21532

Effect of Yttria additives on properties of

)ressureless-sintered silicon nitride

NASA-TP-18991 p 94 N8t-31366

SILOXANES

Formulation/cure technology for ultrahigh molecular

weight sitphenylene-siloxane polymers

NASA-TP-2476] p 96 N85-26990

SILVER ZINC BATTERIES

Improved, low cost inorganic-organic separators for

rechargeable silver-zinc batteries

NASA-TP-1476] p 84 N79-25181

SILVICULTURE

Aerial color infrared photography: Applications in

citricutture --- Florida

[NASA-RP-t067] p 139 N81-21437

SIMILARITY THEOREM

Extension of similarity test procedures to cooled engine

components with insulating ceramic coatings

NASA-TP-1615} p 108 N80-24577

SIMILITUDE LAW

Similitude requirements and scaling relationships as

applied to model testing

NASA-TP-14351 p 33 N79-30176

SIMULATION

Proceedings of the First Annual Meteorological and

Environmental Inputs to Aviation Systems Workshop

NASA-CP-20281 p 158 N78-19711

SKIDDING

Development of a distributed-parameter mathematical

medal for simulat*on of cryogenic wind tunnels

[NASA-TP-2177] p 184 N83-35736

Simulation of lubricating behavior of a thioether liquid

lubricant by an electrochemical method

[NASA-TP-2316] p 95 N84-23764

SIMULATORS

Operating system for a real-time multiprocessor

propulsion system simulator User's manual

lNASA-TP.2426] p 180 N85-17596

SINE WAVES

Drag of two-dimensional small-amplitude symmetric and

asymmetric wavy walls in turbulent boundary layers

lNASA°TP-2318J p 112 N84-25944

SINGLE CRYSTALS

Friction and wear of single-crystal and polycrystalline

maganese-zinc ferrite in contact with various metals

[NASA-TP-1059] p 91 N78-10295

Friction and metal transfer for single-crystal silicon

carbide in contact with various metals in vacuum

[NASA-TP-1191 I p 91 N78-21294

Wear of single-crystal silicon cart_de in contact with

vanous metals in vacuum

[NASA-TP-1198] p 92 N78.21295

Effect of oxygen and nitrogen interactions on fricGon

of single-crystal silicon carbide

fNASA-TP-1265_ p 92 N78-28247

Anisotropic friction and wear of single-crystal

manganese-zinc ferrite in contact with itself

[NASA-TP-1339] p 120 N79-10425

Surface chemistry and wear behavior of single-crystal

silicon carbide sliding against iron at temperatures to 1500

C in vacuum

[NASA-TP-1947] p 94 N82-19374

Growth of high-quality thin-film Ge single crystals by

plasma-enhanced chemical vapor deposition

[NASA-TP-25321 p 100 N86-20586

SINGLE STAGE TO ORBIT VEHICLES

Static aerodynamic characteristics of a winged

single-stage-to-orbit vehicle at Mach numbers from 0.3 to

4.63

[NASA-TP-1233] p 9 N78-30053

SINGULARITY (MATHEMATICS)

Interaction of a turbulent-jet noise source with transverse

modes in a rectangular duct

INASA-TP-1248] p 1 N78-2504g

Translational control of a graphically simulated robot arm

by kinematic rate equations that overcome elbow joint

singularity

I NASA-TP-2376] p 181 N85-15446

SINTERING

Pressureless sintered Sialons with low amounts of

sintering aid

[NASA-TP-1246] p 92 N78-25215

Effect of oxygen-nitrogen ratio on sinterability of

Sialons

[NASA-TP-1382J p 92 N79-21204

Effects of oxide additions and temperature on

sinterability of milled silicon nitride

[NASA-TP-1644] p 93 N8O-21532

Effect of Yttria additives on properties of

pressureiess-sintered silicon nitride

INASA-TP-f899] p 94 N81-31366

SIPHONS

A siphon method of determining resistivities of thin

heat-pipe wicks

INASA-TP-1304] p 106 N79-10379

SITE SELECTION

Viking site selection and certification

[NASA-SP-429] p 207 N81-25992

Large Horizontal-Axis Wind Turbines

{NASA-CP-2230] p 146 N83-19231

Proceedings of the National Conference on Energy

Resource Management Volume 2: Applications

{E83-10336] p 142 N83.26176

Site selection and directional models of deserts used

for ERBE validation targets

INASA'TP'2540) p 167 N86-23160

SIZE (DIMENSIONS)

Subsonic aircraft: Evolution and the matching of size

to performance

[NASA-RP-1060] p 2 N80-29245

Effect of display size on utilization of traffic situation

display for self-spacing task --- transport aircraft

INASA-TP-1885] p 30 N81o29109

SKID LANDINGS

Abrasion behavior of aluminum and composite skin

coupons, stiffened skins and stiffened panels

representative of transport airplane structures

INASA-TP-2520] p 38 N86-133t6

SKIDDING

Friction end wear characteristics of wire-brush skids

INASA-TP-1495J p 33 N79-29171

Tire tread temperatures dunng antiskid braking and

cornering on a dry runway

{NASA-TP-20091 p 35 N82-24193

A-105
SKIN (STRUCTURAL MEMBER)

SKIN (STRUCTURAL MEMBER)

Friction and wear behavior of aluminum and composite

airplane skins

[NASA-TP-2262] p 37 N84-17175

Abrasion behavior of aluminum and composite skin

coupons, stiffened skins and stiffened panels

representative of transport airplane structures

INASA-TP-2520] p 38 N86-133t6

Strength of graphite/epoxy bolted wing-skin splice

specimens subjected to outdoor exposure under constant

load and yearly fatigue loading

INASA-TP-2542| p 83 N86-20508

SKIN FRICTION

Direct measurements and analysis of skin friction and

cooling downstream of multiple flush-slot injection into e

turbulent Mach 6 boundary layer

l NASA-TP-1176 J p 106 N78-33385

Wind-tunnel measurements and comparison w_th flight

of the boundary layer and heat transfer on a hollow cylinder

at Mach 3

INASA-TP-17891 p 16 N81-14975

Drag of two-dimensional small-amphtude symmetnc and

asymmetric wa W walls in turbulent boundary layers

[NASA-TP-2318J p 112 N84-25944

SKYLAB PROGRAM

Skylab, our first space station

I NASA-SP-400 t p 60 N77-27155

Skylab, classroom in space

I NASA-SP-401 _ p 65 N77-29189

Biomedical results from Skylab

[NASA-SP-377] p 169 N77-33780

Remote sensing of oceanic parameters during the

Skylablgamefish experiment

INASA-RP-t012] p 167 N78-12644

Skylab: A chronology

[ NASA-SP-4011 j p61 N78-25115

Skyiab EREP investigations summary

tNASA-SP-399J p 136 N79-t7279

A new sun: The solar results from Skylab

INASA-SP-402] p 209 N79-22991

Catalog of fer-uttravioiot objective-prism

spectrophotometry: Skyleb experiment S-019, ultraviolet

steiler astronomy

JNASA-RP-1031 ] p 210 N79-27057

Handbook on astronaut crew mot;on disturbances for

control system design --- in skylab

INASA-RP-1025] p 71 N79-27237

Skylab's astronomy and space sciences

[ NASA-SP-404] p 199 N79-3411B

The role of satellite altimetry in climate studies

{NASA-TP-1570] p 161 N80-16676

Living and working in space. A history of Skyiab

[NASA-SP-4208] p 63 N84-25737

SKYLAB 1

Skylab, our first space slat=on

{ NASA-SP-400 ] p60 N77-27155

SKYLAB 2

Skyteb, our first space station

INASA-SP-40O] p 60 N77-27155

SKYLAB 3

Skyiab, our first space station

i NASA-SP-400) p 60 N77-27155

SKYLAB 4

Skylab, our first space station

I NASA-SP-4001 p 60 N77-27155

Skyiab explores the Earth

I NASA-SP-380] p 140 N82-12492

SLENDER CONES

In-flight transition measurement on a 10 deg cone at

Math numbers from 0 5 to 20

INASA-TP-1971 _ p 19 N82-26227

SLENDER WINGS

Low-speed tests of a high-aspect-ratio,

supercritical-wing transporl model equipped with a h_gh-lift

flap system in the Langley 4- by 7-meter and Ames 12-foot

pressure tunnels

{ NASA-TP-20971 p26 N85-31010

SLIDING

Friction and wear of iron in corrosive metal

|NASA-TP-19851 p 88 N82-20291

Plastic deformation at surface during unlubnceted

sliding

[NASA-TP-2036] p 122 N83-11496

Regression analysis of traction characteristics of traction

fluids

[NASA-TP-2154] p 123 N83-24862

SLIDING FRICTION

Friction and wear behavior of single-crystal silicon

carbtde in contact with titanium

{NASA-TP-1035J p 91 N77-32312

Friction and deformation behavior of single-crystal

s_licon carbide

[NASA-TP-1053] p 91 N77-33350

Friction and wear of single-crystal and polycrystalline

maganese-zinc ferrde in contact with various metals

{ NASA-TP-1059J p 91 N78-10295

A-106

Friction and wear of selected metals and alloys in sliding

contact with AISt 440 C stainless steel in liquid methane

and in liquid natural gas

[NASA-TP.1150] p 119 N78-20512

Wear of single-crystal silicon carbide in contact with

various metals in vacuum

I NASA-TP-11981 p92 N78-21295

Role of alloying elements in adhesive transfer and friction

of copper-base alloys

[NASA-TP-1256] p 86 N78-26198

Effect of oxygen, methyl mercaptan, and methyl chloride

on friction behavior of copper-iron contacts

I NASA-TP-1309] p 86 N78-30206

Friction and wear of metals with a single-crystal abrasive

grit of silicon carbide: Effect of shear strength of metal

[ NASA-TP-t 293] p 92 N78-30238

Friction and transfer of copper, silver, and gold to iron

in the presence of vanous adsorbed surface films

[NASA-TP-t392] p 120 N79-14386

Fnction and wear characteristics of iron-chromium alloys

in contact with themselves and sihcoe carbide

(NASA-TP-13871 p 120 N79-14387

Friction and wear with a single-crystal abrasive grit of

silicon carbide in contact with iron base binary alloys in

oil: Effects of alloying element and its content

INASA-TP-1394] p 120 N79-17227

Effect of sterilization irradiation on friction and wear of

ultrahigh-molecular-weight polyethylene

INASA-TP-t462J p 92 N79-23216

Anisotropic fnction, deformation, and fracture of

single-crystal silicon carbide at rOom temperature

INASA-TP-1525J p 93 N79-30380

Lubricating and wear mechanisms for a hemisphere

sliding on polyimide-bonded graphite fluoride film

[NASA-TP-t524J p 93 N79-30381

Surface chemistry of iron sliding in air and nitrogen

lubricated with hexadecane and hexadecane containing

dibonzyl-dilsulfide

[NASA-TP-1545J p 79 N79-31346

Evaluation and auger analysis of a

zinc-dialkyt-dithiophosphate antiwear additive in several

dlester lubricants

I NASA-TP-1544J p 93 N79-32359

Friction and wear of iron-base binary alloys in sliding

contact with silicon carbide in vacuum

[NASA-TP-1612J p 93 N80-22494

Relationship between the ideal tensile strength and the

friction properties of metals in contact with nonmetals and

themselves

[ NASA-TP-1883 J p 94 N81-33293

Surface chemistry and wear behavior of single-crystal

silicon carbide sliding against iron at temperatures to 1500

C in vacuum

[NASA-TP-1947] p 94 N82-t9374

Fnction wear and auger analysis of iron implanted with

t.5-MeV nitrogen ions

I NASA-TP-1989t p 88 N82-21300

Surface chemistry, microstructure and friction properties

of some ferrous-bass metallic glasses at temperatures to

750 C

[NASA-TP-2OO6J p 88 N82-22349

Occurrence of spherical ceramic debris in indentation

and sliding contact

[NASA-TP-2048] p 95 N82-32491

Wear mechanism based on adhesion

[NASA-TP-20371 p t22 N82-32737

Effect of sliding speed and contact stress on tripological

properties of ultra-h_h-molecutar-weighf polyethylene

t NASA-TP-2059] p 95 N83-14269

Elastohydrodynamic lubrication of rectangular contacts

INASA-TP-2111J p 123 N63-16759

Sliding induced crystallization of metallic glass

I NASA-TP-2140] p88 N83-21110

X-ray photoelectron spectroscopy and fnction studies

of nickel-zinc and manganese-zinc ferrites in contact with

metals

INASA-TP-2163] p 88 N83-23419

Elastohydrodynamic contacts. Effects of dents and

grooves on traction and local film thickness

[NASA-TP-21751 p 123 N83-28453

Friction and hardness of gold films deposited by ion

plating end evaporation

[NASA-TP-2207] p 89 N83-34019

Friction end morphology of magnetic tapes in sliding

contact with nickel-zinc fernte

I NASA-TP-2267J p 95 N84-16334

Friction end wear of iron in sulfuric acid

[ NASA-TP-2289 ] p89 N84-21716

Friction and wear of nickel in sulfuric acid

INASA-TP-2290] p 89 N84-21721

Friction behavior of silicon in contact with titanium, nickel,

silver and copper

[NASA-TP-2362] p 96 N84-33590

SUBJECT INDEX

Effect of barrier height on friction behavior of the

semiconductors silicon and gallium arsenide in contact with

pure metals

[NASA-TP-2405] p 96 N85-13044

SLIP FLOW

Slip-boundary equations for multicomponent

noneduitibrium airflow

{NASA-TP-2452] p t13 N86-14530

SLIPSTREAMS

Vortex wake alleviation studies with a variable twist

wing

[NASA-TP-2442] p 5 N86-t6187

SLOPES

A study of the cornering forces generated by aircraft

tires on a tilted, free-swiveling nose gear

[NASA-TP-2481 I p 135 N86-11522

SLOTTED WIND TUNNELS

A theory for predicting boundary impedance and

resonance frequencies of slotted-wall wind tunnels,

including plenum effects

INASA-TP-18801 p 17 N81-2909,6

SLUDGE

Laboratory measurements of radiance and reflectance

spectre of a dilute biosolid industria_ waste product

[NASA-TP-1401 ] p 148 N79-17360

SMOG

A diagnostic model for studying daytime urban air quality

trends

INASA-TP-t843] p 149 N61-22587

SMOKE

Effect of primary-zone equivalence ratio on pollutant

formation

[ NASA-TP-1463 ] p 44 N79-23086

SNOW

The Snowmelt-Runoff Model (SRM) user's manual

[NASA-RP-tl001 p 141 N83-23660

Remote Sensing of Snow and Evapotranspiretion

INASA-CP-2363] p 143 N85-23223

SNOW COVER

Microwave emission from polar firn

INASA-TP-1212J p 151 N78-216gO

Estimation of snow temperature and mean crystal radius

from remote multispectral passive microwave

measurements

INASA-TP-1251 J p t51 N78-26677

Preliminary results of passive microwave snow

experiment during February and March 1978

[NASA-TP-1408J p 152 N79-19519

Operational Applications of Satellite Snowcover

Observations

[Ea0-t0167] p 139 N80-25742

Microwave remote sensing of snowpack properties

[NASA-CP-2153] p 139 N81-19511

Applications systems verification and transfer project.

Volume 1 : Operational applications of satellite snow cover

observations: Executive summary --- usefulness of satellite

snow-cover data for water yield prediction

[NASA-TP-1822] p 140 N82-20617

Applications systems verification and transfer prolect.

Volume 2: Operational applications of satellite snow-cover

observations and data-collection systems in the Arizona

test site

/NASA-TP-t823J p 140 N82-20618

Applications systems verification and transfer broject.

Volume 3: Operational applications of satellite snow cover

observations in California

INASA-TP-1824] p 140 N82-20619

Applications systems verification and transfer project.

Volume 4: Operational applications of satellite snow cover

observations. Colorado Field Test Center

INASA-TP-1825J p 140 N82-20620

Appticabons systems verification and transfer p.rolect.

Volume 5: Operational applications of satellite snow-cover

observations, northwest United States

INASA-TP-1826J p 140 N62-20621

Applications systems verification and transfer project.

Volume 6: Operational applications of satellite snow-cover

observations NOAA/NESS support study

[NASA-TP-1827J p 140 N82-20622

Applications systems verification end transfer brolect.

Volume 7: Cost/benefit analysis for the ASVT on

operational applications of satellite snow-cover

obse_ations

[NASA-TP-1828] p 141 N82-20623

Applications systems venficabon and transfer pro_ct,

Volume 8: Satellite snow mapping and runoff prediction

handbook

{NASA-TP-t829J p 141 N82-20624

SOARING

The science and technology of low speed and motortess

flight, part 1

[NASA-CP-2085-PT-1 ] p 2 N79-23889

SOCIOLOGY

The Impact of Science on Society

[NASA-SP-482] p 196 N85-24994
SUBJECT INDEX SOLAR SYSTEM

SOFTWARE ENGINEERING

Space Station Technology, 1983

[NASA-CP-2293} p 67 N84-18277

Technical Workshop: Advanced Helicopter Cockpit

Design

[NASA-CP-2351 j p 31 N85-14806

Space Station Software Issues

[NASA-CP.2361] p 179 N85-20689

Peer Review of a Formal Vedfication/Desi, gn Proof

Methodology

[NASA-CP.2377] p 179 N85-28609

Programmable, automated transistor test system

[NASA-TP-2554] p 103 N86-21755

Space Station Software Recommendations

lNASA-CP-2394] p 180 N86-23314

SOIL MAPPING

Characterization of soil and postlaunch pad debris from

Cape Canaveral launch complex and analysis of soil

interaction with aqueous HCI

[NASA-TP-2076] p 150 N83-12595

SOIL MECHANICS

Cheractedzation of soil and postlaunch pad debris from

Cape Canaveral launch complex and analysis of soil

interaction with aqueous HCI

[NASA-TP-2076J p 150 N83-12595

SOIL MOISTURE

Dielectric constants of soils at microwave

frequencies-2

[NASA-TP-1238} p 138 N78-23538

Soil Moisture Workshop

[NASA-CP-2073} p 138 N79-16329

Preliminary results of SAn soil moisture experiment,

November 1975

[NASA-TP-1404J p 152 N79-16473

SOIL SCIENCE

Dielectric constants of soils at microwave

frequencies-2

{NASA-TP-1238] p 138 N78-23538

SOILS

Laboratory measurements of upwelled radiance and

reflectance spectra of Calvert, Ball, Jordan, and Feldspar

soil sediments

{NASA-TP-f039] p 187 N78-12645

Crash tests of three identical low-wing single-engine

airplane

[NASA-TP-2190] p 30 N83-34921

SOLAR ACTIVITY

A new sun: The solar results from Skylab

{NASA-SP-402] p 209 N79-22991

The Sun as a star

[NASA-SP-450} p 203 N81-27008

The Pinhole/Occulter facility

[NASA-TP-2089] p 209 N83-13048

A comparative look at sunspot cycles

[NASA-TP-2325} p 209 N84-24520

SOLAR ACTIVITY EFFECTS

Sun, weather, and climate

[NASA-SP-428] p 209 N79-20961

Solar Irradiance Variations on Active Region Time

Scales

[NASA-CP.2310] p 209 N84-27635

SOLAR ARRAYS

Evaluation of materials for high performance solar

arrays

[NASA-TP-1220] p 92 N78-22233

A potential-energy scaling model to simulate the initial

stages of thin-film growth

{NASA-TP-2102] p 88 N83-18895

The 17th Aerospace Mechanisms Symposium

{NASA-CP-22731 p 131 N83-24881

Circuit transients due to negative bias arcs on a

high-voltage solar array in low Earth orbit

{NASA-TP-2407} p 75 N85-14858

Space Photovoltaic Research and Technology 1985:

High Efficiency, Space Environment, and Array

Technology

[NASA-CP-2408} p 146 N86-17839

SOLAR ATMOSPHERE

The Sun as a star

[NASA-SP-450} p 203 N81-27008

Solar Terrestrial Physics: Present and Future

INASA-RP-1120} p 200 N84-34332

Measurements of Solar Vector Magnetic Fields

INASA-CP-2374] p 210 N85-29889

SOLAR BACKSCATI'ER UV SPECTROMETER

User's guide for the Solar Backscattered Ultraviolet

(SBUV) and the Total Ozone Mapping Spectrometer

(TOMS) RUT-S and RUT-T data sets: October 31, 1978

to November t, 1980

[NASA-RP-1112] p 165 N83-28828

SOLAR BLANKETS

Space Photovoltaic Research and Technology 1983,

High Efficiency, Radiation Damage, and Blanket

Technology

{NASA-CP-2314] p 146 N84-29307

SOLAR CELLS

Solar Cell High Efficiency and Radiation Damage

{NASA-CP-2020] p 144 N78-13527

Ionized dopant concentrations st the heavily doped

surface of a silicon solar cell

[NASA-TP-1347] p 195 N79-13886

Solar Cell High Efficiency and Radiation Damage,

1979

{NASA-CP-2097] p 144 N79-32640

Annealing of radiation damage in 0,1- and

2-ohm-centimeter Silicon solar cells

{NASA-TP-1559] p 145 N79o33572

Space Photovottsic Research and Technology 1980.

High Efficiency, Radiation Damage and Blanket

Technology

INASA-CP-2169} p 145 N81-17531

Analysis of costs of gallium arsenide and silicon solar

arrays for space power applications

[NASA-TP-181 tl p 77 N81-20173

A simple model of space radiation damage in GaAs solar

cells

[NASA-TP-2242] p 192 N84-13978

Space Photovoltaic Research and Technology 1985:

High Efficiency, Space Environment, end Array

Technology

[NASA-CP-2408] p 146 N86-17839

SOLAR COLLECTORS

An analytical and experimental investigation of a 1.8

by 3,7 meter Fresnel lens solar concentrator

[NASA-TP-1005] p 144 N77-30617

SOLAR CONSTANT

Variations of the Solar Constant --- conference

INASA-CP-2191 ] p 209 N82-17014

SOLAR CORONA

The Pinhole/Occulter facility

[NASA-TP-2089] p 209 N83-13048

Solar Wind FNe

[NASA-CP-2280 ] p 209 N84-13067

Measurements of Solar Vector Magnetic Fields

[NASA-CP-23741 p 210 N85-29869

Solar Flares and Coronal Physics Using P/OF as s

Research Tool

{NASA-CP-2421} p 210 N86-24614

SOLAR CORPUSCULAR RADIATION

Ninteenth International Cosmic Ray Conference SH

sessions, volume 4

[NASA-CP-2376-VOL-4 J p 210 N85-34729

Nineteenth International Cosmic Ray Conference. SH

sessions, volume 5

{NASA-CP-2376-VOL-5} p 21t N85-34991

SOLAR CYCLES

Study of the Solar Cycle from Space

{NASA-CP-2098] p 209 N80-17944

SOLAR ECLIPSES

Orbit dynamics and geographical coverage capabilities

of satellite-based solar OCCUltation experiments for global

monitoring of stratospheric constituents

[NASA-TP-fB06J p 64 N80-19142

SOLAR ENERGY

intensity and absorbed-power distribution in a cylindrical

solar-pumped dye laser

INASA-TP-2321] p 118 N84-23878

Technology for Dayton-cycle powerptants using solar

and nuclear energy

INASA'TP'2558} p 78 N86-21577

SOLAR ENERGY ABSORBERS

Solar absorbtance and thermal emittance of some

common spacecraft thermal-control coatings

[NASA-RP-1121 ] p 82 N84-23698

SOLAR FLARES

Solar Terrestrial Physics: Present and Future

[NASA-RP-t 120] p 200 N84-34332

Ninteenth International Cosmic Ray Conference SH

sessions, volume 4

[NASA-CP-2378-VOL-41 p 210 N85-34729

Solar Flares and Coronal Physics Using P/OF as a

Research Tool

[NASA-CP-2421 I p 210 N86-24614

SOLAR FLUX

Users guide for the Solar Backscattored Ultraviolet

(SBUV) and the Total Ozone Mapl_ng Spectrometer

(TOMS) RUT-S and RUT-T data sets: October 31, 1978

to November 1, 1980

{NASA-RP-ltt2J p 165 N83-28828

SOLAR GENERATORS

TechnolOgy for large space systems: A bibliography with

indexes (supplement 14)

INASA-SP-7046(14)} p 63 N86-28104

SOLAR HOUSES

An evaluation of the NASA Tech House, including live-in

test results, volume 1

INASA-TP-1564] p 145 N80-t1559

SOLAR MAGNETIC FIELD

The Sun as a star

{NASA-SP-450} p 203 N81-27008

Solar Terrestrial Physics: Present and Future

[NASA-RP-1120} p 200 N84-34332

Measurements of Solar Vector Magnetic Fields

{NASA-CP-2374] p 210 N85-29869

SOLAR NEUTRINOS

Nineteenth International Cosmic Ray Conference. SH

sessions, volume 5

[NASA-CP-2376-VOL-5} p 211 N85-34991

SOLAR OBSERVATORIES

Solar Terrestrial Observatory Space Station Workshop

Report

{NASA-CP-2411 I p 76 N86-19349

SOLAR PHYSICS

Guntersville Workshop on Solar-Terrestrial Studies

{NASA-CP-20371 p 144 N78-19600

The Sun as a star

I NASA-SP-4501 p 203 N8t-27008

The Pinhole/Occulter Facility

INASA-TP-21681 p 209 N83-25646

Solar Terrestnat Observatory Space Station Workshop

Report

lNASA-CP-2411 } p 76 N86-19349

Solar Flares and Coronal Physics Using P/OF as a

Research Tool

[NASA-CP-2421 ) p 210 N86-24614

SOLAR POWER SATELLITES

Solar Power Satellite Microwave Transmission and

Reception

[NASA-CP-2141] p 145 N81-18533

Solar power satellite system sizing tradeoffs

{NASA-TP-1804] p 145 N81-18493

Satellite power system: Concept development and

evaluation program Volume 3: Power transmission and

reception. Technical summary and assessment

[NASA-RP-1076] p 145 N81-27622

Technology for large space systems: A bibliography with

indexes (supplement 14)

{NASA-SP-7046(14)] p 83 N86-28104

SOLAR POWERED AIRCRAFT

Some design considerations for solar-powered aircraft

[NASA-TP-1675] p 36 N82-32350

SOLAR PROPULSION

Some design considerations for solar-powered aircraft

{NASA-TP-16751 p 36 N82-32350

SOLAR RADIATION

Terrestrial photovoitaic measurements, 2

INASA-CP-2010) p t36 N77-30521

NASA Workshop on Solar-Terrestrial Studies from a

Manned Space Station

[NASA-CP-2024] p 136 N77-32549

Effect of lrichlorofluoromethane and molecular chlorine

on ozone formation by simulated solar radiation

I NASA-TP-1093 } p84 N78-12167

A simplified method for calculating the atmospheric

heating rate by absorption of solar radiation in the

stratosphere and mesosphere

[NASA-TP-1398J p 159 N79-16493

SOLAR REFLECTORS

Design and fabrication of a low-specific-weight parabolic

dish solar concentrator

[NASA-TP-11521 p 75 N78-17145

Illumination from space with orbiting solar-reflector

spacecraft

{NASA-TP-2065] p 74 N82-33421

SOLAR SIMULATION

Terrestrial photovoltaic measurements, 2

[NASA-CP-20t0} p 136 N77-30521

SOLAR SIMULATORS

Solar-simulator-pumped atomic iodine laser kinetics

INASA-TP-21821 p t18 N83-32044

Threshold kinetics of a solar simulator-pumped iodine

laser

INASA-TP-2241 I p 118 N84-17575

SOLAR SPECTRA

An atlas of solar spectra between 1175 and 1950

angstroms recorded on Skylab with the NRL's Apollo

telescope mount experiment

[NASA-RP-1069J p 209 N81-23004

SOLAR SYSTEM

Evolution of the solar system

{NASA-SP-345J p 203 N77-12959

The Soviet-American Conference on Cosmochemisfty

of the Moon and Planets, part 2

[NASA-SP-370-PT-2] p 203 N78-12958

Asteroids: An Exploration Assessment

{NASA-CP-20531 p 205 N78-29007

Space missions to comets

[ NASA-CP-2089 } p 206 N80-11972

An assessment of ground-based techniques for

detecting other planetary systems Volume 1: An overview

--- workshop conclusions

{NASA-CP-2124-VOL-1 I p 201 N80-18997

Advances in Ultraviolet Astronomy: Four Years of IUE

Research

INASA-CP-22381 p 201 N82-31163

A-107
SOLAR TERRESTRIAL INTERACTIONS SUBJECT INDEX

Airborne Astronomy Symposium. A symposium

commemorating the tenth ann_'ersary of operations of the

Kuiper Airborne Observatory

[NABA-CP-2353] p 202 N85o17848

Future of Ultraviolet Astronomy Based on Six Years of

IUE Research

[NASA-CP-23491 p 203 N85-20961

Planetary geology tn the 1980s

[NASA-SP-467] p 200 N85-23457

SOLAR TERRESTRIAL INTERACTIONS

Solar trrediance Variations on Active Region Time

Scales

[NASA-CP-2310J p 209 N84-27635

Solar Terrestrial Physics: Present and Future

[NASA-RP-11201 p 200 N84-34332

Solar Terrestrial Observatory Space Station Workshop

Report

[ NASA-CP-2411 ] p 76 N86-19349

SOLAR WIND

The Pinhole/Occulter facility

[NASA-TP-2089] p 209 N83-13048

Sotar Wind Five

[NASA-CP-2280J p 209 N84-t3067

Solar Terrestrial Physics: Present and Future

[NASA-RP-t 120} p 200 N84-34332

SOLAR X-RAYS

Solar Flares and Coronal Physics Using P/OF as a

Research Tool

[NASA-CP-2421 I p 210 N86-24614

SOLAR=PUMPED LASERS

A blackbody-pumped CO2-N2 transfer laser

[NASA-TP-23471 p 118 N84-31617

SOLDERING

Welding, Bonding and Fastening, 1984

[NASA-CP-2387] p 79 N86-11227

SOLID LUBRICANTS

Lubricating and wear mechanisms for a hemisphere

sliding on polyimide-bonded graphite fluonde film

INASA-TP-1524} p 93 N79-30381

Tribological properties at 25 C of seven polyimide films

bonded to 440 C high-temperature stainless steel

[NASA-TP-1944] p 94 N82-19373

Tdbology in the 80's Volume 2: Sessions 5 - 8

[NASA-CP-2300-VOL-2] p 124 N84-25047

SOLID MECHANICS

Research in nonlinear structural and sohd mechanics

INASA-CP-2147J p 129 N80-32756

Research in nonlinear structural and solid mechanics

INABA.CP-2147-SUPPL] p 130 N82-11469

Research in structural and solid mechanics, 1982

INASA-CP-2245] p 131 N82-33739

SOLID PROPELLANT ROCKET ENGINES

Essays on the History of Rocketry and Astronautics:

Proceedings of the Third through the Sixth History

Symposia of the International Academy of Astronautics,

volume 2

[NASA-CP-2014-VOL-2} p 212 N77-33048

Nitric oxide production in the stratosphere within the

Space Shuttle's solid rocket motor plumes

INASA-TP-1305] p 68 N78-33135

Proceedings of Shuttle Environmental Effects Program

Review --- conferences

[NASA-CP-2110] p 149 N80-15649

Identification and management of filament-wound case

stiffness parameters

INASA-TP-2117] p 81 N83-16400

Star 48 solid rocket motor nozzle analyses and

instrumented firings

[NASA-TP-2572J p 68 N86-20460

Pocketing mechanics of SRM nozzle liner

[NASA-TP-2577) p 135 N86-23974

SOLID ROCKET PROPELLANTS

Application of s Gaussian multilayer diffusion model to

characterize dispersion of vertical HCI column density in

rocket exhaust clouds

INASA-TP-19561 p 149 N82-14672

SOLID-SOLID INTERFACES

Effect of oxygen and nitrogen interactions on fnction

of single-crystal silicon carbide

INASA-TP-1265} p 92 N78-28247

Effect of oxygen, methyl mercaptan, and methyl chloride

on friction behavior of copper-iron contacts

I NASA-TP-1309J p 86 N78-30206

A potential-energy scaling model to simulate the initial

stages of thin-film growth

INASA-TP-2102] p 88 N83-18895

Galvanic coupling between D6AC steel, 6061-T6

aluminum, Inconel 718 and graphite-epoxy composite

material: Corrosion occurrence and prevention

iNASA-TP-22361 p 89 N84-13263

SOLIDIFICATION

Optical observations of unidirectional solidification m

microgravity

JNASA-TP-2110] p 88 N83-16492

Fundamentals of Alloy Solidification Applied to Industrial

Processes

[NASA-CP-2337} p 90 N84-34589

SOLIDS FLOW

Laboratory measurements of physical, chemical, and

optical characteristics of Lake Chicot sediment waters

[NASA-TP-t941J p 140 N82-13468

SOLUTIONS

A class of nonideal solutions 2: Application to

experimental data

[NASA-TP-1930] p 196 N83-23188

A class of nonideal solutions. 1: Definition and

properties

[NASA-TP-1929} p 196 N83-23189

SONIC BOOMS

A study of the sonic-boom characteristics of a blunt body

at a Mach number of 4.14

I NASA-TP-1015J p 1 N77-32072

Simplified sonic-boom prediction --- using aerodynamic

configuration charts and calculators or slide rules

[NASA-TP-1122] p 7 N78-20078

A wind-tunnel study of the applicability of far-field

sonic-boom theory to the space shuttle orbiter

[NASA-TP-1166] p 8 N78-25061

Sonic-boom minimization with nose-bluntness

relaxation

INASA-TP-1348] p 10 N79-15000

Near-field sonic-boom pressure signatures for the space

shuttle launch and orbiter vehicles at Mech 6

I NASA-TP-f 405 j p68 N79-21119

Wind-tunnel investigation of the validity of a

sonic-boom-minimization concept --- Langley Unitary Plan

Wind Tunnel tests for supersonic transport design

INASA-TP-1421 ] p 12 N80-10102

Sonic-boom wave-front shapes and curvatures

associated with maneuvering flight

INASA-TP-1611J p 13 N80-14045

A study of the sonic-boom characteristics of a btunt body

at a Mach number of 6

INASA-TP-1787} p 3 N81-13915

Charts for determining potential minimum sonic-boom

overpressures for supersonic cruise aircraft

INASA-TP-1820J p 17 N81-21016

An analysis of shock coalescence including

three.dimensional effects with application to sonic boom

extrapolation

[ NASA-TP-2214] p 111 N84-22906

Correlation of predicted and measured sonic boom

characteristics from the reentry of STS-t orbiter

[NASA-TP-2475] p 190 N85-29694

SOOT

Investigation of light scattering as a technique for

detecting discrete soot particles in a luminous flame

[NASA-TP-1235} p 193 N78-27906

Fuel-rich catsly'ec combustion: A soot-free technique

for in situ hydrogen-like enrichment

[NASA-TP-2498} p 85 N85-31244

SOUND GENERATORS

Theoretical prediction of nonlinear propagation effects

on noise signatures generated by subsonic or supersonic

propeller or rotor-blade tips

{NASA-TP-1660] p 14 N80-22265

Empirical source no0se prediction method with

application to subsonic coaxial jet mixing noise

{NASA-TP-2084] p 189 N83-16149

SOUND INTENSITY

Computer program to predict aircraft noise levels

{NASA-TP-t913] p 188 N81-33947

A new measurement method for separating airborne and

structurebome noise radiated by aircraft type panels

{NASA-TP-2079] p 189 N83-11838

SOUND PRESSURE

Experimental study of acoustic loads on an

upper-surface-blown STOL airplane configuration ---

Langley full-scale wind tunnel tests

[NASA-TP-t577J p 187 N80-13879

Numerical Techniques in Acoustics

[NASA-CP-2404] p 190 N86-12007

SOUND PROPAGATION

Finite-difference theory for sound propagation in a lined

duct with uniform flow using the wave envelope concept

{NASA-TP-tO01 I p 185 N77-30908

Prediction of ground effects on aircraft noise

(NASA-TP-11041 p 186 N78-17823

Computation of atmospheric attenuation of sound for

fractional-octave bands

[NASA-TP-14121 p 186 N79-17659

Stochastic analysis of spectral broadening by a free

turbulent shear layer

{NASA-TP-1816J p 188 N81-24854

A study of resonant-cavity and fiberglass-filled parallel

baffles as duct silencers --- for wind tunnels

{NASA-TP-1970} p 188 N82-24052

SOUND TRANSMISSION

Noise transmission loss of aircraft panels using acoust:c

intensity methods

[NASA-TP*2046} p 188 N82-31069

Low-frequency sound absorption measurements in air

[NASA-RP-1128] p 190 N85-11789

SOUND WAVES

Fluctuating sudace pressure and acoustic radiation for

subsonic normat jet impingement

{NASA-TP-1361 I p t86 N79-19813

Consideration of some factors affecting tow-frequency

fuselage noise transmission for propeller aircraft

{NASA-TP-2552} p 191 N86-24393

SOUNDING

Determination of wind from NIMBUS 6 satellite sounding

data

{NASA-RP-10721 p 162 N81-15639

A comparative analysis of rawinsoode and NIMBUS 6

and TIROS N satellite Wofiie data

{NASA-RP-t070J p 162 N81-15640

SOUNDING ROCKETS

Synoptic analyses, 5-, 2-, and 0.4-rnillibar surfaces for

July 1974 through June 1976

[NASA-RP-1023J p 158 N78-28748

Synoptic analyses, 5-, 2°, 1-, and 0A-millioer surfaces

for July 1976 through June 1977

[NASA-RP-t032J p 159 N79-19569

SOUTHERN HEMISPHERE

A new NASA/MSFC missmn analysis global cloud cover

data base

[NASA-TP-2448J p 166 N85-21876

SPACE BASES

Performance requirements analysis for payload delivery

from a space station

{NASA-RP-11101 p 67 N83-32828

SPACE COLONIES

Space settlements: A design study

[NASA-SP-4131 p60 N77-21106

Space resources and space settlements

{NASA-SP-4281 p 62 N79-32225

SPACE COMMERCIALIZATION

Second Symposium on Space Industrialization --- space

commercialization

[ NASA-CP-23131 p63 N85-11011

SPACE COMMUNICATION

Radio-wave propagation for space communications

systems

{NASA-TP-1770J p 70 N81-t8082

Beam impingement angle effects on secondary electron

emission characteristics of textured pyrolytic graphite

[NASA-TP-22851 p 95 N84-18400

SPACE DEBRIS

Orbital Debris

[ NASA-CP-2360 } p63 N85-21188

Procedure for estimating orbital debris risks

{NASA-TP-25071 p 69 N85-33169

SPACE ENVIRONMENT SIMULATION

Ninth Conference on Space Simulation

[NASA-CP-2007] p 61 N79-1go13

EVA assembly of large space structure element

JNASA-TP-1872] p 62 N81.26160

Spacecraft Charging Technology, 1980

(NASA-CP-2182] p 72 N82-14213

Twelfth Space Simutabon Conference: Shuttle Plus One.

A New View of Space

[NASA-CP-2229] p 73 N82-25291

SPACE ERECTABLE STRUCTURES

Large Space Systems Technology, volume 1

[NASA-CP-2035-VOL-t ] p 65 N79-10078

The 1980 Large space systems technology. Volume

2: Base technology

INASA-CP-2168-VOL-2] p 66 N81-19196

The 15tb Aerospace Mechanisms Symposium

[NASA-CP-2181 I p 130 N81-22388

EVA assembly of large space structure element

{NASA-TP-1872] p 62 N81-26160

Space station systems: A bibliography with indexes

(supplement 2)

[NASA-SP-7056(02)] p 63 N86-28105

SPACE EXPLORATION

A geological basis for the exploration of the planets

{NABA.SP-417] p 204 N77.15961

Second International Colloquium on Mars: Abstracts

for a colloquium --- bibliography

{NASA-CP-2072] p 205 N79-16757

Images of Mars: The Viking extended mission

[NASA-SP-444] p 206 N80-26239

The space shuttle at work

(NASA-SP-432] p 68 N80-30367

Voyage to Jupiter

[NASA-SP-439] p 206 N81-10910

Pioneer: First to Jupiter, Saturn, and beyond

[ NABA-SP-446 ] p206 N81-15925

Beyond the atmosphere: Early years of space

science

[NASA-BP-4211 J p 200 N81-20962

A-108
SUBJECT INDEX SPACE SHUTTLE ORBITERS

Orders of magnitude: A history o1 NACA and NASA,

1915 - 1980

[NASA-SP-4403] p 196 N82-14956

Advanced Automation for Space Missions

{NASA-CP-2255] p 76 N83-15348

The 1st Symposium on Chemical Evolution and the

Origin end Evolution o1 Life

[NASA.CP-2276] p 79 N83-24556

Planetary Data Workshop, part 1

[NASA-CP-2343-PT-1] p 208 N84.34366

On Mars: Exploration of the red planet, 1958 - 1978

[NASA.SP-4212] p 208 N84-35248

Planetary cartography in the next decade (1984 -

1994)

[NASA-SP.475] p 208 N85-22323

Planetary geology in the 1980s

[NASA-SP-467] p 200 N85-23457

Far travelers: The exploring machines

[NASA-SP-480] p 63 N85-33126

A spacefering people: Perspectives on early

spaceflight

[ NASA-SP-4405] p2t2 N85-35142

Space Station Planetology Experiments (SSPEX)

[NASA-CP-2424} p 201 N86-27136

Astronautics and aeronautics, 1977: A chronology

[NASA-SP-4022] p 213 N86-31524

SPACE FLIGHT

NASA Space Biology Program: 91h Annual

Symposium

[NASA-CP-2336] p 169 N85-26054

SPACE FLIGHT FEEDING

Controlled Ecological Life Support System: Use of

Higher Plants

[ NASA-CP-2231 ] p 173 N82.24834

Controlled Ecological Life Support System: Research

and Development Guidelines

[NASA-CP-2232] p 173 N82.24835

Food Service and Nutrition for the Space Station

[NASA.CP.2370] p 174 N85-24733

SPACE FLIGHT STRESS

Biomedical results from Skylab

[NASA-SP-377] p 169 N77-33780

The use of nonhuman primates in space

[NASA-CP-005] p 169 N78-11663

SPACE GLOSSARIES

Space Transportation System and associated payloads:

Glossary, acronyms, and abbreviations

[ NASA-RP-1059 ] p68 N81-16111

Space Transportation System and associated payloads:

Glossary, acronyms, and abbreviations

[NASA-RP-1059-REV] p 69 N65-19007

SPACE INDUSTRIALIZATION

Space resources and space settlements

[NASA-SP-426] p 62 N79-32225

Second Symposium on Space Industrialization --- space

commercialization

[ NASA-CP-2313] p63 N85-11011

SPACE LABORATORIES

Orbiting quarantine facility. The Antaeus report

[NASA-SP-454] p 66 N82-20225

SPACE MANUFACTURING

AIAA/MSFC Symposium on Space Industrialization:

Proceedings

[NASA-CP-2026] p 60 N78-18088

Space resources and space settlements

{NASA-SP-428] p 62 N79-32225

Materials processing in space: Early experiments

[NASA-SP-443} p 62 N6t-16075

Advanced Automation for Space Missions

[NASA-CP-2255] p 76 N83-15348

Analytical and numerical studies o1 the thermocapillary

flow in a uniformly floating zone

[NASA-TP-2576] p 113 N86-23851

The 1985 Get Away Special Experimenter's

Symposium

{NASA-CP-2401] p 63 N86-27297

SPACE MISSIONS

Asteroids: An Exploration Assessment

[NASA-CP-20531 p 205 N78-29007

The partnership: A history of the Apollo-Soyuz test

project

[NASA-SP-4209} p 61 N79-10074

OGO program summary, supplement 1 --- updated

bibliography for all OGO missions and scientific results

from OGO 5 and 6 missions

[NASA-SP-7601-SUPPL-1 } p 151 N79-13601

A critical review of the life sciences project management

at Ames Research Center for the Spacetab Mission

development test 3

[NASA-TP-1364] p 196 N79.16709

Skylab's astronomy and space sciences

[NASA-SP-404] p 199 N79-34118

Space missions to comets

[NASA-CP-2089J p 206 N80-11972

The Apollo spacecraft: A chronology volume 4, 21

January t986 - 13 July 1974

[NASA.SP-400g-VOL-4] p 98 N80.20437

Advanced Automation for Space Missions

[NASA-CP-2255] p 76 N83.15348

Living and working in space A history of Skylab

[NASA-SP-4208] p 83 N84.25737

Astronautics and aeronautics, 1977: A chronology

[NASA-SP-4022] p 213 N86-31524

SPACE NAVIGATION

Flight Mechanics/Estimation Theory Symposium --- with

application to autonomous navigation and attitude/orbit

determination

[NASA-CP-2082] p 64 N79-26062

Existence and uniqueness of solutions to a class of

nonlinear -operator-diffe rential equations arising in

automated spaceship navigation

[NASA-TP-1860] p 70 N81-23182

SPACE OBSERVATIONS (FROM EARTH)

Planetary Data Workshop, part 1

[NASA.CP-2343-PT-1} p 208 N84-34366

SPACE PLASMAS

Space plasma physics active experiments

[NASA-CP-2165] p 212 N81-14944

Radiating dipole model o1 interference induced in

spacecraft circuitry by surface discharges

[NASA-TP-2240] p 74 N84-16247

Second Workshop on Spacecraff Glow

[NASA-CP-2391} p 201 N86-13239

SPACE PLATFORMS

Large space systems technology, 1960, volume t

[NASA-CP-2168] p 66 N81-19t64

Large space systems technology, 1981 --

conferences

[NASA-CP-2215-PT-1} p 66 N82-18275

Space Laser Power Transmis_on System Studies ---

conferences

[NASA-CP-22141 p 117 N82-18578

Space Photovoltaic Research and Technology 1982:

High Efficiency, Radiation Damage, and Blanket

Technology

[NASA-CP-22551 p 146 N83-15806

Solar Terrestrial Observatory Space Station Workshop

Report

[NASA-CP-2411 } p 76 N86-19349

Space station systems: A bibliography with indexes

(supplement 2)

[NASA-SP-7056(02)] p 63 N86-28105

SPACE POWER UNIT REACTORS

Comparative analyses o1 space-to-space central power

stations

[NASA-TP-19551 p 66 N82-14202

SPACE PROCESSING

Apollo-Soyuz test project. Volume 1: Astronomy, earth

atmosphere and gravity field, life sciences, and materials

processing

[NASA-SP-412} p 60 N78-17088

AtAA/MSFC Symposium on Space Industrialization:

Proceedings

[NASA-CP-2026] p 60 N78-18088

Materials processing in space: Early experiments

[NASA-SP-443I p 62 N81-16075

Float Zone Workshop

{NASA-CP-2179] p 62 N81-19144

Avenues and incentives for commercial use of a

low-gravity environment

[NASA-TP-19251 p 94 N81-33292

Float Zone Workshop

[NASA-CP-22261 p 62 N82-26330

Approximate analysis of thermal convection in a

crystal-growth cell for Spacelab 3

[NASA-TP-2016] p 62 N82-29335

Second Symposium on Space industrialization --- space

commercialization

[NASA-CP-2313J p 63 N85-11011

Applications of Tethers in Space: Workshop

proceedings, volume 2

[NASA-CP'2422-VOL-2t p 126 N86-27644

SPACE PROGRAMS

Beyond the atmosphere: Early years of space

science

[NASA-SP-4211 } p 200 N61-20962

A spacefaring people: Perspectives on early

spaceflight

[NASA-SP-4405} p 212 N85-35142

SPACE SHUTTLE BOOSTERS

Characterization of large 2219 aluminum alloy hand

forgings for the space shuttle solid rocket booster

[NASA-TP-1383} p 87 N79-t6950

Aerodynamic tests and analysis of a turbojet-boosted

launch vehicle concept (spacejat) over a Mach number

range of 1.50 to 2.86 --- Langley Unitary Plan Wind Tunnel

Tests

[NASA-TP-1888] p 17 N81-29098

Feasibility study of LITVC for shuttle SRB

[NASA-TP-1912] p 77 N81-33231

Vibration. acoustic, end shock design and test criteria

for components on the Solid Rocket Boosters (SRB),

Lightweight External Tank (LWT), and Space Shuffle Main

Engines (SSME)

[NASA.RP-1127] p 134 N65-10405

SPACE SHUTTLE MAIN ENGINE

Space shuffle main engine controller

[NASA-TP-19321 p 176 N62-11764

Vibration, acoustic, and shock design and test cdteria

for components on the Solid Rocket Boosters (SRB),

Lightweight External Tank (LWT), and Space Shuttle Main

Engines (SSME)

[NASA-RP-1127] p 134 N85-10405

Advanced High Pressure O2tH2 Technology

[NASA-CP-2372] p 78 N85-26862

Structural Integrity and Durability of Reusable Space

Propulsion Systems

[NASA.CP-2381] p 78 N85-27941

SPACE SHUTTLE ORBITERS

Entry dynamics o1 space shuttle orbiter with longitudinal

stability and control uncertainties at supersonic and

hypersonic speeds

[NASA-TP.1084] p 70 N77-33259

Entry dynamics of space shuttle orbiter with

lateral-directional stability and controt uncertainties at

supersonic and hypersonic speeds

[NASA-TP-1011 } p 70 N78-13t19

Static and dynamic stability analysis of the space shuttle

vehicle-orbiter

[NASA-TP-1179] p 68 N78-20176

A wad-tunnel study of the app_icabildy of far-field

sonic-boom theory to the space shuttle orbiter

[NASA-TP-1186} p 8 N78-25061

Microstructure and mechanical properties of quenched

and tempered 300M sleel

[NASA-TP-1288} p 127 N78-30610

Aerothermal tests o1 a heat-pipe-cooled leading edge

at Mach 7 -- hypersonic heat transfer for space shuttle

orbiters

{NASA-TP-1320] p 195 N79-13901

Near-field sonic-boom pressure signatures for the space

shuttle launch and orbiter vehicles at Math 6

[NASA-TP-t 405 ] p68 N79-21119

Orbiter landing loads math model description and

correlation with ALT flight data

[NASA-RP-1056} p 71 N60-16091

Comparison of predicted and experimental real-gas

pressure distributions on space shuttle orbiter nose for

shuttle entry air data system

[NASA-TP-1627} p 14 N80-21280

Simulator study of the effect of control-system time

delays on the occurrence of pilot-induced oscillations and

on pilot tracking performance with a space-shuttle-orbiter

configuration

[NASA-TP-1588} p 34 N80-21317

Dynamics stability derivatives of space shuttle orbiter

obtained from wind-tunnel and approach and landing flight

tests

[NASA-TP-1634] p 55 N80-21336

Analysis of space shuttle orbiter entry dynamics from

Math 10 to Mach 2.5 with the November 1976 flight control

system

[NASA-TP-1667] p 71 N80-29417

Use of nose cap and fuselage pressure orifices for

determination of air data for space shuttle orbiter below

supersonic speeds

[NASA-TP-1643] p 39 N80-32389

Development of the reentry flight dynamics simulator

for evaluation of space shuttle orbiter entry systems

{NASA-TP-1700] p 71 N80-32429

Aerothermal analysis of a wing-elevon cove with variable

leakage

[NASA-TP-1703J p 108 N80-32692

Comparison of Space Shuttle Orbiter low-speed static

stability and control derivatives obtained from wind-tunnel

and approach and landing flight tests

{NASA-TP-1779} p 56 N81-13066

The 111h Space Simulation Conference

[NASA-CP-21501 p 99 N81-14138

Cornering characteristics of the nose-gear tire of the

space shuttle orbiter

[NASA-TP-1917} p 130 N82-10430

Force and moment, flow-visualization, and

boundary-layer tests on a shuttle orbiter model at Mach

6

{NASA-TP-1952] p 18 N82-13106

The 161h Aerospace Mechanisms Symposium

[NASA-CP-2221 I p 99 N82-23344

Computational Aspects of Heat Transfer in Structures

{NASA-CP-2216] p 109 N82-23473

Wind-Tunnel/Flight Correlation, 1981

[NASA-CP-2225] p 19 N82-25196

Analysis of gap heating due to stepped tiles in the shuttle

thermal protection system

{NASA-TP-2209 ] p 74 N83-31713

A-109
SPACE SHUTTLE PAYLOADS

Effect of strain isolator pad modulus on inpiane strain

in Shuttle Orbiter thermal protection system tiles

[NASA-TP-21411 p 132 N83-33216

Effect of aerodynamic and angle-of-attack uncertainties

on the May 1979 entry flight control system of the Space

Shuftle from Mach 8 to t 5

J NASA-TP-2365J p 69 N85-15778

Space Shuttle Technical Conference, part 1

JNASA-CP-2342-PT-t ] p 63 N85-16889

Space Shuttle orbiter trimmed center-of-gravity

extension study

[NASA-TP-2284] p 67 N85-19003

SPACE SHUTTLE PAYLOADS

Release mechanism for re_easing and reattaching

experiments on the Space Shuttle

[NASA-TP-1702J p 121 N80-27694

Environmental analysis of the chemical release module

--- space shuttle payload

lNASA-TP-1750] p 209 N81-13912

Twelfth Space Simulation Conference: Shuttle Plus One.

A New View of Space

[NASA-CP-2229] p 73 N82-25291

The Pinhole/Ooculter Facility

{NASA-TP-2168J p 209 N83-25646

Fundamentals of Alloy Solidification Applied to Industrial

Processes

INASA'CP'2337J p 90 N84-34589

Large Space Antenna Systems Technology, 1964

[NASA-CP-2368-PT-2] p 68 N85-23840

The 1985 Get Away Special Expenmenter's

Symposium

[NASA-CP-2401 ] p 63 N86-27297

Applications of Tethers in Space: Workshop

proceedings, volume 2

[NASA-CP-2422-VOL-2] p 126 N86-27644

SPACE SHUTTLES

Research in the use of electrets in measuring effluents

from rocket exhaust of the space shuttle (6.4 percent

scaled model) and Viking 1 launch

[NASA-TP-1073J p 147 N78-11517

Effects of entrained water and strong turbulence on

afterburning within solid rocket motor plumes

[NASA-TP-1111J p 147 N78-15596

N_tnc oxide production in the stratosphere within the

Space Shuttle's solid rocket motor plumes

{ NASA-TP-13051 p68 N78-33135

Space shuttle ective-pogo-suppreseor control design

using linear quadratic regulator techniques

INASA-TP-1217] p 101 N79-14309

Space shuttle afterbody aerodynamics/plume simulation

data summary

INASA-TP-1384J p 11 N79-17810

Government/Industry Workshop on Payload Loads

Technology

[NASA-CP-2075] p 62 N79-20162

Proceedings of the NASA/Florida Institute of

Technology Environmental Engineenng Conference on

Nitrogen Tetroxide --- with emphasis on space shuttle

[NASA-CP-20491 p 136 N79-20424

Exploratory investigation of two resin-matrix composites

subjected to arc-tunnel heating

[NASA-TP-1429) p 80 N79-23141

Shuttle atmospheric lidar research program

[NASA-SP-433J p 117 N80-11414

Proceedings of Shuttle Environmental Effects Program

Review --- conferences

[NASA-CP-2110J p 149 N80-15649

The space shuttle st work

[NASA-SP-432J p 68 N80-30367

Preliminary vibration, acoustic, and shock design and

test criteria for components on the Lightweight External

Tank (LWT)

INASA-RP-10741 p 71 N81-19218

Thermal and aerothermsi performance of a titanium

mutt/wall thermal protection system

[NASA-TP-1961 ] p 72 N82-14277

Sensitivity analysis of the space shuttle to ascent wind

profiles

[NASA-TP-1988] p 69 N82-20236

Twelfth Space Simulation Conference: Shuttle Plus One

A New View of Space

INASA-CP-2229I p 73 N82-25291

Atmospheric constraint statistics for the Space Shuttle

mission planning

[NASA-TP-2069] p 69 N82-33417

identification and management of t/lament-wound case

stiffness parameters

INASA-TP-2117J p 81 N83-16400

Performance of an abletor for Space Shuttle inorbit repair

in an arc-plasma eirstrsem

[NASA-TP-2150] p 74 N83-22317

Calculation of inviscid flow over shuttle-like vehicles at

h_gh angles of attack and comparisons with experimental

data

[ NASA-TP-2103 ] p 119 N83-24808

A-110

Shuttle Performance: Lessons Learned, part 1

[NASA-CP-2283-PT-t ] p 69 N84-101t5

Shuttle Performance: Lessons Learned, part 2

I NASA-CP-2283-PT-2] p 69 N84-10144

Space shuttte exhaust cloud properties

[NASA-TP-2258] p t54 N84-14606

Airborne measurements of launch vehicle effluent of

STS-2 launch on November t2, 1981 at Cape Canaveral,

Florida

[NASA-TP-2260} p 150 N84-18764

Steady internal flow and aerodynamic loads analysis of

shuttle thermal protection system

[NASA-TP-2255] p 74 N84-19393

Get away special experimenter's symposium

I NASA-CP-2324] p 63 N84-27758

Development of in situ stiffness properties for shuttle

booster filament wound case

{NASA-TP-23771 p 93 N84-33521

Vibration, acoustic, and shock design and test criteria

for components on the Solid Rocket Boosters (SRB),

Lightweight External Tank (LWT), and Space Shuttle Main

Engines (SSME)

JNASA-RP-1127] p 134 N85-10405

Reduction method for thermal analysis of complex

aerospace structures

[NASA-TP-2373] p 112 N85-16066

Space Shuttle Technical Conference, pad 1

[NASA-CP-2342-PT-1] p 63 N85-16889

Space Shuttle Technical Conference, pad 2

[NASA-CP-2342-PT-2] p 63 N85-t6937

Spacecraft Environmental interactions Technology,

1983

[NASA-CP-23591 p 75 N85-22470

Investigation of solid plume simulation criteria to produce

flight plume effects on muir/body configuration in wind

tunnel tests

[NASA-TP-2569] p 28 N86-21507

The 1985 Get Away Special Experimenter's

Symposium

[NASA-CP-2401 ] p 63 N86-27297

SPACE SIMULATORS

Ninth Conference on Space Simulation

[NASA-CP-2007] p 61 N79-19013

The 11th Space Simulabon Conference

JNASA-CP-2150] p 99 N81-14138

Twelfth Space Simulation Conference: Shuttle Plus One.

A New View of Space

[NASA-CP-2229] p 73 N82-25291

Thirteenth Space Simulation Conference The Payload:

Testing for Success

[NASA-CP-2340] p 74 N84-34468

SPACE STATIONS

AIAA/MSFC Symposium on Space Industrialization:

Proceedings

[NASA-CP-2026] p 60 N78-18088

A new sun: The solar results from Skylab

[NASA-SP-402J p 209 N79-22991

Integrated Flywheel Technology, 1983

[NASA-CP-2290] p 77 N84-12228

STEP Experiment Requirements

[ NASA-CP-22941 p 67 N84-17211

Space Station Technology, 1983

I NASA-CP-2293 ] p 67 N84-18277

Second Symposium on Space Industrialization --- space

commercialization

(NASA-CP-2313] p63 N85-11011

Space Power

INASA-CP-2352] p 78 N85-13880

Applications of Tethers in Space, volume 1

I NASA-CP-2364] p 125 N85-20339

Large Space Antenna Systems Technology, 1984

[NASA-CP-2368-PT-2] p 68 N85-23840

The 1984 Goddard Space Flight Center Battery

Workshop

[NASA-CP-23821 p 103 N85-31371

Space station rotational equations of motion

{ NASA-TP-2511 ] p 68 N85-34148

Solar Terrestrial Observatory Space Station Workshop

Report

[NASA-CP-2411 ] p 76 N86-19349

Space Station Software Recommendations

INASA-CP-2394] p 180 N86-23314

Space Station Workstation Technology Workshop

Report

[NASA-CP-2414] p 70 N86-23620

Proceedings of a Workshop on Applications of Tethers

in Space: Executive Summery

INASA-CP-2422J p t26 N86-25794

Applications of Tethers in Space: Workshop

proceedings, volume 2

[NASA-CP-2422-VOL-2J p 126 N86-27644

Hybrid routing technique for a fault-tolerant, integrated

information network

[NASA-TP-2605] p 180 N86-27947

SUBJECT INDEX

space station systems: A bibliography with indexes

(supplement 2)

[NASA-SP-7056(02)] g 63 N86-28105

SPACE TECHNOLOGY EXPERIMENTS

Space station systems: A bibliography with indexes

(supplement 2)

INASA-SP-7056(02)] p 63 N86-28105

SPACE TRANSPORTATION

AIAA/MSFC Symposium on Space Industrialization:

Proceedings

[NASA-CP-2026] p 60 N78-18088

Applications of Tethers in Space, volume t

[NASA-CP-2364] p 125 N85-20339

Rail accelerators for space transportation: An

experimental investigation

INASA-TP-2571 j p 78 N86-28123

SPACE TRANSPORTATION SYSTEM

Disposal of radioactive _cline in space

[NASA-TP-1313] p 172 N78-31740

Graphite/Polyimide Composites --- conference on

Composites for Advanced Space Transportation

Systems

INASA-CP-2079] p 80 N79-30297

Comparison of predicted and experimental real-gas

pressure distributions on space shuttle orbiter nose for

shuttle entry air data system

[NASA-TP-1627] p 14 N80-21280

Simulator study of the effect of control-system time

delays on the occurrence of pilot.induced oscillations and

on pilot tracking performance with a space-shuttle-orbiter

configuration

INASA-TP-1588] p 34 N80-21317

Proceedings of the 141h Aerospace Mechanisms

Symposium

[ NASA-CP-2127] p 99 N80-23495

The space shuttle at work

INASA-SP_.32] p 68 N80-30367

Large Space Systems/Low-Thrust Propulsion

Technology

I NASA-CP-2144] p 77 N80-31449

Space Transportation System and assoc=ated payloads:

Glossary, acronyms, and abbreviations

[ NASA-RP-1059] p 68 N81-16111

Aerodynamic tests and analysis of a turbojet-boosted

launch vehicle concept (spacejet) over a Msch number

range of 1.50 to 2.86 --o Langley Unitary Plan Wind Tunnel

Tests

INASA-TP-1888] p 17 N81-29098

The 16th Aerospace Mechanisms Symposium

[NASA-CP-2221 ] p 99 N82-23344

Space Transportation System and associated payloads:

Glossary, acronyms, and abbreviations

{NASA-RP-1059-REVJ p 69 N65-19007

Applications of Tethers in Space, volume 2

[NASA-CP-2365] p 125 N85-20361

SPACE TRANSPORTATION SYSTEM 1 FUGHT

Airborne measurements of launch vehicle effluent:

Launch of Space Shuttle (STS-1) on 12 April 1981

[NASA-TP-2090] p 150 N83-16952

SPACE-TIME FUNCTIONS

The time-space relationship of the data point (Pixets)

of the thematic mapper and multispectral scanner or the

myth of simultaneity

[NASA-TP-1715] p 76 N80-28424

SPACEBORNE ASTRONOMY

HEAO Sotence Symposium

[NASA-CP-2113] p 200 N80-14977

Study of the Solar Cycle from Space

[ NASA-CP-2098 ] p209 N80.17944

Scientific research with the space Telescope:

international Astronomical Union Colloquium no. 54 ---

conferences

[NASA-CP-2111 ] p 200 N80-22130

The UnNerse at Ultraviolet Wavelengths: The first two

years of International Ultraviolet Explorer

INASA-CP-2171] p 203 N81-25893

The Space Telescope Observatory. Special session of

Commission 44, IAU 18th General Assembly

INASA-CP-2244J p 202 N82-33296

The star splitters: The high energy astronomy

observatories

fNASA-SP-466] p 202 N84-22516

Proceedings of the Large Deployable Reflector Science

and Technology Workshop. Volume 1: Executive

Summary

[NASA-CP-2275-VOL-1] p 202 N84-28709

Algorithm for astronomical extended source,

signal-to-noise radio calculations

I NASA-TP-2396] p202 N85-12633

Algorithm for astronomical, point source, signal to noise

ratio calculations

iNASA-TP-2397] p 202 N85-12634
SUBJECT INDEX SPACECRAFT DOCKING

SPACEBORNE EXPERIMENTS

OGO program summary, supplement 1 --- updated

bibliography for all OGO missions and scientific results

from OGO 5 and 6 missions

[NASA-SP-7601-SUPPL-t] p 151 N79-13601

Catalog of far-ultraviolet objective-pnsm

spectrophotometry: Skytab experiment S-019, ultraviolet

staffer astronomy

(NASA-RP-t031] p 210 N79-27057

Skylab's astronomy and space sciences

[NASA-SP-404J p 199 N79-34118

Space plasma physics active experiments

[NASA-CP-2165] p 212 N81-14944

Spacecraft Dynamics as Related to Laboratory

Expenments in Space --- conference

[NASA-CP-2199} p 72 N82-12109

ATS-6 engineering pedormance report. Volume 6:

Scientific experiments

[NASA-RP-1080-VOL-6] p 73 N82-t6152

User's guide for the Solar Beckscettared Ultraviolet

(SBUV) and the Total Ozone Mapping Spectrometer

(TOMS) RUT-S and RUT-T data sets: October 31, 1978

to November 1, 1980

[NASA-RP-1112] p 165 N83-28828

STEP Experiment Requirements

[NASA-CP-2294] p 67 N84-17211

Finite-difference fluid dynamics computer mathematical

models for the design and interpretation of experiments

for space flight --- atmospheric general circulation

experiment, convection in a float zone, and the

Bridgman-Stockbarger crystal growing system

[NASA-TP-2323] p 112 N84-23852

Long Duration Exposure Facility (LDEF) Mission 1

Experiments

[NASA-SP.473] p 67 N84-24632

The 181h Aerospace Mechanisms Symposium

[NASA-CP.2311] p 133 N84.25078

Living and working in space A history of Skylab

(NASA-SP-4208] p 63 N84-25737

Get away special experimenter's symposium

[NASA-CP-2324] p 63 N84-27758

Planetary Data Workshop, part 1

[NASA-CP-2343-PT-1 ] p 208 N84-34366

SPACEBORNE PHOTOGRAPHY

Viking Lander imaging investigation: Picture catalog of

primary mission experiment data record

(NASA-RP-1007] p 205 N78-20042

Apollo over the moon: A view from orbit

[NASA°SP-362] p 61 N78-21174

The voyage of Mariner 10: Missions to Venus and

Mercury

[NASA.SP-424] p 61 N78-27146

The Martian landscape --- Viking Mars mission and

photographs

[NASA-SP-425] p 205 N79-12984

A new sun: The solar results from Skylab

[NASA-SP-402] p 209 N79-22991

Atlas of Mars: The 1:5000000 map series

[NASA-SP-438] p 206 N80-16998

Viking orbiter views of Mars

[NASA-SP-441] p 200 N81-t1966

Viking lander imaging investigation during extended and

continuation automatic missions Volume 1: Lander 1

p*cture catalog of experiment data record

[NASA-RP-1068] p 206 N81-25012

Viking lander imaging investKjation during extended and

continuation automatic missions. Volume 2: Lander 2

p_cture catalog of experiment data record

[NASA-RP-1068-VOL-2] p 207 N82-16028

Phobos: Close encounter imaging from the Viking

Orbiters

[NASA-RP-1109] p 207 N84-32330

SPACEBORNE TELESCOPES

A stochastic model for photon noise induced by charged

particles in multiplier phototubes of the space telescope

fine guidance sensors

[NASA-TP-2337] p 193 N84-26398

Proceedings of the Large Deployable Reflector Science

and Technology Workshop Volume 1: Executive

Summary

[NASA-CP-2275-VOL-t ] p 202 N84-28709

Large Deployable Reflector Science and Technology

Workshop Volume 3: Systems and Technology

Assessment

[NASA-CP-2275-VOL-3} p 202 N84-32318

SPACECRAFT

On the frontier: Flight research at Dryden 1946-198t

[NASA-SP-4303] p 4 N85-17934

SPACECRAFT ANTENNAS

The 1980 Large space systems technology. Volume

2: Base technology

[NASA-CP-2168-VOL-2] p 66 N81-19196

Vibration studies of a lightweight three-sided membrane

suitable for space application

(NASA-TP-2095] p 131 N83-16785

Large Space Antenna Systems Technology, part 2

[NASA-CP-2269-PT-2} p 67 N83-26879

Decoupled control analysis of a large flexible space

antenna with linear quadratic regulator comparisons

[NASA-TP-22931 p 74 N84-23675

Technology for large space systems: A b=bliography with

indexes (supplement 14)

[NASA-SP-7046(14)} p 63 N86-28104

SPACECRAFT CABIN ATMOSPHERES

Water-vapor pressure control in a volume

[NASA-TP-1172] p 147 N78-20654

The Apollo spacecraft: A chronology volume 4, 21

January 1966 - 13 July 1974

[NASA-SP-4009-VOL-4] p 98 N80-20437

SPA ?'ECRAFT CHARGING

Jupiter probe charging study

[NASA-TP-1263] p 70 N79-15149

Spacecraft Charging Technology, 1978

[NASA-CP-2071 ] p 71 N79-24001

Development and design of three monitoring instruments

for spacecraft charging

[NASA-TP-1800] p 76 N81-31282

Spacecraft Charging Technology, 1980

[NASA-CP-2182] p 72 N82-14213

The aerodynamics of bodies in a rarefied ionized gas

with applications to spacecraft environmental dynamics

[NASA-TP-1933] p 72 N82-15116

Radiating dipole model of interference induced in

spececraff circuitry by surface discharges

INASA-TP-2240] p 74 N84-16247

A stochastic model for photon noise induced by charged

particles in multiplier phototubes of the space telescope

fine guidance sensors

[NASA-TP-2337] p 193 N84-26398

Design guidelines for assessing and controlling

spacecraft charging effects

[NASA-TP-2361 ] p 74 N84-33452

Spacecraft Environmental Interactions Technology,

1983

[NASA-CP-23591 p 75 N85-22470

SPACECRAFT COMMUNICATION

ATS-6 engineering performance report. Volume 3:

Telecommunications and power

INASA-RP-1080-VOL-31 p 73 N82-16149

Propagation effects handbook for satellite systems

design. A summary of propagation impairments on 10

to 100 GHz satellite links with techniques for system

design

INASA.RP-t082(03}J p 100 N83-29491

Space Station Technology, 1983

INASA-CP'22931 p 67 N84-18277

Hybrid routing technique for a fault-tolerant, integrated

information network

[NASA-TP-2605] p 180 N86-27947

SPACECRAFT CONFIGURATIONS

Effects of relaxed static longitudinal stability on a

single-stage-to-orbit vehicle design

[NASA-TP-1594] p 55 N80-13052

Measured and predicted shock shapes and aerodynamic

coefficients for blunted cones at incidence in air at Mach

5.9

[NASA-TP-1652} p 108 N80-23600

Calculation of inviscid flow over shuttle-like vehicles at

high angles of attack and comparisons with experimental

data

{NASA-TP-2103J p 110 N83-24808

Space Shuttle wind tunnel testing program

[ NASA-RP-1125 } p74 N85-11127

SPACECRAFT CONSTRUCTION MATERIALS

Outgassing data for spacecraft materials

[NASA-RP-f061 j p 80 N80-30441

Solar absorptance and thermal emiftance of some

common spacecraff thermal-control coatings

[NASA-RP-1121 } p 82 N84-23698

Outgassing data for selecting spacecraft materials

[NASA-RP-11241 p 82 N84-26751

Oxidation and emittance of superalloys in heat shield

applications

[NASA-TP-2578J p 90 N86-26412

SPACECRAFT CONTAMINATION

Theoretical contamination of cryogenic satellite

telescopes

(NASA-TP-11771 p65 N78-21193

Proceedings of the USAF/NASA International

Spacecraft Contamination Conference

INASA-CP-2039] p 62 N79-25048

The 111h Space Simulation Conference

[NABA-CP-2150} p99 N81-14138

Twelfth Space Simulation Conference: Shuttle Plus One

A New View of Space

[NASA-CP-2229J p 73 N82-25291

SPACECRAFT CONTROL

An active nutation damper for spacecraft

_NASA-TP-1108 ] p65 N78-15143

The N-BOD2 user's and programmer's manual

[NASA-TP-1145} p 70 N78-21200

A digital computer program for the dynamic interaction

simulation of controls and structure (DISCOS), volume 1

[NASA-TP-1219-VOL-1 ] p 70 N78-25123

A digital computer program for the dynamic interaction

simulation of controls and structure (DISCOS), volume 2

INASA-TP-1219-VOL-2] p 70 N78-25124

Simulator study of the effect of control-system time

delays on the Occurrence of pilot-induced oscillations and

on pilot tracking performance with a space-shuttle-orbiter

configuration

[NASA-TP-1588] p 34 N80 21317

Viking '75 spacecraft design and test summary Volume

2: Orbiter design

INASA-RP-1027-VOL-2] p 71 N81-10101

Analysis and simulation of a magnetic bearing

suspension system for a laboratory model annular

momentum control device

(NASA-TP-17991 p 99 N81-20311

The 15th Aerospace Mechanisms Symposium

[NASA-CP-2181} p 130 N81-22388

Existence and uniqueness of solutions to a class of

nonlinear-operator-differential equations arising in

automated spaceship navigation

[NASA-TP-1860] p 70 N81-23182

Time and frequency domain analysis of sampled data

controllers via mixed operation equations

[NASA-TP-1817] p 72 N81-25139

Reduced order feedback control equations for linear time

and frequency domain analysis

{NASA-TP-1818] p 72 N81-25140

Structural Dynamics and Control of Large Space

Structures, 1982

[NASA-CP-2266] p 67 N83-22256

Space Shuttle separate-surface control-system study

[NASA-TP-2340] p 58 N84-28801

Space station rotational equations of motion

[NASA-TP-2511 ] p 68 N85-34148

Application of the LOG/LTR technique to robust

controller synthesis for a large flexible space antenna

{NASA-TP-2560} p 75 N86-30800

SPACECRAFT DESIGN

Anthropometric source book. Volume 1: Anthropometry

for designers

[NASA-RP-t024} p 172 N79-11734

Jupiter probe charging study

[NASA-TP-1263} p 70 N79-15149

Effects of relaxed static longitudinal stability on a

single-stage-to-orbit vehicle design

[NASA-TP-1594] p 55 N80-13052

Viking '75 spacecraft design and test summary. Volume

1: Lander design

[NASA-RP-1027-VOL-1 ] p 71 N81-10100

Viking '75 spacecraft design and test summary Volume

2: Orbiter design

[NASA-RP-1027-VOL-2] p 71 N81-10101

Viking '75 spacecraft design and test summary. Volume

3: Engineering test summary

[NASA-RP-1027-VOL-3 } p71 N81-11102

Vibration characteristics of a steadily rotating slender

ring

[NASA-TP-1775} p 130 N81-14343

System analysis approach to deriving design criteria

(loads) for Space Shuttle and its payloads Volume 1:

General statement of approach

[NASA-TP-1949] p 66 N82-14203

Spacecraft Charging Technology, 1980

[NASA-CP-2182J p 72 N82-14213

Interactive design and analysis of future large spacecraft

concepts

INASA-TP-1937} p 72 N82-14276

IPAD: Integrated Programs for Aerospace-vehicle

Design

INASA-CP-2143] p 179 N83-17115

Electroless-plating technique for fabricating thin-wall

convective heat-transfer mode_s

INASA-TP-2349} p 112 N84-31561

Design guidelines for assessing and controlling

spacecraft charging effects

[NASA-TP-2361] p 74 N84-33452

Vibration, acoustic, and shock design and test criteria

for components on the Solid Rocket Boosters (SRB),

Lightweight External Tank (LWT). and Space Shuttle Main

Engines (SSME)

INASA-RP-1127] p 134 N85-10405

Space Shuttle wind tunnel testing program

I NASA-RP-1125J p74 N85-11127

Space Shuttle Technical Conference, part 1

I NASA-CP-2342-PT-1 I p 63 N85-16889

Problems experienced and envisioned for dynamical

physical systems

{ NASA-TP-2508 J p68 N86-11215

SPACECRAFT DOCKING

Automated rendezvous and docking: A parametric

study

[NASA-TP-23141 p 74 N84-23677

A-111
SPACECRAFT ENVIRONMENTS SUBJECT INDEX

SPACECRAFT ENVIRONMENTS

Spacecraft Charging Technology, 1978

[NASA-CP-2071 ] p 71 N7g-24001

Proceedings of the USAF/NASA international

Spacecraft Contamination Conference

[NASA-CP-2039] p 62 NTg-25048

Proceedings of workshops to define engineering

requirements for a space vacuum research facility

[NASA.CP.20gl] p 62 N7g-26076

Skylab's astronomy and space sciences

JNASA-SP-404] p 199 N79.34118

The physiologica_ basis for spacecraft environmental

limits

INASA-RP-1045} p 170 N80-15788

Living and working in space A history of Skyleb

[NASA-SP-42081 p 63 N84-25737

SPACECRAFT EQUIPMENT

High-voltage, high-power, solid-state remote power

controllers for aerospace applications

[NASA-TP-2437J p 78 N85-21263

SPACECRAFT GUIDANCE

Time and frequency domain analysis of sampled data

controllers via mixed otoeration equations

[NASA-TP-1817] p 72 N81-25139

Reduced order feedback control equations for linear time

and frequency domain analysis

[NASA-TP-1818J p 72 N81-25140

SPACECRAFT INSTRUMENTS

Flight Technology Improvement --- spaceborne optical

radiometric instruments, attitude control, and

electromechan+cal and power subsystems

{NASA-CP-2101 I p 75 N80-13152

Aerospace App+ications of Microprocessors

INASA-CP-2158] p 177 N81-tf644

Determination of the

hypersonic-continuumrarefied-flow drag coefficient of the

Viking lander capsule 1 aeroshell from flight data

j NASA-TP-17931 p 3 N81-14961

Solar Terrestrial Observatory Space Station Workshop

Report

I NASA-CP-2411 ] p 76 N86-19349

SPACECRAFT LANDING

Orbiter landing loads math model description and

correlation with ALT flight data

I NASA-RP-t 056 J p 71 N80-16091

SPACECRAFT LAUNCHING

Moonport: A history of Apollo launch facilities and

operations

[ NASA-SP-4204 ] p 64 N79-12127

Sensitivity analysis of the space shuttle to ascent wind

profiles

j NASA-TP-1988 / p 69 N82-20236

Airborne measurements of launch vehicle effluent:

Launch of Space Shuttle (STS-t) on 12 April 1981

[NASA-TP-2090] p 150 N83-16952

Analysis of Jimsphere pairs for use in assessing Space

Vehicle ascent capability

_NASA-TP-2573] p 28 N86-21506

SPACECRAFT LUBRICATION

The 171h Aerospace Mechanisms Symposium

{NASA-CP-22731 p 131 N83-24881

SPACECRAFT MANEUVERS

Two-impulse reorlentation of asymmetric spacecraft

INASA-TP 1554j p 64 N80-13135

SPACECRAFT MODULES

Guntersville Workshop on Solar-Terrestrial Studies

[ NASA-CP-2037 ] p 144 N78-19600

SPACECRAFT MOTION

Spacecraft Dynamics as Related to Laboratory

Experiments in Space --- conference

[NASA-CP-21991 p 72 N82-12109

Twelfth Space Simulation Conference: Shuttle Plus One.

A New View of Space

{NASA-CP 22291 p 73 N82-25291

SPACECRAFT ORBITS

Sixth Annual Flight Mechanics/Estimation Theory

Symposium

I NASA-CP-22051 p 62 N82-10064

Second Workshop on Spacecraft Glow

I NASA-CP-2391 i p 201 N86-13239

SPACECRAFT PERFORMANCE

Effect of propulsion system charactenstics On ascent

performance of dual-fueled single-stage earth-to-orbit

transports

INASA-TP-11151 p 65 N78-13109

SPACECRAFT POWER SUPPLIES

The ATS-6 power system: Hardware implementation

and Orbita_ performance

! NASA-TP-1023} p 76 N77-32229

Future Orbital Power Systems Technology

Requirements

[NASA-CP-2058] p 76 N79-10122

The 1977 Goddard Space Flight Center Battery

Workshop

[NASA-CP-2041 ] p 144 N79-21565

The 1 lth Annual Battery Workshop

[NASA-CP-2088] p 144 N79-2866g

Flight Technology Improvement ... apacabm'ne optical

radiometric instruments, attitude control, and

electromechanical and power subsystems

[NASA-CP-2101] p 75 N80-13152

Sealed-cell nickel-cadmium battery applications

manual

[NASA-RP-1052] p 77 N80-16095

The 1979 Goddard Space Flight Center Battery

Workshop

[NASA-CP-2117] p 145 N80-20820

Synchronous Energy Technology

[NASA-CP-2154] p 77 N80-33465

The 198t Goddard Space Flight Center BaTtery

Workshop

[NASA-CP.2217] p 102 N82.20402

Space power subsystem automation technology

[NASA-CP-2213] p 77 N82-21254

Space Photovoltaic Research and Technology 1982:

High Efficiency, Radiation Damage, end Blanket

Technology

[NASA-CP-2256] p 146 N83-15806

The 1982 Geddard Space Flight Center Battery

Workshop

[NASA-CP-2263] p 102 N83-35230

Space Photovoltaic Research and Technology 1983.

High Efficiency, Radiation Damage, and Blanket

Technology

[NASA-CP-2314] p 146 N84-29307

The 1983 Goddard Space Flight Center Battery

Workshop

[NASA-CP-2331] p 103 N84.33668

Space Power

[NASA-CP-2352] p 78 N85-13880

The 1984 Goddard Space Flight Center Battery

Workshop

{NASA-CP-2382] p 103 N85-31371

Space Photovoltaic Research and Technology 1985:

High Efficiency, Space Environment, and Array

Technology

[NASA-CP-2408] p 146 N86-17839

SPACECRAFT PROPULSION

Large Space Systems/Low-Thrust Propulsion

Technology

[NASA-CP-2144] p 77 N80-31449

The 15th Aerospace Mechanisms Symposium

[NASA-CP-2181J p 130 N81-22388

Electric Flight Systems

[ NASA-CP-22091 p3 N82-19134

Modeling of space vehicle propellant mixing --- cryogenic

propellants

[NASA-TP-2107] p 97 N83-16545

Structural Integrity and Durability of Reusable Space

Propulsion Systems

[NASA-CP-2381J p 78 N85-27941

SPACECRAFT REENTRY

Development of the reentry fright dynamics simulator

for evaluation of space shuffle orbiter entry systems

INASA-TP-17001 p 71 N80-32429

Effect of aerodynamic and angle-of-attack uncertainties

on the May 1979 entry flight control system of the Space

Shuttle from Mach 8 to 1.5

INASA-TP-23651 p 69 N85-15778

SPACECRAFT SHIELDING

Proceedings of workshops to define engineering

requirements for a space vacuum research facility

[NASA-CP-2091] p 62 N79-26076

Meteoroid bumper experiment on Explorer 46

JNASA-TP-1879] p 72 N81-29155

Solar absorptance and thermal emittance of some

common spacecraft thermal-control coatings

INASA-RP.1121 ] p 82 N84-23698

SPACECRAFT STRUCTURES

Computational Aspects of Heat Transfer in Structures

INASA-CP-22161 p 109 N82-23473

Space Shuttle Technical Conference, part 2

[NASA-CP-2342-PT-2] p 63 N85-t6937

SPACECRAFT TRAJECTORIES

Motion about the stable libration points in the linearized,

restricted three-body problem

[NASA-RP-t065] p 203 N81-11970

Slip-boundary equations for multicomponent

nonequilibrium airflow

[NASA-TP-2452] p 113 N86-t4530

SPACECREWS

Biomedical results from Skylab

{NASA-SP-377] p 169 N77-33780

The 15th Aerospace Mechanisms Symposium

[NASA-CP-2181] p 130 N81-22388

Space Physiology and Medicine

[NASA-SP-447] p 170 N83-25349

Living aloft: Human requirements for extended

spaceflight

{NASA-SP-483} p 174 N85-32772

Hybrid routing technique for a fault-tolerant, integrated

information network

[NASA-TP-2605] p 180 N8S-27847

SPACELAB

A cfttioat review Of the life sciences project management

at Ames Research Center for the Spaeelab Mission

development test 3

[NASA.TP-1364] p 196 N79.16709

System analysis approach to denying design cdtena

(loads) for Space Shuttle and its payloads. Volume 1:

General statement of approach

[NASA-TP-1949] p 66 N82-14203

SPACELAB PAYLOADS

Space plasma physics active experiments

[NASA-CP-2165] p 212 N81-14944

Approximate analysis of thermal convection in a

crystal-growth cell for Spaceleb 3

[NASA-TP-20161 p 62 N82-29335

Finite-difference fluid dynamics computer mathematical

models for the design and interpretation of experiments

for space flight --- atmospheric general circulation

experiment, convection in a float zone, and the

Bndgman-Stockbarger crystal growing system

[NASA-TP-2323] p 112 N84-23852

SPALLING

Wear particles of single-crystal silicon carbide in

vacuum

[NASA-TP-1624] p 93 N80-18178

Effect ol Yttria additives on properties of

pressureless-sintered silicon nitrKle

[NASA-TP-1899] p 94 N81-31366

SPANLOADER AIRCRAFT

Preliminary study of a large span-distributed-load

flying-wing cargo airplane concept

[NASA-TP-1158] p 32 N78-25079

An experimental and theoretical investigation of thick

wings at various sweep angles in and OUt of ground

effect

[NASA-TP-2068] p 20 N83-10016

SPANWISE BLOWING

improvement of maneuver aerodynamics by spanwise

blowing

[NASA-TP-1065J p 7 N78-14997

Effects of spanwise nozzle geometry and location on

the longitudinal aerodynamic characteristics of a

vectored-engine-over.wing configuration at subsonic

speeds

[NASA-TP-12151 p 8 N78-25060

Investigation of trailing-edge-flap, spanwise-biowing

concepts on an advanced fighter configuration

[ NASA-TP-22501 p23 N84-18164

Experimental investigation of tangential blowing applied

to a subsonic V/STOL inlet

[NASA-TP-22971 p 23 N84-20493

Low-speed stability and control wind-tunnel

investigations of effects of spanwise blowing on fighter

flight characteristics at high angles of attack --- Langely

12-It low-speed tunnel and 30- by 60-It tunnel

[NASA-TP-2431 I p 26 N85-23708

SPARROW 3 MISSILE

Supersonic aerodynamic characteristics of a Sparrow

3 type missile model with wing controls and comparison

with existing tail-control results

[NASA-TP-1078] p 6 N78-12041

SPATIAL DISTRIBUTION

A general solution to the hidden-line problem --- to

graphically represent aerodynamic stabitityderivatives

{NASA-RP-1085] p 176 N82-21907

Airborne lidar measurements of El Chichon stratospheric

aerosols

[NASA-RP-11481 p 155 N86-13850

Airborne lidar measurements of El Chichon stratoshperic

aerosols

{NASA-RP-11661 p 156 N86-27838

SPATIAL FILTERING

Simulated e_ectron_c heterodyne recording and

processing of pulsed*laser holograms

INASA-TP-1444J p 114 N79-21329

SPATIAL MARCHING

Numerical simulation of steady supersonic flow --- spatial

marching

JNASA-TP-1749] p 17 N81-22018

SPATIAL RESOLUTION

LANDSAT-4 Science Investigations Summary, including

December 1983 Workshop results, volume 2

[E84-10167] p 137 N84-30380

SPECIFIC IMPULSE

Current evaluation of the tripropetlant concept

[NASA-TP-26021 p 78 N86-28124

SPECIMEN GEOMETRY

A cracked orthotropic sheet stiffened by a semi-infinite

orthotropic sheet

[NASA-TP-2455J p 134 N85-32339

A-112
SUBJECT INDEX STAINLESS STEELS

SPECKLE PATTERNS

DIAL with heterodyne detection including speckle noise:

Aircraft/shuttle measurements of 03, H20, and NH3 with

pulsed tunable CO2 lasers

INASA-TP-1725] p 115 N80-30717

SPECTRAL BANDS

The Multispectral Imaging Science Working Group.

Volume 3: Appendices

[E83-10351J p 142 N83-28506

SPECTRAL EMISSION

Emit'ience and absorptance of NASA ceramic thermal

barrier coating system --- for turbine cooling

[NASA-TP-t190J p 43 N78-26148

Spectral flame radiance from a tubular-can combustor

[NASA-TP-1722J p 48 N81-19121

SPECTRAL ENERGY DISTRIBUTION

Terrestrial photovoltaic measurements, 2

{NASA-CP-20t0] p 136 N77-3052t

SPECTRAL RECONNAISSANCE

Earth resources: A continuing bibliography with indexes,

issue 50

[NASA-SP-7041(50)J p 143 N88-31940

SPECTRAL REFLECTANCE

Laboratory and field measurements of upwelied radiance

and reflectance spectra of suspended James River

sediments near Hopewetl, Virginia

[NASA-TP-1292J p 147 N78-33616

Laboratory upwelled radiance and reflectance spectra

of Kerr reservoir sediment waters

[ NASA-TP-1993 j p 180 N82-21774

Spectral reflectances of natural targets for use in remote

sensing studies

(NASA-RP-1139} p 143 N85-30450

SPECTRAL RESOLUTION

LANDSAT-4 Science Characterization Early Results.

Volume 2, part 1: Thematic Mapper (TM)

[E85-10068J p 143 N85-20508

LANDSAT-4 Science Characterization Early Results.

Volume 3, part 2: Thematic Mapper (TM)

IE85-10069t p 143 N85-21724

SPECTRAL SENSITIVITY

LANDSAT-4 Science Characterization Early Results.

Volume 4: Applications --- agriculture, soils land use,

geology, hydrology, wetlands, water quality, biomass

identification, and snow mapping

[E85-10070] p 143 N85-23186

SPECTRAL SIGNATURES

Laboratory measurements of upwelled radiance and

reflectance spectra of Calvert, Ball, Jordan, and Feldspar

soil sediments

[NASA-TP-1039] p 167 N78-12645

Laboratory measurements of radiance and reflectance

spectra of a dilute biosolid industrial waste product

[NASA-TP-1401 J p 148 N79-17360

Investigation of effects of background water on upwelled

reflectance spectra and techniques for analysis of dilute

primary-treated sewage sludge

[NASA-TP-14461 p 168 N79-28864

Laboratory measurements of physical, chemical, and

optical characteristics ol Lake Chicot sediment waters

[NASA-TP-1941 I p 140 N82-13468

SPECTROGRAPHS

An atlas of solar spectra between 1175 and 1950

angstroms recorded on Skylab with the NRL's Apollo

telescope mount experiment

[NASA-RP-tO691 p 209 N81-23004

SPECTROMETERS

Vibrational-Rotational Spectroscopy For Planetary

Atmospheres, volume 1

[NASA-CP-2223-VOL-1 J p 207 N82-25043

User's guide for the Total-Ozone Mapping Spectrometer

(TOMS) instrument first year ozone T data set

[NASA-RP-1098] p 164 N82-28880

User's guide for SBUV/TOMS ozone derivative

products

[NASA-RP-1116] p 165 N84-16720

SPECTRORADIOMETERS

Atmospheric solar absorption measurements in the 9

to 11 mum region using a diode laser heterodyne

spectrometer

[NASA-TP-t7261 p 153 N80-33998

SPECTROSCOPIC ANALYSIS

Experimental study of cluster formation in binary mixture

of H20 and H2SO4 vapors in the presence of an ionizing

radiation source

)NASA-TP-1735] p 149 N81-11565

X-ray photoelectron spectroscopy and friction studies

of nickel-zinc and manganese-zinc ferrites in contact wlth

metals

INASA-TP-2163] p 88 N83-23419

Spectroscopic analysis of radiation-generated changes

in tensile properties of a polyetherimide film

INASA-TP-2429] p 83 N85-25435

SPECTROSCOPY

Second Workshop on Spacecraft Glow

INASA-CP-2391 I p 201 N86-13239

International Ultraviolet Explorer Atlas of O-typespectra

from 1200 to 1900 angstrom

[NASA-RP-1155] p 204 N86-25307

SPECTRUM ANALYSIS

Fluctuation spectra in the NASA Lewis bumpy-torus

plasma

[NASA-TP-1257] p 194 N78-26927

Effect of low-frequency tones and

turbulent-boundary-layer noise on annoyance

[NASA-TP-22021 p 172 N83-34579

Formulation of blade-flutter spectral analyses in

stationary reference frame

[NASA-TP-22961 p 51 N84-20562

SETI science working group report

{NASA-TP-2244} p 175 N84-22178

Solar Irradiance Variations on Active Region Time

Scales

[NASA-CP-2310J p 209 N84-27635

Uranus and Neptune

{ NASA-CP-2330 ] p 208 N85-11927

SPEED CONTROL

Multiroiler traction drive speed reducer: Evaluation for

automotive gas turbine engine

[NASA-TP-20271 p 122 N82-26678

SPHERES

Pressures, forces, moments and shock shapes for a

geometrically matched sphere-cone and hyperboloid at

Mach 20.3 in helium --- 22-inch aerodynamics leg of the

Langley hypersonic helium tunnel facility

{NASA-TP-2100] p 110 N83-16675

SPHERICAL HARMONICS

Parameter estimation applied to Nimbus 6 wide-angle

tongwave radiation measurements

INASA-TP-1307] p 159 N79-13644

Deconvolution and analysis of wide-angle Iongwave

radiation data from Nimbus 6 Earth radiation budget

experiment for the first year

INASA-TP-1746] p 162 N81-13593

SPIN DYNAMICS

Flight investigation of stall, spin and recovery

characteristics of a low-wing, single-engine, T-tail light

airplane

[NASA-TP-2427] p 37 N85-25248

SPIN STABILIZATION

Spin-tunnel investigation of the spinning characteristics

of typical single-engine general aviation airplane designs.

2: Low-wing model A; tail parachute diameter and canopy

distance for emergency spin recovery

[ NASA-TP-1076] p6 N78-12040

Two-impulse reorientation of asymmetric spacecraft

INASA-TP-1554] p 64 N80-13135

SPIN TESTS

Spin-tunnel investigation of the spinning characteristics

of typical single-engine general aviation airplane designs.

1, Low-wing model A: Effects of tail configurations

{NASA-TP-tO09 ] p5 N77-33111

Spin tests of a single-engine, high-wing light airplane

[NASA-TP-1927] p 35 N82-t6068

Lewis Research Center spin rig and its use in vibration

analysis of rotating systems

[NASA-TP-23041 p 51 N84-24578

SPIRAL GALAXIES

Cotlisionless galaxy simulations

[NASA-RP-10371 p 201 N79-24921

Molecular clouds and galactic spiral structure

[NASA-TP-22881 p 204 N84-20457

SPMNE FUNCTIONS

Spline methods for approximating quantile functions and

generating random samples

[NASA-TP-23891 p 184 N85-16865

The algorithms for rational spline interpolation of

surfaces

{NASA-TP-25361 p t 83 N86-18060

SPOILERS

Wind-tunnel investigation at Mach numbers from 1,90

to 2,86 of a canard-controlled missile with ram-air-jet

spoiler roll control --- in the Langley Unitary Plan Wind

Tunnel

I NASA-TP-11241 p 7 N78-20079

An experimental wind-tunnel investigation of a

ram-air-spoiler roll-control device on a forward-control

missile at supersonic speeds

INASA-TP-1353] p tt N79-17809

Low-speed wind-tunnel parametric investigation of flight

spoilers as trailing-vortex-alleviation devices on a transport

aircraft model

IrNASA-TP-14191 p 11 N79-22038

Vortex wake alleviation studies with a variable twist

wing

{ NASA-TP-2442 j p5 N86-16187

Aerodynamic characteristics of sevefal current

helicopter tail boom cross sections including the effect

of spoilers

[NASA-TP-2506J p 27 N86-20349

SPOT WELDS

Loading tests of a wing structure for a hypersonic

aircraft

[NASA-TP-15961 p 34 N80-t5068

SPRAY CHARACTERISTICS

Venture nozzle effects on fuel drop size and nitrogen

oxide emissions

[NASA-TP-20281 p 49 N82-31329

SPRAYED COATINGS

Plasma-sprayed coatings for lubrication of a titanium

alloy in air at 430 deg C

INASA-TP-t5091 p 93 N79-29327

SPRAYERS

Particle sizing by measurement of forward-scattered light

at two angles

[NASA-TP-2156] p 50 N83-24509

SPUTTERING

X-Ray photoelectron spectroscopy study of

radiofrequency-sputtered titanium, carbide, molybdenum

carbide, and titanium boride coatings and their friction

properties

[NASA-TP-t033] p 91 N77-33348

X-ray photoelectron spectroscopy study of

radiofrequency-sputtered refractory compound steel

interfaces

{NASA-TP-1161 ] p 91 N78-20336

Effect of nitrogen-containing plasma on adherence,

friction, and wear of radiofrequency-sputtered titanium

carbide coatings

[NASA-TP-1377] p 92 N79-15184

Improved adherence of sputtered titanium carbide

coatings on nickel- and titanium-base alloys

[NASA-TP-1450] p 78 N79-22194

STABILITY

Rotordynamic Instability Problems in High-Performance

Turbomachinery

[NASA-CP-2250i p 122 N83-15629

Wind-tunnel free-flight investigation of a model of a

fonvard-swept-wing fighter configuration

[NASA-TP-2230] p 57 N84-t7184

STABCAR: A program for finding characteristic root

systems having transcendental stability matrices

{NASA-TP-2165J p 179 N84-27461

Rotordynamic Instability Problems in High-Pertormance

Turbomachinery

{NASA-CP-2338] p 124 N85-14116

Fluid surface behavior in low gravity. Center

discretionary fund no 83-21

[NASA-TP-2486] p 113 N85-28280

STABILITY AUGMENTATION

Realizable optimal control for a remotely piloted research

vehicle --- stability augmentation

[NASA-TP-t854J p 181 N80-25039

Economic evaluation of flying-qualities design criteria for

a transport configured with relaxed static stability

[NASA-TP-t760J p 58 N81-13968

STABILITY DERIVATIVES

Aerodynamic denvatives for an oblique wing aircraft

estimated from flight data by using a maximum likelihood

technique

INASA-TP-1336] p 10 N78-33054

Flight-determined stability and control derivatives for the

F-111 Tact research aircraft

[NASA-TP-1350J p 54 N79-10068

Comparison of analytical and flight test identified

aerodynamic derivatives for a tandem-rotor transport

helicopter

[NASA-TP-158t J p 34 N80-17060

Dynamics stability derivatives of space shuttle orbiter

obtained from wind-tunnel and approach and landing flight

tests

INASA-TP-1634J p 55 Nao-21336

A general solution to the hidden-line problem --- to

graphically represent aerodynamic stability derivatives

[NASA-RP-10851 p 176 N82-21907

Pressures, forces, moments and shook shapes for a

geometrically matched sphere-cone and hyperboloid at

Mach 20.3 in helium --- 22-inch aerodynamics leg of the

Langley hypersonic helium tunnel facility

[NASA-TP-2t00] p 110 N83-16675

A conceptual framework for using Doppler radar

acquired atmospheric data for flight simulation

[NASA-TP-2192] p 36 N83-27977

STABILITY TESTS

Local stability analysis for a planar shock wave

[NASA-TP-23871 p 25 N88-12864

STAGNATION POINT

Influence of thermal boundary conditions on heat

transfer from a cylinder in cross flow

[NASA-TP-1894] p 109 N81-29384

STAINLESS STEELS

Transfer of molybdenum disulfide to various metals

|NASA-TP-f019J p 98 N77-30296

Influence of fretting on flexural fatigue of 304 stainless

steel and mild steel

[NASA-TP-1193J p 86 N78-21269

A-113
STANDARDIZATION SUBJECT INDEX

Mechanical properties and oxidation and corrosion

resistance of reduced-chromium 304 stainless steel

alloys

!NASA-TP-1557 I p87 N80-11188

Mechanical qmpacl tests of materials in oxygen effects

of contamination -- Teflon, stainless steel, and

aluminum

lNASA-TP-1571 I p 97 N80-2155f

Tnbological properties at 25 C of seven polyimide films

bonded to 440 C high-temperature stainless steel

INASA-TP-19441 p 94 N82-19373

Elastic-plastic hnite-eIement analyses of thermally

cycled single-edge wedge specimens

ENASA-TP-19821 p 130 N82-20565

Plastic deformation at surface during unlubricated

sliding

tNASA-TP-2036] p 122 N83-1f49£,

Effect of sliding speed and contact stress on tnbological

properties of ultra-high-molecular-weight polyethylene

I NASA-TP-20591 p 95 N83-14269

Rolling-element fatigue life of AMS 5900 balls

[ NASA-TP-2080 t p 122 N83-16758

STANDARDIZATION

Slandardizatton, certification, maintenance, and

dissemination of large scale engineering software

systems

I NASA-CP-20t 5 ] p 176 N77-33876

NASA Metrology and Calibration, 1980

[NASA-CP-2174] p 115 N8t-23432

STANDARDS

Office of Space Terresthal Applications

(OSTA)/Applications Data Service (ADS) data systems

standards

[ NASA-CP-2196 ] p 65 N62-15095

Techn_calcommunicafion PerspectivesfortheEighties,

part 2

INASA-CP-2203-PT-2] p 197 N82-15966

NASA publications guide

I NASA-SP-7047 I p 197 N83-32671

Group-type hydrocarbon standards for

high-performance liquid chromatographic analysis of

middislillate fuels

I NASA-TP-23171 p 97 N84-23774

STANDING WAVES

Circumferenhally segmented duct lines optimized for

axisymmelric and standing wave sources --- reducing noise

from turbofan eng[nes gaterkin method acoustic

attenuation

INASA.TP-20751 p 188 N82-34190

STARS

Advances in Ultraviolet Astronomy: Four Years of IUE

Research

[ NASA-CP-22381 p 201 N82-31163

Airborne Astronomy Symposium, A symposlurn

commemorating the tenth anniversary of operations of the

Kuiper Airborne Observatory

(NASA-CP-2353_ p 202 N85-17848

STATIC AERODYNAMIC CHARACTERISTICS

Static performance of five twin-engine nonaxisymmetric

nozzles with vectoring and reversing capability

I NASA-TP-1224 ] p 9 N78-28057

Static aerodynamic characteristics of a winged

smgie-stage-to-orbil vehicle at Math numbers from 03 to

4 63

I NASA-TP-12331 p 9 N78-30053

Static infernal performance of single expansion-ramp

nozzles with thrust vectoring and reversing

INASA-TP-1962] p 19 N62-20156

STATIC ELECTRICITY

internationa_ Aerospace and Ground Conference on

Lightning and Static Electricity. 1984 technical papers.

Supplement

[NASA-CP-2356] p f66 N85-16343

STATIC FIRING

State test-stand performance of the YF-102 turbofan

eng_Tle with several exhaust configurations for the Quiet

Short-Haul Research Aircraft (QSRA)

{NASA-TP-1556j p 45 N80-14121

STATIC FRICTION

Steady-state wear and fnction in boundary lubrication

studies

[ NASA TP 1658] p 93 N80-22493

STATIC LOADS

Effects of static tensile load on the thermal expansion

of Gr/PI composite malerial

{NASA-TP-18671 p81 N8f-24179

Static and yawed-rolling mechanical properties of two

type 7 aircraft tires

INASA-TP-1863] p 130 N81-24471

Rolling-element bearings

{NASA-RP-1105] p 123 N83-27214

Results of the first complete static calibration of the

RSRA rotor-load-measurement system

I NASA-TP-2327 ] p37 N84-3f 111

STATIC PRESSURE

Two-dimensional transonic testing with splitter plates

[NASA-TP-1153} p 7 N78-17999

In-flight boundary-layer measurements on a hollow

cylinder at a Mach number of 30

[NASA-TP-1764] p 108 N81-12361

A study of the sonic-boom cheracfenstics of a blunt body

at a Mach number of 6

[NASA-TP-1767} p 3 N81-f3915

Hot-flow tests of a series of t0-percent-scale turbofan

forced mixing nozzles

[NASA-TP-2268] p 111 N84-f 7525

Effects of inlet distortion on a static pressure probe

mounted on the engine hub in an F-15 airplane

fNASA-TP-2411 ] p 52 N85-22394

onfice-induced pressure error studies in Langley 7- by

t0-foot high-speed funnel

INASA-TP-2545} p 27 N86-20347

The application fo airfoils of a tachnique for reducing

orifice-induced pressure error at high Reynolds numbers

{NASA-TP-2537] p 27 N86-20351

STATIC STABILITY

Static and dynamic stability analysis of the space shuttle

vehicle-orbiter

INASA-TP-t 179] p66 N78-20176

Simulator study of stall/post-stall charactenstics of a

fighter airptane with relaxed longitudinal static stability ---

F-16

fNASA-TP-1538 p 55 N80-14136

Comparison of Space Shuttle Orbiter low-speed static

stability and control derivatives obtained from wind-tunnel

and approach and landing flight tests

{NASA-TP-1779 p 56 N81-13066

STATIC TESTS

Experimental and analytical investigation of a

nonaxisymmefric wedge nozzle at static conditions

INASA-TP-1188 p 8 N78-26109

Effect ol several geometric parameters on the static

internal performance of three nonaxisymmetric nozzle

concepts

INASA-TP-t468 p 12 N79-26022

Static and transient performance of YF-102 engine with

up to 14 percent core airbleed for the quiet short-haul

research aircraft

[NASA-TP-1692 p 47 N80-25339

Tire stiffness and damping determined from static and

free-vibration tests --- aircraft tires

[NASA-TP-t67t p 29 N80-27302

The effect of lhroat contounng on two-dimensional

converging-diverging nozzles at static conditions

{NASA-TP-t704J p 15 N80-29250

Static internal performance of single expansion-ramp

nozzles with thrust vectonng and reversing

{NASA-TP-f962 p 19 N82-20156

Fluctuating pressures on fan blades of a turbofan engine:

Static and wind-tunnel investigations

{NASA-TP-1976 p 188 N82-2f037

Test-engine and inlet performance of an aircraft used

for investigating flight effects on fan noise

{NASA-TP-2254J p 189 N84-21277

Static investigation of several yaw vectoring concepts

on nonaxisymmetric nozzles

{NASA-TP-2432J p 26 N85-28924

Static internal performance of a single-engine

onaxisymmetric-nozzle vaned-thrust-reverser design with

thrust modulation capabilities

{NASA-TP-2519} p 27 N86-20348

Static investigation of circular-to-rectangular transition

ducts for high-aspect-ratio nonaxisymmetric nozzles

{NASA-TP-2534} p 52 N86-22576

Static investigation of two STOL nozzle concepts w_th

pitch thrust-vecfohng capability

{NASA-TP-2559} p 28 N86-23559

Static internal performance of a thrust vectoring and

reversing two-dimensional convergent-divergent nozzle

with an aft flap

[NASA-TP-2549} p 28 N86-23560

STATISTICAL ANALYSIS

Statistical model for asperity-contact time fraction in

etastohydrodynamic lubhcation

INASA-TP-1130] p 119 N78-t8429

Statistical comparisons of aircraft flyover noise

adjustment procedures for different weather conditions

INASA-TP-1430} p 187 N79-24773

Application of modified profile analysis to function testing

of the motion/no-motion issue in an aircraft

ground-handling simulation --- statistical analysis

procedure for man machine systems flight simulation

[NASA-TP-1540t p 33 N80-t3024

Rate statistics for radio noise from lightning

[NASA-TP-1665] p 161 N80-23933

Cloud-encounter and particle.concentration variabilities

from GASP data

INASA-TP-18861 p 164 N82-15677

An evaluation and comparison of vertical profile data

from the VISSR Atmospheric Sounder (VAS)

INASA-TP-2425] p 166 N85-16351

Statistical analysis of direct-strike lightning data (1980

to 1962)

INASA-TP-2252] p 167 N66-24090

STATOR BLADES

Cold-air performance of free-power turbine designed for

112-kilowaft automotive gas-turbine engine. 1: Design

Stator-vane-chord setting angle of 35 deg

[NASA-TP-t007} p 42 N78-16053

Two-dimensional cold-air cascade study of • film-cooled

turbine sfator blade. 4: Comparison of experimental and

analytical aerodynamic results for blade w_th 12 rows of

0.076-centimeter-(0.030-inch-) diameter holes having

sfreamwise ejecbon angles

I NASA-TP-1151 J p 42 N78-20130

Two-dimensional cold-air cascade study of a film-cooled

turbine stator blade. 5: Comparison of experimental and

analytical aerodynamic results for blade with 12 rows of

0.03S-centimeter-(0.015 inch) diameter coolant holes

having streamwise ejection angles

{NASA-TP-1204J p 42 N78-20133

Effect of casing treatment on performance of a two-stage

high-pressure-ratio fan

INASA-TP-14091 p 44 N79-16852

Aerodynamic performances of three fan stator designs

operating with rotor having tip speed of 337 meters per

second and pressure ratio of 1.54. 1: Experimental

performance

{NASA-TP-1610} p 46 N80-17071

Aerodynamic performances of three fan stator designs

operating with rotor having tip speed of 337 meters per

second and pressure ratio of t 54. Relation of analytical

code calculations to experimental performance

[NASA-TP-1614J p 46 N80-21324

Performance of single-stage axial-flow transonic

compressor with rotor and stator aspect ratios of 1.19

and 1.26 respectively, and with design pressure ratio of

2.05

{NASA-TP-t659J p 46 N80-21325

Of/-design performance loss model for radial turbines

with pivoting, variable-area stators

[NASA-TP-1708} p 47 N81-11038

Analytic investigation of effect of end-wall contouring

on stafor performance

INASA-TP-f943} p 19 N82-1405t

Performance of single-s_ge axial-flow transonic

compressor with rotor and stator aspect ratios of 1.63

and 1.76, respectively, and with design pressure ratic of

1,82

INASA-TP-1974] p 49 N82-19222

Laser anemometer measurements in an annular

cascade of core turbine vanes and comparison with

theory

|NASA-TP-2018} p 20 N82-26234

STATORS

Analytic investigation of effect of end-wall contounng

on stator performance

[NASA-TP-1943] p 19 N82-14051

Flow visualization study of the horseshoe vortex in a

turbine stator cascade

[NASA-TP-1884] p 110 N82-30498

Performance of • tandem- rot or/tandem-stator

conical-flow compressor designed for a pressure ratio of

3

{ NASA-TP-2034 } p 20 N83-t 1056

Analytical and experimental investigation of stator

endwall contouring in a small axial-flow turbine. 1: Stator

performance

{NASA-TP-2023 } p49 N83-11125

Study of stator-vane fluctuating pressures in a turbofan

engine for static and flight tests

[NASA-TP-22171 p 189 N84-22363

Analytical and experimental investigation of stator

endwall countounng in a small axial-flow turbine

[NASA-TP-2309} p 51 N84-32386

STEADY FLOW

Steady and nonsteady supersonic turbulent afterbody

flow

{NASA-TP-17691 p 16 N81.16977

Numerical simulation of steady Supersonic flow --- spatial

marching

{NASA-TP-1749] p 17 N81-22016

Steady internal flow and aerodynamic loads analysis of

shuttle thermal protection system

INASA-TP-2255] p 74 N84-19393

STEAM FLOW

Effect of steam addition on cycle performance of simple

end recuperated gas turbines

[NASA-TP-1440} p 144 N79-22626

STEAM TURBINES

New features and applications of PRESTO, a computer

code for the performance of regenerative, superheated

steam turbine cycles

INASA-TP-f954] p 145 N82-16477

A-114
SUBJECT INDEX

Analysis of potential benefits "_f integrated-gasifier

combined cycles for a utility system

[NASA-TP-2172] p 146 N83-36549

STEELS

Effecl of double vacuum melting and retained austenite

on rolling-element fatigue life of AMS 5749 bearing steel

[NASA-TP-1060] p 119 N77-33520

X-ray photoelectron spectroscopy study of

radiofrequeney-sputtered refractory compound steel

interfaces

[NASA-TP-1161 ] p 91 N78-20336

Long-term hot-hardness characteristics of five

through.hardened bearing steels

IrNASA-TP-1341 J p 87 N78-33196

Evaluation of CBS 600 carburized steel as a gear

matenal

{NASA-TP-1390] p 120 N79-14389

Galvanic coupling between D6AC steel. 6061-T6

aluminum. Inconel 718 and graphite-epoxy composite

material: Corrosion occurrence and prevention

[NASA-TP-2236J p 89 N84-13263

Mechanism of lubrication by tricresylphosphate (TCP)

[NASA-TP-2274] p 123 N84-18653

Effect of lubricant extreme-pressure additives on surface

fatigue life of AISI 9310 spur gears

[NASA-TP-2408] p 124 N85-13234

Surface fatigue life and failure characteristics of EX-53,

CBS t000M, and AISI 9310 gear matenals

[NASA-TP-25131 p 125 N86-12609

STEERING

Braking and cornering studies on an air cushion landing

system

[NASA-TP-2196] p 36 N83-34935

STELLAR ATMOSPHERES

B Stars with and without emission lines, parts 1 and 2

[NASA-SP-456] p 200 N82-25027

The A-stars: Problems and perspectives, Monograph

series on nonfhermal phenomena in stellar atmospheres

[NASA-SP-463] p 204 N83-32693

Stellar atmosphenc structural patterns

[NASA-SP-471 ] p 204 N84-19253

The Origin of Nonradiative Heating/Momentum in Hot

Stars

[NASA-CP-2358J p 200 N85-t7755

STELLAR ENVELOPES

Stellar atmospheric structural pafferns

[NASA-SP-471 ] p 204 N84-19253

Interrelationships among Circumstellar, Interstellar and

Interplanetary Dust

[NASA-CP-2403] p 201 N86-23493

STELLAR EVOLUTION

Recognition of compact astrophysical objects

[NASA-SP-421 ] p 201 N77-34063

The Origin of Nonradiative Heating/Momentum in Hot

Stars

[NASA-CP-2358J p 200 N85-17755

Future of Ultraviolet Astronomy Based on Six Years of

IUE Research

[NASA-CP-2349] p 203 N85-20961

Search for the universal ancestors

[NASA-SP-477] p 175 N85-32777

Interrelationships among Circumsteller, Interstellar and

Interplanetary Dust

[NASA-CP-2403] p 201 N86-23493

STELLAR MODELS

B Stars with and without emission lines, parts I and 2

[NASA-SP-456] p 200 N82-25027

Stellar atmospheric structural patterns

[NASA-SP-471] p 204 N84-19253

Solar Terrestrial Physics: Present and Future

[NASA-RP-11201 p 200 N84-34332

STELLAR RADIATION

The star splitters: The high energy astronomy

observatories

[NASA-SP-466] p 202 N84-22516

STELLAR SPECTRA

B Stars with and without emission lines, paris 1 and 2

[NASA-SP-456] p 200 N82-25027

STELLAR SPEGTROPHOTOMETRY

Catalog of far-ultraviolet objective-prism

spectrophotometry: Skylab expehment S-019, ultraviolet

atelier astronomy

[NASA-RP-1031] p 210 N79-27057

STELLAR STRUCTURE

The Sun as a star

[NASA-SP-450] p 203 N81-27008

Variations of the Solar Constant --- conference

[NASA-CP-2191] p 209 N82-17014

STELLAR SYSTEMS

Collisionless galaxy simulations

[NASA-RP-t037] p 201 N79-24921

STELLAR TEMPERATURE

The Origin of Nonradiative Heating/Momentum in Hot

Stars

[NASA-CP-2358} p 200 N85-17755

STELLAR WINDS

International Ultraviolet Explorer Atlas of O-typespectra

from 1200 to lg00 angstrom

[ NASA-RP-1155] p 204 N86-25307

STEREOPHOTOGRAPHY

Measurement of model aeroelastic deformations in the

wind tunnel at transonic speeds using

stereophotogrsmmetry

[NASA-TP-1010] p 31 N78-10048

Rapid estimation of frequency response functions by

close-range photogrammetry

[NASA-TP-24711 p 116 N86-12579

STERILIZATION

Effect of sterilization irradiation on friction and wear of

ultrahigh- motecula r-weight polyethylene

[NASA-TP-1462] p 92 N79-23216

STIFFENING

Effect of end-ring stiffness on buckling of

pressure-loaded stiffened conical shells

{NASA-TP-1079J p 127 N78-12475

Fabrication and evaluation of cold/formed/weldbrazed

beta-titanium skin-stiffened compression panels

[NASA-TP-2201 I p 89 N83-35100

Buckling loads of stiffened panels subjected to combined

longitudinal compression and shear: Results obtained with

PASCO. EAL, and STAGS computer programs

[NASA-TP-22151 p 132 N84-16585

STIFFNESS

Tire stiffness and damping determined from static and

free-vibration tests --- aircraft tires

INASA-'iP-1671 ] p 29 N80-27302

Development of in situ stiffness properties for shuffle

booster filament wound case

[NASA-TP-2377J p 83 N84-33521

Comparison of numerical techniques for integration of

stiff ordinary differential equations snsing in combustion

chemistry

INASA-TP-2372] p 51 N85-10065

STOCHASTIC PROCESSES

Optimal regulation in systems with stochastic time

sampling

INASA-TP-1743] p 184 N81-12812

Stochastic differential equations and turbulent

dispersion

I NASA-RP-1103 ] p 110 N83-22546

A stochastic model for particle impingements on orbiting

spacecraff

{NASA-TP-2550] p 184 N86-19095

STOICHIOMETRY

Preliminary tests of an advanced high-temperature

combustion system

[NASA-TP-2203] p 50 N83-33893

STOPPING POWER

Mean excitation energies for stopping powers in various

materials using local plasma oscillator strengths

[NASA-TP-2271J p 210 N84-21485

STORAGE BATrERIES

Secondary aerospace batteries and battery materials:

A biblE)graphy, 1969 o 1974

{NASA-SP-70441 p 144 N77-16437

The 1977 Goddard Space Flight Center Battery

Workshop

[NASA-CP-2041 ] p 144 N79-21565

The 11th Annual Battery Workshop

[NASA-CP-2088] p 144 N79-28669

The t982 Goddard Space Flight Center Battery

Workshop

[NASA-CP-2263] p 102 N83-35230

STORM DAMAGE

Lightning attachment patterns and flight conditions for

storm hazards, 1980

[NASA-TP-20871 p 30 N83-14077

STORMS

Proceedings of the 2nd Annual Workshop on

Meteorological and Environmental Inputs to Aviation

Systems

INASA-CP-2057] p 159 N79-17413

Summary of the NASA/MSFC FY-79 Severe Storm and

Local Weather research review --- cloud physics,

atmospheric electricity, and mesoscsie/storm dynamics

reserach

[NASA-CP-2105} p 160 N79-33722

STORMS (METEOROLOGY)

Exploratory Meeting on Atmospheric Electricity and

Severe Storms

[NASA-CP-2056] p 151 N78-29669

Third National Aeronautics and Space Administration

Weather and climate program science review

[NASA-CP-20291 p 159 N79-20575

NASA/MSFC FY-80 Atmospheric Processes Research

Review

lNASA-CP-2145} p 153 N80-28965

NASA/MSFC FY-81 Atmospheric Processes Research

Review

[NASA-CP-22041 p 164 N82-16660

STRATOSPHERE

A stability analysis of AVE-4 severe weather

soundings

[NASA-TP-2045] p 164 N83-14824

NASA/MSFC FY-82 atmospheric processes research

review

[NASA-CP-2259J p 165 N83-19391

NASA/MSFC FY-83 Atmospheric Processes Research

Review

[NASA-CP-22811 p 165 N83-33494

STRAIN GAGES

Comparison of concurrent strain gage- and pressure

transducer-measured flight loads on a lifting reentry vehicle

and correlation with wind tunnel predictions

[NASA-TP-1331J p 10 N78-33053

A modified T-value method for selection of strain gages

for measuring loads on s low aspect ratio wing

INASA-TP-1748] p 35 N81-12066

Aerodynamic force measurements with a strain-gage

balance in a cryogenic wind tunnel

[NASA-TP-2251 ] p 22 N84-13162

STRAIN RATE

Effect of strain isolator pad modulus on inplane strain

in Shuttle Orbiter thermal protection system tiles

[NASA-TP-2141] p 132 N83-33216

An update of the total-strain version of SRP

[NASA-TP-2499] p 90 N86-12295

STRATOSPHERE

Chloroflueromethanes and the stratosphere

[NASA-RP-f0t0] p 151 N77-31694

The NASA Ames Research Center one- and

two-dimensional stratospheric models Part 1: The

one-dimensional model

[NASA-TP-t002] p 158 N77-32688

The NASA Ames Research Center one- and

two-dimensional stratospheric models Part 2: The

two-dimensional model

[NASA-TP-t0031 p 158 N77-32689

Stratospheric warmings: Synoptic, dynamic and

general-circulation aspects

[NASA-RP-1017] p 158 N78-18630

Synoptic analyses, 5-, 2-, and 0 4-millibar surfaces for

July 1974 through June 1976

[NASA-RP-t023] p 158 N78-28748

An assessment of the effect of supersonic aircraft

operations on the stratospheric ozone content

[NASA-RP-1026] p 159 N78-30774

Nitric oxide production in the stratosphere within the

Space Shuttle's solid rocket motor plumes

[NASA-TP-1305] p 68 N78-33135

Lidar backscaffering measurements of background

stratospheric aerosols

INASA-TP-1381} p 152 N79-17388

The NASA-Ames Research Center stratospheric aerosol

model, 2, Sensitivity studies and comparison with

observatories

[NASA-TP-t363J p 160 N79-21720

The NASA-AMES Research Center stratospheric

aerosol model. 1 Physical processes and computational

analogs

[NASA-TP-1362} p 160 N79-21721

A coupled radiative-convective-photochemical model of

the stratosphere

[NASA-TP-14181 p 136 N79-22580

STRATCOM 8 Data Workshop and supplement

[NASA-CP-2043] p 136 N79-23461

Spatial-frequency response of the limb infrared monitor

of the stratosphere

[NASA-TP-t504J p 148 N79-29679

Programs for calculating cell parameters in electron and

X-ray diffraction --- to identity stratospheric aerosols

[NASA-TP-1529] p 148 N79-30844

The stratosphere: Present and future

[NASA-RP-t049] p 161 N80-14641

Stratospheric aerosol modification by supersonic

transport operations with climate implications

[NASA-RP-1058] p 161 N80-15726

Orbit dynamics and geographical coverage capabilities

of satellite-based solar occultation experiments for global

monitoring of stratospheric constituents

[NASA-TP-1606} p 64 N80-19142

The stratcom 8 effort --- stratospheric photochemistry

[NASA-TP-1640] p 161 N80-22924

Two-dimensional model studies of the effect of

supersonic sircraff operations on the stratospheric ozone

content

{NASA-RP-1064] p 149 N81-17622

Energetics of a sudden stratospheric warming simulated

with a three-dimensional, spectral, quasi-geostrophic

model

[NASA-TP-1847] p 163 N81-23761

SAGE measurements of the stratospheric aerosol

dispersion and loading from the Soufriere Volcano

[NASA-TP-1922] p 153 N82-12687

SAM 2 Measurements of the Polar Stratospheric

Aerosol, volume 2 April 1979 to October 1979

INASA-RP-1088-VOL-21 p 153 N82-t9734

A-115
STRATOSPHERE RADIATION SUBJECT INDEX

SAM 2 measurements of the polar stratospheric aerosol.

Volume 3: October 1979 to April 1980

[NASA-RP-1106] p 154 N83-27520

SAM 2 measurements of the polar stratospheric aerosol.

Volume 4: Apnl 1980 to October 1980

{NASA-RP-1107] p 154 N83-28796

Proceedings of a Workshop on Polar Stratospheric

Clouds: Their Role in Atmospheric Processes

[NASA-CP-23181 p 154 N84-32952

Airborne hdar measurements of El Chichon stratospheric

aerosols. October 1982 to November 1982

[NASA-RP-1136} p 155 N85-19550

SAM 2 measurements o1 the polar stratospheric aerosol.

volume 5

[NASA-RP-1140J p 155 N85-25970

SAM It measurements of the polar stratospheric aerosol.

Volume 6: April to October 1981

[NASA-RP-t 141 ] p t55 N85-27422

Airborne lidar measurements of El Chichon stratospheric

aerosols

{NASA-RP-t148] p 155 N86-13850

Present state of knowledge of the upper atmosphere:

An assessment report; processes that control ozone and

other climatically important trace gases

{NASA-RP-1162J p 156 N86-25911

Description of data on the Nimbus 7 LIMS map archive

tape: Temperature and geopotentisi height

i NASA-TP-2553J p 167 N86-25924

Airborne fidar measurements of El Chichon stratoshperic

aerosols

[ NASA-RP-1166 } p 156 N86-27835

SAM 2 measurements of the polar stratosphenc aerosol,

volume 2

[NASA-RP-t164J p 157 N86-28562

SAM 2 measurements of the polar stratospheric aerosol,

volume 8

{NASA-RP-1165] p 157 N86-29428

STRATOSPHERE RADIATION

SAM 2 measurements of the polar stratospheric aerosol,

volume 1: October to April 1979

[NASA-RP-t081] p 153 N82-t3592

STREAMLINED BODIES

A procedure for designing forebodies with constraints

On cross-section shape and axial area distribution

{NASA-TP-1881J p 17 N81-26078

STRESS ANALYSIS

Advances in engineering science, volume 1

!NASA-CP-2001-VOL-1 } p 98 N77-10230

A critical examination of stresses in an elastic single

lap ioint

[NASA-TP-15071 p 128 N79-3t626

Analysis of surface cracks in finite plates under tension

or bending loads

[NASA-TP-1578] p 129 N80-13512

Stress analysis, and buckling of J-stiffened

graphde-epoxy panel

[NASA-TP 1607] p 129 N80-18427

MEGA16 Computer program for analysis and

extrapolabon of stress-rupture data

fNASA-TP-1809] p 130 N81-23486

Elastic-plastic finite*element analyses of thermally

cycled double-edge wedge specimens

[NASA-TP-1973] p 130 N82-20566

Fracture temperature and flaw growth in nitronic 40 at

cryogenic temperatures

[NASA-TP-2312] p 89 N84-23750

Nonlinear Structural Analysis

[NASA-CP-22971 p 133 N84-31688

Mixed models and recugion techniques for

large-rotation, nonlinear analysis of shells of revolution with

application to tires

{NASA-TP-23431 p 133 N84-34773

Effect of speed and press fit on fatigue life of

roller-bearing inner-race contact

iNASA-TP-2496f p 125 N85-3t511

Star 48 solid rocket motor nozzle analyses and

instrumented firings

I NASA-TP-2572] p 68 N86-20460

STRESS CONCENTRATION

Load concentration due to missing members in planar

faces of a large space truss

[NASA-TP-1522J p 128 N79-33500

Local strain redistribution corrections for 8, simplified

inelastic analysis procedure based on an elastic

finite-element analysis

{NASA-TP-2421 } p 134 N85-20396

STRESS CORROSION

A mechanical probeily and stress corrosion evaluation

of VIM-ESR-VAR work strengthened and direct double

aged Inconel 718 bar material

[NASA-TP-2634] p 68 N86-30753

STRESS INTENSITY FACTORS

Stress-concentration factors for finite orthotropic

laminales with a pin-loaded hole

i NASA-TP-1862 I p81 N81-24178

A cracked orthotropic sheet stiffened by a semi-infinite

orthotropic sheet

{NASA-TP-2455] p 134 N85-32339

STRESS RATIO

Stress-concentration factors for finite orthotropic

laminates with a circular hole and uniaxial loading

[NASA-TP-1469] p 80 N79-23140

STRESS-STRAIN RELATIONSHIPS

Tensile stress-strain behavior of boron/aluminum

laminates

[NASA-TP-1117] p 79 N78-18t35

Comparison of elastic and elastic-plastic structural

analyses for cooled turbine blade airfoils

[NASA-TP-1679] p 129 N80-27719

Elastic-plastic finite-element analyses of thermally

cycled single-edge wedge specimens

[NASA-TP.1982] p 130 N82-20565

Elastic-plastic finite-element analyses of thermally

cycled double.edge wedge specimens

{NASA-TP-1973] p 130 N82-2056G

Buckling and failure characteristics of graphite-polyimide

shear panels

{NASA-TP-2153] p 82 N83-24561

Simplified method for nonlinear structural analysis

[NASA-TP-22oa] p 132 N83-34372

Development of a simplified procedure for cyclic

structural analysis

INASA-TP-2243] p 133 N84-20878

Local strain redistribution corrections for a simplified

inelastic analysis procedure based on an elastic

finite-element analysis

[NASA-TP-2421] p 134 N85-20396

Hertzian contact in two and three dimensions

[NASA-TP-2473] p 125 N85-32331

STRESS-STRAIN-TIME RELATIONS

Long-time creep behavior of the tantalum alloy Aster

811C --- as a function of stress, temperature, and grain

size

{NASA-TP-1691] p 87 N80-32489

STRESSES

A new look at numerical analyses of free-edge stresses

in composite laminates

[NASA-TP-1751] p 130 N81-13373

STRINGERS

Fabrication and evaluation of brazed titanium-clad

borsic/aluminum skin-stringer panels

INASA-TP-1674} p 82 N83-28098

A cracked orthotropic sheet stiffened by e semi-infinite

orlhotropic sheet

[NASA-TP-2455] p 134 N85-32339

STRINGS

Modal analysis of a nonuniform string with end mass

and variable tension

{NASA-TP-2198} p 67 N83-32826

STRUCTURAL ANALYSIS

Standardization. certification, maintenance, and

dissemination of large scale engineering software

systems

(NASA-CP-2015] p 178 N77-33876

Sixth NASTRAN Users' Colloquium

[NASA-CP-2018] p 127 N78-12443

Ferrographic analysis of wear particles from sliding

elestohydrodynamic experiments

[NASA-TP-1230] p 119 N78-22377

Seventh NASTRAN Users Colloquium

[NASA*CP-2062} p 127 N78-32466

Guide to a condensed form of NASTRAN

[NASA-RP-1019] p 178 N78-33791

Comparison of elastic and elesbc-plastic structural

analyses for cooled turbine blade airfoils

[NASA-TP-1679] p 129 N80-27719

Research in nonlinear structural and solid mechamcs

[NASA-CP-2147J p 129 N80-32756

Ninth NASTRAN Users' Colloquium

[NASA-CP-2151] p 129 N80-33782

The 1980 Large space systems technology. Volume

2: Base technology

[NASA-CP-2168-VOL-2] p 66 N81-19196

Computational Aspects of Heat Transfer in Structures

{NASA-CP-2216] p 109 N82-23473

Studies of implicit and explicit solution techniques in

transient thermal analysis of structures

{NASA-TP-2038] p 110 N82-31646

Research in structural and solid mechanics, 1982

INASA-CP-2245] p 131 N82-33739

Matenals consbtutive models for nonlinear analysis of

thermally cycled structures

INASA-TP-2055] p 131 N83-12449

Tenth NASTRAN User's Colloquium

{NASA-CP-2249] p 13t N83-t2452

Determination of airplane model structure from flight data

using splines and stepwise regression

[NASA°TPo2126J p 57 N83-19758

Simplified method for nonlinear structural analysis

{NASA-TP-2208] p 132 N83-34372

Eleventh NASTRAN User's Colloquium

I NASA-CP-2284 ] p 132 N84-15590

Structural efficiency studies of corrugated compression

panels with curved caps and beaded webs

{NASA-TP-2272] p 132 N84-18675

The NASTRAN theoretical manual

[NASA-SP-221(O6)I p 132 N84-18677

Development of • simplified procedure for cyclic

structural analysis

INASA-TP-2243J p 133 N84-20878

The NASTRAN user's manual

{NASA-SP-222(06)J p 133 N84-21899

Nonlinear Structural Analysis

INASA-CP-2297] p 133 N84-31688

Twelfth NASTRAN Users' Colloquium

INASA-CP'2328] p 133 N84-32864

Reduction method for thermal analysis of complex

aerospace structures

INASA-TP-2373] p 1t2 N85-16066

Thirteenth NASTRAN Users' Colloquium

[NASA-CP-2373] p 134 N85-25863

Turbine Engine Hot Section Technology (HOST)

[NASA-CP-2289J p 135 N86-11495

Integrated Composite Analyzer (ICAN): Users and

programmers manual

[NASA-TP-2515] p 83 N86-21614

The NASTRAN demonstration problem manual, level

17.5

[NASA-SP-224(05)] p 130 N81-71592

The NASTRAN programmers manual, level 17.5

{NASA-SP-223(05)J p 130 N81-71594

STRUCTURAL DESIGN

Aerodynamic charactenstics at Mech numbers from 033

to 1 20 of a wing-body design concept for a hypersonic

research airplane

{NASA-TP-1044] p 6 N78-12038

A theoretical investigation of forebody shapes designed

for natural laminar boundary-layer flow

INASA°TP-1375] p 11 N79-15903

Recent Advances in Structures for Hypersonic Flight,

part I --- conferences

INASA-CP-2065-PT-1] p 128 N79-21422

Determination of airplane model structure from flight data

by using modified stepwise regression

[NASA-TP-1916] p 56 N82-10041

Large Space Antenna Systems Technology, part 1

[NASA-CP-2269-PT-1 J p 67 N83-26853

Get away special experimenter's symposium

[NASA-CP-23241 p 63 N84-27758

ACEE Composite Structures Technology: Review of

selected NASA research on composite matenels and

structures

{NASA-CP-2321 j p 83 N84-29969

STRUCTURAL DESIGN CRITERIA

Aerodynamic and directional acoustic performance of

a scoop inlet

[NASA-TP-t028] p 41 N77-31152

Approximation methods for combined thermal/structural

design

I NASA-TP-1428 ] p 128 N79-25427

Preliminary vibration, acoustic, and shook design and

test criteria for components on the Lightweight External

Tank (LWT)

[NASA-RP-1074] p 71 N81-19218

System analysis approach to deriving design criteria

(loads) for Space Shutlle and its payloads. Volume 1:

General statement of approach

[NASA-TP-1949} p 66 N82-14203

System analysis approach to deriving design criteria

(Loads) for Space Shuttle and its payloads. Volume 2:

Typical examples

INASA-TP-1950] p 66 N82-15106

Large space systems technology, 1981 ---

conferences

INASA-CP-2215-PT-1 ] p 66 N82-18275

Application of a computerized vibroaeoustic data bank

for random vibration criteria development

[NASA.TP-1998] p 73 N82-20238

Nonlinear Constitutive Relations for High Temperature

Applications

INASA-CP-2271 J p 132 N83-34351

Eleventh NASTRAN User's Colloquium

{NASA-CP-2284J p 132 N84-15590

Technical Workshop: Advanced Helicopter Cockpit

Design

I NASA-CP-2351 J p 31 N85-t4806

Technology for large space systems: A bibliography with

indexes (supplement 14)

INASA-SP-7046(14)] p 63 N86-28104

STRUCTURAL ENGINEERING

Advances in engineering science, volume 2

[NASA-CP-2001-VOL-2) p 98 N77-10265

Lessons of the NASA Tech House

I NASA-SP-442 J p 199 N80-27219

Research in nonlinear structural and solid mechanics

[NASA-CP-2147-SUPPL) p t30 N82-11489

A-116
SUBJECT INDEX SUPERCRITICAL WINGS

STARS: A general-purpose finite element computer

program for enaly_s of engineering structures

[NASA-RP-1129] p 134 N85-11378

BTRUCTURAL FAILURE

Buckling and structural efficiency of sandwich-blade

stiffened composite compression panels

[ NASA-TP- 1289 ] p 127 N78-32492

Validation of an Active Gear, Flexible Aircraft Take-off

and Landing analysis (AGFATL)

[NASA-TP-2353] p 37 N84-32378

STRUCTURAL MEMBERS

Interactive design and analysis of future large spacecraft

concepts

[NASA-TP-1937] p 72 N82-t4276

Eleventh NASTRAN User's Colloquium

[NASA-CP.2284] p 132 N84-15590

STRUCTURAL PROPERTIES (GEOLOGY)

Volcanic features of Hawaii. A basis for comparison

with Mars

[NASA-SP-403] p 152 N80-23912

Planetary geology in the 1980s

[NASA-SP-487] p 200 N85-23457

Global Mega-Geomorphology

[NASA-CP.2312] p 137 N85-32357

STRUCTURAL STABILITY

Elastic constants for suporplastically

focmed/diffusion-bonded corrugated sandwich core

[NASA-TP-1562] p 129 N80-23677

Fourteenth NASTRAN Users' Colloquium

{NASA.CP.2419] p 135 N86-25823

Impact data from a transport aircraft during a controlled

impact demonstration

[NASA-TP-2589] p 38 N66-30721

STRUCTURAL STRAIN

A solution procedure for behavior of thick plates on a

nonlinear foundation and postbuokling behavior of long

plates

[NASA-TP-2174] p 132 N83-34373

STRUCTURAL VIBRATION

Space shuttle active-pogo-suppressor control design

using linear quadratic regulator techniques

[NASA-TP.1217J p 101 N79-14309

Hydroelastic vibration analysis of partially liquid-filled

shells using a series representation of the liquid

[NASA-TP-1558J p 129 N80-19563

A new measurement method for separating airborne and

structurebome noise radiated by aircraft type panels

[NASA-TP-20791 p 189 N83-11838

Vibration studios of a lightweight three-sided membrane

suitable for space application

[NASA-TP-2095J p 131 N83-16785

STRUTS

Longitudinal aerodynamic characteristics st Mach 0.60

1o 2.86 of a fighter configuration with strut braced wing

[NASA-TP-11021 p 7 N78-16000

STUDENTS

Skylab, classroom in space

[NASA-SP-401| p 65 N77-29189

• LIBCRITICAL FLOW

Experimental and analytical study of the longitudinal

aerodynamic characteristics of analytically and empirically

designed Strske-wing configurations at subcritical

speeds

[NASA-TP-1803] p 17 N61-25040

SUBMILLIMETER WAVES

Large Deployable Reflector Science and Technology

Workshop Volume 3: Systems and Technology

Assessment

[NASA-CP-2275-VOL-31 p 202 N84-32318

Submillimeter local oscillators for speceborne

heterodyne applications

[NASA-RP-1147] p 76 N85-30005

SUBROUTINES

An improved viscous characteristics analysis program

[NASA-TP-1289] p 106 N81-12356

SUBSONIC AIRCRAFT

Wind tunnel investigation of an all flush orifice air data

system for a large subsonic aircraft --- conducted in s

Langley 8 foot transonic pressure tunnel

[NASA-TP-1642] p 38 N80-23304

SUBSONIC FLOW

Induced velocity field of a let in a crossflow

[NASA-TP-1087] p 105 N78-26392

Viscous-inviscid calculations of jet entrainment effects

on the subsonic flow over nozzle afterbodies

[NASA-TP-1626] p 14 N80-22261

Static and dynamic pressure measurements on a NACA

0012 airfoil in the Ames High Reynolds Number Facility

[NASA-TP-2485} p 26 N85-27823

Pressure probe and hot-film probe rsponsas to acoustic

excitation in mean flow

[NASA-TP-2581 ] p 191 N86-27043

SUBSONIC FLUTTER

Effects of wing loading-edge flap deflections on subsonic

longitudinal aerodynamic characteristics of a wing-fusaioge

configuration with a 44 dog swept wing

[NASA.TP.1351] p 10 N79.13002

Generalization of the subsonic kernel function in the

s-plane, with applications to flutter analysis

[NASA.TP.2292] p 23 N84.20480

SUBSONIC SPEED

Effect of wingiots on a first-generation jet transport wing

5: Stability characteristics of a full-span wing with s

generalized fuselage at high subsonic speeds

[NASA.TP.1163] p 8 N78-20081

Aerodynamic characteristics at Mech number 02 of •

wing-body concept for a hypersonic research airpione

[NASA-TP-1169] p 8 N78-25059

Subsonic dynamic stability characteristics of two

close-coupled canard-wing configurations

[NASA-TP-1291] p 9 N78-33050

Fluctuating surface pressure and acoustic radiation for

subsonic normal jet impingement

[NASA-TP-1361 ] p 186 N79-t9813

Longitudinal aerodynamic characteristics of a

vectored.engine.over.wing configuration at subsonic

speeds --- Langley V/STOL tunnel tests

[NASA-TP-1533] p 12 N79-33164

Effect of winglets on a first-generation jet transport wing

6: Stability characteristics for a full-span model at subsonic

speeds --- conducted in Langley 8 foot transonic pressure

tunnel

[NASA-TP-1330] p 12 N80-10101

Estimation of attainable leading-edge thrust for wings

at subsonic and supersonic speeds

[NASA-TP-1500] p 12 N80-10105

Investigation of the flow field surrounding circular-arc

bosttail nozzles st subsonic speeds

(NASA-TP-1633] p 14 N80-22262

Use of nose cap and fuselage pressure orifices for

determination of air data for space shuttle orbiter below

supersonic speeds

[NASA-TP-1643] p 39 N80-32389

Subsonic tests of an all-flush-pressure-orifice air data

system

[NASA-TP-1871] p 39 N81-26144

SUBSONIC WIND TUNNELS

Aeronautical facilities catalogue. Volume 1: Wind

tunnels

[NASA-RP-1132J p 60 N65-18991

SUBSTRATES

Textured carbon on copper: A novel surface with

extremely low secondary electron emission

characteristics

{NASA-TP-2543] p 96 N86-15394

SUBSTRUCTURES

Full-scale crash-test evaluation of two load-limiting

subfloors for general aviation airframes

{NASA-TP-23801 p 134 N85-13267

SUCTION

Performance of a vortex-controlled diffuser in an annular

swirl-can combustor at inlet Mech numbers up to 0.53

[NASA-TP-1452] p 44 N79-22099

Survey and bibliography on attainment of laminar flow

control in air using pressure gradient and suction, volume

1

[NASA-RP-1035] p 107 N79-33438

Amplified crossflow disturbances in the laminar boundary

layer on swept wings with suction

[NASA-TP-1902] p 109 N82-11391

Calibration of sonic valves for the laminar flow control,

leading-edge flight test

[NASA-TP-2423] p 26 N85-23707

SULFATES

Sulfate and nitrate collected by filter sampling near the

tropopause

{NASA-TP-1567J p 149 N60-14581

SULFIDES

Solubility, stability, and electrochemical studies of

sulfur-sulfide solutions in organic solvents

[NASA-TP-1245i p 144 N78-28624

SULFUR DIOXIDES

Carbon-catalyzed oxidation of SO2 by NO2 and air

[NASA-TP-2014J p 85 N82-22330

SULFUR OXIDES

An ultraviolet video technique for visualization of stack

plumes and for measuring sulfur dioxide concentration and

effluent velocity

[NASA.TP-1014] p 147 N77-32622

SULFURIC ACID

Experimental study of cluster formation in binary mixture

of H20 and H2SO4 vapors in the presence of an ionizing

radiation source

|NASA-TP-1735] p 149 N81-t1565

Friction and wear of iron in sulfuric acid

[NASA-TP-2289] p 89 N64-21716

Friction and wear of nickel in sulfuric acid

{ NASA-TP-2290] p89 N84-21721

Rapid estimation of concentration of aromatic classes

in middistiliste fuels by high-performance liquid

chromatography

[NASA.TP.2495] p 98 N85.31307

SUN

Sun, weather, and climate

[NASA-SP-426] p 209 N79.20961

Study of the Solar Cycle from Space

[NASA-CP-2096] p 209 N80-17944

The Sun as a star

[NASA-SP-450] p 203 N81-27006

A comparatwe look st sunspot cycles

[NASA-TP-2325] p 209 N84-24520

Solar Terrestrial Physics: Present and Future

[NASA-RP-1120] p 200 N84-34332

Local Interstellar Medium. International Astronomical

Union Colloquium No. 81

[NASA.CP-2345| p 204 N85.15539

SUNLIGHT

Intensity and absorbed-power distribution in a cylindrical

solar-pumped dye laser

[ NASA-TP-2321 ] p 118 N84-23878

SUNSPOT CYCLE

A comparative look at sunspot cycles

[NASA-TP-2325] p 209 N84-24520

SUPERCONDUCTIVITY

A study of production of misibility gap alloys with

controlled structures

[NASA-TP-2144] p 196 N83-21991

SUPERCRITICAL FLOW

Influence of oil-squeeze-film damping on steady-state

response of flexible rotor operating to supercritical

speeds

[NASA*TP-1094] p 41 N78-13064

Pressure and force data for a flat wing and a warped

conical wing having a shockless recompression at Mach

1.62

[NASA-TP-1759] p 17 N81-22016

Static and dynamic pressure measurements on a NACA

0012 airfoil in the Ames High Reynolds Number Facility

[NASA-TP-24851 p 26 N85-27823

SUPERCRITICAL PRESSURES

Flight measurements of surface pressures on a flexible

supercritical research wing

[NASA-TP-2501] p 27 N86-20350

SUPERCRITICAL WINGS

Fhght evaluation of the transonic stability and control

characteristics of an airplane incorporating a supercritical

wing

[NASA-TP-1167] p 53 N78-20140

Flight-measured buffet characteristics of a supercriticat

wing and a conventional wing on s variable-sweep

airplane

[NASA-TP-1244) p 8 N78-23056

Theoretical estimation of the transonic aerodynamic

characteristics of a supercritical-wing transport model with

trailing-edge controls

lNASA-TP-1253] p 9 N78-30056

Flight comparison of the transonic agility of the F-111A

airplane and the F-111 supercritical wing airplane

[NASA-TP-1368] p 54 N79-13056

The design of supercritical wings by the use of

three-dimensional transonic theory

[NASA-TP-1400] p 11 N79-16604

Advanced aerodynamics and active controls, Selected

NASA research

[NASA-CP-21721 p3 N81-19001

Low-speed aerodynamic performance of a

high-aspect-ratio supercritical-wing transport model

equipped with full-span slat and pad-span double-slotted

flaps

[NASA-TP-1580] p 19 N82-15015

Longitudinal and lateral static stability and control

characteristics of a 1/6-scale model of a remotely piloted

research vehicle with a supercritical wing

[NASA-TP-13601 p 57 N82-15075

Experimental study of wing leading-edge devices for

improved maneuver performance of a supororitical

maneuvenng fighter configuration --- Langley 7- by 10-it

high speed tunnel tests

[NASA-TP-2125J p 21 N83-22162

Low-speed aerodynamic performance of an

aspect-ratio- 10 supercritical-wing transport model

equipped with a full-span slat and part-span and full-span

double-slotted flaps

[NASA-TP-1805] p 21 N83-30390

An experimental investigation of nacelle-pylon

installation on an unswept wing at subsonic and transonic

speeds

[NASA-TP-2246J p 23 N84-18162

Experimental trim drag values and flow-field

measurements for a wide-body transport model with

conventional and supercritical wings

[NASA-TP-2071J p 25 N85-10920

A-117
SUPERGIANT STARS SUBJECT INDEX

Low-speed tests of a high-aspect-ratio,

supercritical-wing tranSpOrt model equipped with a high-lift

flap system in the Langley 4- by 7-meter end Ames 12-foot

pressure tunnels

INASATP2097] p 26 N85-31010

Effect of aileron deflections on the aerodynamic

characteristics of a semispan model of a subsonic

energy-eff=cient transport

(NASA-TP-2478] p27 N86-11t86

Installation effects of long-duct pylon-mounted nacelles

on a twin-let transport model with swept supercritical

wing

I NASA-TP-2457] p 27 N66-20346

Flight measurements of surface pressures on a flexible

supercritical research wing

I NASA-TP-2501 ] p 27 N66-20350

Supercriticat wing technology: A report on flight

evaluations

[NASA-SP-801 J p 6 N77-85474

SUPERGIANT STARS

B Stars with and without emission lines, parts 1 and 2

INASA-SP-456] p 200 N82-25027

SUPERNOVA REMNANTS

An emission-line survey of the Milky Way

I NASA-SP-434] p 201 N80-11966

SUPERPLASTIClTY

Elastic constants for superplastically

formed/diffusion-bonded corrugated sandwich core

I NASA-TP-1562] p t29 N80.23677

Elevated temperature behavior of superplastically

formed/weld-brazed titanium compression panels having

advanced shaped stiffeners

LNASA-TP-2123] p 88 N83-19889

Fabrication and evaluation of superplastically

formed/weld-brazed corrugated compression panels with

beaded webs

INASA-TP-2512] p 90 N86-13406

SUPERSONIC AIRCRAFT

Proceedings of the SCAR Conference, part 1

t NASA-CP-00t-PT-1 ] p 1 N77-17996

Proceedings of the SCAR Conference. pert 2

[NASA-CP-001-PT-2] p 1 N77-16019

Theoretical estimation of the transonic aerodynamic

characteristics of a supercritical-wing transporf model with

trailing-edge controls

j NASA-TP- 1253) p 9 N76-30056

Application of supersonic linear theory and hypersonic

impact methods to three nonslender hypersonic airplane

concepts at Math numbers from 1.10 to 2.86

INASA-TP-1539] p 13 N80-12065

Experimental and theoretical aerodynamic

characteristics of two hypersonic cruise aircraff concepts

at Math numbers of 2.96, 3.96, and 4.63

[NASA-TP-17671 p 16 N81-12021

A simulator study for the development and evaluation

of operating procedures on a supersonic cruise research

transport to minimize airport-community no_sa

[NASA-TP-1742] p 29 N81-12043

Two-dimensional model studies of the effect of

supersonic aircraft operations on the stratospheric ozone

content

[NASA-RP-1064] p 149 N81-17622

Experimental and analytical investigation of

axlsymmetrlc supersonic cruise nozzle geometry at Mach

numbers from 060 to 1 30

[NASA-TP-1953I p 19 N62-14052

Noise and economic characteristics of an advanced

blended supersonic transport concept

[NASA-TP2073) p 4 N82-31294

Effect of fuselage upwash on the supersonic longitudinal

aerodynamic characteristics of 2 fighter configurations

[NASA-TP-23301 p 24 N84-27676

Effect of underwing aft-mounted nacelles on the

]ongitudinsi aerodynamic charactehstics of a high-wing

transport airplane

INASA-TP-2447] p 27 N86-20345

Aerodynamic characteristics of a supersonic fighter

a_rcraft model at Mech 0.40 to 2.47

I NASA-TP-2580] p 28 N86-23561

Low-speed performance of an axisymmetric,

mixed-compression, supersonic inlet with auxiliary inlets

I NASA-TP-2557] p 52 N86-24694

SUPERSONIC AIRFOILS

Supersonic wings with significant leading-edge thrust at

cruise

JNASA-TP-1632] p 14 N80-21279

The highspeed frontter Case histones of four NACA

programs, t920- 1950

I NASA-SP-445} p 3 N81-15969

Wing planform effects at supersonic speeds for an

advanced fighter configuration

I NASA-TP-2269} p 23 N64-20486

Experimental and theoretical study of the longitudinal

aerodynamic characteristics of delta and double-delta

wings at Mach numbers of 1,60. 1,90, and 2.16

INASA-TP-2433} p 26 N65-29922

Effect of leading-edge load constraints on the design

and performance of supersonic wings

[NASA-TP-2446] p 26 N85-29923

SUPERSONIC BOUNDARY LAYERS

Wind-tunnel measurements and comparison with flight

of the boundary layer and heat transfer on a hollow cylinder

at Mach 3

[NASA-TP-1789] p 16 N81-14975

Pressure and heating-rate distributions on a corrugated

surface in a supersonic turbulent boundary layer

[NASA-TP-1024] p 111 N84-10504

SUPERSONIC COMBUSTION

Combustion of hydrogen in a two-dimensional duct with

step fuel injectors

[NASA-TP-1159] p 42 N78-23093

Interaction between step fuel injectors on opposite walls

in a supersonic combuslor model

[NASA-TP-1174 ] p42 N76-23094

An improved viscous characteristics analysis program

[NASA-TP-1289] p 108 N61-12356

SUPERSONIC COMBUSTION RAMJET ENGINES

Interaction between step fuel injectors on opposite walls

in a supersonic combustor model

(NASA-TP-1174} p 42 N78-23094

Criteria for self-ignition of supersonic hydrogen-air

mixtures

[NASA-TP-1457} p 45 N79-29192

Conceptual model of turbulent flameholding for scramjet

combustors

[NASA-TP-1543] p 47 N60-33409

Evaluation of a bulk calorimeter and heat balance for

determination of supersonic combustor efficiency

[NASA-TP.1739] p 48 N81.t3058

Numerical analysis of the scramjet-inlel flow field by

using two-dimensional Navier-Stokes equations

[NASA-TP-1940] p 48 N82-13142

Expanded operational capabilities of the Langley Mach

7 Scrsmjet test facility

[NASA-TP-2186J p B0 N83-36039

SUPERSONIC CRUISE AIRCRAFT RESEARCH

Bibliography of Supersonic Cruise Aircraft Research

(SCAR)

[NASA-RP-10031 p 197 N78-12895

YF-12 experiments symposium, volume 1

[NASA-CP-2054-VOL-1 I p 9 N78-32055

Theoretical evaluation of high-speed aerodynamics for

arrow-wing configurations

[NASA-TP-1358I p 10 N79-14023

Fluctuating loads measured on an over-the-wing

supersonic jet model

[NASA-TP-13661 p 166 N79-16641

Bibliography of Supersonic Cruise Research (SCR]

program from 1977 to mid-1980

[NASA-RP-1063] p 16 N81-14973

Supersonic Cruise Research 1979, part 1

[NASA-CP-2106-PT-1 J p 3 N81-17981

Supersonic Cruise Research 1979, part 2 --- airframe

structures and materials systems integration+ economic

analysis

(NASA-CP-2108-PT-2] p 3 N61-18005

Charts for determining potential minimum sonic-boom

overpressures for supersonic cruise aircraft

INASA-TP-1B20] p 17 N81-21016

Compression panel studies for supersonic cruise

vehicles

[NASA-TP-1617] p 82 N83-26099

Investigation of installation effects on twin-engine

convergent-divergent nozzles

[NASA-TP-2205] p 22 N84-13152

Supersonic cruise technology

[NASA-SP-472] p 4 N85-28912

SUPERSONIC DRAG

Experimental and theoretical aerodynamic

characteristics of two hypersonic cruise aircraft concepts

at Mach numbers of 2.96, 3.96, and 4.63

[NASA-TP-1767] p 16 N81-12021

SUPERSONIC FLIGHT

Supersonic aerodynamic characteristics of a Sparrow

3 type missile model with wing controls and comparison

with existing tail=control results

_NASA-TP-t078] p 6 N78-1204t

Effects of varying podded nacelle-nozzle installations

on transonic aeropropulsive characteristics of a supersonic

fighter aircraft

INASA-TP-2120] p 21 N83-26821

Bibliography of Supersonic Cruise Research (SCR)

program from 1980 to 1963

{NASA-RP-1117] p 24 N64-27674

Supersonic cruise technology

[NASA-SP472] p 4 N85-26912

SUPERSONIC FLOW

Forebody and afterbody solutions of the Navier-Stokes

equations for supersonic flow over blunt bodies in a

generalized orthogonal coordinate system

[NASA-TP-t075J p 104 N78-18362

Wind-tunnel investigation at Mech numbers frOm t.90

to 2.86 of • csnerd-controUed missile with ram.air.jet

spoiler roll control --- in the Langley Unitary Plan Wind

Tunnel

{NASA-TP-1124] p 7 N78-20079

Comparison of two computer programs by predicting

turbulent mixing of helium in a ducted supersonic

airstream

[NASA-TP-1166] p 105 N78-22333

Turbulent-flow separation criteria for overexpanded

supersonic nozzles

[NASA-TP-1207] p t05 N78-30554

Application of a numerically generated orthogonal

coordinate system to the solution of inviscid axisymmetrie

supersonic flow over blunt bodies

[NASA-TP-1619] p 14 N60-19031

Effect of Reynolds number on stability characteristics

of a cruciform wing-body

[NASA-TP-1883] p 15 N80-27283

Steady and nonsteady supersonic turbulent afterbody

flow

[NASA-TP-1769] p 16 N61-16977

Numerical simulabon of steady supersonic flow --- spatial

marching

[NASA-TP-1749] p 17 N61-22018

Crossflow effects on steady and fluctuating pressures

on an ogiva-cylinder cone-frustum model in supersonic

separated flow

[NASA-TP-1951] p 16 N82.13108

The wedge hot-film anemometer in supersonic flow

[NASA-TP-2134] p 189 N63.30164

Wind-tunnel investigation of leading-edge thrust on

arrow wings in supersonic flow

[NASA-TP-2167] p 21 N83-31577

Effect of thrust vectoring and wing maneuver devices

on transonic aeropropulsive characteristics of a supersonic

fighter

[NASA-TP-2119] p 22 N84-10025

An analysis of shock coalescence including

three-dimensional effects with application to sonic boom

extrapolation

I NASA-TP.2214] p 111 N84.22906

Experimental and theoretical study of the longitudinal

aerodynamic characteristics of delta and double-delta

wings at Mach numbers of 1.60, 1.90, and 2.16

[NASA-TP-2433] p 26 N65.29922

Effect of leading-edge load constraints on the design

and performance of supersonic wings

{NASA-TP-2446] p 26 N85-29923

SUPERSONIC FLUTFER

Analysis of supersonic stall bending flutter in axial-flow

compressor by actuator disk theory

[NASA-TP-1345] p 10 N79-13003

SUPERSONIC INLETS

A throat-bypass stability-bleed system using relief valves

to increase the transient stability of a mixed-compression

inlet --- YF-12 aircraft inlet tasls in the Lewis 10 by 10 ft

supersonic wind tunnel

[NASA-TP-t083] p 45 N79-28176

Dynamic response of a Mach 2.5 axisymrne_c inlet and

turbojet engine with a poppet-value controlled inlet stability

bypass system when sublected to internal and external

airflow transients

[NASA-TP-1531 ] p 45 N80-14123

Turbojet-exhaust-nozzle sacondary-airfiow pumping as

an exit control of an inlet-stability bypass system for a

Mach 2.5 axiaymmetric mixed-compression inlet --- Lewis

10- by 10-fl. supersonic wind tunnel test

[NASA-TP-1532] p 46 N80-14124

Low-speed performance of an axisymmetfic,

mixed-compressK)n, supersonic inlet with auxiliary inlets

[NASA-TP-2557] p 52 N86-24694

SUPERSONIC JET FLOW

Supersonic jet noise generated by large scale

instabilities

INASA-TP-2072] p 168 N82-3418g

SUPERSONIC NOZZLES

Turbulent-flow separation critena for overexpended

supersonic nozzles

[NASA-TP-1207] p 105 N78-30554

Effects of varying podded nacelle-nozzle installations

on transonic aeropropulsive characteristics of a supersonic

fighter aircraft

[NASA-TP-2120] p 21 N63-26821

SUPERSONIC SPEED

Proceedings of the SCAR Conference, part 1

[NASA-CP-001-PT-t ] p 1 N77-17996

Effects of roughness size on the position of

boundary-layer transition and on the aerodynamic

characteristics of a 55 deg. swept delta wing at supersonic

speeds

[NASA-TP-1027] p 7 N78-13016

Effects of stores on longitudinal aerodynamic

characteristics of a fighter at supersonic speeds

[ NASA-TP-t 175] p 6 N78-22026

A-118
SUBJECTINDEX SYMBOLS

Wind-tunnel investigation at supersonic speeds of a

canard-controlled missile with fixed and free-rolling tall

fins

[NASA-TP.1316] p 9 N78-32087

Estimation of idadlng-eqge thrust for supersonic wings

of arbitrary plsnform

[NASA-TP.1270] p g N78o33051

An experimental wind-tunnel Investigation of a

rim-air-spoiler roll-control device on a forward-control

missile at supersonic speeds

[NASA-TP-1353] p 11 N7g-1760g

Estimation of attainable teedlng-eqge thrust for wings

It subsonic end supersonic speeds

[NASA.TP.1500] p 12 NS0-10105

Investigation of flow charactedstlce over missile bodies

at supersonic speeds

[NASA-TP-f57g] p 13 N80-13001

Estimation of wing nonlinear aerodynamic

characteristics at supersonic speeds

[NASA-TP-1718] p 15 N81-10004

Wing.alone aerodynamic characteristics for high angles

of attack of supersonic speeds

[NASA-TP-1869] p 18 N81.30087

Experimental investigation of leading-edge thrust at

supersonic speeds

[NASA.TP.2204] p 22 N83-34905

Supersonic aerodynamic characteristics of canard,

tailless, and aff-tsil configurations for 2 wing planforms

[NASA-TP-2434] p 26 N85-27822

Supersonic cruise technology

[NASA-SP-4721 p 4 N85-28912

Lee.side flow over delta wings at supersonic speeds

[NASA-TP.2430] p 26 N85-29921

SUPERSONIC TRANSPORTS

Ground-based and in-flight simulator studies of

low-speed handling characteristics of two supersonic

cruise transport concepts

[NASA-TP-1240] p 32 N78-27111

An assessment of the effect of supersonic aircraft

operations on the stratospheric ozone content

[NASA-RP-1026] p 159 N78.30774

Wind-tunnel investigation of the validity of a

sonic.boom-minimization concept -- Langley Unitary Plan

Wind Tunnel tests for supersonic transport design

[NASA-TP-1421] p 12 N80-10102

Stratospheric aerosol modification by supersonic

_anaport operations with climate implications

[NASA-RP-1058] p 161 N80-15726

Theoretical and experimental investigation of supersonic

aerodynamic characteristics of a twin-fuselage concept

[NASA-TP-2184] p 22 N83-32776

Bibliography of Supersonic Cruise Research (SCR)

program from 1980 to 1983

[NASA-RP-t 117] p24 N84-27674

Supersonic cruise technology

[NASA-SP-472] p 4 N85-28912

SUPERSONIC TURBINES

Performance of a transonic fan stage designed for a

low meridionsi velocity ratio

[NASA-TP-1298] p 43 N78-33107

SUPERSONIC WIND TUNNELS

Noise reduction in a Mech 5 wind tunnel with a

rectangular rod-wall sound shield

[NASA-TP-1672] p 108 N80-26622

Effect of Reynolds number on stability characteristics

of a cruciform wing-body

[NASA-TP-1683] p 15 N80-27283

Description end calibration of the Langley unitary plan

wind tunnel

[NASA-TP-1905J p 18 N82-12035

Wind-Tunnel/Flight Correlation, 1961

[NASA-CP-2225] p 19 N82-25196

Free-stream noise and transition measurements on a

cone in a Mech 3.5 pilot low-disturbance tunnel

[ NASA-TP-2180] p 111 N83-34229

Aeronautical facilities catalogue. Volume 1: Wind

tunnels

[NASA-RP-1132] p 60 N85-18991

SUPERSONICS

Application of supersonic linear theory and hypersonic

impact methods to three nonslendar hypersonic airplane

concepts st Mach numbers from 1.10 to 2.86

[NASA-TP-1539] p 13 N80-12065

Effect of tail-fin span on stability and control

characteristics Of a Canard-controlled missile at supersonic

Math numbers

[NASA-TP-2157] p 21 N83-27959

Supersonic cruise technology

[NASA-SP-472] p 4 N85-28912

SUPPLEMENTS

NASA Thesaurus supplement: A 3-part cumulative

supplement to the 1962 edition of the NASA Thesaurus

[NASA-SP-7051(SUPPL-2)] p 198 N85-12785

SURFACE CRACKS

Analysis of surface cracks in finite plates under tension

or bending loads

[NASA-TP.1578] p 129 N80-f3512

SURFACE DEFECTS

Elastohydrodynamic contacts, Effects of dents and

grooves on traction end local film thickness

[NASA.TP.2175] p 123 N83.28453

SURFACE ENERGY

Relationship between the _dsel tensile strength and the

friction properties of metals in contact with nonmetals and

themselves

[NASA.TP.1883J p 94 N81-33293

SURFACE FINISHING

Morphology of gold and copper ion-plated coatings

[NASA-TP-1262] p 86 N78.26199

Improved adherence of sputtered titanium carbide

coatings on nickel- and titanium-base siioys

[NASA-TP.14501 p 78 N79-22194

SURFACE GEOMETRY

Sonic-boom minimization with nose.bluntness

relaxation

[NASA-TP-1348] p 10 N79-15000

Semianalylic modeliog of aerodynamic shapes

[NASA-TP-24131 p 25 N85-21120

SURFACE PROPERTIES

Geometric relationships for homogenization in

single-phasa binary alloy systems

[NASA-TP-t349] p 87 N79-13137

Friction and wear with a siogle-crystal abrasive grit of

silicon carbide in contact with iron base binary alloys in

oil: Effects of alloying element and its content

(NASA-TP-1394J p 120 N79-17227

Evaluation of high-contact-ratio spur gears with profile

modification

[NASA-TP-14581 p 120 N79-31604

Surface chemistry and friction behavior of the silicon

carbide (0001) surface st temperatures to 1500 deg C

[NASA-TP-1813] p 94 N81-19300

Surface chemistry and wear behavior of single-crystal

silicon carbide sliding against iron at temperatures to 1500

C in vacuum

[NASA-TP-1947) p 94 N82-19374

Influence of corrosive solutions on microhardness and

chemistry of magnesium oxide /001/ surfaces

[NASA-TP-2040J p 122 N82-31691

A tutorise solution to scattering of radiation in s thin

atmosphere bounded below by a diffusely reflecting,

absorbing surface

[NASA-TP-2077) p 154 N82-33918

Tribotogy in the 80's. Volume t: Sessions 1 to 4

[NASA-CP-2300-VOL-1 t p 124 N84-23891

Secondary electron emission characteristics of

ion-textured copper and high-purity isotroplc graphite

surfaces

[NASA-TP-2342} p 95 N84-28989

Effect of five lubricants on life of AISt 9310 spur gears

[NASA-TP-2419} p 116 N85-16099

Monte Carlo lattice models for adsorbed polymer

conformation

{NASA-TP-2453] p 195 N85-24961

Textured carbon on copper: A novel surface with

extremely low secondary electron emission

characteristics

{NASA-TP-25431 p 96 N86-15394

SURFACE REACTIONS

Surface chemistry of iron sliding in air and nitrogen

lubricated with hexadecane and hexadecane containing

dibenzyl-dilsulfide

[NASA-TP-1545] p 79 N79-31346

Changes in surface chemistry of silicon carbide (0001)

surface with temperature and their effect on friction

[NASA-TP-1756J p 94 N81-14079

Influence of mineral oil and additives on microhardness

and surface chemistry of magnesium oxide ((301) surface

[NASA-TP-1986] p 94 N82-20316

Surface fatigue life and tailure characteristics of EX-53,

CBS 1000M, and AISI 9310 gear materials

[NASA-TP-2513] p 125 N86-12609

SURFACE ROUGHNESS

Lubrication and failure mechanisms of molybdenum

disulfide films. 2: Effect of substrate roughness

{NASA-TP-t379J p 92 N79-13159

Frictional heating due to asperity interaction of

elastohydrodynamic line-contact surfaces

[NASA-TP-1882J p 122 N82-25514

Surface roughness effects in elaslohydrodynamic

contacts

[NASA-TP-2488] p 125 N85-32329

SURFACE TEMPERATURE

Method for calculating convective heat-transfer

coefficients over turbine vane surfaces

[NASA-TP-1134] p 104 N78-17338

Effects of a ceramic coating on metal temperatures of

an air-cooled turbine vane

[NASA-TP-1598] p 107 N80-17397

Analysis of uncertainties in turbine metal temperature

predictions

[NASA-TP.t593] p 46 N80.21326

R'Jre tread temperatures during antiskid braking and

cornering on a dry runway

[NASA-TP-200g] p 35 N82.24193

Radlometar requirements for Earth-observation systems

using large space antennas

[NASA-RP-1101] p 116 N83-28410

The Heat Capacity Mapping Mission (HCMM)

anthology

[ES4.f0051 ] p 142 N84-14563

Surface radiation budget for climate applications

[NASA.RP.1169] p t67 N86-28574

SURFACES

Computar-AIdeq Geometry Modeling

[NASA-CP-2272] p 177 N84-22179

SURGES

Circuit transients due to negative bias arcs on a

high-voltage solar array in low Earth orbit

[NASA-TP-2407] p 75 N85-14858

SUSPENSION SYSTEMS (VEHICLES)

Development end valIdation of a piloted simulation of

a helicopter and externsi sling load

[NASA.TP.1285] p 32 N79-14083

SWEEP ANGLE

An experimental and theoretical investigation of thick

wings at various sweep angles in and out of ground

effect

[NASA-TP-2068] p 20 N83-10016

SWEPT FORWARD WINGS

Wind-tunnel expenments on divergence of

forward-swept wings

[NASA-TP-1685] p 34 N80-29287

Aeropropulsive characteristics of twin nonaxisymmetric

vectoring nozzles installed with forward-swept and

aft-swept wings --- in the Langley 16 Foot Transonic

Tunnel

[NASA-TP-1778] p t6 N81-19019

Aeropropulsive charactenstics of tw.n

single-expansion-ramp vectoring nozzles installed with

forward-swept wings and canards --- transonic tunnel

tests

[NASA-TP-2133] p 20 N83-2216t

SWEPT WINGS

Advances in engineering science, volume 4

[NASA-CP-2001-VOL-,4] p 98 N77-t0345

Approximate indicial lift function for tapered, swept wings

in incompressible flow

[NASA-TP-1241] p 9 N78-30054

Aerodynamic characteristics of a hypersonic research

airplane concept having a 70 deg swept double-delta wing

81 Mach number 0.2

[NASA.TP-1252] p 9 N78-31045

Status of linear boundary-layer stabitity and the e to the

cth method, with emphasis on swept-wing applications

[NASA-TP-1645] p 108 N80-22633

Amplified crossflow disturbances in the laminar boundary

layer on swept wings with suction

[NASA-TP-1902] p 109 N82-11391

Low-speed aerodynamic characteristics of a highly

swept, untwisted uncembared arrow wing

[NASA-TP-2176) p 22 N83-36000

Wind-tunnel free-flight investigation of a model of a

forward-swept-wing fighter configuration

[NASA-TP-2230] p 57 N84-17184

Aerodynamic design of the contoured wind-tunnel liner

for the NASA supercritical, laminar-flow-control,

swept-wing experiment

[NASA-TP-2335] p 24 N84-33377

Effect of leading-edge load constraints on the design

and performance of supersonic wings

[NASA-TP-2446] p 26 N85-29923

SWEPTBACK WINGS

Aeropropulsive characteristics of twin nonaxisymmetdc

vectoring nozzles installed with forward-swept and

aft-swept wings --- in the Langley 16 Foot Transonic

Tunnel

[NASA-TP-1778] p 16 N81-19019

Experimental and theoretical study of the longitudinal

aerodynamic characteristics of delta and double-delta

wings at Mach numbers of 160, 1.90, and 2.16

[NASA-TP-2433] p 26 N85-29922

SWIRLING

An experimental investigation of two large annular

diffusers with swirling and distorted inflow

[NASA-TP-1628} p t4 N80-17984

SYMBOLIC PROGRAMMING

Computer formulations of aircraft models for simulation

studies

(NASA-TP-1470] p 2 N79-23008

SYMBOLS

Flight investigation of cockpit-displayed traffic

information utilizing coded symbology in an advanced

operational environment

INASA-TP-1684] p 38 N80-27360

A-119
SYMMETRY SUBJECT INDEX

SYMMETRY

Downwash in the plane of symmetry of an ellipficatly

loaded wing

[NASA-TP-2414} p 25 N85-15693

Solution of the symmetric eigenproblem AX=iambda

BX by delayed division

[NASA-TP-2514] p 135 N86-20857

SYNCHRONISM

Proceedings of the Eleventh Annual Precise Time and

Time Interval (PTI't) Application and Planning Meeting ---

conference

INASA-CP-2129] p 185 N80-29096

Proceedings of the 12th Annual Precise Time and Time

Interval (PTI-I) Applications and Planning Meeting

[ NASA-CP-2175 ] p 117 N81-27467

Proceedings of the t4th Annual Precise Time and Time

interval (PTTI) Applications Planning Meeting

I NASA-CP-2265} p 118 N83-35351

Validation of a fault-tolerant clock synchronization

system

[NASA-TP-2346) p 180 N84-34198

SYNOPTIC METEOROLOGY

Synoptic analyses, 5-, 2-, and 0.4-millibar surfaces for

July 1974 through June 1976

I NASA-RP-1023 [ p 158 N78-28748

Synoptic analyses, 5-, 2-, 1-, and 0 4-millibar surfaces

for July 1976 through June 1977

[NASA-RP-1032] p 159 N79-19569

Atmospheric structure determined from satellite data

[NASA-RP-t071 ] p 162 N81-16678

Current Scientific Issues in Large Scale Atmospheric

Dynamtcs

NASA-CP-2410i p 167 N66-24082

Description of data on Ihe Nimbus 7 LIMS map archive

tape: Temperature and geopotential hefght

NASA-TP-2563} p 167 N86-25924

SYNTHETIC APERTURE RADAR

Preliminary results of SAn soil moisture experiment,

November t975

NASA-TP-1404} p 152 N79-t6473

SYSTEM EFFECTIVENESS

Performance analys_s of grazing incidence imaging

systems --- X ray telescope aberrations

NASA-TP-1088] p 193 N78-11812

Description of an experimental (hydrogen peroxide)

rocket system and its usa in measuring aileron and rudder

eftectlvenass of a light airplane

NASA-TP-1647} p 55 N80-22358

SYSTEM FAILURES

Validation Methods Research for Fault-Tolerant Avionics

and Control Systems: Working Group Meeting, 2

NASA-CP-2130} p 176 N80-23008

SYSTEM GENERATED ELECTROMAGNETIC PULSES

Development and design of three monitoring instruments

for spacecraft charging

NASA-TP-1800] p 76 N8t-31282

SYSTEM IDENTIFICATION

Identification of dynamic systems, theory and

formulation

NASA-RP-11381 p 185 N85-t9784

SYSTEMS ANALYSIS

System analysis approach to deriving design criteria

(loads) for Space Shuttle and its payloads. Volume 1:

General statement of approach

{NASA-TP-1949] p 66 N82.14203

Technology for large space systems: A bibliography with

indexes (supplement 14)

[NASA-SP-7046(14)] p 63 N86-28104

SYSTEMS ENGINEERING

Systems reliability issues for future aircraft

INASA-CP-OO3} p t75 N77-22808

Engineering and Scientific Data Management

INASA'CP'2055] p t78 N78-33776

Proceedings of workshops to define engineering

requirements for a space vacuum research facility

INASA-CP'2091 ] p 62 N79-26076

Description of the VTOL Approach and Landing

Technology (VALT) CH-47 research system

INASA-TP-1436} p 54 N79-29195

Space resources and space sett3ements

{NASA-SP-428] p 62 N79-32225

Control-system techniques for improved departure/spin

resistance for fighter aircraft

{NASA-TP-16891 p 2 N80-29244

Solar Power Satellite Microwave Transmission and

Reception

{NASA-CP-2141 ] p 145 N81-16533

Solar power satellite system sizing tradeoffs

{NASA-TP-1804] p 145 N81-18493

The 1980 Goddard Space Flight Center Battery

Workshop

[NASA-CP-2177J p 145 N61-21493

St ruCtufa[ dynamics and control of large space structures

--- COnference

1NASA-CP-21871 p 66 N81-26166

Space shuttle main engine controller

{NASA-TP-1932] p 178 N82-11784

Propagahon effects handbook for satellite systems

design: A summary of propagation impairments on 10

to t00 GHz satellite links with techniques for system

design

[NASA-RP-t0821 p 100 N82-15270

Problems experienced and envisioned for dynamical

physical systems

[NASA-TP-2508] p 68 N86-11215

SYSTEMS INTEGRATION

Supersonic Cruise Research 1979, part 2 --- airframe

structures and materials, systems integration, economic

analysis

[NASA-CP-2108-PT-2] p 3 N81-ta005

Integrated Flywheel Technology. 1983

INASA-CP-2290] p 77 N84-12228

IPAD 2: Advances in Distributed Data Base Management

for CAD/CAM

[NASA-CP-2301 j p 180 N84.22299

SYSTEMS SIMULATION

Automated decision making and problem solving

Volume 2: Conference presentations

INASA-CP-2ta0-VOL-2} p 184 N61-29gO2

Development and evaluation of a Kalman-filter algorithm

for terminal area navigation using sensors of moderate

accuracy

[NASA-TP-2035] p 31 N83-29193

Thirteenth Space Simulation Conference. The Payload:

Testing for Success

{NASA-CP-2340] p 74 N84-34468

SYSTEMS STABILITY

A method to stabilize linear systems using eigenvalue

gradient information

[NASA-TP-2479 ] p 181 N86-13946

T

TABLES (DATA)

Precision positional data of general aviation air traffic

in terminal air space

[NASA-RP-102O] p 1 N78-25048

A modified T-value method for selection of strain gages

for measuring loads on a low aspect ratio wing

[NASA-TP-1748] p 35 N81-12066

TAIL ASSEMBLIES

Spin-tunnel investigation of the spinning characteriatics

of typical single-engine general aviation airplane designs.

t, Low-wing model A: Effects of tail configurations

[NASA-TP-1009] p 5 N77-33111

Spin-tunnel investigation of the spinning characteristics

of typical single-engine general aviation airplane designs.

2: Low-wing model A; tail parachute diameter and canopy

distance for emergency spin recovery

[NASA-TP-10761 p 6 N78-12040

Supersomc aerodynamic cheractenstics of a Sparrow

3 type missile model with wing controls and comparison

with existing tail-control results

[NASA-TP-1078 } p6 N78-12041

Experimental and theoretical supersonic

lateral-directional stability characteristics of a simplified

wing-body configuration with a series of vertical-tail

arrangements

[NASA-TP-1878} p 17 N81-29095

Effect of nozzle and vertical-tail variables on the

performance of a 3-surface F-15 model at transonic Mach

numbers -- Langley 16 foot transonic tunnel

{NASA-TP-2043} p 20 N82-32320

Effects of twin-vertical-tail parameters on twin-engine

afterbody/nozzie aerodynamic characteristics --- Langley

16-ft transonic tunnel tests

[NASA-TP-21581 p 21 N83-24478

Effect of empennage location on twin-eogine

afterbody-nozzle aerodynamic characteristics at Mach

Numbers from 0.6 to 1.2 --- wind tunnel tests

[NASA-TP-21161 p 21 N83-25666

Aerodynamic characteristics of several current

helicopter tail boom cross sections including the effect

of spoilers

{NASA-TP-2506] p 27 N86-20349

TAKEOFF

Validation of a Flexible Aircraft Take-Off and Landing

Analysis (FATOLA)

[NASA-TP-t025] p 31 N78-10049

Analysis and Monte Cede simulation of near-terminal

aircraft flight paths

[NASA-TP-1997] p 31 N82-23233

Validation of an Active Gear, Flexible Aircraft Take-off

and Landing analysis (AGFATL)

[NASA-TP-2353] p 37 N84-32378

TAKEOFF RUNS

A simulator study for the development and evaluation

of operating procedures on a supersonic cruise research

transport to minimize airporl-community noise

[NASA-TP-17421 p 29 N81-12043

TANDEM WING AIRCRAFT

Parametric study of a canard-configured transport using

conceptual design optimization

(NASA-TP-2400] p 37 N85-1997g

TANK GEOMETRY

Contoured tank outlets for draining of cylindrical tanks

in low-gravity environment --- Lewis Research Center Zero

Gravity Facility

[NASA-TP-14921 p 107 N79-29467

TANKS (CONTAINERS)

Vapor ingestion in Centaur liquid-hydrogen tank

INASA-TP-t061 } p 104 N77-33444

Thermal performance of gaseous-helium-purged

tank-mounted mulfiiayer insulation system during

ground-hold and space-hold thermal cycling and exposure

to water vapor

[NASA-TP-1114 J p65 N78-28150

TANTALUM ALLOYS

Long-time creep behavior of the tantalum alloy Aster

811C --- as a function of stress, temperature, and grain

size

[NASA-TP-169t ] p 87 N80-32489

TAPERING

Lubrication of optimized-design tapered-roller bearings

to 2.4 million DN

_NASA-TP-t7t4] p 121 N80-29734

TARGETS

Spectral reflectances of natural targets for use in remote

sensing studies

[NASA-RP-tt39] p 143 N85-30450

Symmetry considerations in the scattering of identical

composite bodies

iNASA-TP-2548] p 193 N86-23388

TASKS

Twentieth Annual Conference on Manual Control,

volume 2

{NASA-CP-2341-VOL-21 p 174 N85-14535

TAXIING

Effects of cable geometry and aircraft attitude on the

accuracy of a magnetic leader cable system for aircraft

guidance during rotiout end turnoff

{ NASA-TP-t978] p31 N82-22239

Temperature distnbufion in an aircraft tire at low ground

speeds

[NASA-TP-21951 p 132 N83-33217

TEACHING MACHINES

Technical communication: Perspectives for the e_ghties,

part 1. Proceedings of the technical communications

sessions at the 32nd Annual Meeting of the Conference

on College Composition and Communication

(NASA-CP-2203-PT-t I p 197 N82-14960

TECHNICAL WRITING

NASA guidelines on report literature

{NASA-SP-7200] p 197 N79-13914

Technical communication. Perspectives for the Eighties,

part 2

{NASA-CP-2203-PT-2] p 197 N82-15986

NASA publications guide

{NASA-SP-7047] p t97 N83-32671

TECHNOLOGICAL FORECASTING

Proceedings of the 1977 NASA/ISHM Mioroelectronics

Conference

[NASA-CP-2027] p t01 N78-16266

Analysis of data systems requirements for global crop

production forecasting in the 1985 time frame

[NASA.TP-1164} p 138 N78-18497

Future Computer Requirements for Computational

Aerodynamics

[NASA-CP-2032] p 176 N78-19778

Astronomical Microdensitometry Conference

[NASA-CP-2317J p 116 N84-28020

TECHNOLOGIES

The Impact of Science on Society

[NASA-SP-482] p 196 N85-24994

TECHNOLOGY ASSESSMENT

Proceedings of the SCAR Conference, part 2

[NASA-CP-OOt-PT-2} p 1 N77-18019

An Assessment of Technology for Turbojet Engine Rotor

Failures

[NASA-CP-2017] p 41 N78-10068

CTOL transport technology, 1978 --- conferences

[NASA-CP-2036-PT-l} p t N78-27046

Large Space Systems Technology, volume 1

[NASA-CP-2035-VOL-t] p 65 N79-10078

Large Space Systems Technology, volume 2

[NASA-CP-2035-VOL-2] p 66 N79-10097

Future Orbital Power Systems Technology

Requirements

[NASA-CP-2058] p 76 N79-10122

Government/Industry Workshop on Payload Loads

Technology

[NASA-CP-2075] p 62 N79-20162

The 1977 Goddard Space Flight Center Battery

Workshop

[NASA-CP-2041 ] p 144 N79-21565

A-120
SUBJECT INDEX TEMPERATURE PROFILES

The science and technology of low speed and motorless

flight, part 1

[NASA-CP-2085-PT-1] p 2 N79-23889

Premixed Prevaporized Combustor Technology Forum

[NASA-CP-2078] p 44 N79-24994

An evaluation of the NASA Tech House, including live-in

test results, volume 1

INASA-TP-1564] p 145 N80-11559

An assessment of ground-based techniques for

detecting other planetary systems, Volume 1 : An overview

--- workshop conclusions

[NASA-CP-2124-VOL-1] p 201 N80-18997

Advanced technology airfoil research, volume 2 ---

conferences

[NASA-CP-2046] p 14 N80-21283

Lessons of the NASA Tech House

[NASA-SP-442] p 199 N80-27219

Aerospace Applications of Microprocessors

[NASA-CP-2158] p 177 N81-11644

Design and analysis of a torsion braid pendulum

displacement transducer

[NASA-TP-1840] p 115 N81-25352

Vehicle concepts and technology requirements for

buoyant heavy-lift systems

[NASA-TP-t 921 ] p 35 N81-31185

Effects of cable geometry and aircraft attitude on the

accuracy of a magnetic leader cable system for aircraft

guidance during rollout and turnoff

[NASA-TP-t978] p 31 N82-22239

Tropospheric Passive Remote Sensing

[NASA-CP-2237} p 115 N82-26637

Performance of an ablator for Space Shuttle inorbit repair

in an arc-plasma airstream

[NASA-TP-2tS0] p 74 N83-22317

A NASA high-power space-besed laser research and

applications program

[NASA-SP-4641 p 118 N83-27200

Large Deployable Reflector Science and Technology

Workshsp. Volume 3: Systems and Technology

Assessment

[NASA-CP-2275-VOL-3] p 202 N84-32318

The Multispectrsl Imaging Science Working Group.

Volume 1: Executive summary

IE85-1000t] p 142 N85-t1404

The Multispectral Imaging Science Working Group.

Volume 2: Working group reports

[E85-10002] p 142 N85-11405

Gearing

[NASA-RP-lt52J p 125 N86-t4612

Space Station Workstation Technology Workshop

Report

[NASA-CP-2414] p 70 N86-23620

Supercritical wing technology: A report on flight

evaluations

[NASA-SP-30t ] p 6 N77-85474

TECHNOLOGY TRANSFER

Proceedings of the ASPE/MSFC Symposium on

Engineering and Productivity Gains from Space

Technology

[NASA-CP-2019J p 98 N77-30273

Conference of Remote Sensing Educators

(CORSE-78)

[NASA-CP-2t02] p 212 N80-20003

Beyond the atmosphere: Early years of space

science

[ NASA-SP-4211 ] p 200 N81-20962

Western Regional Remote Sensing Conference

Proceedings, 1979

[NASA-CP-2148] p 139 N8t-21440

Field Study for Remote Sensing: An instructor's

manual

[NASA-CP-2155J p 136 N81-32584

Western Regional Remote Sensing Conference

Proceedings, 1981

[E82-10104J p 141 N82-22546

The LANDSAT tutorial workbook: Basics of satellite

remote sensing

[E83-t0001J p 141 N83-10458

Eastern Regional Remote Sensing Applications

Conference

[E83-t0201 ] p 141 N83-21419

TECHNOLOGY UTILIZATION

High altitude perspective --- cost-reimbursable services

using NASA U-2 aircraft

[NASA-SP-427] p 138 N78-31508

Application of space technology to crustal dynamics and

earthquake research

INASA-TP-14641 p 152 N79-31864

Advanced technology airfoil research, volume 2 ---

conferences

[NASA-CP-2046] p 14 N80-21283

Operational Applications of Satellite Snowcover

Observations

[E80-101671 p 139 N80-25742

A catalog of NASA special publications

[NASA-SP-449] p 212 N81-21995

Ruggedized minicomputer hardware and software

topics, 1981: Proceedings of the 4th ROLM MIL-SPEC

Computer User's Group Conference

|NASA-CP-2206] p 180 N82-14829

Applications of Tethers in Space

(NASA-CP-2366] p 125 N85-21659

Applications of Tethers in Space: Workshop

proceedings, volume t

[NASA-CP-2422-VOL-1 ] p 126 N86-28407

TECTONICS

The NASA Geodynamics Program: An overview

[NASA-TP-2147] p 154 N84-10675

Geodynamics

lNASA-CP-2325} p 137 N84-30475

Global Mega-Geomorphology

{NASA-CP-2312] p 137 N85-32357

Geopotential Research Mission (GRM)

{NASA-CP-2390] p 155 N86-12852

TEETERING

Wind-tunnel tests of wide-chord teetering rotors with and

without outboard flapping hinges

[NASA-TP-1046] p 31 N78-11053

TEFLON (TRADEMARK)

Mechanical impact tests of materials in oxygen effects

of contamination --* Teflon, stainless steel, and

aluminum

[NASA-TP-1571] p 97 N80-21551

TELECONFERENClNG

Design of a video teleconference facility for a

synchronous satellite communications link

[NASA-TP-1376] p 100 N79-14275

TELEMETRY

Diversity techniques for omnidirectional telemetry

coverage of the HiMAT research vehicle

[NASA-TP-1830} p 39 N81-20074

Wind-weighting for sounding rockets with a telemetry

system

[NASA-TP-2438} p 70 N85-21246

TELEOPERATORS

Translational control of a graphically simulated robot arm

by kinematic rate equations that overcome elbow joint

singularity

[NASA-TP-2376J p 181 N85-15446

Baseline expenments in teleoperator control

{NASA-TP-2547] p 174 N86-26836

TELESCOPES

Theoretical contamination of cryogenic satellite

telescopes

J NASA-TP-11771 p65 N78-21193

Proton-induced noise in digicons

{NASA-TP-1852} p 76 N81-31281

TELEVISION SYSTEMS

Development of systems and techniques for landing an

aircraft using onboard television

I NASA-TP-11711 p32 N78-20114

Carrier-interference ratios for frequency sharing between

frequency-modulated

band television systems

INASA-TP-1264} p 69 N78-28159

TEMPERATURE CONTROL

Transient shutdown analysis of low-temperature thermal

diodes

[NASA-TP-1369] p 106 N79-t8287

Description and orbit data of variable-conductance

heat-pipe system for the communications technology

satellite

[NASA-TP-1465J p 107 N79-30516

Development of silane-hydrolysate binder for

UV-resistant thermal control coatings

[NASA-TP-1900J p 94 N81-31365

Solar absorptance and thermai emittance of some

common spacecraft thermal-control coatings

[NASA-RP-1121 I p 82 N84-23698

TEMPERATURE DEPENDENCE

Long-time creep behavior of the tantalum alloy Astar

811C --- as a function of stress, temperature, and grain

size

[NASA-TP-t69t j p 57 N80-32489

Mechanism of lubrication by tricresylphosphate (TCP)

[NASA-TP-2274] p t23 N84-18653

TEMPERATURE DISTRIBUTION

Effect of coolant flow ejection on aerodynamic

performance of low-aspect-ratio vanes. 2: Performance

with coolant flow ejection at temperature ratios up to 2

[ NASA-TP-10571 p6 N78-11008

Temperature distributions of a cesium-seedeq

hydrogen-oxygen supersonic free jet

[NASA-TP-1162] p 194 N78-20959

Ceramic coating effect on liner metal temperatures of

film-cooled annular combustor

INASA-TP-1323] p 44 N79-t4098

Pressure and thermal distributions on wings and adjacent

surfaces induced by etevon deflections at Mach 6

[NASA-TP-1356] p 106 N79-20344

Computerized video densitometry method for rapid

analysis of infrared photographic images --- temperature

distribution across a turbine blade

[NASA-TP-1686] p 114 N80-25635

Reduction methods for nonlinear steady-state thermal

analysis

[ NASA-TP-2098t p 110 N83-20032

Temperature distribution in an aircraft tire at fow ground

speeds

[NASA-TP-21951 p 132 N83-33217

TEMPERATURE EFFECTS

Effects of temperature transients at fan inlet of a turbofan

engine

[NASA-TP-1031 ] p 41 N77-31153

Effect of thermal exposure on lubricating properties of

polyimide films and polyimide-bonded graphite fluoride

films

[NASA-TP-1125] p 91 N78-15277

Effects of oxide additions and temperature on

sinterability of milled silicon nitride

[NASA-TP-1644] p 93 N80-21532

Long-time creep behavior of the niobium alloy C-103

[NASA-TP-17271 p 57 N80-33555

Elevated temperature behavior of superplasticatly

formed/weld-brazed titanium compression panels having

advanced shaped stiffeners

NASA-TP-2123] p 88 N83-19889

Reduction methods for nonlinear steady-state thermal

analysis

NASA.TP.2098] p 110 N83-20032

Buckling and failure characteristics of graphite-polyimide

shear panels

NASA-TP-2153] p 82 N83-24561

Three-dimensional turbulent-mixing-length modeling for

discrete-hole coolant injection into a crossfiow

NASA-TP-2200] p 111 N83-34232

Fabrication and evaluation of cold/formed/weldbrazed

beta-titanium skin-stiffened compression panels

NASA-TP-2201] p 89 N83-35100

Operating characteristics of a three-piece-inner-ring

large-bore roller bearing to speeds of 3 million DN

NASA-TP-2355J p 124 N84-29226

Long-term thermal aging of 2 graphite-potyimide

composite matenals

NASA-TP-2369| p 83 N85-12094

Nonlinear Constitutive Relations for High Temperature

Application, 1954

NASA-CP-2369] p 134 N85-31530

TEMPERATURE GRADIENTS

Effects of temperature transients at fan inlet of a turbofan

engine

[NASA-TP-1031 } p 41 N77-31153

Frictional heating due to asperity interaction of

elestohydrodynamic line-contact surfaces

[NASA-TP-1882] p 122 N82-25514

TEMPERATURE MEASUREMENT

Estimation of snow temperature and mean crystat radius

from remote multispectral passive m=crowave

measurements

[NASA-TP-1251J p 151 N78-26677

TACT1, a computer program for the transient thermal

analysis of a cooled turbine blade or vane equipped with

a coolant inserL 1, Users manual

[NASA-TP-1271] p 105 N78-28374

Mechanism of lubrication by tricresylphosphate (TCP)

[NASA-TP-2053] p 85 N83-18863

Solar absorptance and thermal emittance of some

common spacecraft thermal-control coatings

{NASA-RP-1121 ] p 82 N84-23898

Dynamic measurement of total temperature, pressure

and velocity in the Langley 0 3-meter transonic cryogenic

tunnel

[NASA-TP-2584J p 60 N86-24709

TEMPERATURE PROBES

A design handbook for phase change thermal control

and energy storage devices --- selected paraffins

[NASA-TP-10741 p 104 N78-15434

TEMPERATURE PROFILES

Determination of the

hypersonic-continuum/rarefied-flow drag coefficient of the

Viking lander capsule 1 aeroshell from flight data

INASA-TP-1793] p 3 N81-14961

SAM 2 measurements of the polar stratospheric aerosol,

volume 1: October to April 1979

{NASA-RP-1081 ] p 153 N82-13592

SAM 2 Measurements of the Polar Stratospheric

Aerosol, volume 2. April 1979 to October 1979

[NASA-RP-1088-VOL-2] p 153 N82-19734

Optical observations of unidirectional solidification m

microgravity

[NASA-TP-2110J p 98 N83-16492

Expanded operational capabilities of the Langtey Mach

7 Scramjet test facility

[ NASA-TP-21561 p 60 N83-36039

A-121
TEMPERING SUBJECT INDEX

An evaluation and comparison of vertical profile data

from the VlSSR Atmospheric Sounder (VAS)

[NASA-TP-2425] p 166 N85-t6351

TEMPERING

Long-tarm hot-hardness characteristics of five

through-hardened beanng steels

[NASA-TP-1341 ] p 87 N78-33196

TENSILE PROPERTIES

Mechanical properties and oxidation and corrosion

resistance of reduced-chromium 304 stainless steel

alloys

[NASA-TP-1557} p87 N80-11188

Spectroscopic analysis of radiation-generated changes

in tensile properties of a polyetherimide film

[NASA-TP-2429] p 83 N85-25435

The algorithms for rational spline interpolation of

surfaces

[NASA-TP-2536] p 183 N86-18060

TENSILE STRENGTH

Study of austenitic stainless steel welded with low alloy

steel filler metal --- tensile and impact strength tests

[NASA-TP.1460] p 87 N79-28288

Relationship between the ideal tensile strength and the

fr_ctibn properties of metals in contact with nonmetals and

themselves

[NASA-TP-t883J p 94 N81-33293

Experimental data on single-bolt joints in quasi isotropic

graphite/polyimide laminates

[ NASA-TP-20151 p81 N82-25325

Effects of chromium and aluminum on mechanical and

oxidation properties of iron-nickel-base superalloys based

on CG-27

[NASA-TP*2443J p g0 N85-21323

TENSILE STRESS

Tensile stress-strain behavior of boron/aluminum

laminates

{NASA-TP-tlt7] p 79 N78-f8135

Analysis of surface cracks in finite plates under tension

or bending loads

[NASA-TP-1578] p 129 N80-13512

Fracture toughness of boron/aluminum laminates with

various proportions of 0 deg and plus or minus 45 deg

[NASA-TP-1707] p81 N81-11115

Effects of static tensile load on the thermal expansion

of Gr/PI composite material

lNASA-TP-1867] p 81 Nat-24179

TENSION

Ratibnal-spline approximation with automatic tension

adjustment

[NASA-TP-2366] p 182 N84-34204

TENSOR ANALYSIS

Mathematical Modeling of Diverse Phenomena

[NASA-SP-437} p 182 N80-13839

The algorithms for rational spline interpolation of

Sut'laces

[NASA-TP-2536] p 183 N86-18060

TERMINAL CONFIGURED VEHICLE PROGRAM

Terminal configured vehicle program: Test facilities

guide

{NASA-SP-435} p 34 N80-18028

Influence of display and control compatibility on

pilot-induced oscillations

[NASA-TP*1936J p 172 N82.14804

TERMINAL FACILITIES

The 1980 Aircraft Safety and Operating Problems, part

2

[NASA-CP-2170-PT-2] p 29 Nat-tg056

TERMINOLOGY

NASA thesaurus. Volume t: Hierarchical listing

{NASA-SP-7053-VOL-1 J p 198 N86-20168

NASA thesaurus. Volume 2: Access vocabulary

INASA-SP-7053-VOL-2J p 198 N86-20169

TERRAIN

Procedures for gathering ground truth informabon for

a supervised approach to a computer-implemented land

cover classification of LANDSAT-acquired muff_spectral

scanner data

{NASA-RP-1015] p 137 N78-15549

Viking site selection and certification

[NASA-SP_.2gl p 207 N81-25992

TERRESTRIAL RADIATION

Simulation studies of wide and medium field of view

earth radiation data analysis

[NASA-TP-11821 p 158 N78-23679

Middle atmosphere electrodynamics: Report of the

workshop on the Role of the Electrodynamics of the Middle

Atmosphere on Solar Terrestrial Coupling

[NASA-CF-2090] p 152 N79-25608

Earlh Radiation Budget Science, 1978 --- conferences

[NASA-CP-2100] p 180 N79-32797

Companson of data invers=on techniques for remotely

sensed wide-angle observations of Earth emitted

radiation

[NASA-TP-1924] p 164 N82-13620

TEST CHAMBERS

Ice crystal growth in a dynamic thermal diffusion

chamber

[NASA-TP-1651] p 162 N80-23934

TEST FACILITIES

Advanced Technology Airfoil Research, volume 1. part

1 --- conference on development of computational codes

and test facilities

{NASA-CP-2045-PT-f ] p 11 N79-20030

Evaluation of a simplified gross thrust calculation

technique using two prototype Ff00 turbofan engines in

an altitude facility

[NASA-TP-1482] p 44 N79-26057

Terminal configured vehicle program: Test facilities

gu_e

[NASA-SP-435] p 34 N80-18028

development and validation of a hybrid-computer

simulator for a transonic cryogenic wind tunnel

[NASA-TP-1695] p 59 N80-31413

Expanded operational capabilities of the Langley Mach

7 Scramlet test facility

[NASA-TP-2186} p 60 N83-36039

On the frontier: Flight research at Dryden 1946-t981

[NASA-SP-4303] p 4 N85-17934

Aeronautical facilities catalogue. Volume 2: Airbreathing

propulsion and flight simulators

[NASA-RP-1133] p 60 N86-18328

TEST PILOTS

A pilot evaluation of two G-seat cueing schemes

[NASA-TP-t255] p 172 N78-31739

TEST RANGES

A new dimension. Wallops Island flight test range: The

first fifteen years

[NASA-RP-t028] p 64 N79-20166

TETHERED SATELLITES

The 17th Aerospace Mechanisms Symposium

[NASA-CP-2273] p 131 N83-24881

Applications of Tethers in Space, volume 1

t NASA-CP-2364] p 125 N85-2033g

Applications of Tethers in Space, volume 2

INASA-CP-2365] p 125 N85-20361

Applications of Tethers in Space

[NASA-CP-2366J p 125 N85-21659

Proceedings of a Workshop on Applications of Tethers

in Space: Executive Summary

[NASA-CP-2422] p 126 N86-25794

Applications of Tethers in Space: Workshop

proceedings, volume 2

[NASA-CP-2422-VOL-21 p 126 N86-27644

Applications of Tethers in Space: Workshop

proceedings, volume 1

[NASA-CP-2422-VOL-t I p 126 N86-28407

TETHERING

A unique facility for V/STOL aircraft hover testing ---

Langley Impact Dynamics Research Facility

[NASA-TP-1473] p 59 N79-29199

Applications of Tethers in Space, volume 1

[NASA-CP-2364] p 125 N85-20339

TETHERMNES

Applications of Tethers in Space

[NASA-CP-2366] p 125 N85-21659

Proceedings of a Workshop on Applications of Tethers

in Space: Executive Summary

JNASA-CP-2422] p 126 N86-25794

Applications of Tethers in Space: Workshop

proceedings, volume 2

[NASA-CP-2422-VOL-2] p 126 N86-27644

Applications of Tethers in Space: Workshop

proceedings, volume 1

[NASA-CP-2422-VOL-t ] p 126 N86-28407

TEXTURES

Textured carbon on copper: A novel surface with

extremely low secondary electron emission

charectanstics

{NASA-TP-2543] p 96 N86-15394

THEMATIC MAPPING

Operational Applications of Satellite Snowcover

Observations

[E80-10167] p 139 N80-25742

The time-space relationship of the data point (Pixels)

of the thematic mapper and muttispectral scanner or the

myth of simultaneity

{NASA-TP-1715] p 76 N80-28424

Second Eastern Regional Remote Sensing Applications

Conference

[E83-10189J p 141 N83-19141

LANDSAT-4 Science Investigatibns Summary. including

December 1983 Workshop results, volume 1

IE84-10166} p t37 N84-30359

LANDSAT-4 Science Investigations Summary, including

December 1983 Workshop results, volume 2

[E84-10167} p 137 N84-30380

The Multispectrat imaging Science Working Group

Volume t : Executive summary

[E85-10001 } p 142 N85-11404

The Multispectral Imaging Science Working Group

Volume 2: Working group reports

[E85.10002] p 142 N85-11405

LANDSAT-4 Science Characterization Early Results.

Volume 2, part 1: Thematic Mapper (TM)

[E85-10068] p 143 N85-20508

LANDSAT-4 Science Charactenzation Early Results.

Volume 3. part 2: Thematic Mapper ('I'M)

[E85-10069} p 143 N85-21724

LANDSAT-4 Science Characterization Early Results.

Volume 4: Applications --- agriculture, soils land use,

geology, hydrology, wetlands, water quality, biomass

identification, and snow mapping

JE85-100701 p 143 N85-23186

THEODORSEN TRANSFORMATION

Optimization and performance calculation of

dual-rotation propellers

INASA-TP-lg48| p 3 N82-14049

THERAPY

Human Neurological Development: Past, Present and

Future

{NASA-CP-2063} p 212 N79-15887

THERMAL ANALYSIS

Hybrid perturbationlBubnov-Galerkin technique for

nonlinear thermal analysis

[NASA.TP.2145] p 111 N84-22907

Thermal analysis of a planetary transmission with

spherical roller beanngs operating after complete loss of

oil

INASA-TP-2367} p 124 N84-32824

Reduction method for thermal analysis of complex

aerospace structures

[NASA-TP-2373] p 112 N85-16066

THERMAL BOUNDARY LAYER

Influence of thermal boundary condibons on heat

transfer from a cylinder in cross flow

[NASA-TP-1894J p 109 N8t-29384

THERMAL CONDUCTIVITY

Effective thermal conduct_'ity determination for

low-density insulating materials

INASA-TP-1155] p 105 N78-18364

Thermal-conductivity measurements of

tungsten-fiber-reinforced superaltoy composites using a

thermal-conductivity comparator

tNASA-TP-1445] p 80 N79-28234

Computational Aspects of Heat Transfer in Structures

[NASA-CP-2216] p 109 N82-23473

Transport properties ol oxygen

{NASA-RP-1102] p 110 N83-24800

Overv',ew of zirconia with respect to gas turbine

applications

[NASA-TP-2286J p 95 N84-21740

THERMAL CONTROL COATINGS

Formulation of electrically conductive thermal-control

coatings

[NASA-TP-1218] p 78 N78-21218

Analysis of metal temperature and coolant flow with a

thermal-barrier coating on a full-coverage-film-cooled

turbine vane

[NASA-TP-1310] p 43 N78-31109

Industry tests of NASA ceramic thermal barrier coating

--- for gas turbine engine applications

[NASA-TP-1425J p 44 N7g-25023

Effects of a ceramic coating on metal temperatures of

an air-cooled turbine vane

(NASA-TP-15981 p 107 N80-17397

Further industrial tests of ceramic thermal barrier

coatings

[NASA-TP-2057] p 49 N83-10045

THERMAL CYCLING TESTS

Thermal performance of gaseous-helium-purged

tank-mounted multilayer insulation system during

ground-hold and space-hold thermal cycling and exposure

to water vapor

[NASA-TP-1114] p 65 N78-28150

Elastic-plastic finite-element analyses of thermally

cycled single-edge wedge specimens

[NASA-TP-1982] p 130 N82-20565

Elastic-plastic finite-element analyses of thermally

cycled double-edge wedge specimens

[NASA-TP-1973] p t30 N82-20566

Preliminary study of thermomechanical fatigue of

polycrystalline MAR-M 200

{NASA-TP-2280] p 89 N84-17350

THERMAL DEGRADATION

Exploratory investigation of two resin-matrix composites

subjected to arc-tunnel heating

[NASA-TP-1429J p 60 N79-23141

Thermal and oxidative degradabon studies of formulated

C-ethers by gel-permeation chromatography

[NASA-TP-1994] p g4 N82-21332

Long-term thermal degradation and alloying constituent

effects on five boron/aluminum composites

[NASA-TP-1977} p 81 N82-22317

A-122
SUBJECT INDEX THIOLS

THERMAL DIFFUSION

Ice crystal growth in a dynamic thermal diffusion

chamber

[NASA-TP-1651 J p 162 N80-23934

THERMAL DIFFUSIVITY

Transport properties of oxygen

[NASA-RP-1102] p 1t0 N63-24800

THERMAL EMISSION

Solar absorptance and thermal emittance of some

common spacecraft thermal-control coatings

[NASA-RP-1121 ] p 82 N64-23698

THERMAL ENERGY

Thermal Energy Storage: Fourth Annual Review

Meeting

[NASA-CP-2125J p 145 N80-22788

THERMAL ENVIRONMENTS

Thirteenth Space Simulation Conference. The Payload:

Testing for Success

[NASA-CP-2340] p 74 N84-34468

THERMAL EXPANSION

Effects o1 static tensile toad on the thermal expansion

of Gr/PI composite material

[NASA-TP-1867] p 81 N81-2417g

Buckling and failure characteristics of graphite-polyimide

shear panels

[NASA-TP-2153} p 82 N83-24561

Theoretical basis for design of thermal-stress-free

fasteners

[NASA-TP-22261 p 132 N84-13614

THERMAL FATIGUE

Some effects of thermal-cycle-induced deformation in

rocket thrust chambers

[NASA-TP-1834] p 77 N81-20176

Long-term thermal degradation and alloying constituent

effects on five boron/aluminum composites

[NASA-TP-1977] p 81 N62-22317

Preliminary study of thermomechanicel fatigue of

polycrystaltine MAR-M 200

[NASA-TP-2280] p 89 N84-17350

Thermal-fatigue end oxidation resistance of

cobalt-modified Udimet 700 alloy

[NASA-TP-2591 ] p 135 N86-28464

THERMAL INSULATION

Preliminary design procedure for insulated structures

subjected to transient heating

[NASA-TP-1534J p 128 N80-12438

Electroless-pleting technique for fabricating thin-wall

convective heat-transfer models

[NASA-TP-234g] p 112 N84-3t561

THERMAL MAPPING

The Heat Capacity Mapping Mission (HCMM)

anthology

[E84-10051 J p 142 N64-14563

THERMAL PROTECTION

Emittance and absorptance of NASA ceramic thermal

barrier coating system --- for turbine cooling

[NASA-TP-t 190] p 43 N78-26148

Reinforced cart)on-carbon oxidation behavior in

convective and radiative environments

[NASA-TP-1264] p t06 N78-30555

Performance of a Haynes 186 metallic standoff thermal

protection system at Mach 7

[NASA-TP-1802] p 72 N81-21116

Aorodynamic heating on the corrugated surface of a

10.2 de o half-angle blunted cone at Mach 6.7

[NASA-TP-1928] p 109 N62-13383

Thermal end aerothermat performance of a titanium

multiwall thermal protection system

[NASA-TP-1961] p 72 N62-14277

Twelfth Space Simulation Conference: Shuttle Plus One.

A New View of Space

{NASA-CP-2229] p 73 N82-25291

Performance of an ablstor for Space Shuttle inorbd repair

in an arc-plasma airstream

[NASA-TP-2150] p 74 N83-22317

Effect of strain isolator pad modulus on inplane strain

in Shuttle Orbiter thermal protection system tiles

[NASA-TP-2141} p 132 N83-33216

Steady internal flow and aerodynamic loads analysis of

shuttle thermal protection system

[NASA-TP-2255] p 74 N64-19393

Space Shuttle Technical Conference, part 2

[NASA-CP-2342-PT-2] p 63 N85-16937

Experimental aerodynamic heating to simulated space

shuttle tiles in laminar and turbulent boundary layers with

variable flow angles at a nominal Mach number of 7

[NASA-TP-2307] p 113 N85-34351

THERMAL RESISTANCE

Low-cycle tatJ(:jue of thermal-berner coatings at 982 deg

C

[NASA-TP-13221 p 43 N79-13046

Development of silane-hydrolysate binder for

UV-resJstant thermal control coatings

[NASA-TP-1900] p 94 N81-31365

THERMAL SHOCK

Preliminary study of methods for providing thermal shock

resistance to plasma-sprayed ceramic gas-path seals

[NASA-TP-1561J p 93 N80-23453

THERMAL STABILITY

Long-term thermal degradation and alloying constituent

effects on five boron/aluminum composites

[NASA-TP-1977] p 81 N82-22317

THERMAL STRESSES

Thermal stress analysis of ceramic gas-path seal

components for aircraft turbines

[NASA-TP-1437] p 92 N79-21205

Approximation methods for combined thermal/structural

design

[NASA-TP-1428J p 128 N79-25427

Modeling, Analysis, and Optimization Issues for Large

Space Structures

[NASA-CP-2258] p 66 N83-18819

Theoretical basis for design of thermal-stress-free

fasteners

[NASA-TP-2226] p t32 N84-13614

Comparison of predicted end experimental thermal

performance of angular-contact bait bearings

[NASA-TP-2275] p 123 N84-18654

THERMOCHEMISTRY

Laminar heat-transfer distributions on biconics at

incidence in hypersonic-hypervelocity flows

[NASA-TP-22131 p 112 N65-16065

THERMOCOUPLE PYROMETERS

Surface pyrometry in presence of radiation from other

sources with application to turbine blade temperature

measurement

[NASA-TP-t 754J p 47 N81-11039

THERMOCOUPLES

Recovery and radiation corrections and time constants

of several sizes of shielded and unshielded thermocouple

probes for measuring gas temperature

[NASA-TP-t099J p 113 N78-15463

Computer program for pulsed thermocouples with

corrections for radiation effects

[NASA-TP-1896] p 179 N61-33838

THERMODYNAMIC CYCLES

Effect of steam addition on cycle performance of simple

and recuperated gas turbines

INASA-TP-1440] p 144 N79.22626

New features end applications of PRESTO, a computer

code for the performance of regenerative, superheated

steam turbine cycles

[NASA-TP-1954] p 145 N82-16477

Analysis of a topping-cycle, aircraft, gas-turbine-engine

system which uses cryogenic fuel

[ NASA-TP-2294 J p 5t N84-21549

THERMODYNAMIC PROPERTIES

Some physical end thermodynamic properties of rocket

exhaust clouds measured with infrared scanners

[NASA-TP-t041] p 147 N78-11520

Triple point determinations of monomethylhydrazine and

nitrogen tetroxide, 22 percent by weight nitnc oxide

[NASA.RP-1013] p 96 N78-13234

Thermodynamic and related properties of oxygen from

the triple point to 300 K at pressures to 1000 bar

[NASA-RP-1011 ] p 84 N78-16119

Computer program for obtaining thermodynamic and

transport properties of air and products of combustion of

ASTM-A-1 fuel and air

[NASA-TP-11601 p 97 N78-20351

Effects of thermomechenical processing on strength and

toughness of iron - f 2-percent-nickel - reactive metal alloys

at -196 C

[NASA-TP-1308J p 86 N78-31213

WETAIR: A computer code for calculating

thermodynamic and transport properties of air-water

mixtures

[NASA-TP-1466] p 178 N79-23668

Thermodynamic properties of nitrogen gas derived from

measurements of sound speed --- for cryogenic wind

tunnels

{NASA-RP-1051 ] p 97 N80-t4257

Handbook of lunar materials

[NASA-RP-t0571 p 206 N80-16009

Thermodynamic and transport combustion properties of

hydrocarbons with air, Part 1: Properties in SI units

[NASA-TP-19061 p 195 N82-32186

Thermodynamic and transport combustion properties of

hydrocarbons with air. Part 2: Compositions corresponding

to Kelvin temperature schedules in part f

[NASA-TP-1907] p 195 N82-32187

Thermodynamic and transport combustion properties of

hydrocarbons with air Part 3: Properties in US customary

units

[NASA-TP-1908] p 195 N82-32188

Thermodynamic and transport combustion properties of

hydrocarbonswitheir. Part4: Compositionscorresponding

to Rankine temperature schedules in part 3

[NASA-TP-1909] p 195 N82-32189

A class of nonideal solutions. 2: Application to

experimental data

I NASA-TP-1930 J p 196 N83-23188

Engineering and design properties of thallium-doped

sodium iodide and selected properties of sodium-doped

cesium iodide

[NASA-RP-1131 ] p99 N84-33613

Combustion gas properties I-ASTM jet A fuel and dry

air

[NASA-TP-2359] p 51 N85-10064

THERMODYNAMICS

A stability analysis of AVE-4 severe weather

soundings

[NASA-TP-2045] p 164 N83-14824

A class of nonideal solutions. 1: Definition and

properties

[NASA-TP-19291 p 196 N83-23189

INHYD: Computer code for intraply hybrid composite

design. A users manual

[NASA-TP-2239] p 82 N64-13224

Stellar atmospheric structural patterns

[NASA-SP-471 ] p 204 N84-19253

THERMOELECTRIClTY

Analysis of thermoelectric properties of

high-temperature complex alloys of nickel-base, iron-base

and cobalt.base groups

INASA-TP-2278] p 89 N84-18370

THERMOMECHANICAL TREATMENT

Simplified method for nonlinear structural analys=s

l NASA-TP-22081 p 132 N83-34372

THERMOSETTING RESINS

NASA/aircraft industry standard specification for

graphite fiber toughened thermoset resin composite

material

[NASA-RP-1142] p 83 N85-26923

THERMOSPHERE

The 1976 standard atmosphere above 86-km altitude:

Recommendations of task group 2 to COESA

[NASA-SP-398] p 157 N77-10755

Thermosphere Dynamics Workshop, volume 2

[NASA-CP-2389] p 137 N86-29301

THESAURI

NASA Thesaurus supplement: A 3-part cumulative

supplement to the 1982 edition of the NASA Thesaurus

[NASA-SP-7051(SUPPL-2)] p 198 N85-12785

NASA thesaurus. Volume 1: Hierarchical listing

INASA-SP-7053-VOL-1 ] p 198 N86-20168

NASA thesaurus, Volume 2: Access vocabulary

[NASA-SP-7053-VOL-2] p 198 N86-20169

THICKNESS

Gas turbine ceramic-coated-vane concept with

convection-cooled porous metal core

[NASA-TP-1942] p 48 N82-14090

Further industrial tests of ceramic thermal barrier

coatings

[NASA-TP-2057] p 49 N83-10045

Studies of sidewall boundary layer in the Langley 0.3

meter transonic cryogenic tunnel with and without

suction

[NASA-TP-2096] p 110 N83-20031

THICKNESS RATIO

Joint research effort on vibrations of twisted plates1

phase 1: Final results

[NASA-RP-f150} p 135 N86-10579

THIN FILMS

Effect of thermal exposure on lubricating properties of

polyimide films and polyimlde-bonded graph=te fluoride

films

[NASA-TP-1125] p 91 N78-15277

Lubrication and failure mechanisms of graphite fluoride

films

[NASA-TP-1197] p 91 N78-20337

Polytetrafluoroethylene transfer film studied with X-ray

photoelectron spectroscopy

[NASA-TP-1728] p 93 N81-11214

A potential-energy scaling model to simulate the inilial

stages of thin-film growth

[NASA-TP-2102J p 88 N83-18895

Growth of high-qualit'/ thin-film Ge single crystals by

plasma-enhanced chemical vapor deposition

INASA-TP-2532] p 100 N86-20586

THIN WALLED SHELLS

Electroless-pleting technique for fabricahng thin-wall

convective heat-transfer models

[NASA-TP-2349J p 112 N84-3t561

THIN WALLS

Experimental studies of effects of tilt and structural

asymmetry on vibration charactenstics of thin-wall circular

cylinders partly filled with liquid

[NASA-TP-12111 p 127 N79-28480

THIOLS

Effect of oxygen, methyl mercaptan, and methyl chloride

on friction behavior of copper-iron contacts

INASA-TP-1309] p 86 N78-30206

A-123
THREE AXIS STABILIZATION

THREE AXIS STABILIZATION

Decoupled control analysis of a large flexibte space

antenna with linear quadratic regulator comparisons

I NASA-TP-2293} p 74 N84-23675

THREE BODY PROBLEM

Motion about the stable libration points in the linearized,

restricted three-body problem

[ NASA-RP-1065] p203 N81-11970

THREE DIMENSIONAL BOUNDARY LAYER

Advances in engineering science, volume 4

[ NASA-CP-200t-VOL-4 t p 98 N77-10345

Calculation methods for compressible turbulent

boundary layers, 1976

J NASA-SP*422] p 104 N78-13371

Calculation of laminar heating rates on

three-dimensional configurations using the axisymmetric

analogue

I NASA-TP-16981 p 108 N80-33719

Viscous-inviscid interaction method including wake

effects for three-dimensional wing-body configurations

{NASA-TP-19t0 p 24 N84-27682

THREE DIMENSIONAL FLOW

The design of supercritical wings by the use of

three-dimensional transonic theory

INASA-TP-t400 p 11 N79-16804

WIND: Computer program for calculation of three

dimensional potential compressible flow about wind turbine

rotor blades

I NASA-TP-1729 p 15 N80-33357

Fringe localization requirements for three-dimens_onal

flow visualization of shock waves in diffuse-illumination

double-pulse holographic intederometry

[NASA-TP-1868 p 115 N82-22481

Computer program for calculating futl potential transonic,

qua si-t hr ee-dimension al flow through a rotating

turbomachinery blade row

I NASA-TP-2030 p 20 N82-28247

Calculation of inviscld flow over shuttle-like vehicles at

high angles of attack and comparisons with experimental

data

[ NASA-TP-2103 p 110 N83-24808

Three-dimensional turbulent-mixing-length modeling for

discrete-hole coolant injection into a crossflow

I NASA-TP-2200 J p 111 N83-34232

A spatial model of wind shear and turbulence for flight

simulation

INASA-TP-2313) p 165 N84-24044

A numerical simulation of three-dimensional flow in an

adaptive wall wind tunnel

[ NASA-TP-2351 ) p 24 N84-28750

THROATS

The effect of throat contouring on two-dimensional

converging-divergiog nozzles at static conditions

I NASA-TP-1704 ] p 15 N80-29250

THROI-rLING

The aerodynamic performance of several flow control

devices for internal flow systems

I NASA-TP-1972 ) p 59 N83-17560

THRUST

Effects of deflected thrust on the ,longitudinal

aerodynamic characteristics of a close-coupled

wing-canard configuration --- in the Langley V/STOL

tunnel

[ NASA-TP-1090 } p6 N78-13014

Estimation of attainable leading-edge thrust for wings

at subsonic and supersonic speeds

INASA-TP-1500T p 12 N80-10105

Supersonic wings with significant leading-edge thrust at

cruise

INASA-TP-16321 p 14 N80-21279

Investigation of axisymmetric and nonaxisymmetric

nozzles installed on a 0 10 scale F-18 prototype airplane

model --- wind tunnel tests

INASA-TP*t6381 p 15 N80-24267

THRUST AUGMENTATION

Workshop on Thrust Augmenting Ejectors

INASA-CP-2093J p 13 N60-10t07

THRUST BEARINGS

Experimental evaluation of foil-supported resilient-pad

gas-lubricated thrust bearing

INASA-TP-1030J p 118 N77-31502

Operating characteristics of a cantilever-mounted

resilient-pad gas-lubricated thrust bearing

[NASA-TP-14381 p 120 N79-22518

THRUST CHAMBERS

Hydrogen film cooling of a small hydrogen-oxygen thrust

chamber and its effect on erosion rates of various ablative

materials

INASA-TP-t098J p 76 N78-13124

Effect of tow-stillness closeout overwrap on rocket

thrust-chamber life

I NASA-TP-14561 p 77 N79-23132

Some effects of thermal-cycle-induced deformation in

rocket thrust chambers

INASA-TP-18341 p 77 N81-20176

THRUST CONTROL

Digital Electronic Engine Control (DEEC) Flight

Evaluation in an F-15 Airplane

[NASA-CP-2298] p 52 N86-25342

THRUST DISTRIBUTION

Perfect bell nozzle parametric and optimization curves

[NASA-RP-t 1041 p 77 N83-24549

THRUST LOADS

Effect of simulated in-flight thrust reversing on

vertical-tail loads of E-18 and F-15 airplane models ---

conducted in the Langley 16-foot transonic tunnel

[NASA-TP-1890} p 18 N81-30086

THRUST MEASUREMENT

Airflow and thrust calibration of an FIO0 engine, S/N

P680059, at selected flight conditions

I NASA-TP-1069 ] p 42 N78-21112

Altitude calibration of an Ft 00, S/N P680063, turbofan

engine

I NASA-TP-1228J p 42 N78-23095

Comparison of calculated and altitude-facility-measured

thrust and airflow of two prototype FIO0 turbofan

engines

{NASA-TP-t3731 p 43 N79-13044

Evaluation of a simplified gross thrust calculation

technique using two prototype F100 turbofan engines in

an altitude facility

{NASA-TP-1482] p 44 N79-26057

THRUST REVERSAL

Static performance of five twin-engine nonaxisymmetric

nozzles with vectoring and reversing capability

[NASA-TP-12241 p 9 N78-28057

Effect of simulated in-flight thrust reversing on

vertical-tail loads of F-18 and F-15 airplane models ---

conducted in the Langley 16-foot transonic tunnel

INASA-TP-1890] p 18 N81-30086

Static internal performance of single expansion-ramp

nozzles with thrust vectoring and reversing

[NASA-TP-1962] p 19 N82-20156

Static internal performance characteristics of two thrust

reverser concepts for axisymmatric nozzles

[NASA-TP-20251 p 20 N82-26235

Effect of nozzle and vertical-tail variables on the

performance of a 3-surlace F-15 model at transonic Mach

numbers --- Langley 16 foot transonic tunnel

NASA-TP-2043I p 20 N82-32320

Thrust performance of a variable-geometry, divergent

exhaust nozzle on a turbojet engine at altitude

NASA-TP-2171 ] p 50 N83-26839

Effect of thrust reverser operation on the

lateral-directional characteristics of a three-surface F-15

model at transonic speeds

NASA-TP-2234] p 22 N84-13165

Static internal performance including thrust vectoring

and reversing of two-dimensional convorgent-divergent

nozzles

NASA-TP-2253] p 23 N84-18165

Aeropropulsive characteristics of

nonaxisymmetric-nozzle thrust reversers at Mach numbers

from 0 to t 20

NASA-TP-23061 p 23 N84-24538

Static inlernal performance of a singio-engine

onaxisymmetric-nozzte vaned-thrust-reverser design with

thrust modulation capabilities

NASA-TP-25191 p 27 N86-20348

Static internal performance of a thrust vectoring and

reversing two-dimensional convergent-divergent nozzle

with an aft flap

NASA-TP-2549J p 28 N86-23560

THRUST VECTOR CONTROL

Optimal guidance and control for investigating aircraff

noise-impact reduction

NASA-TP-t2371 p 53 N78-23100

Effects of spanwise nozzle geometry and location on

the longitudinal aerodynamic characteristics of a

vectored-engine-over-wing configuration at subsonic

speeds

I NASA-TP-12151 p 8 N78-25060

Static performance of five twin-engine nonaxisymmetric

nozzles with vectoring and reversing capability

INASA-TP'12241 p 9 N78-28057

Feasibility study of LITVC for shuttle SRB

INASA-TP-19121 p 77 N81-33231

Static internal performance of single expansion-ramp

nozzles with thrust vectoring and reversing

[NASA-TP-19621 p 19 N82-20156

Aeropropulsive characteristics of twin

single-expansion-ramp vectoring nozzles installed with

forward-swept wings and canards --- transonic tunnel

tests

I NASA-TP-21331 p 20 N83-22161

Thrust performance of a variable-geometry, divergent

exhaust nozzle on a turbojet engine at altitude

[NASA-TP-2171 ] p 50 N83-26839

SUBJECT INDEX

Effect of thrust vectoring and wing maneuver devices

on transonic aerowopulsive characteristics of a supersonic

fighter

[NASA-TP-2119] p 22 N84-10025

Thrust-induced effects on subsonic longitudinal

aerodynamic characteristics of a

vectored-engine-over-wing configuration

INASA-TP-2228J p 22 N84-13163

Static internal performance including thrust vectoring

and reversing of two-dimensional convergent-divergent

nozzies

I NASA-TP-2253I p 23 N84-t8165

Static internal performance of a two-dimensional

convergent nozzle with thrust-vectoring capability up to

60 deg

INASA-TP-2391 I p 25 N85-18951

Relative control effectiveness technique with application

to airplane control coordination

[NASA-TP-2416J p 37 N85-23753

Static investigation ol several yaw vectonng concepts

on nonaxisymmetric nozzles

[NASA-TP-2432] p 26 N85-28924

Static investigation of two STOL nozzle concepts with

pitch thrust-vectoring capability

INASA-TP-2559] p 28 N86-23559

Static internal performance of a thrust vectoring and

reversing two-dimensional convergent-divergent nozzle

with an aft flap

INASA-TP-25491 p 28 N86-23560

THUNDERSTORMS

Thunderstorm-environment interactions determined with

three-dimensional trajectories

{NASA-RP-10541 p 161 N80-16675

Lightning affachment patterns and flight conditions for

storm hazards, 1980

[NASA-TP-2087] p 30 N83-14077

NASA/MSFC FY-84 Atmospheric Processes Research

Review

[NASA-CP-2329] p 166 N84-34829

THYRISTORS

High-voltage, high-power, solid-state remote power

controllers for aerospace applications

INASA-TP-2437] p 78 N85-21263

TIDES

On the tidal oscillations of the liguid core of the earth

[NASA-TP-1223) p 151 N78-21691

TILES

Aerodynamic heating in gaps of thermal protection

system tile arrays in laminar and turbulent boundary

tayers

|NASA-TP-1187J p 105 N78-28373

Thermal and aerothermal performance of a titanium

multiwall thermal protection system

[NASA-TP-1961 I p 72 N82-14277

Effect of strain isolator pad modulus on inplane strain

in Shuttle Orbiter thermal protection system tiles

{NASA-TP-2141] p 132 N83-33216

Etectrotess-plating technique for fabricating thin-wall

convective heat-transfer models

[NASA-TP-2349] p 112 N84-31561

Experimental aerodynamic heating to simulated space

shuffle tiles in laminar and turbulent boundary layers with

variable flow angles at a nominal Mach number of 7

l NASA-TP-2307] p t13 N85-34351

TILT ROTOR AIRCRAFt"

Quiet powered-lift propulsion

[NASA-CP-2077| p 46 N80-15127

TILT ROTOR RESEARCH AIRCRAFT PROGRAM

An assessment of the capability to calculate tilting

prop-rotor aircraft performance, loads and stability

[NASA-TP-2291 ] p 37 N84-19333

TIMBER INVENTORY

Wildland inventory and resource modeling for Douglas

and Carson City Counties, Nevada, using LANDSAT and

digital terrain data

IE83-10302] p 142 N83-27293

TIMBER VIGOR

Aerial color infrared photography: Applications in

citriculture --- Florida

INASA-RP-1067] p t39 N81 21437

TIME

Temporal and spatial inconsistencies ot time-split

finite-difference schemes

lNASA-TP-17901 p 182 N81-22754

Piloted simulation of an algorithm for onboard control

of time-optimal intercept

INASA'TP'24451 p 58 N85-28949

TIME LAG

Evaluation of several secondary tasks in the

determination of permissible time delays in simulator visual

and motion cues

INASA-TP-t214] p 32 N78-30089

Simulator study of the effect of visual-motion time delays

on pilot tracking performance with an audio side task

INASA-TP-t216] p 32 N78-30090

A-124
SUBJECT INDEX TRAFFIC

TIME MEASUREMENT

Proceedings of the Eleventh Annual Precise Time and

Time Interval (P'I-FI) Application and PJanniog Meeting ---

conference

[NASA-CP-2129] p 185 N80-29096

Proceedings of the 12th Annual Precise Time and Time

Interval {PTTI) Applications and Planning Meeting

{NASA-CP-2175} p 117 N81-27467

Proceedings of the Thirteenth Annual Precise Time and

Time Interval (PTTt) Applications and Planning Meeting

[NASA-CP-222OJ p 118 N82-20494

Proceedings of the 14th Annual Precise Time and Time

Interval (PTTI) Applications Planning Meeting

[NASA-CP-22651 p 118 N83-35351

TIME OPTIMAL CONTROL

Optima[ regulation in systems with stochastic time

sampling

[NASA-TP-1743} p 184 N81-12812

TIME SERIES ANALYSIS

Introduction to time series analys=s

{NASA-RP-1145J p 191 N86-24391

TIME SIGNALS

Proceedings of the Eleventh Annual Precise Time and

Time Interval (PTTI) Application and Planning Meeting ---

conference

{NASA-CP-2129t p 185 N80-29096

Proceedings of the 14th Annual Precise Time and Time

Interval (PTT]) Applications Planning Meeting

{NASA-CP-2265_ p 118 N83-35351

TIP DRIVEN ROTORS

Cold-air performance of a tip turbine designed to dnve

a lift fan. 3: Effect of simulated fan leakage on turbine

performance

[NASA-TP-1109] p 7 N78-t6001

Analytical and experimental investigation of stator

endwall countouring in a small axial-flow turbine

[NASA-TP-23091 p 51 N84-32388

TIP SPEED

Design and performance of a

427-meter-per-second-tip-speed two-stage fan having a

2.40 pressure ratio

[NASA-TP-1314 ] p43 N78-33109

Forward acoustic performance of a model turbofan

designed for a high specific flow (OF-14)

[NASA-TP-19681 p 188 N82-21036

TIRES

Tire Modeling

{NASA-CP-2264} p 131 N83-21391

Mixed models and recugion techniques for

large-rotation, nonlinear analysis of shells of revolution with

application to tires

[NASA-TP-2343} p 133 N84-34773

TIROS N SATELLITE

A comparative analysis of rawinsonde and NIMBUS 6

and TIROS N satellite profile data

{NASA-RP-f070] p 162 N81-15640

VAS Demonstration Sounding Workshop: The

Proceedings of a satellite sounding workshop

[NASA-CP-2157} p 183 N81-19709

TIROS N SERIES SATELLITES

The Conception, Growth, Accomplishments and Future

of Meteorological Satellites

[NASA-CP-22571 p 164 N83-14825

TIROS PROJECT

The Conception, Growth, Accomplishments and Future

of Meteorological Satellites

[NASA-CP-2257] p 164 N83-14825

TISSUES (BIOLOGY)

The Regulatory Functions of Calcium and the Potential

Role of Calcium in Mediating Gravitational Responses in

Cells and Tissues

[NASA-CP-2286J p 169 N84-11720

TITAN LAUNCH VEHICLES

On the Shoulders of Titans: A History of Project

Gemini

[NASA-SP-42031 p 61 N78-20151

TITANIUM

Friction and wear behavior of single-crystal silicon

carbide in contact with titanium

[NASA-TP-1035} p 9t N77-32312

Friction and wear of selected metals and alloys in sliding

contact with AISI 440 C stainless steel in liquid methane

and in liquid naturat gas

[NASA-TP-11501 p 119 N78-20512

Thermal and aerothermal performance of a titanium

multiwall thermal protection system

{NASA-TP-1961 } p 72 N82-14277

Interface control and mechanical property improvements

in silicon carbide/titanium composites

[NASA-I-P-2066} p 81 N82-31451

Joint design for improved fatigue life of diffusion-bonded

box-stiffened panels

{NASA-TP-2480] p 135 N85-33537

TITANIUM ALLOYS

Improved adherence of sputtered titanium carbide

coatings on nickel- and titanium-base alloys

[NASA-TP-1450} p 78 N79-22194

Plasma-sprayed coatings for lubrication of a titanium

alloy in air at 430 deg C

[NASA-TP-t509J p 93 N79-29327

Effects of geometric variables on rub characteristics of

Ti-6AI-4V

[NASA-TP-t835J p 88 N81-20245

Elevated temperature behavior of superplastically

formed/weld-brazed titanium compression panels having

advanced shaped stiffeners

[NASA-TP-2123] p 88 N83-19889

Fabrication and evaluation of brazed titanium*clad

Borsic/aluminum compression panels

{NASA-TP-1573J p 82 N83-28100

Fabrication and evaluation of cold/formed/weldbrazed

beta-titanium skin-stiffened compression panels

[NASA-TP-2201 ] p 89 N83-35100

Fabrication and evaluation of superplastically

formed/weld-brazed corrugated compression panels with

beaded webs

INASA-TP-2512] p g0 N86-t3406

TITANIUM CARBIDES

Effect of nitrogen-containing plasma on adherence,

friction, and wear of radiofrequency-sputtered titanium

carbide coatings

{NASA-TP-1377] p 92 N79-15184

Improved adherence of sputtered titanium carbide

coatings on nickel- and titanium-base alloys

[NASA-TP-1450] p 78 N79-22194

TITANIUM NITRIDES

Nitriding of titanium and titanium: 8 percent aluminum,

f percent molybdenum. I percent vanadium alloy with an

ion-beam source

{NASA-TP-2149J p 89 N83-24640

TOKAMAK DEVICES

Solar Terrestrial Physics: Present and Future

{ NASA-RP-1120J p 200 N84-34332

TOLERANCES (PHYSIOLOGY)

Human exposure in low Earth orbit

[NASA-TP-2344] p 174 N84-29479

Annoyance caused by propeller airplane flyover noise

[NASA-TP-2356J p 190 N84-32124

TOLUENE

Chemical kinetic modeling of benzene and toluene

oxidation behind shock waves

{NASA-TP-1472} p 84 N79-28259

TOOLS

Tools for Embedded Computing Systems Software

[NASA-CP-2064] p 178 N79-13736

TOPOGRAPHY

Remote sensing of Gulf Stream using GEOS-3 radar

altimeter

{NASA-TP-1209J p 167 N78-21737

Atlas of Mercury --- Mariner 10 mission

[NASA-SP-423} p 205 N78-30025

NASA Wallops Flight Center GEOS-3 altimeter data

processing report

{NASA-RP-1066J p 139 N81-tt438

Frontiers of Remote Sensing of the Oceans and

Troposphere from Air and Space Platforms

[NASA-CP-2303] p 142 N84-27262

Planetary cartography in the next decade (1984 -

1994)

[NASA-SP-475] p 208 N85.22323

TOPOLOGY

Numerical grid generation techniques ---conference

[NASA-CP-2166} p t82 N81-14690

Global Mega-Geomorphoiogy

[NASA-CP-2312] p 137 N85-32357

Hybrid routing technique for a fault-tolerant, integrated

information network

[NASA-TP-2605] p 180 N86-27947

TOPPING CYCLE ENGINES

Analysis of a topping-cycle, aircraft, gas-turbine-engine

system which uses cryogenic fuel

{NASA-TP-2294J p 51 N84-21549

TOROIDAL PLASMAS

Fluctuation spectra in the NASA Lewis bumpy-torus

plasma

[NASA*TB-1257J p 194 N78-26927

Ion confinement and transport in a toroidal plasma with

externally imposed radial electric fields

[NASA.TP-141t ] p 195 N79-19867

TOROUE

Dynamics of aircraft antiskid braking systems ---

conducted at the Langley aircraft landing loads and traction

facility

{NASA-TP-1959} p 35 N82-18204

Film thickness measurement for spiral groove and

Rayleigh step lift pad self-acting face seals

{NASA-TP-2058 ] p49 N83-t 1126

TORSION

Wind-tunnel investigation of the effects of blade tip

geometry on the interaction of torsional loads and

performance for an articulated helicopter rotor

[NASA-TP-19261 p 18 N82-13107

TOUCHDOWN

Effect of image tilt of a virtual image display on simulated

transpod touchdown performance

[NASA-TP-1520] p 33 N79-33189

Application of modified profile analysis to function testing

of simulated CTOL transport touchdown-performance

data

{NASA-TP-1541 ] p 33 N80-11089

TOUGHNESS

Standard tests for toughened resin composites, revised

edition

[NASA-RP-1092-REVJ p 82 N83-31730

Tough Composite Materials

{NASA-CP-23341 p 83 N85-12941

TOWING

Results from tests, with van-mounted sensor, of

magnetic leader cable for aircraft guidance during roll-out

and turnoff

{NASA-TP-20921 p 40 N83-16338

TRACE CONTAMINANTS

Tropospheric Passive Remote Sensing

I NASA-CP-2237} p 115 N82-26637

TRACE ELEMENTS

The NASA Ames Research Center one- and

two-dimensional stratospheric models Part 2: The

two-dimensional model

{NASA-TP-tO03] p 158 N77 32689

Measurement techniques for trace metals in coal-plant

effluents: A brief review

{NASA-RP-1047J p 148 N79-33611

Experimental design of an interlaboratory study for trace

metal analysis of liquid fluids --- for aerospace vehicles

lNASA-TP-2148] p 85 N83-24575

TRACKING (POSITION)

Evaluation of several secondary tasks in the

determination of permissible time delays in simulator visual

and motion cues

NASA-TP-1214] p 32 N78-30089

Precision controllability of the YF-17 airplane

NASA-TP-1677J p 55 N80-23327

Simulator study of conventional general aviation

instrument displays in path-following tasks with emphasis

on pilot-induced oscillations

I NASA-TP-1776} p39 Nat-t4997

A general aviation simulator evaluation of a

rate-enhanced instrument landing system display

{NASA-TP-t960J p 39 N82-14085

Nimbus 6 Random Access Measurement System

applications experiments

{NASA-SP-457] p 165 N83-14835

Wind-weighting for sounding rockets with a telemetry

system

[NASA-TP-2438} p 70 N85-21246

TRACKING RADAR

Free Drifting Buoys

{NASA-CP-2003I p 167 N77-16675

TRACTION

Performance of a Nasvytis multiroller traction drive

[NASA-TP-f378] p 120 N79-13369

Traction drive performance prediction for the Johnson

and Tevaarwerk traction model

{NASA-TP-t5301 p 121 N79-33475

Life analysis of multiroller planetary traction drive

[NASA-TP-1710} p 122 N81-20423

Multiroller traction drive speed reducer: Evalualion for

automotive gas turbine eog_ne

[NASA-TP-2027] p 122 N82-26678

Rolling-element fatigue life with traction fluids and

automatic transmission fluid in a high-speed rolling-contact

rig

[NASA-TP-2050} p 122 N83-t3457

Advanced Power Transmission Technology

[NASA-CP-2210] p 123 N83-20119

Regression analysis of traction characteristics of traction

fluids

[NASA-TP-2t 54 ] p 123 N83-24862

Elastohydrodynamic contacts. Effects of dents and

grooves on traction and local film thickness

[NASA-TP-2175} p 123 N83-28453

Design of traction drives

[NASA-RP-1154] p 125 N88-13734

TRADEOFFS

Solar power satellite system sizing tradeoffs

{NASA-TP-18041 p 145 N81-18493

TRAFFIC

Planning for airport access: An analysis of the San

Francisco Bay area

{NASA-CP-2044} p 198 N79-10942

A-125
TRAILING EDGE FLAPS

SUBJECT INDEX

TRAILING EDGE FLAPS

Low-speed tests of a high-aspect-ratio,

supercrtticat-wing transport model equipped with a high-lift

flap system in the Langley 4- by 7.metar and Ames 12-foot

pressure tunnels

[NASA-TP.2097] p 26 N85-31010

TRAILING EDGES

Theoretical estimation of the transonic aerodynamic

characteristics of a supercritical-wing transport model with

trailing-edge controls

{NASA-TP-t253] p 9 N78-30056

Low-speed wind-tunnel investigation of wing fins as

trailing-vortex-allewation devices on a transport airplane

model

[NASA-TP-14531 p 12 N79-24961

Mean-flow and turbulence measurements in the vicinity

of the trailing edge of an NACA (63 sub t)-012 airfoil

INASA-TP-18451 p 109 N81-23410

Investigation of trailing-edge-flap, spanwise-blowing

concepts on an advanced fighter configuration

I NASA-TP-22501 p 23 N84-t8164

Vortex wake alleviation studies with a variable twist

wing

[ NASA-TP-2442 ] p5 N86-16187

Motion and interaction of decaying trailing vortices in

spanwcse shear wind

I NASA-TP-2599 J p 5 N86-29762

TRAILING-EDGE FLAPS

Laminar Flow Control The Research and Technology

Studies 198 t

[NASA-CP-22181 p 19 N82-20149

TRAINING DEVICES

Technical communication: Perspectives for the eighties,

part 1 Proceedings ol the technical communications

sessions at the 32nd Annual Meeting of the Conference

on College Composition and Commumcation

INASA-CP-2203-PT-t I p 197 N82-14960

TRAINING EVALUATION

An Operational evaluation of head up displays for civil

transport operations NASA/FAA phase 3 report

INASA-TP-tBtS1 p 40 N82-33381

TRAINING SIMULATORS

Effects of magnification and visual accommodation on

atmpo_nt esttmation in simulated landings with real end

virtual image displays

INASA-TP-16351 p 17t N80-34099

Guidelines for line-oriented flight training, volume 2

[ NASA-CP-2t 84-VOL-21 p30 N82-13123

TRAJECTORIES

Thunderstorm-environment interactions determined with

three-dimensional trajectories

I NASA-RP-t0541 p 161 N80-16675

Development and evaluation of a Kalman-filter algorithm

for terminal area navigation using sensors of moderate

accuracy

I NASA-TP-2035 ] p 31 N83-29193

TRAJECTORY ANALYSIS

Analysis of fuel-conservative curved decelerating

approach trajectories for powered-lift and CTOL jet

aircraft

I NASA-TP-1650J p 2 N80-19022

Theory for compuhng the size and shape of a region

of influence associated wdh a maneuvering vehicle

INASA-TP-t6481 p 15 N80-24261

Motion about the stable Iibration points in the linearized,

restricted three-body problem

I NASA-RP-1065 I p203 N81-11970

TRAJECTORY CONTROL

A nonlinear traiectory command generator for a digital

flight-control system

[NASA-TP-1221 i p 54 N79-t3057

Configuration management and automatic control of an

augmentor wing aircraft with vectored thrust

[NASA-TP-1222] p 54 N79-17872

TRAJECTORY MEASUREMENT

Planning fuel-conservative descents with or without time

constraints using a small programmable calculator:

Algorithm development and flight test results

I NASA-TP-20851 p 40 N83-17535

TRAJECTORY OPTIMIZATION

A_gorithm lot fixed-range optimal traiectorles

[ NASA-TP-t 5651 p 30 N80-28329

Evaluation of a computer-generated perspective tunnel

display for flight path following

[NASA-TP-17361 p 39 N81-13958

Piloted simulation of an algorithm for onboard control

ot time-ophmal intercept

[NASA-TP-2445J p 58 N85-28949

TRANSCENDENTAL FUNCTIONS

A characterization of the real zeros of a particular

transcendental function

tNASA-TP-14201 p 185 N79-t8679

TRANSDUCERS

Design and anaiysis of a torsion braid pendulum

displacement transducer

[NASA-TP-1840i p 1 t5 N8t-25352

TRANSFER FUNCTIONS

Proceedings and findings of the 1976 Workshop on Ride

Quality --- passenger acceptance of transportation

syatama

[NASA.CP-2006] p 172 N77.27710

Development and application of an optimization

procedure for flutter suppression using the aerodynamic

energy concept

[NASA-TP-1137] p 127 N78.18459

TRANSFER ORBITS

Comparative analyses of space-to-space centrat power

stations

[NASA-TP-1955] p 66 N82-14202

TRANSFORMATIONS (MATHEMATICS)

Vector-algebra approach to extract Denavit-Hartenperg

parameters of assembled robot arms

[NASA.TP-2191] p t82 N83-3466t

Geometric interpretations of the Discrete Fourier

Transform (DFT)

[ NASA-TP-23321 p 177 N84-24114

TRANSIENT HEATING

Preliminary design procedure for insulated structures

subjected to transient heating

[NASA-TP-1534] p 128 N80-12438

TRANSIENT RESPONSE

Stability of numerical integration techniques for transient

rotor dynamics

[NASA-TP-1092} p t19 N78-10474

Static and transient performance of YF-102 engine with

up to t4 percent core airbleed for the quiet short-haul

research aircraft

I NASA-TP-1692] p 47 N80-25339

Effects of different rub models on simulated rotor

dynamics

{NASA-TP-2220J p 123 N84-17590

TRANSITION METALS

Friction and metal transfer for single-crystal silicon

carbide in contact with vahous metals in vacuum

[NASA-TP-t 19t I p 91 N78-2t294

Wear of single-crystal silicon carbide in contaci with

various metals in vacuum

INASA-TP-1198] p 92 N78-21295

TRANSITION PROBABILITIES

Status of linear boundary-layer stabilit!/and the e to the

nth method, with emphasis on swept-wing applications

INASA-TP-1645J p t08 N80-22633

TRANSLATIONAL MOTION

Decoupled control analysis of a large flexible space

antenna with linear quadratic regulator comparisons

INASA'TP'22931 p 74 N84-23675

Translational control of a graphically s0mulated robot arm

by kinematic rate equations that overcome elbow joint

singularity

I NASA-TP-23761 p 181 N85-15446

TRANSMISSION

Atmosphenc effects on CO2 laser propagation

lNASA-TP-13571 p 152 N79-13607

TRANSMISSION EFFICIENCY

Satellite bower system: Concept development and

evaluation program Volume 3: Power transmission and

reception Technical summary and assessment

I NASA-RP-1076] p 145 N81-27622

TRANSMISSION FLUIDS

Rolling-element fatigue life with traction fluids and

automatic transmission fluid in a high-speed rolling-contact

rig

iNASA-TP.20501 p 122 N83-t3457

TRANSMISSION LINES

Se_ice life evaluation of rigid explosive transfer lines

iNASA-TP-2143] p 36 N83-31596

TRANSMISSION LOSS

Noise transmission loss of aircraft panels using acoustic

intensity methods

INASA-TP-20461 p 188 N82-3t069

Noise transmission loss of a rectangular plate in an

infinite baffle

{NASA-TP-2398] p 190 N85-22109

TRANSMISSIONS (MACHINE ELEMENTS)

Comparisons of modified Vasco X-2 and AIS193t0 gear

steels

[NASA-TP-t73t 1 p 122 N81-14322

Multiroller traction drive speed reducer: Evaluation for

automotive gas turbine engine

I NASA-TP-20271 p 122 N82-26678

Advanced Power Transmission Technology

I NASA-CP-2210] p 123 N83-2Ot19

Thermal anaIysis of a planetary transmission with

spherical roller bearings operating after complete toss of

oil

[NASA-TP-23671 p 124 N84-32824

Testing of YUH-61A hehcopter transmission in NASA

Lewis 2240 kW (3000-hp tacility

[NASA-TP-2538 ! p t26 N86-24992

TRANSMITTERS

Spacecraft transmitter reliability

[NASA-CP-21591 p 76 N81-161t9

TRANSONIC COMPRESSORS

Performance with and without inlet radial distortion of

a transonic fan stage designed for reduced loading in the

tip region

[NASA-TP-1294] p 9 N78.30057

Performance of single.stage axial-flow transonic

compressor with rotor and stator aspect ratios of 1.19

end 1.25 respectively, and with design pressure ratio of

2,05

[NASA-TP-155g} p 46 N80-21325

Performance of single stage axial-flow transonio

compressor with rotor and stator aspect reUoa of 1.53

and 1.78. respectively, and with design pressure ratio of

1.82

[NASA-TP-1974] p 49 N82-19222

TRANSONIC FLIGHT

Flight comparison of the transonic agility of the F.'I 11A

airplane and the F-111 supercriticat wing airplane

[NASA.TP-1368] p 54 N79-13056

Wave drag as the objective function in transonic fighter

wing optimization

[NASA-TP-2265] p 23 N84-17127

TRANSONIC FLOW

Advances in engineering science, volume 4

[NASA-CP-20Ot-VOL-4] p 98 N77-10345

Computation of transonic boattail flow with separation

I NASA-TP-1070I p 7 N78-t3017

Two-dimensional transonic testing with splitter plates

[NASA-TP-1153J p 7 N78-17999

Numerical study of transonic flow over oscillating airfoils

using the full potential equation

INASA-TP-1120] p 8 N78-21055

Performance of single-stage axial-flow transonic

compressor with rotor and stator aspect ratios of t19

and 1.26. respectively, and with design pressure ratio of

t .82

[NASA-TP-1338} p 43 N79-10060

Application of shock tubes to transonic airfoil testing

at high Reynolds numbers

{NASA-TP-1268) p 10 N79-12013

The design of supercritical wings by the use of

three-dimensional transonic theory

[NASA-TP-1400J p 11 N79-16804

CAS2D: FORTRAN program for nonrotating

blade-to-blade, steady, potential transonic cascade flows

[NASA-TP-t7051 p 15 N80-27284

Calculation of three-dimensional unsteady transonic

flows past helicopter blades

[NASA-TP-1721] p 15 N80-33356

Numerical solutions of the Navier-Stokes equations for

transonic aflerbody flows

[NASA-TP-1784] p 16 N81-13919

High-speed laser anemometer system for intrarotor flow

mapping in Iurbomachinery

INASA-TP-16631 p 115 N82-19521

Computer program for calculating full potential transonic,

quasi-three-dimensional flow through a rotating

turbomachinery blade row

INASA-TP-2030 j p 20 N82-28247

Effect of thrust vectoring and wing maneuver dev_:es

oi7 transonic aeroproputsNe characteristics Of a supersonic

fighter

[ NASA-TP-2119 J p22 N84-10025

Aerodynamic design for improved manueverability by

use of three-dimensional transonic theory

NASA-TP-22821 p 23 N84-18161

Transonic flow analysis for rotors. Part 1 :

Three-dimensional quasi-steady, full-potential calculation

NASA-TP-2375-PT-t ] p 25 N85-10914

A comparative study of the nonun_queness problem of

the potential equation

NASA-TP-2385] p 25 N85-15694

Calibration of sonic valves for the laminar flow control,

leading-edge flight test

NASA-TP-2423] p 26 N85-23707

Performance test ot laser velocimeter system for the

Langley 16-foot transonic tunnel

NASA-TP-2502} p 118 N86-t6563

The application to aidoits of a technique for reducing

orifice-induced pressure error at high Reynolds numbers

NASA-TP-2537] p 27 N86-20351

Breakdown ot the conservative potential equation

[NASA-TP-2539] p 28 N86-20352

TRANSONIC FLU'n'ER

Experimental and analytical transonic flutter

characteristics of a geared-elevator configuration

{NASA-TP-1666] p 34 N80-25321

TRANSONIC NOZZLES

Boundary-layer separation on isolated boattail nozzles

{NASA-TP-1226J p 9 N78-30052

TRANSONIC SPEED

Flight evaluation of the transonic stability and control

characteristics of an airplane incorporating a superchtical

wing

[ NASA-TP-1167 I p53 N78-20140

A-126
SUBJECT INDEX

A study of canard-wing interference using experimental

pressure data at transonic speeds

[NASA-TP-1355} p 10 N79-15902

Use of nose cap and fuselage pressure orifices for

determination of air data for space shuttle orbiter below

supersonic speeds

[NASA-TP-1643] p 39 N80-32389

Improved method for calculating transonic velocities on

blade-to-blade stream surfaces of a turbomachine

INASA-TP-1772} p 17 N81-22017

Effect of nozzle and vertical-tail variables on the

performance of a 3-surface F-15 model at transonic Math

numbers --- Langley 16 foot transonic tunnel

{NASA-TP-2043_ p 20 N82-32320

Experimental investigation of a 10-percent-thick

helicopter rotor airfoil section designed with a viscous

transonic analysis code

[ NASA-TP-18641 p 21 N83-30389

An experimental investigation of nacelle-pylon

installation on an unswept wing at subsonic and transonic

speeds

[NASA-TP-2246] p 23 N84-18162

Effects of upper-surface nacelles on longitudinal

aerodynamic characteristics of high-wing transport

configuration

INASA-TP-2579} p 28 N86-23562

TRANSONIC WIND TUNNELS

High Reynolds Number Research

{NASA-CP-2009] p 59 N77-27139

Aerodynamic characteristics at Maeh numbers from 033

to 1.20 of a wing-body design concept for a hypersonic

research airplane

[NASA-TP-t044] p 6 N78-12038

Two-dimensional transonic testing with splitter plates

[NASA-TP-1153} p 7 N78-17999

Onset of condensation effects with an NACA 0012-64

airfoil tested in the Langley 0.3-metar transonic cryogenic

tunnel

{NASA-TP-1385} p 12 N79-22043

A theoretical analysis of simulated transonic boundary

layers in cryogenic-nitrogen wind tunnels

[NASA-TP-1631 I p 59 N80-19131

A fan pressure ratio correlation in terms of Much number

and Reynolds number for the Langley 03 meter transonic

cryogenic tunnel

[NASA-TP-1752] p 16 N81-10005

The high-speed frontier Case histories of four NACA

programs, 1920 - 1950

ENASA-SP-4451 p 3 N81-15969

An application of multivadabte design techniques to the

control of the national transonic facility

[NASA-TP-1887} p 181 N81-29840

Simulation of ideal-gas flow by nitrogen and other

selected gases at cryogenic temperatures --- transonic flow

in cryogenic wind tunnels

[NASA-TP-1901 ] p 109 N81-32418

Longitudinal and lateral static stability and control

characteristics of a 1/6-scale model of a remotely piloted

research vehicle with a supercritical wing

[NA_-TP-1360} p 57 N82-15075

Cryogenic Technology, part 1 --- conference

proceedings; cryogenic wind tunnel design and

instrumentation

{NASA-CP-2122-PT-1 } p 99 N82-20357

Cryogenic Technology, part 2 --- conference

proceedings; cryogenic wind tunnel design and

instrumentation

[NASA-CP-2122-PT-2J p 99 N82-20358

Wind-Tunnel/Flight Correlation, 1981

[NASA-CP-2225] p 19 N82-25196

Flow Visualization and Laser Velocimetry for Wind

Tunnels

[NASA-CP-2243} p 116 N82-32663

Cryogenic Wind Tunnel Models. Design and

Fabrication

[NASA-CP-2262] p 59 N83-18748

Two-dimensional aerodynamic characteristics of an

airfoil designed for two

[NASA-TP-1965} p 24 N84-27694

Wind Tunnel Wall interference Assessment and

Correction, 1983

[NASA-CP-2319] p 25 N85-12011

Aeronautical facilities catalogue. Volume 1: Wind

tunnels

[NASA-RP-t 132] p 60 N85-18991

Aerodynamic characteristics of a high-wing transport

configuration with a over-the-wing nacelle-pylon

arrangement

[NASA-TP-2497] p 27 N86-16193

Studies of condensation effects on aidoil testing in the

Langley 0.3-meter transonic cryogenic tunnel

[NASA-TP-2509} p 113 N86-20720

Static internal performance of a thrust vectoring and

reversing two-dimensional convergent-divergent nozzle

with an aft flap

INASA-TP-2549} p 28 N86-23560

R4 airfoil data corrected for sidewall boundary-layer

effects in the Langley 0 3-meter transomc cryogenic

tunnel

INASA-TP'2565] p 28 N86-24662

TRANSPORT AIRCRAFT

EffeCtS of landing approach methods and separation

intervals on single runway landing capacity

[ NASA-TP-1112} p29 N78-13029

Effect of winglets on a first-generation jet transport wing.

4: Stability characteristics for a full-span model at Mach

0.30

{NASA-TP-11191 p 7 N78-17997

Simulator evaluation of a flight-path-angle control system

for a transport airplane with direct lift control

[NASA-TP-11161 p 53 N78-20139

CTOL transport technology, 1978 - - conferences

INASA-CP-2036-PT-t I p 1 N78-27046

CTOL Transport Technology, 1978 - - conferences

[NASA-CP-2036-PT-21 p 1 N78-29046

Low-speed wind-tunnel parametric investigation of flight

spoilers as trailing-vortex-alleviation devices on a transport

aircraft model

tNASA-TP-14191 p 1 t N79-22038

Low-speed wind-tunnel investigation of wing fins as

trailing-vortex-alleviation devices on a transport airplane

model

{NASA-TP-1453] p 12 N79-24961

An experimental and theoretical investigation of the

effect of nonmetric over-the-wing nacelles on wing-body

aerodynamics

INASA-TP-1503J p 12 N79-29146

Effect of winglets on a first-generation jet transport wing.

6: Stability characteristics for a full-span model at subsonic

speeds --- conducted in Langley 8 foot transonic pressure

tunnel

[NASA-TP-1330] p 12 N80-10101

Subsonic aircraft: Evolution and the matching of size

to performance

[NASA-RP-10601 p 2 N80-29245

Economic evaluation of flying qualities design criteria for

a transport configured with relaxed static stability

[NASA-TP-17601 p 56 N81-13968

Use of constrained optimization in the conceptual design

of a medium-range subsonic transport

[NASA-TP-1762J p 35 N81-16039

Advanced aerodynamics and active controls. Selected

NASA research

[NASA-CP-2172} p 3 N81-t9001

An analytical study of the longitudinal response of

airplanes to positive wind shear

[NASA-TP-t765J p 56 N81-20082

Effect of display size on utilization of traffic situation

display for self-spacing task --- transport aircraft

INASA.TP-1885} p 30 N81-29109

Simulator study of vortex encounters by a twin-engine.

commercial, jet transport airplane

INASA-TP-1966] p 57 N82-19225

Small transport aircraft technology

{NASA-SP-460] p 36 N83-20931

Evaluation of g seat augmentation of fixed-base/moving

base simulation for transport landings under two visually

imposed runway width conditions

[NASA-TP-21351 p 36 N83-22191

Evaluation of a total energy-rate sensor on a transport

airplane

{NASA-TP-22121 p 40 N84-12164

Aerodynamic characteristics, including effect of body

shape, of a Mach 6 aircraft concept

[NASA-TP-2235] p 22 N84-13164

Minimum-fuel, 3-dimensional flightpath guidance of

transfer jets

[NASA-TP-23261 p 58 N84-32394

Expenmental trim drag values and flow-field

measurements for a wide-body transport model with

conventional and supercritical wings

|NASA-TP-2071 ] p 25 N85-10920

Simulator study of flight characteristics of several large.

dissimilar, cargo transport airplanes during approach and

landing

[ NASA-TP-2357 ] p 58 N85-11002

Advanced secondary power system for transport

aircraft

[NASA-TP-24631 p 52 N85-28944

Nacelle/pylon/wing integration on a transport model

with a natural laminar flow nacelle

{NASA-TP-24391 p 26 N85-29924

Low-speed tests of a high-aspect-ratio,

supercritical-wing transport model equipped with a high-lift

flap system in the Langley 4- by 7-meier and Ames 12-foot

pressure tunnels

[NASA-TP-2097] p 26 N85-31010

Energy efficient transport technology Program summary

and bibliography

INASA-RP-11351 p 37 N85-33116

TRAPEZOIDAL WINGS

Ground based and in-flight simulator studies of flight

characteristics of a twin-fuselage passenger transport

airplane during approach and landing

NASA-TP-2451 I p 58 N85-34144

Effect ol aileron deflections on the aerodynamic

characteristics of a semispan model of a subsonic

energy-efficient transport

NASA-TP-24781 p 27 N86-11186

Abrasion behavior of aluminum and composite skin

coupons, stiffened skins and stiffened panels

representative of transport airplane structures

NASA-TP-2520] p 38 N86-13316

Aerodynamic characteristics of a high-wing transport

configuration with a over-the-wing nacelle-pylon

arrangement

NASA-TP-24971 p 27 N86-16193

Effect of underwing aft-mounted nacelles on the

longitudinal aerodynamic characteristics of a high-wing

transport airplane

NASA-TP-24471 p 27 N86-20345

Installation effects of long-duct pylon-mounted nacelles

on a twin-jet transport model with swept suparcritical

wing

NASA-TP-24571 p 27 N86-20346

Strength of graphite/epoxy bolted wing-skin splice

specimens subjected to outdoor exposure under constant

load and yearly fatigue loading

NASA-TP-2542} p 83 N86-20508

A methodology for airplane parameter estimation and

confidence interval determination in nonlinear estimation

problems

[ NASA-RP-11531 p 58 N86-22579

Low-speed stability and control characteristics of a

transport model with aft-fuselage-mounted advanced

turboprops

NASA-TP-2535t p 59 N86-22580

Effects of upper-surface nacelles on longitudinal

aerodynamic charactehstics of high-wing transport

configuration

NASA-TP-25791 p 28 N86-23562

TRANSPORT PROPERTIES

Computer program for obtaining thermodynamic and

transport properties of air and products of combustion of

ASTM-A-1 fuel and air

I NASA-TP-1160} p97 N78-20351

ton confinement and transport in a toroidal plasma with

externally imposed radial electric fields

INASA-TP-1411 ) p 195 N79-19867

WETAIR: A computer code for calculating

thermodynamic and transport properties of air-water

mixtures

[NASA-TP-14661 p 178 N79-23688

Thermodynamic and transport combustion properties of

hydrocarbons with air. Part 1: Properties in Sl units

[NASA-TP-1906] p 195 N82-32186

Thermodynamic and transport combustion properties of

hydrocarbons with air Part 2; Compositions corresponding

to Kelvin temperature schedules in part 1

[ NASA-TP- 1907 ] p 195 N82-32187

Thermodynamic and transport combustion properties of

hydrocarbons with air Purl 3: Properties in US customary

units

[NASA-TP-1908] p 195 N82-32188

Thermodynamic and transport combustion properties of

hydrocarbons with air Part 4: Compositions corresponding

to Rankine temperature schedules in part 3

INASA-TP-19091 p 195 N82-32189

Report of Workshop on Mount Saint Hetens: Its

Atmospheric Effects and Potential Climatic Impact

I NASA-SP-458 ] p 154 N82-32915

Heavy ion transporl in the straight ahead

approximation

[NASA-TP-21781 p 210 N83-29169

Numerical modeling of physical vapor transport in a

vertical cylindrical ampoule, with and without gravity

[NASA-TP-26201 p 96 N86-29040

TRANSPORT THEORY

Low-frequency fluctuation spectra and associated

particle transporl in the NASA Lewis bumpy-tofus

plasma

[NASA-TP-1258] p 194 N78-30944

TRANSPORT VEHICLES

Proceedings and findings of the 1976 Workshop on Ride

Quality --- passenger acceptance of transportation

systems

_NASA-CP-20061 p 172 N77-27710

TRAPEZOIDAL WINGS

Experimenta_ and analytical study of the longitudinal

aerodynamic characteristics of analytically and empirically

designed Strake-wmg configurations at subcritical

speeds

I NASA-TP-1803 ] p 17 N81-25040

A-127
TRAVELING WAVE TUBES SUBJECT INDEX

TRAVELING WAVE TUBES

Thermal characteristics of the 12-gigaherlz. 200-watt

output stage tube for the communications technology

satellite

{ NASA-TP-t 344 ] p69 N78-33137

Efficiency enhancement of octave-bandwidth traveling

wave tubes by use of multistage depressed collectors

[NASA*TP-14161 p 101 N79-17139

Analytical prediction with multidimensional computer

programs and experimental verification of the

performance, at a variety of operating conditions, of two

traveling wave tubes with depressed collectors

[NASA-TP-t449] p 101 N79-22375

Efficiency enhancement of dual-mode traveling wave

tubes at saturation and in the linear range by use of

spent-beam refocusing end multistage depressed

collectors

I NASA-TP-1486) p 101 N79-28420

Multistage depyessed co_lector with efficiency of 90 to

94 percent for operation of a dual-mode traveling wave

tube in the tinear region

[NASA-TP-1670] p 101 N80-21669

Spacecraft transmitter relialmlity

INASA-CP-21591 p 76 N81-t6119

Analytical prediction and expenmental verification of

performance at various operating conditions Of a

dual-mode traveling wave tube with multistage depressed

collectors

[NASA-TP-1831 I p 102 N81-28352

Performance of computer-designed small-sized

four-stage depressed collector for operation of dual-mode

traveling wave tube

INASA-TP-16321 p 102 N81-30360

Computer modeling of multiple-channel input signals and

intermodulation losses caused by nonlinear traveling wave

tube amplifiers

{NASA-TP-19991 p 102 N82-25441

Experimental verification of the multistage depressed

collector design procedure for e h_gh-perveance,

helix-type, t_avehng-wave tube --- in commumcat_"_s

satellites

I NASA-TP-21621 p 102 N83-25985

Performance of computer-designed small-size

multistage depressed collectors for a high-perveance

traveling wave tube

[ NASA TP 22481 p 102 N84-15394

Beam impingement angle effects on secondary electron

emission characteristics of textured pyrolytic graphite

{NASA-TP-22851 p 95 N84-18400

Secondary electron emission charactenstics of

ion-textured copper and high-purity isotropic graphite

surfaces

[NASA-TP-2342 j p 95 N84-28989

Verification of computer-aided designs of traveling-wave

tubes utilizing novel dynamic refocusers and graphite

electrodes for lhe multistage depressed collector

INASA-TP-2524J p 103 N86-13643

Textured carbon on copper: A novel surface with

extremely tow secondary electron emission

characteristics

{NASA-TP-2543] p 96 N86-15394

Secondery-electron-emiss0on losses in multistage

depressed collectors and traveling-wave-tube efficiency

_mprovements with carbon collector e)ectrode sudaces

(NASA.TP-2622] p 103 N86-32629

TREADS

Friction characteristics of three 30 by 11,5-14.5, type

8, aircraft tires with venous tread groove patterns and

rubber compounds

[NASA-TP 10801 p 32 N78-13043

Tire tread temperatures during antiskid braking and

cornering on a dry runway

[NASA-TP-2009] p 35 N82-24193

TRENDS

Ozone Trend Detectability

{NASA-CP-2189J p 153 N82-10624

TRIATOMIC MOLECULES

The optical absorption of triatomi¢ carbon C3 for the

wavelength range 260 to 560 nm

{NASA*TP-1141 ] p 191 N78-20927

TRIBOLOG¥

Friction and wear of iron-base binary alloys in sliding

contact with silicon carbide in vacuum

[NASA-TP-16121 p 93 N80-22494

Effects of erodant particle shape and various heat

treatments on erosion resistance of plain carbon steel

[NASA-TP-1755J p 87 N81-t6210

Correlation of =dea_ and actual shear strengths ot metals

with their friction properties

{NASA-TP-189t ] p 94 N81-27282

R_ationship between the Eleal tensile strer_Jth and the

fncben pfopedies of metals in contact with nonmetals and

themselves

I NASA-TP-18831 p94 N81-33293

Tribologicel characteristics of a composite Iotal-sudace

hip replacement

INASA-TP-1853] p 94 N82-16239

Tribologicat properties at 25 C of seven polyimide films

bonded to 440 C high-temperature stainless stee_

{NASA-TP-1944] p 94 N82-19373

Effect of sliding speed and contact stress on tribological

proberties of ultra-high-molecular.weight polyethylene

{NASA-TP-2059} p 95 N83-14269

Fnction end wear of iron in sulfuric acid

[NASA-TP-22891 p 89 N84-21716

Friction and wear of nickel in sulfuric acid

I NASA-TP-2290] p89 N84-21721

Tribology in the 80's. Volume 1: Sessions 1 to 4

lNASA-CP-2300-VOL-t ] p 124 N84-2389t

Tribology in the 80's. Volume 2: Sessions 5 - 8

INASA-CP-2300-VOL-2J p 124 N84-25047

Herlzien contact in twO and three dimensions

[NASA-TP-24731 p 125 N85-32331

TROPOPAUSE

Sulfate and nitrate collected by filter sampling near the

tropopause

{NASA-TP-t567J p 149 N80-14581

TROPOSPHERE

Fronts and trontogenesis as revealed by high time

resolution data

INASA-RP-1005] p 156 N77-30705

Man's impact on the troposphere: Lectures in

tropospheric chemistry

[NASA-RP-1022J p 151 N79-t0634

Report of the NASA working group on tropospheric

program planning

[NASA-RP-tO62J p 153 N81-23742

Tropospheric Passive Remote Sensing

[NASA-CP-2237} p 1t5 N82-2£:,637

Applying modeling Results in designing a global

tropospheric experiment

INASA-CP-2235] p 153 N82-29796

Proceedings of a Workshop on Assessment of

Techniques for Measuring Troposphebc N sub x O sub y

[NASA-CP-2292] p 154 N84-13706

Proceedings of a Workshop on Research Needs in

Heterogeneous Tropospheric Chemistry

[NASA-CP-2320] p 137 N84-28131

Assessment ot Techniques for Measuring Tropospheric

H sub x O sub y

[NASA-CP-2332] p 155 N85-14336

TRUSSES

Load concentration due to missing members in planar

faces of a large space truss

INASA-TP-1522] p 128 N79-33500

Crash tests ot four _ow-wing twin-engine airplanes "_th

truss-reinforced fuselage structure

INASA-TP-2070I p 13t N83-10442

A mobile work station concept for mechanically aided

astronaut assembly of large space trusses

[ NASA-TP-2108J p 74 N83-19806

Vibration charactenstics of a deployable

controUable-geometry truss boom

[NASA-TP-2160_ p 132 N83-28491

TUBES

Experimental pedect-gas study of expansion-tube flow

charactenstics

INASA-TP-1317] p 106 N79-14327

TUNABLE LASERS

Heterodyne systems and technology, part 1 ---

conferences

INASA-CP-2138-PT-1 I p 117 N80-29652

Excess noise in tunable diode lasers

lNASA-TP-1935) p 117 N82-12431

TUNGSTEN

Feasibility study of tungsten as a diffusion barrier

between nickel-chromium-aluminum and Gamma/Gamma

prime - Delta eutaclic alloys

I NASA-TP-1131 ] p 86 N78-15230

Thermal-conductivity measurements of

tungsten-tiber-reitlforced superalloy composites using a

thermal-conductivity comparator

{NASA-TP-1445] p 80 N79-28234

TUNING

Atmospheric solar absorption measurements in the 9

to 1 t mu m region using a diode laser tleterodyne

spectrometer

[NASA-TP-I72£,I p 153 N60-33996

TURBIDITY

Laboratory measurements of physical chemical, and

optical characteristics of Lake Chicot sediment waters

[NASA-TP-1941} p 140 N82-13468

TURBINE BLADES

Experimental flow coefficients of a full-coverage

litre-cooled-vane chamber

INASA-TP-10361 p 41 N77-32153

Effects of film injection angle on turbine vane cooling

[NASA-TP-t0951 p 104 N78-13379

Method for calculating convective heat-transfer

coefficients over turbine vane surfaces

[NASA-TP-tt34J p 104 N78-17338

Effect of cooling-hole geometry on aerodynamic

pedormance of a film-cooled turbine vane tested with cold

air in a two-dimensional cascade

{NASA-TP-1136] p 8 N78-20080

Two*dimensional cold-air cascade study of a film-cooled

turbine stator blade 4: Comparison of experimental and

analytical aerodynamic results for blade with 12 rows of

0.076-centimeter-(0.030-inch-) diameter holes having

streamwise etec_on angles

( NASA-TP-1151 } p 42 N78-20130

Two-dimensional cold-air cascade study of a film-cooled

turbine stator blade 5: Comparison of experimental and

analytical aerodynamic results for blade with 12 rows of

O038-centimetar-(O.015 inch) diameter coolant holes

having streamw_se ejection angles

[ NASA-TP-1204 _ p42 N78-20133

FORTRAN program for calculating coolant flow and

metal temperatures of a full-coverage-film-cooled vane or

blade

[NASA-TP-1259] p 43 N78-28099

Erosion/corros=on of turbine airfoil materials in the

high-velocity effluent of a pressurized fluidized coal

combustor

[NASA-TP*1274] p 86 N78-28225

AnalySis of metal temperature and coolant flow with •

thermal-barrier coating on a full-coverage-film-cooled

turbine vane

I NASA-TP-13101 p43 N78-31109

TACT 1: A computer program for the transient thermal

analysis of • cooled turbine blade or vane equipped with

a coolant insert. 2. Programmers manual

[NASA-TP-1391 } p 106 N79-18288

Thermal stress analysis of ceramic gas-path seal

components for aircraft turbines

[NASA-TP-1437 ] p92 N79-21205

Review and status of liquid-cooling technology for gas

turbines

{NASA-RP-t038) p 106 N79-22427

Flow visualization of discrete-hole film cooling wffh

spanwise injection over a cylinder

INASA'TP't491| p 44 N79-27142

Computer program for generating input for analysis of

impingement-cooled, axial-flow turbine blade

[NASA-TP-16031 p 107 N80-15361

Prediction method for two-dimensional aerodynamic

losses of cooled vanes using integral boundary-layer

parameters

[NASA-TP-1623] p 14 N80-17030

Effects of a ceramic coating on metal temperatures of

an air-cooled turbine vane

{NASA-TP-15981 p 107 N80-17397

Analysis of uncertainties in lurbine metal temperature

predictions

[NASA-TP-1593] p 46 N80-21326

Nonlinear, three-dimensional finite-element anatys_$ ol

air-cooled gas turbine blades

[NASA-TP-1669] p 129 N80-22734

Computerized video densitometry method for rapid

analysis of infrared photographic images --- temperature

distribution across a turbine blade

{NASA-TP-t686J p 114 N80-25635

Comparison of elastic and elastic-plastic structural

analyses for cooled turbine blade airfoils

t NASA-TP 1679] p 129 N80-27719

WIND: Computer program for calculation of three

dimensiona{ potential compressible flow about wind turbine

rotor blades

{NASA-TP-1729] p 15 N80-33357

Experimental performance end analysis of

15.04-centimeter-tip-diameter, radial-inflow turbine with

work factor of 1 126 and thick blading

[NASA-TP-1730[ p 47 N80-33410

Surface pyrometry in presence of radiation from other

sources with application to turbine blade temperature

measurement

[ NASA-TP-1754] p 47 N81-11039

Fluctuating pressures on fan blades of a turbofan engine:

Static and wind-tunnel investigations

[NASA-TP-1976_ p 168 N82-2t037

Laser anemometer measurements in an annular

cascade of core turbine vanes and comparison with

theory

I NASA-TP-2018 j p20 N82-26234

Static internal performance characteristics of two thrust

reverser concepts for axisymmetric nozzles

fNASA-'I-P-20251 p 20 N62-26235

Film-cooling effectiveness with developing cootant flow

through straight and curved tubular passages

(NASA-TP-20621 p 110 N83-12360

Review and status of heat-transfer technology for

internal passages of air-cooled turbine blades

{NASA-TP-2232] p 111 N84-21828

A-128
SUBJECT INDEX TURBOMACHINERY

Detailed flow measurements in casing boundary layer

of 429-meter-per-second-tip-speed two-stage fan

[NASA-TP-2052] p 51 N84-28795

Advanced High Pressure O2/H2 Technology

[NASA-CP-2372] p 78 N85-26862

Joint research effort on vibrations of twisted plates,

phase 1: Final results

[NASA-RP-t150] p 135 N86-t0579

TURBINE ENGINES

Cold-air performance of a tip turbine designed to drive

a lift fan. 3: Effect of simulated fan leakage on turbine

performance

[NASA-TP-tl09] p 7 N78-16001

Aeropropulsion 1979 --- conferences

[NASA-CP-2092] p 45 N80-10205

Off-design performance loss model for radial turbines

with pivoting, variable-area stators

[NASA-TP-17081 p47 N81-11038

Reasons for low aerodynamic performance of

13.5-centimet er-tip-diametar aircraft engine starter

turbine

[NASA-TP-18t0] p 48 N81-20076

Recent trends in aviation turbine fuel properties

[NASA-TP-2056] p 97 N83-11340

Lewis Research Center spin rig and its use in vibration

analysis of rotating systems

[NASA-TP-2304] p 51 N84-24578

TURBINE PUMPS

Comparison of analysis and experiment for self-acting

seals for liquid-oxygen turbopumps

[NASA-TP-1443] p 120 N79-22519

Advanced High Pressure O2/H2 Technology

[NASA-CP-2372] p 78 N85-26862

Passive eddy-current damping as a means of vibration

control in cryogenic turbomachinery

[NASA-TP-2562] p 68 N86-24722

TURBINES

Cold-air performance of a tip turbine designed to drive

a lift fan

[NASA-TP-1126] p 7 N78-14998

Wind Turbine Structural Dynamics

[NASA-CP-2034] p 144 N78-19616

Design and cold-air test of single-stage uncooled turbine

with high work output

{NASA-TP-1680J p 46 N80-25337

Cold-air investigation of a 4 1/2 stage turbine with

stage-loading factor of 4.66 and high specific work output

2: Stage group performance

[NASA-TP-1688] p 47 N80-25338

Analytic investigation of effect of end-wall contouring

on stator performance

[NASA-TP-1943] p 19 N82-14051

Flow visualization study of the horseshoe vortex in a

turbine stator cascade

[NASA-TP-1884] p 110 N82-30498

Computer code for oft-design performance analysis of

radial-inflow turbines with rotor blade sweep

[NASA-TP-2199] p 50 N83-32807

Exploratory wind-tunnel investigation of a

wingtip-mounted vortex turbine for vortex energy

recovery

[NASA-TP-2468J p 26 N85-26667

TURBOCOMPRESSORS

Performance of single-stage axial-flow transonic

compressor with rotor and staler aspect ratios of 1.19

and 1.26, respectively, and with design pressure ratio of

t 82

[NASA-TP-13381 p 43 N79-10060

Analysis of supersonic stall bending flutter in axial-flow

compressor by actuator disk theory

[NASA-TP-t345] p 10 N79-13003

Aerodynamic performance of 1.38-pressure-ratio,

variable-pitch fan stage

lNASA-TP-1502] p 45 N79-31213

Effects of diffusion factor, aspect ratio and solidity on

overall performance of 14 compressor middle stages ---

the effects of varying both diffusion through the rotor and

compressor blades and blade aspect ratio

{NASA-TP-1523] p 45 N79-33210

Performance of single-stage axial-flow transonic

compressor with rotor and stator aspect ratios of 119

and 1.26 respectively, and with design pressure ratio of

2.05

{NASA-TP-1659] p 46 N80-21325

Computer program for aerodynamic and blading design

of multistage axial-flow compressors

[NASA-TP-t946] p 49 N82-15039

STGSTK: A computer code for predicting multistage

axial flow compressor performance by a meanline stage

stacking method

[NASA-TP-2O20] p 49 N82-25250

TURBOFAN AIRCRAFT

Altitude calibration of an Fro0, S/N P680063, turbofan

engine

[NASA-TP-1228] p 42 N78-23095

TURBOFAN ENGINES

Effects of temperature transients at fan inlet of a turbofan

engine

[NASA-TP-1031 ] p 41 N77-31153

Development and verification ol real-time, hybrid

computer simulation of F100-PW-100(3) turbofan engine

iNASA-TP-1034] p 41 N77-31154

F100 multivariable control synthesis program:

Evaluation of a multivariable control using a real-time

engine simulation

[NASA-TP-10561 p 4t N77-3316g

Altitude test of several afterburner configurations on a

turbofan engine with a hydrogen heater to simulate an

elevated turbine discharge temperature

[ NASA-TP-1068 ] p41 N78-11106

Procedures for generation and reduction of linear models

of a turbofan engine

{NASA-TP-1261 ] p 184 N78-30896

DYGABCD: A program for calculating linear A, B, C,

and O matrices from a nonlinear dynamic engine

simulation

[NASA-TP-1295] p 43 N78-33110

Comparison of calculated and altitude-facility-measured

thrust and airflow of two prototype F100 turbofan

engines

[NASA-TP-1373] p 43 N79-13044

Measurements and predictions of flyover and static noise

of a TF30 afterburning turbofan engine

INASA-TP-1372] p 43 N79-t3045

Operating condition and geometry effects on

low-frequency afterburner combustion instability m a

turbofan at altitude

{NASA-TP-1475] p 44 N79-25022

Evaluation of a simplified gross thrust calculation

technique using two prototype F100 turbofan engines in

an altitude facility

[NASA-TP-14821 p 44 N79-26057

Static test-stand performance of the YF-t02 turbofan

engine with several exhaust configurations for the Quiet

Short-Haul Research Aircraft (QSRA)

{NASA-TP-1556] p 45 N80-t4121

Experimental evaluation of a spinning-mode

acoustic-treatment design concept for aircraft inlets ---

suppression of YF-102 engine fan noise

[NASA-TP-t613t p 46 N80-21323

Analysis of uncertainties in turbine metal temperature

predictions

INASA-TP-1593J p 46 N80-21326

Static and transient performance of YF-102 engine with

up to 14 percent core airbleed for the quiet short-haul

research aircraft

INASA-TP-1692] p 47 N80-25339

Off-design correlation for losses due to part-span

dampers on transonic rotors

[NASA-TP-1693] p 47 N80-28352

Flight evaluation of a simplified gross thrust calculation

technique using an FIO0 turbofan engine in an F-15

airplane

[NASA-TP-1782 ] p48 N81-15000

Forward acoustic performance of a model turbofan

designed for a high specific flow (QF-14)

[NASA-TP-1968i p 188 N82-21036

Fluctuating pressures on fan blades of a turbofan engine:

Static and wind-tunnel investigations

[NASA-TP-19761 p 188 N82-21037

Automated procedure for developing hybrid computer

simulations of turbofan engines Part 1: General

description

{NASA-TP-1851 j p 179 N82-33020

Circumferentially segmented duct lines optimized for

axisymmetric and standing wave sources --- reducing noise

from turbofan engines galerkin method acoustic

atlenuation

[NASA-TP-20751 p 188 N82-34190

Gain selection method and model for coupled propulsion

and airframe systems

[NASA-TP-2067J p 57 N83-11139

Design analysis of a self-acting spirai-groove ring seal

for counter-rotating shafts

[NASA-TP-2142] p 50 N83-25712

Incidence loss for fan turbine rotor blade in

two-dimensional cascade

[NASA-TP-2188] p 50 N83-30431

Ft00 multivariable control synthesis program Computer

implementation of the Fro0 muitivariable control

algorithm

[NASA-TP-2231 I p 51 N84-11171

Rot-flow tests of a series of t0-percent-scale turbofan

forced mixing nozzles

[NASA-TP-22681 p 111 N84-17525

Test-engine and inlet performance of an aircraft used

for investigating fiight effects on fan noise

{NASA-TP-2254J p 189 N84-21277

Study of stator-vane fluctuating pressures in a turbofan

engine for static and flight tests

[NASA-TP-2217] p 189 N84-22363

Fluctuating pressures on fan blades of a turbofan engine,

flight test investigation

I NASA-TP-2381 } p 190 N85-19790

Effects of inlet distortion on a static pressure probe

mounted on the engine hub in an F-15 airplane

[NASA-TP-2411 I p 52 N85-22394

Performance and surge limits of a TF30-P-3 turbofan

engine/axisymmetnc mixed-compression inlet propulsion

system at Mach 2.5

{NASA-TP-2461 I p 52 N85-25261

Digital Electronic Engine Control (DEEC) Flight

Evaluation in an F-t5 Airplane

[NASA-CP-2298] p 52 N86-25342

TURBOFANS

Performance of a transonic fan stage designed for a

low meridional velocity ratio

[NASA-TP-1298] p 43 N78-33t07

Aerodynamic pertormance of a 1 35-pressure-ratio

axial-flow fan stage

[NASA-TP-1299] p 10 NTg-t0022

Forward acoustic performance of a shock-swallowing

high-tip-speed fan (QF-t3)

[ NASA-TP-t668} p 187 N80-23100

TURBOGENERATORS

New features and applications of PRESTO, a computer

code for the performance of regenerative, superheated

steam turbine cycles

I NASA-TP-1954 ] p 145 N82-16477

TURBOJET ENGINES

An Assessment of Technology for Turbojet Engine Rotor

Failures

lNASA-CP-2017] p 41 N78-10068

DYGAEICD: A program for calculating linear A, B, C,

and D matrices from a nonlinear dynamic engine

simulation

I NASA-TP-1295 ] p 43 N78-33110

Dynamic response of a Mach 2.5 axisymmettic inlet and

turbojet engine with a poppet-value controlled inlet stability

bypass system when subjected to internal and external

airflow transients

[NASA-TP-1531 } p 45 N80-14123

Turbojet-exhaust-nozzle secondary-airflow pumping as

an exit control of an inlet-stability bypass system for a

Mach 2.5 axisymmetric mixed-compression inlet --- Lewis

10- by t0-ft, supersonic wind tunnel test

[NASA-TP-1532] p 46 N80-t4124

Effect of cage design on characteristics of

high-speed-let-lubricated 35-millimeter-bore ball bearing ---

turbojet engines

[NASA-TP-f732J p t21 N80-33749

Aerodynamic tests and analysis of a turbojet-boosted

launch vehicle concept (spacejet) over a Mach number

range of 1.50 to 2.86 --- Langley Unitary Plan Wind Tunnel

Tests

[NASA-TP-f888_ p 17 N81-29098

Thrust performance of a variable-geometry, divergent

exhaust nozzle on a turbojet engine at altitude

I NASA-TP-2171 J p 50 N83-26839

TURBOMACHINE BLADES

CAS2D: FORTRAN program for nonrotating

blade-to-blade, steady, potential transonic cascade flows

[NASA-TP-1705] p t5 N80-27284

Improved method for calculating transonic velocities on

blade-to-blade stream surfaces of a turbomachine

[NASA-TP-t772] p 17 N81-22017

Computer program for calculating full potential transonic,

quasi-three-dimensional flow through a rotating

turbomachinery blade row

[NASA-TP-2030] p 20 N82-28247

TURBOMACHINERY

Design and performance of a

427-metar-per-second-tip-speed two-stage fan having a

2,40 pressure ratio

[NASA-TP-13141 p 43 N78-33109

Performance of two-stage fan with larger dampers on

first-stage rotor

[NASA-TP-13991 p 44 N79-23967

Aerodynamic performances of three fan stator designs

operating with rotor having lip speed of 337 meters per

second and pressure ratio of 1.54. 1: Experimental

performance

lNASA-TP-t610] p 46 N80-17071

Rotordynamic instability Problems in high-performance

turbomachinery

INASA-CP-21331 p 121 N80-29706

High-speed laser anemometer system for intrarotor flow

mapping in turbomachinery

[NASA-TP-t663] p 115 N82-t952t

Damping seals for turbomachinery

[NASA-TP-1987] p 49 N82-20183

Rotordynamic instability Problems in High-Performance

Turbomachinery

{NASA-CP-2250j p 122 N83-15629

Aerodynamic effect of a honeycomb rotor tip shroud

on a 50.8-centimeter-tip-diameter core turbine

[NASA-TP-2112] p 49 N83-17547

A-129
TURBOPROP AIRCRAFT SUBJECT INDEX

Comparison of two- and three-dimensional flow

computations with taser anemometer measurements in a

transonic compressor rotor

[NASA-TP-1931 I p 22 N83-32774

Lewis Research Center spin rig and its use in vibration

analysis of rotating systems

INASA-TP-2304 J p 51 N84-24578

Detailed flow measurements in casing boundary iayer

of 429-meter-per second-tip-speed two-stage fan

[ NASA-TP-20521 p 51 N84-28795

Rotordynamic Instability Problems in High-Performance

Turbomaehinery

{NASA-CP-2338] p 124 N85-14116

Instability in Rotating Machinery

{NASA-CP-2409] p 126 N86-30160

TURBOPROP AIRCRAFT

Effects of propeller rotation direction on airplane interior

noise levels

[NASA-TP-2444} p 190 N85-30767

TURBOPROP ENGINES

Fuel economy in aviation

[NASA-SP-462] p 36 N84-15144

TURBULENCE

Evaluation of a vortex model of turbulent cavity flow

--- for computing noise generation of fluid flow

INASA-TP-15051 p 187 N79-32057

Proceedings el the Aero-Optics Symposium on

Electromagnetic Wave Propagation from Aircraft

[NASA-CF-2121] p 108 N80-25588

Description and calibration el the Langley unitary plan

wind tunnel

[NASA-TP-1905] p 18 N82-12035

Three-dimensional turbulenl-mixing-length modeling for

discrete-hole coolant iniection rote a crossflow

[NASA-TP-2200] p 111 N83-34232

Transition in Turbines

INASA-CP-2386] p 113 N85-31433

TURBULENCE EFFECTS

Comparison of experimental and theoretical turbulence

reduction eharactenstics for screens, honeycomb, and

honeycomb-screen combinations

INASA-TP-1958J p 19 N82-14055

TURBULENT BOUNDARY LAYER

Representation of turbulent shear stress by a product

of mean velocity differences

INASA-TP-1029} p 104 N77-31441

Calculation methods for compressible turbulent

boundary tayers, 1976

INASA-SP-4221 p 104 N78-13371

Direct measurements and analysis of skin friction and

cooling downstream of multiple flush-slot iniection into a

turbulent Mach 6 boundary layer

I NASA-TP-1176 p 106 N78-33385

Characteristics of Maoh 10 transitional and turbulent

boundary tayers

INASA-TP-1243 p 106 N79-14328

A theoretical analysis of s_mulated transonic boundary

layers in cryogenic-nitrogen wind tunnels

INASA-TP-1631 p 59 N80-19131

Mean-flow and turbulence measurements in the vicinity

of the trailing edge of an NACA (63 sub 1)-012 aidoil

{NASA-TP-1845 p 109 N81-23410

Effect of low-frequency tones and

turbulent-boundary-layer noise on annoyance

{NASA-TP-2202 p 172 N83-34579

Pressure and heating-rate distributions on a corrugated

surface in a supersomc turbulent boundary layer

[NASA-TP-t024 p 111 N84-10504

Drag of two-dimensional small-amplitude symmetric and

asymmetric wavy walls in turbulent boundary layers

[NASA-TP-2318 p 112 N84-25944

Aerothermai tests of a 125 percent cone st Mach 67

for various Reynolds numbers, angtes of attack and nose

shapes --- conducted in Langley 8-foot high temperature

tunnel

{NASA-TP-2345] p 112 N85-17322

Flight-measured laminar boundary-layer transition

phenomena including stability theory anatysis

[ NASA-TP-2417 ] p25 N85-21118

Transition in Turbines

l NASA-CP-23861 p 1 t 3 N85-31433

Experimental aerodynamic heating to simulated space

shuttle tiles in laminar and turbulent boundary layers with

variable flow angles at a nominal Math number of 7

t NASA-TP-2307t p t 13 N85-34351

TURBULENT DIFFUSION

Performance of a short annular dump diffuser using

suction-stabilized vortices at inlet Math numbers to 041

[ NASA-TP-1194 j p42 N78-20131

Stochastic differential equations and turbulent

dispersion

_NASA-RP-lt03! p 110 N83-22546

TURBULENT FLOW

Representation of turbulent shear stress by a product

of mean velocity differences

INASA-TP-1029] p 104 N77-31441

Mean velocity, turbulence intensity, and scale in a

subsonic turbulent jet impinging normal to a large flat

plate

INASA-TP-t037 p 104 N77-32431

Application of a two-dimensional parabolic computer

program to prediction of turbulent reacting flows

l NASA-TP-1169 p 105 N78-20463

Turbulent-flow separation criteria for overexpanded

supersonic nozzles

INASA-TP-1207 p 105 N78-30554

Volume-energy parameters and turbulent-flow density

fluctuations

[NASA-TP-t585 p 107 N80-17398

Progress in turbulence modeling for complex flow fields

including effects of compressibility

(NASA-TP-1517 p 107 N60-20527

Steady and nonsteady supersonic turbulent afterbody

flow

{NASA-TP-1769 p 16 N8t-16977

Wind-tunnel results for a modified 17-percent-thick

low-speed airfoil section

{NASA-TP-1919 p 18 N82-1t033

The wedge hot-film anemometer in supersonic flow

{NASA-TP-2134 ] p 189 N83-30164

Modeling Interface Motion Of Combustion (MiNCe) A

computer code for two-dimensional, unsteady turbulent

combustion

[NASA-TP-2132] p 50 N83-32806

Review and status of heat-transfer technology lor

internal passages of air-cooled turbine blades

INASA-TP-2232] p 111 N84-21828

A spatial model of wind shear and turbulence for flight

simulation

[NASA-TP-23131 p 165 N84-24044

Drag of two-dimensional small-amplitude symmetric and

asymmetric wavy wails m turbulent boundary layers

[ NASA-TP-2318 ] p 112 N84-25944

A critical evaluat)on of vahous turbulence models as

applied to internal fluid flows

[NASA-TP-2474 ] p 112 N85-25757

Nacellepylonwing integration on a transporl model

with a natural laminar flow nacelle

[NASA-TP-24391 p 26 N85-29924

Experimental aerodynamic heating to simulated space

shutlle tiles in laminar and turbulent boundary layers with

variable flow angles at a nominat Mach number el 7

I NASA-TP-2307 ] p 113 N85-34351

TURBULENT JETS

Interaction of a turbulent-iet noise source with transverse

modes in a rectangular duct

{NASA-TP-1248] p 1 N78-25049

TURBULENT MIXING

Comparison of two computer programs by predicting

turbulent mixing of helium in a ducted supersonic

airstream

[NASA-TP-1166] p 105 N78-22333

TWISTED WINGS

Vortex wake alleviation studies with a variabte twist

wing

[NASA-TP-2442] p 5 NBG-t6187

TWISTING

Joint research effort on vibrations el twisted plates,

phase 1: Finat results

[NASA-RP-tt50] p 135 N86-10579

TWO DIMENSIONAL FLOW

Application of a two-dimensional parabolic computer

program to prediction of turbulent reacting flows

[NASA-TP-1169] p 105 N78-20463

Solution of axisymmetrie and two-dimensional inviscid

flow over blunt bodies by the method of lines

[NASA-TP-t154] p 105 N78-22332

Combustion of hydrogen in a two-dimensional duct with

step fuel injectors

[ NASA-TP-1159j p 42 N78-23093

Prediction method for two-dimensional aerodynamic

losses of cooled vanes using integral boundary layer

parameters

INASA-TP-t623] p 14 N80-17030

Some observations on a new numerica_ method for

solving Navier-Stokes equations

[NASA-TP-1934] p 18 N82-11032

Flow visualization study of the horseshoe vortex in a

turbine starer cascade

[NASA-TP-1884] p 110 N82-30498

incidence _oss for fan turbine rotor blade in

two-dimensional cascade

[NASA-TP-2188] p 50 N83-3043t

Modeling interface Motion Of Combustion (MINOC) A

computer code for two-dimensional, unsteady turbulent

combustion

[NASA-TP-2132] p 50 N83-32806

Experiments in a three-dimensional adaptive-wall wind

tunnel

[NASA-TP-2210] p 22 N83-34906

New techniques for experimental generation of

two-dimensional blade-vortex interaction at low Reynolds

numbers

[ NASA-TP-2551 j p 191 N86-21280

TWO PHASE FLOW

Two-phase choked flow of cryogenic fluids in

converging-diverging nozzles

t NASA-TP-14841 p 107 N79-29468

Depressurization and two-phase flow el water containing

high levels of dissolved mtrogen gas

INASA TP-1839] p 109 N81-28389

U

U.S.S.R. SPACE PROGRAM

The partnership: A history of the Apollo-Soyuz test

project

[ NASA-SP-4209 ] p61 N79-10074

U-2 AIRCRAFT

High altitude perspective --- cost-reimbursable services

using NASA U-2 aircrah

[ NASA-SP-427] p 138 N78-31508

UDIMET ALLOYS

Thermal-fatigue and oxidation resistance of

cobalt-modified Udimet 700 alloy

[NASA-TP-2591 ] p 135 N86-28464

ULTRAHIGH FREQUENCIES

Development of UHF radiometer

[NASA-TP-2504] p 103 N86-20678

ULTRAHIGH VACUUM

Proceedings of workshops to define engineering

requirements for a space vacuum research facility

I NASA-CP-2091 J p 62 N79-26076

ULTRASONIC RADIATION

Analytical Ultrasonics in Materials Research and

Testing

[NASA-CP-2383] p 126 N86-22962

ULTRASONICS

Sound speed measurements in liquid oxygen-liquid

nitrogen mixtures

INASA-TP-2464] p 98 N85-35307

Analytical Ultrasonics in Materials Research and

Testing

I NASA-CP-2383 ] p t26 N86-229.62

ULTRAVIOLET ASTRONOMY

Catalog of far-ultraviolet objective-prism

spectrophotometry: Skylab experiment S-019, ultraviolet

stefler astronomy

[NASA-RP-1031 } p 210 N79-27057

Skylab's astronomy and space sciences

[NASA-SP-404] p 199 N79-34118

The Universe at Ultraviolet Wavelengths: The first twO

years of International Ultraviolet Explorer

I NASA-CP-2171 ] p 203 N81-25893

Advances in Ultraviolet Astronomy: Four Years of lUE

Research

I NASA-CP-2238 j p 201 N82-3t 163

The Space Telescope Observatory, Special session of

Commission 44, IAU lath General Assembly

I NASA-CP-2244] p 202 N82-33296

Future of Ultraviolet Astronomy Based on Six Years of

IUE Research

[NASA-CR-2349] p 203 N85-20961

ULTRAVIOLET DETECTORS

Airborne Lidar measurements of aerosols, mixed layer

heights, and ozone during the 1980 PEPE/NEROS summer

field experiment

[NASA-RP-1143] p 150 N86-16748

ULTRAVIOLET PHOTOGRAPHY

An ultraviolet video technique for visualization of stack

plumes and for measunng sulfur dioxide concentration and

effluent velocity

[NASA-TP-1014} p 147 N77-32622

ULTRAVIOLET RADIATION

The stratcom 8 effort --- stratospheric photochemistry

t NASA-TP-1640 ] p 161 N80-22924

Ozone climatology series Volume 1: Atlas of total

ozone, April 1970 - December 1976

INASA-RP-10981 p 154 N83-16992

User's guide tor SBUV/TOMS ozone derivative

products

{NASA-RP-1 1161 p 165 N84-16720

ULTRAVIOLET SPECTRA

International Ultraviolet Explorer Atlas of O-typespectra

Irom 1200 to 1900 angstrom

INASA-RP-11551 p 204 N86-25307

ULTRAVIOLET SPECTROMETERS

User's guide for the Solar Bsckscattered Ultraviolet

(SBUV) instrument first year ozone-S data set

{NASA-RP-10951 p 164 N82-29826

Ozone Correlative Measurements Workshop

INASA-CP-2362j p 137 N85-23112

A-130
SUBJECT INDEX

UNCAMBERED WINGS

Low-speed aerodynamic characteristics of a highly

swept, untwisted uncambered arrow wing

[NASA-TP-21761 p 22 N83-36000

Body and canard effects on an attached-flow maneuver

wing at Mach 1 62

[NASA-TP-2249] p 23 N84-18163

UNIFORM FLOW

Finite-difference theory for sound propagation in a lined

duct with uniform flow using the wave envelope concept

INASA-TP-t00t } p 185 N77-30908

UNIQUENESS THEOREM

Existence and uniqueness of solutions to a class of

nonlinear-operator-differential equations arising in

automated spaceship navigation

[NASA-TP-1860} p 70 N8t-23182

UNITED STATES

Emerging Energy Alternatives for the Southeastern

States

[NASA-CP-2042] p 144 N78-28615

The space shuttle at work

[NASA-SP-432} p 68 N80-30367

Western Regional Remote Sensing Conference

Proceedings, 1981

[E82-t0104] p 141 N82-22546

Second Eastern Regional Remote Sensing Applications

Conference

[E83-10189] p 141 N83-19141

Eastern Regional Remote Sensing Applications

Conference

[E83-10201} p 141 N83-21419

UNIVAC 1100 SERIES COMPUTERS

User's guide to SFTRAN/1100

[ NASA-TP-1200 } p 178 N78-20806

UNIVERSE

Life in the Universe

[NASA-CP-2156J p 175 N82-20884

UNIVERSITIES

CORSE-81: The 1961 Conference on Remote Sensing

Education

[E83-10179} p 141 N83-17942

The MSFC/UAH Data Management Symposium

[NASA-CP-20401 p 177 N78-74659

UNMANNED SPACECRAFT

Far travelers: The exploring machines

[NASA-SP-480] p 63 N85-33126

UNSTEADY FLOW

Steady and nonsteady supersonic turbulent afterbody

flow

[NASA-TP-1769] p 16 N81-16977

Compressible, unsteady lifting-surface theory for a

helicopter rotor in forward flight

[NASA-TP-2503} p 27 N86-18289

New techniques for experimental generation of

two-dimensional blade-vortex interaction at low Reynolds

numbers

[NASA-TP-2551 ] p 191 N86-21280

Expenmental study of the effects Of installation on

singleand counter-rotation propeller noise

[NASA-TP-254t] p 191 N86-26162

UNSWEPT WINGS

Correlation of laser veiocimeter measurements over a

wing with results of two prediction technKlues --- in the

Langley V/STOL tunnel

[NASA-TP-t168J p 105 N78-21410

Application of modal control to wing-flutter

suppression

[NASA-TP-1983} p 57 N82-24209

An experimental investigation of nacelle-pylon

installation on an unswept wing at subsonic and transonic

speeds

{NASA-TP-2246 p 23 N84-18162

UPPER ATMOSPHERE

High Resolution Infrared Spectroscopy Techniques for

Upper Atmosphebc Measurements

[NASA-CP-2134 p 152 N80-27866

NASA/MSFC FY-80 Atmospheric Processes Research

Review

[NASA-CP-2145 p 153 N80-28965

NASA/MSFC FY-81 Atmospheric Processes Research

Review

INASA-CP-2204 p 164 N82-t6660

NASA/MSFC FY-82 atmospheric processes research

review

[NASA-CP-2259 p 165 N83-19391

NASA/MSFC PY-83 Atmospheric Processes Research

Review

[NASA-CP-2281 p 165 N83-33494

Review of spectroscopic parameters for upper

atmospheric measurements

[NASA-CP-2396 p 192 N86-t3064

UPPER SURFACE BLOWN FLAPS

Longitudinal aerodynamic characteristics of a

vectored-engine-over-wing configuration at subsonic

speeds --- Langley V/STOL tunnel tests

INASA-TP-1533] p 12 N79-33164

Experimental study of acoustic _oads dO an

upper-surface-blown STOL airplane configuration ---

Langley full-scale wind tunnel tests

{NASA-TP-15771 p 187 N80-13879

UPWASH

Effect of fuselage upwash on the supersonic longitudinal

aerodynamic characteristics of 2 fighter configurations

[ NASA-TP-2330t p 24 N84-27676

UPWELLING WATER

Laboratory measurements of upwelled radiance and

reflectance spectra ol Calvert, Ball, Jordan, and Feldspar

soil sediments

INASA-TP-1039] p 167 N78-12645

Laboratory and field measurements of upwelled radiance

and reflectance spectra of suspended James River

sediments near Hopewell, Virginia

{NASA-TP-1292] p t47 N78-33616

Laboratory upwelled radiance and reflectance spectra

of Kerr reservoir sediment waters

INASA-TP-1993] p 150 N82-21774

URANUS (PLANET)

Uranus and Neptune

[NASA-CP-23301 p 208 N85-11927

URBAN RESEARCH

A diagnostic mode_ for studying daytime urban air quality

trends

{ NASA-TP-1843} p t49 N81-22587

URBAN TRANSPORTATION

Summary report: Workshop on Vehicle Ride Quality

INASA-CP-20131 p 172 N78-11705

Planning for airport access: An analysis of the San

Francisco Bay area

INASA-CP-2044J p 198 N79-I0942

USER MANUALS (COMPUTER PROGRAMS)

User's guide for SFTRAN/360

INASA-TP-1006t p t76 N78-10746

Sixth NASTRAN Users' Colloquium

INASA-CP-20181 p t27 N78-12443

User's guide to SFTRAN/1100

I NASA-TP-1200 } p 178 N78-20806

The N-BOD2 user's and programmer's manual

I NASA-TP-1145 } p 70 N78-21200

Guide to a condensed form of NASTRAN

iNASA-RP-10tg] p t78 N78-33791

User's manuat for MMLE3, a genera_ FORTRAN program

for maximum likelihood parameter estimation

INASA-TP-1563} p 176 N81-12744

Office of Space Terrestrial Applications

(OSTA)/Applicatlons Data Service (ADS) data systems

standards

J NASA-CP-21961 p 65 N82-15095

Application of a computerized vibroacoustic data bank

for random vibration criteria development

INASA-TP-1998} p 73 N82-20238

User's guide for the Solar Backscattered Ultraviolet

(SBUV) instrument first year ozone-S data set

INASA-RP-t095] p 164 N82-29826

The Snowmelt-Runoff Model (SRM) users manual

INASA-RP-1100] p 141 N83-23660

The NASTRAN theoretical manual

INASA-SP-221(06)] p 132 N84-18677

The NASTRAN user's manual

INASA-SP-222(06)] p 133 N84-21899

Operating system for a real-time mu_tiprocessor

propulsion system simulator Users manual

INASA-TP-2426] p t80 N85-17596

Real-Time Multiprocessor Programming Language

(RTMPL) user's manual

(NASA-TP-2422] p 179 N85-28610

Integrated Composite Analyzer (ICAN): Users and

programmers manual

INASA-TP-2515] p 83 N86-21614

The NASTRAN demonstration problem manual, level

17.5

I NASA-SP-224(05)} p t 30 N81-71592

The NASTRAN programmers manual, level 175

I NASA-SP-223(05) } p 130 N8t-7t 594

USER REQUIREMENTS

Analysis of data systems requirements for global crop

production forecasting in the 1985 time frame

INASA-TP-1164] p 138 N78-18497

Ruggedized minicomputer hardware and software

topics, 1981: Proceedings of the 4th ROLM MIL-SPEC

Computer User's Group Conference

(NASA-CP-2206] p 180 N82-14829

Office of Space Terrestnal Applications

(OSTA)/Applicatlons Data Service (ADS) data systems

standards

INASA-CP-2196] p 65 N82-t5095

Computer Science Research at Langley

INASA-CP-2236] p 176 N82-26996

Space Station Technology, 1983

INASA-CP-2293] p 67 N84-18277

Trends in Planetary Data Analysis Executive summary

of the Planetary Data Workshop

INASA-CP-2333 ] p 208 N84-34363

VAPOR JETS

V

V/STOL AIRCRAFT

Cold-air performance of a tip rE,rhine designed to dnve

a lift fan

[ NASA-TP-11261 p7 N78-14998

A nonlinear frajectory command generator for a digital

flight-control system

[NASA-TP-1221 ] p 54 N79 13057

Configuration management and automatic control of an

augmentor wing aircraft with vectored thrust

INASA-TP-12221 p 54 N79-17872

A comparison of lhe V/STOL handling qualities of the

VAK-191B with the requirements of AGARD report 577

and MIL-F-83300

{NASA-TP-14941 p 54 N79-27182

A unique lacltity for V/STOL aircraft hover testing ---

Langley Impact Dynamics Research Facility

[ NASA-TP-1473 J p 59 N79-29199

Theoretical and experimental investigation of

ground-induced effects for a low-aspect-ratio highly swept

arrow-wing configuration

[ NASA-TP-15081 p 54 N79-31223

VACUUM

Outgassing data for spacecraft matebals

[NASA-RP-1061 I p 80 N80-30441

VACUUM EFFECTS

Materials processing in space: Early experiments

[NASA-SP-443 } p 82 N81-t6075

Effect of vacuum processing on outgassing within an

orbiting molecular shield

{NASA-TP-19801 p 99 N82 19390

VACUUM MELTING

Effect of double vacuum melting and retained austenite

on rolling-element fatigue life of AMS 5749 bearing steel

{NASA-TP-1060] p 119 N77-33520

Comparisons of modified Vasco X-2 and AIS19310 gear

steels

{NASA-TP-1731 ] p 122 N81-14322

A mechanical property and stress corrosion evaluation

of VIM-ESR-VAR work strengthened and direct double

aged Inconel 718 bar material

INASA-TP-2634] p 68 N86-30753

VACUUM TESTS

Fnction and metal transfer for single-crystal silicon

carbide in contact with various metals in vacuum

{NASA-TP-1191 ] p 91 N78-21294

Evaluation of materials for high performance solar

arrays

[NASA-TP-1220] p 92 N78-22233

Outgassing data for selecting spacecraft materials

INASA-RP-1124] p 82 N84-26751

VALUE ENGINEERING

Engineering handbook on the atmospheric

environmental guidelines for use in wind turbine generator

development

{NASA-TP-1359] p 159 N79-14679

VALVES

Single-stage electrohydraulic servosystem for actuating

on airflow valve with frequencies to 500 hertz

{NASA-TP-1678] p 56 N80-29369

VANADIUM ALLOYS

Effects of geometric variables on rub characlenstics ol

Ti-6AI-4V

[NASA-TP-1835] p 88 N81-20245

VANES

Effect of coolant flow ejection on aerodynamE

performance of low-aspect-ratio vanes. 2: Performance

with coolant flow election at temperature ratios up to 2

{NASA*TP-1057] p 6 N78-11008

Method for calculating convective heat-transfer

coefficients over turbine vane surfaces

{NASA-TP-1134] p 104 N78-t7338

Effect of cooling-hole geometry on aeredynam_c

performance of a film-coo_ed turbine vane tested with cold

air in a two-dimensional cascade

{ NASA-TP-11361 p 8 N78 20080

Gas turbine ceramic-coated-vane concept with

convection-cooled porous metal core

[ NASA-TP-19421 p48 N82-t 4090

Study of stator-vane fluctuating pressures in a turbofan

engine for static and flight reels

{NASA-TP-2217} p 189 N84-22363

Expenmental evaluation of two turning vane designs for

high-speed corner of 0 1-scale model of NASA Lewis

Research Center's proposed altitude wind tunnel

[NASA-TP-25701 p 60 N86-28101

VAPOR DEPOSITION

Growth of high-quality thin-film Ge single crystals by

plasma-enhanced chemical vapor deposition

[NASA-TP-25321 p t00 N86-20586

VAPOR JETS

Vapor ingestion in Centaur liquid-hydrogen tank

[NASA-TP-1061 I p 104 N77-33444

A-131
VAPORPHASEEPITAXY SUBJECT INDEX

VAPOR PHASE EPITAXY

Numerical modeling of physica_ vapor transport m a

vertica{ cylindrical ampoule, with and without gravity

{ NASA-TP-2620] p 96 N66-29040

VAPOR PHASES

Physical and numerical sources of computational

inefficiency in integration of chemical kinetic rate

equations: Etiology, treatment and prognosis

[NASA-TP-2590] p 183 N86-28662

VAPOR PRESSURE

Triple point determinations of monomethylhydrazine and

nitrogen {etroxide, 2.2 percent by weight nitric oxide

[NASA-RP-1013] p 96 N78-13234

VAPORIZING

Premixed Prevaporized Combustor Technology Forum

[ NASA-CP-2078] p 44 N79-24994

Effect of degree of fuel vaporization upon emissions

for a premixed partially vaporized combustion system ---

for gas turbine engines

tNASA-TP-1582J p 46 N80-14125

VAPORS

Nitrogen dioxide vapor penetration of chiorobutyl rubber

SCAPE under operational conditions

tNASA-TP-1605_ p 85 N80-16118

VARACTOR DIODES

Topics in the optimization of millimeter-wave mixers

[NASA-TP-2287 ] p 103 N84-20758

VARIABILITY

Variability of annoyance response due to aircraft noise

[NASA-TP-1335J p t86 N79-18687

Cloud-encounter and particle-concentration variabilities

from GASP data

{NASA-TP-1886] p 164 N82-15677

Ozone Correlative Measurements Workshop

INASA-CP-2362J p 137 N85-23112

VARIABLE CYCLE ENGINES

Supersonic cruise technology

{NASA-SP-472] p 4 N85-28912

VARIABLE GEOMETRY STRUCTURES

Off-design performance loss model for radiat turbines

with pivoting, variable-area stators

I NASA-TP-t 7081 p47 N81-11038

Vortex wake alleviation studies with a variable twist

wtng

[NASA-TP-2442] p 5 N86-t6187

VARIABLE PITCH PROPELLERS

Aerodynamic performance of 1 38-pressure-ratio,

variable-pitch fan stage

I NASA-TP-15021 p45 N79-31213

VARIABLE SWEEP WINGS

Flight-measured buffet characteristics of a supercritica]

wing and a conventional wing on a variable-sweep

airplane

[NASA-TP-1244J p 8 N78-23056

VARIATIONS

Fluctuating surface pressure and acoustic radiation for

subsonic normal jet impingement

INASA-TP-1361} p 186 N79-19813

Effects of sound level fluctuations on annoyance caused

by aircraft-flyover noise

[NASA-TP-15761 p 187 N80-13880

VECTOR ANALYSIS

Charactenstic vector analysis of inflection ratio spectra:

New technique for analysis of ocean color data

[NASA-TP-2428 ] p 143 N85-23237

VECTORS (MATHEMATICS)

NASF transposition network: A computing network for

unscrambling p-ordered vectors

INASA-TP-1426} p 180 N79-21822

Simulation development and evaluation of an improved

longitudinal velocity vector control wheel steering mode

and electronic display format

[ NASA-TP-1664 i p 39 N80-30305

Computer simutahon ot random variables and vectors

with arbitrary probability distribution laws

[NASA-TP-18591 p 183 N81-23838

Vector-algebra approach to extract Oenavit-Hartenberg

parameters of assembled robot arms

INASA-TP-2191} p 182 N83-34661

Acceleration ol convergence of vector sequences

INASA-TP-2193] p 182 N84-13885

Measurements of Solar Vector Magnetic Fields

{NASA-CP-23741 p 210 N85-29869

VEGETATION

Demonstration of wetland vegetation mapping in Fionda

from computer-processed satellite and aircraft

multispectrat scanner data

[NASA-TP-1553] p t39 N80-15535

The Multispectral Imaging Science Working Group.

Volume 1: Executive summary

iE85-10001 I p 142 N85-11404

The Multispectral Imaging Science Working Group.

Volume 2: Working group reports

tE85-100021 p 142 N85-11405

VELOCITY

Simulation development and evaluation of an improved

longitudinal velocity vector control wheel steering mode

and electronic display format

[NASA-TP-1664J p 39 N80-30305

VELOCITY DISTRIBUTION

Induced velocity field of a iet in a crossflow

[NASA-TP-1087] p 105 N78-26392

Effect of rotor meridional velocity ratio on response to

inlet radial and circumferential distortion

{NASA-TP-t278] p 45 N79-28177

Velocity field of a round jet in a cross flow for vadous

jet iniect,'on angles and velocity ratios --- Langley V/STOL

tunnel

[NASA-TP-1506] p 107 N79-32500

Improved method for calculating transom¢ velocities on

blade-to-blade stream surfaces of a turbomachioe

[NASA-TP-17721 p 17 N81-22017

Velocity grad,'ent method for caluletiog velocities in an

axisymmetric annular duct

[NASA-TP-20291 p 20 N82-29270

Naturai laminar flow experiments on modern airplane

surfaces

{NASA-TP-22561 p 24 N84-26660

Slip-boundary equations for multicomponent

nonequilibrium airflow

{NASA-TP-24521 p 113 N86-14530

VELOCITY MEASUREMENT

Laser Doppler Velocimetry Workshop

[ NASA-CP-2084 ] p 117 N79-22455

A Scanning taser-vetocimetor technique for measuring

two-dimensional wake-vortex velocity distributions ---

Langley Vortex Research Facility

I NASA-TP-166t I p 114 N80-24594

Dynamic behavior of a beam drag-force anemometer

[NASA-TP-1687] p 114 N80-24595

An experimental and theoretical investigation of

deposition patterns from an agricultural airplane

I NASA-TP-2348t p 25 N84-33379

Dynamic measurement of total temperature, pressure

and velocity in the Langley O.3-meter transonic cryogenic

tunnel

[NASA-TP-25841 p 60 N86-24709

VENTILATION

Performance characteristics of axisymmetric

convergent-divergent exhaust nozzles with longitudinal

slots in the divergent

[NASA-TP-2013} p 19 N82-26231

VENTURI TUBES

Effect of swider-mounted mixing venturi on emissions

of flame-tube combustor using jet A fuel

{NASA-TP-f 393 ] p44 N79-t 4099

Venturi nozzle effects on fuel drop size and nitrogen

oxide emissions

{NASA-TP-2028 ] p4g N82-31329

VENUS (PLANET)

The voyage of Mariner 10: Missions to Venus and

Mercury

[NASA-SP-4241 p 61 N78-27146

Pioneer Venus

iNASA-SP-461 I p 207 N83-30340

The geology of the terrestrial planets

l NASA-SP-469] p 200 N85-18888

VERBAL COMMUNICATION

Technical communication: Perspectives for the eighties,

part 1 Proceedings of the technical communications

sessions at the 32nd Annual Meeting of the Conference

on College Composition and Communication

[NASA-CP-2203-PT-1 ] p 197 N82-14960

VERTICAL DISTRIBUTION

Application of a Gaussian multilayer diffusion model to

characterize dispersion of vertical HCI column density in

rocket exhaust clouds

(NASA-TP-1956J p 149 N82-14672

A stability analysis of AVE-4 severe weather

soundings

INASA-TP-20451 p 164 N83-14824

VERTICAL LANDING

Description of the VTOL Approach and Landing

Technology (VALT) CH-47 research system

INASA-TP-1436] p 54 N79-29195

VERTICAL MOTION

Human discomfort response to noise combined with

vertical vibration

[NASA-TP-t374j o 171 N79-22761

VERTICAL MOTION SIMULATORS

Influence of display and control compatibility on

pilot-induced OScillations

{NASA-TP-1936] p 172 N82-14804

VERTICAL TAKEOFF

Description of the VTOL Approach and Landing

Technotogy (VALT} CH-47 research system

{NASA-TP-t436J p 54 N79-29195

VERTICAL TAKEOFF AIRCRAFT

Study of the application of an implicit model-following

flight controller to lift-fan VTOL aircraft

INASA-TP-t040] p 53 N78-16063

Theoretical flow characteristics of inlets for tilting-nacelle

v'rOL aircraft

[NASA-TP-1205] p 42 N78-21114

Theoretical study of VTOL tilt-nacelle axisymmetric inlet

geometries

[NASA-TP-1380} p 10 N7g-14996

A comparison of the V/STOL handling qualities of the

VAK-191B with the requirements of AGARD report 577

and MIL-F-83300

[NASA-TP-1494] p 54 N79-27182

Aerodynamic performance ot axial-flow fan stage

operated at nine inlet guide vane angles --- to be used

on vertical lift aircraft

[NASA-TP-1510] p 45 N79-31214

Flight tests of the total automatic flight control system

('rafcos) concept on a DHC-6 Twin Otter aircraft

[NASA-TP-1513J p 55 N80-17081

VERY LONG BASE tNTERFEROMETRY

Large Space Antenna Systems Technology, part 1

[NASA-CP-2269-PT-f ] p 67 N83-26853

VIBRATION

Experimental studies of effects of tilt and structural

asymmetry on vibration characteristics of thin-wall circular

cylinders partly filled with liquid

{NASA-TP-1211] p 127 N78-28480

Discomfort criteria for single-axis vibrations

[NASA-TP-t422J p 171 N79-23662

Vibration characteristics of a deployable

controllable-geometry truss boom

{NASA-TP-2160J p 132 N83-28491

Dynamic behavior of spiral-groove and Rayleigh-Step

setf-ectieg face seals

[NASA-TP-2266) p 51 N84-f6181

Lewis Research Center spin rig and its use in vibration

enelys_s of rotating systems

[NASA-TP-2304J p 51 N84-24578

A formulation of rotor-airframe coupling for design

analysis of vibrations of helicopter airframes

[NASA-RP-t089J p 133 N84-33832

Numerical Techniques in Acoustics

[NASA-CP-2404] p 190 N86-12007

Rotorcraft Dynamics 1984

{ NASA-CP-2400] p 38 N86-15280

Testing of YUH-61A helicopter transmission in NASA

Lewis 2240-kW (3000-hp facility

[NASA-TP-2538J p 126 N86-24992

VIBRATION DAMPING

Space shuttle ective-pogo-suppressor control design

using linear quadratic regulator techniques

{NASA-TP-1217} p 101 N79-14309

An analytical technique for predicting the charactanatios

of a flexible wing equipped with an active

flutter-suppression system and comparison with

wind-tunnel data

INASA-TP-1367] p 128 N79-17264

A method for obtaining practical flutter-suppression

control laws using results of optimal control theory

[NASA-TP-1471] p 128 N79-28614

Self-tuning regulators for multicyctic controi of helicopter

vibration

INASA-TP-1996} p 57 N82-20188

Regions of attraction and ultimate boundedness for

linear quadratic regulators with nonlinearities

[ NASA-TP-2322] p 181 N84-28538

Effects of model error on control of large flexible space

antenna with comparisons of decoupled and linear

quadratic regulator control procedures

[NASA-TP-2604] p 75 N86-30801

VIBRATION EFFECTS

An investigation of ride quality rating scales

INASA-TP-1064} p 171 N78-11696

Effect of vibration duration on human discomfort ---

passenger comfort and random vibration

INASA-TP-1283J p 171 N78-327t7

Human discomfort response to noise combined w_th

vertical vibration

INASA-TP-13741 p 171 N79-22761

Vibration characteristics of walls and a plate glass

window representative ol those of a wood-frame house

I NASA-TP-1447 ] p 128 N79-24372

The vibration characteristics of a coupled helicopter

rotor-fuselage by a finite element analysis

[NASA-TP-2118] p 36 N83-18714

VIBRATION ISOLATORS

Pertormance of two-stage fan with a first-stage rotor

redesigned tO account for the presence of a part-span

damper

l NASA-TP-14831 p 45 N79-30191

VIBRATION MEASUREMENT

Joint research effort on vibrations of twisted plates,

phase 1: Final results

(NASA-RP-11501 p 135 N86-10579

A-132
SUBJECT INDEX VOLUME

Instability in Rotating Machinery

[NASA-CP-2409] p 126 N86-30160

VIBRATION MODE

Vibration characteristics of a steadily rotating slender

nog

[NASA-TP-t775] p 130 N81-14343

VIBRATION SIMULATORS

Lewis Research Center spin eg and its use in vibration

analysis of rotating systems

{NASA-TP-2304J p 51 N84-2457B

VIBRATION TESTS

Tire stiffness and damping determined from static and

free-vibration tests --- aircraft tires

[NASA-TP-t671 ] p 29 N80-27302

Rotordynamic Instability Problems in High-Performance

Turbomachinery

[NASA-CP-2250J p 122 N83-15629

Vibration, acoustic, and shock design and test criteria

for components on the Solid Rocket Boosters (SRB),

Lightweight External Tank (LW'T), and Space Shuttle Main

Engines (SSME)

[NASA-RP-11271 p 134 N85-10405

VIBRATIONAL SPECTRA

Vibrational-Rotational Spectroscopy For Planetary

Atmospheres, volume 1

{N_,SA-CP-2223-VOL-t } p 207 N82-25043

VIBRATORY LOADS

Preliminary vibration, acoustic, and shock design and

test cdtena for components on the Lightweight External

Tank (LWT)

[NASA.RP-1074] p 71 N61-19218

Experimental investigation of active loads control for

aircraft landing gear

[NASA-TP-2042J p 36 N62-31321

VIDEO COMMUNICATION

Design of a video teleconference facility for a

synchronous satellite communications link

{NASA-TP-1376} p 100 N79-t4275

VIDEO EQUIPMENT

An ultraviolet video technique for visualization of stack

plumes and for measuring sulfur dioxide concentration and

affluent velocity

[NASA-TP-1014] p 147 N77-32622

VIKING LANDER SPACECRAFT

Viking Lander imaging investigation: Picture catalog of

primary mission experiment data record

{NASA-RP-1007} p 205 N78-20042

Viking '75 spacecraft design and test summary Volume

1: Lander design

[NASA-RP-1027-VOL-1 } p 71 NGt-10100

Viking 75 spacecraft design and test summary. Volume

3: Engineering test summary

[NASA-RP-1027-VOL-3 } p71 N81-11102

On Mars: Exploration of the red planet, 1958 - 1978

{NASA-SP-4212] p 208 N84-35248

Conclusion of Viking Lander Imaging Investigation:

Picture catalog of experiment data record

{NASA-RP-1137} p 208 N85-21099

VIKING LANDER 1

Viking 1: early results --- Mars atmosphere and surface

examinations

{NASA-SP-4Oa} p 70 N76-28296

Determination of the

hypersonic-continuum/rarefied-flow drag coefficient of the

Viking lander capsule 1 aeroshell from flight data

INASA-TP-1793J p 3 N81-14961

Viking lander imaging investigation during extended and

continuation automatic missions. Volume 1: Lander 1

picture catalog of experiment data record

{NASA-RP-1068] p 206 N81-25012

VIKING LANDER 2

Viking lander imaging investigation during extended and

continuation automatic missions. Volume 2: Lander 2

picture catalog of experiment data record

[NASA-RP-1068-VOL-2] p 207 N82-16028

VIKING MARS PROGRAM

The Martian landscape --- Viking Mars mission and

photographs

[NASA-SP-425} p 205 N79-12984

Second International Colloquium on Mars: Abstracts

for a colloquium --- bibliography

[NASA-CP-2072} p 205 N79-16757

Images of Mars: The Viking extended mission

[NASA-SP-444] p 206 N80-26239

Viking '75 spacecraft design and test summary. Volume

1: Lander design

[NASA-RP-1027-VOL-1 ] p 71 N81-10100

Viking '75 spacecraft design and test summary Volume

2: Orbiter design

{NASA-RP-1027-VOL-2J p 71 N81-I0101

Viking orbiter views of Mars

[NASA-SP-441 J p 200 N81-11966

Viking lander imaging investigation during extended and

continuation automatic missions. Volume 1: Lander 1

picture catalog of experiment data record

[NASA-RP-1068t p 206 N81-25012

Viking site selection and certification

[NASA-SP-429} p 207 N81-25992

Viking lander imaging investigation during extended and

continuation automatic missions. Volume 2: Lander 2

picture catalog of experiment data record

[NASA-RP-1068-VOL-2} p 207 N82-t6028

Phobos: Close encounter imaging from the Viking

Orbiters

[NASA-RP-t10g} p 207 N84-32330

VIKING ORBITER SPACECRAFT

Viking '75 spacecraft design and test summary Volume

2: Orbiter design

[NASA-RP-t027-VOL-2} p 71 N81-10101

Viking '75 spacecraft design and test summa_ Volume

3: Engineering test summary

[NASA-RP-1027-VOL-3] p 71 N81-11102

A Catalog of Selected Viking Orbiter Images

INASA-RP-10931 p 207 N83-25636

On Mars: Exploration of the red planet, 1956 - 1976

[ NASA-SP-42121 p 208 N84-35246

VIKING ORBITER I

Viking 1: early results --- Mars atmosphere and surface

examinations

[NASA-SP-408} p 70 N76-28296

VIKING 1 SPACECRAFT

Research in the use of electrets in measuring effluents

from rocket exhaust of the space shuttle (6.4 percent

scaled model) and Viking 1 launch

[NASA-TP-1073] p 147 N76-11517

VIRGIN ISLANDS

SAGE measurements of the stratospheric aerosol

dispersion and loading from the Soufriere Votcano

[NASA-TP-t922J p 153 N82-12687

VIRGINIA

Quantitative analysis of aircraft multispectral-scanner

data and mapping of water-quality parameters in the James

River in Virginia

{NASA-TP-1021 ] p 147 N78-t3628

Laboratory and field measurements of upwelled radiance

and reflectance spectra of suspended James River

sediments near Hopewell, Virginia

[NASA-TP-1292] p 147 N78-33616

VIRTUAL PROPERTIES

Effects of magnification and visual accommodation on

aimpoint estimation in simulated landings with real and

virtual image displays

[NASA-TP-1635] p 171 N80-34099

VISCOELASTICITY

Gaussian step-pressure loading of rigid viscoplastic

plates

[NASA-TP-1123} p I27 N78-20536

VISGOPLASTICITY

Nonlinear Constitutive Relations for High Temperature

Application, 1984

[NASA-CP-2369] p 134 N85-31530

VISCOSITY

Transport properties of oxygen

[ NASA-RP-t 102 ] p 110 N83-24800

Lubrication of machine elements

{NASA-RP-1126] p 124 N84-31640

Measurement of viscosity of gaseous mixtures at

atmospheric pressure

[NASA-TP-2582] p 117 N86-24962

VISCOUS DAMPING

Influence of oil-squeeze-film damping on steady-state

response of flexible rotor operating to supercritical

speeds

[NASA-TP-t0941 p 41 N78-13064

VISCOUS FLOW

The effects of curvature and viscosity on baroclinic

instability: A two-layer model

{NASA-TP-1328] p 159 N76-32641

A hybridized method for computing

high-Reynolds-number hypersonic flow about blunt

bodies

[NASA-TP-1497] p 107 N79-33441

Velocity-split Navier-Stokes solution procedure for

incompressible high Reynolds number external flows

[NASA-TP-16551 p 108 N80-21702

Viscous-inviscid calculations of jet entrainment effects

on the subsonic flow over nozzle afterbodies

[NASA-TP-1626) p 14 N80-22261

Numerical simulation of steady supersonic flow --- spatial

marching

INASA-TP-1749] p 17 N81-22018

Experimental investigation of a t0-percent-thick

helicopter rotor airfoil section designed with a viscous

transonic analysis code

(NASA-TP-1864] p 21 N83-30389

The disturbance flow field produced by an evolving

vortex

I NASA-TP-2245 } p 111 N84-13500

Viscous-inviscid interaction method including wake

effects for three-dimensional wing-body configurations

[NASA-TP-1910J p 24 N64-27682

VISIBLE INFRARED SPIN SCAN RADIOMETER

VISSR Atmospheric Sounder (VAS) Research Review

[NASA-CP-2253} p 165 N83-24028

An evaluation and comparison of vertical profile data

from the VISSR Atmospheric Sounder (VAS)

[NASA-TP-2425_ p 166 N85-16351

VAS demonstration: (VISSR Atmospheric Sounder)

description

{NASA-RP-1151} p 166 N86-13867

VISUAL AIDS

Magnitude of visual accommodation to a heed-up

display

[NASA-TP-t796} p 173 N81-17711

VISUAL CONTROL

Effects of magnification and visual accommodation on

aimpoint estimation in simulated landings with real and

virtual image displays

INASA-TP-1635] p 171 N80-34099

Motion/visual cueing requirements for vodex encounters

dunng simulated transport visual approach and landing

{NASA-TP-2136] p 36 N83-22192

Automated rendezvous and docking: A parametric

study

{NASA-TP-2314] p 74 N64-23677

VISUAL OBSERVATION

Airline pilot scan patterns during simulated ILS

approaches

INASA-TP-1250_ p 171 N79-19682

Procedures for precap visual inspection

INASA-RP-1122} p 103 N85-13156

VISUAL PERCEPTION

Analysis and design of a refractive virtual image

system

{NASA-TP-t066J p 193 N78-12829

Simulator study of the effect of visual-motion time delays

on pilot tracking performance with an audio side task

[NASA-TP-1216] p 32 N78-30090

Head-up transition behavior of pilots during simulated

low-visibility approaches

INASA-TP-16181 p 173 N80-26039

Effects of magnification and visual accommodation on

aimpoint estimation in simulated landings with real and

virtual image displays

INASA.TP-1635} p 171 N80-34099

Motion/visual cueing requirements for vortex encounters

dunng simulated transporf visual approach and landing

[NASA-TP-2136] p 36 N83-22192

VISUAL SIGNALS

Effects of visual and motion simulation cueing systems

on pilot performance dunog takeoffs with engine failures

{NASA-TP*t365] p 32 N79-14082

VISUAL TASKS

Evaluation of several secondary tasks in the

determination of permissible time delays in simulator visual

and motion cues

INASA-TP-1214J p 32 N78-30089

VOICE COMMUNICATION

information transfer problems in the aviation system

[NASA-TP-t875] p 30 N81-31162

VOLATILITY

Outgassing data for spacecraft materials

[NASA-RP-1061 ] p 80 N80-30441

Outgassing data for selecting spacecraft materials

NASA-RP-f 124} p 82 N64-26751

VOLCANOES

Volcanic features of Hawaii A basis for comparison

with Mars

INASA-SP-403] p 152 N80-23912

SAGE measurements of the stratospheric aerosol

dispersion and loading from the Soufdere Volcano

NASA-TP-1922_ p 153 N82-12687

Report of Workshop on Mount Saint Helena: its

Atmospheric Effects and Potential Climatic Impact

NASA-SP-458] p 154 N82-32915

Atmospheric Effects and Potential Ciimatic Impact of

the 1980 Eruptions of Mount St. Helena

NASA-CP-2240] p 136 N83-11534

Airborne rider measurements of El Chichon stratospheric

aerosols, October 1982 to November 1982

NASA-RP-11361 p 155 N65-19550

Airborne lider measurements of El Chichon stratospheric

aerosols

NASA-RP-11481 p 155 N86-13850

SAGE Aerosol Measurements Volume 2: I January -

31 December 1980

NASA-RP-1149] p 156 N86 23088

Airborne lidar measurements of El Chichon stratoshperpc

aerosols

NASA-RP-1166} p 156 N86-27835

VOLCANOLOGY

Planetary geology in the 1980s

[NASA-SP-467J p 200 N85-23457

VOLUME

Geometric relationships for homogenization in

single-phase binary alloy systems

INASA-TP-13491 p 87 N79-13137

A-133
VORTEXALLEVIATION

Volume-energy parameters and turbulent-flow density

fluctuations

[NASA-TP 15851 p 107 N80-17398

Time dependence of solid-particle impingement erosion

of an aluminum alloy

[NASA-TP 2169j p 89 N83-32908

VORTEX ALLEVIATION

Vortex wake alleviation studies with a variable twist

wing

[NASA TP-2442[ p 5 N66-16187

VORTEX AVOIDANCE

Mellon/visual cueing requirements for vortex encounters

during simulated transport visual approach and landing

[ NASA-TP-2136] p 36 N83-22192

VORTEX BREAKDOWN

Wake Vortex Minimization

[NASA-SP-4091 p 6 N78-12017

VORTEX FLAPS

Effects el vortex flaps on the tow-speed aerodynamic

charactenstlcs of an arrow wing

INASA-TP-19141 p 3 N82-11013

Vortex Flow Aerodynamics, volume 1

i NASA-CP-2416-VOL-1 ] p 28 N86-27190

VORTEX GENERATORS

Experimenta} study of wing leading-edge devices for

improved maneuver performance of a supercritical

maneuvenng fighter conhguratien --- Langley 7- by 10-ft

high speed tunnel tests

I NASA TP-21251 p21 N83-22162

Summary Proceedings of a Wind Shear Workshop

[ NASA-CP-22701 p 165 N83-25265

New techniques for experimenta_ generation of

two-dimensional blade-vortex interaclion at low Reynolds

numbers

INASA-TP-2551 b p 191 N86-21280

VORTEX SHEETS

A distributed vortex method for computing the vortex

field of a missile

l NASA-TP-t 183 I p 8 N78-25058

VORTICES

Wake Vortex Mmim_zation

[ NASA.SP-409 ] p6 N78-12017

Performance of a short annular dump diffuser using

suction-stabilized vortices at inlet Mach numbers to 041

INASA-TP-1194 I p 42 N78-20131

Low-speed wind-tunnel parametric investigation of flight

spoilers as traiting-vortex-alleviahon devices on a transport

aircraft model

INASA-TP-f4f91 p tl N79-22038

Performance of a vortex-controlled diffuser in an annular

swirl-can combustor at inlet Maeh numbers up to 053

I NASA-TP 1452 I p44 N79-22099

Low-speed wmd.tunnel investigahon of wing fins as

trading-vortex-alleviation devices on a transport airplane

model

[NASA-TP-1453] p 12 N79-24961

Evaluation of a vortex model of turbulent cavity flow

--- for computing noise generation el fluid flow

[NASA-TP 15051 p 187 N79-32057

inclusion of unsteady aerodynamics in longitudinal

parameter estimation from flight data --- use of vortices

and malhematieal models for parameterization from flight

characteristics

]NASA-TP-t5361 p t3 N80-12995

Evaluahon of hehcopter noise due to b blade-vortex

interaction for five tip configurations --- conducted in the

Langley V/STOL tunnel

iNASA-TP-1608] p 187 N80-14840

A Scanning laser-veloc=meter technique for measuring

two-d_menslona[ wake-vortex velocity distributions ---

Langley Vortex Research Facility

[NASA-TP-1661] p 114 N80-24594

Water-tunnel and analytical investigation of the effect

of strake design vanables on strake vortex breakdown

characteristics

;NASA TP-16761 p 15 N80-28304

Gortler vortices and transihon in wall boundary layers

of two Mach 5 nozzles

[NASA-TP-18691 p 109 N81-31509

Simulator study of vortex encounters by a twm-engine,

commercial jet trat_sport airplane

I NASA-TP-t966] p 57 N82-19225

Ftow visua4ization study of the horseshoe vortex in a

_urbme staler cascade

[NASA-TP-18841 p 110 N82-30498

Motlon/vtsua_ cueing requirements for vortex encounters

during simulated transport visual approach and landing

INASA-TP-21361 p 36 N63-22192

Modeling interface Motion el Combustion (MiNOC), A

computer code for two-dimensional, unsteady turbulent

combustion

[NASA TP 2132! p 50 N83-32806

The disturbance flow field produced by an evolving

vortex

i NASA-TP 2245 ] p 111 N84-13500

Airfoil interaction with impinging vortex

{NASA-TP-2273 ] p 23 N84-18159

Simulation of a cockpit-display concept for executing a

wake-vortex avoidance procedure

[NASA-TP-2300J p 40 N84-21542

Vortex-generating coolant-flow-passage design for

increased film-cooliog effectiveness and surface

coverage

INASA-TP-2388I p 112 N85-12314

Explorator_ wind-tunnel investigation of a

wingtip-mounted vortex turbine for vortex energy

recovery

INASA-TP-24681 p 26 N85-26667

Lee-side flow over delta wings at supersonic speeds

tNASA-TP-2430j p 26 N85-29921

Vortex wake alleviation studies with a variable twist

wing

[NASA-TP-2442J p 5 N86-t6187

Vortex Flow Aerodynamics, volume 1

[NASA-CP-2416-VOL-t j p 28 N86-27190

Motion and interaction of decaying trailing vortices in

spanwise shear wind

]NASA-TP-2599J p 5 N86-29762

VOYAGER PROJECT

Voyager to Jupiter and Saturn

INASA-SP-420] p 205 N77-29046

Voyage to Jupiter

[NASA-SP-4391 p 206 N81-10910

Voyages to Saturn

[NASA-SP-451 I p 207 N82-26152

Voyager 1 and 2 atlas el six Saturnian satellites

[NASA-SP-474 ] p 208 N84-35242

Uranus and Neptune

[ NASA-CP-2330 ] p 208 N85-11927

W

WAKES

Wake-shock interaction at a Mach number of 6

{NASA-TP-11031 p 105 N78-22331

Simulation of a cockpit-display concept for executing a

wake-vortex avoidance procedure

I NASA-TP-23001 p40 N84-21542

Motion and interaction of decaying trailing vortices in

spanwise shear wind

tNASA-TP'2599] p 5 N86-29762

WALL FLOW

Analytic investigation of effect of end wall contouring

on stator performance

[NASA-TP 19431 p 19 N82-14051

Velocity gradient method for calulating velocities in an

axisymmetnc annular duct

INASA'TP'20291 p 20 N82-29270

WALL TEMPERATURE

Film-cooling effectiveness with developing coolant flow

through straight and curved tubular passages

[ NASA-TP-2062 J p 110 N83-12360

Walt-temperature effects on the aerodynamics of a

hydrogen-fueled transport concept in Mech 8 biowdown

and shock tunnels

[NASA-TP-2159] p 21 N83-30391

WALLS

Analytical and expenmental investigation of stator

endwail contounng in a small axial-flow turbine. 1: Staler

performance

[ NASA-TP-2023 j p49 N83-11125

WARNING SYSTEMS

Some human factors issues in the development and

evaluation of cockpit alerting and warning systems

{NASA-RP-1055] p 173 N80-15821

Summary Proceedings of a Wind Shear Workshop

[NASA-CP-2270] p 165 N83-25265

WASTE DISPOSAL

Laboratory measurements of radiance and reflectance

spectra of dilute secondary-treated sewage sludge

{NASA-TP-10891 p 147 N78-12555

Nuclear waste disposal in space

lNASA-TP-1225] p 144 N78-23571

Disposal of radioactive iodine m space

iNASA-TP-1313] p 172 N78-31740

Spectral measurements of ocean-dumped wastes tested

in the marine upwelled spectral signature _aboratory

[NASA-TP-1480t p 168 N79-31890

WASTE TREATMENT

Controlled ecological life support system - biological

problems

I NASA-CP-2233 ] p 173 N82-24836

Controlled Ecological Life Support System First

Principal Investigators Meeting

[ NASA-CP-2247 ] p 174 N83-30016

WASTE WATER

An evaluation of the NASA Tech House, including Iive-m

test results, volume 1

INASA-TP-1564! p 145 N80-11559

SUBJECT INDEX

WATER

Catalytic decomposition of methanol for onboard

hydrogen generation

[ NASA-TP-1247 ] p 97 N78-25236

Low toxic corrosion inhibitors for aluminum in fresh

water

I NASA-TP-1279] p 86 N78-28226

Investigation of effects of background water on upwelled

reflectance spectra and techniques tot analysis of dilute

primary-treated sewage sludge

{NASA-TP-1446] p 168 N79-28864

Experimental study el cluster formation in binary mixture

of H20 and H2SO4 vapors in the presence of an _onlzing

radiation source

INASA-TP-17351 p 149 N81-11565

Optical observations of unidirectional solidification in

microgravity

INASA-TP-2110J p 88 N83-16492

WATER CIRCULATION

North Atlantic Deep Water Formation

[NASA-CP-23671 p 169 N85-26028

WATER POLLUTION

Laboratory and field measurements of upwetled radiance

and reflectance spectra of suspended James River

sediments near Hopewell, Virginia

[NASA-TP-1292J p 147 N78-33616

Quantitative mapping by remote sensing of an ocean

acid-waste dump

[ NASA-TP-1275 ] p 147 N78-33617

Radiometer requirements for Earth-observation systems

using large space antennas

INASA-RP-1101J p 116 N83-28410

WATER QUALITY

Quantitatwe analysis of afrcraff multispectral-scanner

data and mapping of water-quality parameters in the James

River in Virgima

[NASA-TP-1021 I p 147 N78-13626

NASA JSC water monitor system: City of Houston field

demonstration

[NASA-RP-1041 J p 198 N79-28062

Atmospheric Effects and Potenhal Climatic impact of

the 1980 Eruptions of Mount St. Hetens

[NASA-CP-22401 p 136 N83-11534

WATER RUNOFF

Operational Applications of Satellite Snowcover

Observations

IE80-10167] p 139 N80-25742

Applications systems verification and transfer project,

Volume 1 : Operational applications of satellite snow cover

observations: Executive summary --- usefulness of satellite

snow-cover data for water yield prediction

I NASA-TP-18221 p 140 N82-20617

Applications systems verification and transfer project

Volume 2: Operational applications of satellite snow-cover

observations and data-collection systems in the Arizona

test site

INASA-TP-1823] p t40 N82-20618

Applications systems verification and transfer project.

Volume 3: Operational applications of satellite snow cover

observations in California

[NASA-TP-1824] p 140 N82-20619

Applications systems verification and transfer proiect.

Volume 4: Operational applications of satellite snow cover

observations. Colorado Field Test Center

I NASA-TP-1825) p 140 N82-20620

Applications systems verification and transfer project.

Volume 5: Operational applications of satellite snow-cover

observations, northwest United States

INASA-TP-18261 p 140 N82-20621

Applications systems verification and transfer project,

Volume 6: Operational applications of satellite snow-cover

observations NOAA/NESS support study

lNASA-TP-18271 p 140 N82-20622

Applications systems verification and transfer project,

Volume 7: Cost/benefit analysis for the ASVT on

operational applications of satellite snow-cover

observations

[NASA-TP-1828] p 141 N82-20623

Applications systems verification and transfer proiect.

Volume 8: Satellite snow mapping and runoff prediction

handbook

[NASA-TP-t829] p 141 N82-20624

Remote Sensing of Snow and Evapotranspiration

INASA-CP-2363 j p 143 N85-23223

WATER VAPOR

Water*vapor pressure control in a volume

INASA-TP-1172] p t47 N78-20654

DiAL with heterodyne detection including speckle noise:

Aircraft/shuttle measurements of 03, H20, and NH3 with

pulsed tunable CO2 lasers

[NASA-TP-17251 p 115 N80-30717

Two-dimensional model studies of the effect of

supersomc aircraft operations on the stratosphenc ozone

content

]NASA-RP-10641 p 149 N81-17622

A-134
SUBJECT INDEX WEIGHTLESSNESS

Water vapor measurement system in global atmospheric

sampling program, appendix

[NASA-TP-2051 ] p 150 N83-13643

VISSR Atmospheric Sounder (VAS) Research Review

[NASA-CP'2253] p 165 N83-24028

Potential spin-offs of the carbon dioxide observational

platform system (CO-OPS) for remote sensing

opportunities

[NASA-TP-2510] p 68 N85-34149

WATERSHEDS

Operational Applications of Satellite Snowcover

Observations

[E80-10167] p 139 N80-25742

Applications systems verification and transfer project.

Volume 2: Operational applications of satellite snow-cover

observations and data-collection systems in the Arizona

test site

[NASA-TP-1823] p 140 N82-20618

Applications systems verification end transfer proiect,

Volume 4: Operational applications of satellite snow cover

observations. Colorado Field Test Center

[NASA-TP-t825J p 140 N82-20620

WAVE ATTENUATION

Propagation effects on satellite systems at frequencies

below 10 GHz, a handbook for satellite systems design,

1st edition

[NASA-RP-1108] p 100 N84-13397

WAVE DRAG

Wave drag as the objective function in transonic fighter

wing optimization

[NASA-TP-2265] p 23 N84-f7127

WAVE FRONTS

Sonic-boom wave-front shapes and curvatures

associated with maneuvering flight

[NASA-TP-1611] p 13 N80-14045

WAVE PROPAGATION

Atmospheric effects on CO2 laser propagation

[NASA-TP-1357] p t52 N79-13607

Computation of atmospheric attenuation of sound for

fractional.octave bands

[NASA-TP-1412] p 186 N79-17659

The wave structures of the Eady model of baroctinic

instability

[NASA-TP-1548] p 160 N79-32796

Proceedings of the Aero-Opbcs Symposium on

Electromagnetic Wave Propagation from Aircraft

[NASA-CP-2121] p 108 N80-25588

Propagation effects handbook for satellite systems

design: A summary of propagation impairments on 10

to 100 GHz satellite links with techniques for system

design

[NASA-RP-f082] p 100 N82-15270

Analytical Ultrasonics in Materials Research and

Testing

{NASA-CP-2383} p 126 N86-22962

WAVELENGTHS

Surface pyrometry in presence of radiation from other

sources with application to turbine blade temperature

measurement

[NASA-TP-1754] p 47 N81-t103g

Power spectral measurements of clear-air turbulence

to long wavelengths for altitudes up to 14,000 meters

[NASA-TP-1979] p 164 N82-24790

Surface radiation budget for climate applications

[NASA-RP-1169] p 167 N86-28574

WEAR

Effect of carbon content on fdction and wear of cast

irons

[NASA-TP-1052] p 85 N77-32286

Friction and wear behavior of single-crystal silicon

carbide in contact with titanium

NASA-TP-1035] p 91 N77-32312

Friction and wear of single-crystal and polycrystalline

maganese-zinc fernte in contact with various metals

NASA-TP-105g] p 91 N78-10295

Friction and wear of several compressor gas-path seal

movements

NASA-TP-1128] p 86 N78-15229

Friction and wear of polyethylene oxide polymer having

range of molecular weights

NASA-TP-t12g) p 91 N78-15278

Lubrication and failure mechanisms of graphite fluoride

films

NASA-TP-1197] p 91 N78-20337

Friction and wear of radiofrequeney-sputlered bondes,

silicides, and carbides

NASA-TP-1156] p 91 N78-20338

Friction and wear of selected metals and alloys in sliding

contact with AISI 440 C stainless steel in liquid methane

and in liquid natural gas

[NASA-TP-1150] p 119 N78-20512

Ferrographic analysis of wear particles from sliding

elastohydrodynamie experiments

[NASA-TP-1230] p 11g N78-22377

Friction and wear characteristics of iron-chromium alloys

in contact with themselves and silicon carbide

[NASA-TP-1387] p 120 N79-14387

Effect of sterilization irradiation on friction and wear of

ultrahigh-molecular-weight polyethylene

{NASA-TP-1462] p 92 N79-23216

Friction and wear characteristics of wire-brush skids

[NASA-TP-1495] p 33 N79-29171

Lubricating and wear mechanisms for a hemisphere

sliding on potyimide-bonded graphite fluoride film

NASA-TP-15241 p 93 N79-30381

Surface chemistry of iron sliding in air and nitrogen

lubricated with hexadecane and hexadecane containing

dibenzyl-dilsutfide

NASA-TP-1545J p 79 N79-31346

Ferrographic analysis of wear debris from full-scale

bearing fatigue tests

NASA-TP-1511 ] p 121 N79-31605

Lubrication and wear mechanisms of polyimide-bonded

graphite fluoride films subjected to low contact stress

[ NASA-TP-1584 J p93 N80-t7220

Wear particles of single-crystal silicon carbide in

vacuum

NASA-TP-t 6241 p93 N80-18178

Steady-state wear and friction in boundary lubrication

studies

NASA-TP-16581 p 93 N80-22493

Friction and wear of iron-base binary alloys in sliding

contact with silicon carbide in vacuum

NASA-TP-1612] p 93 N80-22494

Effects of geometric variables on rub characteristics of

Ti-6AI.4V

NASA-TP-1835] p 88 N81-20245

Tribological properties at 25 C el seven polyimide films

bonded to 440 C high-temperature stainless steel

NASA-TP-1944t p 94 N82-19373

Surface chemistry and wear behavior of single-crystal

silicon carbide sliding against iron at temperatures to 1500

C in vacuum

[NASA-TP-1947] p 94 N82-19374

Friction wear and auger analysis of iron implanted with

1.5-MeV nitrogen ions

[NASA-TP-1989] p 88 N82-21300

Wear mechanism based on adhesion

[NASA-TP-2037] p 122 N82-32737

Plastic deformation at surface during unlubricated

sliding

[NASA-TP-2036J p 122 N83-11496

Effect of sliding speed and contact stress on triboiogicai

properties of ultra-high-molecular-weight polyethylene

(NASA-TP-2059] p 95 N83-14269

Morphology of an aluminum alloy eroded by a iet of

angular particles impinging at normal incidence

[NASA-TP-21391 p 89 N83-24641

Friction and wear behavior of aluminum and composite

airplane skins

[NASA-TP-22621 p 37 N84-17175

Tribotogy in the 80'a Volume 1: Sessions t to 4

[NASA-CP-2300-VOL-1 I p 124 N84-23891

Effect of humidity on fretting wear of several pure

metals

[NASA-TP*24031 p 90 N85-13006

Effect of five lubricants on life of A_SI 9310 spur gears

[NASA-TP-2419] p 116 N85-16099

WEAR INHIBITORS

Nitridiog of titanium and titanium: 8 percent aluminum,

1 percent molybdenum, 1 percent vanadium alloy with an

ion-beam source

INASA-TP-21491 p 89 N83-24640

WEAR TESTS

Wear of single-crystal silicon carbide in contact with

various metals in vacuum

INASA-TP-1198i p 92 N78-21295

Some effects of composition on friction and wear of

graphite-fiber-reinforced polyimide liners in plain spherical

bearings

[NASA-TP-1229] p 119 N78-25433

Effect of nitrogen-containing plasma on adherence.

friction, and wear of radiofrequency-sputtered titanium

carbide coatings

[NASA-TP-1377] p 92 N79-15184

Friction and wear with a single-crystal abrasive grit of

silicon carbide nn contact with iron base binary alloys in

oil: Effects of alloying etement and its contenl

(NASA-TP-13941 p 120 N79-17227

Wear of aluminum and hypoeutectic aluminum-silicon

alloys in boundary-lubricated pin-on disk sliding

{NASA-TP-14421 p 87 N79-21184

Surface chemistry of iron sliding in air and nitrogen

lubricated w_th hexadecane and hexadecane containing

dibenzyl-dilsulfide

[NASA-TP-1545i p 79 N79-31346

Evaluation and auger analysis of a

zinc-diatkyl-dithiophosphate antiwear addituve in several

diester lubricants

INASA-TP 15441 p 93 N79-32359

Wear, friction, and temperature characteristics el an

aircraft tire undergoing braking and cornering

INASA-TP-1569] p 29 N80-13013

Friction and wear of iron in corrosive metal

INASA-TP-19851 p 88 N82-20291

Occurrence of spherical ceramic debris in indentation

and sliding contact

[NASA-TP-20481 p 95 N82 32491

Sliding induced crystallization of metallic glass

J NASA-TP-21401 p88 N83-21110

Friction and wear of iron in sulfuric acid

{NASA-TP-22891 p 89 N84-21716

Friction and wear of nickel in sulfuric acid

[NASA-TP-2290] p 89 N84-21721

Tribology in the 80's Volume 2: Sessions 5 - 8

[NASA-CP-2300-VOL-2J p 124 N84-25047

WEATHER

Fourth National Aeronautics and Space Administration

Weather and Climate Program Science Review

INASA-CP-2076] p 159 N79-20633

Sun, weather, and climate

[NASA-SP-426] p 209 N79-20961

Summary of the NASA/MSFC FY-79 Severe Storm and

Local Weather research review --- cloud physics,

atmospheric electricity, and mesoscate/storm dynamics

reserech

[NASA-CP-21051 p 160 N79-33722

A comparative analysis of rawinsonde and NIMBUS 6

and TIROS N satellite profile data

[NASA-RP-10701 p 162 N81-15640

Goddard Laboratory for Atmospheric Science, collected

reprints 1978-1979, volume 1

[NASA-TP-1788-VOL-11 p 163 N81-21686

NASA/MSFC FY-81 Atmospheric Processes Research

Review

{NASA-CP-2204] p 164 N82-16660

Proceedings: Fifth Annual Workshop on Meteorological

and Environmental Inputs to Aviation Systems

[NASA-CP-21921 p 3 N82-21t39

NASA/MSFC FY-82 atmospheric processes research

review

[NASA-CP-2259J p 165 N83-19391

NASA/MSFC FY-83 Atmospheric Processes Research

Review

[NASA-CP-2281 J p 165 N83-33494

WEATHER FORECASTING

Third National Aeronautics and Space Administration

Weather and climate program science review

{NASA-CP-2029J p 159 N79-20575

A stability analysis of AVE-4 severe weather

soundings

[NASA-TP-2045] p 164 N83-14824

VISSR Atmospheric Sounder (VAS) Research Review

I NASA-CP-2253] p 165 N83-24028

Global Scale Atmospheric Processes Research Program

Review

INASA-CP-2344] p 166 N85 14360

Meteorological and Environmental inputs to Aviation

Systems

INASA-CP-2388] p 166 N86-11735

Compendium of meteorology scientific issues of 1950

still outstanding

[NASA-RP-1167] p 156 N86-25900

WEBS (SUPPORTS)

Fabrication and evalualion of superplastlcally

formed/weld-brazed corrugated compression panels with

beaded webs

INASA-TP-25121 p 90 N86-t340_

WEDGE FLOW

Expenmental and analytical investigation el a

nonaxisymmetric wedge nozzle at static conditions

[NASA-TP-1186/ p 8 N78-26109

WEDGES

Elastic-plastic finite-e_emenl analyses of lhermal_y

cycled single-edge wedge specimens

{NASA-TP-1982] p 130 N82-20565

Elastic-plastic finite-element analyses of thermally

cycled double-edge wedge specimens

[ NASA-TP-19731 p 130 N82-20566

Experimental investigation of two nonaxisymmetrnc

wedge nozzles at free stream Mach numbers up to 1 20

INASA-TP-20541 p 20 N82-32322

WEIGHTLESSNESS

Liquid jet impingement normal 1o a disk in zero gravity

INASA-TP-10171 p 104 N77-30413

Biomedical results from Skylab

[NASA-SP-377] p 169 N77 33780

]he use of nonhuman primates nn space

[NASA-CP-005] p 169 N78-11663

Draining characteristics of hemispherically bottomed

cylinders in a low-gravity environment

{NASA-TP-1297] p 106 N78-31384

Axial iet mixing of ethanol in cyhndrical containers during

weightlessness

[NASA-TP-1487] p 97 N79-28350

A-135
WEIGHTLESSNESS SIMULATION SUBJECT INDEX

Contoured tank outlets for draining of cylindrical tanks

in _ow-gfavity environment --- Lewis Research Center Zero

Gravity Facility

[NASA-TP-1492J p 107 N79-29467

A mobile work station concept for mechanically aided

astronaut assembly of large space trusses

(NASA-TP-21081 p 74 N83-19806

Analytical and numerical studies of the thermocapillary

flow in a uniformly floating zone

[NASA-TP-2576I p 113 N86-23851

WEIGHTLESSNESS SIMULATION

Physiological responses of women to simulated

weightlessness: A review of the first female bed-rest

study

tNASA-SP-430_ p 170 N79-13686

WELD TESTS

Study of austenitic stainless steel welded with low alloy

steel filler metal --- tensile and impact strength tests

JNASA-TP-1460] p 87 N79-28288

WELDED JOINTS

Fabrication and evsiuatlon of superplestically

formed/weld-brazed corrugated compression panels with

beaded webs

[NASA-TP-2512] p 90 N86-13406

WELDING

Elevated temperature behavior of superplestically

formed/weld-brazed titanium compression panels having

advanced shaped stiffeners

[NASA-TP-2123J p 88 N83-19889

Welding, Bonding and Fastening, 1984

I NASA-CP-2387 ] p 79 N86-11227

WETLANDS

Demonstration of wetland vegetation mapping in Florida

from computer-processed satellite end aircraft

multispectral scanner data

]NASA-TP-1553] p 139 N80-15535

Literature review of orgamc matter transport from

marshes

[E83-10352] p 142 N83-29750

Global Biology Research Program: Biogeochemicsi

Processes in Wetlands

[NASA-CP-23161 p 169 N84.30665

WETTING

Mechanics of a gaseous film barrier to lubricant wetting

of etastohydrodynam,cally lubricated conjunctions

[NASA-TP-25001 p 125 N85-32330

WHEAT

A comparative statistical study of Iong-tarm agroclimatic

condihons affecting the growth of US winter wheat:

Distnbutions of regional monthly average precipitation on

the Great Plains and the state of Maryland and the effect

of agrociimatic conditions on yield in the state of Kansas

{NASA-TP-t?24] p 163 N81-22658

WHEEL BRAKES

Dynamics of aircraft antiskld braking systems ---

conducted at the Langley aircraft landing loads and traction

facility

INASA-TP-1959] p 35 N82-18204

WHISKER COMPOSITES

Microstructure and orientation effects on properties of

discontinuous silicon carbide/aluminum composites

l NASA-TP-2302] p 79 N84-26749

WHITE NOISE

Determination ot no0se equivalent reflectance for a

multispectral scanner: A scanner sensitivity study

INASA-TP-t575J p 114 N80-t2399

WICKS

A siphon method of determining resistivities of thin

heat-pipe wicks

JNASA-TP-13041 p 106 N79-10379

WILDERNESS

Wildland inventory and resource modeling for Douglas

and Carson City Counties. Nevada, using LANDSAT and

digital terrain data

[E83-10302J p 142 N83-27293

WIND (METEOROLOGY)

Engineering handbook on the atmospheric

environmental guidelines for use in wind turbine generator

development

[NASA-TP-13591 p 159 N79-14679

Synoptic analyses, 5-, 2-, 1-. and 0 4-millibar surfaces

for July 1976 through June 1977

[NASA RP 10321 p 159 N79-19569

Large Horizontal-Axis Wind Turbines

[ NASA-CP-2230 ] p 146 N83-19231

NASA/MSFC FY-83 Atmospheric Processes Research

Review

INASA-CF-2281 ] p 165 N83-33494

Space Station Planetology Experiments (SSPEX)

[NASA CP 2424] p 201 N86-27136

WIND EFFECTS

Sensitivdy analysis of the space shuttle to ascent wind

profiles

1NASA-Tp-1988 ] p 69 N82-20236

WIND MEASUREMENT

Sequential high-resolution wind profile measurements

{NASA-TP-1354] p 159 N79-14680

Wind study for high 8Jtitude platform design

[NASA-RP-t044] p 160 N80-12661

First Scientific Working Group Meeting of Airborne

Doppler Lider Wind Velocity Measurement Program

[NASA-CP-2161] p 162 N81.10637

Determination of wind from NIMBUS 6 satellite sounding

data

[NASA-RP-t072] p 162 N81-15639

NASA/MSFC FY-84 Atmospheric Processes Research

Review

[NASA-CP-2329] p 186 N84-34829

Wind-weighting for sounding rockets with a telemetry

system

[NASA-TP-2438J p 70 N85-21246

WIND PROFILES

Development of a procedure to model high-raaotution

wind profiles from smoothed or low-frequency data

[NASA.TP-1071] p 158 N78.t1642

Sequential high-resolution wind profile measurements

[NASA-TP-1354] p 159 N79-14680

Sensitivity analysis of the space shuttle to ascent wind

profiles

[NASA-TP.1988] p 69 N82.20236

A stability analysis of AVE-4 severe weather

soundings

[NASA-TP-2045] p 164 N83-14824

A conceptual framework for using Doppler radar

acquired atmospheric data for flight simulation

[NASA-TP-2192] p 36 N83-27977

A spatlsi model of wind shear and turbulence for flight

simulation

[NASA-TP.2313] p 165 N84-24044

Analysis of Jimsphere pairs for use in assessing Space

Vehicle ascent capability

[NASA.TP-2573] p 28 N86-21506

WIND SHEAR

Fixed.base simulation study of decoupted longitudinal

controls during approach and landing of a medium jet

transport in the presence of wind shear

[NASA.TP.1519] p 55 N79.33218

Simulation comparison of a decoupled longitudinal

control system and a velocity vector control wheel staedng

system during landings in wind shear

[NASA-TP-1734] p 56 N81-12109

An analytical study of the longitudinal response of

airplanes to positive wind shear

[NASA-TP-17651 p 56 N81-20082

Flight evaluation of a simple total energy-rate system

with potential wind-sheer application

JNASA-TP-1854] p 39 N81-24058

Summary Proceedings of a Wind Shear Workshop

(NASA.CP.2270] p 165 N83-25265

NASA/MSFC FY-83 Atmospheric Research Review

[NASA-CP-2288] p 165 N83-36587

Evaluation of a total energy-rate sensor on a transport

airplane

{NASA-TP-2212J p 40 N84.12164

A spatial model of wind shesr and turbulence for flight

simulation

{NASA-TP-2313J p t65 N84-24044

Total energy-rate feedback for automatic glide-slope

tracking during wind-shear penetration

[NASA-TP-2412] p 58 N85-23801

Analysis of Jimsphere pairs for usa in assessing Space

Vehicle ascent capability

{NASA-TP-2573] p 28 N86.21506

WIND TUNNEL APPARATUS

Wind Tunnels of NASA

{NASA-SP-440] p 59 N81-32153

Cryogenic Technology, part t -- conference

proceedings; cryogenic wind tunnel design and

instrumentation

[NASA-CP-2122-PT-l} p 99 N82-20357

Cryogenic Technology, part 2 --- conference

proceedings; cryogenic wind tunnel design and

instrumentation

{NASA-CP-2122-PT-2] p 99 N82-20358

A study of resonant-cavity and fiberglass-filled parallel

baffles as duct silencers --- for wind tunnels

[NASA-TP-197OI p 188 N82-24052

Wind-Tunnel/Flight Correlation, 1981

[NASA-CP-2225J p 19 N82-25196

Recent modifications and calibration of the Langley

low-turbulence pressure tunnel

[NASA.TP-2328] p 24 N84-27675

WIND TUNNEL CALIBRATION

A fan pressure ratio correlation in terms of Mech number

and Reynolds number for the Langley 0,3 meter transonic

cryogenic tunnel

{NASA-TP-1752] p 16 N81-10005

Description and calibration of the Langley unitary plan

wind tunnel

JNASA-TP-1905} p 18 N82-12035

Recent modifications and calibration of the Langley

low-turbulence pressure tunnel

{NASA-TP-2328] p 24 N84-27675

WIND TUNNy, DRIVES

Acoustic I_lbrformance of two 1.83-meter-diametor fans

designed for a wind.tunnel drive system

[NASA-TP-t008] p 185 N77-30909

WIND TUNNEL MODELS

Improvement of maneuver aerodynamics by spanwise

blowing

[NASA-TP-t065] p 7 N78-14997

Effects of spanwise nozzle geometry and locate-on on

the longitudinal aerodynam¢ characteristics of a

vectored-engine-over-wing configuration at subsonic

speeds

NASA-TP-1215] p 8 N78-25060

Aerodynamic characteristics at Mach 6 of a wing-body

concept for a hypersonic research airplane

NASA.TP.t24g] p 9 N78-30055

Similitude requirements and scaling relationships as

applied to model testing

NASA.TP.1435] p 33 N79-30176

Instrument error analysis as it applies to wind-tunnel

testing

NASA-TP-1572] p 114 N80-13430

Flow Visualization and Laser Vaiocimetry for Wind

Tunnels

NASA-CP-2243] p 116 N82.32663

Cryogenic Wind Tunnel Models. Design and

Fabrication

NASA-CP-2262] p 59 N83-18748

A common geometric data-base approach for

computer-aided manufacturing of wind-tunnel models and

theo_retioal aerodynamic analysis

[NASA-TP-2151] p 21 N83-22166

Effect of thrust reverser operation on the

latersi-directional characteristics of a three-surface F-15

model at transonic speeds

[NASA-TP-2234] p 22 N84-13165

Fracture temperature and flaw growth in nitronic 40 st

cryogenic temperatures

[NASA-TP-2312] p 89 N84-23750

Effect of aileron deflections on the aerodynamic

characteristics of a samispan model of a subsonic

energy-efficient transport

[NASA-TP-2478] p 27 N86-11186

WIND TUNNEL NOZZLES

Gortler vortices and transition in wall boundary layers

of two Mach 5 nozzles

[NASA-TP-1869] p 109 N81-31509

WIND TUNNEL STABILITY TESTS

Effect of winglets on a first*generation jet transport wing,

6: Stability characteristics for a full-span modal at subsonic

speeds --- conducted in Langley 8 foot transonic pressure

tunnel

[NASA-TP-1330] p 12 N80-10101

Effect of Reynolds number on stability characteristics

of a cruciform wing*body

[NASA-TP-1683] p t5 N80-27283

WIND TUNNEL TESTS

Aerodynamic and directional acoustic performance of

a scoop inlet

[NASA-TP-1028] p 41 N77-31152

Wind-tunnel tests of wide-chord teetenng rotors with and

without outboard flapping hinges

[NASA-TP-1046] p 31 N78-11053

Effects of deflected thrust on the longitudinal

aerodynamic characteristics of a close-coupled

wing-canard configuration --- in the Langley V/STOL

tunnel

INASA.TP-10g0J p 6 N78.13014

Two-dimensional transonic testing with splitter plates

[NASA-TP.1153] p 7 N78-17999

Wind-tunnel investigation at Mach numbers from 1.90

to 2.86 of • canard-controlled missile with ram-air-jet

spoiler roll control --- in the Langley Unitary Plan Wind

Tunnel

{NASA-TP-1124] p 7 N78-20079

Correlation of laser velocimeter measurements over a

wing with results of two prediction techniques --- in the

Langley V/STOL tunnel

[NASA-TP-tf68J p 105 N78-21410

A wind-tunnel study of the spplicability of far-field

sonic-boom theory to the space shuttle orbiter

[NASA-TP-1186J p 8 N78-25061

Wind-tunnel investigation at supersonic speeds of a

canard-controliad missile with fixed snd free-rolling tail

fins

{NASA-TP-t316J p 9 N78-32067

A study of canard-wing interference using experimental

pressure data at transonic speeds

[NASA-TP-1355J p 10 N79-15902

Experimental investigation of effects of blade tip

geometry on loads and performance for an articulated rotor

system

{NASA-TP-13031 p 33 N79-t5938

A-136
SUBJECT INDEX WIND TUNNEL TESTS

An analytical technique for predicting the characteristics

of a flexible wing equipped with an active

flutter-suppression system and comparison with

wind-tunnel data

INASA-TP-13671 p 128 N79-17264

An experimenta_ wind-tunnel investigation of a

ram-air-spoiler roll-control device on s forward-control

missile at supersonic speeds

[NASA-TP-1353J p 11 N79-17809

Space shuffle afferbody aerodynamics/plume simulation

data summary

[NASA-TP-f384J p 11 N79-17810

Advanced technology airfoil research, volume 1, part 2

INASA-CP-2045-PT-2] p 2 N79-19989

Advanced Technology Airfoil Research, volume I, part

1 --- conference on development of computational codes

and test facilities

[NASA-CP-2045-PT-1 J p It N79-20030

Experimental investigation of three helicopter rotor

airfoils designed analytically --- in the Langley 6 by 19

inch and 6 by 28 inch transonic wind tunnels

[NASA-TP-1396} p 11 N79-22037

Low-speed wind-tunnel parametric investigation of flight

spoilers as trailing-vortex-alleviation devices on a transport

aircraft model

(NASA-TP-1419] p 11 N79-22038

Low-speed wind-tunnel investigation of wing fins as

trailing-vortex-alleviation devices on a transport airplane

model

{NASA-TP-1453} p 12 N79-24961

Effects of wing leading-edge deflection on low-speed

aerodynamic characteristics of a low-aspect-ratio highly

swept arrow-wing configuration --- wind tunnel tests

{NASA-TP-t434J p 12 N79-26020

A throat-bypass stability-bleed system using relief valves

to increase the transient stability of a mixed-compression

inlet --- YF-12 aircraft inlet tests in the Lewis 10 by 10 ff

supersonic wind tunnel

[NASA-TP-1083J p 45 N79-28176

An experimental and theoretical investigation of the

effect of nonmetric over-the-wing nacelles on wing-body

aerodynamics

[NASA-TP-1503] p 12 N79-29146

Similitude requirements and scaling relationships as

applied to model testing

[NASA-TP-1435J p 33 N79-30176

Velocity field of a round jet in a cross flow for various

jet injection angles and velocity ratios --- Langley V/STOL

tunnel

[NASA-TP-1506] p 107 N79-32500

Longitudinal aerodynamic characteristics of a

vectored-engine-over-wing configuration at subsonic

speeds --- Langley V/STOL tunnel tests

[NASA-TP-15331 p 12 N79-33164

Wind-tunnel investigation of the validity ot a

sonic-boom-minimization concept --- Langley Unitary Plan

Wind Tunnel tests for supersonic transport design

INASA-TP-1421 ] p 12 N80-t0102

Evaluation of a wind-tunnel gust response technique

including correlalions with analytical and flight test

results

INASA-TP-1501 ] p 2 N80-11028

Wind-tunnel/flight correlation study of aerodynamic

characteristics of a large flexible supersonic cruise airplane

CXB-70-1). 1: Wind-tunnel tests of a 0.03-scale model

at Mach numbers from 0.6 to 253

{NASA-TP-1514J p 33 Na0-t1068

Aerodynamic characteristics of a hypersomc research

airplane concept having a 70 (;leg swept double-delta wing

at Mach numbers from 0 80 to 1 20, with summary of data

from 0.20 to 6.0 --- Langley 8-ft transonic wind tunnel

INASA-TP-f5521 p 13 N80-12064

Instrument error analysis as it applies to wind-tunnel

testing

[NASA-TP-1572} p 114 N80-13430

Experimental study of acoustic loads on an

upper-surface-blown STOL airplane configuration ---

Langley full-scale wind tunnel tests

INASA-TP-15771 p 187 N80-13879

Turbojet-exhaust-nozzle secondary-airflow pumping as

an exit control of an inlet-stability bypass system for a

Mech 2,5 axisymmeted mixed-compression inlet --- Lewis

10- by 10-ff, supersonic wind tunnel test

INASA-TP-1532] p 46 N80-t4124

Wind-tunnel/flight correlation study of aerodynamic

characteristics of a large flexible supersonic cruise airplane

(XB-70t) 2: Extrapolation of wind-tunnel data to full-scale

conditions

{NASA-TP-15151 p 13 N80-16032

Wind-tunnel/flight correlation study of aerodynamic

characteristics of a large flexible supersonic cruise airplane

(XB-70-1). 3: A comparison between characteristics

predicted from wind-tunnel measurements and those

measured in flight

[NASA-TP-1516] p 14 N80-t7986

Dynamics stability derivatives of space shuttle orbiter

obtained from wind-tunnel and approach and landing flight

tests

[NASA-TP-1634 I p 55 N80-21336

Full-scale wind tunnel-investigation of the Advanced

Technology Light Twin-Engine airptane (ATLIT) --- Langley

full scale tunnel

I NASA-TP-1591 j p 14 N80-22266

Application of two design methods for active flutter

suppressJon and wind-tunnel test results

[NASA-TP-16531 p 129 N80-22737

Investigation of axisymmetric and nonaxisymmetnc

nozzles installed on e 0 10 scate F-t 8 prototype airplane

model --- wind tunnel tests

INASA-TP-1638} p 15 N80-24267

A Scanning taser-veiocimeter technique for measuring

two-dimensional wake-vortex velocity distributions ---

Langley Vortex Research Facility

INASA-TP-16611 p 114 N80-24594

Development and validation Of a combined rotor

fuselage induced flow field computational method ---

Langley V/STOL tunnel

{NASA-TP-1656j p 15 N80-25296

Large-scale wind-tunnel lests of inverting flaps on a

STOL utility aircraft model

I NASA-TP-1696] p 34 N80-25318

Noise reduction in a Mach 5 wind tunnel with a

rectangular rod-wall sound shield

[NASA-TP-16721 p 108 N80-26622

Wind-tunnel experiments on divergence of

forward-swept wings

_NASA-TP-1685] p 34 N80-29287

Aerodynamic characteristics of three helicopter rotor

airfoil sections at Reynolds number from model scale to

full scale at Mach numbers from 035 to 0.90 --- conducted

in Langley 6 by 28 inch transonic tunnel

[NASA-TP-17011 p 15 N80-32333

Use of nose cap and fuselage pressure orifices for

determination of air data for space shuffle orbiter below

supersonic speeds

INASA-TP-1643j p 39 N80-32389

Low-speed aerodynamic performance of

50.8-centimeter-diameter noise-suppressing inlets for the

Quiet, Clean, Short-haul Experimental Engine (QCSEE) ---

Lewis 9- by 15-toot low speed wind tunnel tests

I NASA-TP-11781 p47 N81-11037

Low-speed aerodynamic characteristics of a 13 percent

thick medium speed airfoil designed for general aviation

applications

INASA-TP-1498J p 16 N81-12015

Comparison of Space Shuttle Orbiter low-speed static

stability and control derivatives obtained from wind-tunnel

and approach and landing flight tests

INASA-TP-_79] p 56 N81-13066

Wind-tunnei m,Jasurements and comparison with flight

of the boundary layer and heat transfer on a hollow cylinder

at Mach 3

{NASA-TP-17891 p 16 N81-14975

Aerothermal environment in chordwise gaps between

split elevens at Mach 68

INASA-TP-17831 p 109 N81-15237

Aeropropulsive characteristics of twin nonaxisymmetric

vectoring nozzles installed with forward-swept and

aft-swept wings --- in the Langley 16 Foot Transonic

Tunnel

[NASA-TP-17781 p 16 N81-19019

Subsonic tests of an all-flush-pressure-orifice air data

system

I NASA-TP-1871 j p 39 N81-26144

Aerodynamic tests and analysis of a turbojet-boosted

launch vehicle concept (spacejet) over a Mech number

range of 1 50 to 2,86 --- Langley Unitary Plan Wind Tunnel

Tests

[NASA TP-18881 p 17 Nat-29098

Effects of vortex flaps on the low-speed aerodynamic

characteristics of an arrow wing

I NASA-TP-19141 p 3 N82-110t3

Wind-tunnel results for a modified 17-percent-thick

low-speed airfoil section

{NASA-TP-t919] p 18 N82-11033

Wind-tunnel investigation of the effects of blade tip

geometry on the interaction of torsional loads and

performance for an articulated helicopter rotor

INASA-TP-19261 p 18 N82-13107

Crossflow effects on steady and lluctuating pressures

on an ogive-cylinder cone-frustum model in supersonic

separated flow

[NASA-TP-1951 ] p 18 N82-13108

Fluctuating pressures on fan blades of a turbofan engine:

Static and wind-tunnel investigations

{NASA-TP 19761 p 188 N82-21037

Effects of axisymmetric and normal air jet plumes and

solid plume on cylindrical afterbody pressure distributions

at Math numbers from 1.65 to 2.50

I NASA-TP-20051 p 19 N82-22215

Wind-Tunnel/Flight Correlation, 1981

[NASA-CP-2225] p 19 N82-25196

Effects of wing-leading-edge modifications on a

full-scale, low-wing general aviation airplane: Wind-tunnel

investigation of high-angle-of-attack aerodynamic

charactenstics --- conducted in Langley 30- by 60-foot

tunnel

INASA-TP-20t 1 ] p 4 N82-26217

An experimental and theoretical investigation of thick

wings at various sweep angtes in and out of ground

effect

I NASA-TP-20681 p 20 N83-10016

Investigation of installation effects of single-engine

convergent-divergent nozzles

{NASA-TP-2078J p 20 N83-11059

Low-speed aerodynamic characteristics of a

17-percent-thick medium speed airfoil designed for general

aviation applications

I NASA-TP-1786} p 20 N83-16290

A method for modifying two-dimensional adaptive

wind-tunnel walls _ncluding analytical and experimental

verification

INASA-TP-2081 j p 59 N83-18770

Aeropropulsive characteristics of twin

single-expansion-ramp vectonng nozzles installed with

forward-swept wings and canards --- transonic tunnel

tests

I NASA-TP-2133 } p20 N83-22161

Experimental study of wing leading-edge devices for

improved maneuver performance of a supercritical

maneuvering fighter configuration --. Langley 7- by lO-ft

high speed tunnel tests

JNASA-TP-2125] p 21 N83-22162

Effects of twin-vertical-tail parameters on twin-engine

afferbody/nozzle aerodynamic characteristics --- Langley

16-(1 transonic tunnel tests

INASA-TP-2158] p 21 N83-24478

Effect of empennage location on twin-engine

afterbody-nozzle aerodynamic characteristics at Math

Numbers from 0.6 to 1.2 --- wind tunnel tests

(NASA-TP-2116 J p 21 N83-25666

Effects of flow separation and cove leakage on pressure

and heat-transfer distributions along a wing.cove-eleven

configuration at Mach 6.9 --- Langley 8-ff high temperature

tunnel test

I NASA-TP-21271 p 111 N83-28378

Wall-temperature effects on the aerodynamics of a

hydrogen-fueled transport concept in Math 8 blowdown

and shock tunnels

(NASA-TP-2159} p 21 N83-30391

Wind-tunnel investigation of leading-edge thrust on

arrow wings in supersonic ffow

{NASATP-2167] p 21 N83-31577

Theoretical and experimental investigation of supersonic

aerodynamic characteristics of a twin-fuselage concept

INASA-TP-2184 p 22 N83-32776

Aerodynamic characteristics of a series of bodies with

variations in nose camber

[NASA-TP-2206 p 22 N83-34904

Experiments in a three-dimensional adaptive-wall wind

tunnel

{NASA-TP-2210 p 22 N83-34906

Wind-tunnel free-flight investigation of e model of a

forward-swept-wing fighter configuration

I NASA-TP-2230 p 57 N84-17184

Wing planform effects at supersonic speeds for an

advanced fighter configuration

INASA-TP-2269 p 23 N84-20486

Test-engine and inlet performance of an aircraft used

for investigating flight effects on fan noise

tNASA-TP-2254 p 189 N84-21277

Natural laminar flow experiments on modern airplane

surfaces

I NASA-TP-2256 p 24 N84-26660

KC-135 Winglet Program Review

[ NASA-CP-2211 ] p 24 N84-27686

Two-dimensional aerodynamic characteristics of an

airfoil designed for two

[ NASA-TP-1965 ] p 24 N84-27694

A numerical simulation of three-dimensional flow in an

adaptive wall wind tunnel

I NASA-TP-2351 I p 24 N84-28750

Space Shuttle wind tunnel lasting program

[ NASA-RP-11251 p74 N85-11127

Analysis of noise measured from a propeller in a wake

INASA-TP-2358J p 190 N85-11788

Experimental and predicted heating distributions for

biconics a_ incidence in air el Math 10

INASA-TP-23341 p 112 N85-12313

Flight and wind-tunnel comparisons of the inlet-airframe

interaetton of the F-15 airplane

I NASA-TP-2374 t p 37 N85-12884

Static internal performance of a two-dimensional

convergent nozzle with thrust-vectoring capability up to

60 deg

I NASA-TP-2391 I p 25 N85-18951

A-137
WIND TUNNEL WALLS

Fluctuating pressures on fan blades of a turbofan engine,

fl_Jht test investigation

l NASA-TP-2381 ] p 190 N85-19790

Wind-tunnel investigation of a full-scale

canard-configured general aviation airplane

[ NASA-TP-2382_ p 25 N85-19925

Low-speed stability and control wind-tunnel

investigations of effects of spanwise blowing on fighter

flight characteristics at high angles of attack --- Langely

12-it low-speed tunnel and 30- by 60-It tunnel

(NASA-TP-2431 ] p 26 N85-23709

Exploratory wind-tunnel investigation of a

wingtip-mounted vortex turbine for vortex energy

recovery

j NASA-TP-2468 } p 26 N85-26667

Wind-tunnel evaluation of a 21-percent-scale powered

model of a prototype advanced scout helicopter

INASA-TP-24201 p 26 N85-28923

Static investigation of several yaw vectoring concepts

on nonaxisymmetric nozzles

INASA-TP-2432J p 26 NB5-28924

Effect of leading-edge load constraints on the design

and performance of supersonic wings

[NASA-TP-2446] p 26 N85-29923

Nacelio/pylon/wing integration on a transport model

with a natural laminar flow nacelle

{NASA-TP-2439] p 26 N85-29924

Low-speed tests of a high-aspect-ratio,

supercritical-wing transport model equipped with a high-lift

flap system in the Langley 4- by 7-metar and Ames 12-foot

pressure tunnels

I NASA-TP-2097 ] p26 N85-31010

Vortex wake alleviation studies with a variable twist

wing

[ NASA-TP-24421 p 5 N86-16187

Aerodynamic characteristics of a high-wing transport

configuration with a over-the-wing nacelle-pylon

arrangement

[NASA-TP-2497} p 27 N86-16193

Odfice-induced pressure error studies in Langley 7- by

10-foot high-speed tunnel

[NASA-TP-2545 t p 27 N86-20347

Static internal performance of a single-engine

onaxisymmetric-nozzle vaned-thrust-reverser design with

thrusl modulation capabilities

I NASA-TP-25191 p 27 N86-20348

Studies of condensation effects on airfoil testing in the

Langley 0 3-meter transonic cryogenic tunnel

{ NASA-TP-2509 ] p t13 N86-20720

Investigation of solid plume simulation criteria to produce

flight plume effects on mull/body configuration in wind

tunnel tests

[NASA-TP-2569J p 28 N86-21507

Static investigation of circular-to-rectangular transition

ducts for high-aspect-ratio nonaxisymmetric nozzles

[NASA-TP-2534] p 52 N86-22576

Mach 6 flow field surveys beneath the forebody of an

airbreathing missile

I NASA-TP-2491 ] p 28 N86-23558

Static internal performance of a thrust vectoring and

reversing two-dimensional convergent-d_vergent nozzle

with an aft flap

t NASA-TP-2549] p 28 N86-23560

Effects of upper-surface nacetles on longitudinal

aerodynamic characteristics of high-wing transport

configuration

[NASA-TP-2579] p 28 N86-23562

Oxidation and emit'lance of superalioys in heat shield

applications

{NASA-TP-25781 p 90 N86-26412

Vortex Flow Aerodynamics, volume 1

[NASA-CP-2416-VOL-1 ] p 28 N96-27190

Experimental evaluation of two turning vane designs for

high-speed corner of 0 t-scale model of NASA Lewis

Research Centar's proposed altitude wind tunnel

[NASA-TP-2570] p 60 N86-28101

WIND TUNNEL WALLS

A theory for predicting boundary impedance and

resonance frequencies of slotted-wall wind tunnels,

including plenum effects

INASA-TP-18801 p 17 N81-29096

Wind-Tunnel/Flight Correlation, t981

[NASA-CP-2225] p 19 N82-25196

A method for modifying two-dimensional adaptive

wind-tunnel wa_ls including analytical and experimental

verification

{NASA-TP-2081 1 p 59 N83-18770

Experiments un s three-dimens_onal adaptive-wall wind

tunnel

[NASA-TP-2210] p 22 N83-34906

Aerodynamic design of the contOured wind-tunnel liner

for the NASA supercritical, laminar- flow-control.

swept-wing expernment

l NASA-TP-23351 p 24 N84-33377

Wind Tunnel Wall Interference Assessment and

Correction, 1983

I NASA-CP-2319) p 25 N85-12011

WIND TUNNELS

Eva_uation of flow quality in two large NASA wind tunnels

at transonic speeds

INASA.TP.1737] p t08 N81-13303

Computer analysis of flow perturbations generated by

placement of choke bumps in a wind tunnel

[ NASA-TP-1892] p t8 N81-30088

Wind Tunnels of NASA

I NASA-SP-440 J p 59 N81-32153

The aerodynamic performance of several flow control

devices for internal flow systems

[NASA-TP-1972] p 59 N83-17560

Proposed fast-response Oxygen monitoring and control

system for the Langley 8-foot high-temperature tunnel

INASA-TP-2218] p 116 N84-11460

Correlations of supersonic boundary-layer transition on

cones including effects of large axial variations in

wind-tunnel noise

I NASA-TP-22291 p 111 N84-17534

A numerical simulation of three-dimensional flow in an

adaptive wall wind tunnel

[NASA-TP-2351 ] p 24 N84-28750

Wind Tunnel Seeding Systems for Laser VelDt/meters

[NASA-CP-23931 p 116 N86-11437

Acoustic treatment of the NASA Langley 4- by 7-meter

tunnel: A feasibility study

[NASA-TP-2563] p 191 N86-31337

WIND TURBINES

Wind turbine dynamics

{NASA-CP-2185] p 146 N82-23684

Capturing energy from the wind

{NASA-SP-455} p 146 N92-28783

Large Horizontal-Axis Wind Turbines

[NASA-CP-2230} p 146 N83-19231

WIND VARIATIONS

Analysis of Jimsphere pairs for use in assessing Space

Vehicle ascent capability

[NASA-TP-2573} p 28 N86-21506

WIND VELOCITY

Theoretical study of the effect of wind velocity gradients

on longitudinal stability and control in climbing and level

flight

INASA-TP-1332] p 54 N79-14110

WIND VELOCITY MEASUREMENT

Exploratory Meeting on Airborne Doppler Lidar Wind

Velocity Measurements

INASA-CP-2140] p 162 N80-26999

WINDMILLS (WINOPOWERED MACHINES)

WIND: Computer program for calculation of three

dimensional potential compressible flow about wind turbine

rotor blades

[NASA-TP-1729] p 15 N80-33357

Wind turbine dynam0cs

I NASA-CP-2185] p 146 N82-23684

WINDOWS (APERTURES)

Holography through Optically active windows

INASA-TP-1414) p 114 N79-17195

WlNDPOWER UTILIZATION

Summary of atmospheric wind design criteria for wind

energy conversion system development

[NASA-TP-1389] p 159 N79-14678

Large Wind Turbine Design Characteristics and R and

D Requirements

iNASA-CP-2106] p 145 NB0-t6453

Capturing energy from the wind

[NASA-SP-4551 p 146 N82-28783

Energy saving concepts relating to induction

generators

INASA-TP-1719] p 146 N82-32859

WINDPOWERED GENERATORS

Wind Turbine Structural Dynamics

{NASA-CP-2034] p 144 N78-19616

Engineering handbook on the atmospheric

environmental guidelines for use in wind turbine generator

development

[NASA-TP-1359] p 159 N79-14679

Large Wind Turbine Design Characteristics and R and

D Requirements

[NASA-CP-2106] p 145 N00-16453

Wind turbine dynamics

[NASA-CP-2185] p 146 N82-23684

Energy saving concepts relating to induction

generators

INASA-TP-1719t p 146 N82-32959

Large Horizontal-Axis Wind Turbines

{NASA-CP-2230] p 146 N83-19231

WINDS ALOFT

Wind study for high altitude platform design

[NASA-RP-1044] p 160 N80-12661

SUBJECT INDEX

WING FLAPS

Low-speed aerodynamic performance of an

aspect-ratio- 10 aupercritical-wiog transport model

equipped with a full-span slat and part-span and full-span

double-slotted flaps

[ NASA-TP-t805] p 21 N83-30390

Investigation of jet-iostallation noise sources under static

conditions

{NASA-TP-2181] p 189 N83-33684

Vortex wake alleviation studies with a variable twist

wing

[NASA-TP-2442] p 5 N86-16187

WING LOADING

Preliminary study of a large span-distributed-load

flying-wing cargo airplane concept

[NASA-TP-t 158] p 32 N78-25079

Parametric study of variation in cargo-airplane

performance related to progression from current to

spanioader designs

[NASA-TP-1625] p 34 N80-21318

Estimation of wing nonlinear aerodynamic

characteristics at supersonic speeds

[NASA-TP-1718] p 15 N81-10004

An analytical technique for approximating unsteady

aerodynamics in the time domain

[NASA-TP-17381 p 130 N81-11422

Comparison of analytical and wind-tunnel results for

flutter and gust response of a transport wing with active

controls

[NASA-TP-20t0] p 131 N82-26703

Downwash in the plane of symmetry of an elliptically

loaded wing

[NASA.TP-2414] p 25 N85-15693

WING NACELLE CONFIGURATIONS

An experimental and theoretical investigation of the

effect of nonmetdc over-the-wing nacelles on wing-body

aerodynamics

INASA-TP-1503] p 12 N79-29146

Longitudinal aerodynamic characteristics of a

vectored-engine-over-wing configuration at subsonic

speeds --- Langley V/STOL tunnel tests

INASA-TP-1533] p 12 N79-33164

Investigation of jet-installation noise sources under static

conditions

{NASA-TP-2181 I p 189 N83-33684

Nacelle/pylon/wing integration on a transport model

with a natural laminar flow nacelle

[NASA-TP-24391 p 26 N85-29924

WING OSCILLATIONS

An experimental evaluation of the application of the

Kirchhoff formulation for sound radiation from an oscillating

airfoil

[NASA-TP-t048] p 186 N78-12801

Development and application of an optimization

procedure for flutter suppression using the aerodynamic

energy concept

[NASA-TP-1137] p t27 N78-18459

Application of modal control to wing-flutter

suppression

[NASA-TP-1983] p 57 N92-24209

WING PANELS

Loading tests of a wing structure for a hypersonic

aircraft

INASA-TP-1596] p 34 N80-15068

WING PLANFORMS

Supersonic wings with significant leadiog-edge thrust at

cruise

INASA-TP-t632J p 14 N80-21279

Experimental investigation of leading-edge thrust at

supersonic speeds

[NASA-TP-2204] p 22 N83-34905

Wing planform effects at supersonic speeds for an

advanced fighter configuration

[NASA-TP-2269] p 23 N84-20486

Supersonic aerodynamic characteristics of canard,

tailless, and aft-tail configurations for 2 wing planforms

[NASA-TP-2434] p 26 N85-27822

WING PROFILES

Exploratory study of the effects of wing.leading-edge

modifications on the stall/spin behavior of a light general

aviation airplane

[NASA-TP-1589J p 33 N80-13026

An expehmentat and theoretical investigation of thick

wings at various sweep angles in and out of ground

effect

INASA.TP-2068] p 20 N83-10016

Low.speed tests of a h_gh-aapect-ratio,

supercdtical-wing transport model equipped with a high-lift

flap system in the Langley 4- by 7-metar and Ames 12-foot

pressure tunnels

[NASA-TP-2097] p 26 N85-31010

WING SPAN

Effect of winglets on a first-generation jet transport wing,

5: Stability characteristics of a full-span wing with s

generalized fuselage at high subsonic speeds

{NASA-TP-t 163] p 8 N78-20081

A-138
SUBJECT INDEX ZONE MELTING

Effects of spanwise blowing on the surface pressure

distribution and vortex-liff characteristics of a trapezoidal

wing-strake configuration

[NASA-TP-12901 p 11 N79-16803

Performance evaluation method for dissimilar aircraft

designs --- using the square of the wing span for

nondimensional compansons of aerodynamic

characteristics

{NASA-RP-t0421 p 2 N79-30139

Vortex wake alleviation studies with a variable twist

wing

[NASA-TP-24421 p 5 N86-16187

WING TIPS

Theoretical parametric study of the relative advantages

of winglets and wing-tip extensions

[NASA-TP-t0201 p 5 N77-33t12

Optimization and performance calculation of

dual-rotation propellers

[NASA-TP-19481 p 3 N82-14049

Exploratory wind-tunnel investigation of a

wingtip-mounted vortex turbine for vortex energy

recovery

INASA-TP-2468] p 26 N85-26667

WINGLETS

Theoretica_ parametric study of the relative advantages

of winglets and wing-tip extensions

[NASA-TP-1020] p 5 N77-33112

Effect of winglets on a first-generation jet transport wing.

4: Stability characteristics for a lull-span model at Mach

0.30

INASA-TP-1119) p7 N78-t7997

Effect of winglets on a first-generation jet transport wing.

5: Stability characteristics of a full-span wing with a

generalized fuselage at high subsonic speeds

[NASA-TP-1163} p 8 N78-20081

Effect of winglets on a first-generation jet transport wing.

6: Stability characteristics for a full-span model at subsonic

speeds --- conducted in Langley 6 loot transonic pressure

tunnel

[NASA-TP-1330] p 12 N80-10101

Advanced aerodynamics and active controls. Selected

NASA research

t NASA-CP-2172 t p3 N81-19001

KC-135 Winglet Program Review

[NASA-CP-2211 ] p 24 N84-27686

WINGS

Supersonic aerodynamic characteristics of a Sparrow

3 type missile model with wing controls and comparison

with existing tail-control results

[NASA-TP-1078t p 6 N78-12041

Longitudina/aerodynamic characteristics at Mach 0.60

to 286 of a fighter configuration with strut braced wing

INASA-TP-1102] p 7 N78-16000

Effect of winglets on a first-generation jet transport wing.

4: Stability characteristics for a lull-span model at Mach

0.30

[NASA-TP-1119) p 7 N78-17997

Aerodynamic derivatives for an oblique wing aircraft

estimated from flight data by using a maximum likelihood

technique

{NASA-TP-t336) p t0 N78-33054

A laser velocimeter flow survey above a stalled wing

INASA-TP-1266] p 10 N79-14019

Pressure and thermal distnbutions on wings and adjacent

surfaces induced by elevon deflections at Mach 6

[NASA-TP-t356J p 106 N79-20344

Low-speed wind-tunne_ investigation of wing fins as

trailing-vortex-alleviation devices on a transport airplane

model

[NASA-TP-1453] p 12 N79-24961

Effect of winglets on a first-generation jet transport wing.

6: Stability charectanstics for a lull-span model at subsonic

speeds --- conducted in Langley 8 foot transonic pressure

tunnel

[NASA-TP-1330] p 12 N80-10101

Estimation of attainable leading-edge thrust for wings

at subsonic and supersonic speeds

[NASA-TP-1500] p 12 N80-10105

Aerothermal analysis of 8 wing-elevon cove with vahable

leakage

[NASA-TP-1703] p 108 N80-32692

Wing-alone aerodynamic characteristics for high angles

of attack of supersonic speeds

[NASA-TP-t88gl p 16 N81-30087

GRID30: Computer program for fast generation of

multilevel, three-dimensional boundary-conforming O-type

computational grids

[NASA-TP-lg20] p 18 N81-31t28

Effects of flow separation and cove leakage on pressure

and heat-transfer distributions along a wing-cove-elevon

configuration at Mech 6.9 --- Langley 8-if high temperature

tunnel test

[NASA-TP-2127] p t 11 N83-28378

Effect of thrust vectoring and wing maneuver devices

on transonic aeropropulsive characteristics of a supersonic

fighter

[NASA-TP-21t 91 p22 N84-10025

Reduction method for thermal analysis of complex

aerospace structures

[NASA-TP-2373] p 112 N85-16066

Aerodynamic characteristics of a distinct wing-body

configuration at Mech 6: ExperimenL theory, and the

hypersonic isolation principle

[NASA-TP-2467] p 27 N85-33107

Strength of graphite/epoxy bolted wing-skin splice

specimens subjected to outdoor exposure under constant

load and yearly fatigue loading

[NASA-TP-2542] p 83 N86-20508

WIRE CLOTH

Flow through very porous screens

[ NASA-TP-2436] p 112 N85-20270

WOODEN STRUCTURES

Vibration charactehstics of wails and a plate glass

window representative of those of a wood-frame house

[NASA-TP-1447_ p 128 N79-24372

WORKLOADS (PSYCHOPHYSIOLOOY)

Twentieth Annual Conference on Manual Control,

volume 2

[NASA-CP-2341-VOL-2] p 174 N85-14535

Analytical techniques of pilot scanning behavior and their

application

(NASA-TP-2525] p 172 N86-27920

Twenty-First Annual Conference on Manual Control

[NASA-CP-2428] p 174 N86-32976

WORKSTATIONS

Space Station Workstation Technology Workshop

Report

[NASA-CP-2414] p 70 N86-23620

WRIST

Kinematic control of robot with degenerate wrist

INASA-TP-2341] p 181 N84-28539

Kinematic rate control of simulated robot hand at or

near wrist singularity

{NASA-TP-2440] p 181 N85-27575

Theoretical three.and four-axis gimbal robot wrists

[NASA-TP-2564] p 181 N86-25168

X

X RAY ASTRONOMY

Skylab's astronomy and space sciences

[NASA-SP-404] p lg9 N79-34tt8

HEAD Science Symposium

(NASA-CP-21131 p200 NS0-14977

The Pinhole/Occulter facility

[NASA-TP-2089] p 209 N83-13048

The Pinhole/Occulter Facility

[NASA-TP-2168] p 209 N83-25646

X RAY DIFFRACTION

Programs for calculating cell parameters in electron and

X-ray diffraction --- to identify stratosphenc aerosols

[NASA-TP-15291 p 148 N79-30844

X RAY IMAGERY

Preliminary applications and evaluation results

Lixiscope: Proceedings of the Lixiscope Conference

[NASA-CP-2112] p 114 N80-12384

X RAY SPECTROSCOPY

X-Ray photoelectron spectroscopy study of

radiotrequency-sputtered titanium, carbide, molybdenum

carbide, and titanium bodde coatings and their friction

properties

[NASA-TP-t033J p gl N77-33348

X-ray photoelectron spectroscopy study of

radiofrequency-sputtared refractory compound steel

interfaces

[NASA-TP-11611 p 91 N78-26336

Polytetrafluoroethylene transfer film studied with X-ray

photoelectron spectroscopy

[NASA-TP-1728] p 93 N81-11214

X RAY TELESCOPES

Performance analysis of grazing incidence imaging

systems --- X ray telescope aberrations

[NASA-TP-1088] p 193 N78-11812

XV-15 AIRCRAFT

An assessment of the capability to calculate tilting

prop-rotor aircraft performance, loads and slability

[NASA-TP-2291 ] p 37 N84-19333

Y

YAW

Space Shuttle separate-surface control-system study

[NASA-TP-2340] p 58 N84-26801

Static investigation of several yaw vectoring concepts

on nonaxisymmetric nozzles

INASA-TP-2432] p 26 N85-28924

YAWING MOMENTS

Static and yawed-rolling mechanical properties of two

type 7 aircraft tires

[NASA-TP-1863/ p 130 N81-24471

YC-14 AIRCRAFT

Quiet powered-lift propulsion

[ NASA-CP-20771 p46 N80-15127

YF-12 AIRCRAFT

Phugoid characteristics of a YF-12 airplane with

variable-geometry inlets obtained in flight tests at a Mach

number of 29

INASA-TP-1107) p 52 N78-12100

YF-12 experiments symposium, volume 1

[NASA-CP-2054-VOL-1 ] p 9 N78-32055

A throat-bypass stability-bleed system using relief valves

to increase the transient stability of a mixed-compression

inter --- YF-12 aircraft inlet tests in the Lewis 10 by 10 ft

supersonic wind tunnel

[NASA-TP-1083] p 45 N79-28176

Development and flight test results of an autothrottle

control system at Mech 3 cruise

[NASA-TP-16211 p 56 N80-26328

YIELD

A comparatwe statistical study of tong4erm agroctimatic

conditions affecting the growth of US winter wheat:

Distributions of regional monthly average precipitation on

the Great Plains and the state o1 Maryland and the effect

of agroclimatic conditions on yield in the state of Kansas

[NASA-TP-1724] p 163 N81-22658

YIELD STRENGTH

Effects Of thermomechanical processing on strength and

toughness of iron - 12-percent-nickel - reactive metal alloys

at -196 C

[NASA-TP-1308] p 86 N78-31213

YTTRIUM

Pressureless sintered Sialons with low amounts of

sintering aid

[NASA-TP-1246] p 92 N78-25215

Effect of Yttria additives on properties of

pressureless-sinterecl silicon nitride

INASA-TP-1899I p 94 N81-31366

High-temperature erosion ot plasma-sprayed,

yttria-stabilized zirconia in a simulated turbine

environment

[NASA-TP-2406] p 96 N85-13045

YTTRIUM OXIDES

Effects ol oxide additions and temperature on

sinterability of milled silicon nitnde

J NASA-TP-1644 ] p 93 N80-21532

Z

ZINC

X-ray photoelectron spectroscopy and friction studies

of nickel-zinc and manganese-zinc ferrites in contact with

metals

[NASA-TP-2163] p 88 N83-23419

Humidity effects on adhesion of nickel-zinc ferrite in

elastic contact with magnetic tape and itself

[NASA-TP-24491 p 96 N85-21359

ZINC ALLOYS

Anisotropic friction and wear of single-crystal

manganese-zinc ferrite in contact with itself

[NASA-TP-13391 p 120 N79-10425

Fdction and morphology of magnetic tapes in sliding

contact with nickel-zinc ferrite

[NASA-TP-2267] p 95 N84-16334

Water-vapor effects on friction of magnetic tape in

contact with nickel-zinc temte

[NASA-TP-2279] p 95 N84-16399

ZINC COMPOUNDS

Auger spectroscopy analysis of lubneation with zinc

dialkyldithiophosphate of several metal combinations in

sliding co.act

[NASA.TP-1489] p 92 N79-27308

Performance of alkaline battery cells used in emergency

Ioeator transmitters

[NASA-TP-2277] p 103 N84-2075g

ZINC OXIDES

Formulation of electrically conductive thermal-control

coatings

[NASA.TP-1218J p 78 N78-21216

ZIRCONIUM

High-temperature erosion of plasma-sprayed,

ytt ria-stabilized zirconia in a simulated turbine

environment

[NASA-TP-2406] p 96 N85-13045

ZIRCONIUM OXIDES

Overv,ew of zirconia with respect tO gas turbine

applications

[NASA.TP-2286] p 95 N84-21740

ZONE MELTING

Float Zone Workshop

[NASA-CP-2226] p 62 N82-26330

A-139

PERSONAL AUTHOR INDEX

NASA Scientific end Technical Publications 1977-1986

Typical Personal Author

Index Listing

JONES, W, H. p 14 N83 2892_

[ I

Listings in this index are arranged alphabetically by

personal author. The title of the document provides

the user with a brief description of the subiect

matter. The report number helps to fndicate the

type of document listed (e.g., NASA report,

translation, NASA contractor report) The page and

accession numbers are located beneath and to the

right of the title. Under any one author's name the

accession numbers are arranged m sequence with

the AIAA accession numbers appearing first

A

AABEYOUNIS, W. K .............................. p 26

ABBOT, K. H ........................................... p 40

ABBOTT, I. H. A ................................... p 145

ABBOTT, J. M ......................................... p 41

p 42

p 47

ABBOTT, T. S ......................................... p 54

p 38

p 30

p 4O

p 4O

ABBOTT, W. V., III ............................... p 157

ABDELWAHAB, M ................................ p 41

ABEL, I ................................................... p 127

p 128

p 129

p 181

p 131

ABERCROMBIE, R. A ............................ p 65

ABEYOUNIS, W. K .................................... p 9

p14

p 20

p 27

p 27

ABRAHAMSON, A. L........................... 191

ABSHIRE, J. B ........................................ p 69

117

117

p 37

pl0

D 53

53

39

39

39

40

25

179

59

16

109

128

109

7110

138

138

46

3 172

) 185

) 177

174

)112

30

74

26

69

29

127

128

ACREE, C. W.,JR .................................

ADAMCZYK, J.J ....................................

ADAMS, J.J ............................................

ADAMS, M. S ..........................................

ADAMS, W. M., JR ...............................

ADCOCK, J. B ........................................

ADELMAN, H.M ...................................

ADLER, I ................................................

AHTYE, W. F ...........................................

AHUMADA, A. J., JR ...........................

AINSWORTH, O. R ............................

AKINS, F. R ..........................................

ALBERTSON, C. W ..............................

ALCABIN, M ............................................

ALEXANDER, W., JR .........................

ALEXOVICH, R. E ..................................

ALFARO-BOU, E ...................................

N85-29924

N85-16868

N80-11559

N77-31152

N78-20132

N81-11037

N79o29195

N80-27360

N81-29109

N84-21542

N85-16869

N77-19709

N77-31153

N78-18459

N79-17264

N80-22737

N81-30851

NB2-26703

N78-15143

N78-30052

N80-22262

N82-32322

N86-16193

N86-20345

N86-31337

N78-10200

N78_16354

N78-31413

N84-31111

N79-13003

N78-20142

N78-20143

N81-14997

N81-33203

N82-20180

N84-13182

N85-21120

N84-27461

N80-19131

N81-10005

N81-32418

N80-12438

N82-23473

N82-31646

N78-21526

N78-23537

N80-15129

N83-33538

N84-15880

N85-23305

N85-32772

N85-17322

N85-32101

N84-19393

N85-23707

N79-21120

N78-10034

N78-26494

N80-10512

p 128 N80-11505

p 30 N83-34921

p 38 N86-30721

ALFORD, D. K ...................................... p 173 N82-24834

ALFORD, W. L ...................................... p 143 N86-31945

ALFVEN, H ............................................ p 203 N77-12959

ALLARIO, F........................................... p 153 N81-23742

ALLAWAY, H .......................................... p 68 N80-30367

ALLAWEY, H ........................................ p 199 N80-27219

ALLEN, G. P.......................................... p 120 N79-10424

p 120 N79-22519

p 12t N80-14403

ALLEN, J. L., JR ..................................... p 74 N82-33421

ALLEN, J. M ............................................ p 21 N83-27959

ALLTON, C, S ......................................... p 99 N83-32990

ALLUMS, S. L ...................................... p 144 N77-30617

ALVAREZ, J. M ..................................... p 152 N80-27866

AMOS, A. K ............................................. p 66 N83-18819

ANDERSEN, C. M ................................. p 133 N84-34773

ANDERSON, A ...................................... p 146 N83-14684

ANDERSON, B. J ................................. p 154 N84-14606

ANDERSON, E. C ................................... p 24 N84-33377

ANDERSON, F. W.o JR ........................ p 196 N82-14955

ANDERSON, G. Y ................................... p 48 N81-13058

ANDERSON, M. S .............................. p 132 N84-16585

ANDERSON, N. E.................................. p 87 N78-33196

p 120 N79-13369

p 121 N80-17466

p 192 N82-26678

ANDERSON, R. C ................................. p116 N85-16100

ANDERSON, S. B ................................... p 54 N79-27182

ANDERSON, W. J ................................ p 123 N83-27214

ANDERSSON, L. A ............................... p 207 N83-12031

ANDRIYICH-VARDA, D ......................... p 37 N85-12884

ANGLIN, E. L .......................................... p 26 N85-23708

ANTAR, B. N ........................................... p 72 N82-12109

p 166 N85-20605

ANUTA, P. E.......................................... p 139 N80-16405

APPLIN, Z. T ........................................... p 59 N86-22580

ARBITER, O ............................................ p 28 N86-23561

ARBUCKLE, P. D ................................... p 37 N85-19979

ARDANUY, P. E.................................... p 157 N86-29425

ARDEMA, M. O ....................................... p35 N81-31185

p 185 N85-33745

ARIAS, A ................................................. p92 N78-25215

p 92 N79-21204

p 93 N79-27309

p 93 N80-21532

p 94 N81-31366

ARIAS, S............................................ p 159 N78-32641

p 136 N80-15445

ARMSTRONG, E. S .......................... p 181 N78-22809

p 181 N81-29840

p 75 N86-30800

ARNAIZ, H, H ........................................ p 14 N80-17986

ARNDT, G. D ........................................ p 145 N81-18493

p 145 N81-27622

ARNOLD, J. R ....................................... p 205 N78-16973

ARON, P. R .......................................... p 124 N85-13234

ARPASI, O. J ........................................ p 178 N79-21798

p 179 N85-28610

ARRHENIUS, G ................................... p 203 N77-12959

ARRINGTON, J. P.................................. p 69 N84-10115

p 69 N84-10144

ARTHUR, C. W ..................................... p 65 N78-15142

ASHBY, G. C., JR ................................... p68 N79-21119

p 3 N8t-13915

ASHMORE, T. C ................................... p 208 N85-21099

ASHWORTH, B. R ................................. p 36 N83-18715

p 37 N84-18189

ASIMOV, I .............................................. p 196 N85-24994

AUGLER, R. E .................................... p 14 N80-17030

AUSTIN, L D., JR ............................... p 69 N82-20236

AVERNER, M. M ................................... p 175 N77-12718

AVERY, D. E ....................................... p 105 N78-28373

p72 N81-21116

p 109 N82-13383

p 72 N82-14277

p 112 N84-31561

p 113 N85-34351

AVNI, R .................................................... p 79 N84-20643

AYDELOTT, J. C ................................... p 97 N79-28350

p 97 N83-16545

B

BAALS, D. D ........................................ p 59

p18

p 59

p19

BABB, G. R ............................................ p 67

BABER, B. B ......................................... p 120

BAER, D ................................................. p 103

BAGBY, J. R ........................................... p 66

BAHEI-EL-DIN, Y. A .............................. p 82

BARN, G. S ............................................ p 147

BAILEY, M. C ........................................ p 100

BAINS, N. 3. C ...................................... p 135

BAIR, C. H ............................................. p 115

BAITY, W. A .......................................... p 209

BALAKRISHNA, S .................................. p 59

BALASUBRAMANIAN, R .................... p 112

BALCH, C. D ......................................... p 110

p 111

BALES, J. W ......................................... p 176

BALES, T. T ............................................ p 88

p 82

p 82

p 89

p 90

BALLARD, G. K .................................... p 112

BALOMBIN, J. R .................................. p 187

BAMBERGER, E. N .............................. to 123

BANOEEN, W. R ................................... p 153

BANGERT, L. S ...................................... p 19

p 52

BANKS, D. W .......................................... p 23

BARACAT, W. A ................................... p 126

p 126

p 126

BARBER, D. A ...................................... p 158

BARE, E. A .............................................. p 18

p 20

p21

p 22

p 22

p 28

BAROER, R. L ........................................... p 8

pll

p12

p13

p13

p14

p15

p15

p17

p17

p17

p19

p 25

BARKER, J. L................................... p 137

p 137

p 143

p 143

p 143

p 143

BARKER, K ......................................... p 181

BARKER, L K ....................................... p 184

p 176

p 182

p 182

P 181

p 181

p 181

p 183

BARKER, L. M ..................................... p 172

BARNES, J. C ....................................... p 141

BARNES, S, P ........................................ p 69

BARNWELL, R. W ............................... p 10

p 25

BARRANGER, J. P ............................... p 42

BARRETT, C. A ................................... p 87

BARROW, B. J .................................... p 135

BARTLETT, D, S .................................. p 169

BARTLETT, D. W .................................. p 37

BARTON, C. K ...................................... p 186

BARTON, G. C ....................................... p 98

:-;,_,CE33|NG pAGE BL_;_ ;,_OT FiLll/"3B

N77-27139

N81-31130

N81-32153

N82-25196

N83-32828

N79-31604

N84-33668

N82-20225

N83-33956

N78-13628

N84-20735

N86-20857

N80-30717

N83-25646

N80-31413

N84-25944

N83-20032

N84-22907

N81-21775

N83-19889

N83-28098

N83-28100

N83-35100

N86-13406

N84-31561

N80-18882

N83-33166

N81-23742

N82-26231

N86-22576

N84-18164

N86-25794

N86-27644

N86-28407

N77-30705

N81-30086

N82-32320

N83-24478

N84-13152

N84-13165

N86-23561

N78-25058

N79-15903

N80-10105

N80-13001

N80-14045

N80-22265

N80-24261

N80-32334

N81-22019

N81-26078

N81-29096

N82-25193

N85-21120

N84-30359

N84-30380

N85-20496

N85-20508

N85-21724

N85-23186

N85-27575

N81-10789

N81-21775

N83-25438

N83-34661

N84-28539

N85-15446

N86-25168

N86-27953

N84-22162

N82-20624

N78-28159

N79-14018

N85-12011

N78-22101

N80-11188

N86-28464

N84-30665

N85-33116

N79-14874

N77-30296

B-1
BASHER, R.E,

BASHER, R.E .......................................P 114 N78-28412

BATES, J.R ........................p 199 N79-22979

BATSON, R.M ...............................p 206 N80-16998 p 208 N84-35242

BAI-fERSON, J.G ............................p 56 N82-10041 p 57 N83-19758

BAI-rs, G.W ........................p 69 N82-33417

BAUM, W.A ..................................... p200 N81 11966

BAUMEISTER, K.J .........................p 185 N77*30908 p 1 N78-25049 p 190 N86-12007

BEACH, H. L., JR ..................p 105 N78-20463

BEACH, R.F....................................p 52 N85-28944

BEALL, T.W ................................P 85 N80-16118

BEAMISH, J.K .....................................P 31 N78-10048

BEASELEY, W.D ......................p 20 N83-16290

BEASLEY, G.P ...................P 58 N84-20567

BEASLEY, W.D ..............................p 16 N81-12015 p 18 N82-11033 p 24 N84-27675

BEATrY, M. E., III ..........................p 193 N78-20948

BECHER,J ..............................................p 76 N81-3128t

BECHTEL, R.T ....................................p 78 N85-13850

BECKER, J.V ........................................p3 N81-15969

BECKER,T ........................................P 158 N77-32689

BECKWITH, I.E ..............................P 108 N80-28622 p 109 N81-31509 p 111 N83-34229 p 111 N84-17534

BEHNING, F.P ....................................p 46 N80-25337 p 47 N80-25338 p 48 N81-16050

BELCASTRO, C.M ...........................p 57 N83-33896 p 40 N84-12164 p 58 N85-23801

BELEW, L.F .................................p 60 N77-27155

BELL,J ........................................p 67 N83-32828

BEMENT, L.J ..............................p 62 N81-26160 p 36 N83-31596

BENDURA, R.J ....................................p 150 N83-12595

BENEDICT, G.F..................................p 210 N79-27057

BENNETT,T .......................................p 169 N85-26028

BENSON, C.O ........................................p 64 N79-12127 p 63 N84-25737

BERGERON, H.P ..................................p4 N84-12029

BERGMAN,J ............................p 196 N88-24994

BERGSTRALH, J.T .......................p 208 N85-11927

BERRIER, B.L.............................p 12 N79-26022 p 15 N80-24267 p 16 N81-t4972 p 18 N81-30086 p 19 N82-20156 p 20 N83-11059 p 22 N84-13152 p 26 N85-28924

BERRY, J.D ................................p 26 N65-28923

BESKENIS,S......................................p 179 N85-20689

BESS, T.O ............................P 205 N79-14978 p 162 N81-13593

BEYERLE, R.A .......................p 52 N85-31058

BHANDARKAR, M.D ...............p 85 N84-11230

BHARTIA, P.K ..............p 164 N82-28880 p t64 N62-29826 p 154 N63-16992 p 165 N83-28628

BHAT, R.B ................p 186 N79q3821

BHUSHAN,B .....................p 95 N84-16334

BIDASARIA, H.B.p 192 N83-23t40 p 192 N84-22396

BIESIADNY, T.J ............p 42 N76-21112 p 42 N78-23095

BIGELOW, C.A.p 82 N83-33956

p 134 N85-32339

BILBRO, J.W ..................p 152 N79-13607

BtLL, R.C ...................... p86 N78-15229 p 86 N78-21269 p 92 N79-21205 p 93 N60-23453 p 88 N81 20245 p 89 N84 17350

BILLINGHAM, J.p 175 N78-18771 p 62 N79-32225 p 175 N82-20884 p 169 N85-32708

BILLINGS, C.E ....................p 30 N81-31162

BILSTEIN, R.E .............................p 72 N61-29154

BINGHAM, G.J ......................p 11 N79-22037 p 15 N80-32333 p 24 N84-27694 p 24 N84-28743

BIRCHENOUGH, A.G .....p 100 N78-11301 p 75 N78-17t45 p 101 N81-1t315

BtTTKER. D.A ....................p 84 N78-12167 p 84 N78-20261 p 85 N84-32446

BIZON, P.T ...........................................p 135 N86-28464

BLACK, D.C .......................................p 201 N80-18997 p 201 N80-25224 p 206 N80-27260

BLACKBURN, C.L ...............................p 127 N78-28482

BLACKWELL, K.L .................................p 11 N79-17810

BLAHA, B.J ...........................................P 12 N79-23912

BLAIR, A. B., JR ........................................p7 N78-20079

p9 N78-32067

p 11 N79-17809 p 21 N83-27959

BLAKE, J.B ............................................ p65 N78-15142

BLANCHARD,M ...................................p 199 N77-33003

BLANCHARD, R.C .................................p3 N81-14961

BLANKENBHIP, C.P .............................p 79 N83-12t47

BLASlUB, K,R ......................................p 200 N81-11966

BLAZQUEZ, C.H ..................................p 139 N81-21437

BLECH, R.A ...........................................p 54 N79-28186

BLOCK, P. J.W ....................................P 185 N78-12800 p 187 N79-32057 p 190 N85-11788 p t9t N86-26162 p 191 N86-31341

BLODGET, H.W ...................................p 136 N78-33499

BLOSSER, M.L ...................................p 132 N84-13614

BLOUNT, D.H ........................................p 77 N83-24549

BLUME, H. J.C .....................................P 103 N86-20678

BODLEY, C.S .........................................p 70 N78-25123 p 70 N78-25124

BOGDAN, V,M .......................................p 70 N8t-23182

p 183 N81-23838

BOLDMAN, D.R ...................................p 104 N77-32431 p 60 N86-28t01

BOLES, M.A ..........................................p 42 N78-21114

_MO, A.C ..........................................P 128 N79-22539 p 99 N81-14138 p 99 N83-32990

BONEY,LR ..........................................p 68 N78-33t35

BOOTH, E., JR ......................................P 191 N86-21280

BORUCKI, W.J ....................................p 158 N77-32689 p 149 N81-17622 p 203 N85-17892

BOSTIC, S.W .......................................p 180 N84-22299

BOUGHNER, R.E .................................p 136 N79-22580

BOURNE, G.H ......................................p 169 N78-11663

BOUSE,LF...............................................p1 N78-12999

BOWKER, D.E ....................................p 143 N85-30450

BOWLES, R.L........................................p 36 N83-22192

BOWLEY, C.J ......................................P 141 N82-20624

BOWMAN, H. O., II ...............................p 154 N83-16992

BOWMAN, J. S., JR .................................. p5 N77-33111 p 6 N78-12040

BOYDEN, R.P.......................................p9 N78-33050

p 22 N84-13162

BOYER, W.J .....................................p 66 N82-18275 p 66 N82-19257 p 67 N85-23813 p 68 N85-23840

BOYKIN, F.M .........................................p 70 N85-21246

BOYLE, R.J ........................................p 144 N79-22626 p 19 N62-14051 p 51 N84-32388

BOYNE,H ........................................p 152 N79-19519

BRABBS,T ........................................p 97 N78-25236

BRABBS, T.A ....................................... p85 N85-31244

BRAINARD, W.A .................................p 91 N77-33348 p 91 N78-20336 p 91 N78-20338 p 92 N79-15184 p 87 N79-21184 p 78 N79-22194 p 93 N79-32359 p 87 N80-16141

BRAITHWAITE, W.M ..........................p 41 N77-32154

BRANDL,D .........................................p 154 N83-27520 p 154 N83-28796 p 155 N85-25970 p 155 N85-27422 p 157 N86-28562 p 157 N86-29428

BRANDT, J.C ..................................... p206 N80-11972

BRANNAN, J.R ..............................p 68 N78-33135

BRASS, J.A ......................................p 142 N83-27293

BRAUN, W.H ........................................p 104 N77-31441

BRAY, R.S ...........................................P 40 N82-33381

BREITBACH, E.J ..............................p 55 N80-24324

BRENNECKE, M.W ...............................p 87 N79-16950

BRENTNER, K.S ............................p 22 N83-32776

BREWE, D.E ..............................p 119 N78-30585 p 93 N80-23453

BREWER, D.A ....................p 149 N81-22587

BREWER, W.D ......................................p 86 N78-15236 p 81 N82-31451

BRIDGES, P.M ..................p 206 N80-16998

BRIEHL,D .....................................p 148 N78-33618

BRIGGS, G.A ........................ p200 N81-11966

PERSONAL AUTHOR INDEX

BRINICH, P.F .......................................p 104

BRITSCH, W.R ..................................p 45

BROGKMAN,P .....................................p 115

BRODER, J.O ......................................p 195

BROECKER, W.S ........................p 169

BROOKS, C.G ........................................p 61 p 62 p 98

BROOKS, D.R ..................................p 64 p 64

BROOKS, J.D ........................................p 31

BROOKS, T.F ......................................p 166

BROWELL E.V ....................................p 150

BROWN, A.J .....................................p 140

BROWN, C. A., JR ...............................p 139 p t66

BROWN, G.V ......................................P 51

BROWN, J. S., JR ..................................p 33

BROWN,LWp 58

BROWN, P.W ...... .................................p 55 p 35

BROWN, R'D ..........................................p 91 p 8O

BROWN, R"L ..........................................p 94

BROWN, S.C ........................................P 166

BRUHWEILER, F.C .............................p 204

BRUMFIELD, J.O ................................P 141 p 142

BRUMFIELD, M.L.................................p 67 p 67

BRUN, N,L .......................................... 212

212

BRUNK, W.E ....................................... 201

201

BRUTON, W.M ..................................... 179

BRYANT, E.L....................................... 115

BUCHELE, D.R ...................................... 47

50

BUCKLEY, D.H ...................................... 85

91

91

91

91

91

91

92

86

92

86

92

, 120

3 120

120 i 120

92

93

87

3 93 3 93 3 94 3 B7 3 94 3 94 3 94 3 94 3 88 3 94 3 88 3 88 3 95

!22

3 95

122

122 D 88 s 88

69

p 95 p 89 3 89

123

123

3 95 3 95

123

p 89 p 89 p 90 p 9O p 96

p 124 p 96 p 90 p 96 p 96

BUCKLEY, J.D .......p 79

N77-32431

N79-33210

N60.30717

N79 13886

N85-26028

N78-25115

N79-28203

N80-20437

N76-12113

N80 19142

N78-10048

N78-12601

N85-16748

N82-20619

N81-20492

N83-19411

N84-24578

N79-30176

N84-28801

N80-14136

N82-16068

N78-12223

N79-23141

N81-33292

N85-21878

N85-15539

N83-26155

N83-26176

N83-22256

N84-17211

N78-12997

N81-16973

N80-t8997

N80-25224

N82-33020

N81-25352

N81-11039

N83-24509

N77-32286

N77-32312

N77-33350

N78-10295

N78-12222

N78-15276

N78-21294

N78-21295

N78-26198

N78-28247

N78-30206

N78-30238

N79-10425

N79-14386

N79-14387

N79-17227

N79-27308

N79-30380

N80-15234

N80-18178

N80 22494

N81 14079

N81-16210

N81-19300

N81 27282

N81-33293

N82-19374

N82 20291

N82-20316

N82 21301

N82-22349

N82 22366

N82-31691

N82 32491

N82-32737

N83-11496

N83-21110

N83-23419

N83 24641

N83 24695

N83-32908

N83-34019

N83 38400

N84 13577

N84 16334

N84 18399

N84-16653

N84-21716

N84-21721

N84 28965

N84-31349

N84-31379

N64 32825

N84-33590

N85-13006

N85-13044

N85-2t359

N86-11227

B-2

OJ_ ,P..OO_ Q'd_ITY,
PERSONAL AUTHOR INDEX

BUGLIA, J. J ............................... p 152 N80-13730

p 154 N82-33918

p 157 N86-27839

BULLOCK, T. .......................................... p 66 N82-14203

p 66 N82-15106

BUNCH, T. ...................................... p 199 N77-33003

BUNDICK, W. T, ......................... p 31 N82-22239

p 40 N83-16338

p 57 N83-33896

BUONCRISTIANI, A. M. .................. p t46 N83-18024

BURCHAM, F. W., JR ................... p 43 N79-13045

p 2 N80-15028

p 48 N81-15000

BURCHER, E. E. ............................. p 113 N77-32458

BURGENBAUCH, S. F. ................. p 196 N79-16709

BURGESS, E. ............................... p 61 N78-27146

p 206 N81-15925

p 207 N83-30340

BURK, S. M., JR ....................................... p5 N77-33111

p 6 N78-12040

BURKA, J. A. ............................. p 195 N83-21991

BURKE, J. ........................... p 196 N85-24994

BURKEN, J. J. ......................... p 56 N80-26328

BURLEY, J. R., II .......................... p 20 N83-t1059

p 27 N86-20348

p 52 N86-22576

p 28 N86-23559

BURLEY, R. R. ......................... p 23 N84-20493

BURNS, F. A. .......................................... p 87 N79-28288

BURNS, R. E ............................. p 144 N78-23571

p 172 N78-31740

BURSIK, J. W ............................. p 108 N80-25615

BUSCHMAN, A. ..................... p 103 N86-14498

BUSH, H.G. ................................. p62 N81-26160

p 74 N83-19806

BUSH, J. R., JR ...................................... p77 N81-24167

BUSHNELL, D.M. ........................ p 104 N78-13371

p 107 N79-33438

p 108 N80-22633

BUTERA, M. K ..................................... p 139 N80-15535

BUTLER, C. E. .................................... p 152 N79-17388

p 150 N86-16748

BUTLER, D. M ......................... p 200 N84-34332

BUTLER, R. W ................................. p 180 N84-34198

BUTTERFIELD, A ...................... p 65 N79-10078

p 66 N79-10097

BYRDSONG, T. A. ....................... p 57 N82-15075

BYVlK, C. E. ............................ p 146 N83-18024

C

CAGEAO, R. P. ............................ p 45 N80-11087

CALFO, F. D. ................................ p 114 N80-25635

CAUSE, A. J ............................... p 58 N85-28949

CALLAHAN, J. D. ..................... p 207 N84-32330

CALLAS, G. P. ........................................ p 31 N85-14806

CALLOWAY, R. L ..................... p 106 N79-20345

p 108 N80-23600

p 18 N82-13106

p 110 N83-16675

CAMARDA, C. J .............................. to 195 N79-13901

p 80 N79-32277

p 81 N81-16129

CAMP, D. W ............................ p158 N78-11642

p 158 N78-19711

p 159 N79-17413

p 160 N80-14633

p 162 N81-14555

p 3 N82o21139

p 165 N83-25265

p 4 N83-33827

p 165 N83-36587

p 166 N86-11735

CAMPBELL, C. W ............................... p 184 N83-27679

p 165 N84-24044

p 177 N84-24114

p 183 N85-28656

p 185 N85-28708

CAMPBELL, J. F. ........................ p 7 N78-14997

p 11 N79-16803

p 28 N86-27190

CAMPBELL, J. W ................................ p 153 N82-10624

p 168 N82-10661

CAMPBELL, R. L. ...................... p 18 N81-30088

p 21 N83-22162

p 23 N84-18161

CAMPBELL, W .......................... p 36 N83-27977

CAMPBELL, W. A., JR. ................. p 80 N80-30441

p 82 N84-26751

CAMPBELL, W. J. ....................... p 168 N84-10718

CANADY, J. E, JR ................ p 74 N82-33421

CANNADAY, R. L .........................p 53 N78-13071

CANNON, D. (3. ...................... p 39 N80-33404

CAPONE, F. J .............................. p 53 N78o27136

p 9 N78-28057

p 15 N80-24267

p 16 N81-19019

p 18 N81-30086

p 20 N82-30291

p 20 N83-22161

p 21 N83-26821

p 22 N84-10025

p 23 NB4-24538

p 28 N86-23561

CAPONE, L A. ......................... p 158 N77-32689

p t59 N78-30774

p 149 N81-17622

CAPRON, W, R ............................ 1331 N81-29111

CARDEN, H.D. .............................. p 31 N78-10049

p 128 N79-24372

p 33 N80-13025

p 131 N83-14521

p 133 N84-21901

p 134 N85-13267

GARDEN, J. L ........................... p 173 N82-24835

CARDER, K. L .............................. p 168 N81-31801

CARLE, W. E................................ p 162 N81-15639

p 162 N81-15640

CARLSON, A. B. ............................... p 74 N83-31713

CARLSON, H. W. .............................. p 1 N77-32072

p 7 N78-20078

p 8 N78-25061

p 9 N78-33051

p 11 N79-17806

p 12 N80-10105

p 14 N80-21279

p 15 N81-10004

CARLSON, J. R ............................ p 23 N84-18162

p 52 N86-22576

CARMI, U ................................... p 79 N84-20643

CARNEY, K. S. .............................. p 135 N86-I0579

CARR, L W .................................. p7 N78-17000

CARR, M. H .................................. p 204 N77-15961

p 152 N80-23912

p 206 N80-26239

p 200 N81-11966

p 200 N85-18888

CARR, P. C. .................................... p32 N78-20114

p 13 N80-13002

CARROLL, R. EL ........................ p 207 N83-25636

CARROLL, S. N. ............................... p 68 N85-34148

CARSEY, F. D. ............................... p 168 N84-10718

CARSON, G. 1"., JR ......................... p 8 N78-26109

p t9 N82-t4052

p 23 N84-24538

p 24 N84-32354

CARSON, T. M ............................... p 53 N78-23100

p 187 N80-11869

CARTER, D. L., JR ........................... p 67 N84-24632

CARTER, J. E. ...................................... p 106 N78-32385

CARUSO, S. V. ................................ p 101 N78-16266

CARY, A. M., JR. ........................ p 104 N78-13371

CARZOO, S. W. .......................... p 181 N85-15446

p 181 N85-27575

CASTELLI, A. ............................ p 177 N78-74659

CASTLE, C. B .............................. p 127 N78-26494

p 128 N80-10512

p 30 N83-34921

CASTNER, W. L. .......................... p 99 N83-32990

CASTRUCCIO, P. ........................ p 141 N82-20623

CAUSEY, W. E. ..................................... p 144 N78-23571

CAVlN, R. K. ................................. p68 N78-20176

CAWLEY, J.D. .............................. p 95 N84-21740

CAWTHORN, J. M ......................... p 186 N79-18687

CHAFFEE, N. ................................ p 63 N85-16889

p 63 N85-16937

CHAFFEE, N. H. ............................. p 99 N83-32990

CHAMEIDES, W. L. .............................. p 153 N81-23742

CHAMIS, C. C ............................... p79 N78-13138

p 79 NTB-16098

p 82 N84-13224

p 83 N86-21614

CHAMPINE, R.A. ...................... p 12 N79-23012

CHAN, L. Y. ............................ p 150 N82-27867

13 150 N82-28839

CHANEY, M. J. ............................. p 10 N79-12013

CHANG, A. T. C. ........................... p 151 N78-21690

p 151 N78-26677

p 152 N79-16473

p 152 N79-19519

CHANG, C. K ........................... p 210 N84-21485

CHANG, I. C. .............................. p 25 N85-10914

CHANG, S. ............................... p 175 N85-28562

CHANG, S. C. ............................ p 183 N86-28661

CHAPMAN, G, A. .................................. p 209 N84-27635

CHAPMAN, G. T. ....................... p 10 N79-12013

CHAPMAN, R. O. ...................... p 203 N81-25893

1320I N82-31163

p 203 N85-20961

CHATTOT, J. J ............................ p 15 N80-33356

CHEANEY, E. S ..................................... p 30 N81-31162

CHEGINI, H. .......................... p 117 N86-24962

COY, J. J.

CHEN, F. J ................................... p 111 N83-34229

p 111 N84-17534

CHEN, R. T. N. ............................. 13 55 N80-15138

p 35 N81-22039

CHEN, W. T. ........................... p 138 N78-21526

p 138 N78-23537

CHENG, N.M. ............................ p 162 N81-15640

p 163 N81-16679

CHERNYSHENKO, Y.M. .................... p 161 N80-t6682

CHESTNUTT, D ........................... p 189 N83-10883

CHEVALIER, 1t. L. ........................ p 1 N78-12999

CHIMA, R. V. ............................. p 22 N83-32774

CHIN, D. O. ...................................... p 35 N81-16040

CHOO, Y. K. .......................................... p 145 N82-16477

p 146 N83-36549

CHOUDHURY, B.J. ............................ p 15_ N78-21690

p 152 N79-16473

CHRISTENSEN, L. S. ...................... p 152 N79-30869

CHURCHILL, E. ........................ p 172 N79-11734

CHYU, W.J. ................................ p 68 N78-20176

C|COLANI, L S. .......................... p 54 N79-13057

p 54 N79-17872

p 31 N83-29193

CLARK, A. V. ..................................... p 121 N80-27694

CLARK, B. J. .............................. p 188 N81-33947

CLARK, L.G. .................................. p 67 N84-24632

CLARK, R. K. .............................. p 90 N86-26412

CLARY, J. B. .................................. p 176 N80-23008

p 176 N81-15702

CLAUS, R. W .............................. p 44 N79-14098

p 44 N79-23086

p 48 N81-19121

CLEVENSON, S. .......................... p 187 N80-28150

CLEVENSON, S. A ..................... p 171 N78-32717

p 171 N79-23662

p 171 N80-13769

p 172 N83-34579

p 172 N84-20155

COATES, G. O. ........................... p 171 N78-11696

COCHRAN, R. P. ........................ p 47 N8t-t2089

COE, C. F. ................................... p18 N82-13108

COE, H. H .................................. p119 N78-20513

p 121 N80-15410

p 124 N84-32824

p 125 N85-31511

COE, P. L, JR ................................... p 12 N79-26020

p 54 N79-31223

p 16 N81-14974

p 22 N83-36000

p 59 N86-22580

COFER, W. R., III .................................. p 84 N78-22188

p 84 N79-12178

p 85 N82-22330

COHEN, L .................................. p 209 N81-23004

COLE, G. L. ........................................... p 45 N79-28176

p 180 N85-t7596

COLEMAN, P. J., JR ...................... p 65 N78-15142

COUN, L ................................ p 207 N83-30340

p 208 N86-11137

COLLADAY, R. S. .......................... p 97 N78-20351

COLLINS, F. G. .................................. p 72 N82-12109

COLLOM, R. R. ............................. p 50 N83-26839

COLTON, G. W ............................. p 61 N78-21t74

COMISO, J. C ................................ p 168 N84-10718

COMPTON, W. B., III ....................... p 23 N84-18162

COMPTON, W, D, ........................... p 63 N84-25737

CONEY, 1". A. ........................................ p 149 N80-27832

CONNORS, M.M. ......................... p t99 N7821019

p 174 N85-32772

CONWAY, E, J ............................... p 117 N82-18578

p 118 N83-27200

COOK, A. M .................................. p 32 N79-14082

COOK, W. J ................................ p 10 N79-12013

COOPER, G. E ............................. p 29 N80-22283

COOPER, L. P. ..................... p 46 N80-14125

p 48 N81-24065

COOPER, P, A. ..................................... p 128 N79-31626

p 80 N79-32277

CORLEI_, W. A ........................ p 18 N82-12035

CORUSS, W. R. ................................... p 59 N81-32153

CORRIGAN, J. P. ........................ p 65 N78-15142

COTE, C. E ................................ p 165 N83-14835

COTHRAN, E. K. ........................ p 62 N82-26330

COUNAS, G. ........................... p 152 N79-19519

COVELL, P. F. ......................... p 19 N82-22215

p 22 N83-34904

p 26 N85-27822

p 26 N85-29922

COX, S. C .................................. p 142 N83-28506

p 142 N85-11404

p 142 N85-11405

COY, J. J ..................................... p 119 N78-18429

p 121 N79-32552

p 121 N79-33476

p 122 N81-20423

p 125 N86-14612

B-3
COZZOLONGO, J. V.

COZZOLONGO, J.V .....................p 21 N83-22166

CRABILL, N.L ...................p 207 N8t-25992

CRAFTS, J.L .................................. p69 N85-33169

CREDEUR, L. .......................p 31 N81-29111

CREEDON, J. F. ........................p 39 N81-24058 p 40 N84-12164

CREEL, T. R., JR. .......................p8 N78-25059

p9 N78-31045

p 108 N80-26622 p 111 N83-34229 p 111 N84-17534

CREWS, J. H. JR. .................p 80 N79-23140 p 81 N81-24178 p 83 N86-20508

CRISP, V.K ................................p 177 N85-31839

CRON, A.C. ..................................p 125 N85o20339 p 125 N85-20361 p 125 N85-21659

CROOM, C.C ..................................p 25 N84-33379

CROOM, D.R ..................................p 11 N79-22038 p 12 N79-24961

CROSS, A.E. .........................p 103 N86-20678

CROUSE, J.E. .........................p 47 N80-28352 p 49 N82-15039

CRUGNOLA, A. ................................p 92 N79-23216

CSATI,E .....................................p 138 N79-13475

CUCINOTTA.F...........................p 174 N84-29479

CUCINOTTA. F. A. ........................p 193 N86-30485

CUELLAR,M ................................p 74 N83-22317

CULLOM, R.R .................p 41 N78-11106 p 44 N79-25022

CULPEPPER, R.G .........................p 59 N79-29199

CUMMINGS, W. D. ......................p 65 N78-15142

CUNNAN, W. S. ................................p 43 N78-33109 p 44 N79-23967 p 45 N79-27143

CUNNINGHAM, H.J ............p 127 N78-28481 p 23 N84-20480

CUNNINGHAM. R.E ................p 41 N78-13064 p 68 N86-24722

CUNNOLD, D.M .....................p 153 N82-12687

CURREN, A.N ...................... p69 N78-33137 p 69 N79-21120 p 95 N84-18400 p 95 N84-28989 p 96 N86-15394

CURRY, D.M ...................................p 105 N78-18364 p 106 N78-30555

CURRY, R.E...................................p 54 N79-10068

CUSANO,C ......................................p 123 N83-28453

CUTTS, J.A. .........................p 200 N81-11966

CWYNAR, D. S, ..........................p 41 N77.31154 p 41 N77-33169

p 184 N78-30896 p 177 N80-16742

CYGNAROWICZ, T.A ..................p 169 N78-18673

D

DABBS, J.R .............................p 209 N83-13048 p 209 N83-25646

DASNEY,R ..................................p 74 N84-23677

DAGENHART, J.R ............................p 109 N82-11391

DAILEY, C. .......................................p 200 N80-14977

DAJANI, J.S. ..........................p 198 N79-10942

DAME, T.M ......................................p 204 N84-20457

DANFORD, M.D. ......................p 88 N83-1649t p 89 N84-13263 p 90 N85-22662 p 91 N86-30837

DANIELE, C. J. ............................p2 N79-18796

DANIELS, E. F. ......................p 186 N79-14874 p 188 N82-14879 p 190 N85-30767

DANIELSON, J.A ..............p 140 N82-20620

DARDEN, C.M ......................p 10 N79-t5000 p 12 N80-10102 p 17 N81-21016

p 111 N84-229C'6 p 26 N85-29923

DAUGHERTY, J,C ..............................p 33 N80-11068 p 14 N80-17986

DAUGHERTY, R.H ...........................p 36 N83-34935

p 135 N86-11522

DAVIDSON, R.E. ..............................p3 N82-14049

DAVIES, M.E ...........................p 205 N78-30025

DAVIS, A. ...........................................p 199 N77-33003

DAVIS, B.D. ..............................p 196 N79-19912

DAVIS, C.M .......................... p31 N81-29111

DAVIS, D. D. ............................p 153 N81-23742

DAVIS, Jo G., JR. ...........p 80 N79-30297

DAVIS, J. H. ..................................p 195 N83-21991

DAVIS, M. H. .............................p t63 N82-12715

DAVIS, R.A .......................................p 21 N83-25665

DAVIS, R.C ............................p 127 N78-12475 p t29 N80-18427

B-4

p 130 N82-20567 p 131 N82-28665 p 89 N83-35100 p 132 N84-18675 p 135 N85-33537 p 90 N86-13406

DAVIS, R.E ...........................p 164 N82-15677 p 143 N85-30450

DAVIS, S. ...................................p7 N78-17999

DAVIS, S. M. .................................p 141 N83-17942

DAVIS, W. 1". ......................p 116 N84-11460

DAYAN, M. .............................p 123 N84-13577

DAYTON, J. A., JR. ......................p 101 N79-22375 p 101 N81-20359 p 102 N81-28352 p 102 N83-25985 p 103 N86-13643

DEADMORE, D. L. ........................p 89 N84-26783

DEAL, P. L. ............................................. p32 N78-27111 p 12 N79-23012 p 55 N80-14136 p 29 N81-12043 p 30 N83-14077 p 57 N84-12190 p 58 N85-t1002 p 58 N85-34144

DEATKINS,O ........................................p 67 N83-32828

DEAUX, T. N. ....................................p 32 N79-14083

DECKER, A. J. ............................p 114 N79-17195 p 114 N79-21329 p 115 N82-22481

DEEPAK, A. ...............................p 151 N78-12586 p 154 N82-32915 p 136 N83-11534

DEFIELD, J. G, ...........................p 172 N78-31740

DEFOREST, S.E .............................p 65 N78-t5142

DEI.AAT, J. C. ...........................p 101 N79-32467

DELOACH, R. ...........................p 191 N86-16041

DEMPSEY, T. K. .........................p 171 N78-1t696 p 171 N78-32717 p 186 N79-18687 p 171 N79-23662 p 189 N83-34713

DENOLER, R. P. .........................p 52 N85-28944

DESHPANDE, M.D ..............................p 100 N84-20735

DESMARAIS, R.N ..........................p 23 N84-20480

DEUTCHMAN, P.A. ............................p 193 N85-17690 p 193 N86-21297 p 193 N86-23388 p 193 N86-30485

DEVEIKIS, W. D. ..............................p 111 N83-28378

DEVERS, A. D. ...................................p 70 N78-25123 p 70 N78-25124

DEVINCENZl, D.L ................................p 66 N82-20225 p 79 N83-24556

p 175 N86-26844

DEXTER, It. 13. ....................................p 80 N79-30297

DEYOUNO, R.J. ...........................p 118 N83-27200 p 118 N84-31617

DICARLO, D. J. .......................................p 37 N85-25248

DIEDRICH, J.H ...............................p 47 N81-11037

DIETLEIN,L F. ..........................p 169 N77-33780

DIETRICH, D. A. ................................p 41 N77-31152 p 42 N78-20132

DIETZ, R.H ...................................p 145 N81-16533 p 145 N81-27622

DILL. C. C. ......................................... p28 N86-21507

DILL&RD, J.P. ..............................p 140 N82-20621

DILLON, J.L ...................................p6 N78-12038

p8 N78-25059

p9 N78-30055

p9 N78-31045

p 13 N80-12064

DIRUSSO, E. ............................ p49 N83-11126 p 50 N83-25712 p 51 N84-16181 p 52 N86-15313

DOAZAN, V. ................................p 200 N82-25027

DODS, J. B., JR ...................................... p18 N82-13108

DOGGEI"r, R. V., JR. ......................p 34 N80-25321 p 34 N80-29287

DOLLYHIGH, S. M. ..........................p7 N78-16000

p8 N78-22028

p 10 N79-14023

DOMACK, M.S. ..............................p 89 N84-23750

DONOVAN, L. F. ........................p 196 N83-23188

DODGE, P.M ............................p 96 N78-13234

DOOLIN, B. F. ............................p 176 N82-29904

DORNIK, S.E............................p 205 N78-30025

DORSEY, J.T. .............................p 132 N83-28491

DOUGHERTY, N. S., JR .................p 19 N82-26227

DOW, D.D .............................p 142 N83-29750

DOWNS, S.W .......................................p 138 N78-18497

DOWSON, D. .......................................p 119 N78-28458 p 119 N78-33447

DOYLE, F. J, ........................... p6t N78-21174

PERSONAL AUTHOR INDEX

DRAKE, F. ............................p 175 N84-22178

DREHER, R.C ................................p 33 N79-29171 p 29 N80-27302 p 35 N82-18204 p 35 N82-24193 p 36 N82-31321

DRESSLER, R.F. ........................p 62 N82-29335

DRUMMOND, J. P. ....................p 105 N78-22333

DUBIN,M .........................p 209 N81-13912

DUDZINSKI, T.J ...........................p 148 N79-31841 p 150 N83-13643

DUERR, R. A. .................................p 50 N83-23309

DUFOUR, P.A. ..........................p 175 N86-26844

DUGAN, D.C. .............................p 31 N83-18704

DUKE, J.R ....................................p 161 N80-16682

DUKE, M.B ................................p 205 N78-16973

DULtKRAVICH, D. S. ..................p 15 N80-27284 p 15 N80-33357 p 18 N81-31128

DUNHAM, D. M. .......................p5 N86-16187

DUNHAM, J.R ...........................p 179 N82-24845

DUNN, H.J. ...........................................p 129 N80-22737 p 181 N80-25039 p 130 N81-11422

DUNNE, J. A. ..........................................p 61 N78-27146

DURACHTA, J. ...........................p 76 N85-30005

DURBIN, P. A. ..............................p 110 N83-22546 p 112 N85-20270

DURHAM, D.E ................................p 159 N79-17413

DURMNG, B. J. ...............................p 127 N78-20536

DUSTIN, M.O. ..............................p 45 N79-28176

DUXBURY, T.C ..........................p 200 N81-11966 p 207 N84-32330

DWOYER, D.L .........................p 108 N80-21702 p 182 N81-22754

DWYER, R.E ................................p 139 N81-11438

DYKE, R. A., JR. .............................p 87 N79-28288

E

EBIHARA, S. 1". ...............................p 101 N81-20359 p 103 N86-32629

ECKERT, W. T. ..........................p 14 N80-17984 p 59 N83-17560

ECKSTROM, C.V ..........................p 27 N86-20350

ECONOMOS, A.C. .......................p t70 N83-16018

EDAHL, R. A., JR. ............................p 85 N82-22330

EDDY, J. A. .................................p 209 N79-22991

EDGE, T. M. ...........................................p 179 N81-12760

EDWARDS, C.LW ...............................p 32 N78-16042

p 107 N79-30518 p 74 N83-31713

EGGERS, J. M. ........................................p 42 N78-23093

EGGLETON, R.E ............................p 61 N78-21174

EIKE, D.R ...................................p 70 N86-23620

EKPANYASKUN, S. ......................p 144 N77-16437

EL-BAZ,F........................................p 61 N78-21174

p 138 N80-10538

EL-MAHDI, A. M. ............................p 170 N79-10728

ELBER,W ................................................p 82 N83-24562

ELLERBRUCH, D. .........................p 152 N79-19519

EMERSON, C. M. ................................p 70 N86-23620

ENDERS, J.H ...................................p 165 N83-25265

ENDRES, D. L. ..........................p 163 N81-19709

ENGLISH, R. E. .............................p 78 N86-21577

ENGLUND, D.R ...........................p 150 N83-13643

ENSIGN, C. R. ..............................p 130 N8t-23486

ERCEGOVlC, D.B .......................p 44 N79-14099

ERICKSON, E.F. ...................p 202 N85-17848

ERICKSON, G.E. ...........................p7 N78-14997

p 11 N79-16803

ERICKSON, K.N ..........................p 65 N78-15142

ERICKSON, L. L, ........................p 68 N78-20176

ERLICHMAN, J. ..................................p 199 N77-33003

ERTEL, I.D. ............................ p61 N78-25115 p 98 N80-20437

ERZBERGER,H ......................................p 30 N80-28329 p 30 N85-32101

ESGAR, G.M ....................................p 46 N80-21324

ETHELL, J.L ..............................p 36 N84-15144 p 38 N86-30720

EVANS, A., JR. ............................p 97 N81-29246

EVANS, J.S. ............................p 105 N78o20463

EVANS, N. ......................................p 206 N80-26239 p 208 N84-34363

EVERHART, J. L. ...................................p 59 N83-18770

EXTON, R.J. .............................p 147 N77-32622

EZELL, E. C. ............................p 61 N79-10074

p 208 N84-35248

EZELL, L.N ...............................p 61 N79-10074

13 208 N84-35248
PERSONAL AUTHOR INDEX GRANTHAM, W. D. F

FAHERTY, W.B ............p 64 N79-12127

FALES, C. L. ...........................p 194 N81-13739

FALLER, K.H ...........................p 167 N78-12644

FANALE, F. P. ............................p 208 N86-11137

FARASSAT, F. ................................p 187 N80-27161

FARLEY, G.L. ......................p 81 N81-24179 p 83 N85-26924

FARLOW, N.H ......................................p 148 N79-30844

FARMER, F.H .........................p 168 N79-28864 p 139 N61-20492 p 166 N83-19411

FARRELL, C. A. ...........................p 20 N82-28247

FARRELL, J.E ............................p 172 N83-33538

FASANELLA, E. L. ...............................p 131 N83-t0442 p 38 N86o30721

FAUST, R. P, ........................................p 71 N81-10100 p 71 N81-10101 p 71 N81-11102

FAUT, O. D. ................................ p85 N83-18863 p 123 N84-18653

FAY, T.H ...............................p 177 N85-28563

FEARN, R.L .........................................p 105 N78-26392 p 107 N79-32500

FEDORS, J.C. ......................................p 168 N79-28863

FEISTEL, T.W ...........................p 34 N80-25318

FENBERT, J.W ...........................p 16 N81-14974

FEREBEE, R. C. ..........................p 73 N82-20238

FERNANDEZ, M. A.B ..............p 50 N83-3494t

FERRANTE, J. ............................p 87 N79-21184 p 93 N79-32359 p 88 N82-21300

FERRIS, A. T. ............................p 22 N84-13162

FERRIS, J.C. ............................p 23 N84-18161

FESSLER, T. E. .....................................p 178 N78-10746 p 178 N78-20806 p 178 N79-23688

FICHTEL, C.E.................p 199 N77-20977 p 204 N82-21118

FICHTEI_ G.H ......................p 162 N80-26999

FICHTL, G. H. ...........................p 72 N82-12109

FIELDER, W. L. .........................p 144 N78-28624

FIELDS, J. M. .........................p 189 N83-34713

FIELDS, R. A. .............................p 34 N80-15068

FIMMEL, R. O. ......................................p 205 N77-28055 p 206 N81-15925 p 207 N83-30340

FINELU, G. EL .......................................p 167 N86-24090

FISCHER, E. .............................p 173 N81-13635 p 173 N81-13636

FISCHER, G. K. ...........................p 123 N83-20119

FISHBACH, L. H. .....................p 51 N84-21549

FISHER, B.D ..............................p 32 N78-18044 p 12 N79-23012 p 30 N83-14077

FISHER, D. F. ............................p 19 N82-26227

FISHER, F.A. ........................p 29 N78-11024

FITZMAURICE, M.W ......................p 69 N78-10200

p 117 N78-16354 p 113 N78-17360

FLATLEY, T.W .....................p 65 N78-15143

FLECHNER, S.G .........................p 12 N60-10101 p 38 N80-23304 p 26 N85-26667

FLEIG, A. J. ..............................p 164 N82-28880 p 164 N82-29826 p 154 N83-16992 p 165 N83-28828 p 165 N84-16720

FLEMING, D.P. ....................................p 121 N80-19495

FLEMMING,K .................................p 76 N81-31281

FLOCK, W. L. .......................................p 100 N84-13397

FLORES, F.J .................................p 97 N81-24283

FLOWERS, O. .........................................p 74 N83-22317

FORCE, D. A. ...................................p 103 N86-13643

FORD, W. F. ..........................................p 178 N78-10746 p 178 N78-20806 p 182 N84-13885

FORMAN, R. ...............................p 86 N78-11230

FORREST,K ............................p 99 N84-33613

FORREST, K.A. ............................p 126 N86-32763

FORSYTHE, R.G .......................p 168 N82-16683

FORWARD, R.L ......................p 199 N78-21019

FOSS, W. E., JR ...........................p 17 N81-20026

FOSTER, J. D. ............................p 31 N83-18704

FOSTER, J. M. ...........................p 24 N84-27675

FOUGHNER, J. T., JR ................p 116 N82-32663 p 28 N86-27190

FOURNIER, R.H. ..........................p9 N78-30053

FOUSHEE, H.C .....................p 30 N81-30101 p 30 N82-13123

FOWLER, W.B. .............................p 76 N81-31281

FOWLIS, W.W ......................................p 159 N78-32641 p 160 N79-32796 p 163 N82-12715

FOWUSS, W.W ...............................

FOX, C. H, JR ........................................

FOX, K. ...................................

FOX, T. ....................................

FOX, T. A. ..............................

FRALICK, G.C ..................................

FRANK, A. E. ...........................

FRANK, L. .............................................

FRANKLIN, J. A. .........................

FREAS, G. W, JR .....................

FREDA, M.S. ............................

112 i 166

3 113

136

21

3 207

207

184

:) 101

:) 101

:_ 101

102

114

158

208

56

57

138

138

60

60

FREEMAN, C. E. .............................. 15

FREEMAN, D. C., JR ......................p9

p 55 p 55 p 56

FREIMAN, S. ...............................p 99

FREITAS, R. A., JR ....................p 76

FRICKS, O. It. ...................................p 198

FRIEDL_NDER, A. L. ......................p 67

FRIEDMAN, D. B. .........................p 138

FRIEDMAN, R. ...........................p 97

FRIEND, E. L. .............................p 54

FRINK, N.T. ............................. p15

p17

FRISCH, H.P ..............................p 70 p 7O p 7O p 72 p 72 p 72

FRITZ, T. A. ..............................p 65

FROST, A. L. .................................p 28

FROST,W .................................p 158 p 159 p 159 p 159 p 152 p 160 p 162

p3

p 165

p4

p 166

FRYBURG, G.C ............................p 90

FRYE, R. J. ...................................p 52

FUCHS, A. .....................................p 61

FUCHS, A. J. ...................................p 64

p64

FULLER, D. E. .............................p 13

FULTON, C.L. ...................................p5

FULTON, R.E ................................p 177

FUSARO, R.L. ......................p 91

p91 p 92 p 92 p 93 p 93 p 94 p 95

FUTRAL, S. M, JR ..........................p7

G

GALABOFF, Z.J. .......................p 67

GALLOWAY, W.E ..............................p 144

GANS, R. F. .................................... p111 p 113

GARCIA, F., JR ........................p 190

GARREN, J. F., JR ......................p 54 p 38

GARRE'I'r, H.B. .........................p 74

GARREt-r, L. B. .................p 66 p 72

GARTRELL,LR .............................p 114

GARY, J.P .............................p 179

GASSER, M. G. .......................p 99

GATMN, D. H. ...................................p 53

GATSKI, T. B. .................... p111

GAUGLER, R. E. .....................p 105 p 106 p 129 p 110

GAULT, D. E. .............................p 205

GAULT, J.W ......................p 176

N84-23852

N85-20605

N86-23851

N80-15445

N83-22162

N82-25043

N82-26134

N83-I0876

N79-17139

N79-28420

N80-21669

N81-30360

N80-24595

N77-30705

N86-11137

N81-11044

N82-20187

N78-21526

N78-23537

N85-18991

N86-18328

N80-25296

N78-30053

N80-13052

N80-21336

N81_13066

N84-33613

N83-15348

N79-28062

N83-32828

N79-16329

N83-11340

N79-13056

N80-28304

N81-25040

N78-21200

N78-25123

N78-25124

N81-25138

N81-25139

N81-25140

N78-15142

N86-21507

N78-19711

N79-14678

N79-14679

N79-17413

N79-30869

N80-14633

N81-14555

N82-21139

N83-25265

N83-33827

N66-11735

N84-28958

N85-28944

N78-76855

N79-26082

N80-28389

N80-16032

N77-33112

N84-22179

N78-15277

N78-20337

N79-13158

N79-13159

N79-30381

N80-17220

N82-19373

N83-14269

N78-16001

N83-32826

N78-23571

N84-15427

N85-28260

N85-29694

N79-29195

N80-27360

N84-33452

N82-14202

N82-14276

N80-24594

N84-20208

N84-15327

N78-20140

N64-13500

N78-28374

N79-18288

N80-22734

N82-30498

N78-30025

N80-23008

GAUNTNER, D.J. .......................p 104 N78-17338

GAUNTNER, J.W ......................p 104 N78-13379

GAYLE, J.B. ..................................p 183 N78-31854

GEDEON, L. .............................p 107 N79-30516

GEDNEY, R. T. ..................................p 149 N80-27832

GEE, S. W. .......................................... p32 N78-20114

GELDER, T.F ................................p 46 N80"17071 p 46 N80"21324

GELLER, M. A. ................................p 156 N86-25911

GENTRY, C. L., JR. .......................p 191 N86-31341

GENTRY, G. L., JR ........................p 22 N83-36000

GERA, J. ..........................................p 53 N78-20143

GERSTEIN, M. .............................p 44 N79-25016

GERSTENMAIER, W.H .................p 111 N84-17525

GERSTNER, D. A. ........................p 138 N76-18497

GESSOW, A. ................................... p6 N78-11007

GEYSER, L.C. .............................p 43 N78-33t10

p 181 N84-16843

GEZARI, D.Y. ......................p 202 N84-26519 p 202 N84-26520

GHONEIM, A. F. .............................p 50 N83-32806

GIBBONS, D. E. ............................p t14 N80-12399

GIERE, A. C. ................................p 136 N80-15445

GILBERT, E. ................................p 165 N83-14835

GILBERT, W. P. ...............................p 33 N79-30176 p 13 N80-13002 p 55 N80-14136 p 2 N80-29244 p 26 N85-23708

GILBREATH, W.P. ........................p 62 N79-32225 p 76 N83-15348

GILL_ A. .........................................p 89 N83-24640

GILLESPIE, E.A ..............................p 59 N79-29199

GILYARD, G. B. .................................p 53 N78-21160 p 56 N80-26328

GLADDEN, 14. J. ............................p 107 N80-17397 p 108 N80-24577

GLASSMAN, A.J ........................... p47 N81-11038 p 50 N83-32807

GL&WE, G.E .............................p 113 N78-t5463

GLOERSEN, P. ..................................p 168 N84-10718

GLOSS, B. B. ..................................p 10 N79-15902 p 59 N83-18748 p 27 N86-20347

GLOVER, B. J. ............................p 172 N86-27920

GNOFFO, P.A. ...........................p 104 N78-18362 p 104 N78-18363 p 112 N85-16065

GOEKOGLU, S. A. ...........................p 111 N84-19741

GOLDBERG, EL D. ..........................p 168 N80-12718 p 168 N80-23956

GOLDBERG, R. A. ...........................p 209 N79-20961

GOLDBERG, T.J ............................p 105 N78-30554

GOLDFORD, A.I ............................p 147 N78-28682

GOLDMAN, A. .............................p 192 N80-26125

GOLDMAN, L. J. .............................p 14 N80-17030 p 19 N82-14051 p 20 N82-26234

GOLUB, Ro At. ........................................p 189 N84-21277

GOMBERG, R.L .............................p 147 N78-11520 p 147 N78-15596 p 68 N78-33135 p 152 N80-13730

GONG,t ................................p 108 N81-12361

GOOD, B.S. ..................................p 195 N85-24961

GOODE, M.W ................................p 38 N78-31101 p 55 N80-22358

GOODERUM, P.B .............................p 42 N78-23093

GOODYKOONTZ, J.H .....................p 189 N84-15894

GORDON, D. ...............................p 164 N82-28880 p 164 N82-29826 p 165 N83-28828

GORDON, F., JR ..............................p 76 N80-28424

GORDON, S. ...............................p 195 N82-32186 p 195 N82-32187 p 195 N82-32188 p 195 N82-32189

GOREE, J. G. ...........................p 130 N81-13373

GORLA, R. S, R. ............................p 121 N79-32552

GORRELL, W. T. ........................p 45 N79-27143 p 45 N79o30191 p 49 N82-15039 p 51 N84-28795

GOSSET, B. ...............................p 62 N79-32225

GOTO,H ........................................p 90 N85-13006

GRACEY,W ...............................p 34 N80-24296

GRAFTON, S. B. .........................p 57 N84-17184

GRAHAM, R.W .......................p 104 N77-32432 p 45 N80-11087 p 110 N83-12360

GRANA, D. Co ..........................p 148 N79-14591

GRANTHAM, W. D. ...............................p 32 N78-27111 p 29 N81-12043 p 4 N82-31294

13 57 N84-12190 p 58 N85-11002 p 58 N85-34144

B-5
GRAVES, J. R.

GRAVES, J. R. ............................... p 77 N62-11109

p 77 N62-21254

GRAVES, R. A., JR .......................... p t4 N80-19031

GREAVES, J. R ........................... P 165 N83-24028

GREELEY, R. .......................... p 204 N77-15961

p 152 N80-23912

p 200 N61-11966

p 201 N86-27136

GREEN, D. _ ......................................... P 13 N80-10107

GREEN, R. N. .............................. P 158 N78-23679

p 159 N79-13644

p 161 N80-20986

p 162 N61-13593

p 164 N82-13620

GREENBAUER-SENG, L A. ........... p 85 N83-24575

GREENE, G.C. ..................................... p 5 N86-16187

GREENE, W. H. ............................. p 132 N84-16585

GREGORY, F.D. ..................... p 32 N76-27111

p 55 N80-22358

GREGORY, G. L. ...................... p 150 N83-16952

p 150 N84-16764

GREGORY, R. A ......................... p 34 N80-25321

GREW, G. W. .......................... P 142 N83-26201

p 143 N85-23237

GRIDLEY, D. ............................ p 191 N86-16040

GRIFFIN, R. H., II ...................... p 138 N78-21568

GRIGGS, E. I. ........................... p 104 N78-15434

GRIMWOOD, J. M. ........................... p 62 N79-26203

GROLIER, M. J ............................ p61 N78-21174

GROOM, N. J. .............................. p 98 N78-18252

p 99 N61-203tl

p 101 N61-22261

p 3 N82-19134

p 77 N64-12226

p 78 N65-13850

GROSE, W. L .......................... p t63 N81-23761

p t67 N86-25924

GROSSMITH, S. W, ....................... p 53 N78-26151

GRUNWALD, A.J. .............. p 39 N61-13958

GUEST, J. .................................. p200 N61-I 1966

GULL T. R. .............................. p 201 NB0-11966

GUMBERT, C. R ........................... p 28 N66-20352

GUNTHER, F. J. .................................... p 136 N78-33499

GUPTA, K. K ............................. p 134 N65-11378

GUPTA, R. N ............................... p 1t3 N66-14530

GURGANUS, E. A. ............................. p 147 N76.12554

p 147 N78-12555

p 167 N78-12645

p 147 N78-33616

p 146 N79-17360

p 168 N79-28664

p 166 N79-31890

p 140 N82-13468

p 150 N82-21774

GUY, R. W ............................. p 60 N83-36039

GUY, W. W ............................... p 99 N63-32990

GYORGAK, C. A. ............................ p 87 NB0-11166

H

HAAS, J. E. ......................... p 5 N77-30089

p 5 N77-32082

p 7 N78-14998

p 7 N78-16001

p 47 N80-33410

p 48 N61-20076

p 49 N63-11125

p 5t N84-32368

HACKER, B.C. ............................. p 61 N78-20151

HADY, W. F. ................................... p 120 N79-10424

p 92 N79-23216

HAEHNER, C. ......................................... p 99 N84"33613

HAFTKA, R.T. ........................... p 126 N79-25427

p 110 N82-31646

HAGAMAN, J.A. .............................. p 82 N83-24561

HAGGARD, J. B., JR. .................. p 109 N81-24386

HAGGARD, K. V ........................... p 163 N81-23761

p 167 N86-25924

HAGYARD, M. J ................ p 210 N85-29869

HAINES, R. F. ....................... p 173 N80-26039

p 173 N81-13635

p 173 N61-13636

p 173 N81-17711

HAIR, L M ................................... pll N79-17510

HALFORD, G. R. ....................... p89 N84-17350

p 90 N86-12295

HALL D. N. B, ........................ p 202 N82-33296

RALL J. B. ............................... p 107 N79-30518

HALL, J. Bo, JR. ........................... p 210 N62-33320

HALL R.C. ................................. p 211 N77-33030

p 212 N77-33046

p65 N76-15149

HALL R, M. ....................................... p 12 N79-22043

p 108 N80-25615

p 109 N8t-324t8

p 113 N66-20720

B-6

HALLION, R. P. .......................................... p 4 N85-17934

HALLISSY, J. 15. ............................... p 13 N80-12064

p 57 N82-15076

HALPERT, G ......................................... p 144 N77-16437

p 145 N80-20820

p 145 N81-21493

p 102 N82-20402

p 146 N83-14684

p 102 N83-35230

HALSTEAD, T. W ................................. p 169 N84-18829

p 169 N65-26054

HALYO, N. .............................. p 114 N80-22660

p 115 N61-33452

HAMER, 14. A. ............................... p 53 N78-27138

p 7t N81-13082

p 74 N64-23675

p 75 N8_16250

p 75 N6Pm30801

HAMILL P. .................................. P 160 N79-21720

p 160 N79-2172t

p 161 N80-15726

p 153 N82-19734

p 154 N84-32952

HAMILTON, D. A. ............................ p 71 N60-16091

HAMILTON, 14. 14., tl ............................ p 105 N76-22332

p 107 N79-33441

p 14 N80-19031

p 108 N80-33719

p 110 N83-24608

HAMPSON, R.F. .................................. p 156 N86-25911

HAMROCK, B.J. .................................. P 119 N78-28458

p 119 N76-30585

p 119 N78-33447

p 122 N82-25514

p 123 N83-16759

p 123 N83-27214

p 124 N84-31640

p 125 N85-32329

p 125 N85-32330

HANCOCK, O. W .................................. p 168 N82-16683

HANDSCHUH, R. F. ............................... p 48 N82-14090

HANKINS, W. W., Iit ............................ p 176 N79-33855

p 174 N86-26836

HANNAFORD, J. F. .............................. p 140 N82-20619

HANNUM, N. ................................ p 76 N78-13124

HANNUM, N. P. ............................... p 77 N81-20176

HANS*JUERGEN, C.B. ....................... p 168 N79-28863

HANSCHUH, R. F. .................................. p 96 N85-13045

HANSEN, C. F. ...................................... p 192 N83-27809

HANSEN, I. G. ................................ p 52 N85-28944

HANSEN, J. .................................... p 169 N85-26026

HANSON, P. W ................................... p 2 N79-23689

p 2 N79-27070

p 2 N80-11026

HARDIN, J. C ........................................ p 187 N79-32057

p 166 N81-24854

p 191 N86-24391

HARDY, G. H ........................................... p56 N81-11044

p 56 N81-19131

p 57 N82-20187

p 57 N84-13198

HARNEY, P. F. ................................. p 39 N81-20074

HARRINGTON, R. F. ........................ p 116 N83-28410

HARRIS, J. E. ........................................ p 104 N78-13371

HARRIS, R. L, SR ........................... p 36 N78-31101

p 171 N61-23791

p 172 N62-14804

p 172 N86-27920

HARRISON, A.A. ....................... p 174 N65-32772

HARRISON, R.L. ........................ p 40 N82-33381

HARSHVARDHAN ................................ p 156 N86-22022

HART, M. M. ............................ p 27 N85-33106

HART, S.G. .......................................... p 174 N65-14487

p 174 N85-14535

HARTMAN, H. ................................ p 175 N85-32777

HARTZELL E.J. .......................... p 174 N65-14487

p 174 N65-14535

HARVEY, W.D. ........................... p 108 N61-13303

HARWARD, C. N ............................ p 153 N80-33998

HASS, J. E .................................................. p 6 N78-11008

HASSELL J. L., JR. ........................ p 14 N80-22266

HASTINGS, E. C., JR. ......................... p 29 N78-13029

p 57 N82-19225

HASTINGS, L. J .................................... p 144 N77-30617

HATFIELD, J. J. ........................... p 39 N61-t3958

HAWK, J. D. ....................................... p 10 N79-14996

HAYDEN, R. S. ........................ p 137 N85-32357

HAYDUK, R. J. ............................... p 127 N78-20536

p 35 N80-30296

p 133 N84-21901

p 134 N85-10377

p 135 N66-21933

p 38 N86-30721

HAYES, C. ....................................... p 6 N78-10030

HAYNES, G. A. ............................... p 103 N64-20759

HAYWOOD, W. S., JR. ................. p 38 N78-20128

PERSONAL AUTHOR INDEX

HEAD, J. W., Itl .......................... p61 N78-21174

HEAD, V. L .................................. p111 N84-17525

HEARD, W. Lo, JR. ......................... p 62 N81-26160

p 74 N83-19806

p 75 N85-19015

HEATH, O. F. .............................. p 154 N83-16992

p 165 N83-26826

HEDGLEY, D. R. ............................. p 185 N79-16679

HEDGLEY, D. R., JR .................. p 176 N82-21907

HEER, E .................................. p 184 N81-29902

p 164 N81-30889

HEFNER, J. N .................................. p 108 N80-22633

HEIDELBERG, L J. ..................... p 46 N80-21323

HEILMAN, J. L ......................... p 138 N79-16329

HEINBOCKEL, J. H ..................... p 86 N83-18895

p 90 N66-26413

HELLBAUM, R. F ........................ p 39 N81-24056

p 40 N84-12164

HELMLE, L C. .............................. p 159 N79-16493

HELMREICH, R. L. ........................ p 196 N79-16709

HEMINGWAY, J. C ....................... p 40 N82-33381

p 31 N85-14606

HENDERICKS, R.C. ...................... p 109 N81-24387

HENDERSON, H.R. ...................... p 190 N85-29694

HENDERSON, W. P, ........................ p 10 N79-t3002

p 27 N66-16193

HENDRICKS, R. C. ....................... p 107 N79-29468

p 107 N80-17398

p 109 N62-20467

p 112 N85-14078

p 112 N65-27165

HENDRICKS, W.L. ...................... p 105 N78-23390

HENIZE, K.G. .............................. p 210 N79-27057

HENNINGER, J. 14. ..................... p 82 N84-23698

HENRIKSIEN, S. W ............................... p 151 N76-11545

HENSHAW, M. ......................... p 206 N81-25012

p 207 N82-16028

HEPNER, T. E .......................... p 116 N86-16563

HEPNER, T. P ............................. p 105 N78-21410

HEPPNER, J. P........................... p 209 N81-13912

HERMAN, J.R. ........................... p 209 N79-20961

HERMANN, P. .............................. p 48 N81-20076

HERNANDEZ, G ........................ p 21 N63-27959

HERR, R. W ............................ p 127 N78-28480

p 129 N80-19563

HERRING, H. W. ............................ p 62 N81-16076

HERSHMAN, L W ............................ p 4 N83-33827

HESLIN, T. ................................. p 99 N84-33613

HESLIN, 1"- M. ............................. p 126 N86-32763

HESS, R. V. .................................. p 115 N80-30717

HEYMANN, M. ....................................... p 185 N85-33745

HEYSON, t4. It. .............................. p 5 N77-33t12

HICHO, G .......................................... p 99 N84-33613

HICKMAN, G. D. ............................. p 138 N76-21526

p 138 N78-23537

HIGDON, N. S. ................................ p118 N84-31617

HIGGINS, R. 14. ......................... p 89 N84-13263

p 90 N85-22662

HILL, C. K. ..................................... p 28 N86-21506

HILL, O. ....................................... p 67 N83-32828

HILLJE, E. R. .................................. p 74 N86-11t27

HILSENRATH, E. .................................. p 137 N85-23112

HILTON, D. A. ....................................... p 187 N79-24773

HINDSON, W. S. ......................... p 56 N61-19131

HINKLEY, E. D. ......................... p 153 N81-23742

HINTON, D. A. ............................. p 39 N82-14085

HIPPENSTEELE, S. A. ................... p 41 N77-32153

p 97 N78-20351

p 47 N81-12069

HOAD. D.R. ............................. p 105 N76-21410

p 10 N79-14019

p 167 N80-14840

HOBBS, R. W ........................................ p 206 N80-11972

HODDER, R.S. ..................................... p 119 N77-33520

HODGE, W. F. ........................... p 34 N80-17060

HOOGES, C. A. ...................... p 61 N78-21174

HODGES, D.H. ..................................... p 129 N80-20619

p 134 N85-27258

HOELL J. M. ....................................... p 155 N85-14336

HOELL J. M. JR ............................. p 192 N80-26125

p 153 N80-33998

HOFFMAN, A.C. ....................... p 52 N85-26944

HOFFMAN, C, A ............................. p 79 N84-26749

HOFFMAN, R. W ...................... p 62 N79-26076

HOFFMAN, S. .................................. p 197 N78-12895

p 16 N81-14973

p 24 N84-27674

HOHL F. ................................... p 201 N79-24921

HOLANDA, R, ........................ p 113 N78-15463

p 89 N84-18370

HOLBROOK, G. T. ..................... p 12 N79-24961

p 5 N86-16187

HOLBROW, C. ........................................ p60 N77-21106

HOLDEMAN, J. D. ...................... p 29 N79-33171

p 163 N81-21685

p 164 N82-15677

p 166 N84-31865
PERSONAL AUTHOR INDEX

HOLLAND, W. B. ....................................p 66 N82.14203 p 66 N82-15106

HOLLENBACH, D. ................................p 202 N83-27939

HOLLENBAUGH, D.D. ....................p 172 N84-20155

HOLLEY, B.B. .....................p 109 N81-31509

HOLLINOSWORTH, R. 1". .....................p 73 N82-25291

HOLLOWAY, P. F. .............................p 66 N82-14202

HOLMBERG, N.A. .......................p 71 N81-10100 p 71 N81-10101 p 71 N81-11102

HOLMES, B.J .........................................p 32 N78-18044 p 24 N84-26660 p 25 N84-33379

p25 N85-21118

HOLT, H. M. ...................................p 71 N81-10100 p 71 N81-10101 p 71 N81.11102

HOLT, W.R. .......................................p 80 N80o27428

HOMYAK,L ...................................p 45 N80-14121 p 46 N80-21323 p 47 N80-25339

HONG, C. S. ...................................p 80 N79-23140 p 81 N81-24178

HONG, tt. Y. .......................p 195 N79-19867

HONG, J. Y. ....................................p 194 N78-26927 p 194 N78-30944

HOOD, R. V. ...........................p3 N82-19134

p37 N85-33116

HOPPING, K. A. ....................................p 145 N80-11559

HOPSON, P., JR. ............................p 100 N86-20586

HORN, F. W., JR. .......................p 139 N81-21437

HORNBUCKLE, F. L. .....................p 76 N77-32229

HORNSTEIN, J. ..........................p 207 N82-25043 p 207 N82-26134

HOTZ, G. M. .................................p7 N78-14998

p7 N78-16001

p 47 N80-25338

HOUCK, J. A. ...............................p 181 N85-15446 p 181 N85-27575 p 181 N86-25168

HOUGHTON, W.M ..........................p 168 N83-24133

HOUSE, F. B. .........................................p 160 N79-22709

HOUSNER, J.M ....................................p 129 N80-19563 p 131 N82-33739

HOWARD, F.G. ...........................p 106 N78-33385

HOWARD, J.C. .......................p2 N79-23008

p 182 N80-13839

HOWARD, K. A. ............................p 61 N78-21174

HOWELL, L. ..................................p 184 N83-33631

HOWELL, L.W ...........................p 183 N83-16095 p 185 N84-15880 p 193 N84-26398 p 177 N85-23305 p 63 N86-21559

HOWELL, L. W., JR. ....................p 184 N86-19095

HOWELL W.E .............................p 57 N83-33896

HOWES, W.L ............................p 171 N79-25753 p 194 N83-13979 p 116 N83-33126 p 194 N86-22390

HOWLE, W. M. .............................p 76 N80-33463

HSU, L. .............................p 195 N79-13886

HSU,L C. ............................ p78 N79-21128

HUANG, N. E. .......................p 167 N78-21737

HUBBARD, N.J ...............................p 203 N78-12925 p 203 N78-12958

HUBER, P.W ................................... p45 N79-29192 p 47 N80-33409

HUCEK, R.R ................................p 157 N86-29425

HUCK, F. O. ..............................p 114 N80-22660 p 115 N81-33452

HUDSON, H.S. .............................p 209 N83-13048 p 209 N83-25645 p 209 N84-27635

HUDSON, R. D. ..........................p 151 N77-31694 p 161 N80-14641

HUDSON, R. M. ........................p 210 N86-24614

HUESCHEN, R. M. ........................p 39 N81-24058 p 57 N83-33896 p 40 N84-12164

HUFF, R.G ...................................p 189 N84-19049

HUFFMAN, J.K ............................p 16 N81-14974 p 21 N83-22162

HUGHES, D.L ............................p 52 N85-22394

HULL, G. A. ..........................p 136 N81-32564

HULLER, F. T. ...........................p 121 N80-15410

HUMENIK, F.M .............................p 149 N80-14581

HUMES, D. H. ...............................p 72 N81-29155

p 118 N84-17575

HUMPHRIES, T. S. ..........................p 86 N78-28226

HUMPHRIES, W. R. ........................p 104 N78-15434

HUNDLEY, N.H ..............................p 95 N84-19564 p 96 N85-26990

HUNT, J.L ..........................p 28 N86-23558

HUNT,L E. ...................................p 130 N82-20566 p 131 N83-12449

HUNT,LR ..............................p 109 N81-15237 p 109 N82-13383 p 112 N85-17322

HUNT, Ft. Lo ...............................p 108 N80-32692

HUNTEN, D.M ..........................p 205 N79-16758 p 208 N86-11137

HUNTER, W. W., JR. .......................p 116 N82-32663 p 116 N86-11437 p 118 N86-16563

HUSTON, R.J .......................................p 190 N84-29662

HWANG, S.Y .............................p 134 N85-20396

HWANG,W ...............................p 103 N84-20758

HYPES, W. D. ...........................p 145 N80-11559

HYUN, J.M ................................p 160 N79-32796

lUFF, K.W .....................................p 54 N79-22113

p 176 N81-12744 p 183 N81-27865 p 185 N85-19784

IMHOFF, M. L. ................................p 141 N83-19141

INGARD, K. U. ..................................p1 N78-25049

INGE, J.L .......................................p 206 N80-16998

IHGEBO, R. D. ..........................p 109 N81-16417

INNIS, R. C. .................................p 53 N78-26151 p 56 N81-11044 p 56 N81-19131 p 57 N82-20187

INSPEKTOR, A. .........................p 79 N84-20643

IPPOLITO,L J. ............................p 70 N81-18082

p 100 N83-29491

IRWIN, S.H .........................................p 40 N83-16338

ISE,R ....................................................p 209 N79-22991

ISHIGAKI, H. .......................p 95 N82-22366

p 122 N82-31691

ISMAIL S. ......................................p 150 N86-16748

ISOGAI, K. ............................p8 N78-21055

IVANOVSKY, A.I.................................p 161 N80-16682

IVEY, G. W., JR. .........................p 74 N84-19393

J

JACHIMOWSKI, C.J. .....................p 84 N78-23172 p 84 N79-28259 p 85 N81-14017 p 50 N83-18727 p 55 N83-19825

13 52 N85-22395

JACKSON, C. M., JR ........................p 18 N82-12035

JACKSON, J. E. ...........................p 151 N79-13601

JACKSON, K. E. .........................p 37 N84-17175 p 38 N86-13316

JACKSON, L.R ...........................p 132 N84-18675

JACOBS, P. F, .................................p8 N78-20081

p 25 N85-10920 p 27 N86-11186

JACOBS, R. E. ...................................p 50 N83-33893

JACOBSON, 13. O. .......................p 123 N83-t6759

JACOBSON, T. P. ............................p 119 N78-25433 p 88 N82-21298

JADWICK, J.J ............................p 206 N80-16009

JAGAClNSKI, R. J. ........................p 174 N86-32976

JALINK, A., JR. ..............................p 148 N79-29679

JALUFKA, N.W .............................p 118 N83-16738

JAMESON, A. ................................p 25 N85-15694

JARRETr, O., JR ............................p 139 N81-20492 p 168 N83-19411

JASPERSON, W.H .......................p 166 N84-31865

JAUDON, J. B. ...........................p 53 N78-20143

JAYROE, R. R. ...........................p 202 N85-12833 p 202 N85o12834

JEDLOVEC, G. J. .................................p 166 N85-16351

JEFFERIES, K. S. ..............................p 77 N81-20173 p 52 N85-28944

JEFFERS, E.L ............................p 198 N79-28062

JEFFRIES, W. R, III ........................p 166 N85-21878

JELLISON,J ....................................p 126 N86-26639

JEMIOLA_ J.M ...............................p 62 N79-25048

JENKINS, J. L, JR ....................................p8 N78-28056

JENKINS, R.V ..............................p 108 N81-12356 p 28 N86-24662

JENSEN, J.K ........................................p 74 N83-19806 p 75 N85-19015

JENSEN, K. A. ...............................p 95 N84-18400 p 95 N84-28989 p 96 N86-15394

JENSEN, W.S. ..............................p 144 N77-30617

JERNELLL S. ................................p 32 N78-25079

JERNIGAN, C. M. ..........................p 63 N85-11011

JESKE, J. Ao .........................p 35 N81-22039

JOHANSEN, K. J, ...................p 106 N78-30555

JOHNSEN, R. L. .............................p 41 N78-11106 p 44 N79-25022

KASCAK,A. F.

JOHNSON, C. B. ........................p 106 N79-20344 p 59 N80-19131 p 110 N83-20031 p 60 N86-24709

JOHNSON, D. L. .............................p 159 N79-14680 p 164 N83-14824

JOHNSON, E. R. .......................p 135 N86-20856

JOHNSON, G.A. .............................p 29 N79-31166

JOHNSON, G. M. ........................p t8 N81-31129

JOHNSON, J. L., JR .............................p4 N82-26217

JOHNSON, K.G ..................................p 53 N78-27138 p 56 N81-13065 p 71 N81-13082 p 74 N84-23675 p 75 N86-16250 p 75 N86-30801

JOHNSON, N.J. .......................p 83 N85-12941

JOHNSON, P. J. ............................p 28 N86-23558

JOHNSON, R. D. .........................p 60 N77-21106

JOHNSON, R. W. ..........................p 147 N78-13628

JOHNSON, S. C. ......................p 180 N84-34198

JOHNSON, S.M. ..........................p 49 N82-31329

JOHNSON, 1". V. .......................p 208 N86-11137

JOHNSON,W ..............................p 200 N80-14977 p 57 N82-20188 p 37 N84-19333

JOHNSON, W. G., JR ......................p 22 N84-13162

JOHNSON, W. S. ...........................p 82 N83-33956

JOHNSTON, J. P. ........................p 14 N80-17984

JOHNSTON, K. O. ..........................p 105 N78-23390

JOHNSTON, M.H. ...........................p 88 N83-16492

p 195 N83-21991

JOHNSTON, R. L. ..........................p 99 N83-32990

JOHNSTON, R.S. .......................p 169 N77-33780

JONES, F.C ..................................p 210 N85-33901 p 210 N85-33902 p 210 N85-34006 p 210 N85-34729 p 211 N85-34862 p 211 N85-34991 p 211 N85-35848 p 211 N85-35968 p 211 N85-36066 p 211 N86-28904 p 211 N86-3t483

JONES, J.H ...............................p 190 N85-29694

JONES, J.J. ..............................p 191 N78-20927 p 69 N84-10115 p 69 N84-10144

JONES, J.L .............................p 198 N79-10942

JONES, J. L, JR. ..........................p 67 N84-24632

JONES, K.L .............................p 206 N81-25012 p 207 N82-16028

JONES,LW ...........................p 118 N83-27200

JONES, M. G. ...............................p 191 N86-27043

JONES, R. .................................p 152 N79-19519

JONES, R.E ...........................p 51 N85-10064 p 52 N85-21168 p 52 N85-31058

JONES, R. T. ................................p 13 N80-15033

JONES, W.H ..............................p 180 N83-28921

JONES, W.R.,JR ...........................p 119 N78-2t470 p 119 N78-22377 p 92 N79-23216 p 121 N79-31605 p 93 N80-22493 p 94 N82-16239 p 88 N82-21300 p 94 N82-21332 p 95 N83-16528

JONES, W. T. ....................................p 143 N85-30450

JORDAN, S. D. ...........................p 203 N81-27008

JOSHI, S.M ...............................p 99 N81-20311

p 181 N84-28538 p 75 N86-30800

JOYCE, A. T. ..................................p 137 N78-15549 p 138 N78-21568

JUCKER, J. V. ............................p 198 N79-10942

JUHASZ, A.J ...........................p 42 N78-20131

JUNKIN, B. G. .............................p 177 N79-33858

K

KAAI_ARI, G. E. ......................p 104 N78-t6326

KAHLBAUM, W.M ..............................p 193 N78-12829

KAHLBAUM, W. M., JR. ...............p 148 N79-29679

KAHLRAUM, W. M., JR. ...................p 33 N79-33189

KAUL F. ..................................p 116 N82-29579 p 103 N86-14498

KAMARATOS,E ...........................p 210 N84-21485

KANENKO, R.S. ..........................p 135 N85-33537

KANNING, G. .............................p 31 N83-29193

KANTSIOS, A.G. .........................p 147 N78-11520

KAREGEANNES, C. E. ....................p 211 N77-16981

KASCAK, A. F. ..............................p 119 N78-10474 p 46 N80-15128

B-7
KASPER, H.J.

p 48 N62-14090

p 123 N84-17590

KASPER, H.J ................p 77 N79-23132

KATSANIS,T ................p 20 N82-29270

KATZOFF,S.............p 106 N79-10379

KAUFMAN,A ....................p 43 N79-t3046

p 129 N80-22734 p 129 N80 27719 p 130 N82-20565 p 130 N82-20566 p 131 N83-12449 p 132 N83-34372 p 133 N84-20678 p 134 N85-20396

KAUFMAN, J.W ...........p 162 N80 26999 p 162 N61-10637

KAUFMAN,L G., II .............p 106 N79-20344

KAUL R.D .................................p 100 N82-15270 p 100 N83-29491

KAVEESHWAR, V.G ............p 154 N83-16992

KAYSER, E.G ..........................p 36 N83-31596

KEAFER, L. S., JR .............p 115 N82-26637 p 116 N83-28410

KECKLER, C.R ........................p 77 N84-12228 p 78 N85-13850

KELLER, V.W ......................p 162 N80-23934 p 154 N84-14606

KELLEY, H.L...................p 27 N86-20349

KELLEY, J.S ..........................p 145 N81-27622

KELLEY, W.W .....................p 53 N78-20139

KELLY, H.N .....................p 131 N83o11513

KELLY, J.R ................................p 54 N79-29195 p 55 N80-23326 p 40 N83-36028

KELLY, W. L., IV ............................ p113 N77-32458 p 76 N80-33463 p 178 N81-25690

KENDALL, B.M .....p 168 N79-28863 p 103 N86-20678

KENDALL J.M .......................p 111 N83-34229

KENNEDY, F.E .........................p 92 N79-21205

KENNEL H.F................................p I93 N84-26398

KENT, G.S ..................................p 153 N82-12687

KERN, E,L......................p 62 N82-26330

KERNAGHAN,H ..........p 199 N79-22979

KERR, A.R ..........................................p 103 N84-20758

KERR, P.A .....................................p 74 N84-19393

# 182 N84-34204

KERSHNER, D. D. ......................p 38 N79-23081

KERSLAKE, W.R ..................p 79 N86-28123

KESKAR, O.A ...............................p9 N78-30054

p t3 N80-12995

KESSLER, D.J ............................p 63 N85-21188

KEY, K.F ...............................p 149 N80-29911

KEYES, J.w ...........................p 108 N80-26622

KEYSER, G. L, JR ...................p 38 N80.27360 p 57 N82-19225 p 30 N83-14077 p 57 N84-12190

KNOZEIMEH,K .................p 178 N77-33876

KIANG, C.S ..............p 160 N79-21720 p 160 N79-21721

KIBLER, K.$ .....................p 55 N80.14136

KIEFLING, L.A .........................p 66 N82-14203 p 66 N82-15106

KIELB, R.E ...............p 51 N84-24578

p 135 N86-10579

KIM, Y,C ........................p 194 N78-30944 p t95 N79-19867

KIMBALL, G., JR ....................p 56 N81-12109

KINARD, W.H ....................p 67 N84-24632

KINCADE, R.E ...........................p 67 N83-32828

KING, M.D ...................p 156 N86-22022

KIRSCHNER, R.P ..................p 201 NSO- 11966

KJELGAARD, S.O ..............p 20 N83-10016 p 22 N83-36000 p 26 N85-31010

KL.ASSEN, H.A ........................p6 N78-11002

KLASSEN,W ..........p 169 N79-19592

KLEIN, H.P ............................p 174 N85-29531

KLEIN,V .....................p 11 N79-20071 p 55 N80-24323 p 86 N62-10041 p 57 N83-19758

KLENK, K.F ..........................p 164 N82-28880 p 164 N82-29826 p 154 N83-16992 p 165 N83-28828

KLINE, J.F................................p8 N78-20080

p 50 N83-30431

KLINGLESMITH, D.A.p 116 N84-28020

KLOPP, W.O ......................p 87 N80-32489 p 87 N80-33555

KNIGHT, J.C .....................p 179 N82-24845

KNIGHT,K ...........................p 162 N81-15640

KNIGHT, K.S ......p 162 N8t-16678

B-8

KNIGHT, V. H., JR ................................p 38 N78-20128

KNOCKEMUS, W.W .............................p 91 N86-30837

KNOX, C,E.....................................p 96 N78 13054 p 30 N60-13020 p 39 N80 33404 p 4O N89 17535 p 31 N84-17165 p 40 N85-16868 p 40 N85-26705

KO, W.L..............................................p 129 N80-23677 p 82 N83-28099

KOCMOND, W.C ..........................p 115 N82-15383

KOENIG, D.G ......................................p 13 N80-10107

KOFSKEY, M.G .............................p5 N77-30089

p5 N77 32082

p6 N78 11008

p7 N78-14998

p7 N78-16001

p 42 N78-16053

KOHL, F.J ....................................... p111 N84-19741 p 90 N84-28958

KOHN, J.S...............................................p6 N78-12039

KONDO,Y ...........................................p 201 N82-31163 p 204 N85-15539 p 203 N85-20961

KONRADI,A ..........................................p 65 N78-15142

KOPRIVER, F., lU ..................................p 66 N81-19164 p 66 N81-19196

KORSCH,O .......................................p 193 N76 11812

KOSLIN, M.E .......................................p 114 N78.21431

KOSMAHL, H.G ................................p 101 N79.22375 p 102 N81-28352 p 102 N82-22439 p 102 N82-23397 p 102 N83-25985 p 103 N86-13643

KOSOFSKY, L.J ............................... p61 N78-21174

KOURTIDES, D.A ...............................p 29 N79-31166

KOWITZ, H,R ...............................p 101 N80-33683

KRAUSE,LN ......................................p 113 N78-15463

KRAWCZONEK, W.M ......................p 194 N78-26927 p 194 N78-30944 p 195 N79-19867

KREINDLER,E ..................................p 58 N84-32394

KREINS, E.R .............................p 159 N79-20575 p t59 N79-20633 p 163 N81-21686 p 163 N81-21693

KRIDER, E.P ....................................p 160 N79-22708

KROSEL, S,M .................................p2 N79-16796

p 179 N82-33020

KROSS, O.A ................................. p66 N82-14203 p 66 N82-15106

KRYCUK, G.A .................................... p114 N78-21431

KRYTER, K.D ................................p 174 N84-29465

KUGELMANN,O ...............................p 141 N83-1914_

KUHLTHAU, A.R ..........................p 172 N77-27710 p 199 N80-18990

KULLAS, M.C .......................................p 71 N79-27237

KULTHAU, A.R ............................p 172 N78-11705

KUMAR,A ........................................p 16 N82-11032 p 48 N82-13142

KURKOV, A.P ....................................p 51 N84-20562

KURTENBACH, F.J ....................p 43 N79-13044 p 44 N79-26057 p 48 N81-15000

KUSAKA,T ............................p 96 N85-21359

KVATERNIK, R.G ...................p6 N78 12039

p 133 N84-33832

KYLE, H.L ..........................................p 157 N86-29425

L

L&BONTE, S.J ..................................p 209 N84-27635

L.ABUS, T.L .....................................p 104 N77-30413

LADSON, C.L .......................................p 16 N61-10005

LAESSIG, M.R ......................................p 45 N79-33210

LALLMAN, F.J ....................................p 130 N81-14343 p 37 N85-23753

[AMAR, J.E ....................................p 15 N80-28304 p 17 N81-25040

LAMB,M ..................................p7 N78-13016

p 12 N79-23013 p 15 N80-27283 p 16 N81-14975 p 17 N81-29095 p 18 N81-30087 p 26 N85-29924

LAMBERT,O ...........................p 25 N85-12862

LAMBIOTFE, J. J., JR .................p 182 N78-31836

LANDRUM, E.J ...........................p 17 N81-220t6

LANE, A.G ........................p 59 N79-29199

LANGJAHR,D ............................p 115 N80-30716

LANIER, J. R., JR ...........................p 77 N81-24167

p77 N82-11109

PERSONAL AUTHOR INDEX

LARSEN, J.C ..................p 192 N82-15853

LARSEN, P.A ............................p 138 N78-18497

LARSEN, W.E ...........................p 173 N80-15821

LARSON, T.J ..............................p 38 N80-23304 p 39 N80-32389 p 39 N61-26144

LASAGNA, P.L ........................p 43 N79-13045 p 2 N80-15028

LATT,L ...........................p 149 N81-17622

LAUBACH,LL ............................p 172 N79-11734

LAURER, J.K ...................p 29 N80-22263 p 30 N81-30101 p 30 N82-13123 p 40 N82-33361 p 30 N85 18009

LAUDERDALE, W.W .................p 199 N79-22979

LAURIE, V.J ............................p 138 N78-21526 p 138 N78-23537

LAUVER, M.R ................................p 194 N78-21922

LAVIGNA, T,A .......................................p 76 N77-32229

LAWING, P.L....................................p t05 N78-23389 p 16 N81-10005 p 110 N83-20031

LAWLESS, J.G ....................................p 175 N85-32777

LEAF, C.F.......................................p 140 N82-20620

LEATHERWOOD, J.D .......................p 171 N78-11696 p 171 N78-32717 p 171 N79-22761 p 171 N79-23662 p 171 N80-13769 p 172 N83-34579 p 172 N84-20155 p 172 N84-22162

LEAVITT, L,D ..................................p8 N78-25060

p 12 N79-3316,4 p t6 N81-15976 p 19 N82-26231 p 20 N82-26235 p 21 N83 24478 p 21 N83-25666 p 23 N84-18165 p 25 N85-18951 p 27 N86-20348 p 28 N86-23560

LEE, A.T ...........................................p 30 N85-18009

LEE, B.L ....................................... p31 N78-11053

LEE,D .............................................. p42 N78-21112 p 42 N78-23095 p 165 N84-t6720

LEE, E. E., JR ...................................p 19 N82_14052 p 27 N86-20346

LEE, H.O .......................................p 30 N80-28329

LEE, J.A ..............................................p 195 N83-21991

LEE, J.H ............................................... p118 N84-17575

LEE, J.W .............................................p 118 N86-16563

LEE, K.D ..............................................p 154 N83-16992 p 165 N83-28828

LEE, L.D ........................................p 126 N85-23090 p 167 N86-24090

LEE, P.S .......................................p 164 N81-12812

LEE,Y .............................................p 118 N84-17575

LEFEBVRE, A.H .................................p 84 N77-33297

LEFFERTS,E ......................................p 62 N82-10064

LEHTINEN,B ..................................p 101 N79-14309 p 181 N84-16843

LEIDICH, C.A ......................................p 202 N84-28709 p 202 N84-32318

LEISSA, A,W .....................................p 135 N86-10579

LEITAO, C.D .........................p 167 N78-21737

LEITNER, E.F .......................................p 173 N81-17711

LENNARTSSON,W ................................p 65 N78-15t42

LEOPOLD,L..........................................p 145 N81-27622

LESLIE,F .....................................p 113 N85-28260

LEVINE,A ............................................p 196 N85-166,65

LEVINE, A,S........................................p 196 N83-18551

LEVINE, D,M ....................................p 160 N79-22708 p 161 N80-23933

LEVINE, J.S ......................................p 151 N79-10634

LEVINE, S,R ..........................................p 49 N83-10045

LEWIS, G. W., JR ........................... p43 N78-33107

LEZBERG, E.A .................................p 149 N80-14581

LIEBERT, C.H .................................p 43 N78-26148 p 43 N79-13046 p 44 N79-14098 p 44 N79-25023

p 107 N80-17397 p 48 N82-14090 p 49 N83-10045

LIEBLEIN,S .....................................p 145 N80-16453

LIGHTNER, E.B .................................p 66 N81-26166 p 67 N83-26853 p 67 N83-26879

LIKENS, W,C .......................p 142 N83-27293

LIM, R.S .................................p 177 N77-33868 p 180 N78-30862 p 180 N79-21822 p 177 N79-30947
PERSONAL AUTHOR INDEX MILLER, G. K., JR.

LIN, J.C ................................................. p112 N84-25944

UNDBERG, J.P .....................................p 69 N85-33169

LING, F.F................................................p 94 N82-16239

LINGENFELSER,G ..............................p 167 N86-25924

LISAGOR, W.B ......................................p 85 N84-t1230

UTMAN,V .............................................p 140 N82-19647

LITTLE, S.A ...........................................p 92 N76-22233

LIU, C.H ................................................p 188 N82-34189 p 5 N86-29762

LLOYD,D ..............................................p 141 N82-20623

LOATS,H ..............................................p 141 N82-20623

LOEWENTHAL, S.H ............................p 119 N78-26457 p 120 N79-13369 p 121 N79-31605 p 121 N80-17466 p 122 N8t-20423 p 122 N82-26678 p 122 N83-13457 p 123 N83-24862 p 124 N84-27041 p 125 N86-13734

LOFTIN,L K., JR ......................................p2 N60-29245

p5 N85-32089

LOLLAR,LF ..........................................p 77 N82-11109

LONG, B.H ...........................................p 159 N79-14679

LONG, E. R., JR .....................................p 80 N79-29241 p 93 N80-11226 p 83 N85-25435

LONG, L.N ............................................p 189 N84-13923

LONG, S. A.T .......................................p 170 N79-10728 p 83 N85-25435

LONGAIR, M.S .....................................p 200 N80-22130

LONGWELL" J.P...................................p 97 N78-19325

LOOMIS, W.R ........................................p 93 N80-22493 p 94 N81-21193

LOPEZ, A.E ............................................p 13 N80-10107

LORENZ, C.F.......................................p 101 N79-14309

LORENZO, C.F ......................................p 56 N60-29369

LOWELL, C.E.........................................p 86 N78-28225

LOWRY, S.A ........................................p 110 N83-16680

LU,T............................................................p5 N66-29762

LUCAS, J.G ..........................................p 187 N60-23100 p 188 N62-21036

LUCKRING, J.M .......................................p9 N78-30056

LUDWlCK,/M ......................................p 95 N84-19564

LUDWIG,LP .........................................p 46 N82-14090

LUIDENS, R.W .......................................p 42 N78-21114

LUNDOUIST, C.A ................................p 199 N79-34118

LYONS, V.J ............................................ p46 N82.13143 p 50 N83-23309 M

MILNE,D ...............................................p 169 N65-32708

MAAHS, H.G ..........................................p 84 N80-13191 p 65 N80-25392

MACBAIN, J.C .....................................p 135 N86-10579

MACELROY, R.D .................................p 175 N77-12716 p 173 N82-24836 p 174 N83-30016 p 174 N85-29531

MACK, RoJ .................................................p1 N77-32072

p8 N76-26061

p9 N78-33051

p 12 N80-10102 p 12 N80-10105 p 14 N80-21279 p 15 N81-10OO4 p 21 N83-31577

MACKALL, K.G ........................................p2 N80-15028

p 52 N85-22394

MACKIE, D.B .........................................p 32 N78-27113

MACKINNON, M.J ...............................p 187 N80-23100

MADDALON, D.V ..................................p 19 N82-20149

MADDREA, G./ JR ...........................p 150 N84-18764

MAEDA,C ...............................................p 96 N85-21359

MAGATANI,R .......................................p 165 N84-16720

MAGIDA,M .............................................p 99 N84-33613

MAGIDA, M.B ......................................p 126 N86-32763

MAINE, R.E............................................p 10 N78-33054 p 54 N79-22113

p 176 N81-12744 p 176 N81-27813 p 163 N81-27865 p 185 N85-19784

MAJOR,E..............................................p 141 N83-23660

MAJUMDAR, B.C ................................p 122 N82-25514

MALL, G.H ............................................p 117 N86-24962

MALLOVE, E.F....................................p 199 N76-21019

MALONE, T.B ........................................p 70 N86-23620

MANKE, J.A ........................................... p32 N78-20114

MANN, M.J ................................................p9 N76-30056

p 11 N79-16804 p 13 N80-16032 p 21 N83-22162 p 23 N84-18161

MANTAY, W.R .......................................p 18

MANZO, M.A ..........................................p 84

MARCUM, D. C., JR ...............................p 21

MAREK, C.J ...........................................p 50

MARK,H ................................................p 196

MARQUIS, G.A ......................................p 75

MARRIOTT, R.S ....................................p 80 p 82

MARSHALL, B.T .................................p 167

MARTIN, C.F........................................p 176

MARTIN, C.L..........................................p 77

MARTINEC,J ........................................p 14t

MARTZ, C.W ..........................................p 64

MASON, M.L.............................................p8

MASON, R.M ........................................

MASON, W,H .........................................

MASURSKY,H ........................................

_15

20

20

23

26

28

173

_17

23

D 61

) 200 ) 207

MATAENY, N.W ...................................._ 55

MATHENY, N.W ....................................3 53

MATHES, J.C ....................................... 197

197

MATTHEWS, C.G .................................._ 31

184

MATTHEWS, R.E ................................ 138

MATTOX, R.M ...................................... 178

MAURER, H.E ...................................... 139

MAYES, W.H ........................................ 190

MAYNARD, N.C ................................... 152

MAYO,LS ............................................ 142

MAYO, M.H ............................................_ 55

MAYR, H.G ........................................... 137

MAYS, C.R ............................................._ 67

MAZARIS, G. A., JR ............................._ 195

MAZEL, O. S. ..........................................._ 96

MCALISTER, K.W ....................................p7

p 23 p 25

MCARDLE, J.G ......................................p 45

p47

MCBRIDE, B.J .......................................p 51

p 182 p 52 p 52

MCCAIN, W.E ......................................p 164

MCCARTY, J.L .....................................p 32 p 29

p 130 p 132

MCCARTY, R.D .....................................p 97

MCCLELLAND, E.L .............................p 103

MCCLINTON, C.R ...............................p t05 p 42 p 45 p 48

MCCOMB, H. G., JR .............................p 178 p 128 p 129 p 130

MCCONVlLLE, J.T ..............................p 172

MCCORMICK, M.P ..............................p 153 p 153 p 153 p 154 p 154 p 155 p 155 p 155 p 155 p 155 p 156 p 156 p 157 p 157

MCCROSKEY, W.J ..................................p7

MCCULLEY,G ........................................p 46

MCCURDY, D.A ...................................p 186 p 187 p 150

p190

MCDANELS, D.L...................................p 79

MCDERMOTT,P ...................................p 144

MCDEVITT, J.B .....................................p 26

MCDONALD, W.B ...............................p 186

MCFARLAND, R.E ................................p 36

MCGARY, M.C .....................................p 188 p 189

MCGAW, M.A .........................................p 89

N82-13107

N79-22246

N83-30391

N83-32806

N85-16665

N76-17145

N80-30441

N84-26751

N86-25924

N82-29904

N81-33231

N83-23660

N80-13135

N78-26109

N80-29250

N82-32322

N83-22161

N84-24538

N85-28924

N86-23559

N82-24835

N81-22016

N84-16163

N78-21174

N81-11966

N81-25992

N80-23327

N78-20140

N82-14960

N82-15986

N82-23233

N85-16565

N78-21562

N62-11764

N80-16405

N85-30767

N79-25608

N83-26201

N80-22358

N86-29301

N84-18277

N79-13886

N85-35307

N78-17000

N84-18159

N85-12862

N80-14121

N80-25339

N85-10064

N85-19733

N85-21168

N85-31058

N82-24790

N78-13043

N80-13013

N81-24471

N83-33217

N80-14257

N84-20759

N78-22333

N78-23094

N79-29192

N81-13058

N77-33876

N79-10448

N80-32756

N82-11489

N79-11734

N82-12687

N82-13592

N82-19734

N83-27520

N83-28796

N85-19580

N85-25970

N85o27422

N86-11700

N86-13850

N86-23088

N86-27835

N86-28562

N86-29428

N78-17000

N80-15129

N79-20832

N80-13880

N82*19707

N84-32124

N84-26749

N77-16437

N85-27823

N78-23877

N82-29311

N82-31069

N83-11838

N84-17350

MCGEE, L.A ........................................p 31

MCGEHEE, J.R ......................................p 31 p 33 p 36 p 37

MCGHEE, R.J ..........................p 10

p16

pt8 p 20 p 24

MCINTURFF, R.M ................................p 158

MCIVER, D.E .............................................p1

MCKINNEY,LW ...................................p 18

p19

MCKINZIE, O. J., JR ..........................p 188

MCKISSICK, B.T ................................p 33 p 33 p 36

p37

MCLAIN, A.G ...............................p 84 p 5O p 85 p 52

MCLALLIN, K.L .....................................p 47

MCLAUGHLIN, D.K ...........................p 188

MCLEAN, F.E ....................................p4

MCMASTER, L.R .................................p 154

MCMENOMY,C ....................................p 206 p 2O7

MCMILLAN, J.O ...................................p 168

MCWITHEY, R.R ..............................p 80

p81 p 82 p 82 p 82

p 132

MEAD, J.M .........................................p 201 p 202 p 202 p 203

MEHMEO,O ............................................p 56

MEISSNER, F.T..................................p 107

MEITNER, P.L ......................................p 41 p 43 p 43 p 47 p 5O

MELNIK, R.E ..........................................p 25

MELSON, Wo E., JR ..................................p1

MELVIN, W.W ......................................p 165

MENDOZA, J.P......................................p 24

MENEGHINI,R ......................................p 161

MEREDITH, B.D .................................p 193 p 76 p 178 p 180

MEREDITH, R.W .................................p 190

MERRICK, V.K .......................................p 53

MERRILL" W.C .....................................p 98

METZ, R.N ..............................................p 74 p 75

METZGER, D.E ....................................p 48

MEYER,G ...............................................p 54 p 55 p 55

MEYER, R. R., JR ......................................p7

MEYERS, J.F ........................................p I05

p10

p 118

MEYN, E.H ..............................................p 51

MIAO,D ...................................................p 86

MICHALITSIANOS, A.G .....................) 200

MICHAUD, N.H ....................................D 33

MICHELS, C.J ...................................... 188

MICHELSON,S .......................................D 32

MICOL, J.R .......................................... 112

MIDDLETON, D.B ................................. ;_ 37

MILLER, A.J ....................................... 154

MILLER, B.A ....................................7

MILLER, C. G., III .......................... 106

112

112

MILLER, D.L........................................._ 39

MILLER, D.R ..................................... 144

MILLER, D.S....................................3 t2

317 3 22

22

3 23

23

3 24

26

MILLER, E.F ...................................._ 69

MILLER, G. K., JR ..........................._ 32

32

55

34

N83-18704

N78-10049

N80-13025

N82_31321

N84-32378

N79-14018

N8t-12015

N82-11033

N83-16290

N84-27675

N78-18630

N79-15898

N81-31130

N82-25196

N82-24942

N80-11069

N80-13024

N83-18715

N84-18189

N79-28259

N83-18727

N83-19825

N85-22395

N80-33410

N82-34189

N85-28912

NB4-32952

N81-25012

N82-16028

N82-16683

N78-20256

N81-16130

N83-28098

N83-28099

N83-28100

N84-13614

N82-31163

N84-26519

N84-26520

N85-20961

N80-29369

N79-30518

N77-32153

N78-28099

N78-31109

N81-11036

N83-32607

N65-15694

N78-25046

N83-25265

N84-28750

N80-23933

N78-2094B

N80-33463

N81-25690

N86-27947

N85-11789 N 78-16063

N78-22257

N84-16247

N85-14658

N81-24063

N79-17872

N60-17061

N80-19126

N78-17997

N78-21410

N79-14019

N86-16563

N84-24578

N78-30205

N85-17755

N79-33191

NB2-21036

N78-27113

N85-16065

N85-33116

N83-16992

N78-17998

N79-14327

N85-12313

N85-16065

N80-28349

N7B-19616

N79-23013

N81-22016

N83-32776

N83-34905

N84-18163

N84-20486

N84 27676

N65-29921

N78-28159

N78-30089

N78-30090

N79-33218

N80 21317

B-9
MILLER, I. M.

MILLER, I.M ..............p 84 N79-t4177 p 84 N80-13191 p 85 N80-25392

MILLER,J ...................p 165 N84-16720

MILLER, J.B ..................p 201 N79-24921 p 101 N81-22281

MILLER, N.J ............................p 137 N86-29301

MILLER, R.A. .................p 174 N86-32976

MILLER, T.L ..............................p 112 N84-23852 p 112 N85-13175 p 167 N86-24082 p 96 N86-29040

MILLS, C.T. .............p 132 N84-18675

MINOTT, P.O ................................p 69 N78-10200

p 117 N76-16354

MINZNER, R. A. ........p 157 N77-10755

MIQUEL,J ..............p 170 N83-16018

MISERENTINO, R.p 131 N83-16785

MISHINA, H. ...........................p 96 N84-33590 p 96 N85-13044

MITCHELL, A.M ....................p 126 N86-24992

MITCHELL, C.M ....................p 173 N83-18238

MIT_rLEMAN, D, .......................p 203 N81-11970

MIXON, R. W. .................p 171 N81-23791 p 174 N86-26836

MIXSON, ,.LS ...............p 186 N79-13821 p 191 N86-24393

MWOSHI, K. ...........................p 91 N77-32312 p 91 N77-33350 p 91 N78-10295 p 91 N78-21294 p 92 N78-21295 p 92 N78-28247 p 92 N78-30238

p t20 N79-10425 p 120 N79-14387 p 120 N79-17227 p 93 N79-30380 p 87 N80-15234 p 93 N8C-18178 p 93 N80-22494 p 94 N61-14079 p 94 N81-19300 p 94 N81-27282 p 94 N81-33293 p 94 N82-19374 p 88 N82-20291 p 94 N82-20316 p 88 N82-21301 p 88 N82-22349 p 122 N82-31691 p 95 N82-32491 p 88 N83-21110 p 88 N83-23419 p 89 N83-34019 p 95 N84-16334 p 95 N84-18399 p 89 N84-21716 p 89 N84-21721 p 96 N85-21359

MOCK, W., JR ...............p 80 N80-27428

MOE, K.L. ......................................p 173 N83-16238 p 7O N86-23620

MOEN, G.C .............................p 38 N80-27360 p 30 N81-29109 p 40 N83-18723

MOERDER, D. D. ..................................p 58 N85-28949

MOFFI1-L T. P. ..................................p8 N78-20080

p 46 N80-25337 p 47 N80-25338 p 48 N81-16050 p 49 N83-17547 p 50 N83-36431

MOHAN,H ....................................p 199 N79.22980

MOIK, J. G. ............................p 139 N81-20489

MOLLOY, J.K ...................................p4 N82-31294

MONAGHAN, R.C.p8 N78-23056

MONFORD,L G. .........................p 145 N81-18493

MONTA, W.J ....p6 N78-12041

p7 N78-16000

p8 N78-22028

p 18 N82-12035

MONTANO, J.W ......p 68 N86-30753

MONTEGANI, F.J .......................p 186 N79-17659

MONTGOMERY, H. E.p 166 N86-13867

MONTGOMERY, R.C ................p 184 N81-12812 p 56 N84-28801 p 75 N85-31142

MONTGOMERY, 1".O .......p 54 N79-22113

MONTOYA, R.J. ....................p 57 N83-33896

MOORE, A.S. .............p 45 N80-14121 p 47 N80-25339

MOORE, B., III ............p 173 N82-24836 p 174 N83-30016

MOORE, O.G ..........p 138 N79-16329

MOORE, M.C ..................p 182 N83-25438 p 181 N84-28539

B-10

MOORE, R. D. .....................p 43 N78-33107 p 43 N76-33108 p 10 N79-10022 p 43 N79-10060 p 45 N79-31213 p 45 N79-31214 p 46 N80-21325 p 4g N82-19222 p 49 N82-22269 p 49 N82-33389 p 60 N86-28101

MOOREHEAO, T.W .............................p 201 N86-13239

MORALES,W ....................................p 94 N82-21332 p 95 N83-16528 p 95 N84-23764

MORAVEC, G. F. .................................p 140 N82-20620

MOREA, S. F. ...........................p 76 N85-26862

MORELLI, J. P. .....................p 34 N80-25318

MORELLO, S. A. ........................p 38 N78-13054

MORGAN, H. L., JR ....................p 19 N82-15015 p 21 N83-30390 p 26 N85-31010

MORRIS, C. E. K., JR ...................p 35 N82-11050

MORRIS, D. J. ...........................p6 N78-11007

p 25 N84-33379

MORRIS, O.A. ...............................p 17 N81-29098

MORRIS, R. E. ............................p 5t N64-24578

MORRIS, W.D ........................p 140 N82-13468 p 150 N82-21774

MORRISETTE, E.L ......................p 105 N78-30554

MORRISON, D. ....................................p 205 N78-29007 p 205 N79-16758 p 206 N81-10910 p 207 N82.26152

MORRISON, P. .........................p 175 N78-16771 p 175 N85-32777

MORROW, G.W .......................p 103 N84-33668 p 103 N85-31371

MORT, K.W ......................p 14 N80-17984 p 59 N83-17560

MOSES, P. L. .......................p 135 N85-33537

MOSIER, F.L ...........................p 63 N86-27297

MOSS, J. E., JR. .....................................p 41 N77-32154

MOSS, J.N. ..............................p 1t3 N86-14530

MOTLEY, W. R., Ill ............p 103 N84-20759

MOUL, T.M ...............................p 35 N82-16068

MOYER, D.w ............................p 119 N78-28457

MOYER, V. .........................................p 162 N81-15640

MROZ, T. S. ...........................................p 75 N78-17145

MUELLER, A.W .................p 187 N79-24773 p 188 N81-33945 p 189 N84-22363

MUENGER, E. A. ...................p 213 N86-16185

MUGNAL A. ...............................p 194 N86-17140

MUKHOPADHYAY, V. ........................p 181 N81-30851

MULARZ, E.J. ........................................p 43 N78-27130

MUMMA, M. J. .............................p 207 N82-25043 p 207 N82-26134

MUNAVALLI, S. ...........................p 85 N82-22330

MURAKAMI, M. ....................................p 65 N78-21193

MURAMOTO, K.K ........................p 112 N85-20270

MURCRAY, O.G .........................p 152 N80-27866

MURPHY, P.C. ...........................p 56 N82-10041 p 57 N83-11139 p 58 N84-25717 p 58 N86-22579

MURPHY, R. D. .......................................p 59 N79-29199

MURRI, D. G. ................................ p3 N82-11013 p 57 N84-17184

MURROW, H. N. ........................p 164 N82-24790

MURTHY, A.V ............................p 110 N83-20031

MURTHY, M. V. V. .......................p 130 N82-11488

MURTHY, P.L N. ............................p 63 N86-216t4

MURTY, S. S.R .......................... p152 N79-13607

MUSEN, P. ...............................p 151 N78-21691

MYERS,LP ..........................p 52 N85-22394

MYERS, M.K ..........................p t86 N78-23877

MYRICK, D. L. ........................p 143 N85-30450

N

NACHTtGALL, A.J ................p 43 N79-13046

NAOER, B.A. ..................................p 67 N83-32828

NAGARAJ, H. S. .......................p 119 N78.22377

NAGARAJA, K. S. .................p 13 N80-10107

NAGATANI, R. M. ..........................p 154 N83-16992

NAGY, A. ...........................p 120 N79-31604

NAHM, A. H. ............................p 122 N83-13457

NAISH, J.M .................................p 38 N79-33201 p 39 N80-28349

NALLASAMY, M. .................................p 112 N85-25757

NASTROM, G.D ................................p 163 N81-21685 p 164 N82-15677 p 166 N84-31865

NASVYTIS, A.L ........................p 120 N79-13369

PERSONALAUTHOR INDEX

NAUMANN, E. C. .............................p 65 N79-10078 p 66 N79-10097

NAUMANN, R.J .................................... p62 N81-16075 p 62 N81-19t44

NCHE, P. ..............................p 144 N77-16437

NEALY, J.E ..............................p 136 N79-22580

NEELY, W. R., JR ................................... p58 N85-11002 p 58 N85-34144

NEINER, G. H. .............................. p45 N79-28176

NELSON, J. B. ............................p 83 N85-12094

NELSON, R.W ......................................p 144 N78-23571

NEMETH, M. P. ........................p 135 N86-20856

NEMETH, 7- N. ..............................p 118 N77-31502 p 120 N79-22518

NEUBAUER, M.J. ........................... p32 N78-27111

NEUBAUER, M. J., JR .......................p4 N82-31294

NEUGEBAUER, M. ...........................p 206 N80-11972 p 209 N84-13067

NEUMAN, F. .....................................p2 N80-19022

p 58 N84-32394

NEUMANN, tt. E. ..........................p 52 N85-25261

NEWELL It. E. ......................................p 200 N81-20962

NEWELL, R.E .........................p 154 N82-32915

NEWKIRK, R.W ..................................... p61 N78-25115 p 98 N80-20437

NEWMAN, J. C., JR. ............................p 129 N80-13512

NEWMAN, P. ..................................p 141 N82-20623

NEWMAN, P.A. .....................................p 24 N84-33377 p 25 N85-12011

NEWSOM, J.R .........................p 129 N80-22737 p 181 N81-30851 p 131 N82-26703 p 179 N84-27461

NEWSOM, W. A., JR ........................p 14 N80-22266 p 4 N82-26217

NEWSON, J.R ........................p 128 N79-28614

NGUYEN, L.T ................................. p32 N78-27111 p 55 N80-14136 p 2 N80-29244 p 57 N84-17184

NICHOLAS, J. .............................p 140 N82-19647

NICROLS-BOHLIN, J. ..........................p 204 N86-25307

NICHOLS, C. E,, JR. ......................p 116 N86-11437 p 118 N86-16563

NICKS, O.W ........................................... p63 N85-33126

NICOGOSSlAN, A.E ....................p 170 N77-30735 p 170 N83-25349

NIESSEN, F.R. .......................................p 54 N79-29195 p 55 N80-23326

NIKLAUS, K. ................................p 169 N85-32708

NlSSlM, E. .............................p 127 N78-18459

NOLA, F.J .........................................p 146 N82-32869

NOONAN, K.W ............................p 10 N79-14018 p 11 N79-22037 p 15 N80-32333 p 21 N83-30389 p 24 N84-27694 p 24 N84-28743

NOOR, A. K. ................................p 129 N80-32756 p 130 N82-11489 p 131 N82-33739 p 110 N83-20032 p 82 N83-33957 p 111 N84-22907 p 133 N84-34773 p 134 N85-10377

NORBURY, J.W ........................p 192 N84-22396 p 193 N85-17690 p 193 N86-21297 p 211 N86-21492 p 193 N86-23388 p 193 N86-30485

NORGREN, C.T. ............................p 43 N78-27130 p 49 N82-15040

NORTHAM, A.M ................................p1 N78-25048

NORTHAM, G. B. ...........................p 152 N79-17388

NORUM, T. D. .............................p 186 N79-14872 p 189 N84-25422

NOTA-DONATO, J. J. ........................p 77 N79-23132

NOWAK, R.J ........................................ p131 N83-11513 p 112 N85-17322

NUGENT, J. ...................................p 21 N83-25665

NUSBAUM, W. J. .........................p 42 N78-16053

NUTH, J. A., Ill .........................p 201 N86-23493

NYLAND, T. W. ........................p 148 N79-18479

NYSTROM, P.A ..........................p 187 N80-27161 p 189 N84-10913

0

OAS, S. C. .................................p 43 N79-13045

ORARA, C.J .................................p 24 N84-26660 p 25 N85-21118

OBERHOLTZER, J.D. .........................p 139 N80-16405

OBRIEN, P.J ......................................p 30 N85-32101
PERSONAL AUTHOR INDEX RAJU, S.

OBRYAN, T. C. .............................p 55 N80-22358

OCAMPO, A. C. ...........................p 207 N84-32330

OGBURN, M. E. .............................p 55 N80-14136 p 2 N80-29244

OGELMAN, H. ...............................p 201 N77-34063

OHLHORST, C.W ......................p 147 N78-33617

OHRING,G ..............................p 167 N86-28574

OKUNO, A. F. .....................................p 26 N85-27823

OLEARY, B. .................................p 62 N79-32225

OLSEN, G.C. ..............................p 81 N61-14001 p 81 N82-22317

OLSON, S. I- ...............................p 85 N85-31244

ONCLEY, P. B. .............................p 186 N78-17623

OPPENHEIM, A.K .....................p 50 N83-32806

ORAN, W. A. ............................p 61 N79-13069 p 62 N79-26076

ORANGE, T.W ..........................p 129 N80-15428 p 129 N81-11417

ORDIN, P. M. ................................p 97 N80-21551

ORMISTON, R. A. .....................p 129 N80-20619

OSBORN, M. T. ......................p 155 N85-19550 p 155 N86-13850 p 156 N86-27835

OSBORN, R.F. ...........................p 28 N86-27190

OSBORN, W.M ......................................p 43 N78-33107 p 10 N79-10022 p 45 N79-31213 p 45 N79-33210

OSMK,N ................................................p 165 N83-28828 p 165 N84-16720

OSTROFF, A.J. ......................p 39 N81-24058 p 57 N82-24209 p 57 N63-33896 p 40 N84-12164 p 58 N85-23801

OSWALD, F. B. ....................................p 126 N86-24992

oI-rERSON, D.A. .................p 149 N80-14581 p 97 N84-23774 p 98 N85-31307

OUTLAW, R. A, .......................p 99 N82-19390 p 86 N83-18895

p 100 N86-20586 p 90 N86-26413

OWEN, A.K ..........................p 20 N83-11058

OWEN, F.K ...................................p 108 N81-13303

OWEN, R, S. ........................................p 117 N79-22455 p 88 N83-16492

P

PADIAN, K. ............................................p 169 N85-32708

PAGE, V. R. .............................p 185 N77-30909 p 14 N80-17984

PALMER, R.W .........................p 103 N86-13643

PALUDAN, T. ..........................p 138 N79-13475

PAN, Y.S. ..............................................p 105 N78-22333

PANEl(, R.J .................................p 204 N86-25307

PAO, S.P. ..................................p 186 N78-t7823 p 187 N79-22849

PAPADOPOULOS, K. .................p 200 N84-34332

PAPELL, S. S. .............................. p45 N80-11087 p 109 N81o29384 p 110 N83-12360 p 111 N83-34232 p 112 N85-12314

PAPPA, R. S. ..............................p 131 N83-16785

PAPROTNY, Z. ........................p 199 N78-21019

PARDUE, M. D. .............................p 54 N79-15970

PARK, A. C. ................................ p70 N78-25123 p 70 N78-25124

PARK, H. ...............................p 165 N83-28828

PARK, J. 14. ...............................p 192 N82-15853

PARK, J. J. ..............................................p 80 N80-30441 p 82 N84-26751

PARK, S. K. ......................p 114 N80-22660 p 115 N81-33452

PARKER, J. F., JR .....................p 170 N83-25349

PARKER, L.C. ....................................p1 N78-25048

PARKER, R. A.R .....................p 201 N80-11966

PARKER, R. J. ......................p 119 N77-33520 p 119 N78-21470 p 119 N78-2t473 p 120 N79-14389 p 121 N80-29734 p 122 N83-13457 p 122 N83-16758 p 123 N83-33166 p 123 N84-18654

PARKINSON, C.L. ..........................p 168 N84-10718

PARR, R.A ............................p 195 N83-21991

PARRA, C.G .........................................p 167 N78-21737

PARRIS, B. L. ............................p 32 N79-14082 p 34 N80-15069

PARRISH, R.V. ....p 33 N79-33189 p 33 N80-10193 p 33 N80-11069

p 33 N80-13024 p 36 N83-18715 p 36 N83-22191 p 36 N83-22192 p 37 N84-18189

PARROTT, T.L ..........................p 191 N86-16040 p 191 N86-27043

PARSLEY, P. D. ............................p3 N82-21139

PARSONS, C. L. ........................p 158 N78-27706 p 161 N80-16676

PARSONS, S. B. ........................p 210 N79-27057

PATTERSON, D.J ....................... 1397 N83-22442

PATTERSON, J. C., JR ..............p 26 N85-26667

1326 N85-29924

1327 N86-20345

PATTERSON, W. J. .....................p 94 N81o31365 p 95 N84-19564 p 96 N85-26990

PATTON, J. M., JR. ......................p 12 N79-23012 p 37 N85-25248

PAULSON, J. W., JR. .....................p6 N78-13014

p 13 N80-12994 p 19 N82-15015 p 20 N83-10016 p 22 N84-13163 p 23 N84-18164

PEACOCK, C. L., JR ....................p 92 N78-22233

PEELE, E.L .............................p 179 N84 27461

PELLETT, G.L ............................p 84 N78-22188

p 149 N81-24601 p 149 N82-14672 p 150 N83q2595

PELMGRA, R. ............................p 212 N79-15887

PEMBERTON, D.A. ....................p 138 N78-21526 p 138 N78-23537

PENARANDA, F. E. .........................p 60 N85-18991 p 60 N86-18328

PENDERGRAFT, O. C., JR ..............p 13 N80-11036 p 20 N82-32320 p 22 N84-13165 p 24 N84-32354 p 27 N86-20346

PENLAND, J. A. ..................................p9 N78-31045

p I3 N80-12064 p 21 N83-30391 p 27 N85-33107

PEPPER, S. V. ..................................p 98 N77-30296

PERKINS, P.J. ..................p 148 N78-33618

PERRY, B, III ............................p 131 N82-26703

PERRY, E. ..............................................p 100 N77-30367

PERSON, L. H, JR. ........................p 38 N80-27360

p 172 N82-14804

PESLEN, C.A ........................p 166 N85-14360

PETERS, D.A. ..........................p 129 N80-20619

PETERSON, J. B., JR ....................p 13 N80-16032 p 14 N80-17986 p 24 N84-33377

PETERSON, R. ..............................p 139 N60-25742

PETITT, J. C. ............................p 171 N80-34099

PETLEY, D. H. ............................p 74 N83-31713 p 74 N84-19393 p 26 N85-23707

PETOT, D. .....................................p 25 N85-12862

PETUCHOWSKI, S.J .....................p 76 N85-30005

PHELPS, A. E., I11 ..........................p 26 N85-28923

PHILIPP, W. H. .................................p 78 N79-21128

PHILLIPS, J. D. ......................................p 25 N85-15693

PHILLIPS, P. S. .................................p 23 N84-17127

PHILLIPS, W. H. ..........................p 32 N78-20115 p 54 N78-30141 p 36 N82-32350

PHILLIPS, W. P. ..........................p 67 N65-19003

PIERSON, W.J. .........................p 136 N79-17279

PINEL, S.I .................................p 12t N80-21753 p 121 N80-29734 p 121 N80-33749 p 124 N85-13233

PINELLI, 1". E. ...........................p 197 N82-14960 p 197 N82-I5986

PINES, S. .................................................p 57 N82-24209

PINSON, L. D. ...........................p 66 N83q8819

PITTMAN, B. .......................................p 202 N84-28709

PITTMAN, C. M. ...................................p 91 N78-12223 p 80 N79-23141

PITTMAN, J. L. .......................................p6 N78-12038

p9 N78-30055

p 13 N80-12065 p 16 N81-12021 p 23 N8.4 18163 p 27 N85-33107

PITTMAN, R. B. ........................p 202 N84 32318

PITTS, F.L ....................p 167 N86-24090

PITTS, J. A. ...........................p 170 N68-21097

PLANT, T. J. ...............................p 21 N83-25665

PLEASANT, L. G. .......................p 79 N83-24556

PLENCNER, R. M. .........................p 52 N85 28944

PLENTOVICH, E.B ................................p 27 p 27

PLUMER, J.A. .........................p 29

PODWYSOCKI, M.H ........p 136

POE, (3. C., JR ....................p 79

p81 p 83

POHL, H.O ..........................p 99

POLKOWSKI, G. .......................p 199 p 148

POLLACK, F.G ...........................p 114

POLLACK, J. B. ....................... 13 161

POLVANLR .....................p 99

POMEROY, J.H ...........................p 203 p 203

POPPOFF, I.G ............................p 159 p 161 p 149

PORTER,F ..................................p 166

PORTER, R. L.. ........................................p 68

POSTA, S.J. ....................p 51

POTTER, A.E ...................p 149

POVINELLI, L. A, ..........................p 111

POWELL, C. A. ..................................p 186 p 148 p 148 p 148 p 149 p 149 p 187 p 149 p t50 p 150 p 190

POWELL, J.A. ..................p 115

POWELL, R.W ............................. 70

7O

71

71

58

69

POWERS, El. G. ........................... 52

53

POWERS, E.J. .................................._ 194 , 194

_195

POWERS, L.B .................... 77

PRABHAKARAN,R ........................., 132

PRAHL, J.M .........................3 125

PRATT, D. I". ............................3 183

PREISSER, J.S. ...........................3 186 3 188 3 188 3 189

.191

PRESLEY,L L. .................... 10

PRICE, D. B. ...................... 58

PRICE, R. G., JR. .................... 77

PRICE, T. A. ........................................3 173

PROK, G. M. ........................................... 97

PROUTY, C. R. ......................... 63

PRUST, H. W, JR ............................... 42

42

PURVIS,C K. ............................p 70

74

PUSTER, R. L. .................. 59

116

117

PUTNAM, L.E ........................................ 14

15

28

PUTNAM, T.W ...............p2

Q

N86-20347

N86-20351

N78-11024

N78-33499

N78-18135

N81-11115

N85-11136

N83-32990

N77-33003

N79-30644

N80-25635

N80-15726

N84-33613

N78-12925

N7_ 12958

N78-30774

NC0-15726

N81-17622

N64-34829

N86-20460

N84-24578

N80-15649

N84-17525

N79-20832

N79-28796

N79-32743

N79-32744

N80-28946

N80-29911

N81-21873

N82-12654

N82 19707

N83-1695t

N84-32124

N82-19521

N77-33259

N78-13119

N80-29417

N80-32429

N84-23652

N85-15778

N78-12100

N78-18076

N78-26927

N78-30944

N79 19867

N81-33231

N84-18675

N85-32330

N86-28662

N79-t98t3

N81-24854

N81-33945

N84-21277

N86-16041

N79-12013

N85-26949

N81-20176

N81-13635

N81-24283

N84-27758

N78-20130

N78-20133

N79-15149

N84-33452

N79.18877

N84-11460

N86-20753

N80-22262

N80-29250

N86-23562

N80-15028

QUEIJO, M.J ............................p9 N78-30054

p 13 N80-12995

QUINN, R. D. .......................................p t08 N81-12361

QUINTO, P.F...........p 22 N84-13163 p 23 N84-18164

R

RADHAKRISHNAN,K ............p 51 N8_10065

p 183 N86-28662

RADOSEVlCH, J. D. ..........p 198 N8_21403 p 198 N8_33266

RAGHAVAN, M. ..........p 127 N78 30610

RAJAN,N ............p 185 N85-33745

RAJU, S.B .........................................p 80 N79-32277

RAJU, I.S. .............p 129 N80 13512 p 130 N81 13373 p 81 N81-24178

RAJU, S. .....................p 118 N83 32044

B-11
RAMINS, P. PERSONAL AUTHOR INDEX

RAMINS,P.............................................p 101 N79-17139 p 101 N79-22375 p 101 N79-2S420 p 101 N80-21669 p 102 N81-28352 p 102 N81-30360 p 102 N63-25985 p 102 N84-15394 p 103 N86-13643 p 103 N86-32629

RANDLE, R.J .......................................p 171 N80-34099

RANDLE, R. J, JR ...............................p 173 N80-15821

RANGO,A ............................................p 139 N80-25742 p 139 N81-19511 p t40 N82-206t7 p 141 N82-20624 p 141 N83-23660

RAO, B. C.S ........................................p 123 N83-35400 p 124 N84-32825

RAO, M. S.V .......................................p 157 N77-19709

RAO, P.V ................................................p 68 N83-15413 p 89 N83-24641 p 95 N83-24695 p 90 N84-31349

RAOUET, C.A .....................................p 149 N80-27832

RAUP,D .................................................p 169 N85-32708

RAY, E.J ............................................... p110 N83-2003t

RE, R.J ...................................................p 53 N78-27136 p 12 N79-26022 p 15 N80-29250 p 16 N81-14972 p 19 N82-20156 p 20 N82-26235 p 23 N84-18165 p 28 N86-23560

REA, S.W .............................................. p115 N82-15383

REAGON, P.G ........................................p 42 N76-23093

REARDON,LF......................................p 34 N80-15068

REDD,LT .................................................p2 N80-11028

REDIESS, H.A ...........................................p1 N79-15898

REDIN, P.C .............................................p 35 N81-24048

REED, E.I ..............................................p 161 N80-14641 p 161 N80-22924

REED, E.L ............................................p 136 N79-23461

REHDER, J.J ..........................................p 65 N78-10166 p 65 N76-13109

p 177 N85-31839

REID,L.....................................................p 43 N78-33108 p 43 N79-10060 p 45 N79-31214 p 46 N80-21325 p 46 N82-19222 p 49 N82-22269

REIGEL, C.A ........................................p 149 N81-17622

REMSBERG, E.E.................................p 152 N79-17388 p 149 N81-22567 p 167 N86-25924

RENGSTORFF, G. W.P ........................p 88 N82-20291 p 89 N84-21716 p 89 N84-21721

REUBUSH, D.E ......................................p 12 N79-29146 p 21 N83-26821 p 22 N84-10025

p 118 N86-16563

REYNOLDS,R ........................................p 67 N83-32828

RHEINFURTH,M ....................................p 81 N83-16400

RHEINFURTH, M.H .............................p 183 N83-16095 p 67 N83-32626 p 68 N85-34148

RHODES, D.B ......................................p 114 N80-24594

RHODES, E.L .....................................p t36 N79-20424

RHOUK, H.E ..........................................g 19 N82-14051

RHYNE, R.H .........................................p 164 N82-24790

RICGITIELLO, S.R ................................p 29 N80-13013

RICE, E.J ................................................p 46 N80-21323

RICE, W.J .............................................p 100 N78-1t301 p 101 N81-11315 p 102 N64-16461

RICHARD, R.R .....................................p 114 N80-12399

RICHARDSON, D.J .............................p 192 N82-15853

RICHARDSON, M.O ............................p 100 N79-14275

RICHTER, C.W ....................................p 75 N78-17145

RICKETTS, R.H .....................................p 34 N80-29287

RICKS, G.W .......................................p 67 N83-32828

RtDDLEBAUGH, S.M ...........................p 43 N78-27130 p 49 N62-15040

RIEBE, G.D ................................................p5 N77-33112

p 16 N81-12021

1:) t7 N81-29098 p 22 N84-13164

RIEGEL, C.A .......................................p 166 N77-32689

RILEY, D.R .............................................p 32 N76-30089 p 32 N78-30090 p 34 N80-21317

RIND,E ..................................................p 114 N80-13430 p 115 N81-25352

RINSLAND, C.P ...................................p 192 N82-15853

RITCHIE, E.H .......................................p 212 N81-16973 p 212 N84-25602 p 213 N86-31524

ROBERTS, E., JR .................................p 114 N80-25635

ROBERTS, G.O ...................................p 112 N84-23852 p 113 N66-23651

ROmERTS, J.C .......................................p 94 N82-16239

ROBERTS, W.B .....................................p 47 N80-28352

ROBERTS, W.E .....................................p 76 N78-t3124

ROBERTS, W.T ...................................p 212 N61-14944 p 76 N86-19349

ROBERTI'_N, J.B .................................p 39 N81-13958

ROBINS, A.W .........................................p 12 N79-23013 p 14 N60-21279 p 19 N82-26232

ROBINSON, D.M .................................p 194 N61-13739

ROBINSON, J.C ...................................p 127 N78-284S2 p 110 N62-31646

ROBLES,A ............................................p 206 N81-25012 p 207 N82-16028

RODER, N.M ........................................p 110 N83-24800

RODRIGUEZ, G.E ..................................p 77 N84-12228

RODRIGUEZ, J.R .................................. p42 N78-21112 p 42 N78-23095

ROELKE, R.J .........................................p 48 N81-20076

ROGERS, C.R ......................................p 115 N82-15363

ROGERS, J. L, JR ...............................p 178 N78-33791

ROGERS, R.C ........................................p 85 N81-27223 p 50 N83-18727 p 52 N85-22395

ROGERS, T.G ......................................p 154 N63-16992

ROGOWSKI, R.S ...................................p 85 N82-22330

ROHN, D.A .............................................p 86 N78-21269

p 122 N81-20423 p 122 N82-26678 p 123 N83-24862

ROLAND,A ................................................p4 N85-23683

p4 N85-23664

p 212 N65-35142

ROSCOE, S.N ......................................p 171 N80-34099

ROSENBAUM,D ...................................p 107 N60-15361

ROSENSTEEL, F.J ..............................p 147 N76-11520

ROSENTHAL, I .......................................p 79 N84-20643

ROSNER, D.E ......................................p 111 N84-19741

ROTH, J.R ............................................p 194 N78-26927 p 194 N76-30944 p 195 N76-16867

ROTHMAN,LS ...................................p 192 N62-15853

ROTHSCHILD,R ..................................p 201 N77-34063

ROUSSOS, L.A. ...................................p 190 N85-22109 p 191 N66-24363

ROUX, S.J ............................................p 166 N84-11720

ROWE, A.P.............................................p 86 N78-28225

ROWE, H,E .............................................p 69 N78-10200

p 117 N78-16354

ROWELL, L.F .........................................p 71 N60-32429

ROWLAND, C.W .................................p 117 N82-12431

ROYSTER, D.M ......................................p 80 N78-20256 p 81 N81-16130 p 88 N83-19889 p 82 N83-28098 p 82 N83-2S099 p 82 N83-28100 p 69 N83-35100 p 90 N86-13406

RUBES|N, M.W ....................................p 107 N80-20527

RUF, J.H ................................................. p63 N86-21559

RUGGERI, R.S..........................................p9 N78-30057

RUHUN, C.L .........................................p 34 N80-25321

RUNYAN, H./ .......................................p 27 N86-t6269

RUSSELL, J. M., I1! ..............................p 167 N86-25624

RUSSELL, L.M .......................................p 76 N78-13124

p42 N78-21113 p 44 N79-27142

p 110 N82-30496

RUSTA, D.W .........................................p 77 N80-16095

RUTKOWSKI, M.J .................................p 36 N83-18714

RYAN, R.S ..............................................p 66 N82-14203 p 66 N82-15106 p 68 N86-11215

S

SAKAMOTO, G.M ..................................p 54 N79-13056

SALAS, M.D ...........................................p 25 N85-12864 p 25 N85-15694 p 28 N86-20352

SALIK,J ...................................................p 87 N60-16141 p 87 N61-16210 p 90 N84-28965

SAL_, V.V ...........................p 152 N79-16473

SALTSMAN, J.F....................................p 90 N86-12295

SAI.ZMAN, J.A ....................................p 149 N80-27832

SAMZ,J ..............................................p 206 N81-109t0

SANDERCOCK, D.M .............................p 47 N80-28352

SANDERS, B.W .....................................p 45 N80-14123 p 46 N80-14124

SANDIER,H .........................................p 170 N79-13686

SANGER, N.L ........................................p 45 N79-28177

SANGIORGIO,G ..................................p7 N78-16000

p8 N78-22028

p 11 N79-17608

SANTORO, G.J ....................................p 111 N64-19741

SARMA, G.R ...................................p 39 N81-33203

SATRAN, D.R ...........................................p4 N62-26217

p 26 N85-23708

SATYANARAYANA,B ..............................p7 N78-17999

SAUER, R.L .......................................p 174 N65-24733

SAUNDERS, R.S .............................p 200 N85-16888

SAVAGE, B.D ....................................p 204 N85-15539

SAWYER, J.W ....................................p 128 N79-31626 p 132 N83-33216 p 111 N84-10504 p 133 N84-26053

SAWYER, W.C ....................................... pll N79-17808 p 13 N80-13001 p 13 N80-16032 p 17 N81-29095

SCALLION, W.I ....................................p 67 N85-19003

SCANLON,C ...........................................p 31 N84-17165

SCHAFER,C .........................................p 113 N85-28260

SCHAFER, C.F .....................................p 110 N83-16674 p 110 N83-16680

SCHAIRER, EoT .....................................p 22 N83-34906

SCHATZ, J. G., JR ...............................p 114 N78-21431

SCHEFTER, J.L ..................................p 146 N62-28783

SCHEHL, T.A ......................................... p85 N80-16118

SCHEIMAN,J .........................................p 19 N62-t4055

SCHEIN, D.Bp 191 N86-16040

SCHEXNAYDER, C. J., JR ..................p 105 N78-20463 p 45 N79-29192 p 85 N81-27223

SCHIESS, J.R .......................................p 31 N82-23233

p 182 N64-34204 p 184 N65-16565 p 183 N86-18060

SCHtFF, L.B ...........................................p 17 N81-22016

SCHtFFER, R.A ...................................p 166 N86-13866

SCHIFFMAN, Y.M ................................p 141 N83-26155 p 142 N83-26176

SCHIMMEL, M.L ...................................p 36 N83-31596

SCHLIESING, J.A ..................................p 71 N80-16091

SCHMIDLIN, F.J ..................................p 161 N80-16682

SCHMIDT, J.F...........................................p9 N78-30057

p 46 N80-21324

SCHMIDT, S.F.......................................p 31 N83-29193

SCHMITZ,M ..........................................p 202 N84-26519 p 202 N84-26520

SCHMUGGE,T ......................................p 138 N78-23536 p 143 N65-23223

SCHMUGGE, T.J .................................p 138 N79-16329 p 152 N79-16473

SCHNEIDER, S.R ................................p 140 N82-20622

SCHNEIDER, W.H ...............................p 164 N82-29826

SCHOENSTER, J.A .............................p 187 N80-13879 p 188 N82-21037 p 190 N85-19790

SCHROEDER, D.J ...............................p 202 N85-12834

SCHRYER, D.R ....................................p 151 N79-10634 p 85 N82-22330

SCHULLER, F.T ...................................p 120 N79-18323 p 121 N80-21753 p 121 N60-33749 p 124 N84-29226 p 124 N85-13233 p 126 N66-24992

SCHULLER, F.,T ..................................p 122 N8t-19458

SCHUMANN, H.H ................................p 140 N82-20618

SCHUMANN, L.F ...................................... p6 N78-11002 p 20 N63-11058

SCHUON, S.R ........................................p 90 N85-21323

SCHWING, J.L.....................................p 177 N85-31839

SCHY, A,A ..............................................p 56 N81-13065

SClALDONE, J.J ................................p 147 N78-20654

SClBBE, H.W .......................................p 124 N85-13234

SCOGGINS, J.R ...................................p 162 N81-15639 p 162 N81-15640 p 162 N81-16678 p 163 N81-16679

SCoI-r, B.C ............................................p 40 N82-33381

SCoTr, C.D ......................................... pt13 N86-14530

SCOTT, W.R ..........................................p 77 N80-16095

SCRIBNER, P.C ..................................p 206 N81-25012 p 207 N82-16026

SCULLIN, V.J .........................................p 85 N84-32446

SEASHOLTZ, R.G ...............................p 115 N82-t9521

SEASHULTZ, R.G ................................p 20 N82-26234

SEBACHER, D.I ..................................p 113 N78-13408 p 150 N83-16952 p 150 N84-18764

B-12
PERSONAL AUTHOR INDEX

SEE, M.J ...................................P 21 N83-22166

SEEGER, C.L ...........................p 175 N84-22178

SEFIC, W.J ............................................P 10 N78-33053

SEINER, J. M. ............................p 188 N82-34189 p 189 N83-30164

SEINFELD, J. It- ..........................P 153 N81-23742

SELDNER, K. ..............................P 41 N77-31154 p 41 N77-33169

p 184 N78-30896

SENG, G. T. ...............................p 97 N81-24283 p 97 N84-23774 p 98 N85-31307

SEWALL, J. L. ..........................p 129 N80-19563

SEWALL, W.G. ............................p 24 N84-27694

SEWELL, J. L. ............................p 131 N83-16785

SEYL J.W .................................p 145 N81-27622

SHADE, It. ....................................p 199 N77-33003

SHAEFFER, J. ................................P 170 N79-10728

SHAFER, B. A. ............................P 140 N62-20620

SHAI, M. C. .....................................p 78 N78-21216

SHAUGHNESSY, J. 0. ...........................p 32 N79-14083 p 54 N79-15970 p 4 N84-12029

SHAW, R.J. ..............................p 52 N65-25261

SHEARIN, J.G .............................p 186 N81-22832 p 189 N63-33684 p 189 N84-25422

SHEFFLER, K.D .........................p 87 N80-32489

SHEIBLEY, D.W ..........................p 84 N79-22246 p 84 N79-25181

SHELDON, R. G. ..............................P 10 N78-33053 p 35 N81-12066

SHEPHERD, K.P ..........................P 172 N83-34579 p 189 N83-34713

SHEPHERD, W. 1". .......................P 187 N80-28150

SHERLOCK, J.J .........................p 119 N78-28457

SHERMAN, W. L. ..........................p 54 N79-14110 p 56 N81-20082

SHIBUT, M. A. .......................................P 110 N83-20032

SHIDELER, J.L. ..............................p 72 N82-14277

SHIGAKI,H .............................. p94 N82-20316

SHIMAZAKI, T. ..........................P 158 N77-32689 p 159 N79-16493

SHINN, J. L. .............................p 106 N79-14327 p 14 N80-21280

SHINN, J. M, JR. .......................... p90 N86-13406

SHIPLEY, S. T. ..............................p 150 N86-16748

SHILl, Y. J. ........................................p 116 N83-32044

SHIUE, J.C. ..................................P 152 N79-19519

SHOOK, D.F. ........................................p 149 N80-27832

SHOOSMITH, J.N .........................p 177 N64-22179 p 177 N85-28563

SHORE, C.P. ...................................p 128 N79-25427 p 107 N60-13402 p 131 N83-11513 p 112 N85-16066

SHORT, N. M. ..........................p 141 N83-I0458 p 141 N83-21419 p 142 N84-14563

SHORTAL, J. A. ......................................p 64 N79-20166

SHOWALTER, T.W .....................p 172 N78-31739 p 34 N80-15069

SHROUT, B.L ...................................p6 N78-10030

p 19 N62-26232 p 22 N83-34904

SHUART, M.J ...............................p 62 N83-2456t p 62 N83-33957

SHURNEY, R. E. .............................p 68 N83-16492

SHYNE, R. J. .....................................p 60 N86-28101

SICKLER, G.L ...............................p 160 N79-31885

SIDI, A. ..........................................p 182 N84-13885

SIDIK, S. M. .................................... p119 N78-16429

SIEBER, J. E. ................................p 196 N79-16709

SIEGEL, P. H. ........................................P 103 N84-20756

SIEGEL, R. ...................................p 104 N77-32432

SIEGEL, W. It. ...................................p 34 N80-15066

SIEMERS, P. M., Ill ..........................p 38 N80-23304 p 39 N80-32389 p 39 N81-26144

SIGNER, It. R. ............................p 121 N80-21753 p 121 N80-33749 p 122 N81-19458 p 124 N85-13233

SIGNER, HANS R. ...........................p 121 N80-29734

SILCOX, R. J. ........................................p 187 N80-32188

SIM, A. (3. ................................................p 54 N79-10068

SIMMON, D. A. ..................................p 40 N65-26705

SIMMONDS, R. C. ......................p 169 N78-t1663

SIMONEAU, R.J. ...........................p 107 N79-29468 p 109 N81-28389

SIMONS, T. D. ..................................p 14 N80-17964

SINCLAIR, J. H. .............................p 79 N78-13138 p 79 N76-16096 p 82 N84-13224

SINGER, J. ...................................p 144 N78-28624

SINGH, C. M. ..............................p 194 N78-26927 p 194 N78-30944

SINGH, J. J. ...........................................P !48 N79-33611 p 80 N60-27428 p 149 N61-11565 p 150 N82-27867 p 150 N82-28839 p 116 N84-11460 p 117 N86-20753 p 117 N86-24962

SINGH, R. P. ............................P1 N78-25048

SISK, T. R. ................................P 55 N80-23327

SKILLMAN, W.C ..................................p 163 N81-21686 p 163 N81-21693

SKOLAUT, M. W., JR .................p 113 N77-32458

SLEEPER, R.K ............................p 29 N80-27302 p 35 N82-23244

SLINEY, H.E ..........................p 119 N78-25433 p 93 N79-29327

SLIWA, S.M ..........................................p 56 N81-13968 p 35 N81-16039 p 37 N65-19979

SLOOP, J. L. ..........................p 97 N79-16994

SMALL, W.J ...............................p 32 N78-16042 p 17 N81-29098

SMERNOFF, D.T. ...................p 174 N85-29531

SMITH, A. ....................................p 114 N78-21430

SMITH, A. C. ................................ p149 N81-11565 p 150 N82-28839

SMITH, A. S. ..........................P 150 N82-27867

SMITH, B. A. ........................p 200 N81-11966

SMITH, C. F., JR ....................................p 92 N78-22233

SMITH, D.A. ...............................p 162 N64-13885

SMITH, D. M. ..................................p 74 N83-31713

SMITH, E.G. ..............................p 33 N80-12084

p35 N81-30112 p 35 N82-18204 p 35 N82-23244 p 35 N82-24193

SMITH, G. A. ............................... p55 N80-19126

SMITH, G.L ...........................p 159 N79-13644 p 162 N81-13593

SMITH, I. D. ..................................p 96 N78-13234

SMITH, J. L. ..............................p 194 N83-27846 p 74 N64-23676 p 195 N84-25458 p 75 N85-31141

SMITH, J. M. .................................p 42 N78-20131

p 194 N78-20959 p 44 N79-22099 p 48 N81-21077 p 50 N83-33693

SMITH, J.W .............................p 53 N78-21160

SMITH,L C. .............................p 76 N81-3128t

SMITH, M. A. 14. ...........................P 192 N82-15853 p 192 N86-13064

SMITH, O. E. .............................p 69 N82-20236 p 69 N82-33417

SMITH, P.M ...............................p 32 N78-27111 p 29 N81-12043 p 57 N84-12190 p 58 N65-11002 p 58 N85-34144

SMITH, R. E. ............................p 177 N86-23282

SNETSINGER, K.G. ...........................p 148 N79-30844

SOBIESZCZANSKI-SOBIESKI,J .....p 178 N79-17580

SODERMAN, P.R .........................p 185 N77-30909

SODERMAN, P.T .......................p 188 N82-24052

SOEDER, J. F. ..........................p 41 N77-33169 p 51 N84-11171

p 179 N85-17576

SOFIA, S. ..................................p 209 N82-17014

SOKOL, S. ..................................p 103 N84-20759

SOLDNER, J. K. ........................p 67 N83-32828

SOMERS, D. M. ......................................p 17 N81-24022 p 21 N83-30386

SORRELLS, R. B., Ill ..................p 13 N80-16032

SOVA, J.A. .............................p 79 N78-18135

p81 N81-11115

SPADY, A. A., JR ........................p 171 N79-19682 p 172 N66-27920

SPALVINS, T. ........................p 86 N78-26199 p 89 N83-34019

SPANGLER, L.W .........................p 150 N83-12595

SPENCER, B., JR ..................................p 56 N81-13066

SPRINKLE, D.R .......................p 117 N86-20753

SRIDHAR, S. ..............................p 54 N79-17872

SRINATHKUMAR, S. ..................p 180 N78-18823 p 53 N78-25101

STABE, R.G ...............................p8 N78-20080

p 50 N83-30431

STACK, S. H. ..........................................p 32 N78-16042 p 21 N83-30391

STACY, K. ...............................p 143 N85-30450

STAIGER, P. J. ...................................p 145 N82-16477

STAINRAGK, P.C. ...................p 108 N81-13303 p 60 N86-24709

STALLINGS, R. L, JR ...........................p7 N78-13016

p 15 N80-27283

STUBBS, S. M. p 16 N81-14975 p 18 N81-30087

STALLMAN, S. .........................p 115 N81-33452

STALLMAN, S. 1". .................................p 114 N80-22660

STANKIEWICZ, N. ..............................p t01 N79-22375 p 101 N79-27400 p 102 N81-28352 p 102 N82-25441

STANLEY, H.R ...................................p 139 N81-11438

STARNES, J. H, JR. .................p 130 N82-20567 p 82 N83-33957

STATON,L D. ......................p 115 N80-30717

STATON, W.L ............................p 149 N82-14672

STAYLOR, W. F. ............................p 167 N86-23160

STEARNS, C.A .......................... p111 N84-19741 p 9O N84-28958

STECHER,J ................................p 74 N84-34468

STECKER, F.W .........................p 199 N77-20977

STEELE, It.M ..............................p 153 N82-19734

STEERS, L. L. .....................................p 13 N80-11035

STEFANAKOS, E. K. ...................p 144 N78-28615

STEGER, J. L. .................................p 17 N81-22018

STEIN, B. A. ...............................p 87 N79-13137 p 79 N86-11227

STEIN,M ........................................P 127 N78-32492 p 132 N83-34373 p 135 N86-20656

STEIN, P.A. ...............................p 132 N83-34373

STEINKE, R.J. .........................P 10 N79 10022 p 49 N82-25250

STEINMETZ, G. G. ......................p 38 N78-13054 p 33 N79-33189 p 33 N80-13024 p 39 N80-30305 p 36 N83-22191

STELL, R.E ............................P 114 N78-21430

STENCEL, R. E. ..........................p 203 N86-12168 p 201 N66-23493

STEPHENS, D. G. .............................p 188 N82-31070 p 189 N83-34713

STEPHENS, E.W ...........................p 106 N78-30555

STEPHENS, J. B. ...........................p 147 N78-28682 p 68 N85-34149

STEPHENS, J.R ..............................p 86 N78-31213 p 87 N80-11188

STEPHENSON, J. D. .....................p 57 N82-20187 p 57 N83-16350

STEPKA, F. S. ..............................P 106 N79-22427 p 44 N79-25023 p 46 N80-21326 p 111 N84-21628

STERMER, R. L. ...........................P 194 N84-22402

STETZ, T. T, ...................................p 109 N81-24387 p 109 N82-20467 p 112 N85-14078 p 112 N85-27165

STEVANS,W ................................p 43 N78-33109 p 44 N79-23967

STEVENS, N. J. ..............................p 74 N84-33452

STEWART, D. A. ...................................p 74 N83-22317

STEWART, E. C. .........................p 53 N78-23100

p 187 N80-11869 p 35 N82-16068

STEWART, R.W ...............................p 153 N8t-23742

STICKLE, J.W ..........................p 29 N81-19035 p 29 N81-19056

STITHo J, J, ...........................p 192 N64-13978

STOCK,L V. .........................p 192 N84-13978

STOCKMAN, N.O ............................... p42 N78-21114 p 10 N79-14996

STOKES, J. W., JR .................p 62 N81-26160

STOLARSKI, R. S. ...........................p 156 N86-25911

STONE, It.W ....................................p 70 N77-33259 p 70 N76-13119 p 71 N80-29417 p 58 N84-23652 p 69 N85-15778

STONE, H. W., JR ........................p 71 N80-32429

STONE, N. H. ............................... p72 N82-15116

STOREY, R.W ..........................p 150 N83-12595

STOUGH, 14. P., III .................................p 32 N78-18044 p 37 N85-25248

STRADLING, J. S. .......................p 99 N83-32990

STRAIGHT, D. M. ........................p 50 N83-26839

STRAZISAR, A.J ......................p 115 N82-19521 p 22 N83-32774

STREETr. C.L ...................................p 24 N84-27682

STRGANAC, T.W .....................p 160 N80-12661

STROKOWSKI, A.J ...........................p 106 N78-33385

STROM, R. G. ..........................p 205 N78-30025 p 200 N85-18888

STROUD, W. J. .........................p 132 N84-16585

STUART, L. M., JR. ..................p 142 N84-14563

STUBBS, S. M. ..........................p 33 N80-12084

p 130 N81-24471

p35 N81-30112 p 35 N82-18204

B-13
STUCKEY, R. N.

p 35 N82-24193

p 135 N86-11522

STUCKEY, Ro N. ..........................p 72 N82-14277

STURMAN, J. C. ..............................p 101 N79-32467 p 76 N81-31262 p 78 N85-21263

STURMAN, J.L .....................p 78 N86-25123

SU, S. Y. .....................................p 63 N85-21188

SUCCI, G. P. .....................................p1 N78-25049

SUCEC, J. .................p 104 N78-17338

SUIT, W.T. ............................................p 53 N78-13071 p 35 N82-16068

SUMMERLIN,L El. ....................p 65 N77-29189

SUMMERS, R. L. ...........................p 116 N85-16100

SUMNER, I.E ..........................................p 65 N78-17127 p 65 N78-28150

SUNDARARAJAN, N. ......................p 75 N86-31142 p 75 N86-30800

SUNDBURG, G.R. .......................p 103 N86-21755

SUSKO, M. ...........................................p 147 N76-11517

sUTrLES, J. 1". ....................................p 167 N86-26574

SVEHLA, R.A ....................p 149 N80-27832

SWAN, B.E ................................p 53 N78-26151

SWANSON, R. C., JR ...................p 16 N81-13919

SWARTZ, C. K. ..............................p 145 N79-33572

SWENSON, L. S., JR ......................p 62 N79-28203

SYMONS, E.P. ...................................p 104 N77-33444 p 106 N78-31354 p 107 N79-29467

SZANCA, E.M .............................p 46 N80-25337

SZUCH, J.R ................................. p41 N77-31154 p 41 N77-33169 p 179 N82-33020 T

TALH ...................................................p 27 N86-18289

TAILLON, N.V ........................p 21 N83-25665

TANDBERG-HANSSEN, E. A. .......p 209 N83-13048 p 209 N83-25646

TANDBERG, E. .........................p 210 N86-246t4

TANG, M.H ..................................p 10 N78-33053 p 35 N81-12066

TANNER, J.A. ......................p 33 N60-12084

p 130 N61-24471 p 35 N81-30112 p 130 N82-10430 p 35 N82-16204 p 35 N82-24193 p 131 N63-21391 p 132 N83-33217 p 133 N84-34773

TANNER, S. .............................p 115 N62-29577

TANNER, T, A. .......................p 196 N79-16709

TAYLOR, C.M .......................p 119 N76-30565

TAYLOR,R .......................................p 165 N83-14835

TAYLOR, R_Ep 198 N79-26062

TAYLOR, R. 1". .............................p 29 N76-13029

TESBETTS,I......................p 172 N79-11734

TEICHMAN, L.A ..................................p 79 N83-12147 p 83 N85-12941

TELES,J .........................p 64 N81-11070

TENNEY, EL R. ........................p 86 N78-15236 p 87 N79-13137 p 87 N79-13136

TERRAY, D.E ................p 98 N78-16252

TEVAARWERK, J. L. ...............p 121 N79-33475

THAMES, F.C .........................p 182 N81-22754

THEON, J.S. ...................................p 157 N77-19709

THtBODEAUX, J.J ....................p 59 N80-31413

p 110 N83-20031

THtELE,O ......................p 166 N86-13866

THOMAS, J.L. .....................p 54 N79-31223 p 13 N80-12994 p 17 N81-29095

THOMAS, J. P. ........................p 168 N82-10661

THOMAS, L.R ..................................p 63 N66-27297

THOMAS, M.E .....................p 167 N66-24090

THOMAS, R. N. ..................................p 204 N84-19253

THOMAS, S.R .................................p 60 N83-36039

THOMPSON, A. H. ...........................p 160 N79-31885

THOMSON, R. G. .......................p 133 N84-21901

THORNHILL R. Ft. .........................p 142 N83-27293

THRESHER, R.W .................p t46 N82-23664 p 146 N83-19231

THRONSON, H. A., JR .......................p 202 N85-17848

THURSTON, G.A. .......................p 135 N86-20857

TIRBITS, T.W .....................................p 173 N82-24834

TIEFERMANN, M.W ...........p 148 N79-22654

TIFFANY, S. H. ........................p 179 N84-27461

TILTON, J. C. .................................p 143 N86-31945

TINDAL, M.A ..............................p 138 N80-10537

TITRAN, R.H ........................p 87 N80-32489 p 87 N80-33555

TOBIAS,L ..............................p 30 N85-32101

B-14

TOLL T. A. ............................ 34

TOMKO, J. J. ............................_ 123

TOON, O. B. .............................._ 160

160

161

TORIDIS, T. G. ................................_ 178

TOWNSEND, D.P ........................) 120

121

122

122

124

t16

125

125

TOWNSEND, J.C. ....................... 17

TOWNSEND,LW ...................... t92

192

192

192

193

193

193

211

193

193

TOWSEND, D.P. ........................ 120

TREFNY, C. J. ............................p 52

TREI"PER, S. A. ....................................p 16t

TRIPP, J. H. .................................p 125 p 125

TRIPP, J. S. ................................p 181 p 59 p 184 p 116

TRIVEDI, K. S. .......................p 176 p 176

TROMBKA, J. I, ..........................p 204

TROUT, A. M. ...................................p 48 p 50

p51 p 52

TRUONG, L. V. .....................................p 103

TUCKER, R. S. ................................p 205

TUCKER, W. H. ...........................p 202

TUMA, G.B. ...................................p1 O0

TUNG, C. ...................................p 23

TURCO, R.P. ............................p 158 p 159

p160

p160 p 161

TURNER, R. E. ...............................p 158 p 159 p 159 p 153 p 164 p 165 p 165 p 165

TURNER, R.L .............................p 207

TURNEY, G. E. ..................................p 51

TuI-rLE, J. L. ..........................p 77

TUTTLE, M. It. .............................p 107

U

USER, J. .......................................p 99

UCCELLINI,LW ..............................p 163 p 166

UNDERHILL A. ................................p 200

UNDERHILL A. EL .....................p 200

UNNAM, J. ............................................p 86

p87

p87

p81 p 90

URASEK, D.C. .............................p 43 p 44 p 44 p 45

USRY, J.W .................................p 147 p 147 p 167 p 147 p 146 p 168 p 168 p 140

V

N80-21318

N84-t7590

N79-21720

N79-2t721

N80-15726

N77-33876

N79-14389

N79o32552

N81-14322

N62-32736

N85-13234

N85-16099

N86-12609

N86-t4612

N81-22016

N61-27899

N82-23003

N83-23140

N84-22396

N85-17690

N85-27665

N86-21297

N86-21492

N86-23388

N86-30485

N79-31604

N86-24694

N80-23933

N85-32329

N85-32331

N61-29840

N82-11090

N83-35736

N86-12579

N80-23008

N81-15702

N82-21118

N81-21077

N83-33893

N85-10064

N85-21168

N86-21755

N76-20042

N84-22516

N76-11301

N84-18159

N77-32688

N78-30774

N79-2t720

N79-21721

N80-15726

N78-15641

N79-14678

N79-14679

N80-28965

N62-16660

N83-19391

N83-33494

N83-36587

N83-25636

N84-21549

N83-24549

N79-33436

N84-33813

N81-19709

N86-13867

N82-25027

N65-t7755

N78-15236

N79-13137

N79-13138

N82-31451

N88-26412

N76-33109

N79-16852

N79-23967

N79-27143

N78-12554

N78-12555

N78-t2645

N78-33616

N79-1736O

N79-28864

N79-31890

N82_13468

VAICAITIS, R. .............................p 186 N78-23877

VALLAS, M. .................................p 26 N85-23707

VANALLEN, J. .........................p 206 N81-15925

PERSONAL AUTHOR INDEX

VANBALEN, P.M. ........................p 173 N83-18238

VANOAM, C. P. ...............................p 25 N64-33379

VANDERPLAATS, G. N. ..................p 11 N79-18915

VANFOSSEN, G. J., JR. ....................p t06 N79-22427

VARY, A. ................................................p 126 N66-22962

VAUGHAN, V. L., JR. .....................p 29 N78-I0034

p 128 N80-11505 p 35 N60-30296

VAUGHAN, W. W. .........................p 151 N78-29669 p 159 N79-146RO p 152 N79-30869 p 162 N80-26999 p 164 N83-14625 p 166 N84-34629 p 156 N86-25900

VAUGHN, C. R. ................................p 169 N79-19592

VEERABHADRARAO, P. ...................p 89 N83-32908

VENKAYYA, V.B. ............................p 66 N83-18819

VERDERAIME, V. ...................................p 61 N63-16400 p 83 N84-33521

VERDERAIME, V.S. ............................p 135 N86-23974

VERRILLI, M. J. ............................p 89 N84-17350

VEVERKA, J. .........................................p 200 N85-23457

VICROY, D. D. ..................................p 31 N84-17165 p 40 N85-26705

VILLE, J. M. ...............................p 187 N80-32188

VOGLER, W.A. ............................p 130 N82-10430

VOIGT, S. ..................................p 179 N85-20689 p 180 N66-23314

VOtGT, S.J. ..........................................p 176 N82-26996

VOMASKE, R. F. .....................................p 53 N78-26151

VONPRAGENAU, G.L ................p 49 N82-20183

VOSTEEN,L F. .........................p 83 N85-12941

W

WAITE, J. H., JR. ...........................p 20t N86-13239

WAKE, W. H. ...............................p 136 N81-32564

WAKELYN, N.T. ........................p 84 N78-23172

WALBERG, G. D. .................................p3 N81-14961

p 118 N83-27200

WALBORN, N. R. .............................p 204 N86-25307

WALES, R.O. ................................... p73 N82-16147 p 73 N82-16146 p 73 N82-16149 p 73 N82-16150 p 73 N82-16151 p 73 N82-16152

WABGORA, J, M. ................................p 170 N80-15788

WALKER, G. tt. ................................p 88 N83-18895

WALKER, H.J ..................................p2 N79-30139

WALL S. D. .................................p 206 N81-25012 p 207 N82-16026 p 208 N85-21099

WALLACE, R. (3. ............................p 100 N82-15270 p 100 N83-29491

WALLER, M. C. .............................p 171 N79-33836 p 172 N82-14804

WALLSON, R.E. ....................................p 74 N83-19806

WALSH, M. J. ................................p 105 N76-22331 p 1t2 N84-25944

WALTER,L S. ..........................p 137 N84-30475

WALTON, B. A. .............................p 65 N82-t5095

WALTON, W. C., JR. ....................p 133 N84-33832

WALTZ, J. E. ....................................p 128 N79-33500

WANG, C. R. ..............................p 110 N83-12360 p 111 N83-34232

WANG, J. ..............................p 138 N78-23536

WANG, J. R. ................................p 152 N79-16473

WANG, S. Y. ..........................................p 194 N78-20959

WARD, J. C., JR. ........................ p66 N80-19145

WARDRIP, S.C. ...........................p 185 N80-29096 p 117 N61-27467 p 118 N82-20494 p 118 N63-35351

WARNER, D. M. ............................p 138 N80-I0538

WARNER, D. N., JR. ........................p 57 N84-t3198

WARNER, J.W .......................p 200 N80-22130

WASHBURN, K. E. .......................p 10 N79-15902

WASSERBAUER, J.F. ..................p 52 N65-25261

WASSERBAUER, J.W ......................p 52 N86-24694

WATSON, A.B. ........................p 172 N83-33538

WATSON, C.B. ...........................p 15 N80-27283

WATSON, D.M. .............................p 57 N84-13198

WATSON, J. J. ............................p 75 N85-19015

WATSON, R. D. .............................p 106 N79-14328

WATSON, R. T. ..............................p 156 N86-25911

WATSON, V. R. ............................p 158 N77-32689

WATSON, W.R .............................p 188 N81-33946 p 188 N62-34190 p 190 N84-27543 p 190 N86-13056

WEAR, J.D ...............................p 44 N79-14096 p 47 N80-32396 p 48 N81-21077 p 50 N83-33893
PERSONAL AUTHOR INDEX

p 51 N85-10064

p 52 N85-21168

p 52 N85-31058

WEAVER, W. L. ......................... p 160 N79-22709

p 161 N80-20986

WEAVER, W. R. ........................... p 118 N84-17575

WEBB, J. A., JR. .......................... p 54 N79-28186

p 56 N80-29369

WESS_ L D ................................. p 37 N85-12884

WEBER, L. A. ................................... p 84 N78-16119

WEDEVEN, L D. ......................... p 123 N83-28453

WEHREND, W, R., JR ..................... p 55 N80-17081

WEIDMAN, C. D. ....................... p 160 N79-22708

WEILMUENSTER, K. J. .................. p 107 N79-33441

p 110 N83-24808

WEIMER, D. .................................... p 115 N82-23515

WEINBERG, L ........................... p 195 N79-13886

p 145 N79-33572

WEINSTEIN, L ............................ p 107 N80-13402

p 109 N82-13383

WEIR, 0. S. ............................. p 189 N83-16149

WEISSENBERGER, S. ..................... p 54 N79-13057

WELCH, P.J. ............................... p 191 N79-25861

WELKER, J. ............................... p 163 N81.22658

WELLEMEYER, C. .................... p 165 N84-16720

WELLER, W. H ............................. p 31 N78-11053

p 33 N79-15938

WELLS, H.T. ........................... p211 N77-16981

WELLS, W. C. .............................. p 205 N78-29007

p 136 N84-18716

WELLS, W. R ............................ 139 N78-30054

p 13 N80-12995

WENZEL, A. R ........................ p 186 N78-17823

WESOKY, H. L, ........................ p 42 N78-20132

WESTFALL, L.J. ..................... p 80 N79-28234

WESTON, R. P. .......................... p 105 N78-26392

p 12 N79-26020

p 107 N79-32500

WETTLAUFER, B. M. ........................ p 59 N83-17560

WHARTON, R. A., JR ............... p 174 N83-30016

WHEELER, D. R. ............................... p 91 N77-33348

p 91 N78-20336

p 91 N78-20338

p 92 N79-15184

p 78 N79-22194

p 79 N79-31346

p93 N81 11214

p 85 N83-18863

p 96 N84-31379

WHILOCK, C. H. ......................... p 147 N78-33616

WHITAKER, A. F. ......................... p 92 N78-22233

WHITAKER, E. A. ................... p 207 N83-12031

WHITCOMB, J. D ..................... p 130 N81-13373

WHITE, I1:. A. .............................. p 114 N78-21431

WHITE, J. B. ........................... p178 N82-11784

WHITE, M. D .............................. p 29 N80-22283

WHITE, N. H. ....................................... p 106 N79-20345

p 108 N80-23600

WHITE, W. L. ......................................... p 5 N77-33111

p 6 N78-12040

WHITELEY, S. H. ....................... p 211 N77-16981

WHITLOCK, C. H. .................... p 147 N78-12554

p 147 N78-12555

p 167 N78-12645

13 148 N79-17360

p 168 N79-28864

p 168 N79-31890

p 140 N82-13468

p 150 N82-21774

WHITMORE, S. A. ................... p 37 N85-12884

WHITNAH, A. M ...................... p74 N85-11127

WHITNEY, W. J ............................... p 46 N80-25337

p 47 N80-25338

1348 N81-16050

p 49 N83-17547

WHITTEN, R.C. ............................... p _58 N77-32688

p 158 N7732689

p 159 N78-30774

p 160 N79-21720

p 160 N79-21721

p 161 N80-15726

p 149 N81-17622

WHITTENBERGER, J. D. ................... p 87 N81-19273

WHITTLESEY, A.C. ........................... p 74 N84-33452

WIANT, H. R. ........................... p 80 N78-20256

p 89 N83-35108

p 90 N86-13406

WICHANSKY, A. M. .................. p 199 N80-18990

WICHANSKY, A. W .................... p 172 N78-11705

WICHOREK, G. R ................... p 81 N82-25325

p 83 N86-20508

WIDHOPF, G. F. ................................. p 149 N81-17622

WIEDEMANN, K. E. .................. p 90 N86-26412

WIESE, M. R ........................ p 177 N86-23282

W|ESEMAN, C.D. ........................ p /81 N86-13946

WILCOX, D. C. ....................... p 107 N80-20527

WILHELM, J. M. ........................ p 196 N79-16709

WILHELMS, D.E. .......................... p 200 N85-18888

WILHITE, A.W. ............................... 1355 N80-13852

WILKERSON, T. D ...................... p 138 N78-21526

p 138 N78-23537

WILKINS, J. R. ........................... p 148 N79-14591

WILL, H. A. ............................ p 179 N81-33838

WILLETT, J.A. ...................................... p 69 N82-33417

WILLIAMS, D. ............................ p 138 N78-23538

WILLIAMS, D. H. ......................... p 173 N80-15821

p 40 N83-18723

WILLIAMS, J, G. ........................ p 127 N78-12475

p 127 N78-32492

13 82 N83-33957

WILMAMS, J. 13........................... 13 75 N85-31142

WILLIAMS, L.J. ......................... 13 36 N83-20931

WILLIAMS, M. O. ........................ p 117 N82-18578

p 118 N84-23878

WILLIAMS, M. L. .............................. 13 38 N78-20128

WILMAMS, M.S. ......................... p 131 N83-10442

WILLIAMS, R.C. ............................. 1347 N81-11037

WILLIAMS, R, J. ........................... p 106 N79-t8287

13206 N80-16009

13 201 N86-27136

WILLIAMS, S. O. ........................... p 105 N78-18364

WILLIAMS, T. E ......................... p 169 N78-18673

WILLIAMSON, F. R. ........................ p 79 N78-11200

WILLIS, C. M. .......................... 13 186 N79-16641

p 187 N80-13879

p 188 N82-14879

p 190 N85-30767

WlLLSHIRE, K. F. ....................... p 149 N82-12654

WILLSHIRE, W. L., JR ................. p 187 N81-14788

p 189 N84-10913

WILLSON, R. CL ................................ p 209 N84-27635

WILMOTH, R. G. ............................... p 7 N78-13017

13 147 N78-15596

p 14 N80-22261

WILSON, C. H .......................... p 84 N78-23172

13 84 N79-28259

p 85 N81o14017

WILSON, G.S. ........................... p 161 N80-16675

WILSON, H. W .................................. p 118 N83-32044

WILSON, J. C .............................. p 27 N86-20349

WILSON, J. W ............................... p 206 N81-25012

p 207 N82-18028

p 192 N83-23140

p 210 N83-29169

13192 N84-13978

p 118 N84-17575

13210 N84-21485

p 192 N84-22396

p 174 N84-29479

p 193 N85-27665

1390 N86-26413

WILSON, M. L ............................. p 112 N84-31561

WILSON, R. G ............................... p 148 N79-29679

WILSON, R. M. ............................. p 209 N84-24520

p 210 N86-24614

WINER, W.O. ............................ p 119 N78-22377

WINKLER, C. E. ................................ p 193 N78-11812

WINSA, E. A. ......................................... p 80 N79-28234

WINTER, D. L ........................... p 170 N79-13686

WINTER, W. R. .............................. p 32 N78-20114

WlSANDER, D.H. .......................... p 93 N79-29327

WISANDER, 13'. W ....................... p 86 N78-15229

p 119 N78-20512

p 120 N79-10424

p 93 N80-23453

13 88 N81-20245

WISCOMBE, W. J ....................... p 194 N86-17140

WITMER, E.A. ................................. p 41 N78-10068

WITT, R. G. ........................ p 141 N83-19141

WITTE, W. (3;. ............................. p 147 N78-12554

13 t47 N78-12555

p 187 N78-12645

p 147 N78-33616

t3 148 N79-17360

p 168 N79-28864

p 168 N79-31890

p 140 N82-13488

p 150 N82-21774

WII"TMANN, R .......................... p 152 N79-19519

WITZKE, W. R. ............................ 1386 N78-312}3

WOLAK, J. ...................................... p88 N81-20245

WOLF, W ............................... p 169 N79-19592

WOLFE, J. ..................................... p 175 N78-18771

WOLFE, J. H ............................ p 175 N84-22178

WOLFF, S. C. ................................ p 204 N83-32693

WOLOWlCZ, C. 14. ........................ p 33 N79-30176

WONG, E. L ................................ p84 N78-12167

p 84 N78-20281

WOOD, G. M. ......................... p114 N78-21431

WOOD, J. A ............................... p 175 N85-28562

WOOD, J. R. ..................................... p6 N78-11002

p 17 N81-22017

p 20 N83-11058

ZELEZNIK, F. J.

WOOD, R. M ....................................... p 22 N83-32776

p 22 N83-34905

p 23 N84-20486

p 24 N84-27676

p 26 N85-29921

1326 N85-29922

WOODBURY, G. E. ......................... p 149 N81-22587

WOOI_J, D. C. ............................. p 150 N83-16952

p 150 N84-t8764

WOODWARD, H.T. .................... p 158 N77-32689

WOODWARD, R. P .............................. 13 187 N80-23100

p 188 N82-21036

WOOLLEY, C, T. ............................. 1399 N81-20311

WORLEY, B. A. .............................. p 166 N85-14360

WORNOM, S. F. ............................. p 106 N79-13305

WRAY, A. A. ............................................ 13 18 N81-16977

WRAY, ,11.D. .................................. p 210 N79-27057

WRIGHT, A, S., JR. ......................... p 26 N85-23707

WRIGHT, R. L. ............................... p 73 N82-16153

p 67 N84-18277

WU, S. T ....................................... p 62 N79-26076

1378 N85-26862

WYNNEo E.C. ..................................... p 2 N80-11028

X

XU, Y. J .......................................... 13 210 N84-21485

Y

YAGER, T. J. ......................................... p 32 N78-13043

p 29 N80-13013

YAMADA, Y. ..................................... p 98 N84-31379

YAMAMOTO, 1". .............................. p 122 N82-32737

13 122 N83-11496

YANTSlOS, J. N ................................ p 191 N79-25861

YARDS, S. F. ................................... p 23 N84-17132

YEAGER, W.T. ................................ p 18 N82-13107

YEAGER, W. 7",, JR. ......................... p 8 N78-28056

YEATES, C. M ................................ p208 N86-11137

YEH, F. C ........................................ 13111 N84-21828

YENNI, K. R, ...................................... p 38 N78-31101

13 32 N79-14083

p 38 N80-27360

p 58 N85-34144

YEOMANS, D, K ............................. p 206 N80-11972

YEI"TER, J.A. .................................... 13 16 N81-15976

YIP, L. P. ......................................... p 6 N78-13014

p 8 N78-25060

p 14 N80-22266

p3 N82-11013

I3 24 N84-26660

p 25 N85-19925

YOSHIKAWA, K. K, ...................... p 16 N81-16977

YOUNG, A.T. ................................... 13203 N85-17892

YOUNG, C. P., JR. .......................... p 59 N83-18748

YOUNG, J. C ................................ p 40 N83-16338

YOUNG, J. W ................................. p 56 N81-13065

p 74 N84-23675

p 75 N86-16250

YOUNG, S. G. ................................. p 86 N78-15230

p 88 N82-21298

p 88 N83-15413

p 89 N83-24641

p 95 N83-24695

YOUNG, W. H., JR. ....................... p 105 N78-21410

p 10 N79-14019

YOUNGSLOOD, J. L. ......................... p 127 N78-30610

YOUNGLOVE, S. .......................... p 97 N80-14257

YRASEK, D. C. .............................. p 45 N79-30191

YU, J. C. ................................... p 109 N81-23410

p 191 N86-21280

p 191 N86-31337

YUE, G. K .................................. p 149 N81-11565

p 153 N82-12687

p 150 N82-27867

p 150 N82-28839

Z

ZANA, L. M ................................ p 78 N86-28123

ZANG, 1". A. ............................. p 201 N79-24821

ZARETSKY, E. V ......................... p 119 N78-20513

p 119 N78-21473

p 120 N79-14389

p 122 N81-14322

p 122 N82-32736

p 116 N85-16099

p 125 N85-31511

p 125 N86-13734

p 125 N86-14612

ZELEZNIK, F. J. ......................... p 196 N83-23188

t3 196 N83-23189

p 182 N85-19733

B-15
ZELLARS, G. R.

ZELLARS, G. R. ........................... p 86 N78-15230

p 86 N78-28225

ZOLLER, L. K ................................ p 94 N81-33292

ZORUMSKI, W. E. ....................... p 189 N83-16149

ZUCKERWAR, A.J. ................... p 190 N85-11789

p 98 N85-35307

ZUPPp G. A., JR. ......................... p 71 N80-16091

ZURAWSKI, R. L .............................. p 78 N86-28124

ZWALLY, H.J. ......................... p 168 N84-107t8

PERSONAL AUTHOR INDEX

B-16
NASA Scientific and Technical Publications

Typical Report Number

Index Listing

NASA-CP-2110 p 11 N80-15649

Listings in this index are arranged alphanumerically by report number. The page number

indicatas the page on which the citation is located.

The acceslion number denotes the number by

which the citation is identified. An astensk (*)

indicates that the rtem is a NASA report. A pound

sign (#) indicates that the item is available on

microfiche.

NASA-CP-001-PT-1 ........................ p 1 N77-17996

NASA-CP-001-PT-2 ........................ p 1 N77-18019

NASA-CP-002 ................................. p 199 N77-20977

NASA-CP-003 ................................. p 175 N77-22808

NASA-CP-O04 ................................. p 151 N78-12586

NASA-CP-005 ................................. p 169 N78-11663

NASA-CP-006-PT-1 ........................ p 138 N78o23537

NASA-CP-006-PT-2 ........................ p 138 N78-21526

NASA-CP-007 ................................. p 212 N78-23010

NASA-CP-2001-VOL-1 ................... p 98 N77-10230

NASA-CP-2001-VOL-2 ................... p 98 N77-10265

NASA-CP-2001-VOL-3 ................... p 98 N77-10305

NASA-CP*2001-VOL-4 ................... p 98 N77-10345

NASA-CP-2002 ............................... p 61 N78-76855

NASA-CP-2003 ...............................

NASA-CP-2004-SUPPL .................

NASA-CP-2004 ...............................

NASA-CP-2005 ...............................

NASA-CP-2006 ...............................

NASA-CP-2007 ...............................

NASA-CP-2009 ...............................

NASA-CP-2010 ...............................

NASA-CP-2012 ...............................

NASA-CPo2013 ...............................

NASA-CP-2014-VOL-1 ...................

NASA-CP-2014-VOL-2 ...................

NASA-CP-2015 ...............................

NASA-CP-2016 ...............................

NASAoCP-2017 ...............................

NASA-CP-2018 ...............................

NASA-CP-2019 ...............................

NASA-CP-2020 ...............................

NASA-CP-2021 ..............................

NASA-CP-2024 ...............................

NASA-CP-2025 ...............................

NASA-CP-2026 ...............................

NASA-CP-2027 ...............................

NASA-CP-2028 ...............................

NASA-CP-2029 ...............................

NASA-CP-2030 ...............................

NASA-CP-2031 ...............................

NASA-CP-2032 ...............................

NASA-CP-2033 ...............................

NASA-CP-2034 ...............................

NASA-CP-2035-VOL- 1 ...................

NASA-CP-2035-VOL-2 ...................

NASA-CP-2036-PT-1 .....................

NASA-CP-2036-PT-2 .....................

NASA-CP-2037 ...............................

NASA-CP-2038 ...............................

167 N77-16675

b 151 N77-15564

p t51 N77-15563

41 N77-17081

D 172 N77-27710

61 N79-19013

59 N77-27139

136 N77-30521

176 N77-28750

172 N78-11705

211 N77-33030

212 N77-33048

178 N77-33876

) 84 N77-33297

) 41 N78-10068

127 N78-12443

98 N77-30273

144 N78-13527

41 N78-11063

136 N77-32549

1 N78-12999

60 N78-18088

101 N78-16266

158 N78-19711

t59 N79-20575

138 N78-21562

205 N78-16973

176 N78-19778

97 N78-19325

144 N78-196t6

) 65 N79-10078

) 66 N79-10097

1 N78-27046

1 N78-29046

144 N78-19600

129 N79-21374

NASA-CP-2039 .............................. p 62 N79-25048

NASA-CP-2040 ............................... p 177 N78-74659

NASA-CP-2041 ............................... p 144 N79-21565

NASA-CP-2042 ............................... p 144 N78-28615

NASA-CP-2043 ............................... p 136 N79-23461

NASA-CP-2044 .............................. p 198 N79-10942

NASA-CP-2045-PT- 1 ..................... p 11 N79-20030

NASA-CP-2045-PT-2 ..................... p 2 N79-19989

NASA-CP-2046 ............................... p 14 N80-21283

NASA-CP-2049 .............................. p 136 N79-20424

NASA-CP-2050 .......................... p 64 N79-14121

NASA-CP-2051 ............................. p 170 N79-10728

NASA-CP-2052-PT-1 ..................... p 186 N78-32816

NASA-CP-2052-PT-2 ..................... p 186 N79-10843

NASA-CP-2053 .............................. p 205 N78-29007

NASA-CP-2054-VOL-t .................. p 9 N78-32055

NASA-CP-2055 ............................... p 178 N78-33776

NASA-CP-2056 ............................... p 151 N78-29669

NASA-CP-2057 ............................... p 159 N79-17413

NASA-CP-2058 .............................. p 76 N79-10122

NASA-CP-2059 .............................. p 128 N79-10448

NASA-CP-2060 ............................... p 173 N79-15588

NASA-CP-2061 ............................... p 1 N79-15898

NASA-CP-2062 ............................... p 127 N78-32466

NASA-CP-2063 ............................... p 212 N79-15887

NASA-CP-2064 ............................... p 178 N79-13736

NASA-CP-2065-PT-1 ..................... p 128 N79-21422

NASA-CP-2065-PT-2 ..................... p 128 N79-21435

NASA-CP-2066 ............................... p 29 N79-21021

NASA-CP-2067 ............................... p 44 N79-15961

NASA-CP-2068 ............................... p 205 N79-16758

NASA-CP-2069 ............................... p 61 N79-13069

NASA-CP-2070 ............................... p 169 N79-19592

NASA-CP-2071 ............................... p 71 N79-24001

NASA-CP-2072 ............................... p 205 N79-16757

NASA-CP-2073 ............................... p 138 N79-16329

NASA-CP-2074 ............................... p 80 N79-22196

NASA-CP-2075 ............................... p 62 N79-20162

NASA-CP-2076 ............................... p 159 N79-20633

NASA-CP-2077 ............................... p 46 N80-15127

NASA-CP-2078 ............................... p 44 N79-24994

NASA-CP-2079 ............................... p 80 N79-30297

NASA-CP-2080 ............................... p 120 N79-21352

NASA-CP-2081 ............................... p 128 N79-22539

NASA-CP-2082 ............................... p 64 N79-26082

NASA-CP-2084 ............................... p 117 N79-22455

NASA-CP-2085-PT-1 ..................... p 2 N79-23889

NASA-CP-2085-PT-2 ..................... p 2 N79-27070

NASA-CP-2086 ............................... p 12 N79-23912

NASA-CP-2087 ............................... p 44 N79-25016

NASA-CP-2088 ............................... p 144 N79-28669

NASAoCP-2089 ............................... p 206 N80-11972

NASA-CP-2090 ............................... p 152 N79-25608

NASA-CP-2091 ............................... p 62 N79-26076

NASA-CP-2092 ............................... p 45 N80-10205

NASA-CPo2093 ............................... p 13 N80-10107

NASA-CP-2094 ............................... p 29 N79-31166

NASA-CP-2095 ............................... p 152 N79-30869

NASA-CP-2096 ............................... p 199 N80-18990

NASA-CP-2097 ............................... p 144 N79-32640

NASA-CP-2098 ............................... p 209 N80-17944

NASA-CP-2100 ............................... p 160 N79-32797

NASA-CP-2101 ............................... p 75 N80-13152

NASA-CP-2102 ............................... p 212 N80-20003

NASA-CP-2103 ............................... p 171 N79-33838

NASA-CP-2104 ............................... p 160 N80-14633

NASA-CP-2105 ............................... p 160 N79-33722

NASA-CP-2106 ............................... p 145 N80-16453

NASA-CP-2107 ............................... p 117 N80-13438

NASA-CP-2108-PT-1 ..................... p 3 N81-17981

NASA-CP-2108-PT-2 ..................... p 3 N81-18005

NASA-CP-2109 ............................... p 168 N80-12718

NASA-CP-2110 ............................... p 149 N80-15649

NASA-CP-2111 ............................... p 200 N80-22130

NASA-CP-2112 ............................... p 114 N80-12384

NASA-CP-2113 ............................... p 200 N80-14977

NASA-CP-2114 ............................... p 176 N80-t2741

NASA-CP-2115 ............................... p 139 N80-28798

NASA-CP-2116 .............................. p 139 N80-25742

NASA-CP-2117 ............................... p 145 N80-20820

NASA-CP-2118 .............................. p 66 N80-19145

NASA-CP-2119 ............................... p 80 N80-19193

NASA-CP-2120 ............................... p 29 N80-22283

NASA-CP-2121 ............................... p 108 N80-25588

NASA-CP-2122-PT-1 ..................... p 99 N82-20357

NASA-CP-2122-PT-2 ..................... p 99 N82-20358

NASA-CP-2123 ............................... p 64 N80-28389

NASA-CP-2124-VOL-1 ................... p 201 N80-18997

REPORT NUMBER INDEX

1977-1986

NASA-CP-2124-VOL-2 ..................

NASA-CP-2125 ...............................

NASA-CP-2126 ...............................

NASA-CP-2127 ...............................

NASA-CP-2128 ...............................

NASA-CP-2129 ...............................

NASA-CP-2130 ...............................

NASA-CP-2131 ...............................

NASA*CP-2132 ...............................

NASA-CP°2133 ...............................

NASA-CP-2134 ...............................

NASA-CP-2135 ..............................

NASA-CP-2136 ...............................

NASA-CP-2137 ...............................

NASA-CP-2138-PT-1 .....................

NASA-CP-2138-PT-2 ....................

NASA-CP-2139 ...............................

NASA-CP-2140 ...............................

NASA-CP-2141 ..............................

NASA-CP-2142 ...............................

NASA-CP-2143 ...............................

NASA-CP-2144 ...............................

NASA-CP-2145 ...............................

NASA-CP-2146 ...............................

NASA-CP-2147-SUPPL .................

NASA-CP-2147 ...............................

NASA-CP-2148 ...............................

NASA-CP-2149 ...............................

NASA-CP-2150 ...............................

201

145

46

99

3 161

:) 185

:) 176

) 129

168

121

152

187

192

47

117

117

162

162

145

80

179

77

153

) 47

130

129

139

) 212

) 99

NASA°CP-2151 ............................... 129

NASA-CP-2152 ............................... p 64

NASA-CP-2153 ............................... p 139

NASA-CP-2154 ............................... p 77

NASA-CPo2155 ............................... p 136

NASA-CP-2156 ............................... p 175

NASA-CP-2157 ............................... p 163

NASA-CP-2158 ............................... p 177

NASA-CP-2159 ............................... p 76

NASA-CP-2161 ............................... p 162

NASA-CP-2165 ............................... p 212

NASA-CP-2166 ............................... p 182

NASA-CP-2167 ............................... p 176

NASA-CP-2168-VOL-2 ................... p 66

NASA*CP-2168 ............................... p 66

NASA-CP-2169 ............................... p 145

NASA-CP-2170-PT-1 ..................... p 29

NASA-CP-2170-PT-2 ..................... p 29

NASA-CP-2171 ............................... p 203

NASA-CP-2172 ............................... p 3

NASA-CP-2173 ............................... p 141

NASA-CP-2174 ............................... p 115

NASA-CP-2175 ............................... p 117

NASA-CP-2176 ............................... p 3

NASA-CP-2177 ............................... p 145

NASA-CP-2178 ............................... p 48

NASA-CP-2179 ............................... p 62

NASAoCP-2180-VOL- 1 ................... p 184

NASA-CP-2180-VOL-2 ................... p 184

NASA-CP-2181 ............................... p 130

NASA-CP-2182 ............................... p 72

NASA-CP-2183 ............................... p 1B

NASA-CP-2184-VOL-2 .................. p 30

NASA-CP-2184 .............................. p 30

NASA-CP-2185 ............................. p 146

NASA-CP-2186 ............................... p 102

NASA-CP-2187 ............................... p 66

NASA-CP-2188 ............................... p 168

NASA-CP-2189 ............................... p 153

NASA-CP-2190 ............................. p 48

NASA-CP-2191 ............................... p 209

NASA-CP-2192 ............................... p 3

NASA-CP-2194 ............................... p 168

NASA-CP-2195 ............................... p 14I

NASA-CP-2196 ............................... p 65

NASA-CP-2197 ............................... p 141

NASA-CP-2198 ............................... p 141

NASA-CP-2199 ............................... p 72

NASA-CP-2200 ............................... p 163

NASA-CP-2201 ............................... p 182

NASA-CP-2202 ............................... p 182

NASA-CP-2203-PT- 1 ..................... p 197

NASA-CP-2203-PT-2 .................. p 197

NASA-CP-2204 ............................... p 164

N80-25224

N80-22788

N80-22327

N80-23495

N80-21927

N80-29096

N80-23008

N80-24648

N80-23956

N80-29706

N80-27866

N80-28150

N80-26125

N81-12090

N80-29652

N80-29672

N81-14555

N80-26999

N81-16533

N80-28436

N83-17115

N80-31449

N80-28965

N80-29300

N82-11489

N80-32756

N81-21440

N81-12978

N81-14138

N80-33782

N81-11070

N81-19511

N80-33465

N81-32564

N82-20884

N81-19709

N81-11644

N81-16119

N8t-10637

N81-14944

N81-14690

N81-15702

N81-1919_

N81-19164

N81-17531

N81-19035

N81-19056

N81-25893

N81-19001

N83-21419

N81-23432

N81-27467

N81-21999

N81-21493

N81-24063

N81-19144

N81-30889

N81-29902

N81-22388

N82-14213

N81-31130

N82-13123

N81-30101

N82-23684

N81-26372

N81-26166

N82-10661

N82-10624

N81-31196

N82-17014

N82-21139

N81-31801

N82-22546

N82-15095

N83-17942

N83-19141

N82-12109

N82-12715

N81-33856

N81-33879

N82-14960

N82-15986

N82-16660

C-1
NASA-CP-2205 REPORT NUMBER INDEX

NASA-CP-2205 ....................p 62 N82-10064

NASA-CP-2206 .....................p 180 N82-14829

NASA-CP-2207 .................p 194 N82-15894

NASA-CP-2208 .....................p4 N84-27660

NASA-CP-2209 ........................p3 N82-19134

NASA-CP-2210 ..........................p 123 N83-20119

NASA-CP-2211 .......................p 24 N84-27686

NASA-CP-2212 ......................p 115 N82-15383

NASA-CP-2213 .....................p 77 N52-21254

NASA-CP-2214 .....................p 117 N82-18578

NASA-CP*2215-PT1 ................p 65 N82-18275

NASA.CPo2215-PT-2 ...............p 66 N82-19257

NASA-CP-2216 .............................p 109 N82-23473

NASA-CP*2217 ........................p 102 N52-20402

NASA-CP-2218 .........................p 19 N82-20149

NASA-CP-2219 .............................p 30 N82-23208

NASA-CP-2220 ...................p 118 N82-20494

NASA-CP-2221 .......................p 99 N82-23344

NASA-CP-2222 .............................p 179 N82-24545

NASA-CP-2223-VOL-1 .............p 207 N82-25043

NASA-CP-2223oVOL-2 ...............p 207 N82-26134

NASA-CP-2224 .......................p3 N82-26199

NASA-CP-2225 .........................p 19 N82-25196

NASA-CP-2226 ......................p 82 N82-26330

NASA-CP-2227 .....................p 164 N82-24781

NASA-CP-2228 .....................p 115 N82-27706

NASA-CP-2229 ......................p 73 N82-25291

NASA-CP-2230 .....................p 146 N83-19231

NASA-CP-2231 .........................p 173 N82-24834

NASA-CP-2232 ..........................p 173 N82-24835

NASA-CP-2233 ....................p 173 N82-24836

NASA-CP-2234 ...................p 190 N84-29662

NASA-CP-2235 .....................p t53 N82-29796

NASA-CP-2236 ......................p 176 N82-26996

NASA-CP-2237 ....................p 115 N82-26637

NASA-CP-2238 ........................p 201 N82-31163

NASA-CP-2239 ......................p 210 N82-33320

NASA-CP-2240 ......................p 136 N83-11534

NASAoCP-2241 ........................p 188 N82-31070

NASA-CP-2242 .......................p 189 N83-10883

NASA-CP-2243 .....................p 116 N82-32663

NASA-CP-2244 .......................p 202 N82-33296

NASA-CP-2245 .....................p 131 N82-33739

NASA-CP-2246 ....................p 173 N83-18236

NASA-CP-2247 ......................p 174 N83-30016

NASA-CP-2248 ..............................p 170 N83-16018

NASA-CP-2249 ...............................p 131 N83-12452

NASA-CP-2250 ................p 122 N83-15629

NASA-CP-2251 ...............................p 79 N83-12147

NASA-CP-2253 ....................p 165 N63-24028

NASA-CP-2254 ..............................p 197 N83-18559

NASA-CP-2255 .........................p 76 N63-15348

NASA-CP-2256 ..............................p t46 N83-15806

NASA-CP-2257 ..............................p 164 N83-14825

NASA-CP-2258 ...............................p 66 N83-18619

NASA-CP-2259 ..................p 165 N83-1939t

NASA-CP-2260-VOL-1 ................p 142 N85-1t404

NASA-CP-2260-VOL-2 ................p 142 N85-11405

NASA-CP-2260-VOL-3 ............p 142 N83-28508

NASA-CP-2261-VOL-1 ................p 141 N83-26155

NASA-CP-2261-VOL-2 ...............p 142 N63-26176

NASA-CP-2262 .............................p 59 N83-18748

NASA-CP-2263 .......................p 102 N83-35230

NASA-CP-2264 ...........................p 131 N83-21391

NASA-CP-2265 ........................p 118 N83-35351

NASA-CP-2266 ...................p 67 N83-22256

NASA-CP-2267 ....................p 97 N83-22442

NASA-CP-2268 ...............................p 50 N83-29208

NASA-CP-2269-PT-1 .............p 67 N83-26853

NASA-CP-2269-PT-2 ...............p 67 N83-26879

NASA-CP-2270 .....................p 165 N83-25265

NASA-CP-2271 ....................... t3 132 N83-34351

NASA-CP-2272 ......................p 177 N84-22179

NASA-CP-2273 ..............................p 13t N83-24681

NASA-CP-2274 .......................p4 N83-33627

NASA-CP-2275-VOL-1 ............p 202 N84-28709

NASA-CP-2275-VOL-2 .............p 202 N83-27939

NASA-CP-2275-VOL-3 ............p 202 N84-32318

NASA-CP-2276 .J .................p 79 N83-24556

NASA-CP-2277 ..............................p 57 N83-33896

NASA-CP-2278 ................p 82 N83-33957

NASA-CP-2279 .....................p4 N84-12029

NASA-CP-2280 ........................p 209 N84-13067

NASA-CP-2261 .......................p 165 N83-33494

NASA-CP-2282 .......................p 50 N84-10055

NASA-CP-2283-PT-t ..............p 69 N84-I0115

NASA-CP-2283-PT-2 ............p 69 N84-10144

NASA-CP-2284 ......................p 132 N84-1559(}

NASA-CP-2285 ...................p4 N84-t1099

NASA-CP-2286 ..........................p 169 N64-1t720

NASA-CP-2287 .....................p 99 N84-15327

NASA-CP-2288 ....................P 165 N83-36587

NASA-CP-2289 ...................p 135 N86-1t496

NASA-CP-2290 .....................p 77 N84-12228

NASA-CP-2292 ...................p 154 N84-13706

NASA-CP-2293p 67 NS_ t8277

NASA-CP-2294 ....................p 67

NASA-CP-2295 ...................p 179

NASA-CP-2296 .....................p 58

NASA-CP-2297 ....................p 133

NASA-CP-2298 ......................p 52

NASA-CP-2299 .....................p 169

NASA-CP-2300-VOL-1 .............p 124

NASA-CP-23CO-VOL-2 ............p 124

NASA-CP-2301 ....................p 180

NASA-CP-2302 ....................p 194

NASA-CP-2303 ....................p 142

NASA-CP-2304 .....................p 198

NASA-CP-2305 .....................p 136

NASA-CP-2306 ....................p 40

NASA-CP-2307 .............................p 51

NASA-CP-2309 .....................p 51

NASA-CP-2310 .....................p 209

NASA-CP-231t ....................p 133

NASA-CP-2312 .....................p 137

NASA-CP-2313 .......................p 63

NASA-CP-2314 .....................p 146

NASA-CP-2316 ...............................p 169

NASA-CP-2317 .....................p 116

NASA-CP-2318 ....................p 154

NASA-CP-2319 ......................p 25

NASA-CP-2320 ....................p 137

NASA-CP-2321 .....................p 83

NASA-CP-2323 .........................p 198

NASA-CP-2324 .........................p 63

NASA-CP-2325 ...............................p 137

NASA-CP-232_VOL-1 ............p 137

NASA-CP-2326-VOL-2 .............p 137

NASA-CP-2328 ................p 133

NASA-CP-2329 .................p 166

NASA-CP-2330 ....................p 208

NASA-CP-2331 ........................p 103

NASA-CP-2332 ...............................p t55

NASA-CP-2333 ....................p 208

NASA-CP-2334 ..........................p 83

NASA-CP-2335 ...........................p 134

NASA-CP-2336 ......................p 169

NASA-CP-2337 .....................p 90

NASA-CP-2338 ...................p 124

NASA-CP-2340 ..............................p 74

NASA-CP-2341-VOL1 ............p 174

NASA-CP-2341-VOL-2 ..................p 174

NASA-CP-2342-PT-1 ..............p 63

NASA-CP-2342-PT-2 ..............p 63

NASA-CP-2343-PT-1 .................p 208

NASA-CP-2343-PT-2 .................p 208

NASA-CP-2344 .......................p 166

NASA-CP-2345 ..................p 204

NASA-CP-2346 ......................p 78

NASA-CP-2347 ..................

NASA-CP-2348 .............

NASA-CP-2349 ...........................

NASA-CP-2350 ...................

NASA-CP-235,1 ...................

NASA-CP-2352 ....................

NASA-CP-2353 .......................

NASA-CP-2355-VOL-1 ..............

NASA-CP-2355-VOL-2-PT1 ......

NASA-CP-2355-VOL-3-PT-2 .....

NASA-CP-2355-VOL-4 ..............

NASA-CP-2356 ....................

NASA-CP-2358 ......................

NASA-CP-2359 ...............................

NASA-CP-2360 ...........................

NASA-CP-2361 ............................

NASA-CP-2362 ................

NASA-CP-2363 .....................

NASA-CP-2364 ....................

NASA-CP-2365 .........................

NASA-CP-2366 .............................

NASA-CP-2367 ........................

NASA-CP-2368-PT1 .................

NASA-CP-2368-PT-2 ..............

NASA-CP-2369 ..............................

NASA-CP-2370 .........................

NASA-CP-2371 ..................

NASA-CP-2372 .........................

NASA-CP-2373 ..............................

NASA-CP-2374 ............................

NASA-CP-2376-VOL-10 ..............

NASA-CP-2376-VOL1 ..............

NASA-CP-2376-VOL-2 ...................

NASA-CP-2376-VOL-3 ...........

NASA-CP-2376-VOL-4 ...............

NASA-CP-2376-VOL-5 ............

NASA-CP-2376-VOL-6 ...................

NASA-CP-2375-VOL-7 ............

NASA-CP-2376-VOL-8 .....

NASA-CP-2376-VOL-9 ..........

NASA-CP-2376

NASA-CP-2377 .............................

NASA-CP-2378 ....................

p 67 P 30

203

203

p31 p 78 i 202

143

3 143 3 143 3 143

3166

200

3 75 3 63 3 179 3 137 3 143 3 125 3 125 3 125 3 169 3 87

968

134

3 174 3 134 ) 78 ) 134 ) 210

)211

)210 ) 210

211

210

211

211

211

211

211

210

179

174

N84-17211

N84-20208

N84-20567

N84-31668

N86-25342

N84-18829

N84-23891

N84-25047

N64-22299

N84-22402

N84-27262

N84-21403

N84-18716

N85-10044

N84-23630

N84-20525

N84-27635

N84-25078

N85-32357

N85-11011

N84-29307

N84-30665

N84-28020

N84-32952

N85-12011

N84-28131

N84-29969

N84-33266

N84-27758

N84-30475

N84-30359

N84-30380

N84-32864

N84-34829

N85-11927

N84-33668

N85-14336

N84-34363

N85-12941

N85-10377

N85-26054

N84-34589

N85-14116

N84-34468

N85-14487

N85-14535

N85-16889

N85-16937

N84-34366

N84-34376

N85-14360

N85-15539

N85-13850

N85-16989

N85o18009

N85-20961

N85-17892

N85-14806

N85-13880

N85-17848

N85-20496

N85-20508

N85-21724

N85-23186

N85-16343

N85-17755

N85-22470

N85-21188

N85-20689

N85o23112

N85-23223

N85-20339

N85-20361

N85-21659

N85-26028

N85-23813

N85-23840

N85-31530

N85-24733

N85-33512

N85-26862

N85-25863

N85-29869

N86-28904

N85-33902

N85-34006

N85-34862

N85-34729

N85-34991

N85-35848

N85-35968

N85-36066

N86-31483

N85-33901

N85-28609

N85.29531

NASA-CP-2379 ..................

NASA-CP-2381 ...............................

NASA-CP-2382 ...............................

NASA-CP-2383 ...........

NASA-CP-2384 .........................

NASA-CP-2365 ..........................

NASA-CP-2386 .........................

NASA-CP-2387 ..........................

NASA-CP-2368 ....................

NASA-CP-2369 ...............................

NASA-CP-2390 ...............................

NASA-CP-2391 ............

NASA-CP-2392 ..............................

NASA-CP*2393 ......................

NASA-CP-2394 ..............................

NASA-CP-2395 .....................

NASA-CP-2396 ...........................

NASA-CP-2400 .....................

NASA-CP-2401 ...................

NASA-CPo2403 ......................

NASA-CP-2404 ...............................

NASA-CP-2408 ......................

NASA-CP-2409 .....................

NASA-CP-2410 .......................

NASA-CP-2411 .....................

NASA-CP-2414 ........................

NASA-CP-2416-VOL1 ................

NASA-CP-2419 ...............................

NASA-CP-2421,. ..........................

NASA-CP-2422oVOL1 ..............

NASA-CP-2422-VOL-2 ............

NASA-CP-2422 .......................

NASA-CP-2424 ........................

NASA-CP-2425 .......................

NASA-CP-2428 ........................

NASA-CP-2430 .....................

177 N85-28563

78 N85-27941

103 N85-31371

126 N86-22962

203 N86-12168

83 N86-11260

113 N85-31433

79 N86-11227

166 N86-11735

137 N86-29301

155 N86-12852

) 201 N86-13239

96 N86-28194

116 N86-11437

180 N86-23314

) 135 N86-21933 ) 192 N86-13064 ) 38 N86-15280 ) 63 N86-27297 ) 201 N86-23493 ) 190 N86-12007 ) 146 N86-17839

126 N86-30160

167 N86-24082

3 76 N86-19349 ) 70 N86-23620 ) 28 N86-27190 ) 135 N86-25823

210 N86-24614

) 126 N86-28407 3 126 N86-27644

,126 N86-25794

) 201 N86-27136 3 175 N86-26844

,174 N86-32976

) 137 N66-29282

NASA-RP-1001 .........................p 171 N79-25753

NASA-RP-1002 .....................p 79 N78-11200

NASA-RP-1003 .....................p 197 N78-12895

NASA-RP-1005 .......................p 158 N77-30705

NASA-RP-1006 ...............................p 86 N78-15236

NASA-RP-1007 ....................p 205 N78-20042

NASA-FIP-1008 ..............p 29 N78-11024

NASA-RP-IO09 ...................... p64 N78-12113

NASA-RP-1010 .....................p 151 N77-31694

NASA-RP-1011 ....................... pB4 N78-16119

NASA-RP-1012 ...............................p 167 N78-12644

NASA-RP-1013 .......................p 96 N78-13234

NASA-RP-1015 ...........................p 137 N78-15549

NASA-RP-1016 ..............................p 138 N78-21568

NASA-RP-1017 ......................p 158 N78-18630

NASA-RP-1019 .................p 178 N78-33791

NASA-RP-1020 ............................p1 N78-25048

NASA-RP-1021 ...................p 199 N78-21019

NASA-RP-1022 ......................p 151 N79-10634

NASA-RP-1023 ........................p 158 N76-28748

NASA-RP-1024-VOL-2 .............p 172 N79-13711

NASA-RP-1024-VOL-3 ...............p 173 N79-13712

NASA-RP-1024 ..............................p 172 N79-11734

NASA-RP-1025 ...................p 71 N79-27237

NASA-RP-1026 .........................p 159 N78-30774

NASA-RP-1027-VOL-1 ..............p 71 N61-10100

NASA-RP-1027-VOL-2 ...............p 71 N81-10101

NASA-RP-1027-VOL-3 ...............p 71 N81-t 1102

NASA-RP-1028 ...................p 64 N79-20166

NASA-RP-1029 ....................p 179 N81-12760

NASA-RP-t030 ...............................p 199 N79-22980

NASA-RP-1031 .............................p 210 N79-27057

NASA-RP-1032 ......................p 159 N79-19569

NASA-RP-1034 ...................p 160 N79-31885

NASA-RP-1035 ...............................p 107 N79-33438

NASA-RP-1036 ...........................p 199 N79-22979

NASA-RP-1037 ...................p 201 N79-24921

NASA-RP-1038 ......................p 106 N79-22427

NASA-RP-1039 ....................p 139 N80-16405

NASA-RP-1041 ......................p 198 N79-26062

NASA-RP-1042 ......................p2 N79-30139

NASA-RP-1043 .........................p 33 N79-33t91

NASA-RP-1044 ...............................p 160 N80-12661

NASA-RP-1045 ....................p 170 N80-15788

NASA-RP-1046 .......................p 34 N80-24296

NASA-RP-1047 ......................p 146 N79-33611

NASA-RP-1048 ....................p 177 N79-33858

NASA-RP-1049 ..............p 161 N80-14641

NASA-RP-1050 ...............................p 13 N80-15033

NASA-RP- 1051 ............p 97 N80-14257

NASA-RP- 1052 ............p 77 N80-16095

NASA-RP-1053 ................p 161 N80-16682

NASA-RP-1054 .............p 161 N80-16675

NASA-RP-1055 .........................p 173 N80-15821

NASA-RP-1056 ................p 71 NS0-16091

NASA-RP-1057 ..........................p 206 N80-16009

NASA-RP-1058 ..........................p 161 N80-15726

NASA-RP- 1059-REV ..............p 69 N85-19007

NASA-RP-1059 .............p 68 N81-16111

C-2
REPOR T NUMBER INDEX OF POO;:;_ QL,,_LITY NASA-TP- 1027

NASA-RP-1060 ............................... p 2

NASA-RP-1061 ............................... p 80

NASA-RP-1062 ............................... p 153

NASA-RP-1063 ............................... p 16

NASA-RP-1064 ............................... i 149

NASA-RP-1065 ...............................

NASA-RP-1066 ...............................

NASA-RP-1067 ...............................

NASA-RP-1068-VOL-2 ...................

NASA-RP-1068 ...............................

NASA-RP-1069 ...............................

NASA-RP-1070 ...............................

NASA-RP-1071 ...............................

NASA-RP-1072 ...............................

NASA-RP-1073 ..............................

NASA-RP-1074 ...............................

NASA-RP-1075 ...............................

NASA-RP-1076 ...............................

NASA-RP-1077 ...............................

NASA-RP-1078 ...............................

NASA-RP-1079 ...............................

NASA-RP-1080-VOL-1 ...................

NASA-RP- 1080-VOL-2 ...................

NASA-RP-1080-VOL-3 ...................

NASA-RP-1080-VOL-4 ...................

NASA-FIP-1080-VOL-5 ...................

NASA-RP- 1080-VOL-6 ...................

NASA-FIP- 1081 ...............................

NASA-RP- 1082(03) ........................

NASA-RP-1082 ...............................

NASA-RP-1083 ...............................

NASA-RP-1084 ...............................

NASA-RP-1085 ...............................

NASA-RP-1086 ...............................

NASA-RP-1087 ...............................

NASA-RP-1088-VOL-2 ...................

NASA-RP-1089 ...............................

NASA-RP-1090 ...............................

NASA-RP-1091 ...............................

NASA-RP-1092-REV ......................

NASA-RP-1093 ...............................

NASA-RP-1094 ...............................

NASA-RP-1095 ...............................

NASA-RP-1096 ...............................

NASA-RP-1097 ...............................

NASA-RP-1098 ...............................

NASA-RP-1099 ...............................

NASA-RP-1100 ...............................

NASA-RP-1101 ...............................

NASA-RP-1102 ...............................

NASA-RP-1103 ...............................

NASA-RP-1104 ...............................

NASA-RP-1105 ...............................

NASA-RP-1106 ..............................

NASA-RP-1107 ...............................

NASA-RP-1108 ...............................

NASA-RP-1109 ...............................

NASA-RP-1110 ...............................

NASA-RP-1111 ...............................

NASA-RP-1112 ...............................

NASA-RP-1113 ...............................

NASA-RP- 1115 ..............................

NASA-RP- 1116 ...............................

NASA-RP-1117 ...............................

NASA-RP-1118 ...............................

NASA-RP-1119 ...............................

NASA-RP-1120 ...............................

NASA-RP-1121 ...............................

NASA-RP-1122 ...............................

NASA-RP-1123 ...............................

NASA-RP-1124 ...............................

NASA-RP-1125 ...............................

NASA-RP-1126 ..............................

NASA-RP-1127 ........................

NASA-RP 1128 ..............................

NASA-RP- 1129 ...............................

NASA-RP-1131 ..............................

NASA-RP- t t32 .........................

NASA-RP- 1133 ...............................

NASA-RP- 1134 ...............................

NASA-RP- 1135 ...............................

NASA-RP- 1136 ...............................

NASA-RP-1137 ...............................

NASA-RP- 1138 ...............................

NASA-RP-1139 ", ..............................

NASA-RP- 1140 ...............................

NASA-RP-1141 ...............................

NASA-RP-1142 ...............................

NASA-RP- 1143 ...............................

NASA-RP-1144 ......................

NASA-RP-1145 ...............................

NASA-RP-1147 .........................

NASA-RP-1148 .........................

NASA-RP- 1149 ...............................

NASA-RP-1150 ..............................

NASA RP 1151 ..................

t 203

t 139

t t39

207

t 206

209

, 162

162

, 162

b 163

_71

p 116

145

, 183

141

73

_73

73

73

73

73

73

153

, 100

100

168

192

176

140

115

153

133

192

176

82

207

182

164

164

207

154

146

141

116

110

110

77

123

154

154

100

207

67

103

165

99

174

165

24

2O2

202

200

82

103

124

82

74

124

134

190

134

99

60

60

193

37

155

208

185

143

155

155

83

150

155

191

76

155

156

135

166

N80-29245

N80-30441

N81-23742

N81-14973

N81-17622

N81-11970

N81-11438

N81-21437

N82-16028

N81-25012

N81-23004

N81-15640

N81-16678

N81-15639

N81-16679

N81-19218

N82-29579

N81-27622

N81-27865

N83-10458

N82-16153

N82-16147

N82-16148

N82-16149

N82-16150

N82-16151

N82-16152

N82-13592

N83-29491

N82-15270

N82-16683

N82-15853

N82.21907

N82-19647

N82.29577

N82-19734

N84-33832

N83-27809

N82-29904

N83-31730

N83-25636

N85-19733

N82-29826

N82-28880

N83-1203t

N83-16992

N83-14684

N83-23660

N83-28410

N83-24800

N83-22546

N83-24549

N83-27214

N83-27520

N83-28796

N84-13397

N84-32330

N83-32828

N86-14498

N83-28828

N83-32990

N84-29465

N84-16720

N84-27674

N84-26520

N84-26519

N84-34332

N84-23698

N85-13156

N84-27041

N84-26751

N85-11127

N84-31640

N85-10405

N85-11789

N85-11378

N84-33613

N85-18991

N86-18328

N85-27665

N85-33116

N85-19550

N85-21099

N85-19784

N85o30450

N85-25970

N85-27422

N85-26923

N86-16748

N86-11700

N86-24391

N85-30005

N86-13850

N86-23088

N86-10579

N86-13867

NASA-RP-1152 .................... p 125 N86-14612

NASA-RP-1153 ............................ p 58 N86-22579

NASA-RP-1154 ............................... p 125 N86.13734

NASA-RP-1155 ............................... p 204 N86-25307

NASA-RP-1156 ............................... p 157 N86-27839

NASA-RP-1157 ............................... p 194 N86-17140

NASA-RP-1158 .............................. p 166 N86-13866

NASA-RP-1160 .............................. p 156 N86-22022

NASA-RP-1161 .......................... p 126 N86-26639

NASA-RP-1162 ........................ p 156 N86-25911

NASA-RP-1163 ............................... p 157 N86-29425

NASA-RP-1164 ............................... p 157 N86-28562

NASA.RP-1165 .............................. p 157 N86-29428

NASA-RP-1166 ............................... p 156 N86-27835

NASA-RP-1167 ............................ p 156 N86-25900

NASA-RP-1169 ............................... p 167 N86-28574

NASA-RP-1174 ............................... p 126 N86-32763

NASA-SP-221(06) .......................... p 132 N84-18677

NASA-SP.222(06) .......................... p 133 N84-21899

NASA-SP-223(05) .......................... p 130 N81-71594

NASA.SP-224(05) .......................... p 130 N81-71592

NASA-SP-301 ................................. p 6 N77-85474

NASA.SP.345 ................................. p 203 N77-12959

NASA-SP-349 ................................. p 205 N77-28055

NASA-SP-360 ................................. p 138 N80-10537

NASA-SP-362 ................................. p 61 N78-21174

NASA-SP-365-PT-1 ........................ p 151 N78-11545

NASA-SP-365-PT-2 ........................ p 151 N78-11552

NASA-SP-370-PT-1 ........................ p 203 N78-12925

NASA-SP-370-PT-2 ........................ p 203 N78.12958

NASA-SP-377 ................................. p 169 N77-33780

NASA.SP.380 ................................. p 140 N82-12492

NASA.SP-394 ................................. p 6 N78-11007

NASA-SP-398 ................................. p 157 N77-10755

NASA-SP-399 ................................. p 136 N79-17279

NASA-SP-4009-VOL-4 ................... p 98 N80-20437

NASA-SP-400 ................................. p 60 N77-27155

NASA.SP-4011 ............................... p 61 N78-25115

NASA-SP-4019 ............................... p 212 N78-12997

NASA-SP-401 ................................. p 65 N77-29189

NASA-SP-4020 ............................... p 212 N81.16973

NASA-SP-4021 ............................... p 212 N84-25602

NASA-SP-4022 ............................... p 213 N86-31524

NASA-SP-402 ................................. p 209 N79-22991

NASA-SP-403 ................................. p 152 N80-23912

NASA.SP.404 ................................. p 199 N79-34t18

NASA-SP-406 ................................. p 8 N78-24046

NASA-SP-408 ................................. p 70 N76-28296

NASA-SP-409 ................................. p 6 N78-12017

NASA-SP-4102 ............................... p 196 N83-18551

NASA-SP-4103-VOL-1 ................... p 4 N85-23683

NASA-SP-4103-VOL-2 ................... p 4 N85-23684

NASAoSP-410 ................................. p 157 N77-19709

NASA-SP-411 ................................. p 170 N77-30735

NASA-SP-412-VOL-2 ..................... p 138 N80-10538

NASA-SP-412 ................................. p 60 N78o17088

NASA-SP-413 ................................. p 60 N77-21106

NASA-SP-414 ................................. p 175 N77-12718

NASA-SP-415 ................................. p 1 N77-21022

NASA-SP-416 ................................ p 28 N77o18081

NASA-SP-417 .......................... p 204 N77-15961

NASA-SP-418 ................................. p 204 N77-27053

NASA-SP-419 ................................. p 175 N78-18771

NASA-SP-4203 ............................... p 61 N78-20151

NASA-SP-4204 ............................... p 64 N79-12127

NASA-SP-4205 ............................... p 62 N79-28203

NASA-SP-4206 ............................... p 72 N81-29154

NASA-SP-4208 ............................... p 63 N84-25737

NASA-SP-4209 ............................... p 61 N79-10074

NASA-SP-420 ................................. p 205 N77-29046

NASA-SP-4210 ............................... p 65 N78-15149

NASA-SP-4211 ............................... p 200 N81-20962

NASA-SP-4212 ............................... p 208 N84-35248

NASA-SP-4213 .............................. p 170 N86-21097

NASA-SP-421 ................................. p 201 N77-34063

NASA-SP-422 ................................. p 104 N78-13371

NASA-SP-423 ............................... p 205 N78-30025

NASA-SP-424 ................................. p 61 N78-27146

NASA-SP-425 ................................. p 205 N79-12984

NASA-SP-426 ................................. p 209 N79-20961

NASA-SP-427 ................................. p 138 N78-31508

NASA-SP-428 ................................. p 62 N79-32225

NASA-SP-429 ............................... p 207 N81-25992

NASA-SP-4303 ............................. p 4 N85-17934

NASA-SP-4304 ............................. p 213 N86-16185

NASA-SP-430 ................................. p 170 N79-13686

NASA-SP-431 ................................. p 139 N81-20489

NASA-SP-432 ................................. p 68 N80-30367

NASA-SP-433 .............................. p 117 N80-11414

NASA-SP-434 ................................. p 201 N80-11966

NASA-SP-435 ................................. p 34 NS0-18028

NASA-SP-436 ........................... p 206 N80-27260

NASA-SP-437 ......................... p 182 N80-13839

NASA-SP-438 ............................... p 206 N80-16998

NASA-SP-439 ................................ p 206 N81-10910

NASA-SP-4402 ............................... p 211 N77-t6981

NASA-SP-4403 ............................... p 196 N82-14955

NASA-SP-4404 ............................... p 97 N79-16994

NASA-SP-4405 ............................... p 212 N85-35142

NASA-SP-440 ................................. p 59 N81-32153

NASA-SP-441 ................................. p 200 N81-t1966

NASA-SP-442 ................................. p 199 N80-27219

NASA-SP-443 ................................. p 62 N81-16075

NASA-SP-444 ................................. p 206 N80-26239

NASA-SP-445 ................................. p 3 N81-15969

NASA-SP-446 ................................. p 206 N81-15925

NASA-SP-447 ................................. p 170 N83-25349

NASA-SP-448 ................................. p 81 N81-18096

NASA-SP-449 ................................. p 212 N81-21995

NASA-SP-450 ................................. p 203 N81-27008

NASA-SP-451 ................................. p 207 N82-26152

NASA-SP-453 ................................. p 204 N82-21118

NASA-SP-454 ................................. p 66 N82-20225

NASA-SP-455 ................................. p 146 N82-28783

NASA-SP-456 ................................. p 200 N82-25027

NASA-SP-457 ................................. p 165 N83-14835

NASA-SP-458 ................................. p 154 N82-32915

NASA-SP-459 ................................. p 168 N84-10718

NASA-SP-460 ................................. p 36 N83-20931

NASA-SP-461 ................................. p 207 N83-30340

NASA-SP-462 ................................. p 36 N84-15144

NASA-SP-463 ................................. p 204 N83-32693

NASA-SP-464 ................................. p 118 N83-27200

NASA-SP-465 ................................. p 142 N84-14563

NASA-SP-466 ................................. p 202 N84-22516

NASA-SP-467 ................................. p 200 N85-23457

NASA-SP-468 ................................. p 5 N85-32089

NASA-SP-469 ................................. p 200 N85-18888

NASAoSP-470 ................................. p 197 N83-33792

NASA-SP-471 ................................. p 204 N84-19253

NASA-SP-472 ................................. p 4 N85-28912

NASA-SP-473 ................................. p 67 N84-24632

NASA-SP-474 ................................. p 208 N84-35242

NASA-SP-475 ................................. p 208 N85-22323

NASA-SP-476 ................................. p 175 N85-28562

NASA-SP-477 ................................. p 175 N85-32777

NASA-SP-478 ................................. p 169 N85-32708

NASA-SP-479 ................................. p 208 N86-11137

NASA-SP-480 ................................. p 63 N85-33126

NASA-SP-481 ................................. p 196 N85-16665

NASA-SP-482 ................................. p 196 N85-24994

NASA-SP-483 ................................. p 174 N85-32772

NASA-SP-485 ................................. p 38 N86-30720

NASA-SP-7011(280) ...................... p 170 N86-23265

NASA-SP-7011(288) ...................... p 171 N86-32088

NASA-SP-7037(196) ...................... p 5 N86-23552

NASA-SP-7037(204) ...................... p 5 N86-32389

NASA-SP-7038(08) ........................ p 198 N86-26243

NASA-SP-7039(29)-SECT-1 .......... p 198 N86-28788

NASA-SP-7039(29)-SECT-2 .......... p 198 N86-28789

NASA-SP-7041(50) ........................ p 143 N86-31940

NASA-SP-7043(40) ........................ p 146 N84-21977

NASA-SP-7044 ............................... 13144 N77-16437

NASA-SP-7046(t4) ........................ p 63 N86-28104

NASA-SP-7047 ............................... p 197 N83-32671

NASA-SP-7048 .............................. p 197 N83-22010

NASA-SP-7051(SUPPL-2) ............. p 198 N85-t2785

NASA*SP-7053-VOL-1 ................... p 198 N86-20168

NASA-SP-7053-VOL-2 ................... p 198 N86-20169

NASAoSP-7056(02) ........................ p 63 N86-28105

NASA-SP-7200 ............................... p 197 N79-13914

NASA-SP-7500(20) ........................ p 196 N86-27108

NASA-SP-7601-SUPPL-1 ............. p 151 N79-13601

NASA-TP-1001 ........................... p 185 N77-30908

NASA-TP-1002 ............................ p 158 N77-32688

NASA-TP-1003 ............................... p 158 N77-32689

NASA-TP- 1004 ............................... p 46 N80-15129

NASA-TP-1005 ............................... p 144 N77-30617

NASA-TP-1006 ............................. p 178 N78-10746

NASA-TP- 1007 ............................... p 42 N78-16053

NASA-TP-1008 ..................... p 185 N77-30909

NASA-TP-1009 .......................... p 5 N77-33111

NASA-TP-1010 ............................... p 31 N78-10048

NASA-TP-1011 ............................... p 70 N78-13119

NASAoTP-1012 ............................... p 113 N77-32458

NASA-TP-1013 ............................... p 185 N78-12800

NASA-TP-1014 ............................... p 147 N77-32622

NASA-TP-1015 .............................. p 1 N77-32072

NASA-TP-1016 ............................... p 100 N77-30367

NASA-TP-1017 ............................. p 104 N77-30413

NASA-TP-1018 ............................... p 5 N77-30089

NASA-TP-1019 ......................... p 98 N77-30296

NASA-TP-1020 ............................... p 5 N77-33112

NASA-TP-1021 ............................... p 147 N78-13628

NASA-TP-1022 ............................... p 32 N78-16042

NASA-TP-1023 ........................... p 76 N77-32229

NASA-TP-1024 ................ p 111 N84 10504

NASA-TP-1025 ............................... p 31 N78-10049

NASA-TP-1026 ............................... p 199 N77-33003

NASA-TP-1027 ............................... p 7 N78-13016

C-3
NASA-TP-1028 REPORTNUMBERINDEX

NASA-TP-1028 ...............................p 41 N77-31152

NASA-TP*1029 .......................p 104 N77-31441

NASA-TP-1030 ...........................p 118 N77-31502

NASA-TP-1031p 41 N77-31t 53

NASA-TP-1032 ...............................p5 N77-32082

NASA-TP-1033 ...............................p 91 N77-33348

NASA-TP-1034 ...............................p 41 N77-31154

NASA-TP-1035 ...............................p 91 N77-32312

NASA.TP.1036 ...............................p 41 N77-32153

NASA-TP-1037 ...............................p 104 N77-32431

NASA-TP-1038 ..............................p 147 N78-12554

NASA-TP-1039 ...............................p 167 N78-12645

NASA-TP-1040 ...............................p 53 N75-16063

NASA-TP-1041 ...............................p 147 N78-11520

NASA-TP-1042 ...............................p 29 N78-10034

NASA.TP- 1043 ...............................p 53 N78.13071

NASA-TP-1044 ...............................p6 N78-12038

NASA-TP-1045 ...............................p 65 N78-10186

NASA-TP.1046 ..............................p 31 N78-11053

NASA-TP-1047 ...............................p6 N78-12039

NASA.TP.10,48 ..............................p 156 N78-12801

NASA-TP-1049p 91 N78-12223

NASA-TP-1050 ...............................p6 N78-10030

NASA-TP- 1051 ...............................p 33 N80-12084

NASA-TP-1052 ...............................p 85 N77-32286

NASA-TP- 1053 ............................p 91 N77-33350

NASA-TP-1054 ...............................p 104 N77-32432

NASA-TP-1055 ...............................p 100 N78-11301

NASA-TP-1056 ...............................p 41 N77-33169

NASA-TP-1057 ...............................p6 N78-11008

NASA-TP-1058 ...............................p 41 N77-32154

NASA-TP-1059 ..............................p 91 N78-10295

NASA-TP-1060 ...............................p 119 N77-33520

NASA-TP-1061 ...............................p 104 N77-33444

NASA.TP-1062 ...............................p 69 N78-10200

NASA-TP-1064 ...............................p 171 N78-11696

NASA-TP-1065 ...............................p7 N78-14997

NASA-TP-1066 ...............................p 193 N78-12829

NASA-TP.1067 ...............................p 177 N77-33868

NASA-TP-1068 ...............................p 41 N78-tl 10,6

NASA-TP-1069 ...............................p 42 N78-21112

NASA-TP-1070 ...............................p7 N78-13017

NASA-TP-1071 ..............................p 158 N78-116,42

NASA-TP-1072 ...............................p 158 N78-15641

NASA-TP-1073 ...............................p 147 N78-11517

NASA-TP-t074 ...............................p 104 N78-15434

NASA-TP-1075 ...............................p 104 N75-18362

NASA-TP-1076 ..............................p6 N75-12040

NASA-TP-1077 ............................p 168 N79-25863

NASA-TP- 1078 ..............................p6 N78-12041

NASA-TP-1079 ..............................p 127 N78-12475

NASA-TP-1080 ...............................p 32 N78-t3043

NASA-TP-1081 ...............................p 79 N78-13138

NASA-TP-1082 ...............................p 79 N78-15098

NASA-TP-1083 ...............................p 45 N79-28176

NASA-TP-1084 ...............................p 70 N77-33259

NASA-TP-1085 ..............................p 38 N78-13054

NASA-TP-1086 ..............................p 85 N84-11230

NASA-TP-1057 ...............................p 105 N78-26392

NASA-TP-1085 ...............................p 193 N78-11812

NASA-TP-1089 ...............................p 147 N78-12555

NASA-TP-1090 ...............................p6 N78-13014

NASA-TP-1091 ...............................p6 N78-11002

NASA-TP-1092 ...............................p 119 N78-10474

NASA-TP-1093 .............................. 1384 N78-12167

NASA-TP- 1094 ...................p 41 N78-13064

NASA-TP-1095 ...............................p 104 N78-t3379

NASA-TP-1096 ..............................p 91 N78-12222

NASA-TP-1097 ...............................p 86 N78-11230

NASA-TP-1098 ...............................p 75 N78-13124

NASA-TP-1099 ...............................p 113 N78-15463

NASA-TP-1 tO0 ...............................p7 N75-17000

NASA-TP-1101 ...............................p 55 N78-15142

NASA-TP- 1102 ........................p7 N75-16000

NASA-TP-1103 ...............................p 105 N78-22331

NASA-TP-1104 ..........................p 186 N78-17823

NASA-TP- 1105 .............................p 84 N78-22188

NASA-TP-1106 ...........................p 181 N78-22809

NASA-TP-1107 .................p 52 N78-12100

NASA-TP-1108 ...............................p 55 N78-15143

NASA-TP-1109 ..............................p7 N78-16001

NASA-TP-1110 ...............................p 42 N78-22101

NASA-TP-1111 ............................... 13147 N78-15596

NASA-TP-1112 ............................... p29 N78-13029

NASA-TP-1113 ...............................p 113 N78-13408

NASA-TP-1114 .............................. p55 N78-28150

NASA-TP-1115 ...............................p 55 N78-13109

NASA-TP-1116 ...............................p 53 N78-20139

NASA-TP-1117 ............................... p79 N75-18135

NASA-TP-1118 ...............................p 180 N78-18823

NASA-TP-1119 ............................ p7 N78-17997

NASA-TP-1120 ...............................p5 N78-21055

NASA-TP-1121 .......................p 80 N75-20256

NASA-TP-1122 ..........................p7 N78-20078

NASA-TP-1123 ............................p 127 N78-20536

NASA-TP-1124 ..............................p7 N78-20079

NASA-TP-1125 ...............................p 91 N78-15277

NASA-TP-1126 ...............................p7 N78-14998

NASA-TP- 1127 .............................p 65 N78-17127

NASA-TP-1128 ...............................p 85 N78-15229

NASA-TP-1129 ...............................p 91 N78-15278

NASA-TP-1130 ..............................p 119 N78-15429

NASA-TP-1131 ...............................p 56 N75-15230

NASA-TP-1132 ..............................p7 N78-17998

NASA-TP-1133 ...............................p 104 N76-18363

NASA-TP-1134 ...............................p 104 N78-17338

NASA-TP-1135 ...............................p 32 N75-18044

NASA-TP-1136 ..............................p8 N78-20080

NASA-TP-1137 ...............................p 127 N78-18459

NASA-TP-1138 ...............................p 1t7 N75-16354

NASA-TP-1139 ...............................p 104 N75-16326

NASA-TP-1140 ...............................p 53 N75-20143

NASA-TP-1141 ...............................p 191 N78-20927

NASA-TP-1142 ...............................p 98 N78-18252

NASA-TP-1143 ...............................p 105 N78-23389

NASA-TP-1144 ...............................p 193 N78-20948

NASA-TP-1145 ............................... to 70 N78-21200

NASA-TP-1146 ...............................p 38 N78.20128

NASA-TP-1147 ...............................p 53 N78-20142

NASA*TP-1148 ...............................p 53 N78-18076

NASA-TP-1149 ...............................p 113 N78-17360

NASA-TP-1150 ...............................p 119 N78-20512

NASA-TP-1151 ..............................p 42 N78-20130

NASA-TP-1152 ...............................p 75 N78-17145

NASA-TP-1153 ...............................p7 N78-17999

NASA-TP-1154 ...............................p 105 N75-22332

NASA-TP-1155 ...............................p 105 N78-18364

NASA-TP-1156 ...............................p 91 N78-20338

NASA-TP-1157 ...............................p 32 N78.20115

NASA-TP-1158 ...............................p 32 N78-25079

NASA-TP- 1159 .............................p 42 N78-23093

NASA-TP-1160 ...............................p 97 N78-20351

NASA-TP-1151 ...............................p 91 N78-20336

NASA-TP-1162 ...............................p 194 N78-20959

NASA-TP-1163 ...............................p8 N78-20081

NASA.TP-1164 ...............................p 138 N78-18497

NASA-TP-1165 ...............................p 169 N78-15673

NASA-TP-1166 ...............................p 105 N78-22333

NASA-TP-1157 ...............................p 53 N78-20140

NASA-TP-1165 ..............................p 105 N78-21410

NASA-TP-1169 ...............................p 105 N78-20463

NASA-TP-1170 ...............................p 114 N78-21430

NASA-TP-1171 ............................... p32 N78-20114

NASA-TP-1172 ...............................p 147 N78-20654

NASA-TP-1173 ..............................p 156 N78-23877

NASA-TP-1174 ...............................p 42 N78-23094

NASA-TP-1175 .............................p8 N78-22028

NASA-TP-1175 ...............................p 106 N78-33385

NASA-TP-1177 ...............................p 65 N78-21193

NASA-TP-1178 ............................... p47 N81-11037

NASA-TP-1179 .............................p 68 N78-20176

NASA-TP-1180 ...............................p 53 N78-21160

NASA-TP-1151 ...............................p 84 N78-23172

NASA-TP-1152 ...............................p 158 N78-23679

NASA-TP-1183 ..............................p8 N78-25055

NASA-TP-1184 ..............................p 53 N78-27138

NASA-TP-1185 ...............................p t14 N75-21431

NASA-TP-1186 ...............................p8 N78-25051

NASA-TP-1187 ..............................p 105 N75-28373

NASA-TP-1188 ..............................p8 N78-26109

NASA-TP-1189 ............................p8 N75-25059

NASA-TP-1190 ...............................p 43 N78-25148

NASA-TP-1191 ...........................p 91 N78-21294

NASA-TP-1192 ...............................p 84 N78-20281

NASA-TP-1193 ...............................p 86 N78-21269

NASA-TP-1194 ...............................p 42 N78-20131

NASA-TP-1195 ...............................p 42 N78-21113

NASA-TP-1196 ..............................p 119 N78-20513

NASA-TP-1197 ...............................p 91 N78-20337

NASA-TP-t198 ...............................p 92 N78-21295

NASA-TP-1199 ...............................p 42 N78-20132

NASA-TP-1200 ...............................p 178 N78-20805

NASA-TP-1201 ...............................p 194 N78-21922

NASA-TP-1202 ...............................p 119 N78-21473

NASA-TP-1203 ...............................p 119 N78-21470

NASA-TP- 1204 ...............................p 42 N78-20133

NASA-TP-1205 ...........................p 42 N78-21114

NASA-TP- 1206 ............................p 53 N78-27136

NASA-TP-1207 ..........................p 105 N78-30554

NASA-TP-1208 ...............................p 106 N78-32385

NASA-TF'-1209 ............................... to 167 N78-21737

NASA*TP-1210 ...............................p 127 N78-26494

NASA-TP-t211 ...............................p 127 N78-28480

NASA-TP-1212 ............................p 151 N78-21690

NASA-TP-1213 ..........p8 N78-28055

NASA-TP-1214 ...............................p 32 N78-30089

NASA-TP-1215 .............................p8 N78-25060

NASA-TP-1216 ......................p 32 N78-30090

NASA-TP-1217 ...............................p 101 N79-14309

NASA-TP-t218 .................p 78 N78-21216

NASA-TP-t219-VOL-1 ..................p 70 N78-25123

NASA-TP-1219-VOL-2 ...................p 70 N78-25124

NASA-TP-1220 ....................p 92 N78-22233

NASA-TP-1221 ...............................p 54 N79-13057

NASA-TP- t222 ...............................p 54 N79-t7872

NASA-TP-1223 .........................p 151 N78-21691

NASA-TP- 1224 ..............................p9 N78-28057

NASA-TP-1225 ...............................p 144 N78-23571

NASA-"1"P-1226 ...............................p9 N78-30052

NASA-'TP-1227 ..............................p 105 N78-23390

NASA-TP-1228 ..............................p 42 N78-23095

NASA-TP-1229 ..............................p 119 N78-25433

NASA-TP-1230 ...............................p 119 N78-22377

NASA-TP-1231 ..............................p 98 N78-22257

NASA-TP-1232 .............................p 127 N78-28481

NASA-TP-1233 ...............................p9 N78-30053

NASA-TP- 1234 ...............................p 53 N78-25101

NASA-TP-1235 ...............................p 193 N78-2790,6

NASA-TP-1235 ...............................p 127 N78-28482

NASA-TP-1237 ...............................p 53 N78-23100

NASA-TP-1235 ...............................p 135 N78-23535

NASA-TP-1239 ...............................p 158 N78-27706

NASA-TP-1240 ...............................p 32 N78-27111

NASA-TP-1241 ...............................p9 N78-30054

NASA-TP-1242 ...............................p 54 N78-30141

NASA-TP-1243 ...............................p 106 N79-14328

NASA-TP-1244 ...............................p8 N78-23056

NASA-TP-1245 ...............................p 144 N78-28624

NASA-TP-1246 ...............................p 92 N78-25215

NASA-TP-1247 ...............................p 97 N78-25236

NASA-TP-1245 ...............................p1 N75-25049

NASA-TP-1249 ..............................p9 N78-30055

NASA-TP-1250 ...............................p 171 N79-19,682

NASA-TP-1251 ..............................p 151 N75-26677

NASA-TP-1252 ..............................p9 N75-31045

NASA-TP-1253 ...............................p9 N78-30056

NASA-TP-1254 ...............................p 53 N75-2615t

NASA-TP-1255 ...............................p 172 N78-31739

NASA-TP-1256 ...............................p 86 N78-26198

NASA-TP-1257 ...............................p 194 N78-26927

NASA-TP-1258 ..............................p 194 N75-30944

NASA-TP-1259 ...............................p 43 N78-28099

NASA-TP-1260 ...............................p 43 N78-27130

NASA-TP-1261 ...............................p 184 N75-30896

NASA-TP-1262 ...............................p 86 N78-26199

NASA-TP-1263 ...............................p 70 N79-15149

NASA-TP-1264 ...............................p 69 N78-28159

NASA-TP-1265 ...............................p 92 N78-28247

NASA-TP-1266 ...............................p 10 N79-14019

NASA-TP-1267 ..............................p 32 N78-27113

NASA-TP-1268 ...............................p 10 N79-12013

NASA-TP-1269 ...............................p 127 N78-32492

NASA-TP-1270 ...............................p9 N78-33051

NASA-TP-1271 ...............................p 105 N78-28374

NASA-TP-1272 ...............................p 119 N78-28457

NASA-TP-1273 ...............................p 119 N78-28458

NASA-TP-1274 ...............................p 86 N78-28225

NASA-TP-1275 ...............................p 147 N78-33617

NASA-TP-1276 ...............................p 38 N78-31101

NASA-TP-1277 ...............................p 114 N78-28412

NASA-TP-1278 ...............................p 45 N79-28177

NASA-TP-1279 ..............................p 86 N78-28226

NASA-TP-1280 ...............................p 147 N78-28682

NASA-TP-1281 ...............................p 87 N79-13138

NASA-TP-1282 ...............................p 182 N78-31836

NASA-TP-1253 ...............................p 171 N78-32717

NASA-TP-1284 ...............................p 106 N78-30555

NASA-TP- 1255 ...............................p 32 N79-14083

NASA-TP-1286 ...............................p 180 N78-30862

NASA-TP-1287 .............................p 119 N78-30585

NASA-TP-1288 ...............................p 127 N75-30610

NASA-TP-1259 ...............................p 108 N81-12356

NASA-TP- 1290 ..............................p 11 N79-16803

NASA-TP-1291 ..............................p9 N78-33050

NASA-TP-1292 .......................p 147 N78-33616

NASA-TP- 1293 ...........................p 92 N78-30238

NASA-TP- t294 .............................p9N 78-30057

NASA-TP-1295 ...............................p 43 N78-33110

NASA-TP-1296 ...............................p 86 N78-30205

NASA-TP-1297 ...............................p 106 N78-31384

NASA-TP-1298 ...............................p 43 N78-33107

NASA-TP-1299 ...............................p 10 N79-10022

NASA-TP-1300 ...............................p 178 N79-17580

NASA-TP-1301 ..............................p 187 N79-22849

NASA-TP-1302 ...............................p 106 N79-13305

NASA-TP-1303 ...............................p 33 N79-15938

NASA-TP-1304 .........................p 106 N79-10379

NASA-TP-1305 ..............................p 68 N78-33135

NASA-TP-1306 ...............................p 11 N79-20071

NASA-TP-1307 .............................p 159 N79-13644

NASA-'I'P-1308 ...............................p 86 N78-31213

NASA-TP-1309 ............................p 86 N78-30206

NASA-TP-1310 ...............................p 43 N78-31109

NASA-TP-1311 ...............................p 183 N78-31854

NASA-TP.1312 ...............................p 84 N79-12178

NASA-TP-1313 ...............................p 172 N78-31740

NASA-TP-1314 ...............................p 43 N78-33109

NASA-TP-1315 ...............................p 117 N78-31413

C-4
REPORTNUMBERINDEX NASA-TP-1605

NASA-TP-1316 ...............................p9

NASA-TP-1317 ...............................p 106

NASA-TP-1318 ...............................p 84

NASA-TP-1319 ...........................p 59

NASA-TP-1320 .........................p 195

NASA-TP-1321 ...............................p 186

NASA-TP-1322 ..............................p 43

NASA-TP- 1323 ...............................p 44

NASA-TP-1324 ...............................p 10

NASA-TP- 1325 ...............................p 186

NASA-TP-1326 ...............................p 166

NASA-TP-1327 ...............................p 136

NASA-TP- 1328 ...............................p 159

NASA-TP-1330 ...............................p 12

NASA-TP-1331 ...............................p 10

NASA-TP-1332 ...............................p 54

NASA-TP-1333 ..............................._ 205

NASA-TP- 1334 .............................

NASA-TP-1335 ..............................

NASA-TP-1336 ...............................

NASA-TP-1337 ...............................

NASA-TP-1338 ...............................

NASA-TP-1339 ...............................

NASA-TP-1340 ...............................

NASA-TP-1341 ...............................

NASA-TP-1342 ...............................

NASA-TP-1343 ...............................

NASA-TP-1344 ...............................

NASA-TP-1345 ...............................

NASA-TP-1346 ...............................

NASA-TP-1347 ..............................

NASA-TP-1348 ..............................

NASA-TP-1349 ...............................

NASA-TP-1350 ...............................

NASA-TP-1351 ...............................

NASA-TP-1352 ...............................

NASA-TP-1353 ...............................

NASA-TP-1354 ...............................

NASA-TP-1355 ...............................

NASA-TP-1356 ...............................

NASA-TP-1357 ...............................

NASA-TP-1358 ...............................

NASA-TP-1359 ...............................

NASA-TP- 1360 ...............................

NASA-TP-1361 ...............................

NASA-TP- 1362 ...............................

NASA-TP- 1363 ...............................

NASA-TP-1364 ...............................

NASA-TP- 1365 ...............................

NASA-TP- 1366 ...............................

NASA-TP- 1367 ...............................

NASA-TP- 1368 ...............................

NASA-TP- 1369 ..............................

NASA-TP- 1370 ...............................

NASA-TP-1371 ...............................

NASA-TP- 1372 ...............................

NASA-TP-1373 ...............................

NASA-TP- 1374 ...............................

NASA-TP-1375 ...............................

NASA-TP-1376 ...............................

NASA-TP-1377 ...............................

NASA-TP-1378 ...............................

NASA-TP- 1379 ...............................

NASA-TP-1380 ...................

NASA-TP-1381 ..............................

NASA-TP-1382 .............................

NASA-TP- 1383 .......................

NASA-TP-1384 ...............................

NASA-TP-1385 ...............................

NASA-TP-1386 ............................

NASA-TP- 1387 ...............................

NASA-TP-1388 ..............................

NASA-TP-1389 ...............................

NASA-TP- 1390 ............................

NASA-TP-1391 ..............................

NASA-TP- 1392 ........................

NASA-TP- 1393 ...............................

NASA-TP-1394 ...............................

NASA-TP-1395 ...............................

NASA-TP-1396 ...............................

NASA-TP-1397 ...............................

NASA-TP- 1398 ..............................

NASA-TP-1399 ..........................

NASA-TP- 1400 ..........................

NASA-TP-1401 ...............................

NASA-TP-1402 ...............................

NASA-TP-1404 ...............................

NASA-TP-1405 .............................

NASA-TP- 1406 ...........................

NASA-TP-1407 ...............................

NASA-TP-1408 .............................

NASA-TP-1409 ...............................

NASA-TP-1410 ..............................

NASA-TP-1411 ...............................

NASA-TP-1412 ...............................

NASA-TP-1413 ..............................

148

186

#10 # 43 # 43

120 i 148

87

3 119 3 92 3 69

310 3 120 3 195

310 3 87 3 54

310

311

911 3 159

310 3 106 ) 152

910 3 159 ) 57 3 186 ) 160 ) 160 ) 196

:)32 3 186 ) 126 ) 54 ) 106

)11 3 138

:)43

:)43 ) 171

:)11 ) 100

392 3 120

392

10

152

92

87

11

12

186

120 2

159

120

106

120

44

120

106

11

54

159

44

11

148

160

152

68

11

78

152

44

69

195

186

120

N78-32067

N79-14327

N79-14177

N79-16877

N79-13901

N79-14874

N79-13046

N79-14098

N79-14018

N79-13821

N79-14872

N76-33499

N78-32641

N80-10101

N78-33053

N79-14110

N79-14978

N79-14591

N79-18687

N78-33054

N78-33108

N79-10060

N79-10425

N78-33618

N78-33196

N78-33447

N79-13158

N78-33137

N79-13003

N79ot0424

N79-t3866

N79-15000

N79-13137

N79-10068

N79-13002

N79-17808

N79q7809

N79-14680

N79-15902

N79-20344

N79-13607

N79.14023

N79-14679

N82.15075

N79.19613

N79-21721

N79-21720

N79-16709

N79-14082

N79-16641

N79-17264

N79-13056

N79-16287

N79-t8915

N79-13475

N79-13045

N79-13044

N79-22761

N79-15903

N79-14275

N79-15184

N79-13369

N79-13159

N79-14996

N79-17388

N79-21204

N79-16950

N79-17810

N79-22043

N79-20832

N79-14387

N79-16796

N79-14678

N79-14389

N79-18288

N79-t4386

N79-14099

N79-17227

N79-20345

N79-22037

N79o15970

N79o16493

N79-23967

N79-16804

N79-17360

N79-22709

N79-16473

N79-21119

N79-17806

N79-21128

N79-19519

N79-16852

N79-21120

N79-19867

N79-17659

N79-18323

NASA-TP-1414 ...............................p 114 N79-17195

NASA-TP-1415 ...............................p 148 N79-18479

NASA-TP-1416 ...............................p 10t N79-1713g

NASA-TP-1417 ...............................p 196 N7g-19912

NASA-TP-t418 ...............................p 136 N79-22580

NASA-TP-t419 ...............................p 11 N79o22036

NASA-TP-1420 ...............................p 185 N79-18679

NASA-TP-1421 ...............................p 12 N80-10102

NASA-TP-1422 ...............................p 171 N79-23662

NASA-TP-1423 ...............................p 12 N79-23012

NASA-TP-1424 ...............................p 177 N80-16742

NASA-TP-1425 ...............................p 44 N79-25023

NASA-TP-1426 ...............................p 180 N79-21822

NASA-TP-1427 ...............................p 12 N79-23013

NASA-TP-1428 ...............................p 128 N79-25427

NASA-TP-1429 ...............................p 80 N79-23141

NASA-TP-1430 ...............................p 187 N79-24773

NASA-TP-1431 ...............................p 55 N80-15138

NASA-TP-1432 ...............................

NASA-TP-1433 ...............................

NASA-TP-1434 ...............................

NASA-TP-1435 ...............................

NASA-TP-1436 ...............................

NASA-TP-1437 ...............................

NASA-TP-1438 ............................

NASA-TP-1439 ...............................

NASA-TP- 1440 ...............................

NASA-TP-1441 ...............................

NASA-TP-1442 ...............................

NASA-TP-1443 ...............................

NASA-TP-1444 ...............................

NASA-TP- 1445 ...............................

NASA-TP- 1446 ...............................

NASA-TP-1447 ...............................

NASA-TP- 1448 ...............................

NASA-TP- 1449 ...............................

NASA-TP- 1450 ...............................

NASA-TP-1451 ...............................

NASA-TP-1452 ...............................

NASA-TP-1453 ...............................

NASA-TP-1454 ...............................

NASA-TP-1455 ...............................

NASA-TP- 1456 ...............................

NASA-TP-1457 ...............................

NASA-TP-1458 ...............................

NASA-TP-t459 ...............................

NASA-TP-1460 ...............................

NASA-TP-1461 ...............................

NASA-TP-1462 ...............................

NASA-TP-1463 ...............................

NASA-TP-1464 ...............................

NASA-TP-1465 ...............................

NASA-TP-1466 ...............................

NASA-TP-1467 ...............................

NASA-TP-1468 ...............................

NASA-TP-1469 ...............................

NASA-TP-1470 ...............................

NASA-TP-1471 ...............................

NASA-TP-1472 ...............................

NASA-TP-1473 ...............................

NASA-TP-1474 ..............................

NASA-TP-1475 ...............................

NASA-TP-1476 ...............................

NASA-TP-1477 ..............................

NASA-TP-1478 ...............................

NASA-TP-1479 ..............................

NASA-TP-1480 ...............................

NASA*TP-1481 ...............................

NASA-TP-1482 ..............................

NASA-TP-t483 ...............................

NASA-TP-1484 ...............................

NASA-TP-1485 ...............................

NASA-TP-1486 ...............................

NASA-TP-1487 ..............................

NASA-TP-1488 ..............................

NASA-TP-1489 ..............................

NASA-TP-1490 .............................

NASA-TP-1491 ...............................

NASA-TP-1492 ...............................

NASA-TP-1493 ...............................

NASA-TP-1494 ......................

NASA-TP-1495 ...............................

NASA-TP-1496 ...............................

NASA-TP-1497 .............................

NASA-TP- 1498 .............................

NASA-TP- 1499 ...............................

NASA-TP- 1500 ...............................

NASA-TP- 1501 ...............................

NASA-TP- 1502 ...............................

NASA-TP- 1503 ...............................

NASA-TP- 1504 ...............................

NASA-TP- 1505 .............................

NASA-TP- 1506 ..........................

NASA-TP-1507 .............................

NASA-TP- 1508 ...............................

NASA-TP-1509 ...........................

,187 N80-11869

_148 N79-28796 # 12 N79-26020

33 N79-30176

3 54 N79-29195 D 92 N79-21205

,120 N79-22516 D 84 N79-22246

,144 N79-22626

,178 N79-21798

3 87 N79-21184

120 N79-22619

3 114 N79-21329

80 N79-28234

3 168 N79-28864

,128 N79-24372

3 84 N80-13191

,101 N79-22375

3 78 N79-22194

148 N79-22654

3 44 N79-22099 3 12 N79-24961 3 160 N79-22708 3 t07 N79-30518 3 77 N79-23132 3 45 N79-29192 3 120 N79-31604 3 54 N79-22113 3 87 N79-28288 3 191 N79-25861 3 92 N79-23216 3 44 N79-23086

152 N79-31864

3 107 N79-30516

178 N79-23688

38 N79-23081

12 N79-26022

60 N79-23140 2 N79-23008

128 N79-28614

84 N79-28259

59 N79-29199

80 N79-29241

44 N79-25022

84 N79-2518t

128 N80-10512

148 N79-32743

148 N79-32744

168 N79-31690

126 N60-11505

44 N79-26057

45 N79-30191

107 N79-29468

101 N78-27400

101 N79-28420

97 N79-28350

54 N79-28166

92 N79-27308

93 N79-27309

44 N79-27142

107 N79-29467

45 N79-27143

54 N79-27182

33 N79-29171

80 N79-32277

107 N79-33441

16 N81-12015

38 N79-33201

12 N80-10105 2 N80-11028

45 N79-31213

12 N79-29146

148 N79-29679

187 N79-32057

107 N79-32500

128 N79-31626

54 N79-31223

93 N79-29327

NASA-TP-1510 ...............................p 45 N79-31214

NASA-TP-1511 ...............................p 121 N79-31605

NASA-TP-1512 ...............................p 55 N80-19126

NASA-TP-1513 ...............................p 55 N80-17081

NASA-TP-1514 ...............................p 33 N80-11068

NASA-TP-1515 ...............................p 13 N80-16032

NASA-TP- 1516 ...............................p 14 N80-17986

NASA-TP-1517 ...............................p 107 N80-20527

NASA-TP-1516 ...............................p 176 N79-33855

NASA-TP-1519 ...............................p 55 N79-33218

NASA-TP-1520 ...............................p 33 N79-33189

NASA-TP-1521 ...............................p 13 N80-11036

NASA-TP-1522 ...............................p 128 N79-33500

NASA-TP-1523 ...............................p 45 N79-33210

NASA-TP-1524 ...............................p 93 N79-30361

NASA-TP-1525 ...............................p 93 N79-30380

NASA-TP-1526 ...............................p 148 N79-31841

NASA-TP-1527 ...............................p 101 N79-32467

NASA-TP-1528 ...............................p 177 N79-30947

NASA-TP-1529 ...............................p 148 N79-30844

NASA-TP-1530 ...............................p 121 N79-33475

NASA-TP-1531 ...............................p 45 N80-14123

NASA-TP-1532 ...............................p 46 N80-14124

NASA-TP-1533 ...............................p 12 N79-33t64

NASA-TP-1534 ...............................p 128 N80-12438

NASA-TP-1535 ...............................p 13 N80-12994

NASA-TP-1536 ...............................p 13 N60-12995

NASA-TP-1537 ...............................p 33 N80-10193

NASA-TP-1538 ...............................p 55 N80-14136

NASA-TP-1539 ...............................p 13 N80-12065

NASA-TP-1540 ...............................p 33 N80-13024

NASA-TP-1541 ...............................p 33 N80-11068

NASA-TP-1542 ...............................p 121 N7_32552

NASA-TP-1543 ...............................p 47 N80o33409

NASA-TP-1544 ...............................p 93 N79-32359

NASA-TP-1545 ...............................p 79 N78-31346

NASA-TP-1546 ...............................p 45 N80-11087

NASA-TP-1847 ...............................p 121 N79-33476

NASA-TP-1548 ...............................p 160 N79-32796

NASA-TP-1549 ...............................p 13 N80-11035

NASA-TP-1550 ...............................p 39 N80-28349

NASA-TP-1551 ...............................p 56 N81-11044

NASA-TP-1552 ...............................p 13 N80-12064

NASA-TP-1553 ...............................p 139 N80-15535

NASA-TP-1554 ...............................p 64 N80-13135

NASA-TP-1555 ...............................p 33 N80-13025

NASA-TP-1556 ...............................p 45 N80-14121

NASA-TP-1557 ............................... p87 N80-11188

NASA-TP-1558 ...............................p 129 N80-19563

NASA-TP-1559 ...............................p 145 N79-33572

NASA-TP-1580 ...............................p 29 N79-33171

NASA-TP-1561 ...............................p 93 N80-23453

NASA-TP-1562 ...............................p 129 N80-23677

NASA-TP-1563 ...............................p 176 N81-12744

NASA-TP-1564 ...............................p 145 N80-11559

NASA-TP-1565 ...............................p 30 N80-28329

NASA-TP-1566 ...............................p 129 N80-20619

NASA-TP-1567 ...............................p 149 N80-14581

NASA-TP-1568 ...............................p 93 N80-11226

NASA-TP-1569 ...............................p 29 N80-13013

NASA-TP-1570 ...............................p 161 N80-16676

NASA-TP-1571 ...............................p 97 N80-21551

NASA-TP-1572 ...............................p 114 N80-13430

NASA-TP-1573 ...............................p 82 N83-28100

NASA-TP-1574 ...............................p 30 N80-13020

NASA-TP-1575 ...............................p 114 N80-12399

NASA-TP-1576 ...............................p 187 N80-13880

NASA-TP-1577 ...............................p 187 N80-13879

NASA-TP-1578 ...............................p 129 N80-13512

NASA-TP-1579 ...............................p 13 N80-13001

NASA-TP-1580 ...............................p 19 N82-15015

NASA-TP-1581 ...............................p 34 N80-17060

NASA-TP-1582 ...............................p 46 N80-14125

NASA-TP-1583 ...............................p 121 N80-14403

NASA-TP-1584 ...............................p 93 NSO- 17220

NASA-TP*1585 ...............................p 107 N80-17398

NASA-TP-1586 ...............................p 136 N80-15445

NASA-TP-1587 ...............................p 152 N80-13730

NASA-TP-1588 ...............................p 34 N80-21317

NASA-'TP-1589 ...............................p 33 NSO- 13026

NASA-TP-1590 ...............................p 171 N80-13769

NASA-TP-1591 ...............................p 14 N80-22266

NASA-TP-1592 ...............................p 13 N80-13002

NASA-TP- 1593 ...............................p 46 N80-21326

NASA-TP-1594 ...............................p 55 N80-13052

NASA-TP-1595 ...............................p 107 N60-13402

NASA-TP-1596 ...............................p 34 N80-15068

NASA-TP- 1597 ...............................p 46 N80-15128

NASA-TP*1598 ...............................p 107 NB0-17397

NASA-TP-1599 ...............................p 121 N80-15410

NASA-TP-1600 ...............................p 129 N80-15426

NASA-TP-1601 ...............................p 34 N80-15069

NASA-TP-1602 ...............................p2 N80-15028

NASA-TP-1603 ...............................p 107 N80-15361

NASA-TP-1604 ...............................p 87 N80-15234

NASA-TP-1605 ...............................p 85 N80-16118

C-5
NASA-TP-1606 REPORT NUMBER INDEX

NASA-TP- 1606 ............................... p 64 N80-19142

NASA-TP-1607 ............................... p t29 N80-18427

NASA-TP-1608 ............................. p t87 N80-t4840

NASA-TP- 1609 .............................. p 87 N80-16141

NASA-TP-1610 .............................. p 46 N60-17071

NASA-TP-1611 ............................. p 13 N80-14045

NASA-TP-1612 .......................... p {)3 N80-22494

NASA-TP-1613 ............................ p 46 N80-21323

NASA*TP-1614 ......................... p 46 N80-21324

NASA-TP-1615 .............................. p 108 N80-24577

NASA-TP-1617 ............................ p 82 N83-28099

NASA-TP-1618 ............................... p 173 N80-26039

NASA-TP-1619 ............................... p 14 N80-19031

NASA-TP-1620 ............................... p 55 N80-24324

NASA-TP-1621 ............................... p 56 N80-26328

NASA-TP-1622 .............................. p 121 N80-17466

NASA-TP-1623 ........................... p 14 N80-17030

NASA-TP-1624 ............................... p 93 N80-18178

NASA-TP-1625 ............................ p 34 N80-213t8

NASA-TP-1626 ............................... p 14 N80-22261

NASA-TP-1627 ............................... p 14 N80-21280

NASA-TP-1628 ......................... p 14 N80-17984

NASA-TP-1629 ............................. p 161 N80-20986

NASA-TP-1630 ............................... p 187 N80-18882

NASA-TP-1631 ............................... p 59 N80-19131

NASA-TP-1632 ........................ p 14 N80-21279

NASA-TP-1633 ............................... p 14 N80-22262

NASA-TP-1634 ............................... p 55 N80-21336

NASA-TP-1635 ............................. p 171 N80-34099

NASA-TP-1636 .............................. p 56 N80-25345

NASA-TP-1637 ........................ p 55 N80-24323

NASA-TP- 1636 ............................. p 15 N80-24267

NASA-TP-1639 ............................. p 114 N80-22660

NASA-TP-1640 ............................... p 161 N80-22924

NASA-TP-1641 ............................... p 56 N81-19131

NASA-TP-1642 ............................... p 38 N80-23304

NASA-TP-1643 ............................... p 39 N80-32389

NASA-TP-1644 ............................. p 93 N80*21532

NASA-TP-1645 .............................. p 108 N80-22633

NASA-TP-1646 ............................... p 121 N80-19495

NASA-TP-1647 ............................... p 55 N80-22358

NASA-TP- 1648 .............................. p 15 N80-24261

NASA-TP- 1649 ............................... p 55 N80-23326

NASA-TP-1650 ............................. p 2 N80.19022

NASA-TP-1651 ............................... p 162 N80-23934

NASA-TP-1652 ............................ p 108 N80-23600

NASA-TP-1653 ............................... p 129 N80-22737

NASA-TP-1654 ............................... p 161 N80-25039

NASA-TP-1655 ............................... p 106 N80-21702

NASA-TP-1656 ............................... p 15 N80-25296

NASA-TP-1657 .............................. p 121 N80-21753

NASA-TP- 1658 .............................. p 93 N60-22493

NASA-TP-1659 ............................... p 46 N80-21325

NASA-TP-t 660 .............................. p 14 N80-22265

NASA-TP-1661 .............................. p t14 N80-24594

NASA-TP-t662 ............................... p t87 N80-27161

NASA-TP-1663 .............................. p 115 N82-19521

NASA-TP-1664 ............................... p 39 N80-30305

NASA-TP-1665 ............................... p 161 N80-23933

NASA-TP-1666 ............................... p 34 N80-25321

NASA-TP-1667 ............................. p 71 N80-29417

NASA-TP-1668 ............................. p 187 N60°23100

NASA-TP-1669 ............................... p 129 N80-22734

NASA-TP-1670 ............................... p 101 N80-21669

NASA-TP-1671 ............................... p 29 N80-27302

NASA-TP-1672 ............................... p 108 N80-26622

NASA-TP- 1673 ............................... p 85 N80-25392

NASA-TP-1674 ............................... p 82 N63-28096

NASA-TP-1675 ............................... p 36 N82-32350

NASA-TP- 1676 ............................... p 15 N60-28304

NASA-TP-1677 ............................... p 55 N80-23327

NASA-TP-1678 ............................... p 56 N80-29369

NASA-TP-1679 ............................... p 129 N80-27719

NASA-TP-t680 ............................... p 46 N80-25337

NASA-TP-1681 ............................... p 80 N80-27428

NASA-TP-1682 ............................... p 108 N80-25615

NASA-TP-1683 ............................... p 15 N80-27283

NASA-TP-1B84 ............................... p 38 N80-27360

NASA-TP-1685 ............................... p 34 N80-29287

NASA-TP-168B .............................. p 114 N60-25635

NASA-TP-1687 ............................... p 114 N80-24595

NASA-TP-1688 ............................... p 47 N80-25338

NASA-TP-1689 ............................... p 2 N80-29244

NASA-TP-1690 ............................... p 176 N81-27813

NASA-TP-1691 ............................... p 67 N80-32489

NASA-TP-1692 ............................... p 47 N80-25339

NASA-TP-1693 ............................... p 47 N80-28352

NASA-TP-1694 ............................... p 149 N80-27832

NASA-TP-1695 ............................... p 59 N80-31413

NASA-TP-1696 ............................... p 34 N80-25318

NASA-TP-1697 ............................... p 187 N80-32188

NASA-TP-t698 ............................... p 108 N80-33719

NASA-TP-1699 ............................... p 35 N80-30296

NASA-TP-1700 ............................... p 71 N80-32429

NASA-TP-1701 .............................. p 15 N80-32333

NASA-TP-1702 ............................... p 121 N80-27694

NASA-TP-1703 ............................... p 108 N80-32692

NASA-TP-1704 ............................... p 15 N80-29250

NASA-TP-1705 ............................... p 15 N80-27284

NASA-TP-1706 ............................... p 149 N80-28946

NASA-TP-1707 ............................... p81 N81-11115

NASA-TP-1708 ............................... p 47 N81-11038

NASA-TP-1709 ............................... p 115 N80-30716

NASA-TP-1710 ............................... p 122 N81-20423

NASA-TP-1711 .............................. p 173 N81.13636

NASA-TP-1712 ............................... p 149 N80-2991t

NASA-TP-1713 ............................... p 47 N80-32396

NASA*TP-1714 ............................... p 121 N80-29734

NASA-TP-1715 ............................... p 76 N80-28424

NASA-TP-1716 ............................... p 47 N81-12089

NASA-TP-1717 ............................... p 39 N80-33404

NASA-TP-1718 ............................... p 15 N81-10004

NASA-TP-1719 ............................... p 146 N82-32859

NASA-TP-1720 ............................... p 173 N81-13635

NASA-TP-1721 ............................... p 15 N80-33356

NASA-TP-1722 ............................... p 48 N81-19121

NASA-TP-1724 ............................... p 163 N81-22658

NASA-TP-1725 ............................... p 115 N80-30717

NASA-TP-1726 ............................... p 153 N80-33998

NASA-TP-1727 ............................... p 67 N80-33555

NASA-TP-1728 ............................... p 93 N81-11214

NASA-TP-1729 ............................... p 15 N80-33357

NASA-TP-1730 ............................... p 47 N80-33410

NASA-TP-1731 ............................... p 122 N81-14322

NASA-TP-1732 ............................... p 121 N80-33749

NASA-TP-1733 ............................... p 15 N80-32334

NASA-TP-1734 ............................... p 56 N81-12109

NASA-TP-1735 ............................... p 149 N81-11565

NASA-TP- 1736 ............................... p 39 N81-13958

NASA-TP-1737 ............................... p 108 N81-13303

NASAoTP-1738 ............................... p 130 N81-11422

NASA-TP-1739 ............................... p 48 N81-13058

NASA-TP-1740 ............................... p 71 N81-13082

NASA-TP-1741 ............................... p 76 N80-33463

NASA-TP-1742 ............................... p 29 N81-12043

NASA-TP-1743 ............................... p 184 N81-12812

NASA-TP-1744 ............................... p 184 N81-10789

NASA-TP-1745 ............................... p 101 N80-33683

NASA-TP-1746 ..................... p 162 N81-13593

NASA-TP-1747 ............................ p 187 N81-14788

NASA-TP-1748 ............................... p 35 N81-12066

NASA-TP-1749 ............................... p 17 N81-22018

NASA-TP-1750 .............................. p 209 N81-13912

NASA-TP-1751 ............................. p 130 N81-13373

NASA-TP-1752 ............................. p 16 N81-10005

NASA-TP-1753 ............................... p 129 N81-11417

NASA-TP-1754 ............................... p 47 N81-11039

NASA-TP-1755 ............................... p 87 N81-16210

NASA-TP-1756 ............................. p 94 N81-14079

NASA-TP-1757 ............................... p 101 N81-11315

NASA-TP-1758 ............................ p 56 N81-13065

NASA-TP-t759 ............................ p 17 N81-22016

NASA°TP-1760 ............................... p 56 N81-13968

NASA-TP-1761 ............................... p 81 N81-16130

NASA-TP-1762 ............................... p 35 N81-16039

NASA-TP-1763 ............................... p 194 N81-13739

NASA-TP-1764 ............................... p 108 N81-t2361

NASA-TP-1765 ............................... p 56 N81*20082

NASA-TP-1766 ............................... p 16 N81-t4972

NASA-TP-1767 ............................... p 16 N81-12021

NASA-TP-1768 .............................. p 97 N81-24283

NASA-TP-1769 ...............................

NASA-TP-1770 ...............................

NASA-TP-t771 ..............................

NASA-TP-t 772 ...............................

NASA-TP-1773 ...............................

NASA-TP-1775 ...............................

NASA-TP-1776 ..............................

NASA-TP-1777 ...............................

NASA-TP-1778 ...............................

NASA-TP-1779 ...............................

NASA-TP-1780 ...............................

NASA-TP-1781 ...............................

NASA-TP-1782 ...............................

NASA-TP- 1783 ...............................

NASA-TP-1784 ...............................

NASA-TP- 1785 ...............................

NASA-TP- 1786 ...............................

NASA-TP-1787 ...............................

NASA-TP-1788-VOL- 1 ...................

NASA-TP-1788-VOL-2 ...................

NASA-TPo1789 ...............................

NASA-TP-1790 ...............................

NASA-TP-1791 ...............................

NASA-TP-1792 ...............................

NASA-TP-1793 ...............................

NASA-TP-1794 ..............................

NASA-TP-1795 ...............................

NASA-TP- 1796 ...............................

NASA-TP- 1797 ..............................

NASA-TP- 1798 ..............................

NASA-TP- 1799 ...............................

p 16 N81-16977

p 70 N81-18082

D 16 N81-15976

_) 17 N81-22017

35 N81-22039

,130 N81-14343

39 N81-14997

16 N81-14974

16 N81-19019

56 N81-13066

48 N81-16050

87 N81-19273

48 N8t-15000

109 N81-15237

16 N81-13919

81 N81-16129

20 N83-16290

3 N81-13915

163 N81-21686

163 N81-21693

16 N81-t4975

182 N81-22754

109 N81-16417

109 N81°24387

3 N81-14961

85 N81-14017

81 N81-14001

173 N81-17711

35 N81-16040

48 N82-13143

99 N81-20311

NASA-TP-1800 ..........................

NASA-TP-1801 ..........................

NASA-TP- 1802 ..............................

NASA-TP-1803 .............................

NASA-TP- 1804 .....................

NASA-TP-1805 .......................

NASA-TP- 1806 .........

NASA-TP-1807 .............

NASA-TP-1808 ..............

NASA-TP- 1609 ............................

NASA-TP-1810 ..............................

NASA TP-1811 ..........................

NASA-TP-1812 .............................

NASA-TP-1813 ...........................

NASA-TP-1814 ......................

NASA-TP-1815

NASA-TP-1816 ............

NASA-'rP- 1817 ....................

NASA-TP-1818 ..............................

NASA-TP.1819 ......................

NASA-TP-1820 ...........................

NASA-TP-1821 ..............................

NASA-TP- 1822 .........................

NASA-TP-1823 ............

NASA-TP-1824 ................

NASA-TP-1825 ...............

NASA-TP-1826 ............................

NASA-TP-1827 ..........................

NASA-TP-1828 .............................

NASA-TP-1829 ..........................

NASA-TP-1830 ...............................

NASA-TP-1831 .............................

NASA-TP-1832 ...............................

NASA-TP-1833 ..........................

NASA-TP- 1834 ............................

NASA-TP- 1835 ..............................

NASA-TP-1836 ...........................

NASA-TP- t837 ...............................

NASA-TP-1838 ........................

NASA-TP- 1839 ...............................

NASA-TP- 1840 ............................

NASA-TP- 1841 ..........................

NASA-TP- t842 .............................

NASA-TP-1843 ..........................

NASA-TPq 844 .......................

NASA-TP-1845 ..........................

NASA-TP-1846 .............

NASA-TP-1847 ..............................

NASA-TP-1851 .................

NASA-TP- 1852 ..........................

NASA-TP-1853 .........................

NASA-TP- 1854 .............................

NASA-TP-1855 ...........

NASA-TP-1856 ............................

NASA-TP-1857 ...............................

NASA-TP-I858 ............................

NASA-TP-1859 .........................

NASA-TP-1860 ..............................

NASA-TP-1861 .............................

NASA-TP-1862 .....................

NASA-TP-1863 .............

NASA-TP-1864 ..............................

NASA-TP-1865 .....

NASA-TP-1866 ........................

NASA-TP-1867 ...............................

NASA-TP-1868 .............

NASA-TP-1869 ......................

NASA TP 1870 ...........................

NASA-TP-1871 .........................

NASA-TP-1872 ................

NASA-TP- 1873 .............

NASA-TP-1875 ............................

NASA-TP-1876 ..........................

NASA-TP- 1877 ..............................

NASA-TP-1878 ............................

NASA-TP-1879 ...............................

NASA-TP- 1880 ..........................

NASA-TP-1881 ...........................

NASA-TP-1882 ................

NASA-TP-1883 ..........................

NASA-TP-1884 ......................

76 N81-31282

149 N81-24601

72 N6t-21116

17 N81-25040

145 N81-18493

21 N83-30390

48 N81-21077

163 N81-2t685

122 N81-19458

130 N8t-23486

3 48 N81 20076

3 77 N81-20173

3 94 N81-21193

3 94 N81-19300

3 72 N81-25138

3 40 N82-33381

3 188 N81-24854

3 72 N81-25139

3 72 N81-25140

3 176 N81 21775

3 17 N81-21016

3 139 N81-20492

3 140 N82-20617

3 140 N82-20618

3 140 N82-20619

3 t40 N82 20620

,140 N82 20621

,140 N82-20622

3 141 N82-20623

3 t41 N82-20624

3 39 N81-20074

3 102 N81-28352

3 102 N81-30360

3 187 N81-21873

3 77 N81-20176

3 88 N81-20245

3 101 N81-20359

3 17 N81-20026

3 101 N81-22281

3 109 N81-28389

,115 N81-25352

109 N81-24368

3 48 N61 24065

3 149 N81-22587

31 N81-29111

109 N81-23410

3 171 N81-23791

163 N81-23761

179 N82-33020

76 N61-31281

94 N82-16239

39 N61-24058

35 N81-24048

85 N81-27223

17 N61-22019

188 N61-22832

163 N81-23838

70 N81-23182

17 N81-24022

61 N81-24178

130 N81-24471

21 N83-30389

2t N83-30366

18 N81-31t29

81 N81-24179

115 N82-22481

109 N81-31509

178 N81-25690

39 N61-26144

62 N81-26160

77 N81-24167

30 N81-31162

181 N81-3065t

35 N81-30112

17 N81-29095

72 N81-29155

17 N81-29096

17 N81-26078

t22 N82-255t4

94 N61-33293

110 N82-30498

NASA-TP-1885 ..................... p 30 N81-29109

NASA-TP-1886 ......................... p 164 N82-15677

NASA-TP-1887 ........................ p 161 N81-29840

NASA-TP-1886 .......................... p 17 N81-29096

NASA-TP-1889 ........................... p 18 N81-30087

NASA-TP-1890 ............................ p 18 N81-30086

NASA-TP-1891 .................... p 94 N81-27282

NASA-TP-1892 ............................... p 18 N81-30088

NASA-TP-1893 ........................... p 192 N81-27899

NASA-TP-1894 .............................. p 109 N81-29384

NASA-TP.1895 ........................... p 179 N61-33838

NASA-TP-1896 ................... p 97 N81-29246

NASA-TP-1897 .............................. p 115 N81-33452

NASA-TP-1898 ....................... p 188 N81-33945

NASA-TP-1899 ............................ p 94 N61-31366

C-6

.G,,_u_,_AL FACE IS

D£ _.OOR QUALITY,
REPORT NUMBER INDEX NASA-TP-2197

NASA-TP-1900 ...............................p 94 N81-31365

NASA-TP*1901 ...............................p 109 N81-32418

NASA-TPo1902 ...............................p 109 N82-11391

NASA-TP-1903 ...............................p 130 N82-11488

NASA-TP-1904 ...............................p 188 N81-33946

NASA-TP-1905 ...............................p 18 N82-12035

NASA-TP-1906 ...............................p 195 N82-32186

NASA-TP-1907 ...............................p 195 N82-32187

NASA-TP-1908 ...............................p 195 N82-32188

NASA-TP-1909 ...............................p 195 N82-32189

NASA-TP-1910 ...............................p 24 N84-27682

NASA-TP-1911 ...............................p 57 N82-20187

NASA-TP-1912 ...............................p 77 N81-33231

NASA-TP-t913 ...............................p 188 N81-33947

NASA-TP-1914 ...............................p3 N82-11013

NASA-TP-1915 ...............................p 39 N81-33203

NASA*TP-1916 ...............................p 56 N82-10041

NASA-TP-1917 ...............................p 130 N82-10430

NASA*TP-1918 ...............................p 35 N82-11050

NASA-TP-1919 ...............................p 18 N82-11033

NASA-TP-1920 ...............................p 18 N81-31128

NASA-TP-1921 ...............................p 35 N81-31185

NASA-TP-1922 ...............................p 153 N82-12687

NASA-TP-1923 ...............................p 59 N82-11090

NASA-TP-1924 ...............................p 164 N82-13620

NASA-TP-1925 ...............................p 94 N81-33292

NASA-TP-1926 ...............................p 18 N82-13107

NASA-TP-1927 ...............................p 35 N82-16068

NASA-TP-1928 ...............................p 109 N82-13383

NASA-TP-1929 ...............................p 196 N83-23189

NASA-TP-1930 ...............................p 196 N83-23188

NASA-TP-1931 ...............................p 22 N83-32774

NASA-TP-1932 ...............................p 178 N82-11784

NASA-TP-1933 ...............................p 72 N82-15116

NASA-TP-1934 ...............................p 18 N82-11032

NASA-TP-1935 ...............................p 117 N82-12431

NASA-TP-1936 ...............................p 172 N82-14804

NASA-TP-1937 ...............................p 72 N82-14276

NASA-TP-1938 ...............................p 149 N82-t2654

NASA-TP-1939 ...............................p 77 N82-11109

NASA-TP-1940 ...............................p 48 N82-13142

NASA-TP-1941 ...............................p 140 N82-13468

NASA-TP- 1942 ...............................p 48 N82-14090

NASA-TPo1943 ...............................p 19 N82-14051

NASA-TP-1944 ...............................p 94 N82-19373

NASA-TP-1945 ...............................p 49 N82-15040

NASA-TP-1946 ...............................p 49 N82-15039

NASA-TP-1947 ...............................p 94 N82-19374

NASA-TP-1948 ...............................p3 N82-14049

NASA-TP-1949 ...............................p 66 N82-14203

NASA-TP-1950 ...............................p 66 N82-15106

NASA-TP- 1951 ...............................p 18 N82-13108

NASA-TP- 1952 ...............................p 18 N82-13106

NASA-TP-1953 ..............................p 19 N82-14052

NASA-TP-1954 ...............................p 145 N82-16477

NASA-TP-1955 ...............................p 66 N82-14202

NASA-TP-1956 ...............................p 149 N82-14672

NASA-TP-1958 ...............................p 19 N82-14055

NASA-TP-1959 ...............................p 35 N82-18204

NASA-TP-1960 ...............................p 39 N82-14085

NASA-TP-1961 ...............................p 72 N82-14277

NASA-TP-1962 ...............................p 19 N82-20156

NASA-TP-1963 ...............................p 39 N82-20180

NASA*TP-t964 ...............................p 188 N82-14879

NASA.TP-1965 ...............................p 24 N84-27694

NASA-TP-1966 ...............................p 57 N82-19225

NASA-TP-1967 ...............................p 109 N82-20467

NASA-TP-1968 ...............................p 188 N82-21036

NASA-TP-1969 ...............................p 150 N82-19707

NASA-TP*1970 ...............................p 188 N82-24052

NASA-TP-1971 ...............................p 19 N82-26227

NASA-TP-1972 ...............................p 59 N83-17560

NASA-TP-1973 ...............................p 130 N82-20566

NASA-TP-1974 ...............................p 49 N82-19222

NASA-TP-1976 ...............................p 188 N82-21037

NASA-TP-1977 ...............................p 81 N82-22317

NASA-TP-1978 ...............................p 31 N82-22239

NASA-TP-1979 ...............................p 164 N82-24790

NASA-TP-t 980 ...............................p 99 N82-19390

NASA-TP-1981 ...............................p 130 N82-20567

NASA-TP-1982 ...............................p 130 N82-20565

NASA-TP-1983 ...............................p 57 N82-24209

NASA-TP-1984 ...............................p 35 N82-23244

NASA-TP-1985 ...............................p 88 N82-20291

NASA-TP-1986 ...............................p 94 N82-20316

NASA-TP*1987 ...............................p 49 N82-20183

NASA*TP-1988 ...............................p 69 N82-20236

NASA-TP-1989 ...............................p 88 N82-21300

NASA-TP-1990 ...............................p 88 N82-21298

NASA-TP-1991 ...............................p 88 N82-21301

NASA-TP-1992 ...............................p 102 N82-22439

NASA-TP-1993 ...............................p 150 N82-21774

NASA-TP-1994 ...............................p 94 N82-21332

NASA-TP-1995 ...............................p 188 N82-24942

NASA-TP-1996 ...............................p 57 N82-20188

NASA-TP-1997 ...............................p 31 N82-23233

NASA-TP-1998 ...............................p 73 N82-20238

NASA-TP-1999 ...............................p 102 N82-25441

NASA-TP-2000 ...............................p 24 N84-28743

NASA-TP-2001 ...............................p 49 N82-22269

NASA-TP-2002 ...............................p 95 N82-22366

NASA-TP-2003 ...............................p 192 N82-23003

NASA-TP-2004 ...............................p 189 N84-10913

NASA-TP-2005 ...............................p 19 N82-222t5

NASA-TP-2006 ...............................p 88 N82-22349

NASA-TP-2007 ...............................p 115 N82-23515

NASA-TP-2008 ...............................p 102 N82-23397

NASA-TP-2009 ...............................p 35 N82-24193

NASA-TP-2010 ...............................p 131 N82-26703

NASA-TP-20t1 ...............................p4 N82-26217

NASA-TP-2012 ...............................p 19 N82-25193

NASA-TP-2013 ...............................p 19 N82-26231

NASA-TP-2014 ...............................p 85 N82-22330

NASA-TP-2015 ...............................p 81 N82-25325

NASA-TP-2016 ...............................p 62 N82-29335

NASA-TP-2017 ...............................p 21 N83-25665

NASA-TP-2018 ...............................p 20 N82-26234

NASA-TP-2020 ...............................p 49 N82-25250

NASA-TP-2022 ...............................p 142 N83-29750

NASA-TP-2023 ...............................p 49 N83-t 1125

NASA-TP-2024 ...............................p 19 N82-26232

NASA-TP-2025 ...............................p 20 N82-26235

NASA-TP-2026 ...............................p 36 N82-29311

NASA-TP-2027 ...............................p 122 N82-26678

NASA-TP-2028 ...............................p 49 N82-31329

NASA-TP-2029 ...............................p 20 N82-29270

NASA-TP-2030 ...............................p 20 N82-28247

NASA-TP-2031 ...............................p 150 N82-27867

NASA-TP-2032 ...............................p 13t N82-28665

NASA-TP-2033 ...............................p 57 N83-16350

NASA-TP-2034 ...............................p 20 N83-11058

NASA-TP-2035 ...............................p 31 N83-29193

NASA-TP-2036 ...............................p 122 N83-11496

NASA-TP-2037 ...............................p 122 N82-32737

NASA-TP-2038 ...............................p 110 N82-31646

NASA-TP-2039 ...............................p 150 N82-28839

NASA-TP-2040 ...............................p 122 N82-31691

NASA-TP-2042 ...............................p 36 N82-31321

NASA-TP-2043 ...............................p 20 N82-32320

NASA-TP-2044 .........................p 20 N82-30291

NASA-TP-2045 ...............................p 164 N83-14824

NASA-TP-2046 ...............................p 188 N82-31069

NASA-TP-2047 ...............................p 122 N82-32736

NASA-TP-2048 ...............................p 95 N82-32491

NASA-TP-2049 ...............................p 49 N82-33389

NASA-TP-2050 ...............................p 122 N83-13457

NASA-TP-2051 ...............................p 150 N83-13643

NASA-TP-2052 ...............................p 51 N84-28795

NASA-TP-2053 ...............................p 85 N83-18863

NASA-TP-2054 ...............................p 20 N82-32322

NASA-TP-2055 ...............................p 131 N83-12449

NASA-TP-2056 ...............................p 97 N83-11340

NASA-TP-2057 ...............................p 49 N83-10045

NASA-TP-2058 ...............................p 49 N83-11126

NASA-TP-2059 ...............................p 95 N83-14269

NASA-TP-2060 ...............................p 194 N83-13979

NASA-TP-2061 ...............................p 88 N83-15413

NASA-TP-2062 ...............................p 110 N83-12360

NASA-TP-2063 ...............................p 95 N83-16528

NASA-TP-2065 ...............................p 74 N82-33421

NASA-TP-2066 ...............................p 81 N82-31451

NASA-TP-2067 ...............................p 57 N83-11139

NASA-TP-2068 ...............................p 20 N83-10016

NASA-TP-2069 ...............................p 69 N82-33417

NASA-TP-2070 ...............................p 131 N83-10442

NASA-TP-2071 ...............................p 25 N85-10920

NASA-TP-2072 ...............................p 188 N82-34189

NASA-TP-2073 ...............................p4 N82-31294

NASA-TP-2074 ...............................p 131 N83-11513

NASA-TP-2075 ...............................p 188 N82-34190

NASA*TP-2076 ...............................p 150 N83-12595

NASA-TP-2077 ...............................p 154 N82-33918

NASA-TP-2078 ...............................p 20 N83-11059

NASA-TP-2079 ...............................p 189 N83-11838

NASA-TP-2080 ...............................p 122 N83-16758

NASA-TP-2081 ...............................p 59 N83-18770

NASA-TP-2082 ...............................p 40 N83-18723

NASA-TP-2083 ...............................p 131 N83-14521

NASA-TP-2084 ...............................p 189 N83-16149

NASA-TP-2085 ...............................p 40 N83-17535

NASA.TP-2086 ...............................p 184 N83-10876

NASA-TP-2087 ...............................p 30 N83-14077

NASA-TP-2088 ...............................p 146 N83-18024

NASA-TP-2089 ...............................p 209 N83-13048

NASA-TP-2090 ...............................p 150 N83-16952

NASA-TP-2091 ...............................p 118 N83-16738

NASA-TP-2092 ...............................p 40 N83-16338

NASA-TP-2094 ...............................p 168 N83-19411

NASA-TP-2095 ...............................p 131 N83-16785

NASA-TP-2096 ...............................p 110 N83-20031

NASA-TP-2097 ...............................p 26 N85-31010

NASA-TP-2098 ...............................p 110 N83-20032

NASA-TP-2100 ...............................p 110 N83-16675

NASA-TP-2101 ...............................p 150 N83-16951

NASA-TP-2102 ...............................p 88 N83-18895

NASA-TP-2103 ...............................p 1t0 N83-24808

NASA-TP-2105 ...............................p 183 N83-16095

NASA-TP-2106 ..............................p 36 N83-18715

NASA-TP*2107 ............................p 97 N83-16545

NASA-TP-2108 ...............................p 74 N83-19806

NASA-TP-2109 ...............................p 31 N83-18704

NASA-TP-2110 ...............................p 88 N83-16492

NASA-TP-2111 ...............................p 123 N83-16759

NASA-TP-2112 ...............................p 49 N83-17547

NASA-TP-2113 ...............................p 88 N83-16491

NASA-TP-2114 ...............................p 50 N83-18727

NASA-TP-2115 ...............................p 110 N83-16674

NASA-TP-2116 .............................p 21 N83-25666

NASA-TP-2117 ...............................p 81 N83-16400

NASA-TP-2118 ...............................p 36 N83-18714

NASA-TP-2119 ...............................p 22 N84-10025

NASA-TP-2120 ...............................p 21 N83-26821

NASA-TP-2121 ...............................p 189 N83-34713

NASA-TP-2122 ...............................p 40 N84-13182

NASA-TP-2123 ...............................p 88 N83-19889

NASA-TP-2124 .............................p 110 N83-16680

NASA-TP-2125 ...............................p 21 N83-22162

NASA-TP-2126 .............................p 57 N83-19758

NASA-TP-2127 ..............................p 111 N83-28378

NASA-TP-2128 ...............................p 57 N84-13198

NASA-TP-2129 ..............................p 85 N83-t9825

NASA-TP-2130 ...............................p 168 N83-24133

NASA-TP-2131 ...............................p 50 N83-23309

NASA-TP-2132 ...............................p 50 N83-32806

NASA-TP-2133 ...............................p 20 N83-22161

NASA-TP-2134 ...............................p 189 N83-30164

NASA-TP-2135 ...............................p 36 N83-22191

NASA-TP-2136 ...............................p 36 N83-22192

NASA-TP-2137 ...............................p 142 N83-27293

NASA-TP-2138 ...............................p 192 N83-23140

NASA-TP-2139 ...............................p 89 N83-24641

NASA-TP-2140 ...............................p 88 N83-21110

NASA-TP-2141 ...............................p 132 N83-33216

NASA-TP-2142 ..............................p 50 N83-25712

NASA-TP-2143 .............................p 36 N83-31596

NASA*TP-2144 ...............................p 195 N83-21991

NASA-TP-2145 ...............................p tll N84-22907

NASA-TP-2146 ...............................p t23 N83-35400

NASA-TP-2147 ...............................p t54 N84-10675

NASA-TP-2148 ...............................p 85 N83-24575

NASA-TP-2149 ..............................p 89 N83-24640

NASA*TP-2150 ..............................p 74 N83-22317

NASA-TP-2151 ...............................p 21 N83-22166

NASA-TP-2152 ...............................p 82 N83-24562

NASA-TP-2153 .......................p 82 N83-24561

NASA-TP-2154 ..............................p 123 N83-24862

NASAoTP-2155 ...............................p 182 N83-25438

NASA-TP-2156 ...............................p 50 N83-24509

NASA-TP-2157 ...............................p 21 N83-27959

NASA-TP-2158 ...............................p 21 N83-24478

NASA-TP-2159 ...............................p 21 N83-30391

NASA-TP-2160 ...............................p 132 N83-26491

NASA-TP-2161 ...............................p 95 N83-24695

NASA-TP-2162 ...............................p 102 N83-25985

NASA-TP-2163 ...............................p 88 N83-23419

NASA-TP-2164 ...............................p 142 N83-26201

NASA-TP-2165 ...............................p 179 N84-27461

NASA-TP-2166 ...............................p 116 N83-33126

NASA-TP-2167 ...............................p 21 N83-31577

NASA-TP-2168 ...............................p 209 N83-25646

NASA-TP-2169 ..............................p 89 N83-32908

NASA-TP-2171 ...............................p 50 N83-26839

NASA-TP*2172 ...............................p 146 N83-36549

NASA-TP-2173 ...............................p 184 N83-27679

NASA-TP-2174 ...............................p 132 N83-34373

NASA-TP-2175 ...............................p 123 N83-28453

NASA-TP-2176 ...............................p 22 N83-36000

NASA-TP-2177 ...............................p 184 N83-35736

NASA-TP-2178 .............................p 210 N83-29169

NASA-TP-2179 ...............................p 180 N83-28921

NASA-TP-2180 ...............................p 111 N83-34229

NASA-TP-2181 ...............................p 189 N83-33684

NASA-TP-2182 ...............................p 118 N83-32044

NASA-TP-2183 ..............................p 57 N84-12190

NASA-TP-2184 ...............................p 22 N83-32776

NASA-TP-2185 ...............................p 194 N83-27846

NASA-TP-2186 ..............................p 60 N83-36039

NASA-TP-2187 ...............................p 82 N83-33956

NASA-TPo2188 ...............................p 50 N83-30431

NASA-TP-2189 ...............................p t23 N83-33166

NASA*TP-2190 ...............................p 30 N83-34921

NASA-TP-2191 ...............................p 182 N83-34661

NASA-TP-2192 ...............................p 36 N83-27977

NASA-TP-2193 ...............................p 182 N84-13885

NASA-TP-2194 ...............................p 40 N83-36028

NASA-TP-2195 ...............................p 132 N83-33217

NASA-TP-2196 ...............................p 36 N83-34935

NASA-TP-2197 ...............................p 189 N84-13923

C-7
NASA-TP-2198 REPORT NUMBER INDEX

NASA-TP-2198 ............................... p67 N83-32826

NASA-TP-2199 ...............................p 50 N83-32807

NASA-TP-2200 ...............................p 111 N83-34232

NASA-TP-2201 ...............................p 89 N83-35100

NASA-TP-2202 ...............................p 172 N83-34579

NASA-TP-2203 ...............................p 50 N83-33893

NASA-TP-2204 ...............................p 22 N83-34905

NASA-TP-2205 ...............................p 22 N84-13152

NASAoTP-2206 ...............................p 22 N83-34904

NASA-TP-2207 ...............................p 89 N83-34019

NASA-TP-2208 ...............................p 132 N83-34372

NASA-TP-2209 ...............................p 74 N83-31713

NASA-TP-2210 ...............................p 22 N83-34906

NASA-TP-2211 ...............................p 172 N83-33538

NASA-TP-2212 ...............................p 40 N84-12164

NASA-TP-2213 ...............................p 112 N85-16065

NASA-TP-2214 ...............................p 111 N84-22906

NASA-TP-2215 ...............................p 132 N84-16585

NASA-TP-2216 ...............................p 184 N83-33631

NASA-TP-2217 ...............................p 189 N84-22363

NASA-TP-2218 ...............................p 116 N84-11460

NASA-TP-2220 ...............................p 123 N84-17590

NASA-TP-2221 ...............................p 181 N84-16843

NASA-TP-2225 ...............................p 111 N84-19741

NASA-TP-2226 ...............................p 132 N84-13614

NASA-TP-2227 ...............................p 50 N83-34941

NASA-TP*2228 ...............................p 22 N84-13163

NASA-TP-2229 ...............................p 111 N84-17534

NASA-TP-2230 ...............................p 57 N84-17184

NASA-TP-2231 ...............................p 51 N84-11171

NASA-TP-2232 ...............................p 111 N84-21828

NASA-TP-2234 ...............................p 22 N84-13165

NASA-TP-2235 ...............................p 22 N84-13164

NASA-TP-2236 ...............................p 89 N84-13263

NASA-TP-2237 ...............................p 189 N84-19049

NASA-TP-2238 ...............................p 102 N84-16461

NASA-TP-2239 ...............................p 82 N84-13224

NASA-TP-2240 ...............................p 74 N84-16247

NASA-TP-2241 ...............................p t18 N84-17575

NASA-TP-2242 ...............................p 192 N84-13978

NASA-TP-2243 ...............................p 133 N84_20878

NASA-TP-2244 ...............................p 175 N84-22178

NASA-TP-2245 ...............................p 111 N84-13500

NASA-TP-2246 ...............................p 23 N84-18162

NASA-TP-2247 ...............................p 37 N84-18189

NASA-TP-2248 ...............................p 102 N84-15394

NASA-TP-2249 ...............................p 23 N84-18163

NASA-TP-2250 ...............................p 23 N84-18164

NASA-TP-2251 ...............................p 22 N84-13162

NASA-TP-2252 ...............................p 167 N86-24090

NASA-TP-2253 ...............................p 23 N84-18165

NASA-TP-2254 ...............................p 189 N84-21277

NASA-TP-2255 ...............................p 74 N84-19393

NASAoTP-2256 ...............................p 24 N84-26660

NASA-TP-2257 ...............................p 123 N84-13577

NASA-TP-2258 ...............................p 154 N84-14606

NASA-TP-2259 ...............................p 189 N84-15894

NASA-TP-2260 ..............................p 150 N84-18764

NASA-TP-2261 ...............................p 172 N84-20155

NASA-TP-2262 ...............................p 37 N84-17175

NASA-TP-2263 ...............................p 111 N84-15427

NASA-TP-2264 ...............................p 185 N84-15880

NASA-TP-2265 ...............................p 23 N84-17127

NASA-TP-2266 ...............................p 51 N84-16181

NASA-TP-2267 ...............................p 95 N84-16334

NASA-TP-2268 ...............................p 111 N84-17525

NASA-TP-2269 ...............................p 23 N84-20486

NASA-TP-2270 ...............................p 23 N84-17132

NASA-TP-2271 ...............................p 210 N84-21485

NASA-TP-2272 ...............................p 132 N84-18675

NASA-TP-2273 ...............................p 23 N84-18159

NASA-TP-2274 ...............................p 123 N84-18653

NASA-TP-2275 ...............................p 123 N84-18654

NASA-TP-2276 ...............................p 100 N84-20735

NASA-TP-2277 ...............................p 103 N84-20759

NASA-TP-2278 ...............................p 89 N84-18370

NASA-TP-227g ...............................p 95 N84-18399

NASA-TP-2280 ..............................p 89 N84-17350

NASA-TP-2281 ...............................p 31 N84-17165

NASA-TP-2282 ...............................p 23 N84-18161

NASA-TP-2283 ...............................p 58 N84-23652

NASA-TP-2284 ...............................p 67 N85-19003

NASA-TP-2285 ...............................p 95 N84-18400

NASA-TP-2286 ...............................p 95 N84-21740

NASA-TP-2287 ...............................p 103 N84-20758

NASA-TP-2288 ...............................p 204 N84-20457

NASA-TP-2289 ...............................p 89 N84-21716

NASA-TP-2290 ...............................p 89 N84-21721

NASA-TP-2291 ...............................p 37 N84-19333

NASA-TP-2292 ...............................p 23 N84-20480

NASA-TP-2293 ...............................p 74 N84-23675

NASA-TP-2294 ...............................p 51 N84-21549

NASA-TP-2295 ...............................p 95 N84-19564

NASA-TP-2296 ...............................p 51 N84-20562

NASA-TP-2297 ...............................p 23 N84-20493

NASA-TP-2298 ...............................p 133 N84-21901

NASA-TP-2299 ...............................p 172 N84-22162

NASA-TP-2300 ...............................p 40 N84-21542

NASA-TP-2301 ...............................p 79 N84-20643

NASA-TP-2302 ...............................p 79 N84-26749

NASA-TP-2303 ...............................p 166 N84-31865

NASA-TP-2304 ...............................p 51 N84-24578

NASA-TP-2305 ...............................p 192 N84-22396

NASA-TP-2306 ...............................p 23 N84-24538

NASA-TP-2307 ...............................p 113 N85-34351

NASA-TP-2308 ...............................p 189 N84-25422

NASA-TP-2309 ...............................p 51 N84-32388

NASA-TP-2310 ...............................p 190 N84-27543

NASA-TP-2311 ...............................p 58 N84:25717

NASA-TP-2312 ...............................

NASA-TP-2313 ............................... N ASA-TP-2314 ...............................

NASA-TP-2315 ...............................

NASA-TP-2316 ...............................

NASA-TP-2317 ...............................

NASA-TP-2318 ...............................

NASA-TP-2319 ...............................

NASA-TP-2320 ...............................

NASA-TP-2321 ...............................

NASA-TP-2322 ...............................

NASA-TP-2323 ...............................

NASA-TP-2324 ...............................

NASA-TP-2325 ...............................

NASA-TP-2326 ...............................

NASA-Tpo2327 ...............................

NASA-TP-2328 ...............................

NASA-TP-2330 ...............................

NASA-TP-2331 ...............................

NASA-TP-2332 ...............................

NASA-TP-2333 ...............................

NASA-TP-2334 ...............................

NASA-TP-2335 ...............................

NASA-TP-2337 ...............................

NASA-TP-2338 ...............................

NASA-TP-2339 ...............................

NASA-TP-2340 ...............................

NASA-TP-2341 ...............................

NASA-TP-2342 ...............................

NASA-TP-2343 ...............................

NASA-TP-2344 ...............................

NASA-TP-2345 ...............................

NASA-TP-2346 ...............................

NASA-TP-2347 ...............................

NASA-TP-2348 ...............................

NASA-TP-2349 ...............................

NASA-TP-2351 ...............................

NASA-TP-2353 ...............................

NASA-TP-2354 ...............................

NASA-TP-2355 ...............................

NASA-TP-2356 ...............................

NASA-TP-2357 ...............................

NASA-TP-2358 ...............................

p 89 N84-23750

165 N84-24044

p 74 N84-23677

;) 74 N84-23676

95 N84-23764

97 N84-23774

112 N84-25944

90 N84-28958

85 N84-32446

118 N84-23878

3 181 N84-28538 3 112 N84-23852 3 133 N84-26053 3 209 N84-24520 3 58 N84-32394 3 37 N84-31111

24 N84-27675

3 24 N84-27676 3 195 N84-25458

177 N84-24114

24 N84-32354

112 N85-12313

24 N84-33377

193 N84-26398

89 N84-26783

90 N84-31349

58 N84-28801

181 N84-28539

95 N84-28989

133 N84-34773

174 N84-29479

112 N85-17322

180 N84-34198

118 N84-31617

25 N84-33379

112 N84-31561

24 N84-28750

37 N84-32378

) 90 N84-28965

124 N84-29226

190 N84-32124

) 58 N85-11002

190 N85-11788

NASA-TP-2359 ...............................p 51 N85-10064

NASA-TP-2360 ...............................p 96 N84-31379

NASA-TP-2361 ...............................p 74 N84-33452

NASA-TP-2362 ...............................p 96 N84-33590

NASA-TP-2363 ...............................p 193 N85-17690

NASA-TP-2365 ...............................p 69 N85-15778

NASA-TP-2366 ...............................p 182 N84-34204

NASA-TP-2367 ...............................p t24 Ne4-32824

NASA-TP-2368 ...............................p 124 N84-32825

NASA-TP-2369 ...............................p 83 N85-12094

NASA-TP-2370 ............................... p83 N85-11136

NASA-TP-2371 ...............................p 75 N85-31142

NASA-TP-2372 ...............................p 51 N85-10065

NASA-TP-2373 ...............................p 112 N85-16066

NASA-TP-2374 ...............................p 37 N85-12884

NASA-TP-2375-PT-1 ......................p 25 N85-10914

NASA-TP-2376 ...............................p 181 N85-15446

NASA-TP-2377 ...............................p 83 N84-33521

NASA-TP-2378 ...............................p 179 N85-17576

NASA-TP-2379 ...............................p 75 N85-19015

NASA-TP-2380 ...............................

NASA-TP-2381 ...............................

NASA-TP-2382 ...............................

NASA-TP-2383 ...............................

NASA-TP-2385 ...............................

NASA-TP-2386 ...............................

NASA-TP-2387 ...............................

NASA-TP-2388 ...............................

NASA-TP-2389 ...............................

NASA-TP-2390 ...............................

NASA-TP-2391 ...............................

NASA-TP-2393 ...............................

NASA-TP-2394 ...............................

NASA-TP-2396 ...............................

NASA-TP-2397 ...............................

NASA-TP-2398 ...............................

NASA-TP-2399 ...............................

NASA-TP-2400 ...............................

NASA-TP-2403 ...............................

NASA-TP-2404 ...............................

134 N85-13267

b 190 N85-19790

25 N85-19925

p 40 N85-16868

25 N85-15694

40 N85-16869

25 N85-12864

112 N85-12314

3 184 N85-16565 3 112 N85-14078

25 N85-18951

40 N85-26705

112 N85-13175

202 N85-12833

202 N85-12834

190 N85-22109

25 N85-12862

37 N85-19979

90 N85-13006

124 N85-13233

NASA-TP-2405 ...............................

NASA-TP-2406 ...............................

NASA-TP-2407 ...............................

NASA-TP-2408 ...............................

NASA-TP-2409 ...............................

NASA-TPo2411 ...............................

NASA-TP-2412 ...............................

NASA-TP-2413 ...............................

NASA-TP-2414 ...............................

NASA-TP-2415 ...............................

NASA-TP-2416 ...............................

NASA-TP-2417 ...............................

NASA-TP-2419 ...............................

NASA-TP-2420 ...............................

NASA-TP-2421 ...............................

NASA-TP-2422 ...............................

NASA-TP-2423 ...............................

NASA-TP-2424 ...............................

NASA-TP-2425 ...............................

NASA-TP-2426 ...............................

NASA-TP-2427 ...............................

NASA-TP-2428 ...............................

NASA-TP-2429 ...............................

NASA-TP-2430 ...............................

NASA-TP-2431 ...............................

NASA-TP-2432 ...............................

NASA-TP-2433 ...............................

NASA-TP-2434 ...............................

NASA-TP-2435 ...............................

NASA-TP-2436 ...............................

NASA-TP-2437 ...............................

NASA-TP-2438 ...............................

NASA-TP-2439 ...............................

NASA-TP-2440 ...............................

NASA-TP-2441 ...............................

NASA-TP-2442 ...............................

NASA-TP-2443 ...............................

NASA-TP-2444 ...............................

NASA-TP-2445 ...............................

NASA-TP-2446 ...............................

NASA-TP-2447 ...............................

NASA-TP-2448 ...............................

NASA-TP-2449 ...............................

NASA-TP-2450 ...............................

NASA-TP-2451 ...............................

NASA-TP-2452 ...............................

NASA-TP-2453 ...............................

NASA-TP-2454 ...............................

NASA-TP-2455 ...............................

NASA-TP-2456 ...............................

96 N85-13044

g6 N85-13045

75 N85-14858

124 N85-13234

3 126 N85-23090 3 52 N85-22394 3 58 N85-23801 3 25 N85-21120

25 N85-15693

3 52 N85-22395

37 N85-23753

;) 25 N85-21118

;) 116 N85-16099

26 N85-28923

,134 N85-20396

179 N85-28610

3 26 N85-23707

116 N85-16100

3 166 N85-16351

;) 180 N85-17596

37 N85-25248

143 N85-23237

83 N85-25435

26 N85-29921

26 N85-23708

26 N85-28924

26 N8_29922

26 N8_27822

52 N8_21168

112 N85-20270

78 N85-21263

70 N85-21246

26 N85-29924

181 N85-27575

83 N85-26924 5 N86-16187

90 N85-21323

190 N85-30767

58 N85-28949

26 N85-29923

27 N86-20345

166 N85-21878

96 N85-21359

166 N85-20605

58 N85-34144

113 N86-14530

195 N85-24961

177 N85-31839

134 N85-32339

177 N85-23305

NASA-TP-2457 ...............................p 27 N86-20346

NASA-TP-2458 ...............................p 27 N85-33106

NASA-TP-2459 ...............................p 90 N85-22662

NASA-TP-2460 ...............................p 112 N85-27165

NASA-TP-2461 ...............................p 52 N85-25261

NASA-TP-2463 ...............................p 52 N85-28944

NASA-TPo2464 ...............................p 98 N85-35307

NASA-TP-2467 ...............................p 27 N85-33107

NASA-TP-2468 ...............................p 26 N85-26667

NASA-TP-2469 ...............................

NASA-TP-2470 ...............................

NASA-TP-2471 ...............................

NASA-TP-2472 ...............................

NASA-TP-2473 ...............................

NASA-TP-2474 ...............................

NASA-TP-2475 ...............................

NASA-TP-2476 ...............................

NASA-TP-2477 ...............................

NASA-TP-2478 ...............................

NASA-TP-2479 ...............................

NASA-TP-2480 ...............................

NASA-TP-2481 ..............................

NASA-TP-2484 ...............................

NASA-TP-2485 ...............................

NASA-TP-2486 ...............................

NASA-TP-2487 ...............................

NASA-TP-2488 ...............................

NASA-TP-2489 ...............................

NASA-TP-2491 ...............................

NASA-TP-2493 ...............................

NASA-TP-2494 ...............................

NASA-TP-2495 ...............................

NASA-TP-2496 ...............................

NASA-TP-2497 ...............................

NASA-TP-2498 ...............................

NASA-TP-2499 ...............................

NASA-TP-2500 ...............................

NASA-TP-2501 ...............................

NASA-TP-2502 ...............................

NASA-TP-2503 ...............................

NASA-TP-2504 ...............................

NASA-TP-2505 ...............................

NASA-TP-2506 ...............................

NASA-TP-2507 ...............................

NASA-TP-2508 ...............................

NASA-TPo2509 ...............................

185 N85-28708

) 134 N85-27258

116 N86-12579

191 N86-16040

125 N85-32331

112 N85-25757

190 N85-29094

p 96 N85-26990

:) 52 N85-31058

327 N86-11186

181 N86-13946

135 N85-33537

3 135 N86-11522 3 75 N86-16250 3 26 N85-27823

113 N85-28260

185 N85-33745

3125 N85-32329

_183 N85-28656 3 28 N86-23558

30 N85-3210t

75 N85-31141

98 N85-31307

125 N85,-31511

27 N86-16193

85 N85-31244

90 N86-12295

125 N85-32330

27 N86-20350

118 N86-16563

) 27 N86-18289

103 N86-20678

191 N86-16041

) 27 N86-20349 ) 69 N85-33169

)68 N86-11215

113 N86-20720

C-8
1 Report No. 2. Government Accession No. 3. Recipient's Catalog No.

NASA SP-7063

5. Report Date

A Catalog September, 1987

4. Title and Subtitle

NASA Scientific and Technical Publications:

of Special Publications, Reference Publications,

Conference Publications, and Technical Papers, 1977-1986

7 Author(s)

6. Performing Organization Code

8. Performing Organization Report No.

t0. Work Unit No

11. Contract or Grant No

13. Type of Report and Period Covered

14. Sponsoring Agency Code

9 Performing Organization Name and Address

Office of Management

Scientific and Technical Information Division

National Aeronautics and Space Administration

Washington, DC 20546

12 Sponsoring Agency Name and Address

National Aeronautics and Space Administration

Washington, DC 20546 " '

15 Supplementary Notes

16 Abstract

This catalog lists 2311 citations of all NASA Special Publications, NASA Reference Publications, NASA Conference

Publications, and NASA Technical Papers that were entered into the NASA scientific and technical database during

the decade 1977 through t986. The entries are grouped by subject category. Indexes of subject terms, personal

authors, and NASA report numbers are provided.

17 Key Words (Suggested by Authors(s))

Catalogs (Publications)

18. Distribution Statement

Unclassified - Unlimited

Subject Category 82

19 Security Classif Iof Ibis report) 20 Security Classif. (of this page) 21. No. of Pages 22 Price *

Unclassified Unclassified 394 Free

NASA FORM 1626 I,:_ .:4.' Available from the National Technical Information Service.

Springfield, Virginia 22161 as PR 655B.

._J

C-5
REPORT NUMBER INDEX

NASA-TP-2510 .............p 68

NASA-TP-2511 .......................p 68

NASA-TP-2512 ................p 90

NASA-TPo2513 ......................p 125

NASA-TP-2514 ..................p 135

NASA-TP-2515 ...................p 83

NASA-TP-2518 ....................p 190

NASA-TP-2519 ............................p 27

NASA-TP-2520 ...................p 38

NASA-TP-2522 ...................p 193

NASA-TP.2524 ...........................p 103

NASA-TP-2525 .......................p 172

NASA-TP-2527 ........................p 211

NASA.TP.2528 .......................p 135

NASA-TP-2529 ....................p 183

NASA-TP-2531 .............................p 117

NASA-TP-2532 ......................p t00

NASA-TP-2533 .......................p 177

NASA-TP.2534 .....................p 52

NASA-TP-2535 ..................p 59

NASA-TP-2536 ......................p 183

NASA-TP-2537 ....................p 27

NASA-TP-2538 ..........................p 126

NASA-TP-2539 .......................p 28

NASA-TP-2540 ..........................p 167

NASA-TP-2541 ...................p 191

NASA-TP-2542 .............p 83

NASA*TP-2543 .....................p 96

NASA-TP-2544 ...................p 52

NASA-TP-2545 ......................p 27

NASA-TP-2547 ...................p 174

NASA-TP-2548 ....................p 193

NASA-TP-2549 ......................p 28

NASA-TP-2550 .............................p 184

NASA-TP.2551 ......................p 191

NASA-TP-2552 ...................p 191

NASA-TP-2553 .....................p 167

NASA-TP-2554 ......................p 103

NASA-TP-2555 ...................p 194

NASA-TP-2557 ..................p 52

NASA-TP-2558 ...........................p 78

NASA-TP-2559 ........................p 28

NASA-TP-2560 ............................p 75

NASA-TP-2562 ...................p 68

NASA-TP-2563 ......................b 191

NASA-TP-2564 ..............................p 181

NASA-TP-2565 .......................D 28

NASA-TP-2568 ..............................D 90

NASA-TP-2569 ............................3 28

NASA-TP-2570 .............3 60

NASA-TP-2571 ..........................3 78

NASA-TP-2572 ......................._ 68

NASA-TP-2573 ..................... :} 28

NASA-TP-2575 ..................... 63

NASA-TP-2576 ............................ 113

NASA-TP-2577 ............... 135

NASA-TP-2578 ........................... 90

NASA-TP-2579 ..................... 28

NASA-TP-2580 .............................. 28

NASA-TP-2581 ......................... 191

NASA-TP-2582 ................... 117

NASA-TP-2584 ..................... 60

NASA-TP-2585 ................. 183

NASA-TP-2589 ........................... 38

NASA-TP-2590 ............................. 183

NASA-TP-2591 ............. 135

NASA-TP-2595 .................... 143

NASA-TP-2599 ......................5

NASA-TP-2600 ..................... 193

NASA-TP-2602 ......................... 78

NASA-TP-2604 ................... 75

NASA-TP-2605 ............................... 180

NASA-TP-2609 ................... 191

NASA-TP-2620 ................... 96

NASA-TP-2622 ................... 103

NASA-TP-2634 ........................... 68

NASA-TP-2636 ................... 91

N85-34149

N85-34148

N86-13406

N86-12609

N86-20857

N86-21614

N86-13056

N86-20348

N86-13316

N86-21297

N86-13643

N86-27920

N86.21492

N86-20856

N86-28661

N86-20753

N86-20586

N86-23282

N86-22576

N86-22580

1"486-18060

N86-2035t

N86-24992

N86.20352

N86.23160

N86-26162

N86-20508

N86-15394

N86-15313

N86-20347

N86-26836

N86-23388

N86-23560

N86-19O95

N86-21280

N86-24393

N86-25924

N86-21755

N86-22390

N86-24694

N86-21577

N86-23559

N86-30800

N86-24722

N86-31337

N86-25168

N86-24662

N86-26413

N86-21507

N86-28101

N86-28123

N86-20460

N86-21506

N86-21559

N86-23851

N86-23974

N86-26412

N86-23562

N86-23561

N86-27043

N86-24962

N86-24709

N86-27953

N86-30721

N86-28662

N86-28464

N86-31945

N86-29762

N86-30485

N86-28124

N86-3080t

N86-27947

N86-31341

N86-29040

N86-32629

N86-30753

N86-30837

OR/GINA3J PAGE IS

OF. POOR QUALIT_

NASA-TP-2636