NASA SPr7063 (06) AD-A264 373

NASA SCIENTIFIC AND

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A CATALOG OF SPECIAL PUBLICATIONS, REFERENCE,

PUBLICATIONS, CONFERENCE PUBLICATIONS, AND

TECHNICAL PAPERS 1991-1992

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NASA SP-7063 (06)

NASA SCIENTIFIC AND

TECHNICAL PUBLICATIONS

A CATALOG OF SPECIAL PUBLICATIONS, REFERENCE

PUBLICATIONS, CONFERENCE PUBLICATIONS, AND

TECHNICAL PAPERS 1991-1992

DTIC CTUALIY TLZSPECT-D 5

Accesion For

NTIS CRA&i

Di i tIO• I.,t

"A ' •diihiL !ýty 2-cles

National Aeronautics and Space Administration

Scientific and Technical Information Program

Washington. DC 1993

I _ _ _ _ _ _ _ _ _
This publication was prepared by the NASA Center for AeroSpace Landing Information. 800 Elkridge Road, Linthicum Heights, M ID 21090-2934, (301)621-0390.1
PREFACE

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

understanding of our world and the universe we live in. The contributions of NASA through 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, archaeologists, aircraft

engineers, aerospace decision makers, land-use planners, historians, and rescue teams ail make use

of the results of NASA's research. The findings of this research and development are published in NASA's

scientific and technical report series as a part of NASA's mandate to disseminate the results of the

agency's far-reaching work.

This catalog provides a cumulative list of NASA publications from four report series entered into the

NASA Scientific and Technical Information Database during the accession years 1991 through 1992. For

previous lists, see Records of Achievement: NASA Special Publications, NASA SP-470 (accession

number N83-33792), NASA Scientific and Technical Publications: A Catalog of Special Publications,

Reference Publications, Conference Publications, and Technical Papers, 1977-1986. NASA SP-7063(01)

(accession number N87-30218). Supplements 02 through 05 of this catalog list NASA publications

announced during 1987 through 1990.

Two monthly abstract journals cover all aspects of aeronautics and space research, NASA and non-NASA,

nationally and worldwide. STAR (Scientific and Technical Aerospace Reports). focuses on scientific and

technical reports, and IAA (International Aerospace Abstracts), covers the open literature. These are

available by subscription from the NASA Center for AeroSpace Information and the American Institute

of Aeronautics and Astronautics. Inc.

This catalog includes publicly available reports from four NASA report series: Special Publications (SPs).

Reference Publications (RPs), Conference Publications (CPs), and Technical Papers (TPs). The scope

of each series is defined as follows:

Special Publications are often concerned with subjects of substantial public interest. They report

scientific and technicai information derived from NASA programs for audiences of diverse technicai

backgrounds.

Reference Publications contain compilations of scientific and technical data 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 citations for reports from each of these series. An explanation of the elements in a

typical citation follows. Accession numbers (N numbers) at the end of a citation are separate citations

to articles within the report. Please use STAR to locate these citations.

Also note that some bibliographies in the NASA SP-7000 series are issued periodically. This catalog

lists only the last accessioned report in each bibliography series. The periodicity of each bibliography

is as follows:

NASA SP-7011 Aerospace Medicine and Biology: Monthly plus

A Continuing Bibliography with Indexes annual cumulative index

NASA Cr 7037 Aeronautical Engineering: Monthly plus

A Continuing 3ibfiqor.phy with Indexes annual cumulative index

NASA ýP-7039 NASA PatentAbstracts Bibliography: Semiannual

A Continuing Bibliography

Section 1: Abstracts; Section 2: Indexes
NASA SP-7085 Large Space Structures and Systems Semiannual

in the Space Station Era:

A Bibliography with Indexes

NASA SP-7500 Management: Annual

A Bibliography for NASA Manragers

Please note that the reports cited in this catalog are available for purchase from the NASA Center for

AeroSpace information. They are also available at any Federal Regional Depository Library. Additional

availability information including current CASI price schedules, can be found in the Appendix at the back

of this publication.

iv
NASA Scientific and Technical Publications 1991-1992

TABLE OF CONTENTS

AERONAUTICS For related information see also Astronautics.

01 A ERO NAUTIC S (G ENERAL) .............. .... ..... ...... .......... 1............................. 1

0 2 A E R O D Y N A M IC S ........................................................................... ........... ........... .......... . . 2.............. 2

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 Tralcifer.

03 AIR TRANSPORTATION AND SAFETY ...................................................................... 9

Includes passenger and cargo air transport operations; and aircraft accidents, For related information see

also 16 Space Transportation anu 85 Urban Technology and Transportation.

04 AIRCRAFT COMMUNICATIONS AND NAVIGATION .................................................... 10

Includes digital and voice communication with aircraft; air navigation systems (satellite and ground based):

and air traffic control. For related information see also 17 Space Communications, Spacecraft Communications.

Command and Tracking and 32 Communications and Radar.

05 AIRCRAFT DESIGN, TESTING AND PERFORMANCE .............................. 10

Includes aircraft simulation technology. For related information see also 18 Spacecraft Design. Testing and

Performance and 39 Structural Mechanics. For land transportation vehicles see 85 Urban Technology and

Transportation.

06 AIRCRAFT INSTRUMENTATION ....... .............................. ... 11

Includes cockpit and cabin display devices; and flight instruments. For related information see also 19 Space

craft instrumentatinn and 35 Instrumentation and Photography

07 AIRCRAFT PROPULSION AND POWER .................................. ....................... . 12

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 20 Spacecraft Propulsion

and Power 28 Propellants and Fuels, and 44 Energy Production and Conversion.

08 AIRCRAFT STABILITY AND CONTROL ........................................... ................................ .......... . 12

Includes aircraft handling qualities; piloting; flight controls; and autopilots, For related information see also 05

Aircraft Design, Testing and Performance.

09 RESEARCH AND SUPPORT FACILITIES (AIR) ............................ .......................... 13

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 For related information see also Aeronautics.

12 A S T R O N A U T IC S (G E N E R A L ) ...................................... .............................. ....... ............. ....... 13

For extraterrestrial exploration see 91 Lunar and Planetary Exploration13 A S T R O D Y N A M IC S ..................... ............ ................. 13........................................ 13

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

14 GROUND SUPPORT SYSTEMS AND FACILITIES (SPACE) ................................... ....... ... ...... 14

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 .............................................................................. 14

Includes boosters: operating problems of launch/space vehicle systems: and reusable vehicles. For related

information see also 20 Spacecraft Propulsion and Power

16 SPAC E TR A N SPO RTATIO N .. . . ...... ........ ................... 15.................................15

Includes passenger and cargo space transportation, e.g., shuttle operations, and space rescue lechniques.

For related information see also 03 Air Transportation and Safety and 18 Spacecraft Design. Testing and

Performance. For space suits see 54 Man/System Technology and Life Support.

17 SPACE COMMUNICATIONS, SPACECRAFT COMMUNICATIONS, COMMAND AND TRACKING . 16

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

N.A.A-n abstracts were assigned to this category for this issue.

V
18 SPACECRAFT DESIGN, TESTING AND PERFORMANCE ................. 16

Includes satellites; space platforms; space stations: spacecraft systems and components such as thermal

and envirorimental controls; and attitude controls. For life support systems see 54 Man/System Technology

and Life Suppoii. For related information see also 05 Aircraft Design, Testing and Performance, 39 Structural

Mechanics, and 16 Space Tranrsportation.

19 SPACECRAFT INSTRUMENTATION .......................................................... ....... 19

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

20 SPACECRAFT PRO PULSIO N AND POW ER ................................ ..................... .... ... 1...........9.......... 19

Includes main propulsion systems and components, e g., rocket engines, and spacecraft auxiliary power

sources. For related information see also 07 Aircraft Propulsion and Power 28 Propellants and Fuels. 44

Energy Production and Conversion, and 15 Launch Vehicles and Space Vehicles.

CHEMISTRY AND MATERIALS

23 CHEM ISTHY AND M ATERIALS (G ENERAL)................... ..................... ................... ................... 20

24 C O M P O S IT E M A T E R IA LS ...................... ............................................. ..................... .......... ...... ...... 20

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

ceramic materials see 27 Nonmetallic Materials.

25 INORGANIC AND PHYSICAL CHEMISTRY ............................ .................. 22

Inclides chemical analysis, e.g., chromatography, combustion theory; electrochemistry; and photochemistry

For related information see also 77 Thermodynamics and Statistical Physics.

26 METALLIC MATERIALS ............................................................. 22

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

27 NONMETALLIC MATERIALS .............................................................. 23

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

adhesives, and ceramic materials. For composite materials see 24 Composite Materials.

28 PROPELLANTS AND FUELS .................................................... N.A.

Includes rocket propellants, igniters and oxidizers; their storage and handling procedures. and aircraft fuels.

For related information see also 07 Aircraft Propulsion and Power, 20 Spacecraft Propulsion and Power, and

44 Energy Production and Conversion.

29 M ATERIA LS PRO CESSING ..................................... ..... . .................................... ... .... .. 24

Includes space-based development of products and processes for commercial application. For biological

materials see 55 Space Biology

ENGINEERING For related information see also Physics.

31 E N G IN E E R IN G (G E N E R A L) .................. ...................................................... .................. ... . 244............ 

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

32 COMMUNICATIONS AND RADAR ............................................................... 25

Includes radar; land and global communications: communications theory; and optical comi-,unications. 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

Safety, and 16 Space Transportation.

33 ELECTRONICS AND ELECTRICAL ENGINEERING ....................................... 25

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 ......... .......... . .................. 25.................... 25

Includes boundary layers- hydrodynamics, fluidics: mass transfer and ablation cooling. For related information

see also 02 Aerodynamics and 77 Thermodynamics and Statistical Physics

35 INSTRUM ENTATIO N AND PHOTOG RAPHY .............................. .............. ............................ ... .. 27

Includes remote sensors: measuring instruments and gauges; 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 ........................ ........ .............. NA.

Includes parametric amplifiers For related information see also 76 Solid-State Physics.

V1
37 M ECHANICAL ENG INEERING ....................................................... 28

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

38 QUALITY ASSURANCE AND RELABILITY ..................................... 28

Includes product sampling procedures and techniques, and quality control.

39 S T R U C T U R A L M E C H A N IC S .................. I.... ..... ................... ... ............ ..... .... ... ....................... ... 2.. 29

Includec 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.

GEOSCIENCES For related information see also Space Sciences

42 G EO S C IE N C E S (G E N ER A L) .... ................... .................. ............ .............. 32_----_-----.........

32

43 EARTH RESOURCES AND REMOTE SENSING ....................................................... ................ ... 32

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 ........................................ ............... 33

Includes specific energy conversion systems, e.g., fuel cells; global sources of energy; geophysical conversion:

and windpower. For related intormation see also 07 Aircraft Propulsion and Power, 20 Spacecraft Propulsion

and Power and 28 Propellants and Fue!3.

45 ENVIRONMENT POLLUTION .................................................. 33

Includes atmospheric, noise, thermal, and water pollution.

46 G EO PHYSIC S ..... ......... ... ..................... ........... .... . ...................................................................... - 33

Includes aeronomy; upper and lower atmosphere studies; ionospheric and magnetospheric physics: and

geomagnetism. For space radiation see 93 Space Radiation.

47 METEOROLOGY AND CLIMATOLOGY ................................................ 34

Includes weather forecasting and modification.

4 8 O C E A N O G R A P H Y ................................... 36..........................................

36

Includes biological, dynamic, and physical oceanography; and marine resources. For related information see

also 43 Earth Resources and Remote Sensing.

LIFE SCIENCES

51 LIFE SC IEN C ES (G EN E R A L) ........................................................................ ........ ........... 36

52 AEROSPACE MEDICINE .......................................................... 36

Includes physiological factors: biological effects of radiation: and effects of weightlessness on man and animals.

53 BEHAVIORAL SCIENCES ........................................................ 39

Includes psychological factors; individual and group behavior: crew training and evaluation, and psychiatric

research.

54 MAN/SYSTEM TECHNOLOGY AND LIFE SUPPORT ................. ............................. ............. . , 40

Includes human engineering; biotechnology: and space suits and protective clothing. For related information

see also 16 Space Transportation.

55 S P A C E B IO L O G Y ............................................... ................ .................... .. 4 1................ 1

Includes exobiology; planetary biology; and extraterres t

rial life.

MATHEMATICAL AND COMPUTER SCIENCES

59 MATHEMATICAL AND COMPUTER SCIENCES (GENERAL) ...................... ........ ............ .... 41

60 COMPUTER OPERATIONS AND HARDWARE . ............................... ............................... N.A.

Includes hardware for computer graphics, firmware, and data processing, For components see 33 Electronics

and Electrical Engineering.

61 COMPUTER PROGRAMMING AND SOFTWARE .............. ................................................ .... .... 42

Includes computer rograms, routines, algorithms, and specific applications. e.g., CAD/CAM.

6 2 C O M P U T E R S Y S T E M S . . . . .42..................................................... ................................... ... ............ 4 2

Includes computer networks and special application computer systems.

Vii
6 3 C Y B E R N E T IC S .......... ..... ...... .. . . ................................... ..................................... . 43............. 4 3

Includes feedback and control theory, artificial intelligence, robotics and expert systems. For related information see also 54 Man/System Technology and Lite Support.

64 NUMERICAL ANALYSIS ..................................................... N.A.

Includes iteration, difference equations, and numerical approximation.

65 STATISTIC S A N D PR O BA B ILITY .................. ................................. .............................................. 43

Includes data sampling and smoothing; Monte Carlo method; and stochastc processes,

66 S Y S T E M S A N A LY S IS ..................... ................................................... .............................. ................. 43

Includes mathematical modeling; network analysis; and operations research.

67 THEORETICAL MATHEMATICS .............................................. ........ N.A.

Includes topology ana number theory.

PHYSICS For related information see also Engineering.

70 P H Y S IC S (G E N E R A L ) .............................................. ..................... ......... .... ... 4-.................................

44

For precision time and time interval (PTTI) see 35 Instrumentation and Photography: for geophysics.

astrophysics or solar physics see 46 Geophysics, 90 Astrophysics. or 92 Solar Physics.

71 ACOUSTICS ....................................................... ........................................ ............. 44

Includes sound generation, transmission, and attenuation, For noise pollution see 45 Environment Pollution

72 ATOMIC AND MOLECULAR PHYSICS ................................ ................................ N.A.

Includes atomic structure, electron properties, and molecular spectra,

73 NUCLEAR AND HIGH-ENERGY PHYSICS.......................... .................... ................ 46

Includes elementary and nuclear particles: and reactor theory For space radiation see 93 Space Radiation.

7 4 O P T IC S ........ .............................................. .......................... ....... ............ . . .. . 4 6

Includes light phenomena and optical devices For lasers see 36 Lasers and Masers

75 PLASMA PHYSICS .............................................. ..... .... 46

Includes magnetohydrodynamics and plasma fusion. For ionospheric plasmas see 46 Geophvsics. For space

plasmas see 90 Astrophysics.

76 S O L ID -S TA T E P H Y S IC S ................................. ............................ .. 4................6............... 46

Includes superconductivity. For related information see also 33 Electronics and Electrical Engineering and 36

Lasers and Masers

77 THERMODYNAMICS AND STATISTICAL PHYSICS ............................................ N.A.

Includes quantum mechanics; theoretical physics. and Bose and Fermi statistics. For related information see

also 25 Inorganic and Physical Chemistry and 34 Fluid Mechanics and Heat Transfer

SOCIAL SCIENCES

80 S O C IA L S C IE N C E S (G E N E R A L) .. .. ... ....... ........ ....... ...... ..... ........... ................................. N .A . Includes educational matters.

81 ADM IN ISTRATIO N AND M AN AG EM ENT ........... .................. ............................ .... .. 4.................6.... 46

Includes management planning and research.

82 DOCUMENTATION AND INFORMATION SCIENCE ............ ............ . ......... . 47

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 . ....... ... ...... ............. ....... .. . N.A.

Includes cost effectiveness studies.

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 ....... N.A.

Includes applications of space technology to urban problems, technology transfer: technology assessment.

and surface and mass transportation For related information see 03 Air Tr..nsportation and Safety 16 Space

Transportation. and 44 Energy Production and Conversion.

ViII
SPACE SCIENCES For related information see also Geosciences,

88 SPACE SCIENCES (GENERAL) ....... 48........................ 48

8 9 A S T R O N O M Y ........... ... ..... ........... ............. . ... 4..........9................................. 4 9

Includes radio, gamma-ray, and infrared astronomy: and astrometry,

90 ASTROPHYSICS ... ................. 4......... 49

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 ..... .. ............ .. ..... 49

Includes planetology; and manned and unmanned flights. For spacecraft design or space stations see 18

Spacecra.ft Design, Testing and Performance.

92 SOLAR PHYSICS ......................... ... ................ 50

Includes solar activity, solar flares, solar radiation and sunspots. For related information see 93 Space Radiation

9 3 S P A C E R A D IA T IO N . .. .. .... .. ....... .... ........ ... .... ... .... ..... .. ..... ... .. ........ ..................... . 5.. 5 0

Includes cosmic radiation; and inner and outer earths 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 .. . ... . . ."..I..... 51

SUBJECT INDEX ............................................ . ... . .. ..................... .. .......... 1APE R S O N A L A U TH O R ......................... IN D EX ... ............ .... ...... .. . ... ... ............. ....... ...... B -1

R EPORT N UM BE R IND EX ............... .... .... C....................................i...... C -1

A P PE N D IX ... .P I X ....................... .. ................. ........ . ........................ ......... P C -1

Ix
TYPICAL CITATION AND ABSTRACT

NASA SPONSORED

ION MICROFICHE

ACCESSION NUMBER -- -N92-20063# National Aeronautics and Space Administralion. -- CORPORATE SOURCE

Goddard Space Flight Center. Greenbelt, MD

TITLE - . LONG-TERM LIFE TESTING OF GEOSTATIONARY

OPERATIONAL ENVIRONMENTAL SATELLITE (GOES)

ENCODER LAMPS

AUTHOR --- CHARLES E. POWERS Feb. 1992 120 p

(RTOP 030-09-01-01) PUBLICATION DATE

REPORT NUMBERS (NASA-RP-1273: REPT-92300013: I\AS 1.61 1273) Availý CASI - AVAILABILITY SOURCE

HC A06/MF A02

PRICE CODE -- The aging characteristics and lifetimes of tungsten filament

encoder lamps were determined as a function of operating voltage

and filament matenal. For pure tungsten and thoria doped (lpct.)

filament lamps. crystal grain growth over the center portion of the

filament leads to the ultimate failJre of the lamp. The development

of notches associated with this grain growth is the cause of lamp

burn out. Eventually, one of the notches will 'etch' through the filament,

causing it to tail open. For rhenium doped (3 pct.) filament lamps,

distortion of the filament lea(- to the ultimate failure of the lamp. The

lifetime of these lamps is at .ul 1 year at an operating voltage of 5.0

volts. The pure tungsten filament 13amps have the longest average

lifetime, and the thoria doped filament lamps have the shortest at 5.0

volts. The lifetimes of these lamps is about 7 ywars at an operating

voltage of 3.5 volts. Data suggest that the rhenium doped lamps will

have the longest average lifetime at 3.5 volts, and the thoria doped

will have the shortest. These lifetimes are comparable to the desired

lifetimes of 7 years. Author

TYPICAL CITATION AND SUBJECT TERMS

NASA SPONSORED

ON MICROFICHE

ACCESSION NUMBER---N92-31640*# National Aeronaut:;,s and Space Administration.-- CORPORATE SOURCE

Lewis Research Center, Cleveland, OH.

TITLE - SUPERSONIC THROUGHFLOW FAN TEST FACILITY AT

NASA. LEWIS RESEARCH CENTER

AUTHORS --- DONALD C. URASEK, WALTER S. CUNNAN. RICHARD L. LANTZ,

DENNIS L. FRONEK, RONALD A. DAWSON, and JEFFREY C.

BROWN Sep. 1990I,25 p

(RTOP 505-f -61) PUBLICATION DATE

REPORT NUMBERS -------- (NASA-TP-3038: E-53981 NAS 1.60:3038) Avail: CASI HC

PRICE CODE - A03/MF A01 ' - AVAILABILITY SOURCE

PROPULSION SYSTEM CONFIGURATIONS. PROPULSION

SYSTEM PERFORMANCE. SUPERSONIC FLOW. SUPERSONIC

SPEED, SUPERSONIC TEST APPARATUS, SUPERSONIC

TURBINES, SUPERS...C. ',ND TUNNELS, TURBOFANS. WIND

TUNNEL DRIVES
SCIENTIFIC AND

TECHNICAL PUBLICATIONS 1991-1992

February 1993

01 components, equipment and systems; ground support systems:

and theoretical and applied aspects of aerodynamics and general A

AERONAUTICS (GENERAL) fluid dynamics. Author

N91-15979 National Aeronautics and Space Administration,

Washington, DC. R

AERONAUTICAL ENGINEERING: A CONTINUING

N91-10002" National Aeronautics and Space Administration, BIBLIOGRAPHY WITH INDEXES (SUPPLEMENT 259) A

Washington, NCa Dec. 1990 202 p C

AERONAUTICAL ENGINEERING: A CONTINUING (NASA-SP-7037(259); NAS 1.21:7037(259)) Avail: CASI HC A10 T

AEBLIORO ALHY ENGHINDEXERIG ASUPPLENTINUThis bibliography lists 774 reports, articles, and other documents S

BIBLIOGRAPHY WITH INDEXES (SUPPLEMENT 256) introduced into the NASA scientific and technical information

Sep. 1990 129 p

(NASA-SP-7037(256); NAS 1.21:7037(256)) Avail: CASI HC A07 system in November, 1990. Subject coverage includes: design,

This bibliography lists 426 reports, articles, and other documents construction and testing of aircraft and aircraft engines: aircraft

introduced into the NASA scientific and technical information components, equipment and systems; ground support systems'

system in August 1990. Subject coverage includes: design, and theoretical and applied aspects of aerodynamics and general

construction and testing of aircraft and aircraft engines; aircraft fluid dynamics. Author

components, equipment and systems; ground support systems;

and theoretical and applied aspects of aerodynamics and general N91-19024*# National Aeronautics and Space Adminstration.

fluid dynamics. Author Langley Research Center, Hampton, VA.

JOINT UNIVERSITY PROGRAM FOR AIR TRANSPORTATION

N911- 12589 National Aeronautics and Space Administration, RESEARCH, 1989-1990 Washington, DC. FREDERICK R. MORRELL, comp. Washingi,")n Dec. 1990

AERONAUTICAL ENGINEERING: A CONTINUING 183 p Conference held in Athens, OH, 14-15 Jun. 1990:

BIBLIOGRAPHY WITH INDEXES (SUPPLEMENT 257) sponsored by NASA and FAA

Oct. 1990 156 p (RTOP 505-66-01-02)

(NASA-SP-7037(257); NAS 1.21:7037(257)) Avail: CASI HC A08 (NASA-CP-3095; L-16848; NAS 1.55:3095) Avail: CASI HC

This bibliography lists 560 reports, articles, and other documents A09/MF A02

introduced into the NASA scientific and technical information AIR TRANSPORTATION, AIRCRAFT PERFORMANCE,

system in September 1990. Subject coverage includes: design, AVIONICS, CONTROL THEORY, EXPERT SYSTEMS, GUIDANCE

construction and testing of aircraft and aircraft engines; aircraft (MOTION). NAVIGATION, UNIVERSITY PROGRAM

components, equipment and systems; ground support systems;

and theoretical and applied aspects of aerodynamics and general N91-23073' National Aeronautics and Space Administration,

fluid dynamics. Author Washington, DC.

AERONAUTICAL ENGINEERING: A CUMULATIVE INDEX TO A

N91-13399* National Aeronautics and Space Administration, CONTINUING BIBLIOGRAPHY (SUPPLEMENT 261)

Washington, DC. Feb. 1991 562 p

AERONAUTICAL ENGINEERING: A CONTINUING (NASA-SP-7037(261); NAS 1.21:7037(261)) Avail: CASI HC A24

BIBLIOGRAPHY WITH INDEXES (SUPPLEMENT 258) This publication is a cummulative index to the at stracts

Dec. 1988 167 p contained in Supplements 249 through 260 of Aeronautical

(NASA-SP-7037(258); NAS 1.21:7037(258)) Avail: CASI HC A08 Engineering: A Continuing Bibliogiaphy. The bibliographic series is

This bibliography lists 536 reports, articles, and other documents compiled through the cooperative efforts of the American Institute

introduced into the NASA scientific and technical information of Aeronautics and Astronautics (AIAA) and the National

system in October 1990. Subject coverage includes: design, Aeronautics and Space Administration (NASA). Seven indexes are

construction and testing of aircraft and aircraft engines; aircraft included -- subject, personal author, corporate source, foreign

components, equipment and systems; ground support systems; technology, contract number. rer rt number and accession

and theoretical and applied aspects of aerodynamics and general number. Author

fluid dynamics. Author

N91-23074* National Aeror'iutics and Space Administration,

N91-15978 National Aeronautics and Space Administration, Washington, DC

Washington, DC. AERONAUTICAL ENGINEERING: A CONTINUING

AERONAUTICAL ENGINEERING: A CONTINUING BIBLIOGRAPHY WITH INDEXES (SUPPLEMENT 262)

BIBLIOGRAPHY WITH INDEXES (SUPPLEMENT 260) Feb. 1991 142 p

Jan. 1991 132 p (NASA-SP-7037(262); NAS 1.21:7037(262)) Avail: CASI HC A07

(NASA-SP-7037(260); NAS 1.21:7037(260)) Avail: CASI HC A07 This bibliography lists 474 reports, articles, and other documents

This bibliography lists 405 reports, articles, and other documents introduced into the NASA scientific and technical information

introduced into the NASA scientific and technical iformation system in Jan. 1991. Subject coverage includes: design,

system in December, 1990. Subject coverage includes: design, construction and testing of aircraft and aircraft engines; aircraft

construction and testing of aircraft and aircraft engines; aircraft components, equipment and systems; ground support systems:
01 AERONAUTICS (GENERAL)

and theoretical and applied aspects of aerodynamics and general N91-30077' National Aeronautics and Space Administration,

fluid dynamics Author Washington, DC

AERONAUTICAL ENGINEERING: A CONTINUING

N91-24095" National Aeronautics and Space Administration, BIBLIOGRAPHY WITH INDEXES (SUPPLEMENT 268)

Wa.hington, DC Aug 1991 131 p

AERONAUTICAL ENGINEERING: A CONTINUING (NASA-SP-7037(268), NAS 1 21 7037(268)) Avail CASi rHG A07

BIBLIOGRAPHY WITH INDEXES (SUPPLEMENT 265) This bibliography lists 406 reports, articles, and other documents

May 1991 152 p introduced into the NASA scientific and technical information

(NeSA-SP-7037(265); NAS 1,21:7037(265)) Avail: CASI HC A08 system in July, 1991 Subject coverage includes design,

This bibliogaphy tists 554 reports, articles, and other documents construction and testing of aircraft and aircraft engines, aircraft

introduced into the NASA scientific and technical information components, equipment and systems, ground support systems,

system in Apr 1991. Subject coverage includes design, and theoretical and applied aspects of aerodynamics and general

construction jnd testing of aircraft and aircraft engines, aircraft fluid dynamics Author

components, equipment and systems, ground support systems,

and theoretical and applied aspects of aerodynamics and general N92-10001* National Aeronautics and Space Administration.

fluid dynamics. Author Washington, DC

AERONAUTICAL ENGINEERING: A CONTINUING

N91-24096' National Aeronautics and Space Administration, BIBLIOGRAPHY WITH INDEXES (SUPPLEMENT 267)

Washington. DC Jul 1991 188 p

AERONAUTICAL ENGINEERING: A CONTINUING (NASA-SP-7037(267), NAS 1 21 7037(267)) Avail CASI HC A09

BIBLIOGRAPHY WITH INDEXES (SUPPLEMENT 263) This bibliography lists 661 reports, articles, and other documents

Mar. 1991 146 p introduced into the NASA scientific and technical information

(NASA-SP.7037(263), NAS 1 21 7037(263)) Avail CASI HC A07 system in June, 1991, Subject coverage includes design.

This bibliography lists 517 reports, articles, and other documents construction and testing of aircraft and aircraft engines, aircraft

introduced into the NASA scientific and technical information components, equipment and systems, ground support systems.

system in Feb 1991 Subject coverage includes, design, theoretical and applied aspects o0 aerodynamics and general tluid

construction and testing of aircraft and aircraft engines; aircraft dynamics, electrical engineering, aircraft control, remote sensing.

components, equipment and systems, ground support systems, computer sciences; nuclear physics, and social sciences Author

and theoretical and applied aspects of aerodynamics and general

fluid dynamics Author

N92-10973" National Aeronautics and Space Administration,

N91-24097° National Aeronautics and Space Administration. Washington, DC

Washington DC AERONAUTICAL ENGINEERING: A CONTINUING

AERONAUTICAL ENGINEERING: A CONTINUING BIBLIOGRAPHY WITH INDEXES (SUPPLEMENT 270)

BIBLIOGRAPHY WITH INDEXES (SUPPLEMENT 264) Oct 1991 176 p

Apr 1991 159 p (NASA-SP-7037(270); NAS 1,21 7037(270)) Avail CASI HC A09

(NASA-SP-7037(264) NAS 1 21 7037(264)) Avail' GAS HC A08 This bibliography lists 600 reports, articles, and other documents

This bibliography lists 558 reports, articles, and other documents introduced into the NASA scientific and technical information

introduced into the NASA scientific and technical information system in September, 1991 Subject coverage includes design.

system in Mar 1991 Subtect coverage includes: d..sign. construction and testing of aircraft and aircraft engines. aircraft

construction and testing of aircraft and aircraft engines: aircraft components, equipment and systems, ground support systems.

components, equipment and systems; ground support systems, and theoretical and applied aspects of aerodynamics and gcneral

and theoretical and applied aspects of aerodynamics and general fluid dynamics Author

fluid dynamics Author

N92-10974" National Aeronautics and Space Administration. N91-26113"# Nan.onaI Aeronautics and Space Administration, Washington. DC

Hugh L Dryden Flight Research Facility, Edwards, CA AERONAUTICAL ENGINEERING: A CONTINUING

DEVELOPMENT OF AN INTEGRATED AE93SERVOELASTIC BIBLIOGRAPHY WITH INDEXES (SUPPLEMENT 269) ANALYSIS PF3GRAM AND CORRELATION WITH TEST DATA Sep. 1991 153 p

K K GUPTA. M J BRENNER, and L S VOELKER (NASA-SP-7037(269) NAS 1,21'7037(269)? Avail CASI HC A08

Washington May 1991 105 p This bibliography lists 539 reports, articles, and other documents

(RTOP 53302-51) introduced into the NAS.A scientific and terhnr'aI information

(NASA-TP-3120, H-1543; NAS 1603120) Avail: CASI HC system in August, 1991. Subtect coverage includes: design,

A06/MF A02 construction and testing of aircraft and aircraft engines. aircraft

AEROELASTICITY. COMPUTER PROGRAMS, DYNAMIC components, equipment and systems. ground support systems,

RESPONSE. DYNAMIC STRUCTURAL ANALYSIS, FINITE and theoretical and applied aspects of aerodynamics and general

ELEMENT METHOD, FLIGHT CONTROL, MATHEMATICAL fluid dynamics. Author

MODELS. SERVOCONTROL, STRESS ANALYSIS

N91-27122" National Aeronautics and Space Administration, N92-14967° National Aeronautics and Space Administration.

Washington. DC Waahington DC.

AERONAUTICAL ENGINEERING: A CONTINUING AERONAUTICAL ENGINEERING: A CONTINUING

BIBLIOGRAPHY WITH INDEXES (SUPPLEMENT 266) BIBLIOGRAPHY WITH INDEXES (SUPPLEMENT 271)

Jun 1991 175 p Nov. 1991 184 p

(NASA-SP-7037(266). NAS 1.21 7037(266), (NASA-SP-7037(271). NAS 1.21:7037(271)) Avail CASI HC A09

This bibliography listr. 645 reports, articles, and other documents This bibliography lists 666 reports, articles, and other documents

introduced into the NASA scientific and technical information introduced into the NASA scientific and technical information

system in May 1991 Subject coverage includes design. system in October, 1991. Subject coverage includes design.

construction and testing of aircraft and aircratt engines, aircraft construction and testing of aircraft and aircraft engines, aircraft

components, equipment and systems. ground sup'ort systems; components, equipment and systems, ground suppol systems.

and theoretical and applied aspects of aerodynamics and general and theoretical and applied aspects of aerodynamics and general

fluid dynamics Author fluid dynamics Author

2
02 AERODYNAMICS

N92-17984"# National Aeronautics and Space Adminis!-ation. N92-27929' National Aeronautics and Space Administration.

Langley Research Center, Hampton, VA. Washington, DC

JOINT UNIVERSITY PROGRAM FOR AIR TRANSPORTATION AERONAUTICAL ENGINEERING: A CONTINUING

RESEARCH, 1990-1991 BIBLIOGRAPHY WITH INDEXES (SUPPLEMENT 277)

FREDERICK A. MORRELL, comp. Washington Dec. 1991 Apr 1992 137 p

183 p Conference held in Athens, OH, 20-21 Jun. 1991, (NASA-SP-7037(277): NAS 1 21.7037(277)) Avail CASI HC A07

sponsored by NASA and FAA This bibliography lists 467 reports, articles, and other documents

(RTOP 505-64-52-01) introduced into the NASA scientific and technical information

(NASA-CP-3131; L-17017; NAS 1.55:3131) Avail: CASI HC system in Mar. 1992 Subject coverage includes, the engineering

A09/MF A02 and theoretical aspects of design, construction. evaluation, testing,

AIR TRANSPORTATION, AIRCRAFT SAFET'i. NATIONAL operation, and performance of aircraft (including aircraft engines).

AIRSPACE SYSTEM, NAVIGATION, UNIVERSITY PROGRAM and associated aircraft components. equipment, and systems It

also includes research and development in ground support systems.

N92-21729" National Aeronautics and Space Administration, theoretical and applied aspects of aerodynamics, and general fluid

Washington, DC. dynamics. Aut? :r

AERONAUTICAL ENGINEERING: A CONTINUING

BIBLIOGRAPHY WITH INDEXES (SUPPLEMENT 273) N92-28677' National Aeronautics and Space Administration.

Jan. 1992 219 p Washington, DC.

(NASA-SP-7037(273); NAS 1,21:7037(273)) Avail: CASI HC A10 AERONAUTICAL ENGINEERING: A CONTINUING

This bibliography lists 808 reports, articles, and other documents BIBLIOGRAPHY WITH INDEXES (SUPPLEMENT 278)

introduced into the NASA scientific and technical information f.'ay 1992 128 p

system in Dec. 1991. Subject coverage includes: design, •NASA-SP-7037(278); NAS 1 21:7037(278)) Avail CASI HC A07

construction and testing of aircraft and aircraft engines; aircraft This bibliography lists 414 reports, articles, and other documents

components, equipment, and systems; ground support systems, introduced into the NASA scientific and technical information

and theoretical and apolied aspects of aerodynamics and general system in April 1992 Author

fluid dynamics. Author

N92-28679' National Aeronautics and Space Administration.

N92-21844" National Aeionautics and Space Administration, Washington, DC

Washington, DC. AERONAUTICAL ENGINEERING: A CONTINUING

AERONAUTICAL ENGINEERING: A CONTINUING BIBLIOGRAPHY WITH INDEXES (SUPPLEMENT 275)

BIBLIOGRAPHY WITH INDEXES (SUPPLEMENT 272) Feb. 1992 112 p

Dec. 1991 192 p (NASA-SP-7037(275): NAS 1.21 7037(275)) Avail. CASI HC A06

(NASA-SP-7037(272); NAS 1.21:7037(272)) Avail: CASI HC A09 This bibliography lists 379 reports, articles, and other documents

This bibliography lists 719 reports, articles, and other documents introduced into the NASA scientific and technical information

itroduced into the NASA scientific and technical information system in Jan. 1991. Author

system in Novembe:., 1991. Subject coverage includes: design.

construction and testing of aircraft and aircraft engines; aircraft N92-314566 National Aeronautics and Space Admirstration.

components, equipment, and systems; ground support systems; Washington, DC,

and theoretical and applied aspects of aerodynamics and general AERONAUTICAL ENGINEERING: A CONTINUING

fluid dynamics. Author BIBLIOGRAPHY WITH INDEXES (SUPPLEMENT 280)

Jul. 1992 172 p

N92-22505°# National Aeronautics and Space Administration. (NASA-SP-703:(280). NAS 1.21.7037(280)) Avail CASI HC A08

Langley Research Center, Hampton, VA. This bibliography lists 647 reports, articles, and other documents

THE HIGH RESOLUTION ACCELEROMETER PACKAGE introduced into the NASA scientific and technical information

(HIRAP) FLIGHT EXPERIMENT SUMMARY FOR THE FIRST 10 system in June. 1991. Subject coverage includes aerodynamics.

FLIGHTS air transportation salety, aircraft communication and navigation.

ROBERT C. BLANCHARD (Lockheed Engineering and Sciences aircraft design and performance, aircraft instrumentation, aircraft

Co., Hampton, VA.), K. T. LARMAN, and M. BARRETT (Lockheed propulsion, aircraft stability and control, research facilities,

Engineering and Sciences Co., Hampton, VA.) Apr. 1992 astronautics, chemistry and materials, engineering, geosciences.

318 p computer sciences, physics, and social sciences Author

(RTOP 506-48-11 -011

(NASA.RP-1267; L-16900; NAS 1.61:1267) Avail: CASI HC

A14/MF A03 02

Tihe High Resolution Accelerometer Package (HiRAP)

instrument is a triaxial, orthogonal system of gas damped

accelerometers with a resolution of 1 x 10(exp -6) g (1 micro-g). AERODYNAMICS

The purpose of HiRAP is to measure the low frequency component

of the total acceleration along the orbiter vehicle (OV) body axes Includes aerodynamics of bodies, combinations, wings. rotors, and

while the OV descends through the rarefied flow flight regime. control surfaces; and internal flow in ducts and turbomachinery. Two HiRAP instruments have flown on a total of 10 Space Transport System (STS) missions. The aerodynamic component of the

acceleration measurements was separated from the total N91-10007"# National Aeronautics and Space Administration

acceleration. Instrument bias and orbiter mechanical system Ames Research Center, Moffett Field, CAr

acceleration effects were incorporated into one bulk bias. The TRANSONIC FLOW ANALYSIS FOR ROTORS. PART 3:

bulk bias was subtracted from the acceleration measurements to THREE-DIMENSIONAL, QUASI-STEADY, EULER

produce aerodynamic descent data sets for all 10 flights. The CALCULATION

aerodynamic acceleration data sets were input to an aerodynamic I-CHUNG CHANG Jun. 1990 23 p

coefficient model. The aerodynamic acceleration data and (RTOP 505-61-51)

coefficient model were used to estimate the atmospheric density (NASA-TP-2375; A-86374.PT.3, NAS 1.60:2375) Avail CASI HC

for the altitude range of 140 to 60 km and a downrange distance A03/MF A01

of 600 km. For 8 of 10 flights results from this model agree with COMPUTER PROGRAMS. EULER EOUATIONS OF MOTION.

expected results For the results that do not agree with expected FINITE VOLUME METHOD, LIFTING ROTORS, ROTOR

results, a variety of error sources have been explored. Author AERODYNAMICS, TRANSONIC FLOW

3
02 AERODYNAMICS

N91-10839"# National Aeronautics and Space Administration. (NASA-TP-3047, L-16743, NAS 1 60 3047) Avail CASI HC

Ames Research Center, Moffett Field, CA. A05/MF A02

NASA COMPUTATIONAL FLUID DYNAMICS CONFERENCE. AERODYNAMIC INTERFERENCE. AIRCRAFT DESIGN.

VOLUME 1: SESSIONS 1-6 ENGINE AIRFRAME INTEGRATION, TRANSPORT AIRCRAFT,

Sep. 1989 475 p Conference held at Moffett Field, CA. 7-9 WING NACELLE CONFIGURATIONS

Mar. 1989 Original contains color illustrations

(RTOP 505-60-01) N9t-14316"# National Aeronautics and Space Administration

(NASA-CP-10038-VOL-1; A-89160-VOL-1; NAS Langley Research Center. Hampton, VA

1.55:10038-VOL-1) Avail: CASt HC A20/MF A04; 25 functional PARAMETRIC STUDY OF AFTERBODY/NOZZLE DRAG ON

color pages TWIN TWO-DIMENSIONAL CONVERGENT-DIVERGENT

COMPUTATIONAL FLUID DYNAMICS, COMPUTATIONAL NOZZLES AT MACH NUMBERS FROM 0.60 TO 1.20

GRIDS, CONFERENCES. GRID GENERATION (MATHEMATICS), ODIS C. PENDERGRAFT, JR, JAMES R BURLEY. II. and E

MATHEMATICAL MODELS. SIMULATION, SUPERCOMPUTERS, ANN BARE Oct. 1986 267 p

TURBULENCE MODELS (RTOP 505-62-91 -01)

(NASA.TP.2640: L-16158. NAS 1 602640) Avail: CASI HC

N91-10868"# National Aeronautics and Space Administration. A12/MF A03

Ames Research Center, Moffett Field, CA, AERODYNAMIC COEFFICIENTS, AFTERBODIES. CONVERNASA COMPUTATIONAL FLUID DYNAMICS CONFERENCE. GENT-DIVERGENT NOZZLES, DRAG MEASUREMENT

VOLUME 2: SESSIONS 7-12 PARAMETERIZATION

Sep. 1989 525 p Conference held at Moffett Field, CA, 7-9

Mar, 1989 Original contains color illustrations N91-16990*# National Aeronautics and Space Administration

(RTOP 505-60-01) Langley Research Center, Hampton, VA.

(NASA-CP-10038-VOL-2; A-89160-VOL-2; NAS A PARAMETRIC EXPERIMENTAL INVESTIGATION OF A

1,55:10038-VOL-2) Avail: CASI HC A22/MF A04; 30 functional SCRAMJET NOZZLE AT MACH 6 WITH FREON AND ARGON

color pages OR AIR USED FOR EXHAUST SIMULATION

ALGORITHMS, COMPUTATIONAL FLUID DYNAMICS, JAMES M. CUBBAGE (Vigyan Research Associates, Inc , Hampton,

CONFERENCES, HYPERSONICS, SHORT TAKEOFF AIRCRAFT, VA.) and WILLIAM J. MONTA Washington Feb. 1991 106 p

SPACECRAFT DESIGN, SUPERCOMPUTERS (RTOP 763-01-31-24)

(NASA-TP-3048; L-16707; NAS 1.60:3048) Avail CASI HC

N91-10902*# National Aeronautics and Space Administration. A06/MF A02

Langley Research Center, Hampton, VA. EXHAUST FLOW SIMULATION. EXHAUST GASES, EXHAUST

PREDICTION OF EFFECTS OF WING CONTOUR NOZZLES, FLOW DISTRIBUTION, NOZZLE FLOW, SUPERSONIC

MODIFICATIONS ON LOW-SPEED MAXIMUM LIFT AND COMBUSTION RAMJET ENGINES

TRANSONIC PERFORMANCE FOR THE EA-6B AIRCRAFT

DENNIS 0. ALLISON and E. G. WAGGONER Washington Nov- N91-18030"# National Aeronautics and Space Administration.

1990 48 p Langley Research Center, Hampton, VA.

(RTOP 505-61-21-03) DETAILED FLOW-FIELD MEASUREMENTS OVER A 75 DEG

(NASA-TP-3046; L-16741; NAS 1.60:3046) Avail: CASI HC SWEPT DELTA WING

A03/MF A01 SCOTT 0. KJELGAARD and WILLIAM L SELLERS, III

COMPUTER PROGRAMS, CONTOURS, MANEUVERABILITY, Washington Oct. 1990 45 p Original contains color

PANEL METHOD (FLUID DYNAMICS), PERFORMANCE illustrations

PREDICTION, TRANSONIC FLOW, WIND TUNNEL TESTS, WING (RTOP 505-60-11-03)

PROFILES (NASA-TP-2997; L-16718, NAS 1.60:2997) Avail: CASI HC

A03/MF AO; 16 functional color pages N91-13401"# National Aeronautics and Space Administration. DELTA WINGS. FLOW DISTRIBUTION, FLOW

Langley Research Center, Hampton, VA. VISUALIZATION, FREE FLOW. JET FLOW. SWEPT WINGS,

NAVIER-STOKES AND EULER SOLUTIONS FOR LEE-SIDE VORTICES

FLOWS OVER SUPERSONIC DELTA WINGS. A

CORRELATION WITH EXPERIMENT N91-18031"# National Aeronautics and Space Administration

S. NAOMI MCMILLIN (National Aeronautics and Space Langley Research Center, Hampton, VA.

Administration. Langley Research Center, Hampton, VA.), JAMES PHYSICALLY WEIGHTED APPROXIMATIONS OF UNSTEADY

L. THOMAS (National Aeronautics and Space Administration. AERODYNAMIC FORCES USING THE MINIMUM-STATE

Langley Research Center, Hampton, VA.). and EARLL M. MURMAN METHOD

(Massachusetts inst. of Tech., Cambridge.) Washi.gton Dec. MORDECHAY KARPEL (Technion - Israel Inst. of Tech. Haifa)

1990 103 p Original contains color illustrations and SHERWOOD TIFFANY HOADLEY Washington Mar 1991

(RTOP 505-61-71-01) 46 p

(NASA-TP-3035; L-16751; NAS 1.60:3035) Avail: CASI HC (RTOP 505-63-21.04)

A06/MF A02; 19 functional color pages (NASA-TP-3025: L-16491; NAS 1.60:3025) Avail: CASI HC

COMPUTER PROGRAMS, DELTA WINGS. EULER A03/MF A01

EQUATIONS OF MOTION, FLOW DISTRIBUTION, AERODYNAMIC COEFFICIENTS, COMPUTER PROGRAMS,

NAVIER-STOKES EQUATION. SUPERSONIC FLOW LEAST SQUARES METHOD, MATRICES (MATHEMATICS).

UNSTEADY AERODYNAMICS

N91-13402"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, VA. N91-18032"# National Aeronautics and Space Administration.

EFFECT OF LOCATION OF AFT-MOUNTED NACELLES ON Langley Research Center, Hampton, VA

THE LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF AN EXPLICIT UPWIND ALGORITHM FOR SOLVING THE

A HIGH-WING TRANSPORT AIRPLANE PARABOLIZED NAVIER-STOKES EQUATIONS

WILLIAM K. ABEYOUNIS (National Aeronautics and Space JOHN J KORTE Washington Feb 1991 71 p Original

Administration. Langley Research Center, Hampton, VA.) and contains color illustrations

JAMES C. PATTERSON, JR. (Vigyan Research Associates, Inc., (RTOP 506-80-11-01)

Hampton, VA.) Washington Dec. 1990 98 p (NASA-TP-3050. _-167531 NAS 1.60:3050) Avail CASI HC

(RTOP 505-62-41-05) A04/MF A01, 1 functional color page

4
02 AERODYNAMICS

ALGORITHMS, FLOW DISTRIBUTION, GAS FLOW, contains color illustrations

HYPERSONIC FLOW, NAVIER-STOKES EQUATION, PARABOLIC (NASA-CP-3078, E-5296; NASA-CP-10045, NAS 1.55:3078)

DIFFERENTIAL EQUATIONS Avail: CASI HC A99/MF A06; 10 functional color pages

COMBUSTIBLE FLOW, COMBUSTION CHAMBERS,

N91-19042*# National Aeronautics and Space Administration. COMPUTATIONAL FLUID DYNAMICS, CONFERENCES, GRID

Langley Research Center, Hampton, VA. GENERATION (MATHEMATICS), PROPULSION SYS;TEM

EXPERIMENTAL INVESTIGATION OF POROUS-FLOOR PERFORMANCE, TURBOMACHINERY, TURBULENCE MODELS

EFFECTS ON CAVITY FLOW FIELDS AT SUPERSONIC

SPEEDS N91-22069*# National Aeronautics and Space Administration.

FLOYD J. WILCOX, JR. Washington Nov. 1990 105 p Langley Research Center, Hampton. VA

(RTOP 505-61-71-01) AEROPROPULSIVE CHARACTERISTICS OF CANTED TWIN

(NASA-TP-3032; L-16711; NAS 1.60:3032) Avail: CASI HC PITCH-VECTORING NOZZLES AT MACH 0.20 TO 1.20

A06/MF A02 FRANCIS J. CAPONE. MARY L. MASON, and GEORGE T.

CAVITIES, CAVITY FLOW. FLOW DISTRIBUTION, MACH CARSON, JR. Washington May 1991 257 p

NUMBER, POROSITY, SUPERSONIC SPEED, VENTS, WIND (RTOP 505-62-71-01)

TUNNEL MODELS (NASA-TP-3060; L-16823; NAS 1.60:3060) Avail. CASI HC

N91-1905 # National Aeronautics and Space Administration. A12/MF A03

Lewis Lewis Resear Research Center, entionalevelanautis Cleveland, OH. OH. SpCONVERGENT-DIVERGENT SURFACES), FLOW DISTRIBUTION, NOZZLES, NOZZLE FLAPS GEOMETRY. (CONTROL

THREE-COMPONENT LASER ANEMOMETER MEASUREMENT PROPULSIV FFIC TRUTIVECTOR CONTROL

SYSTEMS PROPULSIVE EFFICIENCY, THRUST VECTOR CONTROL

LOUIS J. GOLDMAN Washington Jan. 1991 20 p

(NASA-TP-3080; E-5526; NAS 1.60:3080) Avail: CASI HC N91-22070'# National Aeronautics and Space Administration

A03/MF A01 Langley Research Center, Hampton, VA.

ANNULAR FLOW, LASER ANEMOMETERS, LASER DOPPLER NUMERICAL STUDY OF THE AERODYNAMIC EFFECTS OF

VELOCIMETERS, LASER INTERFEROMETRY, THREE USING SULFUR HEXAFLUORIDE AS A TEST GAS IN WIND

DIMENSIONAL FLOW, TURBOMACHINERY TUNNELS

W. KYLE ANDERSON Washington Jan, 1991 26 p Previously

N91-19058*# National Aeronautics and Space Administration, announced in IAA as A90-37958

Ames Research Center, Moffett Field, CA. (RTOP 505-60-01-01)

PANEL METHODS: AN INTRODUCTION (NASA-TP-3086; L-16849; NAS 1.60:3086) Avail: CASI HC

LARRY L. ERICKSON Washington Dec. 1990 64 p A03/MF A01

(RTOP 505-60-21) AIRFOILS, INVISCID FLOW, SUBSONIC FLOW. SULFUR

(NASA-TP-2995; A-89266; NAS 1.60:2995) Avail: CASI HC FLUORIDES, TRANSONIC FLOW, TURBULENT FLOW. WIND

A04/MF A01 TUNNEL TESTS

BOUNDARY CONDITIONS, COMPUTER PROGRAMS,

INVISCID FLOW. PANEL METHOD (FLUID DYNAMICS), N91-24132"# National Aeronautics and Space Administration.

POTENTIAL FLOW, SUBSONIC SPEED, SUPERSONIC SPEED Langley Research Center, Hampton, VA.

TRANSONIC SYMPOSIUM: THEORY, APPLICATION AND

N91-20043"# National Aeronautics and Space Administration. EXPERIMENT, VOLUME 2

Langley Research Center, Hampton, VA. JEROME T. FOUGHNER, JR., comp. Apr. 1989 241 p

WALL-INTERFERENCE ASSESSMENT AND CORRECTIONS Symposium held in Hampton, VA, 19-21 Apr. 1988

FOR TRANSONIC NACA 0012 AIRFOIL DATA FROM VARIOUS (RTOP 505-60-11-01)

WIND TUNNELS M.S. Thesis - George Washington Univ., 1988 (NASA-CP-3020-VOL-2; L-16502-VOL-2, NAS 1.55:3020-VOL-2)

LAWRENCE L. GREEN and PERRY A. NEWMAN Apr 1991 Avail: CASI HC A11/MF A03

63 p Presented at AIAA Meeting, Honolulu, HI, 8-10 Jun. 1987 AERODYNAMIC CHARACTERISTICS. AIRCRAFT DESIGN,

(RTOP 505-61-01-04) BODY-WING CONFIGURATIONS, COMPUTATIONAL FLUID

(NASA-TP-3070; L-16721; NAS 1.60:3070; AIAA PAPER 87-1431) DYNAMICS, FLIGHT TESTS, TRANSONIC FLOW, WIND TUNNEL

Avail: CASI HC A04/MF A01 TESTS

AERODYNAMIC INTERFERENCE, AIRFOIL PROFILES,

BOUNDARY LAYER FLOW, TRANSONIC FLOW, WALL FLOW, N91-25103*# National Aeronautics and Space Administration.

WIND TUNNEL WALLS Langley Research Center, Hampton, VA.

N91-21059"# National Aeronautics and Space Administration. LOW-SPEEO, POWERED GROUND EFFECTS OF A GENERIC,

Langley Research Center, Hampton, VA HYPERSONIC CONFIGURATION

STATIC THRUST-VECTORING PERFORMANCE OF GREGORY M GATLIN 1990 62 p

NONAXISYMMETRIC CONVERGENT-DIVERGENT NOZZLES (RTOP 763-01-31-22)

WITH POST-EXIT YAW VANES M.S. Thesis - George (NASA-TP-3092; L-16861; NAS 1.60:3092) Avail. CASI HC

Washington Univ., Aug. 1988 AO4/MF A01

ROBERT J. FOLEY (George Washington Univ., Washington, DC.) AERODYNAMIC CHARACTERISTICS, AIRCRAFT MODELS.

and ODIS C. PENDERGRAFT, JR. May 1991 81 p GROUND EFFECT (AERODYNAMICS), HYPERSONIC AIRCRAFT,

(RTOP 505-62-71-01) LOW SPEED, SCALE MODELS, WIND TUNNEL TESTS

(NASA-TP-3085; L-16784; NAS 1.60:3085) Avail: CASI HC

A05/MF A01 N91-27124'# National Aeronautics and Space Administration

CONVERGENT-DIVERGENT NOZZLES, JET VANES, NOZZLE Langley Research Center, Hampton, VA

GEOMFTRY, STATIC TESTS, STATIC THRUST, THRUST EFFECTS OF YAW ANGLE AND REYNOLDS NUMBER ON

VECTOR CONTROL, YAW RECTANGULAR-BOX CAVITIES AT SUBSONIC AND

TRANSONIC SPEEDS

N91-21062"# National Aeronautics and Space Administration. E. B. PLENTOVICH, JULIO CHU, and M. B. TRACY Washington

Lewis Research Center, Cleveland, OH. Jul. 1991 54 p

COMPUTATIONAL FLUID DYNAMICS SYMPOSIUM ON 'r,TOP 505-68-91-12)

AEROPROPULSION (NASA-TP-3099: L-16847; NAS 1.60:3099) Avail: CASI HC

Washington Jan. 1991 687 p Symposium held in Cleveland, A04/MF A01

OH, 24-26 Apr. 1990 Supersedes NASA-CP-10045 Original CAVITIES, FLOW DISTRIBUTION. HIGH REYNOLDS NUMBER,

5
02 AERODYNAMICS

MACH NUMBER, PRESSURE DISTRIBUTION, SUBSONIC FLOW. CAVITIES. EXTERNAL STORE SEPARATION, FLAT PLATES,

TRANSONIC FLOW, YAW FLOW DISTRIBUTION. MOMENTS. PRESSURE MEASUREMENT.

SUPERSONIC SPEED

N9 1-27140"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, VA. N92-10Ol1 # National Aeronautics and Space Administration

SHOCK WAVE INTERACTION WITH AN ABRUPT AREA Ames Research Center. Motfett Field. CA

CHANGE TRANSONIC AND SUPERSONIC EULER COMPUTATIONS OF

MANUEL D. SALAS Washington Aug. 1991 16 p VORTEX-DOMINATED FLOW FIELDS ABOUT A GENERIC

(RTOP 505-62-31-07) FIGHTER

(NASA-TP-3113; L-16878; NAS 1.60:3113) Avail: CASI HC AGA M. GOODSELL and JOHN E. MELTON Nov 1991 44 p

A03/MF A01 (RTOP 505-60-11)

COMPUTATIONAL FLUID DYNAMICS, EULER EQUATIONS OF (NASA-TP-3156; A-90161; NAS 1 60:3156) Avail: CASI HC

MOTION, MATHEMATICAL MODELS, NUMERICAL ANALYSIS, A03IMF A01

SHOCK WAVE INTERACTION. SHOCK WAVES, UNIQUENESS ANGLE OF ATTACK, BODY-WING CONFIGURATIONS, EULER

THEOREM EQUATIONS OF MOTION, FIGHTER AIRCRAFT. FLOW

DISTRIBUTION. PRESSURE DISTRIBUTION

N91-28136"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, OH.

EVALUATION OF A TECHNIQUE TO GENERATE N92-10975"# National Aeronautics and Space Administration

ARTIFICIALLY THICKENED BOUNDARY LAYERS IN Langley Research Center, Hampton, VA.

SUPERSONIC AND HYPERSONIC FLOWS STATIC INTERNAL PERFORMANCE OF VENTRAL AND REAR

A. R. PORRO (National Aeronautics and Space Administration. NOZZLE CONCEPTS FOR SHORT-TAKEOFF AND

Lewis Research Center, Cleveland, OH.). W. R. HINGST (National VERTICAL-LANDING AIRCRAFT

Aeronautics and Space Administration. Lewis Research Center, RICHARD J. RE and GEORGE T. CARSON. JR. Washington

Cleveland, OH.), D. 0. DAVIS (Washington Univ., Seattle.), and A' Sep. 1991 71 p

B. BLAIR. JR. (National Aeronautics and Space Administration. (RTOP 505-62-30-01)

Langey eserchCentr, amponVA.) Wasingon ug. (NASA-TP-3103: L-16902; NAS 1.60:3103) Avail: CASt HC

1991 28 p A4M ~ (RTOP 505-80-21) AIRCRAFT CONFIGURATIONS, EXHAUST NOZZLES.

(NASA-TP-3142; E-5660; NAS 1.60:3142) Avail: CASI HC EXHAUST SYSTEMS, FIGHTER AIRCRAFT, PROPULSION

A03/MF A01 SYSTEM CONFIGURATIONS. SHORT TAKEOFF AIRCRAFT,

BOUNDARY LAYERS, COMPRESSIBLE FLOW, HONEYCOMB VERTICAL LANDING

STRUCTURES, HYPERSONIC FLOW. SUPERSONIC FLOW,

TURBULENT BOUNDARY LAYER. WIND TUNNEL MODELS N92-10981'# National Aeronautics and Space Administration.

Ames Research Center, Moftett Field. CA.

N91-28143"# National Aeronautics and Space Administration. NACA 0015 WING PRESSURE AND TRAILING VORTEX

Langley Research Center. Hampton, VA. MEASUREMENTS

LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF A K, W. MCALISTER and R. K. TAKAHASHI Washington Nov.

SUBSONIC, ENERGY-EFFICIENT TRANSPORT 1991 141 p

CONFIGURATION IN THE NATIONAL TRANSONIC FACILITY (RTOP 505-61-51)

PETER F. JACOBS and BLAIR B. GLOSS Aug. 1989 70 p (NASA-TP-3151; A-91056; NAS 1.60:3151,

(RTOP 505-61 -21-03) AVSCOM-TR-91-A-003) Avail: CASI HC A07IMF A02

(NASA-TP-2922; L-16569; NAS 1 60:2922) Avail: CASI HC LOW SPEED, PRESSURE MEASUREMENT, SEMISPAN

A04/MF A0l MODELS, TRAILING EDGES. VELOCITY MEASUREMENT.

AEROELASTICITY, BOUNDARY LAYER TRANSITION, VORTICES, WING TIPS, WINGS

LONGITUDINAL STABILITY, NONADIABATIC CONDITIONS.

SUBSONIC SPEED, SUPERCRITICAL WINGS, WALL N92-12994"# National Aeronautics and Space Administration.

TEMPERATURE Langley Research Center, Hampton. VA.

WIND TUNNEL INVESTIGATION OF THE INTERACTION AND

N91-30098"# National Aeronautics and Space Administration. BREAKDOWN CHARACTERISTICS OF SLENDER WING

Langley Research Center, Hampton, VA.VOTCSTSUONTR SNIADUESNI

FULL-SCALE SEMISPAN TESTS OF A BUSINESS-JET WING VORTIEDS A USNC RNO ,ADSPROI

WITHA LAINARFLO NTURA AIROILGARY E. ERICKSON Washington Nov. 1991 226p

DAVID E. HAHNE and FRANK L. JORDAN. JR. Sep. 1991 (RTOP 505-68-71-03)

52 p (NASA-TP-31 14; L-16803; NAS 1.60:3114) Avail: CASt HC

(RTOP 505-61-41-01) A1M 0

(NASA-TP-3133; L.16905; NAS 1.60:3133) Avail: CASI HC AERODFNAM03 HRCEITC, ET IGFO

A04/M A01DISTRIBUTION. LASERS. LEADING EDGES, SLENDER WINGS.

AIRFOIL PROFILES. FLAPPING, FULL SCALE TESTS, JET VORTICES

AIRCRAFT, LAMINAR FLOW AIRFOILS, LOW SPEED, SEMISPAN

MODELS, WIND TUNNEL TESTS

N92-14968"# National Aeronautics and Space Administration

N92-10005"# National Aeronautics and Space Administration. Lewis Research Center, Cleveland, OH.

Langley Research Center, Hampton, VA. WIND TUNNEL INVESTIGATION OF VORTEX FLOWS ON

MEASUREMENTS OF FORCES, MOMENTS, AND PRESSURES F/A-IS CONFIGURATION AT SUBSONIC THROUGH

ON A GENERIC STORE SEPARATING FROM A BOX CAVITY TRANSONIC SPEED

AT SUPERSONIC SPEEDS GARY E. ERICKSON Washington Dec. 1991 166 p

ROBERT L. STALLINGS, JR. (Lockheed Engineering and Sciences (RTOP 505-68-30-03)

Co. Hampton, VA.), FLOYD J. WILCOX. JR., and DANA K. (NASA.TP.3111; L-16799; NAS 1.60:3111) Ava~i: CASI HC

FORREST Sep. 1991 186 p AOB/MF A02

(RTOP 505-68-91-12) F-l8 AIRCRAFT, FOREBODIES, INTERACTIONAL

(NASA-TP-31 10; L-16866; NAS 1.60:3110) Avail: CASt HC AERODYNAMICS. LEADING EDGES. VORTEX BREAKDOWN,

A09/MF A02 VORTICES. WIND TUNNEL TESTS, WINGS
02 AERODYNAMICS

N92-17131'# National Aeronautics and Space Administration- N92-20545"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, VA. Langley Research Center, Hampton, VA

TWO-DIMENSIONAL STABILITY OF LAMINAR FLAMES DIFFRACTED AND HEAD WAVES ASSOCIATED WITH WAVES

H. S. MUKUNDA and J. PHILIP DRUMMOND Washington Feb. ON NONSEPARABLE SURFACES

1992 30 p RAYMOND L. BARGER Apr 1992 17 p

(RTOP 763-01-21-16) (RTOP 505-59-53-01)

(NASA-TP-3131; L-16604; NAS 1.60:3131) Avail: CASI HC (NASA-TP-3169; L-16968; NAS 1.60-3169) Avail: CASI HC

A03/MF A01 A03/MF A01

ACTIVATION ENERGY, COMBUSTION CHEMISTRY, FLAME SURFACE WAVES, THIN WALLED SHELLS, WAVE

STABILITY, LAMINAR FLOW, LEWIS NUMBERS, PREMIXED DIFFRACTION

FLAMES

N92-23095 # National Aeronautics and Space Administration.

N92-19002"# National Aeronautics and Space Administration. Langley Research Center, Hampton, VA

Langley Research Center, Hampton, VA. STATIC PERFORMANCE OF A CRUCIFORM NOZZLE WITH

INSTALLATION EFFECTS OF WING-MOUNTED TURBOFAN MULTIAXIS THRUST-VECTORING AND REVERSE-THRUST

NACELLE-PYLONS ON A 1/17-SCALE, TWIN-ENGINE, CAPABILITIES

LOW-WING TRANSPORT MODEL DAVID J. WING and SCOTT C ASBURY Apr. 1992 82 p ODIS C. PENDERGRAFT, JR- (Aerospace Research Labs., (RTOP 505-62-30-01)

Wright-Patterson AFB, OH.), ANTHONY M. INGRALDI (Aerospace (NASA-TP-3188; L-16958; NAS 1.60:3188) Avail. CASI HC

Research Labs., Wright-Patterson AFB, OH.), RICHARD J. RE A05/MF A01

(Aerospace Research Labs., Wright-Patterson AFB, OH.), and CONVERGENT-DIVERGENT NOZZLES, PERFORMANCE

TIMMY T. KARIYA (Vigyan Research Associates, Inc., Hampton, TESTS, THRUST REVERSAL, THRUST VECTOR CONTROL, TWO

VA.) Mar. 1992 108 p DIMENSIONAL FLOW, WIND TUNNEL TESTS

(RTOP 535-03-10-01)

(NASA-TP-3168; L-16960; NAS 1.60:3168) Avail: CASI HC N92-25133"# National Aeronautics and Space Administration

A06/MF A02 Langley Research Center, Hampton, VA.

AERODYNAMIC INTERFERENCE, BYPASS RATIO, COMPARISON OF JET PLUME SHAPE PREDICTIONS AND

INTERACTIONAL AERODYNAMICS, SUPERCRITICAL WINGS, PLUME INFLUENCE ON SONIC BOOM SIGNATURE

TURBOFAN ENGINES, TURBOFANS, WING NACELLE RAYMOND L. BARGER and N. DUANE MELSON Mar 1992

CONFIGURATIONS 23 p

(RTOP 505-59-53-01)

N92-19175"# National Aeronautics and Space Administration. (NASA-TP-3172; L-16970; NAS 1.60:3172) Avail: CASI HC

Langley Research Center, Hampton, VA. A03/MF A01

A WEAKLY NONLINEAR THEORY FOR WAVE-VORTEX PLUMES, PREDICTIONS, SHAPES, SIGNATURES, SONIC

INTERACTIONS IN CURVED CHANNEL FLOW BOOMS

BART A. SINGER (High Technology Corp., Hampton, VA.),

GORDON ERLEBACHER (Institute tor Computer Applications in N92-25202"# National Aeronautics and Space Administration.

Science and Engineering. Hampton, VA.), and THOMAS A. ZANG Langley Research Center, Hampton, VA.

Mar. 1992 26 p THE NATURAL FLOW WING-DESIGN CONCEPT

(RTOP 505-59-50-01) RICHARD M. WOOD and STEVEN X. S. BAUER May 1992

(NASA-TP-3158; L-16989; NAS 1.60:3158) Avail: CASI HC 44 p Previously announced in IAA as A89-49677

A03/MF A01 (RTOP 505-61-71-01)

CHANNEL FLOW, FLUID DYNAMICS, NONLINEARITY, (NASA-TP-3193; L-16837; NAS 1,60:3193) Avail: CASI HC

TOLLMIEN-SCHLICHTING WAVES, VORTICES A03/MF A01

AERODYNAMIC CHARACTERISTICS. AIRCRAFT CONFIGN92-20038*# National Aeronautics and Space Administration. URATIONS. AIRCRAFT DESIGN, FLOW DISTRIBUTION, LEADLangley Research Center, Hampton, VA. ING EDGES. SLENDER WINGS. SUPERSONIC FLOW. SWEPT

INFLUENCE OF AIRFOIL GEOMETRY ON DELTA WING WINGS

LEADING-EDGE VORTICES AND VORTEX-INDUCED

AERODYNAMICS AT SUPERSONIC SPEEDS N92-25276"# National Aeronautics and Space Administration.

RICHARD M. WOOD (Lockheed Engineering and Sciences Co., Langley Research Center, Hampton, VA.

Hampton. VA.), JAMES E. BYRD, and GARY F. WESSELMANN WIND-TUNNEL STATIC AND FREE-FLIGHT INVESTIGATION

(Arnold Engineering Development Center, Arnold Air Force Station, OF HIGH-ANGLE-OF-ATTACK STABILITY AND CONTROL

TN) Washington Feb. 1992 86 p CHARACTERISTICS OF A MODEL OF THE EA-68 AIRPLANE

(RTOP 505-61-71-01) FRANK L. JORDAN, JR. and DAVID E. HAHNE May 1992

(NASA-TP-3105; L-16851; NAS 1.60:3105) Avail: CASI HC 60 p

A05/MF A01 (RTOP 505-61-71-07)

AIRFOIL PROFILES, DELTA WINGS, LEADING EDGES, (NASA-TP-3194; L-16813; NAS 1.60:3194) Avail: CASI HC

SUPERSONIC SPEED, VORTICES, WIND TUNNEL TESTS A04/MF A01

AERODYNAMIC STABILITY, AIRCRAFT CONTROL, ANGLE

N92-20494"# National Aeronautics and Space Administration. OF ATTACK, DIRECTIONAL STABILIT'V DYNAMIC STABILITY,

Langley Research Center, Hampton, VA. FREE FLIGHT, STAT:C TESTS, WIND TUNNEL TESTS

COMPARISON OF A TWO-DIMENSIONAL ADAPTIVE-WALL

TECHNIQUE WITH ANALYTICAL WALL INTERFERENCE N92-28477"# National Aeronautics and Space Administration

CORRECTION TECHNIQUES Langley Research Center, Hampton, VA.

RAYMOND E, MINECK Apr. 1992 73 p CALCULATION OF UNSTEADY TRANSONIC FLOWS WITH

(RTOP 505.59-10-03) MILD SEPARATION BY VISCOUS-INVISCID INTERACTION

(NASA-TP-3132; L-16911; NAS 1.60:3132) Avail: CASI HC JAMES T. HOWLETT Jun. 1992 39 p

A04/MF A01 (RTOP 509-10-02-03)

AERODYNAMIC INTERFERENCE, AIRFOILS, CORRECTION. (NASA-TP-3197; L-16996; NAS 1.60 3197) Avail: CASI HC

MODELS, REYNOLDS NUMBER, TRANSONIC WIND TUNNELS, A03/MF A01

WALL FLOW, WIND TUNNEL WALLS BOUNDARY LAYERS, FLOW DISTRIBUTION. FLOW

7
02 AERODYNAMICS

EQUATIONS, MATHEMATICAL MODELS, THREE DIMENSIONAL RAYMOND L BARGER Jul 1992 15 p

FLOW, TRANSONIC FLOW, UNSTEADY FLOW, VISCOUS (RTOP 505-59-53-01)

FLOW (NASA-TP-3232; L-17054; NAS 1.60:3232) Avail CAS) HC

A03/MF A01

N92o28980*# National Aeronautics and Space Administration. COMPUTATIONAL GRIDS, CURVE FITTtNG, FUNCTION

Lewis Research Center, Cleveland, OH. SPACE, G,'ID GENERATION (MATHEMATICS), MATHEMATICAL

LASER ANEMOMETER MEASUREMENTS AND MODELS, SMOOTHING, TRAJECTORIES

COMPUTATIONS IN AN ANNULAR CASCADE OF HIGH

TURNING CORE TURBINE VANES N92-30909"# National Aeronautics and Space Administration

LOUIS J. GOLDMAN and RICHARD G, SEASHOLTZ Jul. 1992 Langley Research Center. Hampton, VA.

38 p DIRECT SIMULATION OF HIGH-SPEED MIXING LAYERS

(RTOP 505-62-52) H. S. MUKUNDA, B. SEKAR (General Electric Co., Cincinnati. OH.),

(NASA-TP-3252; E-6354; NAS 1.F,0:3252) Avail: CASI HC M. H. CARPENTER, J. PHILIP DRUMMOND, and AJAY KUMAR

A03/MF A01 Jul. 1992 63 p

ANNULAR FLOW, CASCADE FLOW, CRITICAL VELOCITY, (RTOP 505-62-40-06)

LASER ANEMOMETERS. TURBINE BLADES, TURBOMACHIN- (NASA-TP-3186; L-16929; NAS 1.60:3186) Avail. CASI HC

ERY. TURBULENCE, TURBULE:4T FLOW, VANES A04/MF A01

COMPUTATIONAL GRIDS, COMPUTERIZED SIMULATION,

CONVECTION, FLOW CHARACTERISTICS, FREE WING

N92-29625*# National Aeronautics and Space Administration. AIRCRAFT, MIXING LAYERS (FLUIDS), TURBULENCE

Ames Research Center, Moffatt Field, CA.

NASA WORKSHOP ON FUTURE DIRECTIONS IN SURFACE N92-31532*# National Aeronautics and Space Administration.

MODELING AND GRID GENERATION Langley Research Center, Hampton. VA.

W_ R. VANDALSEM (National Aeronautics and Space WIND TUNNEL AERODYNAMIC CHARACTERISTICS OF A

tAdministration. Langley Research Center, Hampton, VA.), R. E. TRANSPORT-TYPE AIRFOIL IN A SIMULATED HEAVY RAIN

SMITH (National Aeronautics and Space Administration. Langley ENVIRONMENT

Research Center, Hampton, VA.), Y. K. CHOO (National GAUDY M BEZOS, R. EARL DUNHAM, JR., GARL L. GENTRY,

Aeronautics and Space Administration. Lewis Research Center, JR., and W. EDWARD MELSON, JR. (National Aeronautics and

Cleveland, OH.), L. D. BIRCKELBAW, and A. A. VOGEL Mar. Space Administration. Wallops Flight Facility, Wallops Island, VA.)

1992 24 p Workshop held at Moffett Field, CA, 5-7 Dec. 1989 Aug. 1992 68 p

(ATOP 505-59-00) (RTOP 505-68-01-02)

(NASA-CP-10092; A-92072; NAS 1.55:10092) Avail: CASI HC (NASA-TP-3184; L-16959; NAS 1.60:3184) Copyright Avail:

A03/MF A01 CASI HC A04/MF A01

COMPUTATIONAL FLUID DYNAMICS, CONFERENCES, GRID AERODYNAMIC CHARACTERISTICS. AIRFOILS. ENVIGENERATION (MATHEMATICS), NASA PROGRAMS RONMENT EFFECTS. ENVIRONMENT SIMULATION. PERFORMANCE PREDICTION. RAIN. SCALE MODELS. WIND TUNNEL

H92-30295 # National Aeronautics and Space Administration. TESTS

Langley Research Center, Hampton, VA.

VALIDATION OF THREE-DIMENSIONAL INCOMPRESSIBLE N92-32480"# National Aeronautics and Space Administration.

SPATIAL DIRECT NUMERICAL SIMULATION CODE: A Langley Research Center, Hampton, VA.

COMPARISON WITH LINEAR STABILITY AND PARABOLIC A METHOD FOR DESIGNING BLENDED WING-BODY

STABILITY EQUATION THEORIES FOR BOUNDARY-LAYER CONFIGURATIONS FOR LOW WAVE DRAG

TRANSITION ON A FLAT PLATE RAYMOND L. BARGER Sep. 1992 19 p

RONALD D. JOSLIN, CRAIG L. STREETT, and CHAU-LYAN (RTOP 505-59-53-01)

CHANG (High Technology Corp., Hampton, VA.) Jul. 1992 (NASA-TP-3261; L-17095; NAS 1.60:3261) Avail: CASI HC

49 p A03/MF A01

(RTOP 505-59-50-01) AERODYNAMIC CONFIGURATIONS, AIRCRAFT DESIGN.

(NASA-TP-3205; L-17026; NAS 1.60:3205) Avail: CASI HC BODY-WING CONFIGURATIONS, COMPUTATIONAL GRIDS,

A03/MF A01 DRAG REDUCTION, SUPERSONIC AIRCRAFT, WAVE DRAG

BOUNDARIES, BOUNDARY CONDITIONS, BOUNDARY

LAYER TRANSITION, BOUNDARY LAYERS, COMPUTERIZED

SIMULATION, FINITE DIFFERENCE THEORY, FLAT PLATES, N92-33484"# National Aeronautics and Space Administration

FLUID DYNAMICS, FOURIER SERIES, INCOMPRESSIBLE FLOW, Langley Research Center, Hampton, VA

RUNGE-KUTTA METHOD, WAVE REFLECTION APPLICATIONS OF A DIRECT/ITERATIVE DESIGN METHOD TO COMPLEX TRANSONIC CONFIGURATIONS

N92-30394*# National Aeronautics and Space Administration. LEIGH ANN SMITH and RICHARD L. CAMPBELL Sep. 1992

Langley Research Center, Hampton, VA 36 p

TWO-DIMENSIONAL AERODYNAMIC CHARACTERISTICS OF (RTOP 505-59-10-03)

SEVERAL POLYGON-SHAPED CROSS-SECTIONAL MODELS (NASA-TP-3234; L-16962; NAS 1.60:3234) Avail- CASI HC

APPLICABLE TO HELICOPTER FUSELAGES A03/MF A01

HENRY L. KELLEY, CYNTHIA A CROWELL, and JOHN C. AERODYNAMIC DRAG, AIRCRAFT CONFIGURATIONS.

WILSON Aug. 1992 30 p AIRCRAFT DESIGN, DRAG REDUCTION, INDUCED DRAG,

(DA PROJ. 1L2-J6003-D-313; RTOP 505-59-36-01) INTERFERENCE DRAG, NACELLES, TRANSPORT AIRCRAFT

(NASA-TP-3233; L-16951; NAS 1.60:3233;

AVSCOM-TR-92-B-002) Avail: CASI HC A03/MF A01 N92-33625"# National Aeronautics and Space Administration

AERODYNAMIC CHARACTERISTICS, AIRCRAFT MODELS, Langley Research Center, Hampton, VA.

BLUNT BODIES, CROSS SECTIONS, FUSELAGES, A NOZZLE INTERNAL PERFORMANCE PREDICTION METHOD

HELICOPTERS, POLYGONS, WIND TUNNEL TESTS JOHN R. CARLSON Oct. 1992 50 p

(RTOP 505-62-30-01)

N92-30747"# National Aeronautics and Space Administration. (NASA-TP-3221; L-16965; NAS 1.60:3221) Avail: CASI HC

Langley Research Center, Hampton, VA. A03/MF A01

TRAJECTORY FITTING IN FUNCTION SPACE WITH DISCHARGE COEFFICIENT. FLOW DISTRIBUTION,

APPLICATION TO ANALYTIC MODELING OF SURFACES NAVIER-STOKES EQUATION. NOZZLE DESIGN, NOZZLE

8
03 AIR TRANSPORTATION AND SAFETY

EFFICIENCY, NOZZLE FLOW, NOZZLE THRUST COEFFICIENTS. N91-11682"# National Aeronautics and Space Administratiron

PERFORMANCE PREDICTION. PITCHING MOMENTS, ROLLING Langley Researn'h Center, Hampton, VA

MOMENTS, YAWING MOMENTS AIRBORNE WIND SHEAR DETECTION AND WARNING

SYSTEMS. SECOND COMBINED MANUFACTURERS' AND

N92-33656*# National Aeronautics and Space Administration. TECHNOLOGISTS' CONFERENCE, PART 1

Langley Research Center, Hampton, VA. AMOS A. SPADY, JR., comp., ROLAND L. BOWLES, comp. and SURVEY AND ANALYSIS OF RESEARCH ON SUPERSONIC HERBERT SCHLICKENMAIER, comp. (Federal Aviation

DRAG-DUE-TO-LIFT M ONIMIZATION WITH Administration. Washington, DC) Jul. 1990 347 p Conference

RECOMMENDATIONS FOR WING DESIGN held in Williamsburg, VA, 18-20 Oct. 1988

HARRY W. CARLSON (Lockheed Engineering and Sciences Co., (RTOP 505-67-41-54)

Hampton, VA.) and MICHAEL J. MANN Sep. 1992 158 p (NASA-CP-10050-PT-1; NAS 1.55:10050.PT-1) Avail: CASI HC

(RTOP 505-68-70-02) A15/MF A03 (NASA-TP-3202R L-16963; NAS 1.60:3202) Avail: CASI HC AIRBORNE EQUIPMENT, AIRCRAFT HAZARDS,

AO8/MF A02 CONFERENCES, DETECTION. WARNING SYSTEMS. WIND

AIRCRAFT DESIGN, BODY-WING CONFIGURATIONS. SHEAR

CAMBERED WINGS. SUPERSONIC AIRCRAFT, SUPERSONIC N91-11695"# National Aeronautics and Space Administration

DRAG, SURVEYS. TWISTED WINGS, WINGS Langley Research Center, Hampton, VA.

AIRBORNE WIND SHEAR DETECTION AND WARNING

N92-337068# National Aeronautics and Space Administration. SYSTEMS. SECOND COMBINED MANUFACTURERS' AND

Langley Research Center, Hampton, VA. TECHNOLOGISTS' CONFERENCE, PART 2

EFFECT OF AFTERBODY GEOMETRY ON AERODYNAMIC AMOS A. SPADY, JR., comp., ROLAND L. BOWLES, comp., and

CHARACTERISTICS OF ISOLATED NONAXISYMMETRIC HERBERT SCHLICKENMAIER, comp. (Federal Aviation

AFTERBODIES AT TRANSONIC MACH NUMBERS Administration, Washington, DC.) Jul. 1990 452 p Conference

LINDA S. BANGERT and GEORGE T. CARSON, JR. Sep. 1992 held in Williamsburg, VA, 18-20 Oct. 1988

265 p (RTOP 505-67-41-54)

(RTOP 505-62-30-01) (NASA-CP-10050-PT-2; NAS 1.55:10050-PT-2) Avail: CASI HC

(NASA-TP-3236; L-17034; NAS 1.60:3236) Avail: CASt HC A20/MF A04

A12/MF A03 AIRCRAFT GUIDANCE, CONFERENCES. DETECTION,

AERODYNAMIC CHARACTERISTICS, AFTERBODIES, MICROBURSTS (METEOROLOGY), WARNING SYSTEMS, WIND

AIRCRAFT CONFIGURATIONS, AIRCRAFT MODELS, SHEAR

BOATTAILS, FIGHTER AIRCRAFT, INTERACTIONAL

AERODYNAMICS, WIND TUNNEL MODELS, WIND TUNNEL N91-15141*# National Aeronautics and Space Administration

TESTS Langley Research Center, Hampton, VA

REPORT OF THE WORKSHOP ON AVIATION

N92-34193"# National Aeronautics and Space Administration. SAFETY/AUTOMATION PROGRAM

Langley Research Center, Hampton, VA. SAMUEL A. MORELLO, ed. Oct. 1990 45 p Workshop held

PARAMETRIC INVESTIGATION OF in Virginia Beach, VA, 10 Oct. 1989

SINGLE-EXPANSION-RAMP NOZZLES AT MACH NUMBERS (RTOP 505-64-13-22)

FROM 0.60 TO 1.20 (NASA-CP-10054; NAS 1.55:10054) Avail: CASI HC A03/MF

FRANCIS J_ CAPONE. RICHARD J. RE. and E. ANN BARE Oct. A01

1992 276 p AIR TRAFFIC CONTROL, AIR TRAFFIC CONTROLLERS

(RTOP 505-62-30-01) (PERSONNEL), COMPUTER TECHNIQUES, CONFERENCES,

(NASA-TP-3240; L-17067; NAS 1.60:3240) Avail: CASI HC FLIGHT MANAGEMENT SYSTEMS, WORKSTATIONS

A13/MF A03

AERODYNAMIC COEFFICIENTS, AERODYNAMIC DRAG, N91-24140*# National Aeronautics and Space Administration.

CONVERGENT NOZZLES, CONVERGENT-DIVERGENT Langley Research Center, Hampton, VA.

NOZZLES, MACH NUMBER, NOZZLE DESIGN, NOZZLE FLOW, AIRBORNE WIND SHEAR DETECTION AND WARNING

PROPULSION SYSTEM PERFORMANCE, WIND TUNNEL TESTS SYSTEMS- THIRD COMBINED MANUFACTURERS' AND

TECHNOLOGISTS' CONFERENCE, PART 2

DAN D. VICROY, comp. (National Aeronautics and Space

Administration. Langley Research Center, Hampton, VA.), ROLAND

03 L. BOWLES, comp. (National Aeronautics and Space Administration. Langley Research Center, Hampton, VA), and

HERBERT SCHLICKENMAIER, comp. (Federal Aviation

AIR TRANSPORTATION AND SAFETY Administration, Washington, DC.) Jan. 1991 464 p Conference

held in Hampton, VA. 16-18 Oct. 1990 Prepared in cooperation

Includes passenger and cargo air transport operations; and aircraft with Federal Aviation Administration, Washington. DC

accidents. (RTOP 505-64-12)

(NASA-CP-10060-PT-2; NAS 1.55:10060-PT-2;

DOT/FAA/RD-9t/2-PT-2) Avail: CASI HC A20/MF A04

N91-10936"# National Aeronautics and Space Administration. AIRBORNE EQUIPMENT, CONFERENCES. DOPPLER RADAR,

Langley Research Center, Hampton, VA METEOROLOGICAL RADAR, MICROBURSTS (METEOROLOGY).

AVIATION SAFETY/AUTOMATION PROGRAM CONFERENCE OPTICAL RADAR, RADAR DETECTION, WARNING SYSTEMS.

SAMUEL A. MORELLO, comp. Washington Oct. 1990 270 p WIND SHEAR

Conference held in Virginia Beach, VA, 11-12 Oct. 1989

(RTOP 505-67-21-07) N91-24166'# National Aeronautics and Space Administration

(NASA-CP-3090; L-16840; NAS 1 55:3090) Avail: CASI HC Langley Research Center, Hampton, VA

A12/MF A03 AIRBORNE WIND SHEAR DETECTION AND WARNING

AIR TRAFFIC CONTROL, AIRCRAFT SAFETY, AVIONICS, SYSTEMS: THIRD COMBINED MANUFACTURERS' AND

COCKPITS, CONFERENCES, HUMAN FACTORS ENGINEERING. TECHNOLOGISTS' CONFERENCE, PART 1

MAN MACHINE SYSTEMS, MAN-COMPUTER INTERFACE, TEST DAN D. VICROY, comp. (National Aeronautics and Space

FACILITIES Administration. Langley Research Center. Hampton, VA I, ROLAND

9
03 AIR TRANSPORTATION AND SAFETY

L. BOWLES, comp. (National Aeronautics and Space MANAGEMENT, DATA TRANSMISSION, DIGITAL DATA,

Administration. Langley Research Center, Hampton, VA.), and GROUND-AIR-GROUND COMMUNICATION, PULSE COMMUNIHERBERT SCHLICKENMAIER, comp. (Federal Aviation CATION

Administration, Washington, DC.) Jan. 1991 490 p Conference

held in Hampton, VA, 16-18 Oct. 1990 Prepared in cooperation

with FAA, Washington, DC

(RTOP 505-64-12) 05

(NASA-CP-10060-PT-i; NAS 1.55:10060-PT-I;

DOT/FAA/RD-91/2-PT-1) Avail: CASI HC A21/MF A04 AIRCRAFT DESIGN, TESTING AND

AERODYNAMICS, AIRCRAFT PERFORMANCE, FLIGHT PERFORMANCE

HAZARDS, FLIGHT MANAGEMENT SYSTEMS, FLIGHT TESTS,

MICROBURSTS (METEOROLOGY), RAIN, WARNING SYSTEMS,

WIND SHEAR Includes aircraft simulation technology.

N91-70436*# National Aeronautics and Space Administration. N91-14323°# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, CA. Langley Research Center, Hampton, VA.

THE DEVELOPMENT OF THE NASA AVIATION SAFETY A METHOD FOR THE DESIGN OF TRANSONIC FLEXIBLE

REPORTING SYSTEM WINGS

W. D. REYNARD, C. E. BILLINGS, E. S. CHEANEY, and R. LEIGH ANN SMITH and RICHARD L. CAMPBELL Washington

HARDY Nov. 1986 192 p Dec. 1990 41 p

(RTOP 505-67-41) (RTOP 505-61-21-03)

(NASA-RP-1114; A-85127; NAS 1.61:1114) Avail: CASI HC A09 (NASA-TP-3045; L-16762; NAS 1,60:3045) Avail: CASI HC

A03/MF A01

N92-10994C# National Aeronautics and Space Administration. AERODYNAMIC LOADS, AEROELASTICITY, AIRCRAFT

Langley Research Center, Hampton, VA. DESIGN, AIRFOIL PROFILES, FLEXIBLE WINGS. TRANSONIC

A COMPARISON OF AIRBORNE WAKE VORTEX DETECTION SPEED

MEASUREMENTS WITH VALUES PREDICTED FROM

POTENTIAL THEORY N91-17014"# National Aeronautics and Space Administration.

ERIC C. STEWART Washington Nov. 1991 38 p Langley Research Center, Hampton, VA.

(RTOP 505-68-10-01) STATIC FOOTPRINT LOCAL FORCES, AREAS, AND ASPECT

(NASA-TP-3125; L-16899; NAS 1.60:3125) Avail: CASI HC RATIOS FOR THREE TYPE 7 AIRCRAFT TIRES

A03/MF A01 WILLIAM E. HOWELL (National Aeronautics and Space

ALGORITHMS, FLIGHT SAFETY, FLOW DISTRIBUTION, Administration. Langley Research Cen'ter, Hampton, VA.), SHARON

IN-FLIGHT MONITORING, NEAR WAKES. VORTICES, WAKES E. PEREZ, and W!'LUAM A. :)GLER (Lockheed Engineering and

Scicnces Co., Hampton, VA. Washington Feb. 1991 95 p

N92-30395"# National Aeronautics and Space Administration. (RTOP 505-63-41-021

Lewis Research Center, Cleveland, OH. (NASA-TP-2983; L-16521; NAS 1.60:2983) Avail: CASI HC

LEWIS ICING RESEARCH TUNNEL TEST OF THE A05/MF A01

AERODYNAMIC EFFECTS OF AIRCRAFT GROUND AIRCRAFT TIRES, AREA, ASPECT RATIO, LOAD

DEICING/ANTI-ICING FLUIDS DISTRIBUTION (FORCES), VEHICULAR TRACKS

L. JAMES RUNYAN (Boeing Commercial Airplane Co., Seattle,

WA.), THOMAS A. ZIERTEN (Boeing Commercial Airplane Co., N91-19082°# National Aeronautics and Space Administration.

Seattle, WA.), EUGENE G. HILL (Boeing Commercial Airplane Co., Ames Research Center, Moffett Field, CA.

Seattle, WA.), and HAROLD E. ADDY, JR. Aug. 1992 134 p STATE ESTIMATION APPLICATIONS IN AIRCRAFT

(RTOP 505-68-11) FLIGHT-DATA ANALYSIS: A USER'S MANUAL FOR SMACK

(NASA-TP-3238; E-5808; NAS 1.15:3238) Avail: CASI HC RALPH E. BACH, JR. Mar. 1991 134 p

A07/MF A02 (RTOP 505-66-41)

AERODYNAMIC CHARACTERISTICS, BOEING AIRCRAFT, (NASA-RP-1252; A-88203; NAS 1.61:1252) Avail: CASI HC

DEICING, ICE FORMATION, NEWTONIAN FLUIDS, RHEOLOGY, A07/MF A02

WIND TUNNEL TESTS The evolution in the use of state estimation is traced for the

analysis of aircraft flight data. A unifying mathematical framework

for state estimation is reviewed, and several examples are

04 presented that illustrate a general approach for checking instrument

accuracy and data consistency, and for estimating variables that

are difficult to measure. Recent applications associated with

AIRCRAFT COMMUNICATIONS AND NAVIGATION research aircraft flight tests and airline turbulence upsets are

described. A computer program for aircraft state estimation is

Includes digital and voice communication with aircraft; air navigation discussed in some detail. This document is intended to serve as

systems (satellite and ground based); and tir traffic control. a user's manual for the program called SMACK (SMoothing for

AirCraft Kinematics). The diversity of the applications described

emphasizes the potential advantages in using SMACK for flight-data

N92-21459*# National Aeronautics and Space Administration. analysis. Author

Langley Research Center. Hampton, VA.

FLIGHT DECK BENEFITS OF INTEGRATED DATA LINK N91-20071*# National Aeronautics and Space Administration

COMMUNICATION Hugh L. Dryden Flight Research 7acifity, Edwards, CA.

MARVIN C. WALLER Washington NASA. Langley Research PROCEEDINGS OF THE X-15 FIRST FLIGHT 30TH

Center Apr, 1992 49 p ANNIVERSARY CELEBRATION

(RTOP 505-64-13-01) Washington Jan. 1991 174 p Symposium held in Edwards,

(NASA-TP-3219: L-16845; NAS 1.60:3219) Avail: CASI HC CA. 8 Jun. 1989

A03/MF A01 (RTOP 533-02-00)

AIR TRAFFIC CONTROL, AIRCRAFT COMMUNICATION, (NASA-CP-3105; H-1622; NAS 1.55:3105) Avail: CASI HC

COMPUTERIZED SIMULATION, DATA LINKS, DATA A08/MF A02

10
06 AIRCRAFT INSTRUMENTATION

AIRCRAFT DESIGN. CONFERENCES, HISTORIES, N92-33874*# National Aeronautics and Space Administration

HYPERSONIC FLIGHT, NASA PROGRAMS, RESEARCH AND Langley Research Center, Hampton, VA.

DEVELOPMENT, SPACE FLIGHT, X-15 AIRCRAFT HIGH-SPEED RESEARCH: SONIC BOOM, VOLUME 1

CHRISTINE M. DARDEN, comp. Washington Oct. 1992

195 p Workshop held in Hamp .jn, VA, 25-27 Feb, 1992

N91-21127"# National Aeronautics and Space Administration. (RTOP 537-03-21-01)

Langley Research Center, Hampton, VA. (NASA-CP-3172; L-17145-VOL-1; NAS 1.55,3172) Avail: CASI

SPAN REDUCTION EFFECTS ON THE FLUTTER HC A09/MF A03

CHARACTERISTICS OF ARROW-WING SUPERSONIC ATMOSPHERIC EFFECTS, ATMOSPHERIC TURBULENCE,

TRANSPORT CONFIGURATIONS SHOCK WAVE PROPAGATION, SONIC BOOMS, TURBULENCE

DONALD F. KELLER and ELLEN PARKER BULLOCK 26 Dec- EFFECTS

1990 55 p

(RTOP 505-63-21)

(NASA-TP-3077; L-16807; NAS 1.60:3077) Avail: CASI HC 06

A04/MF A01

AIRCRAFT CONFIGURATIONS, ARROW WINGS, DYNAMIC

PRESSURE, FLUTTER ANALYSIS, SUPERSONIC TRANSPORTS, AIRCRAFT INSTRUMENTATION

TRANSONIC FLUTTER, WIND TUNNEL TESTS, WING SPAN

Includes cockpit and cabin display devices, and flight instruments.

NSI-24199*# National Aeronautics and Space Administration.

Langley Research Center, Hampton, VA. N91-17020"# National Aeronautics and Space Administration,

EVALUATION OF CLOUD DETECTION INSTRUMENTS AND Washington, DC.

PERFORMANCE OF LAMINAR-FLOW LEADING-EDGE TEST SPACE TRANSPORTATION AVIONICS TECHNOLOGY

ARTICLES DURING NASA LEADING-EDGE FLIGHT-TEST SYMPOSIUM. VOLUME 2: CONFERENCE PROCEEDINGS

PROGRAM Aug. 1990 742 p Symposium held in Williamsburg, VA, 7-9

RICHARD E. DAVIS (National Aeronautics and Space Nov. 1989

Administration. Langley Research Center, Hampton, VA.), DAL V. (NASA-CP-3081-VOL-2; NAS 1.55:3081-VOL-2) Avail: CASI HC

MADDALON (National Aeronautics and Space Administration. A99/MF A06

Langley Rese.acri Center, Hampton, VA.), RICHARD D. WAGNER AVIONICS, COMPUTER PROGRAMMING, CONFERENCES,

(National Aeronautics and Space Administration. Langley Research SOFTWARE ENGINEERING, SPACE TRANSPORTATION

Center, Hampton, VA.), DAVID F. FISHER (National Aeronautics SYSTEM, SYSTEMS ENGINEERING, SYSTEMS INTEGRATION

and Space Administration. Ames Research Center, Moffett Field,

CA.), and RONALD YOUNG (National Aeronautics and Space N91-31143*# National Aeronautics and Space Administration.

Administration. Hugh L. Dryden Flight Research Facility, Edwards, Langley Research Center, Hampton, VA.

CA.) Apr. 1989 58 p FLIGHT TESTS WITH A DATA LINK USED FOR AIR TRAFFIC

(RTOP 505-60-31-01) CONTROL INFORMATION EXCHANGE

(NASA-TP-2888; L-16509; NAS 1,60:2888) Avail: CASI HC CHARLES E. KNOX and CHARLES H. SCANLON Sep. 1991

A04/MF A01 38 p

AIRCRAFT DESIGN, AIRLINE OPERATIONS, BOUNDARY (RTOP 505-64-13-01)

LAYER CONTROL, CLOUDS, DETECTION, FLIGHT SIMULATION, (NASA-TP-3135; L-16936; NAS 1.60:3135) Avail: CASI HC

HAZE, LAMINAR BOUNDARY LAYER, LEADING EDGES A03/MF A01

AIR TRAFFIC CONTROL, CIVIL AVIATION, DATA LINKS,

N91-24200"# National Aeronautics and Space Administration. FLIGHT OPERATIONS, FLIGHT TESTS, RADIO FREQUENCIES,

Langley Research Center, Hampton, VA. SAFETY FACTORS, SYSTEMS ENGINEERING, VOICE

NASA-LARC FLIGHT-CRITICAL DIGITAL SYSTEMS COMMUNICATION

TECHNOLOGY WORKSHOP

C. W. MEISSNER, JR., ed., J. R. DUNHAM, ed., and G. CRIM, N92-13065"# National Aeronautics and Space Administration.

ed. Apr. 1989 191 p Workshop held in Hampton, VA, 13-15 Langley Research Center, Hampton, VA.

Dec. 1988 EFFECT OF SHORT-TERM EXPOSURE TO STEREOSCOPIC

(RTOP 505-66-21-03) THREE-DIMENSIONAL FLIGHT DISPLAYS ON REAL-WORLD

(NASA-CP-10028; REPT-412U-3181-29; NAS 1.55:10028) Avail: DEPTH PERCEPTION

CASI HC A09/MF A02 ANTHONY M. BUSQUETS, RUSSELL V. PARRISH, and STEVEN

COMPUTER SYSTEMS DESIGN, DIGITAL SYSTEMS, FLIGHT P. WILLIAMS Washington Oct. 1991 26 p

CONTROL, QUALITY CONTROL, RELIABILITY ENGINEERING, (DA PROJ. 1L1-61102-AH-45; RTOP 505-64-13-32)

SYSTEMS ENGINEERING, TECHNOLOGY ASSESSMENT (NASA-TP-3117; L-16897; NAS 1.60:3117;

AVSCOM-TR-91-B-014; AD-A242333) Avail: CASI HC A03/MF

A01

N92-13054"# National Aeronautics and Space Administration. DEPTH, DISPLAY DEVICES, FLIGHT INSTRUMENTS, HUMAN

Langley Research Center, Hampton, VA. FACTORS ENGINEERING, PILOT PERFORMANCE, SPACE

PLANFORM CURVATURE EFFECTS ON FLUTTER PERCEPTION, STEREOSCOPIC VISION

CHARACTERISTICS OF A WING WITH 56 DEG

LEADING-EDGE SWEEP AND PANEL ASPECT RATIO OF 1.14 N92-20546"# National Aeronautics and Space Administration.

DONALD F. KELLER, MAYNARD C. SANDFORD, and THERESA Langley Research Center, Hampton, VA.

L. PINKERTON (Illinois Univ., Urbana.) Washington Sep. 1991 VENTURI AIR-JET VACUUM EJECTORS FOR HIGH-VOLUME

46 p ATMOSPHERIC SAMPLING ON AIRCRAFT PLATFORMS

(RTOP 505-63-50-13) GERALD F. HILL (Lockheed Engineering and Sciences Co.,

(NASA-TP-3116; L-16858; NAS 1.60:3116) Avail: CASt HC Hampton, VA.), GLEN W. SACHSE, DOUGLAS C. YOUNG, LARRY

A03/MF A01 0. WADE (Lockheed Engineering and Sciences Co., Hampton,

AEROELASTICITY, CURVATURE, FLUTTER ANALYSIS, VA.), and LEWIS G. BURNEY Apr. 1992 38 p

LEADING EDGE SWEEP, PLANFORMS, SWEPT WINGS, (RTOP 464-54-17-70)

TRANSONIC FLUTTER, WIND TUNNEL MODELS, WIND TUNNEL (NASA-TP-3183; L-16937; NAS 1.60:3183) Avail: CASI HC

TESTS A03/MF A01

11
07 AIRCRAFT PROPULSION AND POWER

AIR JETS, AIR SAMPLING, AIRBORNE EQUIPMENT, Mar. 1991: sponsored by NASA. Ames Research Center Orginal

EJECTORS, ELECTRA AIRCRAFT. FLYING PLATFORMS, contains color illustrations

VACUUM PUMPS, VENTURI TUBES (RTOP 505-62-52)

(NASA-CP-10078; E-6374, NAS 1.55:10078)

ALGORITHMS, COMPUTATIONAL FLUID DYNAMICS, FLOW

DISTRIBUTION, MATHEMATICAL MODELS, NUMERICAL

ANALYSIS, REAL GASES, RESEARCH AND DEVELOPMENT

AIRCRAFT PROPULSION AND POWER

08

Includes prime propulsion systems and systems components, e.g.,

gas turbine engines and compressors; and onboard auxiliary power AIRCRAFT STABILITY AND CONTROL

plants for aircraft.

Includes aircraft handling qualities, piloting, flight controls, and

N91-20086*# National Aeronautics and Space Administration. autopilots.

Lewis Research Center, Cleveland, OH.

AEROPROPULSION 1991

Mar. 1991 574 p Conference held in Cleveland, OH, 20-21 N91-10079"# National Aeronautics and Space Administration.

Mar. 1991 Hugh L. Dryden Flight Research Facility, Edwards, CA.

(RTOP 505-62-00) FLIGHT CHARACTERISTICS OF A MODIFIED SCHWEIZER

(NASA-CP-10063; E-5954; NAS 1.55:10063) Avail: CASI HC SGS1-36 SAILPLANE AT LOW AND VERY HIGH ANGLES OF

A24/MF A04 ATTACK

AIR BREATHING ENGINES, AIRCRAFT DESIGN, AIRCRAFT ALEX G. SIM Jul. 1990 48 p

ENGINES, COMPUTER PROGRAMS, CONTROL SYSTEMS (RTOP 505-45-21)

DESIGN, FLUID MECHANICS, PROPULSION SYSTEM (NASA-TP-3022; H-1563; NAS 1,60:3022) Avail: CASI HC

CONFIGURATIONS, STRUCTURAL DESIGN A03/MF A01

AERODYNAMIC STABILITY, ANGLE OF ATTACK, FLIGHT

N92-22510°# National Aeronautics and Space Administration. CHARACTERISTICS, GLIDERS, PARAMETER IDENTIFICATION.

Lewis Research Center, Cleveland, OH. PILOT PERFORMANCE

AEROPROPULSION 1987

Washington Feb. 1990 498 p Conference held in Cleveland, N91-20128"# National Aeronautics and Space Administration

OH, 17-19 Nov. 1987 Previously announced as N88-16697, Langley Research Center, Hampton, VA.

N88-15785, N88-15790, N88-15794, N88-15800 and N88-15807 A CONTROLS ENGINEERING APPROACH FOR ANALYZING

(RTOP 505-62-3B) AIRPLANE INPUT-OUTPUT CHARACTERISTICS

(NASA-CP-3049: E-3798; NAS 1.55:3049) Avail: CASI HC P. DOUGLAS ARBUCKLE Washington Apr 1991 22 p

A21/MF A04 (RTOP 505-66-71-03)

AIRCRAFT ENGINES, CONFERENCES, ENGINE DESIGN, (NASA-TP-3072; L-16798; NAS 1.60:3072) Avail[ CASI HC

PROPULSION SYSTEM CONFIGURATIONS, PROPULSION A03/MF A01

SYSTEM PERFORMANCE AIRCRAFT CONTROL, AIRCRAFT MODELS, CONTROL

SYSTEMS DESIGN, MODAL RESPONSE

N92-22863*# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, OH. N91-25151*# National Aeronautics and Space Administration.

DESIGN AND PERFORMANCE OF CONTROLLED-DIFFUSION Langley Research Center, Hampton, VA.

STATOR COMPARED WITH ORIGINAL DEVELOPMENT OF AN ADAPTIVE FAILURE DETECTION AND

DOUBLE-CIRCULAR-ARC STATOR IDENTIFICATION SYSTEM FOR DETECTING AIRCRAFT

THOMAS F. GELDER, JAMES F. SCHMIDT, KENNETH L. SUDER, CONTROL ELEMENT FAILURES

and MICHAEL D. HATHAWAY (Army Aviation Systems Command, W. THOMAS BUNDICK 1990 150 p Sponsored in part by

Cleveland, OH.) Mar. 1989 80 p Presented at the 1987 Planning Research Corp., Hampton, VA

Aerospace Technology Conference and Exposition, Long Beach, (RTOP 505-66-41-04)

CA, 5-8 Oct. 1987; sponsored by SAE (NASA-TP-3051; L-16801; NAS 1.60:3051) Avail. CASI HC

(DA PROJ. 1L1-61102-AH-45; RTOP 505-62-51) A07/MF A02

(NASA-TP-2852; E-4195; NAS 1.60:2852; AVSCOM-TR-88-C-013; ADAPTIVE CONTROL, AIRCRAFT CONTROL, ATMOSPHERIC

SAE-871783) Avail: CASI HC A05/MF A01 TURBULENCE, FAILURE ANALYSIS, FAULT TOLERANCE

DIFFUSION, ENERGY CONVERSION EFFICIENCY, FAN

BLADES, STATOR BLADES, STATORS N91-30154*# National Aeronautics and Space Administration.

Hugh L. Dryden Flight Research Facility. Edwards, CAN92-25712"# National Aeronautics and Space Administration. APPLICATION AND FLIGHT TEST OF LINEARIZING

Lewis Research Center, Cleveland, OH. TRANSFORMATIONS USING MEASUREMENT FEEDBACK TO

WORKSHOP ON GRID GENERATION AND RELATED AREAS THE NONLINEAR CONTROL PROBLEM

Apr. 1992 160 p Workshop held in Cleveland, OH, 14-15 Nov. ROBERT F. ANTONIEWICZ (National Aeronautics and Space

1991 Administration. Hugh L. Dryden Flight Research Center, Edwards.

(RTOP 505-62-52) CA.), EUGENE L. DUKE (National Aeronautics and Space

(NASA-CP 10089; E-6823; NAS 1.55:10089) Avail: CAS) HC Administration. Hugh L. Dryden Flight Research Center, Edwards,

A08/MF A02 CA.), and P. K. A. MENON (Georgia Inst. of Tech., Atlanta.) Sep.

COMPUTATIONAL GRIDS, CONFERENCES, GRID 1991 56 p

GENERATION (MATHEMATICS), MULTIGRID METHODS, (RTOP 505-60-21)

SURFACES (NASA-TP-3154; H-1629; NAS 1.60:3154) Avail: CASI HC

A04/MF A01

N92-25808"# National Aeronautics and Space Administration. AIRCRAFT CONTROL, CONTROL SYSTEMS DESIGN,

Lewis Research Center, Cleveland, OH. CONTROLLERS. F-15 AIRCRAFT, FEEDBACK CONTROL,

COMPUTATIONAL FLUID DYNAMICS FLIGHT CONTROL, NONLINEAR SYSTEMS. TRAJECTORY

Feb. 1992 219 p Conference held at Moffett Field, CA, 12-14 CONTROL

12
13 ASTRODYNAMICS

N92-10027"# National Aeronautics and 'pace Administration. (RTOP 506-40-41-02)

Langley Research Center, Hampton, VA. (NASA-CP-10031; NAS 1.55:10031) Avail: CASI HC A08/MF

ON THE FORMULAT!ON OF A MINIMAL UNCERTAINTY A02

MODEL FOR ROBUST CONTROL WITH STRUCTURED AEROTHERMODYNAMICS, COMPUTATIONAL FLUID

UNCERTAINTY DYNAMICS, HYPERSONIC AIRCRAFT, HYPERVELOCITY FLOW,

CHRISTINE M. BELCASTRO (Drexel Univ., Philadelphia, PA.), B.-C. TECHNOLOGY ASSESSMENT

CHANG, and ROBERT FISCHL (Drexel Univ., Philadelphia, PA.)

Sep. 1991 34 p N92-31640"# National Aeronautics and Space Administration

(RTOP 505-66-01-02) Lewis Research Center, Cleveland, OH.

(NASA-TP-3094; L-16893; NAS 1.60:3094) Avail: CASI HC SUPERSONIC THROUGHFLOW FAN TEST FACILITY AT

A03/MF A01 NASA. LEWIS RESEARCH CENTER

CONTROL SYSTEMS DESIGN, FEEDBACK CONTROL, DONALD C. URASEK, WALTER S. CUNNAN, RICHARD L. LANTZ.

MATRICES (MATHEMATICS), ROBUSTNESS (MATHEMATICS), DENNIS I.. FRONEK, RONALD A. DAWSON, and JEFFREY C.

TRANSFER FUNCTIONS BROWN Sep. 1990 25 p

(RTOP 505-62-61)

N92-20195"# National Aeronautics and Space Administration. (NASA-TP-3038; E-5398; NAS 1.60:3038) Avail: CASI HC

Langley Research Center, Hampton, VA. A03/MF A01

CONTROL INTEGRATION CONCEPT FOR HYPERSONIC PROPULSION SYSTEM CONFIGURATIONS, PROPULSIK)N

CRUISE-TURN MANEUVERS SYSTEM PERFORMANCE, SUPERSONIC FLOW, SUPERSONIC

DAVID L. RANEY and FREDERICK J. LALLMAN Feb. 1992 SPEED, SUPERSONIC TEST APPARATUS, SUPERSONIC

63 p TURBINES, SUPERSONIC WIND TUNNELS, TURBOFANS. WIND

(RTOP 505-64-40-01) TUNNEL DRIVES

(NASA-TP-3136; L-16928; NAS 1.60:3136) Avail: CASI HC

A04/MF A01

AIRCRAFT MANEUVERS, AIRCRAFT PERFORMANCE,

FLIGHT CONTROL, HYPERSONIC FLIGHT, HYPERSONIC 12

VEHICLES ASTRONAUTICS (GENERAL)

N92-21410"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, VA.

A METHODOLOGY FOR COMPUTING UNCERTAINTY BOUNDS

OF MULTIVARIABLE SYSTEMS BASED ON SECTOR

STABILITY THEORY CONCEPTS N91-20147*# National Aeronautics and Space Administration.

MARTIN R. WASZAK Apr. 1992 42 p Ames Research Center, Moffett Field, CA.

(RTOP 505-66-71-01) MANUAL CONTROL ASPECTS OF ORBITAL FLIGHT

(NASA-TP-3166; L-16846; NAS 1.60:3166) Avail: CASI HC Abstracts Only

A03/MF A01 ADAM R. BRODY, ed. (Sterling Software. Palo Alto, CA.) and

CONTROL STABILITY, CONTROL THEORY, LINEAR STEPHEN R. ELLIS, ed. Dec. 1990 14 p Workshop held at

SYSTEMS, MIMO (CONTROL SYSTEMS), MULTIVARIABLE Moffett Field, CA, 22 Feb. 1990

CONTROL, SYSTEMS STABILITY (RTOP 506-47-31)

(NASA-CP-10056; A-90286; NAS 1.55:10056) Avail: CASI HC

A03/MF A01

HUMAN FACTORS ENGINEERING, MANUAL CONTROL, 09 ORBITAL MANEUVERS, SPACE STATIONS, SPACE

TRANSPORTATION SYSTEM

RESEARCH AND SUPPORT FACILITIES (AIR) N91-22139r# National Aeronautics and Space Administration.

Includes airports, hangars and runways; aircraft repair and overhaul Lewis Research Center, Cleveland, OH.

facilities; wind tunnels; shock tubes; and aircraft engine test VISION-21: SPACE TRAVEL FOR THE NEXT MILLENNIUM

stands. GEOFFREY A. LANDIS, ed. (Sverdrup Technology. Inc., Brook

Park, OH.) Apr. 1990 600 p Symposium held in Cleveland,

OH, 3-4 Apr. 1990

N91-13461"# National Aeronautics and Space Administration. (NASA-CP-10059; E-5838; NAS 1.55:10059) Avail: CASI HC

Langley Research Center, Hampton, VA. A25/MF A06

CALIBRATION OF THE 13- BY 13-INCH ADAPTIVE WALL CONFERENCES, MISSION PLANNING, NUCLEAR

TEST SECTION FOR THE LANGLEY 0.3-METER TRANSONIC PROPULSION, NUCLEAR REACTORS, PROJECT PLANNING

CRYOGENIC TUNNEL REACTOR DESIGN, REACTOR TECHNOLOGY, SPACE

RAYMOND E. MINECK and ACQUILLA S HILL Washington EXPLORATION; SPACECRAFT PROPULSION

Dec. 1990 111 p

(RTOP 505-61-21-03)

(NASA-TP-3049; L-16787; NAS 1.60:3049) Avail: CASI HC 13

A06/MF A02

AIRFOIL PROFILES, CALIBRATING, FLEXIBILITY, FLOW

DISTRIBUTION, WIND TUNNEL WALLS ASTRODYNAMICS

Ng1-24211"# National Aeronautics and Space Administration. Includes powered and free-flight trajectories; and orbital and

Langley Research Center, Hampton, VA. launching dynamics.

ADVANCED HYPERVELOCITY AEROPHYSICS FACILITY

WORKSHOP

ROBERT D. WITCOFSKI, comp. and WILLIAM 1. SCALLION, N91-10092"# National Aeronautics and Space Administration.

comp. May 1989 170 p Workshop held in Hampton, VA, Marshall Space Flight Center, Huntsville, AL.

10-11 May 1988 LONG-TERM ORBITAL LIFETIME PREDICTIONS

13
13 ASTRODYNAMICS

P. E. DREHER and A. T. LYONS Oct. 1990 26 p mediums, and evaluation testing for three-dimensional laser

(NASA-TP-3058; NAS 1.60:3056) Avail: CAS, HC A031MF A01 windows. Author

BOILER PLATE, LONG DURATION EXPOSURE FACILITY.

LONG TERM EFFECTS, OR3iTAL LIFETIME, PERFORMANCE

PREDICTION 15

N91-17073'# National Aeronautics and Space AdministrationL

Goddard Space Flight Center, Greenbelt, MD. LAUNCH VEHICLES AND SPACE VEHICLES

FLIGHT MECHANICS/ESTIMATION THEORY SYMPOSIUM,

1990 Incluaes boosters; operating problems of launch/space vehicle

THOMAS STENGLE, ed, Dec. 1990 549 p Symposium held systems; and reusable vehicles.

in Greenbelt, MD, 22-24 May 1990

(NASA-CP-3102; REPT-91B00018; NAS 1.55:3102) Avail: CASI

HC A23/MF A04 N91-18180"# National Aeronautics and Space Administrat,,n.

AERODYNAMICS, ATTITUDE (INCLINAtION). CONFER- Langley Research Center, Hampton, VA.

ENCES. ESTIMATES, FLIGHT MECHANICS, SATELLITE ATTI- PARAMETRIC TRADE STUDIES ON A SHUTTLE 2 LAUNCH

TUDE CONTROL, SPACECRAFT ORBITS. SPACECRAFT TRA- SYSTFM ARCHITECTURE

JECTORIES DOUGLAS 0. STANLEY, THEODORE A. TALAY, ROGER A.

LEPSCH, W. DOUGLAS MORRIS, J. CHRISTOPHER NAFTEL,

N92-14070"# National Aeronautics and Space Administration. and CHRISTOPHER I. CRUZ Washington Mar. 1991 56 p

Goddard Space Flight Center, Greenbelt, MD. (RTOP 506-40-61 -01)

FLIGHT MEC'HANICS/ESTIMATION THEORY SYMPOSIUM, (NASA-TP-3059; L-16790; NAS 1.60:3059) Avail: CASI HC

1991 A04/MF A01

THOMAS STENGLE, ed. Washington Oct. 1991 490 p COOSTER ROCKET ENGINES, LAUNCH VEHICLE

Symposium held in Greenbelt, MD, 21-23 May 1991 CONFIGURATIONS, PROPULSION SYSTEM CONFIGURATIONS,

(NASA-CP-3123; REPT-91B00133; NAS 1.55:3123) Avail: CASI SPACECRAFT CONFIGURATIONS, SPACECRAFT DESIGN,

HC A21/MF A04 THRUST-WEIGHT RATIO

ATTITUDE (INCLINATION), MISSION PLANNING, ORBIT Nc

CALCULATIC'•, ORBIT DECAY N91-20177*# National Aeronautics and Space Ad-inistration.

Langley Research Center, Hampton, VA.

BENEFITS FROM SYNERGIES AND ADVANCED

TECHNOLOGIES FOR AN ADVANCED-TECHNOLOGY SPACE

14 STATION

L. BERNARD GARPETT (National Aeronautics and Space Administration. Langtey Research Center, Hampton, VA.), MELVIN

GROUND SUPPORT SYSTEMS AND FACILITIES J. FEREBEE, JR. (Nalional Aeronautics and Space Administration.

(SPACE) Langley Research Center, Hampton, V'W.), MANUEL J. QUEIJO

(Bionetics Corp., Hampton, VA.), and ANSEL J. BUTTERFIELD

Includes launch complexes, research and production facilities; (Bionetics Corp., Hampton, VA) Washington Apr. 1991 25 p

ground support equipment, e.g., mobile transporters; and (RTOP 506-49-31-01)

simulators. (NASA-TP-3067; L-16616; NAS 1.60:3067) Avail: CASl HC

A03/MF A01

ARTIFICIAL GRAVITY, SPACE STATIONS, SPACECRAFT

N92-12010"# National Aeronautics and Space Administration. CABINS, SPACECRAFT CONFIGURATIONS. SYSTEMS

Lyndon B. Johnson Space Center. Houston, TX. ANALYSIS

CONTROL CENTER TECHNOLOGY CONFERENCE

PROCEEDINGS t.31-27177*# National Aeronautics and Space Administration.

Aug. 1991 641 p Conference held in Clsat Lake, TX, 18-20 Langley Researcr Center, Hampton, VA.

Jun. 1991 Sponsored in part by Houston Univ., Clear Lake, TX TECHNOLOGY FOR THE FUTURE: IN-SPACE TECHNOLOGY

(NASA-CP-lO081; NAS 1.35:10081) Avail: CASI HC A99/MF EXPERIMENTS PROGRAM, PART 1

".J6 ROGER A BRECKENRIDGE, c,,np. (National Aeronautics and

ARCHITECTURE (COMPUTERS), COMMUNICATION Space Administration. Langley Research Center. Hampton, VA.),

NETWORKS. COMPUTER NETWORKS, CONFERENCES, FLIGHT LENWOOD G. CLARK, comp. (National Aeronautics and Space

CONTROL, GROUND BASED CONTROL, GROUND SUPPORT ,dministration. Langley Research Center, Hampton, VA.), KELLI

EQUIPMENT. GROUND SUPPORT SYSTEMS, INTEGRATED F. WILLSHIRE, camp. (National Aeronautics 2nd Space

MISSION CONTROL CENTER Administration. Langley Research Center, Hampton, VA.),

SHERWIN M. BECK, comp. (National Aeronautics and Space

N92-30307"# National Aeronautics and Space Administration. Administration. Langley Research Center, Hampton, VA.), and LISA

Lewis Research Center, Cleveland, OH. D. COLL!ER, comp. (Computer Technology Associates, Inc.,

THREE-DIMENSIONAL LASER WINDOW FORMATION Hampton, VA.) Jun. 1991 304 p Workshop held in Atlana3,

VINCENT G. VERHOFF Jul. 1992 12 p GA, 6-9 Dec. 1988

(RTOP 505-62-84) (RTOP 506-44-41-01)

(NASA-RP-1280; E-6096; NAS 1.61:1280) Avail: CASI HC (NASA-CP-10073-PT-1; NAS 1 55:10073-PT-1) Avail: CASI HC

A03/MF A01 At4/MF A03

The NASA Lewis Research Center has developed and CONFERENCES, INDUSTRIES, NASA SPACE PROGRAMS,

implemented a unique process for forming flawless SPACE STATIONS, UNIVERSITY PROGRAM

three-dimensional laser windows. These windows represent a major

part of specialized, nonintrusive laser data acquisition systems N91-27178"# Nationa! Aeronautics and Space Administration.

used in a variety of compressor and turbine research test facilities. Langley Research Center, Hampton, VA.

This report discusses in detail the aspects of three-dimensional TECHNOLOGY FOR THE FUTURE: IN-SPACE TECHNOLOGY

laser window formation. It focuses on the unique methodology EXPERIMENTS PROGRAM. PART 2

and the peculiarities associated with the formation ot these ROGER A. BRECKENRIDGE, comp. (National Aeronautics and

windows Included in this discussion are the design criteria, bonding Space Administration. Langley Research Center. Hampton, VA),

14
16 SPACE TRANSPORTATION

LENWOOD G CLARK, comp. (National Aeronautics and Space 46

Administration. Langley Research Center, Hampton, VA.), KELLI

F. WILLSHIRE, comp. (National Aeronautics and Space SPACE TRANSPORTATION

Administration. Langley Research Center, Hampton, VA.),

SHERWIN M. BECK, comp. (National Aeronautics and Space

Administration. Langley Research Center, Hampton, VA.), and LISA Includes passenger and cargo space transportation, e g., shuttle

0. COLUER, comp. (Computer Technology Associates, lic., operations; and space rescue techniques

Hampton, VA.) Jun. 1991 304 p Workshop held in Atlanta,

GA, 6-9 Dec. 1988

(RTOP 506-44-41-01) N91-27180°# National Aeronautics and Space Administration

(NASA-CP-10073-PT-2; NAS 1.55:10073-PT-2) Avail: CASI HC Langley Research Center, Hampton, VA

A14/MF A03 LAUNCH VEHICLE INTEGRATION OPTIONS FOR A LARGE

CONFERENCES, INDUSTRIES, NASA SPACE PROGRAMS, EARTH SCIENCES GEOSTATIONARY PLATFORM CONCEPT

SPACE STATIONS, UNIVERSITY PROGRAM JAMES L. GARRISON and LAWRENCE F. ROWELL Jul. 1991

49 p

(RTOP 506-49-21-02) (NASA-TP-3083; L-16819; NAS 1.60:31083) Avail: CASI HC

A03/MF A01

N91-29209'# National Aeronautics and Space Administration. EARTH SCIENCES, GEOSYNCHRONOUS ORBITS, LAUNCH

Marshall Space Flight Center, Huntsville, AL. VEHICLES, ORBIT TRANSFER VEHICLES, ORBITAL ASSEMBLY,

RESOURCE ENVELOPE CONCEPTS FOR MISSION PLANNING PAYLOAD INTEGRATION, SPACE ERECTABLE STRUCTURES,

K Y IBRAHIM (National Aeronautics and Space Administration. SPACE STATIONS, SPACECRAFT LAUNCHING, SYNCHRONOUS

Marshall Space Flight Center, Huntsville, AL.), J. D. WEILER PLATFORMS

(National Aeronautics and Space Administration. Marshall Space

Flight Center, Huntsville, AL.), and J. C. TOKAZ (Sverdrup

Technology. Inc., Huntsville, AL.) Aug. 1991 74 p

(NASA-TP-3139; M-666; NAS 1.60:3139) Avail; CASI HC

A04/MF A01

COST ANALYSIS. MISSION PLANNING, RESOURCES N92-15082"# National Aeronautics and Space Administration

MANAGEMENT. SPACE STATION FREEDOM, SPACE Lewis Research Center, Cleveland, OH.

STATIONS SEALS FLOW CODE DEVELOPMENT

Mar. 1991 172 p Workshop held in Cleveland, OH, 26 Mar.

1991

(RTOP 506-42-72)

N92-31251"# National Aeronautics and Space Administration. (NASA-CP-10070; E-6219; NAS 1.55:10070) Avail: CASI HC

Lewis Research Center, Cleveland, OH. A08/MF A02

GRAPHITE/EPOXY COMPOSITE ADAPTERS FOR THE SPACE COMPUTATIONAL FLUID DYNAMICS, MATHEMATICAL

SHUTTLE/CENTAUR VEHICLE MODELS, PUMP SEALS

HAROLD J. KASPER and DARRYL S. RING (General Dynamics

Corp., San Diego, CA.) Sep. 1990 34 p

(NAS3-2290)

(NASA-TP-3014; E-4969; NAS 1.6073014) Avail: CASI HC A03/MF A01 A ACOMPOSITE N92-20676*# National Aeronautics and Space Administration. ADAPTERS, CENTAUR LAUNCH VEHTEOLE, COMPOSIE John F. Kennedy Space Center, Cocoa Beach. FL.

STRUCTURES, GRAPHITE-EPOXY COMPOSITES. LAUNCH PALDSYDORANRDITRAES

VEHICLE CONFIGURATIONS, SPACE SHUTTLE PAYLOADS, PAYLOAD RAY DOORS AND RADIATOR PANELS

SPACECRAFT CONSTRUCTION MATERIALS, SPACECRAFT FAMILIARIZATION HANDBOOK

DESIGN. SPACECRAFT STRUCTURES, STRUCTURAL JOHN A. GOOBOLD 1992 92 p LIMITED REPRODiCIgILITY.

ANALYSIS, UPPER STAGE ROCKET ENGINES More than 20% of this document may be affected by color

photographs Original contains color illustrations

(NASA-TM-107793; NASA-TP-POD-2; NAS 1.15:107793)

AERODYNAMIC FORCES, BAYS (STRUCTURAL UNITS),

CONTAMINATION, DOORS, FAIRINGS. PANELS, PAYLOADS, N92-32456"# National Aeronautics and Space Administration. SPACE SHUTTLES, THERMAL PROTECTION

Lewis Pesearch Center, Cleveland, OH.

RELIABILITY TRAINING

VINCENT R. LALLI, ed., HENRY A. MALEC, ed. (Siemens

Stromberg-Carlson, Albuquerque, NM.), RICHARD B. DILLARD

(Martin Marietta Corp., Orlando, FL.), KAM L. WONG (Hughes

Aircraft Co., El Segundo. CA.), FRANK J. BARBER, and FRANK N92-22660'# National Aeronautics and Space Administration

J. BARINA Jun. 1992 225 p A reliability/probability device Langley ReseJrch Center, Hampton, VA.

as supplement SPACE TRANSPORTATION MATERIALS AND STRUCTURES

(RTOP 572-10-00) TECHNOLOGY WORKSHOP. VOLUME 1: EXECUTIVE

(NASA-RP-1253; E-5456; NAS 1.61:1253) Avail: CASI HC SUMMARY

A10/MF A03 F. W. CAZIER, JR., comp. and J. E. GARDNER, comp. Apr.

Discussed here is failure physics, the study of how products, 1992 34 p Workshop held in Newport News, VA. 23-26 Sep

hardware, software, and systems fail and what can be done about 1991

it. The intent is to impart useful information, to extend the limits (RTOP 506-43-31-07)

of production capability, and to assist in achieving low cost reliable (NASA-CP-3148-VOL-1; L-17098; NAS 1.55:3148-VOL-1) Avail:

products. A review of reliability for the years 1940 to 2000 is CASI HC A03/MF A01

given. Next, a review of mathematics is given as well as a GOVERNMENT/INDUSTRY RELATIONS, SPACE

c:escription of what elements contribute to product failures. Basic TRANSPORTATION, SPACECRAFT CONSTRUCTION

reliability theory and the disciplines that allow us to control and MATERIALS, SPACECRAFT STRUCTURES. STRUCTURAL

eliminate failures are elucidated. Author ENGINEERING

15
17 SPACE COMM., SPACECRAFT COMM., COMMAND & TRACKING

17 COMPRESSION. IMAGE RESOLUTION, LIFE SCIENCES PULSE

COMMUNICATION, VIDEO DATA

SPACE COMM., SPACECRAFT COMM., COMMAND

& TRACKING 18

Includes telemetry; space communications networks;

astronavigation and guidance, and radio blackout SPACECRAFT DESIGN, TESTING AND

PERFORMANCE

N92-11039'# National Aeronautics and Space Administration. Includes satellites, space platforms, space stations, spacecraft

Goddard Space Flight Center, Greenbelt, MD systems and components such as thermal and environmental

SPACE NETWORK CONTROL CONFERENCE ON RESOURCE controls; and altitude controls

ALLOCATION CONCEPTS AND APPROACHES

KAREN L. MOE, ed, Sep 1991 298 p Conference held in

Greenbelt, MD. 12-13 Dec. 1990 N91-11041*# National Aeronautics and Space Administration

(NASA-CP-3124, REPT-91B00130; NAS 1 553124) Avail: CASI Langley Research Center, Hampton. VA

HC A13/MF A03 THERMAL-DISTORTION ANALYSIS OF A SPACECRAFT BOX ALGORITHMS. DATA LINKS. NETWORK CONTROL. TRUSS IN GEOSTATIONARY ORBIT

RESOURCE ALLOCATION, SPACE COMMUNICATION PATRICK A. COSGROVE (Lockheed Engineering and Sciences

Co., Hampton, VA.), JEFFERY T. FARMER, and LAWRENCE F

N92-19762"# National Aeronautics and Space Administration, ROWELL Washington Nov. 1990 26 p

Lewis Research Center. Cleveland, OH (RTOP 506-49-21-02)

DESTINATION-DIRECTED, PACKET-SWITCHING (NASA.TP-3054: L-16828; NAS 1,60:3054) Avail CASi HC

ARCHITECTURE FOR 30/20-GHZ FDMA/TDM A03/MF A01

GEOSTATIONARY COMMUNICATIONS SATELLITE NETWORK DISTORTION. GEOSYNCHRONOUS ORBITS. HEAT FLUX,

WILLIAM D. tVANCIC and MARY JO SHALKHAUSER Feb. POINTING CONTROL SYSTEMS, SYNCHRONOUS PLATFORMS,

1992 14 p Previously announced as N92-14204 THEHMAL ANALYSIS, TRUSSES

(RTOP 650-60-21)

(NASA-TP-3201: E-6539; NAS 1,60:3201) Avail: CASI HC N91-17114"# National Aeronautics and Space Administration

A03/MF A01 Langley Research Center, Hampton, VA.

ARCHITECTURE (COMPUTERS), COMMUNICATION ON-ORBIT STRUCTURAL DYNAMIC PERFORMANCE OF A

SATELLITES, FREQUENCY DIVISION MULTIPLEXING, PACKET 15-METER MICROWAVE RADIOMETER ANTENNA

SWITCHING, SATELLITE COMMUNICATION, SATELLITE DEBORAH M. WAHLS (National Aeronautics and Space

NETWORKS, TIME DIVISION MULTIPLEXING Administration. Langley Research Center, Hampton, VA ). JEFFERY

T. FARMER (National Aeronautics and Space Administration

N92-2200 1 # National Aeronautics and Space Administration. Langley Research Center, Hampton, VA.), and DAVID W. SLEIGHT

Lewis Research Center, Cleveland, OH. (Illinois Univ., Urbana.) Washington Dec. 1990 44 p

ADVANCED MODULATION AND CODING TECHNOLOGY (RTOP 506-49-21-02)

CONFERENCE (NASA-TP-3041; L-16795: NAS 1.60:3041) Avail CASI HC

Feb. 1992 324 p Conference held in Cleveland, OH, 21-22 A03/MF A01

Jun. 1989 ANTENNA DESIGN. COMPUTER AIDED DESIGN.

(RTOP 650-60-21) GEOSYNCHRONOUS ORBITS, MICROWAVE RADIOMETERS,

(NASA-CP-10053; E-5535; NAS 1.55:10053) Avail: CASI HC MODAL RESPONSE. STRUCTURAL DESIGN, SYNCHRONOUS

A14/MF A03 PLATFORMS

CODING, CONFERENCES, FREQUENCY SHIFT KEYING,

MODULATION. PHASE SHIFT KEYING, SATELLITE N91-18186*# National Aeronautics and Space Administration

COMMUNICATION, SATELLITE INSTRUMENTS Langley Research Center, Hampton, VA.

THE 5TH ANNUAL NASA SPACECRAFT CONTROL

LABORATORY EXPERIMENT (SCOLE) WORKSHOP, PART I

N92-26667"# National Aeronautics and Space Administration. LAWRENCE W. TAYLOR. JR., comp Dec. 1990 383 p

Goddard Space Flight Center, Greenbelt, MD, Workshop held in Lake Arrowhead. CA, 31 Oct. 1988

SMALL EXPLORER DATA SYSTEM MIL-STD-1773 FIBER (RTOP 506-46-1 1-01)

OPTIC BUS (NASA-CP-10057-PT-1; NAS 1.55:10057-PT-1) Avail: CASI HC

MARK FLANEGAN and KEN LABEL Jun. 1992 30 p A17/MF A03

(NASA-TP-3227; NAS 1.60:3227; REPT-92B00041) Avail: CASI CONTROL SYSTEMS DESIGN, LARGE SPACE STRUCTURES,

HC A03/MF A01 MATHEMATICAL MODELS. SPACECRAFT CONTROL

DATA SYSTEMS, EXPLORER SATELLITES, FIBER OPTICS,

SMALL SCIENTIFIC SATELLITES, SPACECRAFT EQUIPMENT N91-18189f# National Aeronautics and Space Administration

Marshall Space Flight Center, Huntsville, AL.

N92-33933"# National Aeronautics and Space Administration. SECOND CONFERENCE ON NDE FOR AEROSPACE

Ames Research Center, Moffett Field, CA REOUIREMENTS

THE EFFECTS OF VIDEO COMPRESSION ON KENNETH W. WOODIS, comp, (National Aeronautics and Space

ACCEPTABILITY OF IMAGES FOR MONITORING LIFE Administration. Marshall Space Flight Center, Huntsville, AL ).

SCIENCES EXPERIMENTS CRAIG C. BRYSON, comp. (National Aeronautics and Space

RICHARD F. HAINES (Foothill-De Anza Community Coll., Los Altos Administration. Marshall Space Flight Center, Huntsville. AL ), and

Hills. CA.) and SHERRY L. CHUANG Jul. 1992 18 p Presented GARY L. WORKMAN, comp. (Alabama Univ., Huntsville.)

at the IEEE Computer Society Data Compression Conference, Washington Dec. 1990 276 p Conference held in Huntsville,

Snowbird, UT, 24-26 Mar. 1992 AL, 22-24 Aug, 1989; sponsored by NASA. Marshall Space Flight

(RTOP 476-14-03) Cenier and Alabama Univ.

(NASA-TP-3239; A-92040; NAS 1.60:3239) Avail: CASI HC (NASA-CP-3091; M-646; NAS 1,55-3091) Avail: CASI HC

A03/MF A01 A13/MF A03

ACCEPTABILITY, ALGORITHMS, BANDWIDTH, DATA ACOUSTIC MEASUREMENT, AEROSPACE SYSTEMS,

16
18 SPACECRAFT DESIGN, TESTING AND PERFORMANCE

COMPUTER AIDED TOMOGRAPHY. CONFERENCES, 1991 377 p Workshop held in Hampton, VA, 25-27 Sep 1990

INSPECTION, NONDESTRUCTIVE TESTS, ULTRASONIC FLAW (RTOP 590-14.11-02)

DETECTION (NASA.CP-10066-PT-1. NAS t55:10066-P1-1) Avail CASI HC

A17/MF A03

N91-18199" National Aeronautics and Space Administration, AEROSPACE ENGINEERING, MAGNETIC SUSPENSION.

Washington, DC. REDUCED GRAVITY, SUPERCONDUCTIVITY, TECHNOLOGY

LARGE SPACE STRUCTURES AND SYSTEMS IN THE SPACE UTILIZATION

STATION ERA: A BIBLIOGRAPHY WITH INDEXES

JOHN J. FERRAINOLO, ed (National Aeronautics and Space N91-21203*# National Aeronautics and Space Administration

Administration. Langley Research Center. Hampton, VA.) Nov. Langley Research Center, Hampton, VA

1990 350 p AEROSPACE APPLICATIONS OF MAGNETIC SUSPENSION

(NASA-SP-7085(0O); NAS 1.21:7085(01)) Avail: CASt HC A15 TECHNOLOGY, PART 2

Bibliographies and abstracts are listed for 1372 reports, articles. NELSON J. GROOM, ed. (National Aeronautics and Space

and other documents introduced into the NASA scientific and Administration. Langley Research Center, Hampton, VA) and

technical information system between January 1, 1990 and June COLIN P. BRITCHER. ed. (Old Dominion Univ., Norfolk, VA.) Mar

30. 1990. Its purpose is to provide helpful information to the 1991 394 p Workshop held in Hampton, VA, 25-27 Sep 1990

researcher, manager, and designer in technology development and (RTOP 590-14-11-02)

mission design according to system, interactive analysis and design, (NASA-CP-10066-PT-2; NAS 1 55 10066-PT-2) Avail CASI HC

structural and thermal analysis and design, structural concepts A17/MF A04

and control systems, electronics, advanced materials, assembly CONTROL SYSTEMS DESIGN. CONTROL THEORY.

concepts, propulsion, and solar power satellite systems. Author MAGNETIC BEARINGS, MAGNETIC SUSPENSION, POINTING

CONTROL SYSTEMS. SUPERCONDUCTIVITY

N91-19122*# National Aeronautics and Space Administration.

Langley Research Center, Hampton, VA. N91-22302'# National Aeronautics and Space Administration

THE 5TH ANNUAL NASA SPACECRAFT CONTROL Langley Research Center, Hampton, VA.

LABORATORY EXPERIMENT (SCOLE) WORKSHOP, PART 2 RIGID-BODY-CONTROL SUBSYSTEM SIZING FOR AN EARTH

LAWRENCE W. TAYLOR, JR., comp. Dec. 1990 369 p SCIENCE GEOSTATIONARY PLATFORM

Workshop held in Lake Arrowhead, CA, 31 Oct. 1988 A. DON SCOTT (National Aeronautics dnd Space Administration.

(RTOP 506-46-11 -01) Langley Research Center, Hampton, VA.), JAMES A DURICY

(NASA-CP-10057-PT-2; NAS 1.55:10057-PT-2) Avail: CASI HC (George Washington Univ.. Hampton, VA.), and CHERYL C

A16/MF A03 JACKSON (Flight Mechanics and Control. Inc., Hampton. VA.)

CONFERENCES, CONTROL SYSTEMS DESIGN, DYNAMIC Washington May 1991 22 p

STRUCTURAL ANALYSIS, FLEXIBLE SPACECRAFT, LARGE (RTOP 506-49-21-02)

SPACE STRUCTURES, MATHEMATICAL MODELS, SPACECRAFT (NASA.TP-3087; L-16796; NAS 1.60:3087) Avail: CASI HC

CONTROL A03/MF A01

CONTROL SYSTEMS DESIGN, EARTH SCIENCES, POINTING

N91-19126*# National Aeronautics and Space Administration. CONTROL SYSTEMS, REACTION WHEELS. RIGID

Goddard Space Flight Center, Greenbelt, MD. STRUCTURES, SATELLITE ATTITUDE CONTROL, SPACECRAFT

SIXTEENTH SPACE SIMULATION CONFERENCE CONFIRMING CONTROL, SYNCHRONOUS PLATFORMS

SPACEWORTHINESS INTO THE NEXT MILLENNIUM

JOSEPH L. STECHER, 111, ed. Washington Nov. 1990 464 p N91-22307°# National Aeronautics and Space Administration

Symposium held in Albuquerque, NM, 5-8 Nov. 1990; sponsored Langley Research Center, Hampton, VA

by NASA, Inst. of Ervironmental Sciences, AIAA, and the American FOURTH NASA WORKSHOP ON COMPUTATIONAL CONTROL

Society for Testing and Materials OF FLEXIBLE AEROSPACE SYSTEMS, PART 1

(NASA-CP-3096; REPT-tP0B00146; NAS 1.55:3096) Avail: CASI LAWRENCE W. TAYLOR, JR., comp Mar 1991 457 p

HC A20/MF A04 Workshop held in Williamsburg, VA, 11-13 Jul. 1990

CONFERENCES, SPACE ENVIRONMENT SIMULATION, (RTOP 506-46-11-01)

SPACECRAFT CONTAMINATION, THERMAL SIMULATION (NASA-CP-10065-PT-1; NAS 1.55:10065-PT-1) Avail: CASI HC

A20/MF A04

N91-21185"# National Aeronautics and Space Administration. AEROSPACE SYSTEMS, CONTROL SYSTEMS DESIGN,

Lewis Research Center, Cleveland, OH. CONTROL THEORY, FLEXIBLE SPACECRAFT, ROBOT

A NEW FABRICATION METHOD FOR PRECISION ANTENNA CONTROL, SPACECRAFT CONTROL

REFLECTORS FOR SPACE FLIGHT AND GROUND TEST

G. RICHARD SHARP, JOYCE S. WANHAINEN, and DEAN A, N91-22331"# National Aeronautics and Space Administration

KETELSEN Washington Mar. 1991 19 p Presented at the Langley Research Center, Hampton, VA.

13th International Communications Satellite Systems Conference, FOURTH NASA WORKSHOP ON COMPUTATIONAL CONTROL

Los Angeles, CA, 11-15 Mar. 1990; sponsored by AIAA Previously OF FLEXIBLE AEROSPACE SYSTEMS, PART 2

announced in IAA as A90-25627 Original contains color LAWRENCE W TAYLOR, JR., comp. Mar. 1991 464 p

illustrations Workshop held in Williamsburg, VA, 11-13 Jul. 1990

(RTOP 650-60-20) (RTOP 506-46-11.01)

(NASA-TP-3078: E-5176; NAS 1.60:3078) Avail: CASI HC (NASA-CP-10065-PT-2; NAS 1.55:10065-PT-2) Avail: CASI HC

A03/MF A01; 2 functional color pages A20/MF A04

ANTENNA DESIGN, COMMUNICATION SATELLITES, DESIGN AEROSPACE SYSTEMS, AIRCRAFT CONTROL,

ANALYSIS, FABRICATION, REFLECTOR ANTENNAS, CONFERENCES, DYNAMIC STRUCTURAL ANALYSIS, FLEXIBLE

REFLECTORS, SATELLITE ANTENNAS SPACECRAFT, FLEXIBLE WINGS, FLUTTER, LARGE SPACE

STRUCTURES, OPTIMAL CONTROL, ROBOTICS, VIBRATION

N91-21188"# National Aeronautics and Space Administration. DAMPING

Langley Research Center, Hampton, VA.

AEROSPACE APPLICATIONS OF MAGNETIC SUSPENSION N91-27182"# National Aeronautics and Space Administration.

TECHNOLOGY, PART 1 Langley Research Center, Hampton, VA.

NELSON J. GROOM, ed. (National Aeronautics and Space PACKAGING, DEVELOPMENT, AND ON-ORBIT ASSEMBLY

Administration. Langley Research Center, Hampton, VA.) and OPTIONS FOR LARGE GEOSTATIONARY SPACECRAFT

COLIN P. BRITCHER, ed. (Old Dominion Univ., Norfolk, VA.) Mar. WILLIAM T. DAVIS (National Aeronautics and Space

17
18 SPACECRAFT DESIGN, TESTING AND PERFORMANCE

Administration. Langley Research Center, Hampton, VA.) and Sep. 1991 369 p Symposium held in League City, TX, 6-8

CHARLES B. KING (Bionetics Coip., Hampton, VA.) Washington Aug. 1991

Jul. 1991 34 p (NASA-CP-10083-VOL-i-PT-2; S-653-VOL-1-PT-2: NAS

(RTOP 506-49-31-01) 1t55:10083-VOL-1-PT-2) Avail: CASI HC A16/MF A03

(NASA-TP-3088" L-16863; NAS 1,60:3088) Avail: CASt HC CONFERENCES, EXPERT SYSTEMS, SPACE STATION

A03/MF A01 FREEDOM

GEOSYNCHRONOUS ORBITS, LARGE SPACE STRUCTURES,

LAUNCH VEHICLES, ORBITAL ASSEMBLY, PAYLOAD N92-17768"# National Aeronautics and Space Administraton,

INTEGRATION, SPACE ERECTABLE STRUCTURES,

SPACECRAFT DESIGN, SYNCHRONOUS SATELLITES Washington, DC.

BEYOND THE BASELINE 1991: PROCEEDINGS OF THE

SPACE STATION EVOLUTION SYMPOSIUM. VOLUME 2:

Ngl-28191* National Aeronautics and Space Administration. SPACE STATION FREEDOM, PART 1

Washington, DC. Sep. 1991 273 p Symposium held in League City. TX, 6-8

LARGE SPACE STRUCTURES AND SYSTEMS IN THE SPACE Aug. 1991

STATION ERA: A BIBLIOGRAPHY WITH INDEXES Aug. 1991 JOHN J, FERRAINOLO. comp. and GEORGE F. LAWRENCE. (NASA-CP-10083-VOL-2-PT-1, S-653-VOL-2-PT-., NAS

cOmH Ma 191 329 mp. an1.55:10083-VOL-2-PT-1) Avail: CASI HC A12/MF A03

comp. May 1991 329 p AEROSPACE ENGINEERING, CONFERENCES, DISTRI-

(NASA-SP-7085(02); NAS 1.21:7085(02)) Avail: CASl HC A15 BUTED PARAMETER SYSTEMS, FUNCTIONAL DESIGN

Bibliographies and abstracts are listed for 1219 reports, articles, SPECIFICATIONS, MISSION PLANNING, PROJECT PLANNING.

and other documents introduced into the NASA scientific and SPACE STATION FREEDOM, SPACECRAFT DESIGN. USER

technical information system between July 1, 1990 and December REQUIREMENTS

31, 1990. The 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, N92-22317* National Aeronautics and Space Administration,

structural and thermal analysis and design, structural concepts Washington, DC.

and control systems, electronics, advanced materials, assembly LARGE SPACE STRUCTURES AND SYSTEMS IN THE SPACE

concepts, propulsion, and solar power satellite systems. Author STATION ERA: A BIBLIOGRAPHY WITH INDEXES

(SUPPLEMENT 03)

N92-11087"# National Aeronautics and Space Administration. Dec. 1991 324 p

Langley Research Center, Hampton, VA. (NASA-SP-7085(03); NAS 1.21:7085(03)) Avai: CASI HC A14

MULTIDISCIPLINARY OPTIMIZATION OF CONTROLLED Bibliographies and abstracts are listed for 1221 reports, articles,

SPACE STRUCTURES WITH GLOBAL SENSITIVITY and other documents introduced into the NASA scientific and

EQUATIONS technical information system between January 1, 1991 and June

SHARON L. PADULA, BENJAMIN B. JAMES, PHILIP C. GRAVES 30, 1991. Topics covered include large space structures and

(Vigyan Research Associates, Inc., Hampton, VA.), and STANLEY systems, space stations, extravehicular activity, thermal

E. WOODARD Nov. 1991 39 p environments and control. tethering, spacecraft power supplies.

(RTOP 506-43-41-01) structural concepts and cointrol systems, electronics, advanced

(NASA-TP-3130; NAS 1.60:3130) Avail: CASI HC A03/MF A01 materials, propulsion, policies and international cooperation,

CONTROL SYSTEMS DESIGN, LARGE SPACE STRUCTURES, vibration and dynamic controls, robotics and remote operations,

OPTIMIZATION, SPACECRAFT CONTROL, SPACECRAFT data and communication systems, electric power generation. space

DESIGN, SPACECRAFT STRUCTURES, WEIGHT REDUCTION commercialization, orbital transfer, and human factors

engineering. Author

N92-17098*# National Aeronautics and Space Administration,

Washington, DC. N92-27721"# National Aeronautics and Space Administration.

BEYOND THE BASELINE 1991: PROCEEDINGS OF THE Langley Research Center, Hampton, VA.

SPACE STATION EVOLUTION SYMPOSIUM. VOLUME 1: INTERNATIONAL SYMPOSIUM ON MAGNETIC SUSPENSION

SPACE STATION FREEDOM, PART 1 TECHNOLOGY, PART I

Sep. 1991 336 p Symposium held in League City, TX, 6-8 NELSON J. GROOM, ed. and COLIN P. BfIiCHER, ed. (Old

Aug. 1991 Dominion Univ., Norfolk, VA.) Washington May 1992 470 p

(NASA.CP-10083-VOL-1-PT-1; S-653-VOL-I-PT-1: NAS Symposium held in Hampton, VA, 19-23 Aug. 1991

1.55:10083-VOL-1-PT-1) Avail: CASt HC A15/MF A03 (RTOP 590-14-11-02)

SPACE STATION FREEDOM, SPACECRAFT (NASA-CP-3152-PT-1; L-17092-PT-1; NAS 1.55:3152-PT-1)

CONFIGURATIONS, SPACECRAFT DESIGN, USER Avail: CASI HC A20/MF A04

REQUIREMENTS CONFERENCES, CONTROL EQUIPMENT. MAGNETIC

BEARINGS, MAGNETIC CONTROL, MAGNETIC LEVITATION

N92-17348 # National Aeronautics and Space Administration, VEHICLES. MAGNETIC SUSPENSION, SUPERCONDUCTING

Washington, DC. MAGNETS

BEYOND THE BASELINE 1991: PROCEEDINGS OF THE

SPACE STATION EVOLUTION SYMPOSIUM. VOLUME 2:

SPACE STATION FREEDOM, PART 2 N92-27786"# National Aeronautics and Space Administration

Sep. 1991 464 p Symposium held in League City, TX, 6-8 Langley Research Center. Hampton, VA

Aug. 1991 INTERNATIONAL SYMPOSIUM ON MAGNETIC SUSPENSION

(NASA-CP-10083-VOL-2-PT-2; S-653-VOL-2-PT-2; NAS TECHNOLOGY, PART 2

1.55:10083-VOL-2-PT-2) Avail: CASI HC A20/MF A04 NELSON J. GROOM, ed. (Cray Research, Inc., Albuquerque. NM.)

CONFERENCES. EVOLUTION (DEVELOPMENT), PROJECT and COLIN P. BRITCHER, ed. (Old Dominion Univ., Norfolk. VA.)

PLANNING, SOFTWARE ENGINEERING, SPACE STATION Washington May 1992 459 p Symposium held in Hampton,

FREEDOM, SYSTEMS ENGINEERING VA, 19-23 Aug. 1991

(RTOP 590-14-11-02)

N92-17409°# National Aeronautics and Space Administration, (NASA-CP-3152-PT-2; L-17092-PT-2: NAS 1.55:3152-PT-2)

Washington, DC. Avail: CASI HC A20/MF A04

BEYOND THE BASELINE 1991: PROCEEDINGS OF THE CONTROL SYSTEMS DESIGN, MAGNETIC BEARINGS,

SPACE STATION EVOLUTION SYMPOSIUM. VOLUME 1: MAGNETIC SUSPENSION. SUPERCONDUCTING MAGNETS.

SPACE STATION FREEDOM, PART 2 SUPERCONDUCTIVITY

18
20 SPACECRAFT PROPULSION AND POWER

N92-28730"# National Aeronautics and Space Administration. N91-19182"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, VA. Lewis Research Center, Cleveland, OH.

ONGOING PROGRESS IN SPACECRAFT CONTROLS SPACE PHOTOVOLTAIC RESEARCH AND TECHNOLOGY,

DAVE GHOSH, ed. (Lockheed Engineering and Sciences Co., 1989

Hampton, VA.) Jul. 1992 143 p Workshop held in Hampton, Washington Jan. 1991 515 p Tenth conference held in

VA, 13 Jan. 1992 Cleveland, OH, 7-9 Nov. 1989

(RTOP 506-59-61-01) (RTOP 506-41.11)

(NASA-CP-10099; NAS 1.55:10099) Avail: CASI HC A07/MF (NASA-CP-3107; E-5728; NAS 1.55:3107) Avail: CASI HC

A02 A22/MF A04

ADAPTIVE CONTROL, CONTROL SYSTEMS DESIGN, CONFERENCES, PHOTOVOLTAIC CELLS, PHOTOVOLTAIC

DYNAMIC STRUCTURAL ANALYSIS, MANNED MARS MISSIONS. CONVERSION, SOLAR ARRAYS, SOLAR CELLS, SPACECRAFT

MANNED SPACECRAFT, NASA SPACE PROGRAMS, ROBOTICS, POWER SUPPLIES

SPACE EXPLORATION, SPACECRAFT CONTROL

N91-24307"# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, OH.

19 STRUCTURAL INTEGRITY AND DURABILITY OF REUSABLE SPACE PROPULSION SYSTEMS

Apr. 1989 259 p Conference held in Cleveland, OH, 18-19

SPACECRAFT INSTRUMENTATION Apr. 1989

(RTOP 553-13-00)

(NASA-CP-10030; E-4628; NAS 1.55:10'30) Avail: CASI HC

A12/MF A03

CONFERENCES, DYNAMIC STRUCTURAL ANALYSIS, LIFE

N92-25147*# National Aeronautics and Space Administration. (DURABILITY), PREDICTION ANALYSIS TECHNIQUES,

Langley Research Center, Hampton, VA. PROPULSION SYSTEM CONFIGURATIONS, REUSABLE ROCKET

FEASIBILITY STUDY OF A LOW-ENERGY GAMMA RAY ENGINES

SYSTEM FOR MEASURING QUANTITY AND FLOW RATE OF

SLUSH HYDROGEN N91-25176"# National Aeronautics and Space Administration.

JAG J. SINGH, CHIH-PING SHEN, and DANNY R. SPriINKLE Washington, DC.

(Old Dominion Univ., Norfolk, VA.) Apr. 1992 14 p SPACE TRANSPORTATION PROPULSION TECHNOLOGY (RTOP 307-50-10-02) SYMPOSIUM. VOLUME 1: EXECUTIVE SUMMARY

(NASA-TP-3150; L-16980; NAS 1.60:3150) Avail: CASI HC May 1991 36 p Symposium held in State College, PA, 25-29

A03/MF A01 Jun. 1990

FEASIBILITY ANALYSIS, FLOW VELOCITY, GAMMA RAYS, (NASA.CP-3112; NAS 1.55:3112) Avail: CASI HC A03/MF A01

SLUSH HYDROGEN X RAYS BOOSTER ROCKET ENGINES, PROPULSION, PROPULSION

SYSTEM CONFIGURATIONS, SPACE TRANSPORTATION,

SPACE TRANSPORTATION SYSTEM

20 N91-28193 # National Aeronautics and Space Administration,

Washington, DC.

SPACECRAFT PROPULSION AND POWER SPACE TRANSPORTATION PROPULSION TECHNOLOGY

SYMPOSIUM. VOLUME 2: SYMPOSIUM PROCEEDINGS

Includes main propulsion systems and components, e.g., rocket May 1991 693 p Symposium held in State College, PA. 25-29

engines; and spacecraft auxiliary power sources. Jun. 1990

(NASA-CP-3112-VOL-2; NAS 1.55:3112-VOL-2) Avail: CASI HC

A99/MF A06

N91-11800"# National Aeronautics and Space Administration. PROPULSION SYSTEM CONFIGURATIONS, PROPULSION

Lewis Research Center, Cleveland, OH SYSTEM PERFORMANCE, SPACE TRANSPORTATION, SPACE

METALLIZED PROPELLANTS FOR THE HUMAN TRANSPORTATION SYSTEM, SPACECRAFT POWER SUPPLIES

EXPLORATION OF MARS

BRYAN A. PALASZEWSKI Nov. 1,990 14 p 491-2823S $# National Aeronautics and Space Administration,

(RTOP 506-42-00) Washington, DC.

(NASA-TP-3062; E-5544; NAS 1.60:3062) Avail: CASI HC SPACE TRANSPORTATION PROPULSION TECHNOLOGY

A03/MF A01 SYMPOSIUM. VOLUME 3: PANEL SESSION SUMMARIES AND

EARTH ORBITS, LAUNCHING, MANNED MARS MISSIONS, PRESENTATIONS

METAL PROPELLANTS, MISSION PLANNING, PAY'LOADS, May 1991 620 p Symposium held !n State College. PA, 25-29

SPACE TRANSPORTATION Jun. 1990

(NASA-CP-3112-VOL-3; NAS 1.55:3112.VOL-3) Avail: CASI HC

N91-15308*# National Aeronautics and Space Administration. A99/MF A06

Lewis Research Center, Cleveland, OH. CONFERENCES, PROPULSION SYSTEM CONFIGURATIONS,

LUNAR MISSIONS USING CHEMICAL PROPULSION: SYSTEM SPACE TRANSPORTATION, SPACE TRANSPORTATION

DESIGN ISSUES SYSTEM, SPACECRAFT PROPULSION

BRYAN PALASZEWSKI Jan. 1991 13 p Presented at the

26th Joint Propulsion Conlerence, Orlando, FL, 16-18 Ju, l. 1990: N91-30203"# National Aeronautics and Space Adminstration

sponsored in part by AIAA, ASME, SAE, and ASEE Previously Lewis Research Center, Cleveland, OH.

announced as A90-47221 SPACE PHOTOVOLTAIC RESEARCH AND TECHNOLOGY

(RTOP 506-42-51) CONFERENCE

(NASA-TP-3065: E-5542, NAS 1.60:3065) Avail: CASI HC Aug. 1991 471 p The 11th Conference was held in Cleveland,

A03/MF A01 OH, 7-9 May 1991

CHEMICAL PROPULSION, HYDRAZINES, LUNAR BASES, (RTOP 506-41-11)

METAL PROPELLANTS. PAYLOADS, PROPELLANT ADDITIVES, (NASA-CP.3121; E-6161; NAS 1 55:3121) Avail. CASI HC

PROPULSION SYSTEM CONFIGURATIONS, PROPULSION A20/MF A04

SYSTEM PERFORMANCE, SPACE TRANSPORTATION AEROSPACE ENVIRONMENTS, CONFERENCES, ELECTRON

19
20 SPACECRAFT PROPULSION AND POWER

IRRADIATION, EXPOSURE, PHOTOVOLTAIC CONVERSION, ABSORPTIVITY, COMBUSTION PRODUCTS, EXHAUST

PROTON IRRADIATION, RADIATION DAMAGE, SOLAR CELLS, EMISSION, OPTICAL MEASUREMENT, ROCKET EXHAUST,

SPACECRAFT POWER SUPPLIES SLAGS, SOLID PROPELLANT ROCKET ENGINES, SOLID

ROCKET PROPELLANTS, SPACE DEBRIS, SPACE SHUTTLE

N92-10044c# National Aeronautics and Space Administration. BOOSTERS, THERMAL EMISSION

Lewis Research Center, Cleveland, OH.

MAGNETOPLASMADYNAMIC THRUSTER WORKSHOP N92-21517*# National Aeronautics and Space Administration

1991 178 p Workshop held in Washington, DC, 16 May 1991; Lewis Research Center. Cleveland, OH. '

sponsored in part by NASA, Washington ROCKET-BASED COMBINED-CYCLE (RBCC) PROPULSION

(RTOP 506-42-31) TECHNOLOGY WORKSHOP. TUTORIAL SESSION

(NASA-CP-10084; E-6518; NAS 1.55:10084) Avail: CASI HC 1992 259 p Workshop held in Huntsville, AL, 23-27 Mar.

A09/MF A02 1992; sponsored by NASA, Washington

CONFERENCES, ELECTRIC ROCKET ENGINES, LOW (RTOP 590-21-11)

THRUST PROPULSION, MAGNETOPLASMADYNAMICS, PLASMA (NASA-CP-10090; E-6929; NAS 1.55:10090) Avail: CASI HC

PROPULSION A12/MF A03

AEROSPACE PLANES, ENGINE PARTS. Hii FEAS3,IC

N92-11088"# National Aeronautics and Space Administration. FLIGHT, ROCKET ENGINE DESIGN, ROCKET ENGINES

Lewis Research Center, Cleveland, OH.

NUCLEAR THERMAL PROPULSION: A JOINT N92-27130"# National Aeronautics and Space Administration.

NASA/DOE/LOD WORKSHOP Marshall Space Flight Center. Huntsville, AL

JOHN S. CLARK, ed. 1991 500 p Workshop held in Cleveland, THE 1990 NASA AEROSPACE BATTERY WORKSHOP

OH, 10-12 Jul. 1990 LEWIS M KENNEDY. comp. Washington May 1991 888 p

(RTOP 593-71-00) Workshop held in Huntsville, AL, 4-6 Dec. 1990

(NASA-CP-10079; E-6456; NAS 1.55:10079) Avail: CASI HC (NASA-CP-3119; M-661; NAS 155:3119) Avail: CASI HC

A21/MF A04 A99/MF A10

NUCLEAR ENGINE FOR ROCKET VEHICLES, NUCLEAR AEROSPACE ENGINEERING, CONFERENCES. LITHIUM

PROPULSION, PROJECT MANAGEMENT, PROJECT PLANNING, SULFUR BATTERIES, NICKEL CADMIUM BATTERIES. NICKEL

PROPULSION SYSTEM CONFIGURATIONS, PROPULSION HYDROGEN BATTERIES, SILVER ZINC BATTERIES,

SYSTEM PERFORMANCE, REACTOR DESIGN, REACTOR SPACECRAFT POWER SUPPLIES. TECHNOLOGY

TECHNOLOGY, RESEARCH PROJECTS, ROCKET ENGINE ASSESSMENT

DESIGN

N92-12052"# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, AL. 23

AUTOMATING A SPACECRAFT ELECTRICAL POWER

SYSTEM USING EXPERT SYSTEMS CHEMISTRY AND MATERIALS (GENERAL)

L. F. LOLLAR Washington Oct. 1991 22 p

,NASA-TP-3161; M-670; NAS 1.60:3161) Avail: CASt HC

A03/MF A01

AUTOMATIC CONTROL, AUTONOMY, BREADBOARD

MODELS, EXPERT SYSTEMS, SPACE STATION FREEDOM, N91-20207*# National Aeronautics and Space AdministrationSPACECRAFT POWER SUPPLIES Langley Research Center, Hampton. VA_

N92-14108"# National Aeronautics and Space Administration. NATIONAL EDUCATORS' WORKSHOP: UPDATE 1988.

Marshall Space Flight Center, Huntsville, AL. STANDARD EXPERIMENTS IN ENGINEERING MATERIALS

LIMIT CYCLE VIBRATIONS IN TURBOMACHINERY SCIENCE AND TECHNOLOGY

S. G. RYAN Dec. 1991 84 p JAMES E. GARDNER, comp. (National Aeronautics and Space

(NASA-TP-3181; M-676; NAS 1.60:3181) Avail: CASI HC Administration. Langley Research Center. Hampton, VA.) and A05/MF A01 JAMES A. JACOBS, comp. (Norfolk State Univ., VA.)

ROTOR DYNAMICS, ROTORS, SPACE SHUTTLE MAIN Washington Jan. 1990 83 p Workshop held in Gaithersburg,

ENGINE, TURBINE PUMPS, TURBOMACHINERY, VIBRATION MD, 10-12 May 1988: sponsored by NASA, Washington and NIST.

Gaithersburg, MD

N92-17151"# National Aeronautics and Space Administration. (NAG1-976; RTOP 505-63-01-15)

Lewis Research Center, Cleveland, OH. (NASA-CP-3060; L-16732; NAS 1.55:3060) Avail: CASI HC

UPPER STAGES USING LIQUID PROPULSION AND A05/MF A01

METALLIZED PROPELLANTS CONFERENCES, EDUCATION, EXPERIMENTATION.

BRYAN A. PALASZEWSKI Washington Feb. 1992 .22 p FRACTURE SUECNDC2S MECHANICS, FRACTURING, ISETINpAIORPYHIGH TEMPERATURE

(RTOP 506-42-72) SUPERCONDUCTORS, INSPECTION, RADIOGRAPHY.

(NASA-TP-3191; E-6105; NAS 1.60:3191) Avail: CASI HC RESEARCH AND DEVELOPMENT, TECHNOLOGIES

A03/MF A01

GELLED PROPELLANTS, INERTIAL UPPER STAGE, LAUNCH

VEHICLES, METAL PROPELLANTS, PROPELLANT ADDITIVES, 24

SPACE MISSIONS, SPACE TRANSPORTATION, SPACE

TRANSPORTATION SYSTEM, SPACECRAFT PROPULSION COMPOSITE MATERIALS

N92-20949'# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville. AL. Includes physical, chemical, and mechanical properties of laminates

OPTICAL MEASUREMENTS ON SOLID SPECIMENS OF SOLID and other composite materials.

ROCKET MOTOR EXHAUST AND SOLID ROCKET MOTOR

SLAG

F E. ROBERTS, ill Washington Dec, 1991 20 p N91-10127°# National Aeronautics and Space Administration

(RTOP 476-50-03) Lewis Research Center, Cleveland, OH

(NASA-TP-3177; M-674; NAS 1.60:3177) Avail: CASI HC STRUCTURAL PROPERTIES OF LAMINATED DOUGLAS

A03/MF A01 FIR/EPOXY COMPOSITE MATERIAL

20
24 COMPOSITE MATERIALS

DAVID A- SPERA (Sverdrup Technology, Inc, Cleveland, OH.). COMPOSITES, HOLE DISTRIBUTION (MECHANICS), IMPACT

JACK B. ESGAR (Gougeon Bros., Inc.. Bay City, MI.), MEADE DAMAGE, LAMINATES. THERMOPLASTIC RESINS

GOUGEON, and MICHAEL D. ZUTECK (Gougeon Bros., Inc.. Bay

City. MI.) May 1990 140 p N91-18216"# National Aeronautics and Space Administration

(NAS3-25266; DE-AI01-76ET-20320; RTOP 776-33-41) Langley Research Center. Hampton, VA

(NASA-RP-1236; E-4720: NAS 1.61:1236: DOE/NASA/20320-76) INVESTIGATION OF MICROSTRUCTURAL CHANGES IN

Avail: CASt HC A07/MF A02 POLYETHERETHER-KETONE FILMS AT CRYOGENIC

This publication contains a compilation of static and fatigue TEMPERATURES BY POSITRON LIFETIME SPECTROSCOPY

strength data for laminated-wood material made from Douglas fir JAG J SINGH (National Aeronautics and Space Administration

and epoxy. Results of tests conducted by several organizations Langley Research Center, Hampton, VA ), ABE EFTEKHARI

are correlated to provide insight into the effects of variables such (Analytical Services and Materals, Inc, Hampton, VA ), TERRY L

as moisture, size, lamina-to-lamina joint design. wood veneer grade, ST CLAIR (National Aeronautics and Space Administration Langley

and the ratio of cyclic stress to steady stress during fatigue testing. Research Center, Hampton, VA), and DANNY R SPRINKLE

These test data were originally obtained during development of Washington Mar. 1991 13 p

wood rotor blades for large-scale wind turbines of the (RTOP 506-43-21-05)

horizontal-axis (propeller) configuration. Most of the strength (NASA.TP.3064, L-16841; NAf- I3O4' A',3.151 CASI HC

property data in this compilation are not found in the published A03/MF A01

literature. Test sections ranged from round cylinders 2.25 in. in COOLING, MICROSTRUCTURE, PEEK, POSITRON

diameter to rectangular slabs 6 by 24 in. in cross section and ANNIHILATION, SPECTROSCOPY. TEMPERATURE EFFECTS

approximately 30 ft. long. All specimens were made from Douglas

fir veneers 0.10 in. thick, bonded together with the WEST epoxy N91-21242*# National Aeronautics and Space Administration

system developed for fabrication and repair of wood boats. Loading Marshall Space Flight Center. Huntsville. AL

was usually parallel to the grain. Size effects (reduction in strength A NOVEL METHOD OF TESTING THE SHEAR STRENGTH OF

with increase in test volume) are observed in some of the test THICK HONEYCOMB COMPOSITES

data, and a simple mathematical model is presented that includes A. J. HODGE and A. T. NETTLES Mar 1991 16 p

the probability of failure. General characteristics of the wood/epoxy (NASA-TP.3108; NAS 1 60:3108) Avail: CASI HC A03/MF A01

laminate are discussed, including features that make it useful for HONEYCOMB CORES, HONEYCOMB STRUCTURES. IMPACT

a wide variety of applications, Author DAMAGE, IMPACT TESTS, IMPACT TOLERANCES. SHEAR

STRENGTH

N91-13492"# National Aeronautics and Space Administration. N91-29240"# National Aeronautics and Space Administration

Langley Research Center, Hampton, VA. Langley Research Center, Hampton, VA

AN INVESTIGATION OF MICROSTRUCTURAL NASA WORKSHOP ON IMPACT DAMAGE TO COMPOSITES

CHARACTERISTICS OF CONTACT-LENS POLYMERS C_ C. POE, JR. Jul 1991 476 p Workshop held in Hampton,

JAG J SINGH (National Aeronautics and Space Administration. Va, 19-20 Mar. 1991

Langley Research Center, Hampton, VA.), ABE EFTEKHARI (RTOP 505-63-50.04)

(Analytical Services and Materials, Inc., Hampton, VA.), BILLY T. (NASA-CP-10075; NAS 1.55:10075) Avail. CASI HC A21/MF

UPCHURCH (National Aeronautics and Space Administration, A04

Langley Research Center, Hampton, VA.). and KAREN S. BURNS COMPOSITE STRUCTURES, CONFERENCES. IMPACT

(Old Dominion Univ., Norfolk, VA.) Washington Dec. 1990 DAMAGE, POLYMER MATRIX COMPOSITES

12 p

(RTOP 412.20-26-01) N92-10067*# National Aeronautics and Space Administration

(NASA-TP-3034. L-16817, NAS 1.60:3034) Avail: CASI HC Langley Research Center, Hampton, VA

A03/MF A01 PROPERTIES OF THREE GRAPHITE/TOUGHENED RESIN

CONTACT LENSES. GASEOUS DIFFUSION. MICROSTRUC- COMPOSITES

TURE, PERMEABILITY. VOLUME DONALD L. SMITH (Lockheed Enginei-'g and Sciences Co.

Hampton, VA.) and MARV"I C DOW Washington Sep 1991

N91-14437"# National Aeronautics and Space Administration. 50 p

Goddard Space Fiight Center, Greenbelt, MD (RTOP 505-63-50-05)

OUTGASSING DATA FOR SELECTING SPACECRAFT (NASA-TP-3102: L-16910; NAS 1 60 3102) Avail. CASI HC

MATERIALS, REVISION 2 A03/MF A01

WILLIAM A. CAMPBELL, JR. and JOHN J SCIALDONE COMPRESSION TESTS, GRAPHITE-EPOXY COMPOSITES.

Washington Nov. 1990 398 p IMPACT DAMAGE, IMPACT LOADS, IMPACT TESTS.

(NASA-RP- I 124-REV-2; REPT-90B00 1 38-REV-2; NAS LAMINATES

1.61 1124-REV-2; NASA-RP-1014: NASA-TN-D-7362;

NASA-TN-D-8008) Avail CASI HC A17/MF A04 N92-11142"# National Aeronautics and Space Adminstraton

Outgassing data, derived from tests at 398 K (125 C) for 24 Marshall Space Flight Center. Huntsville, AL

hours in vacuum as per ASTM E 595-77, were compiled for AN EXAMINATION OF THE DAMAGE TOLERANCE

numerous materials for spacecraft use. The data presented are ENHANCEMENT OF CARBON/EPOXY USING AN OUTER

the total mass loss (TML) and the collected volatile condensable LAMINA OF SPECTRA (R) Final Report

materials (CVCM). The various materials are listed by likely usage 0 G, LANCE and A T NETTLES Washington Oct 1991

and alphabetically Author 33 p

(PROJ 90-17)

(NASA-TP-3160, M-671, NAS I 603160) Avail CASI HC

N91-18215"# National Aeronautics and Space Administration A03/MF A01

Langlby Research Center, Hampton, VA. DAMAGE, EPOXY MATRIX COMPOSITES. IMPACT TESTS,

COMPRESSION BEHAVIOR OF GRAPHITE-THERMOPLASTIC PLATES (STRUCTURAL MEMBERS). POLYETHYLENES.

AND GRAPHITE-EPOXY PANELS WITH CIRCULAR HOLES OR RESIDUAL STRENGTH. TOLERANCES (MECHANICS)

IMPACT DAMAGE

DAWN C JEGLEY Washington Mar 1991 18 p N92-20679'# National Aeronautics and Space Administration

(RTOP 505-63-01-09) Langley Research Center, Hampton. VA

(NASA-TP3071, L.16853, NAS 1 603071) Avail CASI HC OPTIMIZATION OF COMPOSITE SANDWICH COVER PANELS

A03/MF A01 SUBJECTED TO COMPRESSIVE LOADINGS

AXIAL COMPRESSION LOADS, GRAPHITE-EPOXY JUAN R CRUZ Dec 1991 13 p

21
24 COMPOSITE MATERIALS

(RTOP 505-63-50-08) CONFERENCES, FIBER COMPOSITES. FINITE ELEMENT

(NASA-TP-3173; L-16942, NAS 1.60:3173) Avail: CASI HC METHOD, MATHEMATICAL MODELS, MECHANICAL

A03/MF A01 PROPERTIES, STRUCTURAL DESIGN

COMPOSITE STRUCTURES, COMPRESSION LOADS,

COMPUTER PROGRAMS, DESIGN ANALYSIS, OPTIMIZATION, N92-32574"# National Aeronautics and Space Administration.

SANDWICH STRUCTURES, STRUCTURAL DESIGN, WING Langley Research Center, Hampton, VA

PANELS EIGHTH DOD/NASA/FAA CONFERENCE ON FIBROUS

COMPOSITES IN STRUCTURAL DESIGN,-ART 2

N92-20950*# National Aeronautics and Space Administration. JAMES H. STARNES, JR., comp., HERMAN L BOHON. comp

Marshall Space Flight Center, Huntsville, AL. (Lockheed Engineering and Sciences Co., Hampton, VA), and

A STATISTICAL COMPARISON OF TWO CARBON SHERRY B. GARZON, comp. Sep. 1990 315 p Conference

FIBER/EPOXY FABRICATION TECHNIQUES held in Norfolk. VA. 28-30 Nov. 1989

A. J. HODGE Washington Dec. 1991 12 p (RTOP 505-63-01-09)

(NASA-TP-3179: M-673; NAS 1.60:3179) Avail: CASI HC (NASA-CP-3087-PT-2; L-16832-PT-2; NAS 1.55:3087-PT-2)

A03/MF A01 Avail: CASI HC A14/MF A03

AUTOCLAVES, CARBON FIBER REINFORCED PLASTICS, AIRCRAFT CONSTRUCTION MATERIALS, COMPOSITE

CARBON FIBERS, COMPRESSIVE STRENGTH, CURING. EPOXY STRUCTURES, CONFERENCES, FIBER COMPOSITES,

MATRIX COMPOSITES, PRESSES STRUCTURAL ANALYSIS, STRUCTURAL DESIGN

N92-21605"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, MD. 25

AMSAHTS 1990: ADVANCES IN MATERIALS SCIENCE AND

APPLICATIONS OF HIGH TEMPERATURE

SUPERCONDUCTORS INORGANIC AND PHYSICAL CHEMISTRY

LARRY H. BENNETT, ed., YURY FLOM, ed., and KISHIN

MOORJANI, ed. (Johns Hopkins Univ., Laurel, MD.) Jan. 1991 Includes chemical analysis, e.g., chromatography, combustion

488 p Conference held in Greenbelt, MD, 2-6 Apr. 1990; theory; electrochemistry; and photochemistry.

sponsored in cooperation with NASA, NIST, JHU, and DARPA

Previously announced as N90-27792

(NASA-CP-3100; REPT-90B00018; NAS 1.55:3100) Avail: CASI N92-28374"# National Aeronautics and Space Administration.

HC A21/MF A04 Langley Research Center, Hampton. VA.

HIGH TEMPERATURE SUPERCONDUCTORS, OXIDES, AN ANALYSIS OF COMBUSTION STUDIES IN SHOCK

REACTION KINETICS, -URFACE REACTIONS, THER- EXPANSION TUNNELS AND REFLECTED SHOCK TUNNELS

MODYNAMIC PROPERTIES CASIMIR J. JACHIMOWSKI Jul. 1992 12 p

(RTOP 505-62-40-04)

N92-23981"# National Aeronautics and Space Administration. (NASA-TP-3224; L-17025; NAS 1.60:3224) Avail: CASI HC

Langley Research Center, Hampton, VA. A03/MF A01

EFFECT OF LOW-SPEED IMPACT DAMAGE AND DAMAGE COMBUSTION CHAMBERS, COMBUSTION CHEMISTRY,

LOCATION ON BEHAVIOR OF COMPOSITE PANELS COMBUSTION PHYSICS, HYPERSONIC FLIGHT, REACTION

DAWN C. JEGLEY May 1992 27 p Presented at the 9th KINETICS, SHOCK TUNNELS

DOD/NASA/FAA Conference on Fibrous Composites in Structural

Design, Lake Tahoe, NV, 4-7 Nov. 1991

(RTOP 505-63-50-08) 26

(NASA-TP-3196; L-17031; NAS 1.60:3196) Avail: CASI HC

A03/MF A01

BUCKLING, GRAPHITE-EPOXY COMPOSITES, IMPACT METALLIC MATERIALS

DAMAGE, IMPACT TESTS, LAMINATES, LOW SPEED

Includes physical, chemical, and mechanical properties of metals.

N92-25160*# National Aeronautics and Space Administration. e.g., corrosion; and metallurgy.

Langley Research Center, Hampton, VA.

BUCKLING BEHAVIOR OF LONG SYMMETRICALLY

LAMINATED PLATES SUBJECTED TO COMBINED LOADINGS N91-13522*# National Aeronautics and Space Administration

MICHAEL P. NEMETH May 1992 31 p Presented at the Langley Research Center, Hampton, VA.

Ninth DoD/FAA Confercnce on Fibrous Composites in Structural OXIDATION CHARACTERISTICS OF TI-25AL-10NB-3V-IMO

Design, Lake Tahoe, NV, 4-7 Nov. 1991 INTERMETALLIC ALLOY

(RTOP 505-63-50-07) TERRYL A. WALLACE (National Aeronautics and Space

(NASA-TP-3195; L-17035; NAS 1.60:3195) Avail: CASI HC Administration. Langley Research Center, Hampton, VA ). RONALD

A03/MF A01 K. CLARK (National Aeronautics and Space Administration. Langley

ANISOTROPIC PLATES, BENDING, BUCKLING, LAMINATES, Research Center, Hampton, VA.), SANKARA N SANKARAN

LOADS (FORCES). STIFFNESS, STRUCTURAL ANALYSIS (Analytical Services and Materials, Inc, Hampton, VA.), and KARL

E. WIEDEMANN (Analytical Services and Materials, Inc., Hampton,

N92-32513'# National Aeronautics and Space Administration. VA.) Washington Dec. 1990 18 p

Langley Research Center, Hampton, VA. (RTOP 506-43-71-01)

EIGHTH DOD/NASA/FAA CONFERENCE ON FIBROUS (NASA-TP-3044; L-16808; NAS 1.60:3044) Avail: CASI HC

COMPOSITES IN STRUCTURAL DESIGN, PART 1 A03/MF A01

JAMES H STARNES, JR., comp., HERMAN L. BOHON, comp. ALUMINIDES, OXIDATION, REACTION KINETICS,

(Lockheed Engineering and Sciences Co., Hampton, VA.), and TEMPERATURE EFFECTS, TITANIUM ALLOYS

SHERRY B. GARZON, comp. Sep. 1990 383 p Conference

held in Norfolk, VA, 28-30 Nov. 1989 N91-17206*# National Aeronautics and Space Administration.

(RTOP 505-63-01-09) Marshall Space Flight Center, Huntsville, AL

(NASA-CP-3087-PT- 1, L-16832-PT- 1 NAS 1.55:3087-PT- 1) ELECTROCHEMICAL STUDIES OF CORROSION INHIBITORS

Avail: CASI HC A17/MF A03 M. D. DANFORD Washington Nov. 1990 21 p

/.IRCRAFT DESIGN. COMPOSITE STRUCTURES, (NASA-TP-3066; NAS 1.60:3066) Avail. CASI HC A03/MF A0l

22
27 NONMETALLIC MATERIALS

CORROSION, CORROSION PREVENTION, ELECTROCHEM- 27

ISTRY, INHIBITORS, OXYGENATION, THERMODYNAMIC

PROPERTIES NONMETALLIC MATERIALS

Includes physical, chemical, and mechanical properties of plastics,

N91-20266 # National Aeronautics and Space Administration. elastomers, lubricants, polymers, textiles, adhesives, and ceramic

Langley Research Center, Hampton, VA. materials.

SURFACE EFFECTS ON HYDROGEN PERMEATION THROUGH

TI-14AL-21NB ALLOY

SANDARA N. SANKARAN (Analytical Services and Materials, Inc., N92-17070 # National Aeronautics and Space Administration

Hampton, VA.), RONALD A. OUTLAW, and RONALD K. CLARK Lewis Research Center. Cleveland, OH.

Washington Apr. 1991 15 p HIGH-TEMPERATURE DURABILITY CONSIDERATIONS FOR

(RTOP 506-43-71-01) HSCT COMBUSTOR

(NASA-TP-3109; L-16826: NAS 1.60:3109) Avail: CASI HC NATHAN S JACOBSON Washington Jan. 1992 19 p

A03/Mr A01 (RTOP 505-63-20)

ALUMINUM ALLOYS, HYDROGEN, NIOBIUM ALLOYS, (NASA-TP-3162; E-6343; NAS 1.60:3162) Avail: CASI HC

PERMEABILITY, PERMEATING, TITANIUM ALLOYS, ULTRAHIGH A03/MF A01

VACUUM CERAMIC MATRIX COMPOSITES, COMBUSTION

CHAMBERS, HIGH TEMPERATURE TESTS, LININGS, REFRACTORY MATERIALS, THERMAL STABILITY

N91-29318 # National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, AL.

THE INTERACTION OF HYDROGEN WITH METAL ALLOYS

M. D. DANFORD and J. W. MONTANO Aug. 1991 38 p

(NASA-TP-3128; M-664; NAS 1.60:3128) Avail: CASI HC N92-22593*# National Aeronautics and Space Administration.

A03/MF A01 Goddard Space Flight Center, Greenbelt, MD.

ALLOYS, GAS-METAL INTERACTIONS, GASEOUS SHORTCOMINGS IN GROUND TESTING, ENVIRONMENT

DIFFUSION, HELIUM, HYDROGEN, HYDROGEN SIMULATIONS, AND PERFORMANCE PREDICTIONS FOR

EMBRITTLEMENT, METAL HYDRIDES SPACE APPLICATIONS

E. G. STASSINOPOULOS and G. J. BRUCKER (General Electric

Co., West Long Branch, NJ.) Apr. 1992 18 p

N91-30318"# National Aeronautics and Space Administration. (NASA-TP-3217; NAS 1.60:3217; REPT-92B00001) Avail: CASI

Lewis Research Center, Cleveland, OH. HC A03/MF A01

EQUIVALENT CRYSTAL THEORY OF ALLOYS ENVIRONMENT SIMULATION, GROUND TESTS,

GUILLERMO BOZZOLO (Analex Corp,, Fairview Park, OH.) and PERFORMANCE PREDICTION, RADIATION DAMAGE,

JOHN FERRANTE Sep. 1991 26 p SATELLITES, SINGLE EVENT UPSETS, SPACECRAFT

(RTOP 505-90-51)

(NASA-TP-3155; E-5996; NAS 1.60:3155) Avail: CASI HC

A03/MF A01

BINARY ALLOYS, COHESION, CRYSTAL DEFECTS, CRYSTAL

LATTICES, CRYSTAL STRUCTURE, ENERGY OF FORMATION,

LATTICE PARAMETERS N92-27194"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, VA.

EFFECT OF TEMPERATURE AND GAP OPENING RATE ON

THE RESILIENCY OF CANDIDATE SOLID ROCKET BOOSTER

N92-20063*# National Aeronautics and Space Administration. O-RING MATERIALS

Goddard Space Flight Center, Greenbelt, MD. CYNTHIA L. LACH Jul. 1992 14 p

LONG-TERM LIFE TESTING OF GEOSTATIONARY (RTOP 505-63-50-03)

OPERATIONAL ENVIRONMENTAL SATELLITE (GOES) (NASA-TP-3226, L-17023; NAS 1.60:3226) Avail: CASI HC ENCODER LAMPS A03/MF A01 CHARLES E. POWERS Feb. 1992 120 p DEFLECTION, ELASTOMERS, 0 RING SEALS, RESILIENCE.

(RTOP 030-09-01-01) SEALING, TEMPERATURE EFFECTS

(NASA-RP-1273; REPT-92B00013; NAS 1.61:1273) Avail: CASI

HC A06/MF A02

The aging characteristics and lifetimes of tungsten filament

encoder lamps were determined as a function of operating voltage

and filament material, For pure tungsten and thoria doped (1 pct.)

filament lamps, crystal grain growth over the center portion of the

filament leads to the ultimate failure of the lamp. The development N92-31278"# National Aeronautics and Space Administration.

of notches associated with this grain growth is the cause of lamp Marshall Space Flight Center, Huntsville, AL.

burn out. Eventually, one of the notches will 'etch' through the GIBBS FREE ENERGY OF REACTIONS INVOLVING SIC,

filament, causing it to fail open, For rhenium doped (3 pct.) filament S13N4, H2, AND H20 AS A FUNCTION OF TEMPERATURE

lamps, distortion of the filament leads to the ultimate failure of AND PRESSURE

the lamp. The lifetime of these lamps is about 1 year at an operating M. A ISHAM Aug. 1992 18 p

voltage of 5.0 volts. The pure tungsten filament lamps have the (RTOP 593-71-51)

longest average lifetime, and the thoria doped filament lamps have (NASA-TP-3275, M-694; NAS 1.60:3275) Avail: CASf HC

the shortest at 5.0 volts. The lifetimes of these lamps is about 7 A03/MF A01

years at an operating voltage of 3.5 volts. Data suggest that the CERAMIC COATINGS, GIBBS FREE ENERGY, HYDROGEN,

rhenium doped lamps will have the longest average lifetime at 35 PRESSURE DEPENDENCE. SILICON CARBIDES, SILICON

volts, and the thoria doped will have the shortest. These lifetimes NITRIDES. SURFACE REACTIONS, TEMPERATURE

are comparable to the desired lifetimes of 7 years. Author DEPENDENCE, THERMODYNAMICS, WATER

23
29 MATERIALS PROCESSING

29 N92-11218*# National Aeronautics and Space Administration

Marshall Space Flight Center, Huntsville, AL

MATERIALS PROCESSING A GENERALIZED METHOD FOR MULTIPLE ROBOTIC

MANIPULATOR PROGRAMMING APPLIED TO VERTICAL-UP

WELDING Includes space-based development of products and processes for KENNETH R. FERNANDEZ (Vanderbilt Univ Nashville, TN),

commercial applications. GEORGE E COOK (Vanderbilt Univ., Nashville, TN), KRISTINN

ANDERSEN (Vanderbilt Univ.. Nashville, TN), ROBERT JOEL

BARNETT, and SALEH ZEIN-SABATTOU (Vanderbilt Univ, N92-13340"# National Aeronautics and Space Administration. Nashville, TN,) Washington Oct. 1991 30 p

Lyndon B. Johnson Space Center, Houston, TX. (NASA-TP-3163; M-672; NAS 1.60:3163) Avail: CASt HC

ANALYSIS OF GRAVITY-INDUCED PARTICLE MOTION AND A03/MF A01

FLUID PERFUSION FLOW IN THE NASA-DESIGNED ALGORITHMS, MANIPULATORS, NUMERICAL CONTROL,

ROTATING ZERO-HEAD-SPACE TISSUE CULTURE VESSEL PLASMA ARC WELDING, ROBOT ARMS, ROBOT CONTROL.

DAVID A. WOLF and RAY P. SCHWARZ (Krug International, ROBOT DYNAMICS

Houston, TX.) Washington Oct. 1991 16 p

(RTOP 694-01-23-05) N92-13343*# National Aeronautics and Space Administration

(NASA-TP-3143; S-644; NAS 1.60:3143) Avail: CASI HC Marshall Space Flight Center, Huntsville, AL

A03/MF AO1 A NONLINEAR ESTIMATOR FOR RECONSTRUCTING THE

CULTURE TECHNIQUES, DIFFUSION, FLOW VELOCITY. ANGULAR VELOCITY OF A SPACECRAFT WITHOUT RATE

FLUID MECHANICS, GRAVITATIONAL EFFECTS, PARTICLE GYROS

MOTION, REDUCED GRAVITY, TISSUES (BIOLOGY) M E. POLITES and W. D. LIGHTSEY Washington Dec. 1991

24 p

(NASA-TP-3178; M-675; NAS 1.60:3178) Avail CASt HC

N92-30263"# National Aeronautics and Space Administration. A03/MF A01

Langley Research Center, Hampton, VA. ANGULAR VELOCITY, ATTITUDE GYROS, AXES

NATIONAL EDUCATORS' WORKSHOP: UPDATE 1991. (REFERENCE LINES), ESTIMATORS, KALMAN FILTERS,

STANDARD EXPERIMENTS IN ENGINEERING MATERIALS NONLINEAR SYSTEMS, SATELLITE ATTITUDE CONTROL

SCIENCE AND TECHNOLOGY

JAMES E. GARDNER, comp., JAMES A, JACOBS, comp. (Norfolk N92-22235"# National Aeronautics and Space Administration

State Univ., VA.), and JAMES 0. STIEGLER, comp. (Oak Ridge Marshall Space Flight Center, Huntsville, AL

National Lab., TN.) Washington Jun. 1992 369 p Workshop THE ROLE OF FAILURE/PROBLEMS IN ENGINEERING: A

held in Oak Ridge, TN, 12-14 Nov. 1991; sponsored by NASA, COMMENTARY OF FAILURES EXPERIENCED - LESSONS

DOE, Norfolk State Univ.. and NIST LEARNED

(RTOP 505-63-50-01) R. S. RYAN Mar. 1992 142 p

(NASA-CP-3151; L-17099; NAS 1.55:3151) Avail: CASI HC (NASA-TP-3213; M-684: NAS 1.60:3213) Avail: CASI HC

A16/MF A03 A07/MF A02

COMPOSITE MATERIALS, CONFERENCES, EDUCATION, FAILURE ANALYSIS, HUBBLE SPACE TELESCOPE, SATURN

EXPERIMENTATION, FRACTURE MECHANICS, METALLURGY, 5 LAUNCH VEHICLES, SPACE SHUTTLE BOOSTERS, SPACE

STRUCTURAL ANALYSIS SHUTTLE MAIN ENGINE, SPACE SHUTTLES, TOTAL QUALITY

MANAGEMENT

N92-28436"# National Aeronautics and Space Administration

Lewis Research Center, Cleveland, OH

INTERNATIONAL WORKSHOP ON VIBRATION ISOLATION

31 TECHNOLOGY FOR MICROGRAVITY SCIENCE

APPLICATIONS

JOSEPH F. LUBOMSKI. ed. May 1992 405 p Workshop held

ENGINEERING (GENERAL) in Cleveland, OH, 23-25 Apr. 1991

(RTOP 694-03-OC)

Includes vacuum technology; control engineering; display (NASA-CP-10094: E.7035; NAS 1.55:10094) Avail CASI HC

engineering; cryogenics; and fire prevention A18/MF A04

CONFERENCES, CONTROLLERS, REDUCED GRAVITY,

SPACE MANUFACTURING, SPACE SHUTTLES, SPACE STATION

N91-25303"# National Aeronautics and Space Administration. FREEDOM, VIBRATION ISOLATORS

Marshall Space Flight Center, Huntsville, AL.

METHODS OF APPLIED DYNAMICS N92-29677 # National Aeronautics and Space Administration

M. H RHEINFURTH and H. 8. WILSON (Alabama Univ., Marshall Space Flight Center, Huntsville, AL

Tuscaloosa.) Washington May 1991 210 p DEFINITION AND DESIGN OF AN EXPERIMENT TO TEST

(NASA-RP-1262; M-659, NAS 1.61:1262) Avail: CASI HC RASTER SCANNING WITH ROTATING UNBALANCED-MASS

AtO/MF A03 DEVICES ON GIMBALED PAYLOADS

The monograph was prepared to give the practicing engineer W D. LIGHTSEY, D. C. ALHORN, and M. E. POLITES Jun a clear understanding of dynamics with special consideration given 1992 19 p

to th. dynamic analysis of aerospace systems. It is conceived to (NASA-TP-3249; M-691, NAS 1.60:3249) Avail CASI HC

be both a desk-top reference and a refresher for aerospace A03/MF A01

engineers in government and ,ndustry It could also be used as a EXPERIMENT DESIGN. FEASIBILITY ANALYSIS, PAYLOADS,

supplement to standard texts for in-house training courses on the RASTER SCANNING, ROTATING BODIES, SERVOMECHANISMS

sublect Beginning with the basic concepts of kinematics and SERVOMOTORS

dynamics, the discussion proceeds to treat the dynamics of a system of particles Both classical and modern formulations of N92-30378°# National Aeronautics and Space Administration

the Lagrange equations, including constraints, are discussed and Goddard Space Flight Center, Greenbelt. MD

applied to the dynamic modeling of aerospace structures using CABLE COMPLI, NCE

the modal synthesis technique Author J KERLEY, W EKLUND (NSI Technology Services Corp.

24
34 FLUID MECHANICS AND HEAT TRANSFER

Greenbelt, MD.), R. BURKHARDT (NSI Technology Services Corp., piloted aircraft, helicopters, and geostationary satellites. This text

Greenbelt, MD.), and P. ROSSONI Jun. 1992 138 p is comprised of compiled experimental results for the expressed

(NASA-TP-3216; NAS 1.60:3216; REPT-92B00026) Avail: CASI use of communications engineers, designers of planned Land

HC A07/MF A02 Mobile Satellite Systems (LMSS), and modelers of propagation

CABLES (ROPES), HUMAN FACTORS ENGINEERING, JOINTS effects. The results presented here are mostly derived from

(JUNCTIONS), MAN MACHINE SYSTEMS, PROSTHETIC systematic studies of propagation effects for LMSS geometries in

DEVICES, ROBOT ARMS, ROBOTICS the United States associated with rural and suburban regions

Where applicable, the authors also draw liberally from the results

N92-33601"# National Aeronautics and Space Administration. of other related investigations in Canada, Europe. and Australia.

Marshall Space Flight Center. Huntsville, AL. Frequencies near 1500 MHz are emphasized to coincide with

RECONFIGURING THE RUM EXPERIMENT TO TEST frequency bands allocated for LMSS by the International

CIRCULAR SCANNING WITH ROTATING UNBALANCED-MASS Telecommunication Union, although earlier experimental work at

DEVICES ON GIMBALED PAYLOADS 870 MHz is also included. Author

M, E_ POLITES and D. C. ALHORN Sep. 1992 19 p

(NASA-TP-3282; M-696; NAS 1.60:3282) Avail' CASt HC

A03/MF A01

COMPUTERIZED SIMULATION, ROTATION, SCANNERS, 33

SCANNING, SERVOMECHANISMS, SERVOMOTORS

ELECTRONICS AND ELECTRICAL ENGINEERING

32 Includes test equipment and maintainability; components, e.g.

tunnel diodes and transistors; microminiaturization; and integrated

COMMUNICATIONS AND RADAR circuitry.

Includes radar, land and global communications; communications

theory; and optical communications. N92-11252' # National Aeronautics and Space Administration

Lewis Research Center, Cleveland, Or-.

THE 23 TO 300 C DEMAGNETIZATION RESISTANCE OF

N91-27436*# National Aeronautics and Space Administration. SAMARIUM-COBALT PERMANENT MAGNETS

Lewis Research Center, Cleveland, OH. JANIS M. NIEDRA (Sverdrup Technology, Inc., Brook Park, OH)

A THREE-DIMENSIONAL FINITE-ELEMENT and ERIC OVERTON Washington Nov. 1991 11 p

THERMAL/MECHANICAL ANALYTICAL TECHNIQUE FOR (RTOP 590-13-11)

HIGH-PERFORMANCE TRAVELING WAVE TUBES (NASA-TP-3119; E-6123; NAS 1.60:3 19) Avail: CASI HC

KAREN F. BARTOS, E. BRIAN FITE, KURT A. SHALKHAUSER, A03/MF A01

and G. RICHARD SHARP Washington Jun. 1991 17 p COBALT, DEMAGNETIZATION, PERMANENT MAGNETS.

Original contains color illustrations SAMARIUM, TEMPERATURE EFFECTS

(RTOP 650-60-20)

(NASA-TP-3081; E-5917; NAS 1.60:3081) Avail: CASI HC N92-20492# National Aeronautics and Space Administration

A03/MF A01; 5 functional color pages Marshall Space Flight Center, Huntsvlle, AL.

COMPUTER PROGRAMS, FAILURE ANALYSIS, FINITE MaRshall Space Fg C HnvlA

ELEMENT METHOD, STRUCTURAL FAILURE, THERMAL NONSTATIONARY SIGNAL VIA THE MODIFIED WIGNER

ANALYSIS, THREE DIMENSIONAL MODELS, TRAVELING WAVE DISTRIBUTION TUBES DSRBTO

T. F. ZOLADZ, J. H. JONES, and J. JONG (Wyle Labs.. Inc.,

N92-14202*# National Aeronautics and Space Administration. Huntsville, AL.) Washington Mar. 1992 35 p

Lewis Research Center, Cleveland, OH. (NASA-TP-3215; M-685; NAS 1.60:3215) Avail: CASI HC

SPACE COMMUNICATIONS TECHNOLOGY CONFERENCE: A03/MF A01

ONBOARD PROCESSING AND SWITCHING HIGH FREQUENCIES, SIGNAL ANALYSIS, SIGNAL

Washington Nov. 1991 288 p Conference held in Cleveland, PROCESSING. SPACE SHUTTLE MAIN ENGINE

OH, 12-14 Nov. 1991

(RTOP 650-60-21)

(NASA-CP-3132; E-6548; NAS 1.55:3132) Avail: CASI HC

A13/MF A03 34

COMMUNICATION NETWORKS, COMMUNICATION

SATELLITES, CONFERENCES, NETWORK CONTROL,

ONBOARD DATA PROCESSING, SATELLITE COMMUNICATION, FLUID MECHANICS AND HEAT TRANSFER

SATELLITE NETWORKS, SPACE COMMUNICATION,

SWITCHING Includes boundary layers. hydrodynamics, fluidics. mass transfer.

and ablation cooling

N92-20404"# Johns Hopkins Univ., Laurel, MD. Applied Physics

Lab

PROPAGATION EFFECTS FOR LAND MOBILE SATELLITE N91-15499'# National Aeronautics and Space Administration

SYSTEMS: OVERVIEW OF EXPERIMENTAL AND MODELING Ames Research Center, Moffett Field, CA.

RESULTS FLOW-INDUCED RESONANCE OF SCREEN-COVERED

JULIUS GOLDHIRSH and WOLFHARD J VOGEL Feb. 1992 CAVITIES

142 p Prepared in cooperation with Texas Univ, Austin PAUL T. SODERMAN Oct. 1990 48 p

(RTOP 643.10-03) (RTOP 505-61.-11)

(NASA-RP-1274; NAS 1 61 1274) Avail: CASI HC A07/MF A02 (NASA-TP-3052: A-89252, NAS 1.60:3052) Avail CASI HC

Models developed and experiments performed to characterize A03/MF A01

the propagation environment associated with land mobile ACOUSTIC EXCITATION, AEROACOUSTICS, CAVITIES.

communication using satellites are discussed Experiments were PRESSURE OSCILLATIONS, RESONANT VIBRATION, SCREENS.

carried out with transmitters on stratospheric balloons, remotely VISCOUS FLOW, VORTEX SHEDDING

25
34 FLUID MECHANICS AND HEAT TRANSFER

N91-17310"# National Aeronautics and Space Administration. MATHEMATICAL MODELS, NATIONAL AEROSPACE PLANE

Langley Research Center, Hampton, VA. PROGRAM, SKIN TEMPERATURE (NON-BIOLOGICAL),

RELATIVE EFFICIENCY AND ACCURACY OF TWO THERMAL PROTECTION

NAVIER-STOKES CODES FOR SIMULATING ATTACHED

TRANSONIC FLOW OVER WINGS N91-24542*# National Aeronautics and Space Administration.

DARYL L. BONHAUS and STEPHEN F. WORNOM Washington Lyndon B. Johnson Space Center. Houston, TX.

Feb. 1991 125 p SATURATION POINT MODEL FOR THE FORMATION OF

(RTOP 505-62-31-06) METAL NITRATE IN NITROGEN TETROXIDE OXIDIZER

(NASA-TP-3061; L-16811; NAS 1.60:3061) Avail: CASI HC PAUL R. TORRANCE Washington May 1991 19 p

A06/MF A02 (NASA-TP-3107: S-630; NAS 1.60:3107) Avail: CASI HC

COMPUTATIONAL GRIDS, FLOW DISTRIBUTION, A03/MF A01

NAVIER-STOKES EQUATION, PRESSURE DISTRIBUTION, DIFFUSION, NITRATES, NITROGEN TETROXIDE, OXIDIZERS.

TRANSONIC FLOW, WING PROFILES SATURATION (CHEMISTRY)

N91-18381"# National Aeronautics and Space Administration. N91-25352*# National Aeronautics and Space Administration

Langley Research Center, Hampton, VA. Ames Research Center, Moffett Field, CA.

AN UPWIND-BIASED SPACE MARCHING ALGORITHM FOR AEROACOUSTIC AND AERODYNAMIC APPLICATIONS OF

SUPERSONIC VISCOUS FLOW THE THEORY OF NONEQUILIBRIUM THERMODYNAMICS

FRANCIS A. GREENE Washington Mar. 1991 44 p W. CLIFTON HORNE (National Aeronautics and Space

(RTOP 506-40-91-01) Administration. Ames Research Center, Moffett Field, CA.).

(NASA-TP-3068; L-16788; NAS 1.60:3068) Avail: CASI HC CHARLES A. SMITH (National Aeronautics and Space

A03/MF A01 Administration. Ames Research Center. Moffett Field, CA.), and

ALGORITHMS, FLOW DISTRIBUTION, SPATIAL MARCHING, KRISHNAMURTY KARAMCHETI (Florida Agricultural and

SUPERSONIC FLOW, VISCOUS FLOW Mechanical Univ., Tallahassee.) Washington Jun. 1991 26 p

(RTOP 505-61-00)

N91-20418"# National Aeronautics and Space Administration. (NASA-TP-3118; A-90084; NAS 1.60:3118) Avail: CASI HC

Ames Research Center, Moffett Field, CA. A03/MF A01

HYPERVELOCITY ATMOSPHERIC FLIGHT: REAL GAS FLOW AEROACOUSTICS. AERODYNAMIC CHARACTERISTICS,

FIELDS ENERGY DISSIPATION, ENTROPY. FLOW STABILITY,

JOHN T. HOWE Nov. 1990 249 p NONEQUILIBRIUM THERMODYNAMICS, THERMODYNAMIC

(RTOP 506-40-91) EQUILIBRIUM, VISCOUS FLOW

(NASA-RP-1249; A-90143; NAS 1.61:1249) Avail: CASI HC

A11/MF A03 N92-10161"# National Aeronautics and Space Administration.

Flight in the atmosphere is examined from the viewpoint of Langley Research Center, Hampton, VA.

including real gas phenomena in the flow field about a vehicle NUMERICAL ANALYSIS AND SIMULATION OF AN ASSURED

flying at hypervelocity. That is to say, the flow field is subject not CREW RETURN VEHICLE FLOW FIELD

only to compressible phenomena, but is dominated by energetic K. JAMES WEILMUENSTER, ROBERT E. SMITH, JR., and

phenomena. There are several significant features of such a flow FRANCIS A. GREENE Washington Sep. 1991 37 p

field, Spatially, its composition can vary by both chemical and (RTOP 506-40-91-01,

elemental species. The equations which describe the flow field (NASA-TP-3101; L-16836; NAS 1.60:3101) Avail: CASI HC

include equations of state and mass, species, elemental, and A03/MF A01

electric charge continuity; momentum; and energy equations. These FLOW DISTRIBUTION, HYPERSONIC FLOW. INVISCID FLOW,

are nonlinear, coupled, partial differential equations that were LIFTING REENTRY VEHICLES, RESCUE OPERATIONS, SPACE

reduced to a relatively compact set of equations of a self-consistent STATION FREEDOM

manner (which allows mass addition at the surface at a rate

comparable to the free-stream mass flux). The equations and their N92-11285"# National Aeronautics and Space Administration.

inputs allow for transport of these quantities relative to the Langley Research Center, Hampton, VA

mass-averaged behavior of the flow field. Thus transport of mass CALCULATIONS AND CURVE FITS OF THERMODYNAMIC

by chemical, thermal, pressure, and forced diffusion; transport of AND TRANSPORT PROPERTIES FOR EQUILIBRIUM AIR TO

momentum by viscosity; and transport of energy by conduction, 30000 K

chemical considerations, viscosity, and radiative transfer are ROOP N. GUPTA (Vigyan Research Associates, Inc., Hampton,

included. The last of these complicate the set of equations by VA.), KAM-PUI LEE, RICHARD A. THOMPSON, and JERROLD

making the energy equation a partial integrodifferential equation. M. YOS (Textron Defense Systems, Wilmington, MA.)

Each phenomenon is considered and represented mathematically Washington Oct. 1991 76 p

by one or more developments. The coefficients which pertain are (RTOP 506-40-91-01)

both thermodynamically and chemically dependent. Solutions of (NASA-RP-1260; L-16907; NAS 1.61:1260) Avail: CASI HC

the equations are presented and discussed in considerable detail, A05/MF A01

with emphasis on severe energetic flow fields. For hypervelocity, A self-consistent set of equilibrium air values were computed

flight in low-density environments where gaseous reactions proceed for enthalpy, total specific heat at constant pressure, compressibility

at finite rates, chemical nonequilibrium is considered and some factor, viscosity, total thermal conductivity, and total Prandtl number

illustrations are presented. Finally, flight where the flow field may from 500 to 30,000 K over a range of 10(exp -4) atm to 10(exp

be out of equilibrium, both chemically and thermodynamically, is 2) atm. The mixture values are calculated from the transport and

presented briefly. Author thermodynamic properties of the individual species provided in a

recent study by the authors. The concentrations of the individual

N91-22509"# National Aeronautics and Space Administration. species, required in the mixture relations, are obtained from a

Langley Research Center, Hampton, VA. free energy minimization calculation procedure Present calculations

NUMERICAL STUDIES OF CONVECTIVE COOLING FOR A are based on an 1 t-species air model For pressures less than

LOCALLY HEATED SKIN 10(exp -2) atm and temperatures of about 15,000 K and greater,

STEPHEN J. SCOTTI Washington May 1991 22 p the concentrations of N( 4 4-) and O( ..- ) become important, and

(RTOP 506-43-71-04) consequently, they are included in the calculations determining

(NASA-TP-3100; L-16867; NAS 1 60:3100) Avail. CASI HC the various properties. The computed properties are curve fitted

A03/MF A01 as a function of temperature at a constant value of pressure

CONVECTIVE HEAT TRANSFER, COOLANTS, These curve fits reproduce the computed values within 5 percent

26
35 INSTRUMENTATION AND PHOTOGRAPHY

for the entire temperature range considered here at specific TRANSFER, NAVIER-STOKES EQUATION. RADIATIVE HEAT

pressures and provide an efficient means for computing the TRANSFER, REACTING FLOW, SHOCK LAYERS, STAGNATION

flowfield properties of equilibrium air, provided the elemental POINT. VISCOUS FLOW

composition remains constant at 0.24 for oxygen and 0.76 for nitrogen by mass. Author N92-32245*# National Aeronautics and Space Administration.

N92-11299# National Aeronautics and Space Administration. Goddard Space Flight Center, Greenbelt, MD_

Lewis Research Center, Cleveland, OH. TENTH WORKSHOP FOR COMPUTATIONAL FLUID DYNAMIC

MODELING OF THE HEAT TRANSFER IN BYPASS APPLICATIONS IN ROCKET PROPULSION, PART 2

TRANSITIONAL BOUNDARY-LAYER FLOWS R. W. WILLIAMS, comp Washington Jul. 1992 755 p

FREDERICK F. SIMON and CRAIG A. STEPHENS (PRC Kentron. Workshop held in Huntsville, AL, 28-30 Apr. 1992

Inc.,EdwardFs, Washingto CAA.) .STE9HES (5 K n (NASA-CP-3163-PT-2; M-693-PT-2: NAS 1.55:3163-PT-2) Avail:

Inc., Edwards, CA.) Washington Oct. 1991 15 p CASI HC A99/MF A05

(RTOP 505-62-52) COMPUTATIONAL FLUID DYNAMICS, CONFERENCES,

(NASA-TP-3170; E-6046; NAS 1.60:3170) Avail: CASl HC HYDROGEN OXYGEN ENGINES, LIQUID PROPELLANT ROCKET AO3/MF A~t ENGINES, PROPULSION SYSTEM CONFIGURATIONS, ROCKET

BOUNDARY LAYER FLOW, BOUNDARY LAYER TRANSITION, ENGINE DESIGN. SOLID PROPELLANT ROCKET ENGINES,

BYPASSES. COMPUTERIZED SIMULATION, HEAT TRANSFER, SPACE SHUTTLE MAIN ENGINE, SPACECRAFT PROPULSION

K-EPSILON TURBULENCE MODEL, LEADING EDGES,

PREDICTION ANALYSIS TECHNIQUES, TRANSITION FLOW

N92-32278'# National Aeronautics and Space Administration.

N92-20677*# National Aeronautics and Space Administration. Goddard Space Flight Center, Greenbelt, MD.

Langley Research Center, Hampton, VA. TENTH WORKSHOP FOR COMPUTATIONAL FLUID DYNAMIC

SIMULATION OF REAL-GAS EFFECTS ON PRESSURE APPLICATIONS IN ROCKET PROPULSION. PART 1

DISTRIBUTIONS FOR AEROASSIST FLIGHT EXPERIMENT R. W. WILLIAMS, comp. Washington Jul. 1992 721 p

VEHICLE AND COMPARISON WITH PREDICTION Workshop held in Huntsville, AL, 28-30 Apr. 1992

JOHN R. MICOL Apr. 1992 70 p (NASA-CP-3163-PT-1; M-693-PT-1; NAS 1.55:3163-PT-1) Avail.

(RTOP 506-40-41-01) CASI HC A99/MF A05

(NASA-TP-3157; L-16923; NAS 1.60:3157) Avail: CASI HC COMPUTATIONAL FLUID DYNAMICS, CONFERENCES, GRID

A04/MF A01 GENERATION (MArHEMATICS), HEAT TRANSFER, LIQUID

AEROASSIST, BASE PRESSURE, BLUNT BODIES, DENSITY PROPELLANT ROCKET ENGINES, PROPELLANT COMBUSTION,

DISTRIBUTION, FOREBODIES, HYPERSONIC SPEED, ORBIT SOLID PROPELLANT ROCKET ENGINES, SPACECRAFT

TRANSFER VEHICLES, PRESSURE DISTRIBUTION, REAL PROPULSION, TURBOMACHINERY

GASES, SIMULATION

N92-24514"# National Aeronautics and Space Administration.

Lewis Research Center. Cleveland. OH.

WORKSHOP ON ENGINEERING TURBULENCE MODELING 35

LOUIS A. POVINELLI, ed., W. W. LIOU, ed., A. SHABBIR, ed.,

and T.-H. SHIH, ed. Mar. 1992 510 p Workshop held in INSTRUMENTATION AND PHOTOGRAPHY

Cleveland, OH, 21-22 Aug. 1991

(NASA ORDER C-99066-G; RTOP 505-62-21)

(NASA-CP-10088; E-6830; ICOMP-92-02; CMOTT-92-02; NAS Includes remote sensorsd measuring instruments and gages,

1.55:10088) Avail: CASI HC A22/MF A04 detectors; cameras and photographic supplies; and holography.

COMPUTATIONAL FLUID DYNAMICS, CONFERENCES,

PROPULSION, TURBULENCE, TURBULENCE MODELS N91-14574*# National Aeronautics and Space Administration.

Lewis Research Center, Cleveland, OH.

N92-24797*# National Aeronautics and Space Administration. HIGH RESOLUTION, HIGH FRAME RATE VIDEO

Langley Research Center, Hampton, VA. TECHNOLOGY

A SIMPLIFIED METHOD FOR THERMAL ANALYSIS OF A Washington May 1990 102 p Workshop held in Cleveland.

COWL LEADING EDGE SUBJECT TO INTENSE LOCAL OH, 11-12 May 1988 List of attendees included as supplement

SHOCK-WAVE-INTERFERENCE HEATING (ATOP 694-03-03)

DAVID M. MCGOWAN, CHARLES J. CAMARDA, and STEPHEN (NASA-CP-3080; E-5044; NAS 1.55:3080) Avail: CASI HC

J SCOTTI Washington Mar. 1992 40 p A06/MF A02

(RTOP 506-43-31-04) DATA COMPRESSION, DATA TRANSMISSION, FRAMES

(NASA-TP-3167; L-16505; NAS 1.60:3167) Avail: CASI HC (DATA PROCESSING), HIGH RESOLUTION, IMAGE

A03/MF A01 PROCESSING, IMAGING TECHNIQUES. VIDEO DATA

AERODYNAMIC HEATING, AERODYNAMIC INTERFERENCE,

COWLINGS, HEAT AFFECTED ZONE, LEADING EDGES, SHOCK

WAVES, THERMAL ANALYSIS N91-22538"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, VA.

N92-31281*# National Aeronautics and Space Administration. LOW-ENERGY POSITRON FLUX GENERATOR FOR

Langley Research Center, Hampton, VA. MICROSTRUCTURAL CHARACTERIZATION OF THIN FILMS

STAGNATION-POINT HEAT-TRANSFER RATE PREDICTIONS JAG J. SINGH (National Aeronautics and Space Administration.

AT AEROASSIST FLIGHT CONDITIONS Langley Research Center, Hampton, VA.), ABE EFTEKHARI

ROOP N. GUPTA, JIM J. JONES (Analytical Mechanics Associates, (Analytical Services and Materials, Inc., Hampton, VA.), and TERRY

Inc., Hampton. VA.), and WILLIAM C. ROCHELLE (Lockheed L. ST.CLAIR Washington May 1991 19 p

Engineering and Sciences Co., Houston, TX.) Sep 1992 21 p (RTOP 506-43-21-05)

(RTOP 506-40-91-02) (NASA-TP-3074; L-16881; NAS 1.60:3074) Avail: CASI HC

(NASA-TP-3208; L-17039; NAS 1.60:3208) Avail: CASI HC A03/MF A01

A03/MF A01 FILM THICKNESS. INSULATORS, MICROSTRUCTURE,

AEROASSIST, COMPUTATIONAL FLUID DYNAMICS, FLIGHT POSITRON ANNIHILATION, SPECTROSCOPY, THIN FILMS,

CONDITIONS, HYPERSONIC FLOW, HYPERSONIC HEAT TUNGSTEN

27
35 INSTRUMENTATION AND PHOTOGRAPHY

N92-29228*# National Aeronautics and Space Administration, situations Some guidance on applying these fundamentals to the

Langley Research Center, Hampton, VA. solution of engineering problems is also provided Author

SIXTEENTH INTERNATIONAL LASER RADAR CONFERENCE,

PART I N91-30540'# National Aeronautics and Space Administration

M PATRICK MCCORMICK, ed. Washington Jul. 1992 407 p Goddard Space Flight Center. Greenbelt. MD.

Conference held in Cambridge, MA, 20-24 Jul. 1992 sponsored THE EFFECT OF BANDWIDTH ON TELEROBOT SYSTEM

by NASA. Langley Research Center, AFOSR, AF Phillips Lab., PERFORMANCE

American Meteorological Society, and the Optical Society of MARK UEBEL (Maryland Univ., College Park) MICHAEL S ALl

America (National Aeronautics and Space Administration. Goddard Space

(RTOP 665-45-20-21) Flight Cent-', Greenbelt, MD.), and IOANNIS MINIS (Maryland

(NASA-CP-3158-PT-1; L-17126-PT-1: NAS 1.55:3158-PT-1) Uiv., College Park.) Sep. 1991 44 p

Avail: CASI HC A18/MF '04 (NASA-TP-3152; REPT-91E02561, NAS 1 60:3152) Avail: CASI

ATMOSPHERIC CIRCULATION, ATMOSPHERIC, EFFECTS, HC A03/MF A01

BACKSCATTERING, CLIMATE CHANGE, IMAGING BANDWIDTH, FEEDBACK CONTROL, ROL, T CONTROL,

TECHNIQUES, OPTICAL RADAR, RADAR MEASUREMENT, TELEROBOTICS

REMOTE SENSING, RESEARCH FACILITIES, STRATOSPHERE,

VOLCANOES N92-10195"# National Aeronautics and Space Administration

Lewis Research Center, Cleveland, OH.

N92-31013"# National Aeronautics and Space Administration. A METHOD FOR DETERMINING SPIRAL-BEVEL GEAR TOOTH

Langley Research Center, Hampton, VA. GEOMETRY FOR FINITE ELEMENT ANALYSIS

SIXTEENTH INTERNATIONAL LASER RADAR CONFERENCE, ROBERT F. HANDSCHUH and FAYDOR L. LITVIN (Illinois Univ.

PART 2 Chicago.) Aug. 1991 16 p Original contains color illustrations

M. PATRICK MCCORMICK. ed. Washington Jul. 1992 361 p (DA PROJ. 1L1-62211-A-47-A; RTOP 505-63-51)

Conterence held in Cambridge, MA, 20-24 Jul. 1992; sponsored (NASA-TP-3096; E-5837; NAS 1.60:3096; AVSCOM-TR-91-C-020.

by NASA. Langley Research Center, AFOSR, AF Phillips Lab., AD-A242332) Avail: CASI HC A03/MF A01; 1 functional color

American Meteorological Society, and the Optical Society of page

America APPLICATIONS PROGRAMS (COMPUTERS), COMPUTER

(RTOP 665-45-20-21) AIDED DESIGN. FINITE ELEMENT METHOD, GEaR TEETH,

(NASA-CP-3158-PT-2; L 17126-PT-2; NAS 1.55:3158-PT-2) MATHEMATICAL MODELS, SURFACE GEOMETRY, THREE

Avail: CASI HC A16/MF A03 DIMENSIONAL MODELS

CONFERENCES, DOPPLER RADAR, IMAGING TECHNIQUES,

LASERS, MESOSPHERE, OPTICAL RADAR, OZONE, REMOTE N92-14346'# National Aeronautics and Space Administration

SENSING, TROPOSPHERE Lewis Research Center, Cleveland, OH.

ROTORDYNAMIC INSTABILITY PROBLEMS IN

HIGH-PERFORMANCE TURBOMACHINERY, 1990

Washington Oct. 1991 458 p Workshop held in College

37 Station, TX, 21-23 May 1990; sponsored by Texas A and M Univ.

and NASA. Lewis Research Center

(RTOP 553-13-00)

MECHANICAL ENGINEERING (NASA-CP-3122; E-5628, NAS 1.55:3122) Avail: CASI HC

A20/MF A04

Includes auxiliary systems (nonpower); machine elements an,,. CONFERENCES, ROTOR DYNAMICS, STRUCTURAL

processes; and mechanical equipment. VIBRATION. TURBOMACHINERY. VIBRATION DAMPING

N92-30396*# National Aeronautics and Space Administration

N91-129S6*# National Aeronautics and Space Administration. Lewis Research Center, Cleveland, OH.

Lewis Research Center, Cleveland, OH. DEVE'.OPMENT OF A FULL-SCALE TRANSMISSION TESTING

EXPERIMENTAL AND ANALYTICAL EVALUATION OF PROCEDURE TO EVALUATE ADVANCED LUBRICANTS

EFFICIENCY OF HELICOPTER PLANETARY STAGE DAVID G. LEWICKI, HARRY J. DECKER. and JOHN T. SHIMSKI

TIMOTHY L. KRANTZ Nov. 1990 20 p Prepared in cooperation (Naval Air Propulsion Test Center, Trenton, NJ.) Aug 1992

with Army Aviation Systems Command, Cleveland, OH 25 p

(DA PROJ. IL1-6221147-A; RTOP 505-63-51) (DA PROJ. 1L 1.62211 -A-47-A; RTOP 505.63-36)

(NASA-TP-3063; E-5268; NAS 1.60:3063; AVSCOM-TR-90-C-0011 (NASA-TP-3265; E-6531; NA ,i 1.60:1265; AVSCOM-TR-9 t-C-026)

Avail: CASI HC A03/MF A01 Avail: CASI HC A03/MF A01

HELICOPTER PROPELLER DRIVE, HELICOPTERS, POWER GEARS, HELICOPTER PROPELLER DRIVE, LUBRICANT

LOSS, SYSTEM EFFECTIVENESS, TRANSMISSIONS (MACHINE TESTS, LUBRICATING OILS. LUBRICATION, ROTARY WINGS,

ELEMENTS) TEST ST,,.NDS, TRANSMISSIONS (MACHINE ELEMENTS). WEAR

TESTS

N91-30531"# Ohio State Univ., Columbus. Dept. of Mechanical

Engineering.

FUNDAMENTALS OF FLUID LUBRICATION 38

BERNARD J. HAMROCK Washington NASA Aug. 1991

670 p Sponsored by NASA. Lewi. Research Center

(RTOP 505-90-21) QUALITY ASSURANCE AND RELIABILITY

(NASA-RP-1255; E-3758; NAS 1.61:1255) Avail: CASI HC

A99/MF A06 Includes product sampling procedures 'nd techniques; and quality

The aim is to coordinate the topics of design, engin(ring control.

dynamics, and fluid dynamics in order to aid researchers in the

area of fluid film lubrication, The lubrication principles that are

coveied can serve as a basis tor the engineering design of machine N91-14618* # National Aeronautics and Space Administration.

elements. The fundamentals of fluid film lubrication are presented Langley Research Center Hampton, VA

clearly so that students that use the book will have confidence in AXISYMMETRIC SHELL ANALYSIS OF THE SPACE SHUTTLE

their ability to apply these principles to a wide range of lubrication SOLID ROCKET BOOSTER FIELD JOINT

28
39 STRUCTURAL MECHANICS

MICHAEL r. NEMETH (National Aeronautics and Space N91-13751 '# National Aeronautics and Space Administration

Administration. Langley Research Center, Hampton, VA.) and Langley Research Center, Hampton, VA

MELVIN S. ANDERSON (Old Dominion Univ., Norfolk, VA.) FAILURE BEHAVIOR OF GENERIC METALLIC AND

Washington Jan. 1991 5F p COMPOSITE AIRCRAFT STRUCTURAL COMPONENTS UNDER

(RTOP 505-63-01-08) CRASH LOADS

(NASA-TP-3033: L-16746; NAS 1.60:3033) Avail: CASI HC HUEY D. CARDEN and MARTHA P. ROBINSON Washington

A04IMF A01 "ov. 1990 48 p

DYNAMIC STRUCTURAL ANALYSIS, JOINTS (JUNCTIONS), (RTOP 505-63-01-11)

0 RING SEALS, SOLID PROPELLANT ROCKET ENGINES, SPACE (NASA-RP-1239; L-16744; NAS 1.61:1239) Avai: CASI HC

SHUTTLE BOOSTERS A03/MF A01

Failure behavior results are presented from crash dynamics

research using concepts of aircraft elements and substructure not

necessarily designed or optimized for energy absorption or crash

loading considerations. To achieve desired new designs

incorporating improved energy absorption capabilities often requires

39 an understanding of how more conventional designs behave under

crash loadings. Experimental and analytical data are presented STRUCTURAL MECHANICS which indicate some general trends in the failure behavior of a class of composite structures including individual fuselage frames,

skeleton subfloors with stringers and floor beams without skin

Includes structural element design and weight analysis; fatigue; covering, and subfloors with skin added to the frame-stringer

and thermal stress. arrangement. Although the behavior is complex, a strong similarity

in the static/dynamic failure behavior among these structures is

illustrated through photographs of the experimental results and

N91-10301"# National Aeronautics and Space Administration. through analytical data of generic composite structural models

Langley Research Center, Hampton, VA. Author

RESEARCH IN STRUCTURES, STRUCTURAL DYNAMICS AND

MATERIALS, 1990 N91-16413"# National Aeronautics and Space Administration.

JEAN-FRANCOIS M. BARTHELEMY, comp. and AHMED K. NOOR, Marshall Space Flight Center. Huntsville, AL.

comp. (George Washington Univ., Hampton, VA.) Washington PLATE AND BUTT-WELD STRESSES BEYOND ELASTIC

Mar. 1990 283 p The 31st conference was held in Long LIMIT, MATERIAL AND STRUCTURAL MODELING

Beach, CA, 2-4 Apr. 1990; sponsored by AIAA, ASME, ASCE, V. VERDERAIME Washington Jan. 1991 63 p

AHS, and ASC (NASA-TP-3075; M-654; NAS 1.60:3075) Avail: CASI HC

(RTOP 505-63-01-07) A04/MF AO0

(NASA-CP-3064: L-16735; NAS 1.55:3064) Avail: CASI HC AXIAL LOADS, BENDING, SAFETY FACTORS, STRESS

A13/MF A03 ANALYSIS, STRESS-STRAIN RELATIONSHIPS. STRUCTURAL

BEAMS (SUPPORTS), BUCKLINC, COMPOSITE ANALYSIS, WELDED JOINTS

STRUCTURES, CONFERENCES, CONTROL SYSTEMS DESIGN,

DYNAMIC RESPONSE, DYNAMIC STRUCTURAL ANALYSIS, N91-2n503*# National Aeronautics and Space Administration.

LOADS (FORCES) Langley Research Center, Hampton, VA.

BUCKLING AND VIBRATION ANALYSIS OF A SIMPLY

SUPPORTED COLUMN WITH A PIECEWISE CONSTANT

N91-10328*# National Aeronautics and Space Administration. CROSS SECTION

Hugh L. Dryden Flight Research Facility, Edwards, CA. MARK S. LAKE and MARTIN M. MIKULAS, JR, Washington

DESIGN OF CONTROL LAWS FOR FLUTTER SUPPRESSION Mar. 1991 13 p

BASED ON THE AERODYNAMIC ENERGY CONCEPT AND (RTOP 506-43-41-02)

COMPARISONS WITH OTHER DESIGN METHODS (NASA-TP-3090; L-16854: NAS 1.60:3090) Avail: CASI HC

ELI NISSIM (Technion - Israel Inst. of Tech., Haifa.) Oct 1990 A03/MF A01

59 p Previously anounced in IAA as A89-31 100 BUCKLING. COLUMNS (SUPPORTS), DYNAMIC

(RTOP 505-66-71) STRUCTURAL ANALYSIS, STRUCTURAL STABILITY,

(NASA-TP-3056; H-1549; NAS 1.60 3056, AIAA PAPER 89-1212) STRUCTURAL VIBRATION. TAPERING

Avail CASI HC A04/MF A01

AEROELASTIC RESEARCH W1rGS, CONTROL SYSTEMS N91-20506"# Computer Software Management and Information

DESIGN, CONTROL THEORY, ENERGY METHODS, FLUTTER Center, Athens, GA.

ANALYSIS, VIBRATION DAMPING NINETEENTH NASTRAN (R) USERS' COLLOQUIUM

Washington NASA Apr. 1991 194 p Colloquium held ir

Williamsburg, VA, 22-26 Apr. 1991 Sponsoreo by NASA,

N91-I3750°# National Aeronautics and Space Administration. Washington

Langley Research Center, Hampton, VA. (NASA-CP.3111; NAS 1.55:3111) Avail: CASI HC A09/MF A03

FREE VIBRATIONS OF THIN-WALLED SEMICIRCULAR CONFERENCES, FINITE ELEMENT METHOD, NASTRAN,

GRAPHITE-EPOXY COMPOSITE FRAMES STRUCTURAL ANALYSIS

AHMED K NOOR (National Aero autics and Spa,;e Administration.

Langley Research Center, Hampton, VA.), HUEY 0. CARDEN N91-21556"# National Aeronautics and Space Administration

(National Aeronautics and Space Administration. Langley Research Langley Research Center, Hampton, VA.

Center, Hampton, VA.), and JEANNE M. PETERS (Joint Inst. for DETERMINATION OF THE FLIGHT HARDWARE

Advancement of Flight Sciences. Hampton, VA.) Washington CONFIGURATION OF AN ENERGY ABSORBING

Nov 1r.90 43 p Original contains color illustrations ATTENUATOR FOR THE PROPOSED SPACE STATIflN CREW

(NAG1-730; RTOP 505-63-01-11) AND EQUIPMENT TRANSLATION AID CART

(NASA-TP-3010; L-16726: NAS 1.60:3010) Avail: CASI HC EDWIN L. FASANELLA (Lockheed Engineeiing and Sciences Co,

A03/MF A01; 4 functional color pages Hampton, VA), KAREN E. A KSON 'Army Aviation Research

COMPOSITE STRUCTURES, FRAMES, GRAPHITE-EPOXY and Development Command, Hampton, VA.), LISA E. JONES

COMPOSITES, LAMINATES, STRUCTURAL ANALYSIS, (National Aeronautics and Space Administration. Langley Research

STRUCTURAL VIBRATION, VIBRATION EFFECTS Center, Hampton. VA.), and JOHN E, TETER, JR. 1991 58 p

29
39 STRUCTURAL MECHANICS

(RTOP 505-63-01-11) C(2!.STRAtNTS, COUPLED MODES, DYNAMIC STRUCTURAL

(NASA-TP-3084. L-16852: NAS 160 3084; AD-A235901) Avail. ANALYSIS, LOADS (FORCES). MODAl RESPONSE STEADY

CASI HC A04/MF A01 STATE, TRUNCATION ERRORS

ATTENUATORS, BRAKES (FOR ARRESTING MOTION),

CARTS, COLUMNS (SUPPORTS). HONEYCOMB STRUCTURES, N92-22227*# National Aeronautics and Space Administration

RAIL TrPANSPORTATION, SHOCK ABSORBERS. SPACE Lewis Research Center. Cleveland, OH

STATIONS IMPROVED ACCURACY FOR FINITE ELEMENT STRUCTURAL

ANALYSIS VIA A NEW INTEGRATED FORCE METHOD

N91-22576"# National Aeronautics and Space Administration. SURYA N. PATNAIK (Ohio Aerospace Inst, Brook Park), DALE

Langley Research Center, Hampton, VA A. HOPKINS. ROBERT A AIELLO. and LASZLO BERKE Apr

COMPUTATIONAL METHODS FOR FRICTIONLESS CONTACT 1992 28 p WITH APPLICATION TO SPACE SHUTTLE ORBITER (RTOP 505-63-5B) NOSE-GEAR TIRES (NASA.TP-3204; E-5638. NAS 1 60:3204) Avail. CASt HC

KYUN 0. KIM (George Wasington Univ., Hampton, VA.), JOHN A03/MF A01

A. TANNER (National Aeronautics and Space Administration COMPUTER PROGRAMS. FINITE ELEMENT METHOD,

Langley Research Center, Hampton, VA.), AHMED K. NOOR MATHEMATICAL MODELS, MEASURE AND INTEGRATION,

(Virginia Univ. Charlottesville,). and MARTHA P. ROBINSON SOLID MECHANICS, STRESS-STRAIN RELATIONSHIPS

Wasnington May 1991 36 p Original contains color STRUCTURAL ANALYSIS

illustrations N92-23115"# National Aeronautics and Space Administration

(RTOP 505-63-41-02) Langley Research Center, Hampton, VA (NASA-TP-3073; L-16750; HAS 11.60ý307' Avail: CASI HC EXPERIMENTAL BEHAVIOR OF GRAPHITE-EPOXY

A03/MF A01; 2 functional color pages Y-STIFFENED SPECIMENS LOADED IN COMPRESSION

AIRCRAFT TIRES, COMPUTATION, FINITE ELEMENT P. DANIEL SYDOW and MARK J SHUART May 1992 20 p

METHOD, FRICTIONLESS ENVIRONMENTS, LANDING GEAR, (RTOP 505-63.50-08)

ROCKET NOSE CONES, ROLLING CONTACT LOADS, SPACE (NASARTP-3171; L.16918; NAS 160:3171) Avail CAS HC

SHUTTLE ORBITERS. VARIATIONAL PRINCIPLES A03/MF A01

COMPRESSION TESTS, GRAPHITE-EPOXY COMPOSITES,

N91-24603"# Jet Propulsion Lab., California Inst, of Tech., REINFORCED PLATES, STIFFENING. WEBS (SUPPORTS)

Pasadena.

THE 25TH AEROSPACE MECHANISMS SYMPOSIUM N92-24205"# National Aeronautics and Space Administration

May 1991 346 p Symposium held in Pasadena, CA, 8-10 May Langley Research Center. Hampton, VA

1991; sponsored by NASA, Washington, California Inst. of Tech., THERMAL AND STRUCTURAL TESTS OF RENE 41

and LMSC HONEYCOMB INTEGRAL-TANK CONCEPT FOR FUTURE

(NAS7-918) SPACE TRANSPORTATION SYSTEMS

(NASA-CP.3113; NAS 1.55:3113) Avail: CASI HC A15/MF A03 JOHN L. SHIDELER, ROGER A. FIELDS, LAWRENCE F

ACTUATORS. AEROSPAC- ENGINEERING, CONFERENCES, REARDON, and LESLIE GONG (National Aeronautics and Space

CRYOGENICS, GROUND SUPPORT EQUIPMENT, LATCHES, Administration. Hugh L. Dryden Flight Research Facility. Edwards,

ROBOTICS, TRIBOLOGY, VACUUM CA.) May 1992 77 p

(RTOP 506-43-71-05)

N92-186053# National Aeronautics and Space Administration. (NASA-TP-3145; L-16752; NAS 1.60:3145) Avail CASt HC

Langley Research Center. Hampton. VA. A05/MF A01

EFFECT OF CRASH PULSE SHAPE ON SEAT STROKE HIGH TEMPERATURE TESTS, HONEYCOMB STRUCTURES,

REQUIREMENTS FOR LIMITING LOADS ON OCCUPANTS OF RENE 41, SANDWICH STRUCTURES. STRAIN MEASUREMENT.

AIRCRAFT STRESS ANALYSIS. THERMAL ANALYSIS

HUEY 0. CARDEN Washington Feb. 1992 23 p

(RTOP 505-63-50-09) N92-24324*# Computer Software Management and Information

(NASA-TP-3126; L-16941; NAS 1.60:3126) Avail: CASI HC Center, Athens, GA.

A03/MF A01 TWENTIETH NASTRAN (R) USERS' COLLOQUIUM

CRASHES, CRASHWORTHINESS. DYNAMIC TESTS, Washington NASA Apr. 1992 186 p Colloquium held in

GENERAL AVIATION AIRCRAFT, LOADS (FORCES), SEATS, Colorado Springs, CO, 27 Apr. - 1 May 1992 Sponsored by

SHAPES NASA, Washington

(NASA.CP-3145; NAS 1.55:3145) Avail: CASI HC A09/MF A02

FINITE ELEMENT METHOD. NASTRAN, STRUCTURAL

N92-19355*# National Aeronautics and Space Administration. ANALYSIN

Marshall Space Flight Center, Huntsville, AL.

STRUCTURAL DETERMINISTIC SAFETY FACTORS N92-24546"# National Aeronautics and Space Administration

SELECTION CRITERIA AND VERIFICATION Langley Research Canter, Hampton. VA.

V. VERDERAIME Feb. 1202 50 p STIFFNESS AND STRENGTH TAILORING IN UNIFORM

(NASA-TP.3203, M-683; NAS 1.60:3203) Avail: CASI HC SPACE-FILLING TRUSS STRUCTURES

A03/MF A01 MARK S. LAKE Apr. 1992 30 p Presented at the Ninth

METALS. PROBABILITY THEORY, RELIABILITY ANALYSIS, DOD/NASA/FAA Conference on Fibrous Composites in Structural

SAFETY FACTORS, STANDARD DEVIATION, STRESS Design, Lake Tahoe, NV, 4-7 Nov. 1991

ANALYSIS, STRUCTURAL FAILURE. STRUCTURAL (RTOP 506-43-41-02)

RELIABILITY (NASA-TP-3210: L-17001; NAS 1 60:3210) Avail: CASI HC

A03/MF A01

N92-21457"# National Aeronautics and Space Administration. CRYSTALLOGRAPHY. LOADS (FORCES), SPACECRAFT

Ma;shall 3pacc Flight Center, Huntsville, AL. STRUCTURES, STIFFNESS, STRUCTURAL DESIGN,

THE EFFECT OF ACCELERATION VERSUS DISPLACEMENT STRUCTURAL DESIGN CRITERIA, TRUSSES

METHODS ON STEADY-STATE BOUNDARY FORCES

0 S. MCGHEE Washington NASA, Marshall Space Flight N92-25067*# National Aeronautics and Space Administration

Center Apr. 1992 31 p Goddard Space Flight Center, Greenbelt, MD.

(NASA-TP-3218; M-686; NAS 1.60:3218) Avail: CASI HC THE 26TH AEROSPACE MECHANISMS SYMPOSIUM

A03/MF A01 Washington May 1992 386 p Symposium held in Greenbelt.

30
39 STRUCTURAL MECHANICS

MD, 13-15 May 1992; sponsored by NASA. Washington, California (NASA-TP-3214; S-763: NAS 1.60:3214) Avail CA';l HC

Inst. of Tech, and LMSC A03/MF A01

(NASA-CP-3147; REPT-92B00052; NAS 155:3147) Avail: CASI FASTENERS, LARGE SPACE STRUCTURES. ORBITAL

HC A17/MF A04 ASSEMBLY, ROBOTS, SPACE COMMERCIALIZATION, SPACE

ACTUATORS, AEROSPACE ENGINEERING, CONFERENCES, ERECTABLE STRUCTURES, TRUSSES

CONNECTORS, LARGE SPACE STRUCTURES, LATCHES

N92-28620"# National Aeronautics and Space Admir. 'ration

N92-25911"# National Aeronautics and Space Administration. Goddard Space Flight Center, Greenbelt, MD

Langley Research Center, Hampton, VA. TYPES AND CHARACTERISTICS OF DATA FOR

COMPUTATIONAL STRUCTURES TECHNOLOGY FOR GEOMAGNETIC FIELD MODELING

AIRFRAMES AND PROPULSION SYSTEMS R. A. LANGEL, ed. ana H. T. BALDWIN, ed (Hughes STX. Irnc.,

AHMED K. NOOR, comp. (Virginia Univ., Hampton.), JERROLD Lanham, MD.) Washington Jun. 1992 353 p Symposium

M. HOUSNER, comp., JAMES H. STARNES, JR., comp., DALE held in Vienna. Austria, 23 Aug. 1991

A. HOPKINS, comp., and CHRISTOS C. CHAMIS, comp. (National (NASA-CP-3153; REPT-92BO0061; NAS 1.55:3153) Avail: CASI

Aeronautics and Space Administration. Lewis Research Center, HC A16/MF A03

Cleveland, OH.) Washington May 1992 516 p Workshops CONFERENCES, DATA REDUCTION, GEODESY,

held in Cleveland, OH, 26-27 Jun. 1991 and in Hampton, VA, 4-5 GEOMAGNETISM, GEOPHYSICS

Sep. 1991; sponsored by NASA, Washington and Virginia Univ., Hampton (RTOP 505-63-53-01) N92-30106"# National Aeronautics and Space Administration

(NASA-CP-3142; L-17049; NAS 1.55:3142) Avail: CASI HC Langley Research Center, Hampton, VA.

A22/MF A04 THE 1991 INTERNATIONAL CONFERENCE ON AGING

AIRCRAFT DESIGN, AIRCRAFT STRUCTURES, AIRFRAMES, AIRCRAFT AND STRUCTURAL AIRWORTHINESS

CIVIL AVIATION, COMPUTER AIDED DESIGN, CONFERENCES, CHARLES E. HARRIS, ed. Washington Jul. 1992 470 p

PROPULSION SYSTEM CONFIGURATIONS, SPACECRAFT Conference held in Washington, DC, 19-21 Nov. 1991; sponsored

DESIGN. SPACECRAFT STRUCTURES, STRUCTURAL by NASA, Washington and FAA

ANALYSIS, STRUCTURAL DESIGN, SUPERSONIC (RTOP 538-02-10-01)

TRANSPORTS (NASA-CP-3160; L-17094; NAS 1.55:3160) Avail: CASI HC

A20/Mý- A04

AGING (MATERIALS), AIRCRAFT INDUSTRY, AIRCRAFT

N92-25997"# National Aeronautics and Space Administration. MAINTENANCE, AIRCRAFT PERFORMANCE, AIRCRAFT

Langley Research Center, Hampton, VA. RELIABILITY, AIRCRAFT STRUCTURES, CONFERENCES,

STRESS CONCENTRATIONS FOR STRAIGHT-SHANK AND NONDESTRUCTIVE TESTS

COUNTERSUNK HOLES IN PLATES SUBJECTED TO

TENSION, BENDING, AND PIN LOADING

K. N. SHIVAKUMAR (Analytical Services and Materials, Inc., N92-31279"# National Aeronautics and Space Administration.

Hampton, VA.) and J. C. NEWMAN, JR. Jun. 1992 36 p Langley Research Center, Hampton, VA.

(RTOP 505-63-50-04) ANALYSIS AND PREDICTION OF MULTIPLE-SITE DAMAGE

(NASA-TP-3192; L-17027; NAS 1.60:3192) Avail: CASI HC (MSD) FATIGUE CRACK GROWTH

A03/MF A01 D. S. DAWICKE (Analytical Mechanics Associa- Inc., Hampton,

BEND TESTS, FINITE ELEMENT METHOD, HOLES VA.) and J. C. NEWMAN, JR. Aug. 1992 18

(MECHANICS), STRESS CONCENTRATION, TENSILE TESTS, (RTOP 505-63-50-04)

THREE DIMENSIONAL MODELS (NASA-TP-3231; L-17006; NAS 1.60:3231) Avail: CASI HC

A03/MF A01

N92-26537"# National Aeronautics and Space Administration. CRACKING BOUNDARY (FRACTURING). ELEMENT METHOD, DAMAGE. CRACK FATIGUE PROPAGATION, (MATERIALS),

Langley Research Center, Hampton, VA. CRACKING FACT ORS

IDENTIFICATION OF LINEAR SYSTEMS BY AN STRESS INTENSITY FACTORS

ASYMPTOTICALLY STABLE OBSERVER

MINH 0. PHAN, LUCAS G. HORTA, JER-NAN JUANG, and N92-31280"# National Aeronautics and Space Administration,

RICHARD W. LONGMAN (Columbia Univ., New York, NY.) Jun. Marshall Space Flight Center, Huntsville, AL_

1992 69 p APPLICATIONS OF FEM AND BEM IN TWO-DIMENSIONAL

(RTOP 590-14-61-01) FRACTURE MECHANICS PROBLEMS

(NASA-TP-3164; L-16940; NAS 1.60:3164) Avail: CASI HC J. B. MIN, B. E. STEEVE, and G. A. SWANSON Aug 1992

A04/MF A01 23 p

EIGENVALUES, LINEAR SYSTEMS, MARKOV PROCESSES, (NASA-TP-3277; M-695; NAS 1.60:3277) Avail: CASI HC

NUMERICAL STABILITY, SYSTEM IDENTIFICATION A03/MF A01

BOUNDARIES, BOUNDARY ELEMENT METHOD, CRACK

N92-26669 # National Aeronautics and Space Administration. TIPS, ELASTIC PLATES, FINITE ELEMENT METHOD, FRACTURE

Marshall Space Flight Center, Huntsville, AL. MECHANICS, PLANE STRAIN. STRESS INTENSITY FACTORS

EFFECT OF TYPE OF LOAD ON STRESS ANALYSIS OF

THIN-WALLED DUCTS N92-33476"# National Aeronautics and Space Administration.

J. B. MIN and P. K. AGGARWAL Jun. 1992 13 p Lewis Research Center, Cleveland, OH

(NASA-TP-3248; M-688; NAS 1.60:3248) Avail: CASI HC INFLUENCE OF MASS MOMENT OF INERTIA ON NORMAL

A03/MF A01 MODES OF PRELOADED SOLAR ARRAY MAST

DUCTS, LOADS (FORCES), PIPES (TUBES), SPACE SHUTTLE SASAN C. ARMAND and PAUL LIN (Cleveland State Univ., OH.)

MAIN ENGINE, STRESS ANALYSIS, THIN WALLS Aug. 1992 12 p

(RTOP 474-46-10)

N92-27974*# National Aeronautics and Space Administration. (NASA-TP-3273; E-6847: NAS 1.60:3273) Avail: CASI HC

Lyndon B. Johnson Space Center, Houston, TX. A03/MF A01

DEVELOPMENT OF A TRUSS JOINT FOR ROBOTIC BEAMS (SUPPORTS), BENDING, DYNAMIC

ASSEMBLY OF SPACE STRUCTURES CHARACTERISTICS, DYNAMIC STRUCTURAL ANALYSIS,

GEORGE F. PARMA Jul. 1992 31 p MOMENTS OF INERTIA, SOLAR ARRAYS, SPACECRAFT

(RTOP 472-46-07-17) ANTENNAS, SPACECRAFT STRUCTURES, V18RATION MODE

31
42 GEOSCIENCES (GENERAL)

42 N91-32528"# National Aeronautics and Space Administration

Ames Research Center, Moffett Field, CA

GEOSCIENCES (GENERAL) INTERNATIONAL WORKSHOP ON STRATOSPHERIC

AEROSOLS: MEASUREMENTS, PROPERTIES, AND EFFECTS

RUDOLF F. PUESCHEL, ed. Feb. 1991 76 p Workshop held

at Moffett Field, CA, 27-30 Mar. 1990, sponsored in part by IAMAP

Radiation Commission and the NASA Upper Atmosphere Research

Program N91-20541"# National Aeronautics and Space Administration. (RTOP 573-01-21-04)

Goddard Space Flight Center, Greenbelt, MD. (NASA-CP-3114: A-90293; NAS 1.55:3114) Avail CASI HC

WEST ANTARCTIC ICE SHEET INITIATIVE. VOLUME 1: A05/MF A01

SCIENCE AND IMPLEMENTATION PLAN AEROSOLS, CLIMATOLOGY, ICE CLOUDS, POLAR

ROBERT A. BINDSCHADLER, ed. Washington Apr. 1990 METEOROLOGY, SOOT, STRATOSPHERE, VOLCANOES

61 p Conference held in Greenbelt, MD, 16-18 Oct. 1990

(NSF DPP-90-17562)

(NASA-CP-3115-VOL-1; REPT-9 1A01040-VOL-1; NAS

1.55:3115-VOL-1) Avail: CASI HC A04/MF A01 N92-10208*# National Aeronautics and Space Administration

ANTARCTIC REGIONS, CLIMATE CHANGE, ICE, ICE Langley Research Center, Hampton, VA.

ENVIRONMENTS, METEOROLOGICAL PARAMETERS, MISSION DESCRIPTION AND IN-FLIGHT OPERATIONS OF

PREDICTION ANALYSIS TECHNIQUES ERBE INSTRUMENTS ON ERBS AND NOAA 9 SPACECRAFT,

NOVEMBER 1984 - JANUARY 1986

WILLIAM L. WEAVER (ST Systems Corp., Hampton. VA.), N91-26573*# National Aeronautics and Space Administration. KATHRYN A. BUSH (ST Systems Corp., Hampton, VA.), CHRIS

Goddard Space Flight Center, Greenbelt, MD. J. HARRIS (ST Systems Corp, Hampton, VA.), CLAYTON E

WEST ANTARCTIC ICE SHEET INITIATIVE. VOLUME 2: HOWERTON, and CAROL J. TOLSON (STX Corp., Hampton,

DISCIPLINE REVIEWS VA.) Washington Aug. 1991 282 p

ROBERT A. BINDSCHADLER, ed. Washington May 1991 (RTOP 665-45-20)

147 p Workshop held in Greenbelt, MD, 16-18 Oct. 1990; (NASA-RP-1256; L-16895; NAS 1.61:1256) Avail: CASI HC

sponsored in part by NASA, Washington, and NSF, Washington, A13/MF A03

DC Instruments of the Earth Radiation Budget Experiment (ERBE)

(NASA-CP-3115-VOL-2; REPT-91A01040-VOL-2; NAS are operating on three different Earth orbiting spacecrafts- the

1.55:3115-VOL-2) Avail: CASI HC A07/MF A02 Earth Radiation Budget Satellite (ERBS). NOAA-9, and NOAA-t0.

ANTARCTIC REGIONS, CLIMATOLOGY, ICE, SEA LEVEL An overview is presented of the ERBE mission, in-orbit

environments, and instrument design and operational features. An

overview of science data processing and validation procedures is

also presented. In-flight operations are described for the ERBE 43 instruments aboard the ERBS and NOAA-9. Calibration and other

operational procedures are described, and operational and

instrument housekeeping data are presented and discussed.

EARTH RESOURCES AND REMOTE SENSING Author

Includes remote sensing of earth resources by aircraft and

spacecraft; photogrammetry; and aerial photography. N92-32127"# National Aeronautics and Space Administration,

Langley Research Center, Hampton, VA.

N91-15615"# National Aeronautics and Space Administration. MISSION DESCRIPTION AND IN-FLIGHT OPERATIONS OF

Goddard Space Flight Center, Greenbelt, MD. ERBE INSTRUMENTS ON ERBS, NOAA 9, AND NOAA 10

MULTISOURCE DATA INTEGRATION IN REMOTE SENSING SPACECRAFT Report, Feb. 1986 - Jan. 1987

JAMES C. TILTON, ed. Washington Jan. 1991 155 p Workshop WILLIAM L. WEAVER, KATHRYN A. BUSH (ST Systems Corp..

held in College Park, MD, 14-15 Jun. 1990; sponsored by NASA. Hampton, VA.), KEITH T. DEGNAN (ST Systems Corp., Hampton,

Goddard Space Flight Cetier and IEEE VA.), CLAYTON E. HOWERTON (ST Systems Corp., Hamptcn,

(NASA-CF 3099; REPT-90B00122; NAS 1.55:3099) Avail: CASI VA.), and CAROL J. TOLSON (ST Systems Corp., Hampton, VA.,

HC A08/MF A02 Aug. 1992 217 p

DATA ACQUISITION, DATA INTEGRATION, IMAGE ANAL YSIS, (RTOP 665-45-20)

IMAGE PROCESSING, MULTISENSOR APPLICATIONS, REMOTE (NASA-RP-1279; L-17069; NAS 1.61:1279) Avail, CASI HC

SENSING, REMOTE SENSORS A10/MF A03

Instruments of the Earth Radiation Budget Experiment (ERBE)

are operating on three different Earth-orbiting spacecraft. The Earth

N91-30588"# National Aeronautics and Space Administration, Radiation Budget Satellite (ERBS) is operated by NASA, and NOAA

Washington, DC. 9 and NOAA 10 weather satellites are operated by the National

EARTH OBSERVATIONS AND GLOBAL CHANGE DECISION Oceanic and Atmospheric Administration (NOAA). This paper is

MAKING: A SPECIAL BIBLIOGRAPHY, 1991 the second in a series that describes the ERBE mission, and

Jun. 1991 99 p data processing and validation procedures. This paper describes

(NASA-SP-7092; NAS 1 21:7092) Avail: CASI HC A05/MF A02 the spacecraft and instrument operations for the second full year

The first section of the bibliography contains 294 bibliographic of in-orbit operations, which extend from February 1986 through

citations and abstracts of relevant reports, articles, and documents January 1987. Validation and archival of radiation measurements

anncunced in 'Scientific and Te-hnical Aerospace Reports (STAR)' made by ERBE instruments during this second year of operation

and 'International Aerospace Abstracts (IAA)'. These abstracts are were completed in July 1991. This period includes the only time.

categorized by the following major subject divisions: aeronautics, November 1986 through January 1987, during which all ERBE

astronautics, chemistry and materials, engineering, geosciences, instruments aboard the ERBE, NOAA 9, and NOAA 10 spacecraft

life sciences, mathematical and computer sciences, physics, social were simultaneously operational. This paper covers normal and

sciences, space sciences and general. Following the abstract special operations of the spacecraft and instruments, operational

section, seven indexes are provided for further assistance. anomalies, and the responses of the instruments to in-orbit and

Author seasonal variations in the solar environment. Author

32
46 GEOPHYSICS

44 N91-16467"# National Aeronautics and Space Administration

Goddard Space Flight Center, Greenbelt, MD

ENERGY PRODUCTION AND CONVERSION THE ATMOSPHERIC EFFECTS OF STRATOSPHERIC

AIRCRAFT: A CURRENT CONSENSUS

A. R. DOUGLASS (National Aeronautics and Space Administration

Includes specific energy conversion systems, e.g., fuel cells; global Goddard Space Flight Center, Greenbelt, MD). M A CARROLL

sources of energy; geophysical conversion; and windpower. (National Oceanic and Atmospheric Administration. Boulder, CO.),

W. B. DEMORE (Jet Propulsion Lab, California Inst. of Tech,

Pasadena.), J. R. HOLTON (Washington Univ., Seattle). I S A

N9-32549°# National Aeronautics and Space Administration. ISAKSEN (Oslo Univ. (Norway).), H. S. JOHNSTON (California

Lewis Research Center, Cleveland, OH. Univ., Berkeley ý, and M. K. W. KO (Atmospheric and Environmental

SPACE ELECTROCHEMICAL RESEARCH AND TECHNOLOGY Research, Inc., Cambridge, MA.) Jan. 1991 46 p

Sep. 1991 244 p Third Conference held in Cleveland, OH, (NASA-RP-1251; NAS 1.61:1251) Avdil: CASI HC A03/MF A01

9-10 Apr. 1991 In the early 1970's, a fleet of supersonic aircraft flying in the

(RTOP 506-41-21) lower stratosphere was proposed. A large fleet was never built

(NASA-CP-3125; E-6089; NAS 1.55:3125) Avail: CASt HC for economic, political, and environmental reasons. Technological

AEl /MF A03 improvements may make it economically feasible to develop ELECTRIC BATTERIES, ELECTROCHEMISTRY, FUEL CELLS supersonic aircraft for current markets. Some key results of earlier

N92-22740*# National Aeronautics and Space Administration, scientific programs designed to assess the impact of aircraft

emissions on stratospheric ozone are reviewed, and factors that Marshall Space Flight Center, Huntsville, AL. must be considered to assess the environmental impact of aircraft

THE 1991 NASA AEROSPACE BATTERY WORKSHOP exhaust are discussed. These include the amount of nitrogen oxides

JEFFREY C. BREWER, comp. Washington Feb. 1992 855 p injected in the stratosphere, horizontal transport, and

Workshop held in Huntsville, AL, 29-31 Oct. 1991 stratosphere/troposphere assessment models are presented.

(NASA-CP-3140; M-682; NAS 1.55:3140) Avail: CASI HC Areas in which improvements in scientific understanding and model

CONFE ELECI Brepresentation must be made to reduce the uncertainty in model

BATTERIES, CONFERENCES, NICKEL ELECTRIC CADMIUM BATTERIES, BATTERIES, METAL NICKEL AIR calculations are identified. Author

HYDROGEN BATTERIES, SILVER ZINC BATTERIES, SODIUM

SULFUR BATTERIES, SPACECRAFT POWER SUPPLIES, N92-19121"# National Aeronautics and Space Administration,

ZINC-OXYGEN BATTERIES Washington, DC.

THE ATMOSPHERIC EFFECTS OF STRATOSPHERIC

N92-26895*# Lockheed Missiles and Space Co., Sunnyvale, AIRCRAFT: A FIRST PROGRAM REPORT

CA. MICHAEL J. PRATHER, HOWARD L. WESOKY, RICHARD C.

MILSTAR'S FLEXIBLE SUBSTRATE SOLAR ARRAY: LESSONS MIAKE-LYE, ANNE R. DOUGLASS, RICHARD P. TURCO, DONALD

LEARNED, ADDENDUM J. WUEBBLES, MALCOLM K. W. KO, and ARTHUR L.

JOHN GIBB 1990 17 p Presented at the 26th Aerospace SCHMELTEKOPF (National Oceanic and Atmospheric

Mechanisms Symposium Administration, Washington. DC.) Jan. 1992 227 p

(NASA-CP-3147-ADD; NAS 1.55:3147-ADD) Avail: CASI HC (NASA-RP-1272; NAS 1,61:1272) Avail: CASI HC AI1/MF A03

A03/MF A01 Studies have indicated that, with sufficient technology

SOLAR ARRAYS, SPACE STATION FREEDOM development, high speed civil transport aircraft could be

economically competitive with long haul subsonic aircraft. However,

uncertainty about atmospheric pollution, along with community 45 noise and sonic boom, continues to be a major concern; and this

is addressed in the planned 6 yr HSRP begun in 1990. Building

on NASA's research in atmospheric science and emissions ENVIRONMENT POLLUTION reduction, the AESA studies particularly emphasizing stratospheric

ozone effects. Because it will not be possible to directly measure Includes atmospheric, noise, thermal, and water pollution, the impact of an HSCT aircraft fleet on the atmosphere, the only

means of assessment will be prediction. The process of establishing

credibility for the predicted effects will likely be complex and mvclve

N91-16466*# National Aeronautics and Space Administration, continued model development and testing against climatological

Washington, DC. patterns. Lab simulation of heterogeneous chemistry and other

THE ATMOSPHERIC EFFECTS OF STRATOSPHERIC effects will continue to be used to improve the current models.

AIRCRAFT: A TOPICAL REVIEW For individual titles, see N92-19122 through N92-19127.

HAROLD S, JOHNSTON (California Univ., Berkeley.), M. J.

PRATHER, and R. T. WATSON Jan. 1991 32 p

(NASA-RP-1250; NAS 1.61:1250) Avail: CASI HC A03/MF A01

In the late 1960s the aircraft industry became interested in 46

developing a fleet of supersonic transports (SSTs). Between 1972

and 1975, the Climatic Impact Assessment Program (ClAP) studied

the possible environmental impact of SSTs. For environmental GEOPHYSICS

and economic reasons, the fleet of SSTs was not developed. The

Upper Atmosphere Research Program (UARP) has recently Includes aeronomy; upper and lower atmosphere studies:

undertaken the responsibility of directing scientific research needed ionospheric and magnetospheric physics; and geomagnetism.

to assess the atmospheric impact of supersonic transports. The

UARP and the High-Speed Research Program asked Harold

Johnston to review the current understanding of aircraft emissions N91-18505"# National Aeronautic3 and Space Administration.

and their effect on the stratosphere. Johnston and his colleagues Langley Research Center, Hampton, VA.

have recently re-examined the SST problem using current models SAM 2 MEASUREMENTS OF THE POLAR STRATOSPHERIC

for stratospheric ozone chemistry. A unique view is given here of AEROSOL. VOLUME 9: OCTOBER 1982 - APRIL 1983

the current scientific issues and the lessons learned since the L. R. MCMASTER (National Aeronautics and Space Administration

beginning of ClAP, and it links the current research program with Langley Research Center, Hampton, VA.) and K. A. POWELL (ST

the assessment process that began two years ago. Author Systems Corp., Hampton, VA.) Washington Feb. 1991 77 p

33
46 GEOPHYSICS

(RTOP 665-10-40-04) 47

(NASA-RP-1244; L-16802-VOL-9; NAS 1.61:1244) Avail: CASI

HC A05/MF A01 METEOROLOGY AND CLIMATOLOGY

The Stratospheric Aerosol Measurement (SAM) 11 sensor

aboard Nimbus 7 is providing 1.0 micron extinction measurements

of Antarctic and Arctic stratospheric aerosols with a vertical Includes weather forecasting and modification.

resolution of 1 km. Representative examples and weekly averages

including corresponding temperature profiles provided by NOAA

for the time and place of each SAM II measurement are presented. N91-10448"# National Aeronautics and Space Administration.

Contours of aerosol extinction as a function of altitude and longitude Langley Research Center, Hampton, VA.

or time are plotted, and aerosol optical depths are calculated for FIRE SCIENCE RESULTS 1988

each week. Typical values of aerosol extinction and stratosphpric DAVID S. MCDOUGAL, ed. and H. SCOTT WAGNER, ed.

optical depth in the Arctic are unusually large due to the presence Washington Jul. 1990 394 p Workshop held in Vail, CO,

of material from the El Chichon volcano eruption in the Spring of 11-15 Jul. 1988; sponsored in cooperation with NASA, NSF, ONR,

1982. For example, the optical depth peaked at 0.068, more than DOE, AFGL, and NOAA

50 times background values. Typical values of aerosol extinction (RTOP 672-22.10-70)

and stratospheric optical depth in the Antarctic varied considerably (NASA-CP-3083; L-16814; NAS 1.55:3083) Avail: CASI HC

during this period due to the transport and arrival of the material A17/MF A04

from the El Chichon eruption. For example, the stratospheric optical CIRRUS CLOUDS, CLIMATOLOGY, CONFERENCES, FIRE

depth varied from 0.002 in October 1982, to 0.021 in January (CLIMATOLOGY), MARINE METEOROLOGY, PARAME1983. Polar stratospheric clouds were observed during the Arctic TERIZATION, SATELLITE OBSERVATION, STRATOCUMUwinter, as expected. A representative sample is provided of the LUS CLOUDS

ninth 6-month period of data to be used in atmospheric and climatic

studies. Author N91-13043"# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, MD,

USER'S GUIDE: NIMBUS-7 EARTH RADIATION BUDGET

N91-21641 # National Aeronautics and Space Administration. NARROW-FIELD-OF-VIEW PRODUCTS. SCENE RAD;,P NCE

Goddard Space Flight Center, Greenbelt, MD. TAPE PRODUCTS, SORTING INTO ANGULAR BINS

VOLCANISM-CLIMATE INTERACTIONS PRODUCTS, AND MAXIMUM LIKELIHOOD CLOUD

LOUIS S. WALTER, ed. and SHANAKA DESILVA, ed. (Lunar and ESTIMATION PRODUCTS

Planetary Inst., Houston, TX.) Washington Feb. 1991 145 p H. LEE KYLE (National Aeronautics and Space Administration.

Workshop held in College Park, MD. 18-19 Jun. 1990 Goddard Space Flight Center, Greenbelt, MD-), RICHARD R.

(RTOP 465-44-11) HUCEK (Research and Data Systems, Inc., Greenbelt, MD.), BRIAN

(NASA-CP-10062; REPT-91800055; NAS 1.55:10062) Avail: GROVEMAN (Research and Data Systems, Inc., Greenbelt, MD.),

CASI HC A07/MF A02 and RICHARD FREY (Research and Data Systems, Inc-. Greenbelt,

AEROSOLS, ATMOSPHERIC CHEMISTRY, ATMOSPHERIC MD.) Nov. 1990 77 p

MODELS, CLIMATE, CLOUD PHYSICS, CONFERENCES, (NAS5-29373)

GEOLOGY, PARTICLE SIZE DISTRIBUTION, VOLCANOLOGY (NASA-AP-1246; REPT-90B00143; NAS 1.61:1246) Avail: CASI

HC A05/MF A01

The archived Earth radiation budget (ERB) products produced N92G32655"# National Aeronautics and Space Administration, from the Nimbus-7 ERB narrow field-of-view scanner are described.

Goddard Space Flight Center, Greenbelt, MD. The principal products are broadband outgoing Iongwave radiation

STEADY MNDUCTIONAL EFFECTSION OGEOMAGNETISC. PA(4.5 to 50 microns), reflected solar radiation (0.2 to 4.8 microns),

CA: STEADY MOTIONAL INDUCTION OF GEOMAGNETIC and the net radiation. Daily and monthly averages are presented

CHAOS on a fixed global equal area (500 sq knm), grid for the period May

COERTE V. VOORHIES Sep. 1992 31 p 1979 to May 1980. Two independent algorithms are used to

(NASA-Til: 3272-PT-lA; NAS 1.60:3272-PT-iA; REPT-92B00100) estimate the outgoing fluxes from the observed radiances. The

Ai:CHAOS, CORE A LO. A EO M, Kalgorithms are described and the results compared. The products

CHAOS, CORE FLOW, GEOMAGNETISM, KINEMATICS, are divided into three subsets: the Scene Radiance Tapes (SRT)

MAGNETIC EFFECTS. MAGNETIC FLUX. MAGNETIC contain the calibrated radiances; the Sorting into Angular Bins

INDUCTION, PALEOMAGNETISM (SAB) tape contains the SAB produced shortwave, Iongwave, and

net radiation products; and the Maximum Likelihood Cloud

N92-33097 # National Aeronautics and Space Administration. Estimation (MLCE) tapes contain the MLCE products. The tape

Langley Research Center, Hampton, VA. formats are described in detail. Author

SAGE 1 DATA USER'S GUIDE

LEONARD R. MCMASTER, WILLIAM P. CHU, and MICHAEL W. N91-14683"# National Aeronautics and Space Administration.

ROWLAND (ST Systems Corp., Hampton, VA.) Aug. 1992 Langley Research Center, Hampton, VA.

26 p LIMB-DARKENING FUNCTIONS AS DERIVED FROM

(RTOP 665-45-30-21) ALONG-TRACK OPERATION OF THE ERBE SCANNING

(NASA-RP-1275; L-16879; NAS 1.61:1275) Avail: CASI HC RADIOMETERS FOR AUGUST 1985

A03/MF A01 G. LOUIS SMITH (National Aeronautics and Space Administration.

A guide for using the data products from the Stratospheric Langley Research Center, Hampton, VA.), NATIVIDAD D. MANALO

Aerosol and Gas Experiment 1 (SAGE 1) for scientific investigations (Lockheed Engineering and Sciences Co., Hampton, VA.), and

of stratospheric chemistry related to aerosol, ozone, nitrogen LEE M. AVIS Washington Dec. 1990 41 p

dioxide, dynamics, and climate change is presented. A detailed (RTOP 672-40-05-70)

description of the aerosol profile tape, the ozone profile tape, and (NASA-RP-1243; L-16779; NAS 1.61:1243) Avail: CASI HC

the nitrogen dioxide profile tape is included. These tapes are the A03/MF A01

SAGE 1 data products containing aerosol extinction data and ozone During August 1985, the scanning radiometers of the Earth

and nitrogen dioxide concentration data for use in the different Radiation Budget Experiment aboard the Earth Radiation Budget

scientific investigations. Brief descriptions of the instrument Satellite (ERBS) and the NOAA-9 satellite were operated in

operation, data collection, processing, and validation, and some along-track scanning modes. These data were analyzed to produce

of the scientific analyses that were conducted are also included, limb darkening functions for Earth-emitted radiation, which relates

Author the radiance in any given direction to the radiant exitence. Limb

34
47 METEOROLOGY AND CLIMATOLOGY

darkening functions are presented and Shown as figures for day the temperatures, which were used in the cloud detection algorithm

and night for each spacecraft. The scene types were computed and came originally from the Air Force 3-dlimensional nephanalysis

using measurements within 10 deg of zenith The models have dataset The seasonal changes are described The interaction of

values near zenith of 1 02 to 1,09. with values near 1 06 being clouds and the radiation budget is briefly discussed Author

typical. The typical value of the model is 1-06 for both day and

night for ERBS, and for NOAA-9, the typical value at zenith is N91-25556 *# National Aeronautics and Space Administration

1.06 for day and 1 05 for night. Mean models are formed for the Goddard Space Flight Center. Greenbelt. MID

ERBS and for the NOAA-9 results and are found to differ less THE ROLE OF WATER VAPOR IN CLIMATE. A STRATEGIC

than I percent. the ERBS results being the higher. The models RESEARCH PLAN FOR THE PROPOSED GEWEX WATER

vary about 1 percent with latitude near zenith. Author VAPOR PROJECT (GVAP)

D, OC STARR. ed and S HARVEY MELFI. ed Washington

N91-16500*# National Aeronautics and Space Administration Jul 1991 54 p Workshop held in Easton, MD, 30 Oct - 1

Marshall Space Fligh, Center. Huntsville, AL. Nov. 1990. sponsored by NASA and the GEWEX Science Steering

NASA/MSFC FY90 GLOBAL SCALE ATMOSPHERIC Group

PROCESSES RESEARCH PROGRAM REVIEW (NASA-CP-3120. REPT-916BOO108. NAS i55 3120) Avail CASI

FRED W. LESLIE, oct Washington Oct. 1990 5B p Conference HC A04/MF AOI

held in Huntsville, AL, 20.21 Aug 1990 ATMOSPHERIC MOISTURE ('lIMATE. CL[IMAT(' CHANGEý

(NASA-CP-3093. M-651-, NAS 1.55.3093) Avail. CASt HC ENERGY BUDGETF, PRECIPITATION (METEOROLOGY). WATER

A04/MF A01 VAPOR

ATMOSPHERIC CIRCULATION. ATMOSPHERIC MODELS,

ATMOSPHERIC PHYSICS. ATMOSPHERIC SOUNDING. EARTH N91-26651*# National Aeronautics and Space Adfmnintratron

ATMOSPHERE. GLOBAL ATMOSPHERIC RESEARCH Goddard Space Flight Center. Greenbelt. MID

PROGRAM METEOROLOGY, NUMERICAL WEATHER NIMBUS-7 TOMS ANTARCTIC OZONE ATLAS: AUGUST -

FORECASTING, REMOTE SENSING, WEATHER DECEMBER 1990

ARLIN J KRUEG--ER (National Aefronautics anid Spacie

N91-24719*# National Aeroiautics and Space Administration. Administration Goddard Space Flight Center. Oreenboil, MDI

Langley Research Center. Hampton, VA LANNING M PENN (Research and Data Systems. Inc,. Greenbelt

ATLAS OF WIDE-FIELD-OF-VIEW OUTGOING LONOWAVE MD),. PATRICIA T GUIMARAES (ST Systemns Corp . Vienna. VA f,

RADIATION DERIVED FROM NIMBUS 7 EARTH RADIATION COURTNEY J SCOTT (ST Systems Corp. Vienna. VA I, DAViD

BUDGET DATA SET, NOVEMBER 1985 TO OCTOBER 1987 E LARKO (ST Systems Corp. Vienna. VA I. and S(I,OTI D

T DALE BESS and G LOUIS SMITH Washington Jun 19,91 DOIRON (ST Systems Corp. Vienna, VA I Washingte.n Jun

53 p 1991 216 p

IRTOP 665-45-30-01) (NAS5-29373)

(NASA RP. 126 1. L -16934. NAS 1 61 1261, A,ýail CASI HC INASA-RP-1264, REPT.9t600103. NAS 1 61 1264) AvaI '-AS.'

A04/MF AOl HC A10/MF A03

An alias of monthly outgoing longwave radi,1ton global contour Because of the greal environmental signifiance of oznrloi noi

maps and associated s.pherical harmoriic coetffenls is presented to support continuinc; research at the Antarctic aniol Clii. Soniitjti-rn

The~ atlas contains 23 mionths (, data from Nov ýmber 1985 to Hemisphere stations, the development nf the '990 OZ~cni.'ho~t,

October 198h7 The data were derived from !h,. secoi d Earth was monitored using data from the, Nimros. 7 Toit~il OzoneM p

Hadiation Budglet (ERB) package, which was flown on the Nimbus Spvctrometer ( TOMS) instrument. orotickd in ntea' real timei.

7 Sit;ri synchronous satellite in 1987 This data sitI is a companion Atlias provides a compilee ser of daily polar orlfteqraphi proitcltin, , 'sW a-1i Pyo~1 r".ln to sm!rilr o'tases that documeicnted -10 years of 0 the TOMS Iotal ozone measur#4rnents over thie Soutiho in

ouL!o0nq longwave radiation results fromn Nimbus 6 ant Nimbus 7 Hemnisphere for the period 1 Aug through 31 Dec 19 j

saltirflis I his atlas arid the r-ompanion atlases give .3 lala set 199(0 ozone hole develtope.d in a manne, ,irnloai to that1 rt I 10597

cooti 2-year ffpndadwlbevr sul!nstudying antI 1989. reaching a comparabNen depth n oarl 00 tý,r Tik

diff'.ront as;pects of our changing climate '71he data sitl also was in sharp contras3t Ito the much w;iaki' hiwlno 1e t -i5t

Iprovidesý a 3* ykear overlap with the current Earth Radliatnori rBudget, 1990 ozone hole? remained at polar Iaittli~idos 1,, I1 flt'I~d nNty

Exporinwien IERF R3 Aul hor contrast to other rec n I years when Incý ho~ld I'3⁄4t n'iq qI:;t' 1

betore, disappearing Daily 0ozne vatýn's, Alt veil ' -

N9 1-24720' #t rjit!onat Aeronautics and Space Admininstialicinrn litroisohere stations an, ltroentertit.am' ' "

,,~drjad Spat. F iig fit Ce.nt r Groeenbelt,. MO ~ the 1 990 ozone( dis;ftrihi ion to that of 01 hi r -A n~W , i

ATLAS OF THE EARTH'S RADIATION BUDGET AS sChi-tniŽ IVeriorn 6I was 1o~ed 1o proti's-" 10 i!tW

MF ASURED BY NIMBUS-7: MAY 1979 TO MAY 1980 'wtil ais to rsItolxss th of( provittit' vanst

K i•yi I (Na l ttii' ai Aeronautic s: anrd Space, Artmtrni~sratt oi

i' !i) pan4 eF itht 6o'irIreoribelt. MD I, RICHARDI H N91-32599'#/ National Avrornaul,ts wo.' pt At~ttli

HIP' C'lireseart; i and Data S~yste~ms, Inc,. G reernhelt. ME) I a nd orin IF Koenulnfy Space( > eoh'r ( -o a Rlea, i f L

F04 f j VA[ 1, ET t[ E. f`os,-arch and Data Systlems. Inc. THE 1991 INTERNATIONAL AEROSPACE AND GROUND

t, M0 DI Wajishtrwt~ May 1i99I 13 7 p CONFERENCE ON LIGHTNING AND STATIC ELECTRICITY,

INAY, ý'1'1) VOLUME 1

INWI A H1,' [4 % AN, 1 f; 1 126'4, RFpT-iii F 0008 AVOa! CASI .?( . 't ~;p oi-.i 116dlit ini iioa rii'a 't

i i( At,i7'. A ý, 'i - s ponsored in px b' ly NASA. it,, Nt~isio ln~teial

I its at.,- lishito , tue .iasornal (.haniles in the. F..artti' i .i. I. ' i~nn , p ind F lorid, ;rsf, of Tot"i~

rattialci)n hut','r 'hit tI3 mroon period. May' 11979 to May I I1 lJsA NA I i IP I(h VOl, 1, NAN, 1 7 2,31(1 VC~l 1; AvillA-.! '

II hi'lps lto i, t 0o strfong lit ta ni.ti~sn by wttii:h At'ý ,1 Ait f5a

trio I aIrthft-tln,ileo ritoracts with thi'- fop of The alinosphIrnni Ai i ,ýIi Al(I- VIHI(1Itf S AMHCRAI I i A, AfIf)S A,ýrAT;(O

irtsoiation to1 rrniiif.( thi' one~rqy that varinonu rigijons, absorb ftomr MF Tf CU~I NT[ 10 NI .fS I it [Tf1' i ' 5 iAtK I S i i(,i

Itf. Sort !. t l i yC ip' s ao .l- u' rlo ti wtiii..h are linked to thHA, AinW - '' l, t l(,iitNsNI, I['Il--.i S AI

iurfan tlrilwtei .inI !t,;, riilipn~til clilnati are k.'y ttel~ntels- in F L .1 iiDi r

hi',ntert:.1iott Arint~i t ,i airno andrti oetifly maps of the albedo.

(ii ol l~il)i.0 nt n1t 'vlalion nroorntnoii boilu cover aini N91 32660't a t:nIl A''tonaut, a mud f t

'nia ltorraiat',urf~wiii Iernp-aiimritt are, prorsenilfnt / unojal artid Marshaill Npw It ` ilgil Iine uiail At

atnti'I *:1gStj for'. inq-ipl 0 p -I iI5 ol ivi n All of too'nui'nli' NASA IMSFC FY91 GLOBAL SCALE ATMOSPHE RIC

rln finnivitIt !rom Ninotw,,!' ,ateiliti' nnasinnnerlsirept for PROCESSES RESEARCH PROGRAM REVIEW

35
47 METEOROLOGY AND CLIMATOLOGY

FREDW. LESLIE, ed. Washington Sep. 1991 94 p Conference (NASA-RP.1277; REPT-92B00059; NAS 1.61:1277) Avail: CASI

held in Huntsville, AL, 28-31 May 1991 HC A03/MF A01

(NASA-CP-3126; M-669; NAS 1.55:3126) Avail: CASI HC This publication serves as an introduction to the Air-Sea

A05/MF A01 Interaction Research Facility at NASA/GSFC/Wallops Flight

ATMOSPHERIC PHYSICS, DATA PROCESSING, EARTH Facility. The purpose of this publication is to provide background

ATMOSPHERE, EARTH OBSERVATIONS (FROM SPACE), information on the research facility itself, including capabilities,

METEOROLOGICAL PARAMETERS, METEOROLOGY, available instrumentation, the types of experiments already done,

SATELLITE OBSERVATION, WEATHER FORECASTING ongoing experiments, and future plans. Author

N 0 1-32693"# National Aeronautics and Space Administration. N92-27930*# National Aeronautics and Space Administration

John F. Kennedy Space Center, Cocoa Beach, FL. Wallops Flight Facility, Wallops Island, VA.

THE 1991 INTERNATIONAL AEROSPACE AND GROUND A SELF-ZEROING CAPACITANCE PROBE FOR WATER WAVE

CONFERENCE ON LIGHTNING AND STATIC ELECTRICITY, MEASUREMENTS

VOLUME 2 STEVEN R. LONG Jun. 1992 45 p

Aug. 1991 459 p Conference held in Cocoa Beach, FL, 16-19 (NASA-RP-1278; REPT-92B00058; NAS 1 61:1278) Avail: CASI

Apr. 1991; sponsored in part by NASA, the National Interagency HC A03/MF A01

Coordination Group, and Florida Inst. of Tech. The wave probe developed at the Air-Se i Interaction Research

(NASA-CP-3106-VOL-2; NAS 1.55:3106-VOL-2) Avail: CASt HC Facility was designed to measure the surface elevation fluctuations

A20/MF A04 of water waves. Design criteria included being linear in response,

ELECTROMAGNETIC COUPLING, ELECTROMAGNETIC self-zeroing to the mean water level, having multiple operating

PULSES, LIGHTNING, STATIC ELECTRICITY, WEATHER ranges so that the instrument's maximum output could be matched

FORECASTING to the maximum surface elevation over varying conditions, and be

as noise-free as possible. The purpose of this publication is to

N92-33482*# National Aeronautics and Space Administration. provide a detailed description of the design and construction of

Langley Research Center, Hampton, VA. this probe. Author

INERTIAL OSCILLATION OF A VERTICAL ROTATING DRAFT

WITH APPLICATION TO A SUPERCELL STORM

ROBERT C. COSTEN and LARRY V. STOCK (Hampton Univ., 51

VA.) Sep. 1992 47 p A video recording supplement L-0592-97

N92-24346 is available from CASI $12 Original contains color

illustrations LIFE SCIENCES (GENERAL)

(RTOP 506-41-41-01)

(NASA-TP-3230; L-16987; NAS 1.60:3230) Avail: CASt HC

A03/MF A01; 1 functional color page

ANTICYCLONES, ATMOSPHERIC CIRCULATION. ATMOSPHERIC PHYSICS, CORIOLIS EFFECT, INERTIA. MATHEMAT- N91-13842"# National Aeronautics and Space Administration,

ICAL MODELS. OSCILLATIONS. THUNDERSTORMS, WIND WashiNloro, DC.

SHEAR BIOLOGICAL LIFE SUPPORT TECHNOLOGIES: COMMERCIAL

OPPORTUNITIES

N92-34246* National Aeronautics and Space Administration. MARK NELSON, ed. (Space Biospheres Ventures. Oracle, AZ.)

La igley Research Center, Hampton, VA. and GERALD SOFFEN, ed. (Space Biospheres Ventures, Oracle,

INERTIAL OSCILLATION OF A VERTICAL ROTATING DRAFT AZ.) Nov. 1990 117 p Workshop held in Tucson, AZ, 30

WITH APPLICATION TO A SUPERCELL STORM: VIDEO Oct. - 1 Nov. 1989

SUPPLEMENT TO NASA TECHNICAL PAPER 3230 (Video (NASA-CP-3094; NAS 1.55:3094) Avail: CASI HC A06/MF A02

Recording) BIOSPHERE, CLOSED ECOLOGICAL SYSTEMS,

ROBERT C. COSTEN and LARRY V. STOCK (Hampton Univ., ENVIRONMENTAL ENGINEERING. REGENERATION (PHYSIOLVA.) 15 Sep. 1992 This supplements NASA-TP-3230; OGYi. SPACE COMMERCIALIZATION

N92-33482 Video Recording: 8 min., color, sound. VHS

(RTOP 506-41-41-01)

(NASA-TP-3230-VIDEO-SUPPL; L-0592-97; NAS

1.60:3230-VIDEO-SUPPL) Avail: Issuing Activity (Center for 52

AeroSpace Information) Video Recording $12

ATMOSPHERIC CIRCULATION, ATMOSPHERIC MODELS, AEROSPACE MEDICINE

COMPUTERIZED SIMULATION, MATHEMATICAL MODELS,

OSCILLATIONS. ROTATION, THUNDERSTORMS, VERTICAL AIR Includes physiological factors; biological effects of radiation, and

CURRENTS effects of weightlessness on man and animals.

48 N91-10574*# National Aeronautics and Space Administration

Lyndon B. Johnson Space Center, Houston, TX.

WORKSHOP ON EXERCISE PRESCRIPTION FOR

OCEANOGRAPHY LONG-DURATION SPACE FLIGHT

BERNARD A. HARRIS, ,jR, ed. and DONALD F. STEWART, ed.

Includes biological, dynamic, and physical oceanography: and Washington Oct. 1989 125 p Workshop held in Houston. TX,

marine resources. 1986

(RTOP 073-36-00-00-72)

(NASA-CP-3051; S-597; NAS 1.55:3051) Avail: CASI HC

N92-25981*# National Aeronautics and Space Administration. A06/MF A02

Wallops Flight Facility, Wallops Island, VA. BONE DEMINERALIZATION, CARDIOVASCULAR SYSTEM,

NASA WALLOPS FLIGHT FACILITY AIR-SEAJNTERACTION DECONDITIONING, EXERCISE PHYSIOLOGY. LONG DURATION

RESEARCH FACILITY SPACE FLIGHT MUSCULOSKELETAL SYSTEM, PHYSICAL

STEVEN R. LONG Jun. 1992 34 p EXERCISE, WEIGHTLESSNESS

36
52 AEROSPACE MEDICINE

N91-10594" National Aeronautics and Space Administration, MICHAEL R MCGINNIS, ed (T- (as Univ, Galveston ). S K

Washington, DC. MISHRA, ed. (Krug Life Sciences, Inc., Houston. TX.), and

AEROSPACE MEDICINE AND BIOLOGY: A CONTINUING CHRISTINE F. WOGAN, ed (Krug Intenational. Houston. TX)

BIBLIOGRAPHY WITH INDEXES (SUPPLEMENT 341) Washington Feb. 1991 40 p Conference held in Houston.

Oct. 1990 50 p TX, 6-8 Nov. 1989

(NASA-SP-7011(341); NAS 1.21:7011(341)) Avail: CASI HC A03 (NASA-CP-3108; S-619: NAS 1.55:3108) Avail CASI HC

This bibliography lists 133 reports, articles and other documents A03/MF A01

introduced into the NASA Scientific and Technical Information EXOBIOLOGY. HEALTH. MICROBIOLOGY. MICROORSystem during September 1990. Subject coverage includes: GANISMS, RESEARCH AND DEVELOPMENT. SPACE STATION

aerospace medicine and psychology, life support systems and FREEDOM. SPACE STATIONS, SPACECREWS

controlled environments, safety equipment, exobiology and

extraterrestrial life, and flight crew behavior and performance. N91-19711 ° # National Aeronautics and Space Administration

Author John F. Kennedy Space Center, Cocoa Beach, FL

RESPONSES OF WOMEN TO ORTHOSTATIC AND EXERCISE

N91-13063" National Aeronautics and Space Administration, STRESSES Technical Report, 1976 - 1977

Washington, DC. G W. HOFFLER (National Aeronautics and Space Administration.

AEROSPACE MEDICINE AND BIOLOGY: A CONTINUING John F. Kennedy Space Center, Lompoc, CA.). M M. JACKSON

BIBLIOGRAPHY WITH INDEXES (SUPPLEMENT 342) (National Aeronautics and Space Administration Lyndon B.

Nov. 1990 81 p Johnson Space Center, Houston, TX.). R. L. JOHNSON (National

(NASA-SP-7011(342); NAS 1.21:7011(342)) Avail: CASI HC A05 Aeronautics and Space Administration. Lyndon B. Johnson Space

This bibliography lists 208 reports, articles and other documents Center, Houston, TX.), J. T. BAKER (Krug International. San

introduced into the NASA Scientific and Technical Information Antonio. TX.). and D. TATRO (Bionetics Corp., Cncoa Beach. FL)

System during October 1990. Subject coverage includes: aerospace Washington Oct. 1990 77 p

medicine and psychology, life support systems and controlled (NAS9-14880; NAS10-1 1624)

environments, safety equipment, exobiology and extraterrestrial life, (NASA-TP-3043; NAS 1.60:3043) Avail: CASI HC A05/MF A01

and flight crew behavior and performance. Author ANTHROPOMETRY. DATA BASES, FEMALES, HISTORIES.

PHYSICAL EXERCISE, PHYSIOLOGY. REDUCED GRAVITY,

N91-1471 1 National Aeronautics and Space Administration, STATISTICAL CORRELATION

Washington. DC.

AEROSPACE MEDICINE AND BIOLOGY: A CONTINUING N91-23700 National Aeronautics and Space Administration,

BIBLIOGRAPHY WITH INDEXES (SUPPLEMENT 343) Washington, DC.

Dec. 1990 82 p AEROSPACE MEDICINE AND BIOLOGY: A CONTINUING

(NASA.SP-7011(343); NAS 1.21:7011(343)) Avail: CASI HC A05 BIBLIOGRAPHY WITH INDEXES (SUPPLEMENT 346)

This bibliography lists 125 reports, articles and other documents Feb. 1989 50 p

introduced into the NASA Scientific and Technical Information (NASA-SP-7011(346); NAS 1.21:7011(346)) Avail: CASI HC A03

System during January, 1989. Subject coverage includes: This bibliography lists 134 reports, articles and other documents

aerospace medicine and psychology, life support systems and introduced into the NASA Scientific and Technical Information

controlled environments, safety equipment, exobiology and System during Jan. 1991. Subject coverage includes: aerospace

extraterrestrial life. and flight crew behavior and performance. medicine and psychology, life support systems and controlled

Author environments, safety equipment, exobiology and extraterrestrial life.

and flight crew behavior and performance. Author

N91-14712" National Aeronautics and Space Administration.

Washington, DC. N9 1-23701" National Aeronautics and Space Administration.

AEROSPACE MEDICINE AND BIOLOGY: A CONTINUING Washington, DC.

BIBLIOGRAPHY WITH INDEXES (SUPPLEMENT 344) AEROSPACE MEDICINE AND BIOLOGY: A CONTINUING

Jan. 1991 92 p BIBLIOGRAPHY WITH INDEXES (SUPPLEMENT 347)

(NASA-SP.7011(344); NAS 1.21.7011(344)) Avail: CASI HC A05 Feb. 1989 64 p

This bibliography lists 125 reports, articles and other documents (NASA-SP-701 1(347); NAS 1.21:7011(347)) Avail: CASI HC A04

introduced into the NASA Scientific and Technical Information This bibliography lists 166 reports, articles and other documents

System during January, 1989. Subject coverage includes: introduced into the NASA Scientific and Technical Information

aerospace medicine and psychology, life support systems and System during Feb. 1991. Subject coverage includes, aerospace

controlled environments, safety equipment, exobiology and medicine and psychology, life support systems and controlled

extraterrestrial life, and flight crew behavior and performance. environments, safety equipment, exobiology and extraterrestrial life,

Author and flight crew behavior and performance. Author

N91-16547" National Aeronautics and Space Administration,

Washington, DC. N91-23702° National Aeronautics and Space Administration,

AEROSPACE MEDICINE AND BIOLOGY: A CUMULATIVE Washington, DC_

INDEX TO A CONTINUING BIBLIOGRAPHY (SUPPLEMENT AEROSPACE MEDICINE AND BIOLOGY: A CONTINUING

345) BIBLIOGRAPHY WITH INDEXES (SUPPLEMENT 348)

Jan. 1991 233 p Apr 1991 60 p

(NASA-SP-7011(345); NAS 1.21:7011(345)) Avail: CASI HC All (NASA.SP.7011(348); NAS 1.2137011(348)) Avail- CASI HC A04

This publication is a cumulative index to the abstracts contained This bibliography lists 154 reports, articles and other documents

in Supplements 333 through 344 of Aerospace Medicine and introduced into the NASA Scientific and Technical Information

Biology: A Continuing Bibliography. Seven indexes are included -- System during Mar. 1991. Sublect coverage includes, aerospace

subject. personal author, corporate source, foreign technology, medicine and psychology, life support systems and controlled

contract number, report number, and accession number. Author environments, safety equipment, exobiology and extraterrestrial lite,

and flight crew behavior and performance. Author

N91-18573"# National Aeronautics and Space Administration.

Lyndon B Johnson Space Center, Houston. TX N91-24731 National Aeronautics and Space Administration.

MICROBIOLOGY ON SPACE STATION FREEDOM Washington, DCr

DUANE L. PIERSON, ed. (National Aeronautics and Space AEROSPACE MEDICINE AND BIOLOGY: A CONTINUING

Administration. Lyndon B. Johnson Space Center, Houston, TX.), BIBLIOGRAPHY WITH INDEXES (SUPPLEMENT 349)

37
52 AEROSPACE MEDICINE

May 1991 50 p controlled environments, safety equipment, exobiology and

(NASA-SP.7011(349); NAS 1.21:7011(349)) Avail: CASI HC A03 extraterrestrial life, and flight crew behavior and performance.

This bibliography lists 149 reports, articles and other documents Author

introduced into the NASA Scientific and Technical Information

System during April, 1991. Subject coverage includes: aerospace N92-12412° National Aeronautics and Space Administration,

medicine and psychology, life support systems and controlled Washington, DC.

environments, safety equipment, exobiology and extraterrestrial life, AEROSPACE MEDICINE AND BIOLOGY: A CONTINUING

and flight crew behavior and performance. Author BIBLIOGRAPHY WITH INDEXES (SUPPLEMENT 355)

Nov. 1991 59 p

N91-25600" National Aeronautics and Space Administration, (NASA-SP-7011(355); NAS 1.21:7011(355)) Avail: CASI HC A04

Washington, DC. This bibliography lists 147 reports, articles and other documents

AEROSPACE MEDICINE AND BIOLOGY: A CONTINUING introduced into the NASA Scientific and Technical Information

BIBLIOGRAPHY WITH INDEXES (SUPPLEMENT 350) System during October, 1991. Subject coverage includes:

Jun. 1991 56 p aerospace medicine and psychology, life support systems and

(NASA-SP-7011(350); NAS 1.21:7011(350)) Avail: CASI HC A04 controlled environments, safety equipment, exobiology and

This bibliography lists 152 reports, articles and other documents extraterrestrial life, and flight crew behavior and performance.

introduced into the NASA Scientific and Technical Information Author

System during May 1991. Subject coverage includes: aerospace

medicine and psychology, life support systems and controlled N92-15538" National Aeronautics and Space Administration,

environments, safety equipment, exobiology and extraterrestrial life, Washington, DC.

and flight crew behavior and performance. Author AEROSPACE MEDICINE AND BIOLOGY: A CONTINUING

BIBLIOGRAPHY WITH INDEXES (SUPPLEMENT 356)

N91-27756" National Aeronautics and Space Administration, Dec. 1991 71 p

Washington, DC. (NASA-SP-7011(356); NAS 1.21:7011(356)) Avail: CASI HC A04

AEROSPACE MEDICINE AND BIOLOGY: A CONTINUING This bibliography lists 192 reports, articles and other documents

BIBLIOGRAPHY WITH INDEXES (SUPPLEMENT 351) introduced into the NASA Scientific and Technical Information

Jul. 1991 92 p System during November 1991. Subject coverage includes:

(NASA-SP.7011(351); NAS 1.21:7011(351)) Avail: CASI HC A05 aerospace medicine and psychology, life support systems and

This bibliography lists 255 reports, articles and other documents controlled environments, safety equipment, exobiology and

introduced into the NASA Scientific and Technical Information extraterrestrial life, and flight crew behavior and performance.

System during Jun. 1991. Subject coverage includes: aerospace Author

medicine and psychology, life support systems and controlled

environments, safety equipment, exobiology and extraterrestrial life, N92-16553*# National Aeronautics and Space Administration.

and flight crew behavior and performance. Author Lyndon B. Johnson Space Center, Houston, TX.

EVALUATION OF NONINVASIVE CARDIAC OUTPUT

N91-28729° National Aeronautics and Space Administration, METHODS DURING EXERCISE

Washington, DC ALAN D. MOORE (Krug Life Sciences, Inc., Houston, TX.), LINDA

AEROSPACE MEDICINE AND BIOLOGY: A CONTINUING H. BARROWS (Krug Life Sciences, Inc., Houston, TX.), MICHAEL

BIBLIOGRAPHY WITH INDEXES (SUPPLEMENT 352) RASHID, and STEVEN F. SICONOLFI Jan. 1992 10 p

Aug. 1991 61 p (NASA-TP-3174; S-657; NAS 1.60:3174) Avail: CASI HC

(NASA-SP-7011(352); NAS 1.21:7011(352)) Avail: CASI HC A04 A02/MF A01

This bibliography lists 147 reports, articles and other documents BIOMEDICAL DATA, CARBON DIOXIDE, CARDIAC OUTPUT,

introduced into the NASA Scientific and Technical Information REBREATHING

System during July 1991. Subject coverage includes: aerospace

medicine and psychology, life support systems and controlled N92-16554*# National Aeronautics and Space Administration.

environments, safety equipment, exobiology and extraterrestrial life, Lyndon B. Johnson Space Center, Houston, TXand flight crew behavior and performance. Author FUEL UTILIZATION DURING EXERCISE AFTER 7 DAYS OF

BED REST

N91-31760* National Aeronautics and Space Administration, LINDA H. BARROWS (Krug Life Sciences, Inc., Houston, TX.),

Washington, DC. BERNARD A. HARRIS (Krug Life Sciences, Inc., Houston, TX.),

AEROSPACE MEDICINE AND BIOLOGY: A CONTINUING ALAN D. MOORE (Krug Life Sciences, Inc., Houston, TX.), and

BIBLIOGRAPHY WITH INDEXES (SUPPLEMENT 353) STEVEN F. SICONOLFI Washington Jan. 1992 11 p

Feb. 1989 84 p (NASA.TP-3175; S-658; NAS 1.60:3175) Avail: CASI HC

(NASA.SP-7011(353); NAS 1.21:7011(353)) Avail: CASI HC A05 A03/MF A01

This bibliography lists 238 reports, articles, and other documents BED REST, CALORIC REQUIREMENTS, CARBOHYDRATE

introduced into the NASA Scientific and Technical Information METABOLISM, GRAVITATIONAL EFFECTS, PHYSICAL

System in August 1991. Subject coverage includes: aerospace EXERCISE, PHYSICAL FITNESS, PROTEINS

medicine and psychology, life support systems and controlled

environments, safety equipment, exobiology and extraterrestrial life, N92-17022"# National Aeronautics and Space Administration.

biotechnology, human factors engineering, and flight crew behavior Lyndon B. Johnson Space Center, Houston. TX,

and performance. Author TECHNIQUES FOR DETERMINATION OF IMPACT FORCES

DURING WALKING AND RUNNING IN A ZERO-G

N92-12404* National Aeronautics and Space Administration, ENVIRONMENT

Washington, DC MICHAEL GREENISEN (Krug Life Sciences, Inc., Houston, TX),

AEROSPACE MEDICINE AND BIOLOGY: A CONTINUING MARLEI WALTON (Alabama Univ., Tuscaloosa.), PHILLIP BISHOP,

BIBLIOGRAPHY WITH INDEXES (SUPPLEMENT 354) and WILLIAM SQUIRES (Texas Lutheran Coll., Seguin.)

Oct. 1991 86 p Washington Jan. 1992 18 p

(NASA-SP-7011(354); NAS 1 21:7011(354)) Avail: CASI HC A05 (NASA-TP-3159; S-651; NAS 1.60:3159) Avail: CASI HC

This bibliography lists 225 reports, articles and other documents A03/MF A01

introduced into the NASA Scientific and Technical Information BONE DEMINERALIZATION. GRAVITATIONAL PHYSIOLOGY.

System during September. 1991. Subject coverage includes IMPACT LOADS, MUSCULOSKELETAL SYSTEM, REDUCED

aerospace medicine and psychology, life support systems and GRAVII Y. WALKING, WEIGHTLESSNESS SIMULATION

38
53 BEHAVIORAL SCIENCES

N92-17645"# National Aeronautics and Space Administration. N92-27068" National Aeronautics and Space Administration,

Lyndon B, Johnson Space Center, Houston. TX Washington, DC

ECCENTRIC AND CONCENTRIC MUSCLE PERFORMANCE AEROSPACE MEDICINE AND BIOLOGY: A CONTINUING

FOLLOWING 7 DAYS OF SIMULATED WEIGHTLESSNESS BIBLIOGRAPHY WITH INDEXES (SUPPLEMENT 362)

JUDITH C. HAYES (Krug Life Sciences Inc., Houston. TX.), MARY May 1992 118 p

L ROPER (Krug Life Sciences, Inc., Houston, TX.), AUGUSTUS (NASA-SP-7011(362); NAS 1.21:7011(362)) Avail: CASI HC A06

D. MAZZOCCA (Krug Life Sciences, Inc., Houston. TX.), JOHN J. This bibliography lists 357 reports, articles and other documents

MCBRINE (Krug Life Sciences, Inc., Houston, TX.), LINDA H. introduced into the NASA Scientific and Technical Information

BARROWS (Krug Life Sciences, Inc., Houston, TX.), BERNARD System during May 1992 Subjecl coverage includes aerospace

A. HARRIS, and STEVEN F. SICONOLFI Washington Feb. medicine and physiology, life support systems and man/system

1992 13 p technology, protective clothing, exobiology and extraterrestrial life,

(NASA-TP-3182; S-665; NAS 1.60:3182) Avail: CASI HC planetary biology, and flight crew behavior and performance

A03/MF A01 Author

BED REST, HUMAN PERFORMANCE, MUSCLES, MUSCULAR

FUNCTION, MUSCULOSKELETAL SYSTEM, WEIGHTLESSNESS N92-27433* National Aeronautics and Space Administration,

SIMULATION Washington, DC

AEROSPACE MEDICINE AND BIOLOGY: A CONTINUING

BIBLIOGRAPHY WITH INDEXES (SUPPLEMENT 361)

N92-21714" National Aeronautics and Space Administration, Apr. 1992 56 p

Washington, DC. (NASA-SP-7011(361); NAS 1.21:7011(361)) Avail. CASI HC A04

AEROSPACE MEDICINE AND BIOLOGY: A CONTINUING This bibliography lists 141 reports, articles and other documents

BIBLIOGRAPHY WITH INDEXES (SUPPLEMENT 357) introduce" into the NASA Scientific and Technical Information

Jan. 1992 69 p System during Mar. 1992. Subject coverage includes. aerospace

(NASA-SP-7011(357); NAS 1.21:7011(357)) Avail: CASI HC A04 medicine and physiology. life support systems and man/system

This bibliography lists 186 reports, articles and other documents technology, protective clothing, exobiology and extraterrestrial life,

introduced into the NASA Scientific and Technical Information planetary biology, and flight crew behavior and performance.

System during Dec. 1991. Subject coverage includes: aerospace Author

medicine and physiology, life support systems and man/system

technology, protective clothing, exobiology and extraterrestrial life, N92-30987" National Aeronautics and Space Administration,

planetary biology, and flight crew behavior and performance. Washington, DC.

Author AEROSPACE MEDICINE AND BIOLOGY: A CONTINUING

BIBLIOGRAPHY WITH INDEXES (SUPPLEMENT 363)

Jun. 1992 69 p N92-21715* National Aeronautics and Space Administration, (NASA-SP-7011(363); NAS 1.21:7011(363)) Avail: CASI HC

Washington, DC. A04/MF A01

AEROSPACE MEDICINE AND BIOLOGY: A CONTINUING This bibliography lists 164 reports, articles an,' other documents

BIBLIOGRAPHY WITH INDEXES (SUPPLEMENT 359) introduced into the NASA Scientific and Techni"l Information

Feb 1992 60 p System during Jan. 1992. Subtect coverage includes aerospace

(NASA-SP-7011(359), NAS 1.21:7011(359)) Avail: CASI HC A04 medicine and physiology, life support systems and man/system

This bibliography lists 164 reports, articles and other documents technology, protective clothing, exobiology and extraterrestrial life.

introduced into the NASA Scientific and Technical Information planetary biology, and flight crew behavior and performance.

System during Jan. 1992. Subject coverage includes: aerospace Author

medicine and physiology, life support systems and man/system

technology, protective clothing, exobiology and extraterrestrial life, N92-34154"# National Aeronautics and Space Administration

planetary biology, and flight crew behavior and performance. Langley Research Center. Hampton, VA

Author TRACK STRUCTURE MODEL OF CELL DAMAGE IN SPACE

FLIGHT

ROBERT KATZ (Nebraska Univ., Lincoln.), FRANCIS A

N92-22026* National Aeronautics and Space Administration, CUCINOTTA, JOHN W. WILSON, JUDY L SHINN, and DUC M

Washington, DC. NGO (Old Dominion Univ., Norfolk, VA) Oct. 1992 32 p AEROSPACE MEDICINE AND BIOLOGY: A CUMULATIVE (RTOP 199-04-16-11) INDEX TO A CONTINUING BIBLIOGRAPHY (SUPPLEMENT (NASA-TP-3235; L-17058; NAS 1.60:3235) Avail CASI HC 358) A03/MF A01

Jan 1992 229 p BIOLOGICAL EFFECTS, CELLS (BIOLOGY), EXPOSURE.

(NASA-SP-7011(358). NAS 1.21:7011(358)) Avail: CASI HC All EXTRATERRESTRIAL RADIATION, LINEAR ENERGY TRANSFER

This publication is a cumulative index to the abstracts contained (LET), RADIATION DAMAGE, RELATIVE BIOLOGICAL

in Supplements 346 through 357 of Aerospace Medicine and EFFECTIVENESS (RBE), SURVIVAL

Biology: A Continuing Bibliography. It includes seven indexes:

subject, personal author, corporate source, foreign technology,

contract number, report number and accession number. Author

53

N92-22186"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, VA. BEHAVIORAL SCIENCES

MULTIPLE LESION TRACK STRUCTURE MODEL

JOHN W WILSON. FRANCIS A. CUCINOTTA, and JUDY L Includes psychological factors. individual and group behavior: crew

SHINN Mar 1992 14 p Sponsored in part by the Armed training and evaluation, and psychiatric research

Forces Radtobiotogy Research Institute

(RTOP 199-04-16.11)

(NASA-TP-3185; L-16988, NAS 1 603185) Avail: CASI HC N92-21467*# National Aeronautics and Space Administration

A03(MF A01 Ames Research Center, Moffett Field, CA.

CELL DIVISION. CELLS (BIOLOGY), HEAVY IONS, LESIONS. VISUALLY GUIDED CONTROL OF MOVEMENT

MATHEMATICAL MODELS, RADIATION DAMAGE. RADIATION WALTER W JOHNSON, ed and MARY K KAISER, ed Apr

EFFECTS. X RAYS 1991 236 p Workshop held at Moffett Field. CA. 26 Jun - 14

39
54 MAN/SYSTEM TECHNOLOGY AND LIFE SUPPORT

Jul. 1989 (NASA-TP-3153; S-648; NAS 1.60:3153) Avail: CASI HC

(RTOP 505-67-51) A03/MF A01

(NASA-CP-3118; A-90200; NAS 1.55:3118) Avail: CASI HC EXTRAVEHICULAR ACTIVITY, FATIGUE TESTS. NEUTRAL

A11/MF A03 BUOYANCY SIMULATION, PHYSICAL EXERCISE, SPACE SUITS.

AIRCRAFT CONTROL, CONFERENCES, CONTROL THEORY, WORK CAPACITY

SPACE PERCEPTION, VISUAL CONTROL, VISUAL

PERCEPTION

N92-25961"# National Aeronautics and Space Administration.

Lyndon B. Johnson Space Center, Houston, TX.

54 NUTRITIONAL REQUIREMENTS FOR SPACE STATION

FREEDOM CREWS

MAN/SYSTEM TECHNOLOGY AND LIFE HELEN W. LANE (Krug Life Sciences, Inc., Houston, TX.),

SUPPORT BARBARA L. RICE, and CHRISTINE F. WOGAN, ed. (Krug Life

Sciences, Inc., Houston, TX.) Washington Jun. 1992 15 p

Panel held in Houston, TX, 4-5 Feb. 1991

Includes human engineering; biotechnology; and space suits and (NASA-CP-3146; S-672; NAS 1.55:3146) Avail: CASI HC

protective clothing. A03/MF A01

ASTRONAUTS, BIOLOGICAL EFFECTS, NUTRITIONAL

REQUIREMENTS, SPACE FLIGHT FEEDING, SPACE STATION

N91-24744*# National Aeronautics and Space Administration. FREEDOM

Ames Research Center, Moffett Field, CA.

CONTROLLED ECOLOGICAL LIFE SUPPORT SYSTEMS:

NATURAL AND ARTIFICIAL ECOSYSTEMS

ROBERT D. MACELROY, ed. (National Aeronautics and Space N92-26538"# National Aeronautics and Space Administration.

Administration. Ames Research Center, Moffett Field, CA.), BRAD Lyndon B. Johnson Space Center, Houston, TX.

G. THOMPSON, ed. (Alberta Research Council, Edmonton THE VALIDATION OF A HUMAN FORCE MODEL TO PREDICT

(Canada).), THEODORE W. "I IBBITTS, ed. (Wisconsin Univ., DYNAMIC FORCES RESULTING FROM MULTI-JOINT

Madison.), and TYLER VOLK, ed. (New York Univ., New York.) MOTIONS

Dec. 1989 185 p The 27th COSPAR Meeting was held in ABHILASH K. PANDYA (Lockheed Engineering and Sciences Co.,

Espoo, Finland, 18-29 Jul. 1988; sponsored by Subcommission Houston. TX.), JAMES C. MAIDA (Lockheed Engineering and

F.4 Sciences Co., Houston, TX.), ANN M. ALDRIDGE (Texas Woman's

(RTOP 199-61-12) Univ., Houston.), SCOTT M. HASSON (Texas Womens Univ.

(NASA-CP-1.0040; A-89105; NAS 1.55:10040) Avail: CASI HC Research Inst., Denton.), and BARBARA J. WOOLFORD Jun.

A09/MF A02 1992 33 p

ALGAE, CLOSED ECOLOGICAL SYSTEMS, ECOSYSTEMS, (NAS9-17900)

REGENERATION (PHYSIOLOGY), WASTE TREATMENT (NASA-TP-3206; S-670; NAS 1.60:3206) Avail: CASI HC

A03/MF A01

N92-11638"# National Aeronautics and Space Administration. HUMAN PERFORMANCE, INVERSE KINEMATICS,

Ames Research Center, Moffett Field, CA. MUSCULAR STRENGTH, SHOULDERS, TORQUE, WRIST

HUMAN MACHINE INTERFACES FOR TELEOPERATORS AND

VIRTUAL ENVIRONMENTS CONFERENCE

Mar. 1990 175 p Conference held in Santa Barbara, CA, 4-9

Mar. 1990 N92-26682"# National Aeronautics and Space Administration.

(NASA-CP-10071; NAS 1.55:10071; AD-A240716) Avail: CASI Lyndon B. Johnson Space Center, Houston, TX.

HC A08/MF A02 CORRELATION AND PREDICTION OF DYNAMIC HUMAN

COMPUTERIZED SIMULATION, FLIGHT SIMULATION. ISOLATED JOINT STRENGTH FROM LEAN BODY MASS

MAN-COMPUTER INTERFACE, OPERATORS (PERSONNEL), ABHILASH K. PANDYA, SCOTT M. HASSON, ANN M. ALDRIDGE

SENSORY PERCEPTION, TELEOPERATORS (Lockheed Engineering and Sciences Co., Houston, TX.), JAMES

C. MAIDA, and BARBARA J. WOOLFORD Jun. 1992 64 p

N92-16562 # National Aeronautics and Space Administration. (NAS9-17900)

Lyndon B. Johnson Space Center, Houston, TX. (NASA-TP-3207; S-671; NAS 1.60:3207) Avail: CASI HC

RELIABILITY OF A SHUTTLE REACTION TIMER A04/MF A01

RUSSELL D. HAYS (Krug Life Sciences, Inc., Houston, TX.), BIODYNAMICS, DYNAMIC MODELS, HUMAN BEINGS,

AUGUSTUS D. MAZZOCCA (Krug Life Sciences, Inc., Houston, JOINTS (ANATOMY), LEAST SQUARES METHOD, PREDICTION

TX.), MICHAEL RASHID, and STEVEN F. SICONOLFI ANALYSIS TECHNIQUES, REGRESSION ANALYSIS,

Washington Jan. 1992 9 p STATISTICAL CORRELATION, TORQUE

(NASA-TP-3176; S-659; NAS 1.60:3176) Avail: CASI HC

A02/MF A01

ASTRONAUT PERFORMANCE, AUDITORY STIMULI,

BIOASTRONAUTICS, COMPONENT RELIABILITY, REACTION N92-28897"# National Aeronautics and Space Administration.

TIME, SPACE SHUTTLES, SWITCHES, TIMING DEVICES, VISUAL Lyndon B. Johnson Space Center, Houston, TX.

STIMULI EXPERIMENTAL MEASUREMENT OF THE ORBITAL PATHS

OF PARTICLES SEDIMENTING WITHIN A ROTATING

N92-19772"# National Aeronautics and Space Administration. VISCOUS FLUID AS INFLUENCED BY GRAVITY

Lyndon B Johnson Space Center, Houston, TX. DAVID A. WOLF and RAY P. SCHWARZ (Krug Life Sciences,

A METHOD OF EVALUATING EFFICIENCY DURING Inc., Houston, TX.) Jun. 1992 19 p

SPACE-SUITED WORK IN A NEUTRAL BUOYANCY (RTOP 694-01-23-05)

ENVIRONMENT (NASA-TP-3200; S-668; NAS 1.60:3200) Avail: CASI HC

MICHAEL C. GREENISEN (Krug International, Houston, TX.), A03/MF A01

PHILLIP WEST, FREDERICK K. NEWTON, JOHN H. GILBERT, BIOREACTORS, CELLS (BIOLOGY), CULTURE TECHNIQUES,

and WILLIAM G. SQUIRES (Texas Lutheran Coll., Seguin.) Oct. REDUCED GRAVITY. ROTATING FLUIDS, SEDIMENTS, TISSUES

1991 11 p (BIOLOGY), VISCOUS FLUIDS

40
59 MATHEMATICAL AND COMPUTER SCIENCES (GENERAL)

55 59

SPACE BIOLOGY MATHEMATICAL AND COMPUTER SCIENCES

(GENERAL)

Includes exobiology; planetary biology; and extraterrestrial life.

N91-14725'# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, CA. N91-20641"# National Aeronautics and Space Administration

EXOBIOLOGY IN EARTH ORBIT: THE RESULTS OF SCIENCE Lyndon B Johnson Space Center. Houston, TX

WORKSHOPS HELD AT NASA, AMES RESEARCH CENTER FOURTH ANNUAL WORKSHOP ON SPACE OPERATIONS

D. DEFREES, ed., D. BROWNLEE. ed., J. TARTER, ed., D. USHER, APPLICATIONS AND RESEARCH (SOAR 90)

ed., W. IRVINE, ed., and H. KLEIN, ed. 1989 142 p Original ROBERT T SAVELY, ed Washington Jan. 1991 495 p

contains color illustrations Workshop held in Albuquerque, NM, 26-28 Jun. 1990: sponsored

(RTOP 199-52-12-01) by NASA, Washington. AF, and New Mexico Univ

(NASA-SP-500; NAS 1.21:500) Avail: CASI HC A07/MF A02; (NASA-CP-3103-VOL-1; S-618-VOL-1; NAS 1.55:3103-VOL-1)

also available SOD HC $6.50 as 033-000-01057-5; 5 functional Avail: CASI HC A21 /MF A04

color pages CONFERENCES, HUMAN FACTORS ENGINEERING, LIFE

The Workshops on Exobiology in Earth Orbit were held to SCIENCES, OPERATIONS RESEARCH, ROBOTICS

explore concepts for orbital experiments of exobiological interest

and make recommendations on which classes of experiments

should be carried out. Various observational and experimental

opportunities in Earth orbit are described including those associated

with the Space Shuttle laboratories, spacecraft deployed from the

Space Shuttle and expendable launch vehicles, the Space Station, N91-20702"# National Aeronautics and Space Administration.

and lunar bases. Specific science issues and technology needs Lyndon B, Johnson Space Center, Houston, TX.

are summarized. Finally, a list of recommended experiments in FOURTH ANNUAL WORKSHOP ON SPACE OPERATIONS

the areas of observational exobiology, cosmic dust collection, and APPLICATIONS AND RESEARCH (SOAR 90)

in situ experiments is presented. M.G. ROBERT T. SAVELY, ed. Washington Jan. 1991 316 p

Workshop held in Albuquerque, NM, 26-28 Jun. 1990; sponsored

by NASA, Washington. AF, and New Mexico Univ.

(NASA-CP-3103-VOL-2; S-618-VOL-2; NAS 1.55:3103-VOL-2)

Avail: CASI HC A14/MF A03

CONFERENCES. EXPERT SYSTEMS, HUMAN FACTORS

ENGINEERING, MAN-COMPUTER INTERFACE, OXIDATION,

SPACE SHUTTLE ORBITERS. SPACE STATIONS, SPACECRAFT

CONSTRUCTION MATERIALS

N91-15691*# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, CA.

EXOBIOLOGY ON MARS

0, L. DEVINCENZI, ed.. J. R. MARSHALL, ed,, and D. ANDERSEN,

ed. Dec. 1990 35 p Proceedings held at Moffett Field, CA, N92-12425"# National Aeronautics and Space Administration,

27-28 Feb, 1989 Goddard Space Flight Center, Greenbelt, MD.

(RTOP 199-59-12-05) SPACE AND EARTH SCIENCE DATA COMPRESSION

(NASA-CP-10055; A-90320; NAS 1.55:10055) Avail: CASI HC WORKSHOP

A03/MF A01 JAMES C. TILTON, ed. Washington Nov. 1991 85 p Workshop

EQUIPMENT SPECIFICATIONS, EXOBIOLOGY. EXPERIMENT held in Snowbird, UT, 11 Apr. 1991; sponsored by NASA and

DESIGN, MARS (PLANET), MISSION PLANNING, NASA SPACE IEEE

PROGRAMS, SPACE EXPLORATION, U.S,S.R. SPACE (RTOP 590-32-14-01)

PROGRAM (NASA-CP-3130; REPT-91B00149; NAS 1.55:3130) Avail: CASI

HC A05/MF A01

DATA COMPRESSION, EARTH OBSERVATIONS (FROM

SPACE), IMAGE PROCESSING, INFORMATION SYSTEMS.

SIGNAL PROCESSING, SPACE OBSERVATIONS (FROM

EARTH)

N92-13586' # National Aeronautics and Space Administration,

Washington, DC N92-22324*# National Aeronautics and Space Adminislration

FOURTH SYMPOSIUM ON CHEMICAL EVOLUTION AND THE Lyndon B. Johnson Space Center, Houston, TX

ORIGIN AND EVOLUTION OF LIFE Abstracts Only FIFTH ANNUAL WORKSHOP ON SPACE OPERATIONS

ROBERT A WHARTON, JR., ed, DALE T. ANDERSEN. e-d.. SARA APPLICATIONS AND RESEARCH (SOAR 1991), VOLUME 2

E BZIK. ed (National Aeronautics and Space Administration. Ames KUMAR KRISHEN, ed. Feb 1992 391 p Workshop held in

Research Center, Moffett Field, CA), and JOHN D. RUMMEL, ed Houston. TX. 9-11 Jul 1991, sponsored in cooperation with NASA.

Oct. 1991 129 p Symposium held at Moffett Field, CA, 24-27 Washington, AF, and Houston Univ., Clear Lake. TX

Jul 1990 (NASA-CP-3127-VOL-2; S-650-VOL-2, NAS 1 55!3127-VOL-2)

(RTOP 199-52-00) Avail: CASI HC A17/MF A04

(NASA.CP-3129, NAS 1 55.3129) Avail: CASI HC A07/MF A02 AEROSPACE MEDICINE. CONFERENCES. EXPERT

BIOLOGICAL EVOLUTION, CHEMICAL EVOLUTION, SYSTEMS, HUMAN FACTORS ENGINEERING. LIFE SCIENCES.

CONFERENCES, COSMIC DUST, EXOBIOLOGY, ROBOTICS. SPACE DEBRIS, SPACE PLASMAS, SPACE

GEOCHEMISTRY SHUTTLES. SPACE STATIONS, SPACECRAFT CONTROL

41
61 COMPUTER PROGRAMMING AND SOFTWARE

61 JOSEPH GIARRATANO, ed. (Houston Iniv., Clear Lake, TX) and

CHRISTOPHER J. CULBERT. ed. Sep. 1991 280 p Conference

COMPUTER PROGRAMMING AND SOFTWARE held in Houston, TX, 23-25 Sep. 1991

(NASA-CP-10085-VOL-2; S-662-VOL-2; NAS 1 55:10085-VOL-2)

Avail: CASI HC A13/MF A03

Includes computer programs, routines, ind algorithms, and specific CONFERENCES, EXPERT SYSTEMS, KNOWLEDGE BASES

applications, e.g., CAD/CAM. (ARTIFICIAL INTELL;GENCE), SOFTWARE TOOLS

N91-17559"# National Aeronautics and Space Administration. N92-23432"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, VA. Marshall Space Flight Center, Huntsville, AL.

NASA FORMAL METHODS WORKSHOP, 1990 TECHNIQUE TO ELIMINATE COMPUTATIONAL INSTABILITY

RICKY W. BUTLER, comp. Nov. 1990 504 p Workshop held IN MULTIBODY SIMULATIONS EMPLOYING THE LAGRANGE

in Hampton, 'VA, 20-23 Aug. 1990; sponsored by NASA, MULTIPLIER

Washington G. WATTS Apr. 1992 30 p

(RTOP 505-66-21-01) (NASA-TP-3220; M-687; NAS 1.60:3220) Avail: CASt HC

(NASA-CP-10052; NAS 1.55:10052) Avail: CASt HC A22/MF A03/MF A01

A04 COMPUTER TECHNIQUES, COMPUTERIZED SIMULATION,

AVIONICS, CONFERENCES, CONTROL SYSTEMS DESIGN, DYNAMICAL SYSTEMS, FLEXIBLE BODIES. LAGRANGE

DIGITAL SYSTEMS, FAULT TOLERANCE, FLIGHT CONTROL. MULTIPLIERS

LOGIC DESIGN

N91-25624"# National Aeronautics and Space Administration. N92-24397"# National Aeronautics and Space Administration

Langley Research Center, Hampton, VA. Langley Research Center, Hampton, VA.

GUIDANCE, NAVIGATION, AND CONTROL SUBSYSTEM SOFTWARI SURFACE MODELING AND GRID GENERATION

EQUIPMENT SELECTION ALGORITHM USING EXPERT STEERING COMMITTEE

SYSTEM METHODS ROBERT E. SMITH, ed. Washington Apr 1%2 510 p CHERYL L. ALLEN Washington May 1991 12 p Workshop held in Hampton. VA, 28-30 Apr. 1992 sponsored by

(RTOP 506-49-21-02) NASA, Washington

(NASA-TP-3082; L-16896: NAS 1.60:3082) Avail: CASI HC (RTOP 505-90-53-02)

A03/MF A01 (NASA.CP-3143; L-17093; NAS 1.55:3143) Avail: CASI HC

ALGORITHMS. ARCHITECTURE (COMPUTERS), COMPUTER A22/MF A04

AIDED DESIGN, CONTROL SYSTEMS DESIGN, EXPERT COMPUTATIONAL FLUID DYNAMICS, COMPUTER AIDED SYSTEMS, SPACECRAFT DESIGN, SPACECRAFT DESIGN, CONFERENCES, GRID GENERATION IMATHEMATiCS).

SYSTRMEMTS.E MATHEMATICAL MODELS, SOFTWARE ENGINEERING.

INSTRUMENTS SURFACE PROPERTIES

N91-25629"# National Aeronautics and Space Administrati n.

Marshall Space Flight Center, Huntsville, AL.

A SCHEME FOR BANDPASS FILTERING MAGNETOMETER

MEASUREMENTS TO RECONSTRUCT TETHERED SATELLITE 62

SKIPROPE MOTION

M E POLITES Vvashington Jun 1991 25 p

(NASA-TP-3123. M-663. NAS 1.60:3123) Avail: CASI HC COMPUTER SYSTEMS

A03/MF A01

BANDPASS F!LTERS. COMPUTERIZED SIMULATION, Includes computer networks and special application computer

DYNAMIC STABILITY, MAGNETIC MEASUREMENT. SATELLITE systems.

CONTROL, SPACECRAFT MOTION. VIBRATION DAMPINO

N92-11685*# National Aeronautics and Space Administration. N92-22285"# National Aeronautics and Space Administration

Langley Research Center. Hampton, VA Langley Research Center, Hampton. VA

CELLULAR REPAIR/MISREPAIR TRACK MODEL FAULT TOLERANCE OF ARTIFICIAL NEURAL NETWORKS

JOHN A WILSON and FRANCIS A. CUCINOTTA Washington WITH APPLICATIONS 'A CRITICAL SYSTEMS

Nov 1991 1i p PETER W PROTZEL, Dt

ANiEL L PAt UMBO, and MICHAEL K

(RTOP 199.04-16.111 ARRAS (Institute for Computer Ap.,ications in Science and

INASA-TP-3124. L-16949 NAS 1 60 3124) Avail CASI HC L..gineering, Hampton. VA) Apr 1992 50

A03;MF A01 (RTOP 307-50-10-12)

BfOLOGICAL EFFECTS, CELLS (BIOLOGY). KINETICS. (NASA-TP-3187' L-16969. NAS 1 603187) Avall CASI HC

LETHALIT'. RADIATION EFFECTS, RELATIVE BIOLOGICAL A03/MF A01

EFFECTIVENESS (ROE) COMP'1TERIZED SIMI li ATION. DISTRIBUT-r' PROCESS;NG.

FAULT TOLERANCE. NEuiH,,L NETS, PERFOHM E TESTS.

N92-16568"# National Aeronautics and Space Administration REAL TIME OPERATION, RELIABILITY ENGINEERIt.G

Lyndon B Johnson Space Center. Houston, TX

SECOND CLIPS CONFERENCE PROCEEDINGS, VOLUME 1

JOSEPH "•IARRATANO, ed (HouSton Univ, Clear Lake, TX ) and N92-27589*# National Aeror'aulics and Space Admirnstration

C';IRiSTOPHER J CULRERT. ed Sep 1931 232 p Conference Langley Research Center, Hampton, VA

head in Houston. TX. 2325 Sep 1991 EXPERIMENTAL VALIDATION OF CLOCK

,NASA CP 1 005 VOL- 1, S-662-VOL- I: NAS 1 55 10085-VOL-1) SYNCHRONIZATIOV ALGORITHMS

Avail CiASI eC AIlt MF A03 DANIEL L PALUMBO and R LYNN GRAHAM (PRC Kentron.

COMPUTER AIDED DESIGN, CONFEFNCES. EXPERT Inc. Hamnton. VA) Jul. 1992 24 p

S15 IFMS KNCWi.EDGE REPRESE-NTATION (RTOP 505-64-10-07)

(NASA, TP-3209, L-17015. NAS 1 A9 32-'9) Avail C,/SI HC

N92-16590"# National Aeronautics and Space Adminmistration A03/MF A01

',-ndfon B johnson Spac.e C enter. Houston. TX ALGORITHMS, CLOCKS, FAILURE MODES, SYNCHRONISM,

SECOND CLIPS CONFERENCE PROCEEDINGS, VOLUME 2 TIME MEASUREMENT

42
66 SYSTEMS ANALYSIS

63 LARGE SPACE STRUCTURES. ORBITAL ASSEMBLY, flEMOTE MANIPULATOR SYSTEM. ROBOT ARMS. ROBOT

CYBERNETICS CONTROL. ROBOTICS, ROBOTS, TELEROBOTICS

N92-28375"# National Aeronautics and Space Administration

Includes feedback and contol theory, artificial intelligence, robotics Langley Research Center, Hampton, VA.

and expert systems. SOFTWARE DESIGN FOR AUTOMATED ASSEMBLY OF

TRUSS STRUCTURES

CATHERINE L. HERSTROM, CAROLYN GRANTHAM, CHERYL

N91-20811*# National Aeronautics and Space Administration. '. ALLEN, WILLIAM R. DOGGETT, and RALPH W. WILL Jun.

Lyndon B. Johnson Space Center, Houston, TX. 1992 47 p

PROCEEDINGS OF THE SECOND JOINT TECHNOLOGY (RTOP 506-43-41-02)

WORKSHOP ON NEURAL NETWORKS AND FUZZY LOGIC, (NASA-TP-3198; L-16983. NAS 1.60:3198) Avail: C/A.SI HC

VOLUME 2 A03/MF A01

ROBERT N. LEA, ed- and JAMES A. VILLARREAL, ed. Feb. AUTOMATIC CONTROL, CONSTRUCTION, ORBITAL

1991 278 p Workshop held in Houston, TX, 10-13 Apr. 1990; ASSEMBLY, SOFTWARE ENGINEERING, SPACE ERECTABLE

sponsored by NASA, Washington, NASA. Johnson Space Center, STRUCTURES, TRUSSES

and Houston Univ.

(NASA-CP-10061-VOL-2; S-624-VOL-2; NAS 1.55:10061-VOL-2)

Avail: CASI HC A13/MF A03

AUTOMATIC CONTROL, CONFERENCES, CONTROLLERS, 65

DECISION MAKING, FUZZY SETS, IMAGE PROCESSING,

NEURAL NETS, PATTERN RECOGNITION, SET THEORY, STATISTICS AND PROBABILITY

SPEECH RECOGNITION

N91-21 Includes data sampling and smoothing; Monte Carlo method; and 778"# National Aeronautics and Space Administration. stochestic processes.

Lyndon B. Johnson Space Center, Houston, TX.

PROCEEDINGS OF THE SECOND JOINT TECHNOLOGY

WORKSHOP ON NEURAL NETWORKS AND FUZZY LOGIC, Ng1-25741*# National Aeronautics and Space Administration.

VOLUME 1 Langley Research Center, Hampton, VA.

ROBERT N. LEA, ed. and JAMES VILLARREAL, ed. Feb. 1991 MODEL REDUCTION BY TRIMMING FOR A CLASS OF

240 p Workshop held in Houston, TX, 10-13 Apr. 1990; sponsored SEMI-MARKOV RELIABILITY MODELS AND THE

by NASA, Washington, NASA. Johnson Space Center, and Houston CORRESPONDING ERROR BOUND

Univ. ALLAN L. WHITE and DANIEL L PALUMBO May 1991 11 p

(NASA-CP-10061-VOL-1; S-624-VOL-1; NAS 1.55:10061-VOL-1) Presented at the Annual Reliability and Maintainability Symposium,

Avail: CASI HC A11/MF A03 1990

CONFERENCES, DECISION MAKING, EXPERT SYSTEMS, (RTOP 505-66-21)

FUZZY SETS, FUZZY SYSTEMS, LOGIC CIRCUITS, NEURAL (NASA-TP-3089; L-16862; NAS 1.60:3089) Avail: CASI HC

NETS, SIGNAL PROCESSING A03/MF A0t

N91-22769"# National Aeronautics and Space Administration. COMPLEX SYSTEMS, ERROR ANALYSIS, MARKOV

Goddard Space Flight Center, Greenbelt, MD. PROCESSES, MATHEMATICAL MODELS, RELIABILITY

THE 1991 GODDARD CONFERENCE ON SPACE ANALYSIS

APPLICATIONS OF ARTIFICIAL INTELLIGENCE

JAMES L. RASH, ed. Washington May 1991 361 p Conference

held in Greenbelt, MD, 13-15 May 1991 66

(NASA-CP-31 10; REPT-91B00064; NAS 1.55:3110) Avail: CASI

HC A16/MF A03 SYSTEMS ANALYSIS

ARTIFICIAL INTELLIGENCE, COMPUTER VISION,

CONFERENCES, CONTROL THEORY, INFORMATION

MANAGEMENT, KNOWLEDGE REPRESENTATION, NEURAL Includes mathematical modeling; network analysis; and operations

NETS, ROBOTICS, SYSTEMS ENGINEERING research.

N92-23356"# National Aeronautics an-' Space Administration.

Goddard Space Flight Center, Greenbelt, MD. N91-18753*# National Aeronautics and Space Administration.

THE 1992 GODDARD CONFERENCE ON SPACE Langley Research Center, Hampton, VA.

APPLICATIONS OF ARTIFICIAL INTELLIGENCE STRUCTURAL FACTORING APPROACH FOR ANALYZING

JAMES L. RASH, ed. Washington 1992 251 p Conference STOCHASTIC NETWORKS

held in Greenbelt, MD, 5-6 May 1992 KELLY J. HAYHURST (National Aeronautics and Space

(RTOP 030-09-01-25) Administration. Langley Research Center, Hampton, VA.) and

(NASA-CP-3141; REPT-92B00045; NAS 1.55:3141) Avail: CASI DOUGLAS R. SHIER (College of William and Mary, Williamsburg,

HC A12/MF A03 VA.) Washington Mar. 1991 24 p

AEROSPACE ENGINEERING, ARTIFICIAL INTELLIGENCE, (RTOP 505-66-21-01)

FAULT lOLERANCE, NEURAL NETS (NASA-TP-3069; L-167ýj4; NAS 1.60:3069) Avail: CASI HC

A03/MF A01

N92-27763*# National Aeronautics and Space Administration. COMMUNICATION NETWORKS, CRITICAL PATH METHOD,

Langley Research Center, Hampton, VA. DATA LINKS, STOCHASTIC PROCESSES

AUTOMATION AND ROBOTICS FOR SPACE-BASED

SYSTEMS, 191I N92-33483 # National Aeronautics and Space Administration

ROBERT L. WILLIAMS, II, ed. May 1992 254 p Workshop Langley Research Center, Hampton, VA.

wis held in Hampton, VA, 10 Dec. 1991 ADVANCED TFCHNIOUES IN RELIABILITY MODEL

(RTOP 595-1 1-22) REPRESENTATION AND SOLUTION

(NASA-CP-10098; NAS 1.55-10098) Avail: CASt HC A12/MF DANIEL L. PALUMBO and DAVID M. NICOL (College of William

A03 and Mary, Williamsburg, VA.) Oct. 1992 18 p

43
70 PHYSICS (GENERAL)

(RTOP 505-64-10-07) 71

(NASA-TP-3242; L-17048; NAS 1.60:3242) Avail: CASI HC

A03/MF A01 ACOUSTICS

COMPUTER SYSTEMS PERFORMANCE, COMPUTERIZED

SIMULATION, DISTRIBUTED PROCESSING. FAILURE ANALYSIS,

FAILURE MODES, FAULT TOLERANCE, FLIGHT CONTROL, Includes sound generation, transmission, and attenuation

MATHEMATICAL MODELS, PARALLEL PROCESSING (COMPUTERS). RELIABILITY ANALYSIS, SOFTWARE TOOLS N911-12315"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, VA

WAKE GEOMETRY EFFECTS ON ROTOR BLADE-VORTEX

INTERACTION NOISE DIRECTIVITY

R. M. MARTIN (National Aeronautics and Space Administration

Langley Research Center. Hampton, VA), MICHAEL A.

MARCOLINI (National Aeronautics and Space Administration

70 Langley Research Center, Hampton. VA.). W R

SPLETTSTOESSER (Flugwissenschaftliche Forschungsanstalt,

Munich (Germany. F.R.).), and K.-J. SCHULTZ (Deutsche

PHYSICS (GENERAL) Forschungsanstalt fuer Luft- und Raumfahrt, Brunswick, Germany,

F.R. ) Nov. 1990 23 p Original contains color illustrations

(RTOP 505-63-51-06)

(NASA-TP-3015; L-16723; NAS 1.60:3015) Avail: CASI HC

A03/MF A01; 6 functional color pages

N91-25755*# Jet Propulsion Lab., California Inst. of Tech., BLADE TIPS, BLADE-VORTEX INTERACTION,

Pasadena. INTERACTIONAL AERODYNAMICS, WAKFS, WIND TUNNEL

THE 22ND ANNUAL PRFCISE TIME AND TIME INTERVAL TESTS

(PTTI) APPLICATIONS AND PLANNING MEETING

RICHARD L. SYDNOR, ed. May 1990 618 p Meeting held in N91-15848"# National Aeronautics and Space Administration.

Vienna, VA, 4-6 Dec. 1990 Lewis Research Center, Cleveland. OH.

(NASA-CP-3116; NAS 1.55:3116; REPT-91B00084; AD-A239372) MONOGRAPH ON PROPAGATION OF SOUND WAVES IN

Avail: CASI HC A99/MF A06 CURVED DUCTS

ATOMIC CLOCKS, FREQUENCY STANDARDS, HYDROGEN WOJCIECH ROSTAFINSKI Jan. 1991 97 p

MASERS, METEOROLOGY, SATELLITE INSTRUMENTS, (RTOP 505-69-61)

TELECOMMUNICATION, TIME, TIME MEASUREMENT (NASA-RP-1248; E-5480; NAS 1.61.1248) Avail: CASI HC

A05/MF A02

After reviewing and evaluating the existing material on sound

propagation in curved ducts without flow, it seems strange that.

N92-13756"# National Aercnautics and Space Administration. except for L, J Rayleigh in 1878, no book on acoustics has treated

Langley Research Center, Hampton, VA. the case of wave motion in bends. This monograph reviews the

BENCHMARK SOLUTIONS FOR THF GALACTIC HEAVY-ION available analytical and experimental material, nearly 30 papers

TRANSPORT EQUATIONS WITH ENkRGY AND SPATIAL published on this subject so far, and concisely summanzes what

COUPLING has been learned about the motion of sound in hard-wall and

BARRY D. GANAPOL (Arizona Univ., Tucson.), LAWRENCE W. acoustically lined cylindrical bends. Author

TOWNSEND (Old Dominion Univ., Norfolk, VA.), STANLEY L.

LAMKIN (Old Dominion Univ., Norfolk, VA.), and JOHN W. N91-16679"# National Aeronautics and Space Administration.

WILSON Washington Oct. 1991 58 p Langley Research Center, Hampton, VA.

(RTOP 199.04-16-11) WIND TURBINE ACOUSTICS

(NASA-TP-3112; L-16909; NAS 1.60:3112) Avail: CASI HC HARVEY H. HUBBARD and KEVIN P. SHEPHERD Dec. 1990

A04/MF A01 49 p Submitted for publication Prepared in cooperation with

GALACTIC COSMIC RAYS, HEAVY IONS, NEUTRONS, NASA, Lewis Research Center and American Society of Mechanical

NUCLEAR INTERACTIONS, RADIATION DOSAGE, RADIATION Engineers

SHIELDING, TRANSPORT THEORY (DE-AIO1-76ET-20320; RTOP 776-33-41)

(NASA-TP-3057: E-5663; DOE/NASA/20320-77: NAS 1.60:3057)

Avail: CASI HC A03/MF A01

ACOUSTICS. DYNAMIC STRUCTURAL ANALYSIS,

N92-33350"# National Aeronautics and Space Administration. HARMONICS, NOISE MEASUREMENT, PREDICTION ANALYSIS

Goddard Space Flight Center, Greenbelt, MD. TECHNIQUES, SOUND WAVES, SPECTRA, WIND SHEAR, WIND

PROCEEDINGS OF THE 23RD ANNUAL PRECISE TIME AND TURBINES

TIME INTERVAL (PTTI) APPLICATIONS AND PLANNING

MEETING N91-16682*# National Aeronautics and Space Administration

RICHARD L. SYDNOR, ed. (Jet Propulsion Lab., California Inst. of Langley fResearch Center, Hampton, VA.

Tech., Pasadena.) et al Washington Jul. 1992 440 p Meeting FOURTH INTERNATIONAL SYMPOSIUM ON LONG-RANGE

held in Pasadena, CA, 3-5 Dec. 1991; sponsored by NASA. SOUND PROPAGATION

Goddard Space Flight Cetner, JPL, Naval Observatory, Space and WILLIAM L. WILLSHIRE, JR.. comp. Washington Dec. 1990

Naval Warfare Systems Command, NRL, Army Electronics 274 p Symposium held in Hampton, VA, 16-17 May 1990;

Technology and Devices Lab., and AFOSR sponsored by NASA, Langley Research Center, Mississippi Univ.,

(NAS5-31000) and Open Univ. of England

(NASA-CP-3159; REPT-92B00083; NAS 1.55:3159) Avail: CASI (RTOP 505-61-11-02)

HC A19/MF A04 (NASA-CP-3101; L-16875; NAS 1.55:3101) Avail: CAS; HC

CONFERENCES, FREQUENCY STANDARDS, NAVIGATION A12/MF A03

SATELLITES, OPTICAL TRACKING, SATELLITE INSTRUMENTS, ACOUSTIC MEASUREMENT, ACOUSTIC PROPAGATION,

TIME MEASUREMENT, TRACKING NETWORKS, TRAPPED AIRCRAFT NOISE, CONFERENCES, NOISE INTENSITY. SOUND

PARTICLES PROPAGATION

44
71 ACOUSTICS

N91-19823"# National Aeronautics and Space Administration. (RTOP 505-63-51-09)

Ames Research Center, Moffett Field, CA. (NASA-TP-3104; L-16850; NAS 1.60:3104) Avail: CASI HC

J-85 JET ENGINE NOISE MEASURED IN THE ONERA Si A04/MF A01

WIND TUNNEL AND EXTRAPOLATED TO FAR FIELD AERODYNAMIC NOISE, AIRCRAFT NOISE, PROPELLER

PAUL T. SODERMAN (National Aeronautics and Space NOISE, PROPELLERS, PSYCHOACOUSTICS. TURBOFAN

Administration. Ames Research Center, Moffett Field, CA.), ALAIN AIRCRAFT, TURBOPROP AIRCRAFT

JULIENNE (Office National d'Etudes et de Recherches

Aerospatiales, Paris, France ), and ADOLPH ATENCIO, JR.

Washington Jan. 1991 181 p

(RTOP 307-50-81) N92-11765"# National Aeronautics and Space Administration.

(NASA-TP-3053; A-89265; NAS 1.60:3053) Avail: CASI HC Langley Research Center, Hampton. VA.

A09/MF A02 A LOUDNESS CALCULATION PROCEDURE APPLIED TO

ANOMALIES, ENGINE NOISE, FAR FIELDS, J-85 ENGINE, SHAPED SONIC BOOMS

SOUND FIELDS, SUBSONIC FLOW, WIND TUNNEL TESTS KEVIN P. SHEPHERD and BRENDA M. SULLIVAN (Lockheed

Engineering and Sciences Co., Hampton, VA) Washington Nov.

N91-19824*# National Aeronautics and Space Administration. 1991 13 p

Ames Research Center, Moffett Field, CA. (RTOP 537-03-21-03)

LARGE-SCALE AEROACOUSTIC RESEARCH FEASIBILITY (NASA-TP-3134; L-16913; NAS 1.60:3134) Avail: CASI HC

AND CONCEPTUAL DESIGN OF TEST-SECTION INSERTS A03/MF A01

FOR THE AMES 80- BY 120-FOOT WIND TUNNEL LOUDNESS, SONIC BOOMS, SUPERSONIC TRANSPORTS

PAUL T. SODERMAN and LARRY E. OLSEN Dec. 1990 50 p

(RTOP 307-50-62-11)

(NASA-TP-3020; A-88007; NAS 1.60:3020) Avail: CASI HC

A03/MF A01 N92-14779"# National Aeronautics and Space Administration.

ACOUSTIC MEASUREMENT, ACOUSTIC PROPERTIES, Langley Research Center, Hampton, VA.

AEROACOUSTICS, AERODYNAMIC CHARACTERISTICS, AEROACOUSTICS OF FLIGHT VEHICLES: THEORY AND

INSERTS, INSTALLING, LININGS, WALLS, WEDGES, WIND PRACTICE. VOLUME 2: NOISE CONTROL

TUNNEL APPARATUS, WIND TUNNEL TESTS HARVEY H. HUBBARD, ed. Washington Aug. 1991 443 p

Sponsored in cooperation with the Army Aviation Systems

N91-21828"# National Aeronautics and Space Administration. Command

Ames Research Center, Moffett Field, CA. (F33615-84-C-3202; RTOP 535-03-11-03)

ACOUSTIC AND AERODYNAMIC STUDY OF A (NASA-RP-1258-VOL-2; L-16926-VOL-2; NAS 1.61:1258-VOL-2;

PUSHER-PROPELLER AIRCRAFT MODEL WRDC-TR-90-3052-VOL-2) Avail: CASI HC A19/MF A04

PAUL T. SODERMAN and W. CLIFTON HORNE Washington Flight vehicles and the underlying concepts of noise generation,

Sep. 1990 67 p noise propagation, noise prediction, and noise control ae studied.

(RTOP 505-61-11) This volume includes those chapters that relate to flight vehicle

(NASA-TP-3040; A-89038; NAS 1.60:3040) Avail: CASt HC noise control and operations: human response to aircraft noise;

A04/MF A01 atmospheric propagation; theoretical models for duct acoustic

AEROACOUSTICS, AIRCRAFT MODELS, AIRCRAFT WAKES, propagation and radiation; design and performance of duct acoustic

INTERACTIONAL AERODYNAMICS, PROPELLER BLADES, treatment; jet noise suppression; interior noise; flyover noise

PROPELLER NOISE measurement and prediction; and quiet aircraft design and

operational characteristics. For individual titles, see N92-14780

N92-10598"# National Aeronautics and Space Administration. through N92-14787.

Langley Research Center, Hampton, VA.

AEROACOUSTICS OF FLIGHT VEHICLES: THEORY AND

PRACTICE. VOLUME 1: NOISE SOURCES

HARVEY H. HUBBARD, ed. Washington Aug. 1991 601 p N92-20479*# National Aeronautics and Space Administration.

Sponsored in cooperation with Wright Research and Development Langley Research Center, Hampton, VA.

Center and Army Aviation Systems Command ANNOYANCE CAUSED BY AIRCRAFT EN ROUTE NOISE

(F33615-84-C-3202; RTOP 535-03-11-03) DAVID A. MCCURDY Mar. 1992 40 p

(NASA-RP-1258-VOL-1; L-16926-VOL-1; NAS 1.61:1258-VOL-1; (RTOP 535-03-11-03)

WRDC-TR-90-3052-VOL-1; AD-A241141) Avail: CASI HC (NASA-TP-3165; L-16975; NAS 1.60:3165) Avail: CASI HC

A99/MF A06 A03/MF A01

Methodology recommended to evaluate aeroacoustic related AIRCRAFT NOISE. ANECHOIC CHAMBERS. COMMERCIAL

problems is provided, and approaches to their solutions are AIRCRAFT, JUDGMENTS, PROP-FAN TECHNOLOGY, TAKEOFF,

suggested without extensive tables, nomographs, and derivations. TURBOFAN AIRCRAFT, TURBOPROP AIRCRAFT

Orientation is toward flight vehicles and emphasis is on underlying

physical concepts. Theoretical, experimental, and applied aspects are covered, including the main formulations and comparisons of

theory and experiment. The topics covered include: propeller and N92-32948 # National Aeronautics and Space Administration.

propfan noise, rotor noise, turbomachinery noise, jet noise classical Langley Research Center, Hampton, VA.

theory and experiments, noise from turbulent shear flows, jet noise FOURTH AIRCRAFT INTERIOR NOISE WORKSHOP

generated by large-scale coherent motion, airframe noise, DAVID G. STEPHENS, comp. Jul. 1992 335 p Workshop

propulsive lift noise, combustion and core noise, and sonic booms. held in Friedrichshafen, Fed. Republic of Germany, 19-20 May For individual titles, see N92-10599 through N92-10608. 1992; sponsored by NASA, Society of Automotive Engineers, and

the German Aerospace Research Establishment

N92-11758"# National Aeronautics and Space Administration. (RTOP 535-03-11-03)

Langley Research Center, Hampton, VA. (NASA-CP-10103; NAS 1.55:10103) Avail: CASI HC A15/MF

ANNOYANCE CAUSED BY ADVANCED TURBOPROP A03

AIRCRAFT FLYOVER NOISE: COMPARISON OF DIFFERENT AEROACOUSTICS, AERODYNAMIC NOISE, AIRCRAFT

PROPELLER CONFIGURATIONS NOISE, CONFERENCES, NOISE MEASUREMENT, NOISE

DAVID A. MCCURDY Washington Oct. 1991 69 p PREDICTION, NOISE REDUCTION

45
73 NUCLEAR AND HIGH-ENERGY PHYSICS

73 76

NUCLEAR AND HIGH-ENERGY PHYSICS SOLID-STATE PHYSICS

Includes elementary and nuclear particles; and reactor theory. Includes superconductivity.

N91-13985*# National Aeronautics and Space Administration. N92-10677"# National Aeronautics and Space Administration.

Langley Research Center, Hampton, VA. Langley Research Center. Hampton, VA.

INCLUSIVE INELASTIC SCATTERING OF HEAVY IONS AND POSITRON LIFETIME MEASUREMENTS IN CHIRAL NEMATIC

NUCLEAR CORRELATIONS LIQUID CRYSTALS

FRANCIS A. CUCINOTTA (Rockwell International Corp., Houston, JAG J. SINGH (Hampton Univ., VA.). ABE EFTEKHARI (Hampton TX.), LAWRENCE W. TOWNSEND (National Aeronautics and Inst., VA.), and DEVENDRA S. PARMAR Oct. 1991 14 p Space Administration. Langley Research Center, Hamnton, VA.), (NASA-TP-3122; L-16948; NAS 1.60:3122) Avail: CASI HC

JOHN W. WILSON (National Aeronautics and Space Administration. A03/MF A01

Langley Research Center, Hampton, VA.), and GOVIND S. LIQUID CRYSTALS, OPTICAL ACTIVITY, POSITRON

KHANDELWAL (Old Dominion Univ., Norfolk, VA.) Washington ANNIHILATION, POSITRONS, TIME MEASUREMENT

Nov. 1990 22 p

(RTOP 199-04-16-11)

(NASA-TP-3026; L-16793; NAS 1.60:3026) Avail: CASI HC 81

A03/MF A01

ANGULAR DISTRIBUTION, HEAVY IONS, INELASTIC

SCATTERING, ION SCATTERING, IONIC COLLISIONS, ADMINISTRATION AND MANAGEMENT

MOMENTUM TRANSFER, RELATIVISTIC PARTICLES

Includes management planning and research.

74 N91-11591"# National Aeronautics and Space Administration.

John F. Kennedy Space Center, Cocoa Beach, FL.

OPTICS TWENTY-SECOND ANNUAL NASA SUPPLY AND EQUIPMENT

MANAGEMENT CONFERENCE

Includes light phenomena; and optical devices. 1989 384 p Conference held in Cocoa Beach, FL, 5-7 Dec.

1989

(NASA-CP-10042; NAS 1.55:10042) Avail: CASI HC A17/MF

N92-22045"# National Aeronautics and Space Administration. A03

Goddard Space Flight Center, Greenbelt, MD. CONFERENCES, INVENTORIES, LOGISTICS, MANAGEMENT

WORKSHOP ON SQUEEZED STATES AND UNCERTAINTY METHODS, PROJECT MANAGEMENT, REGULATIONS, SAFETY

RELATICNS N91-13347"# National Aeronautics and Space Administration,

DAESOO HAN, ed. (Maryland Univ., College Park.), Y. S. KIM, Washington, DC.

ed., and W. W. ZACHARY, ed. (Howard Univ., Washington, DC.) ISSUES IN NASA PROGRAM AND PROJECT MANAGEMENT

Washington Feb. 1992 385 p Workshop held in College FHANCIS T. HOBAN, ed. Jul. 1990 57 p Park, MD, 28-30 Mar. 1991 (NASA-SP-6101(03); NAS 1.21:6101(03)) Avail: CASI HO

(NASA-CP-3135; HO A17/MF A04 REPT-92B00024; NAS 1.15:3135) Avail: CASI A04/MF A4M A01 0

TO (PHYICS) G P This volume is the third in an ongoing series on aerospace CONFERENCES, FIELD THEORY (PHYSICS), GROUP project management at NASA. Articles in this volume cover the THEORY, HEISENBERG THEORY, LASERS, POINCARE attitude of the program manager, program control and performance PROBLEM, QUANTUM MECHANICS, QUANTUM OPTICS, measurement, risk management, cost plus award fee contracting,

QUANTUM THEORY, SQUEEZED STATES (QUANTUM lessons learned from the development of the Far Infrared Absolute

THEORY) Spectrometer (FIRAS), small projects management, and age

distribution of NASA scientists and engineers. A section on resources for NASA managers rounds out the publication. 75 Author

N91-24936" National Aeronautics and Space Administration.

PLASMA PHYSICS Washington, DC.

MANAGEMENT: A BIBLIOGRAPHY FOR NASA MANAGERS

Includes magnetohydrodynamics and plasma fusion. Mar. 1991 195 p

(NASA-SP-7500(25); NAS 1.21:7500(25)) Avail: CASI HC A09

This bibliography lists 731 reports, articles and other documents

N91-17713*# National Aeronautics and Space Administration. introduced into the NASA Scientific and Technical Information

Marshall Space Flight Center, Huntsville, AL. System in 1990. Items are selected and grouped according to

CURRENT COLLECTION FROM SPACE PLASMAS their usefulness to the manager as manager. Citations are grouped

NAGENDRA SINGH, ed. (Alabama Univ., Huntsville.), K. H. into ten subject categories: human factors and personnel issues; WRIGHT, JR.. ed. (Alabama Univ., Huntsville.), and NOBLE H. management theory and techniques; industrial management and

STONE, ed. Washington Dec. 1990 368 p Workshop held manufacturing; robotics and expert systems; computers and

in Huntsville, AL, 24-25 Apr. 1989; sponsored by NASA. Marshall information management; research and development; economics,

Space Flight Center and Alabama Univ. costs and markets: logistics and operations management: reliability

(NASA-CP-3089; M-644; NAS 1.55:3089) Avail: CASI HC and quality control; and legality, legislation, and policy. Author

A16/MF A03

CONFERENCES, EARTH ORBITS, PLASMA PHYSICS, N91-28026"# National Aeronautics and Space Administration,

PLASMA PROBES, SPACE CHARGE, SPACE PLASMAS, Washington, DC.

SPACECRAFT CHARGING ISSUES IN NASA PROGRAM AND PROJECT MANAGEMENT

46
82 DOCUMENTATION AND INFORMATION SCIENCE

FRANCIS T. HOBAN, ed. 1991 62 p the NASA Thesaurus includes the Hierarchical Listing (Part 1),

(NASA-SP-6101(04); NAS 1.21:6101(04)) Avail: CASI HC Access Vocabulary (Part 2), Definitions (Part 3). and Changes

A04/MF A01 (Part 4). The semiannual supplement gives complete hierarchies

This volume is the third in an ongoing series on aerospace and accepted upper/lowercase forms for new terms. Author

project management at NASA. Articles in this volume cover ".,

attitude of the program manager, program control and performance N91-13374*# National Aeronautics and Space Administration.

measurement, risk management, cost plus award fee contracting, Washington, DC.

lessons learned from the development of the Far Infrared Absolute NASA SCIENTIFIC AND TECHNICAL PUBLICATIONS: A

Spectrometer (FIRAS), small projects management, and age CATALOG OF SPECIAL PUBLICATIONS, REFERENCE

distribution of NASA scientists and engineers. A section on PUBLICATIONS, CONFERENCE PUBLICATIONS, AND

resources for NASA managers rounds out the publication, TECHNICAL PAPERS, 1989

Author Feb. 1990 61 p

(NASA-SP-7063(04); NAS 1.21:7063(04)) Avail: NTIS HC free as

N92-22665" National Aeronautics and Space Administration, PR-869; NASA Scientific and Technical Information Facility, BWI

Washington, DC. Airport, MD free

CONTINUOUS rIPROVEMENT: A BIBLIOGRAPHY WITH This catalog lists 190 citations of all NASA Special Publications,

INDEXES, 1989-1991 NASA Reference Publications, NASA Conference Publications, and

Feb. 1992 59 p NASA Technical Papers that were entered into the NASA scientific

(NASA-SP-7097; NAS 1.21:7097) Avail: CASI HC A04 and technical information database during accession year 1989.

This bibliography contains 198 annotated references to reports The entries are grouped by subject category IndeAes of subject

and journal articles entered into the NASA Scientific and Technical terms, personal authors, and NASA report numbers are provided.

Information Data base during 1989 to 1991. Author Author

N92-27080" National Aeronautics and Space Administration, N91-17833" National Aeronautics and Space Administration,

Washington, DC. Washington, DC.

MANAGEMENT: A BIBLIOGRAPHY FOR NASA MANAGERS NASA PATENT ABSTRACTS BIBLIOGRAPHY: A CONTINUING

Mar. 1992 168 p BIBLIOGRAPHY. SECTION 1: ABSTRACTS (SUPPLEMENT 38)

(NASA.SP.7500(26): NAS 1.21:7500(26)) Avail: CASI HC A08 Jan. 1991 64 p

This bibliography lists 630 reports, articles and other documents (NASA-SP-7039(38)-SECT-1; NAS 1.21:7039(38)-SECT-I) Avail:

introduced into the NASA Scientific and Technical Information CASI HC A04

System in 1991. Items are selected and grouped according to Abstracts are provided for 132 patents and patent applications

their usefulness to the manager as manager. Citations are grouped entered into the NASA scientific and technical information system

into ten subject categories: human factors and personnel issues; during the period July 1990 through December 1990 Each entry

management theory and techniques; industrial management and consists of a citation, an abstract, and in most cases, a key

manufacturing; robotics and expert systems; computers and illustration selected from the patent or patent application. Author

information management; research and development; economics,

costs and markets; logistics anri operations management; reliability N91-17834" National Aeronautics and Space Administration,

and quality control; and legality, legislation, and policy. Author Washington, DC.

NASA PATENT ABSTRACTS BIBLIOGRAPHY: A CONTINUING

N92-27609*# National Aeronautics and Space Administration, BIBLIOGRAPHY. SECTION 2: INDEXES (SUPPLEMENT 38)

Washington, DC. Jan. 1991 537 p

ISSUES IN NASA PROGRAM AND PROJECT MANAGEMENT (NASA-SP-7039(38)-SECT-2; NAS 1.21:7039(38)-SECT-2) Avail:

FRANCIS T. HOBAN, ed. 1992 58 p CASI HC A23

(NASA-SP.6101(05); NAS 1.21:6101(05)) Avail: CASI HC A subject index is provided for over 4900 patents and patent

A04/MF A01 applications for the period May 1969 through December 1990.

This volume is the fifth in an ongoing series on aerospace Additional indexes list personal authors, corporate authors, contract

project management at NASA. Articles in this volume cover: an numbers, NASA case numbers. U.S. patent class numbers. U.S.

overview of the project cycle; SE&W management for manned space patent numbers, and NASA accession numbers, Author

flight programs; shared experiences from NASA Programs and

Projects - 1975; cost control for Mariner Venus/Mercury 1973; N91-19962"# National Aeronautics and Space Administration,

and the Space Shuttle - a balancing of design and politics. A Washington, DC.

section on resources for NASA managers rounds out the NASA THESAURUS SUPPLEMENT: A FOUR PART

publication. Author CUMULATIVE SUPPLEMENT TO THE 1988 EDITION OF THE

NASA THESAURUS (SUPPLEMENT 5) Semiannual Report

Mar. 1991 49 p

82 (NASA-SP-7064-SUPPL-5; NAS 1.21:7064-SUPPL-5) Avail: CASI

HC A03/MF A01

The four-part cumulative supplement to the 1988 edition of

DOCUMENTATION AND INFORMATION SCIENCE the NASA Thesaurus includes the Hierarchical Listing (Part 1),

Access Vocabulary (Part 2). Definitions (Part 3), and Changes

Includes information management; information storage and retrieval (Part 4). The semiannual supplement gives complete hierarchies

technology; technical writing; graphic arts; and micrography. and accepted upper/lowercase forms for new terms. Author

N91-24939*# National Aeronautics and Space Administration,

N91-10604"# National Aeronautics and Space Administration, Washington, DC.

Washington, DC. NASA SCIENTIFIC AND TECHNICAL PUBLICATIONS: A

NASA THESAURUS SUPPLEMENT: A FOUR PART CATALOG OF SPECIAL PUBLICATIONS. REFERENCE

CUMULATIVE SUPPLEMENT TO THE 1988 EDITION OF THE PUBLICATIONS, CONFERENCE PUBLICATIONS, AND

NASA THESAURUS (SUPPLEMENT 4) Semiannual Report TECHNICAL PAPERS, 1987-1990

Sep. 1990 26 p Feb. 1991 174 p

(NASA-SP-7064-SUPPL-4; NAS 1.21:7064-SUPPL-4) Avail: CASI (NASA-SP-7063(05); NAS 1.21:7063(05); AD-A235956) Avail:

HC A03/MF A01 NTIS HC free as PR-890; NASA Center for AeroSpace

The four-part cumulative supplement to the 1988 edition of Information, BWI Airport, MD free

47
82 DOCUMENTATION AND INFORMATION SCIENCE

This catalog lists 783 citations of all NASA Special Publications, N92-31455° National Aeronautics and Space Administration,

NASA Reference Publications, NASA Conference Publications, and Washington, DC.

NASA Technical Papers that were entered into NASA Scientific NASA PATENT ABSTRACTS BIBLIOGRAPHY: A CONTINUING

and Technical Information Database during the year's 1987 through BIBLIOGRAPHY. SECTION 2: INDEXES (SUPPLEMENT 41)

1990. The entries are grouped by subject category. Indexes ot Jul. 1992 578 p

subject terms, personal authors, and NASA report numbers are (NASA-SP-7039(41)-SECT-2; NAS 1.21:7039(41)-SECT.2) Avail

provided. Author CASI HC A25

A subject index is provided for over 5200 patents and patent

N91-27009*# National Aeronautics and Space Administration. applications for the period May 1969 through June 1992, Additional

Goddard Space Flight Center, Greenbelt, MD. indexes list personal authors, corporate authors, contract numbers,

PROCEEDINGS OF THE SECOND ANNUAL NASA SCIENCE NASA case numbers, U.S. patent class numbers, U-S. patent

INTERNET USER WORKING GROUP CONFERENCE numbers, and NASA accession numbers. Author

LENORE A. JACKSON, ed. (ST Systems Corp., Lanham, MD.)

and J. PATRICK GARY, ed. Washington May 1991 429 p

Conference held in San Mateo, CA, 11-14 Feb. 1991 88

(RTOP 656-63-00)

(NASA-CP-3117; REPT-91800089; NAS 1.55:3117) Avail: CASI

HC A19/MF A04 SPACE SCIENCES (GENERAL)

COMPUTER INFORMATION SECURITY, COMPUTER

NETWORKS, CONFERENCES, MANAGEMENT METHODS,

POLICIES, SOFTWARE ENGINEERING

N91-28042" National Aeronautics and Space Administration, N91-12401"# National Aeronautics and Space Administration.

Washington, DC. Marshall Space Flight Center, Huntsville, AL.

NASA PATENT ABSTRACTS BIBLIOGRAPHY: A CONTINUING MEASUREMENT AND CHARACTERIZATION OF THE

BIBLIOGRAPHY. SECTION 1: ABSTRACTS (SUPPLEMENT 39) ACCELERATION ENVIRONMENT ON BOARD THE SPACE

Jul. 1991 63 p STATION

(NASA-SP-7039(39)-SECT-1; NAS 1.21:7039(39)-SECT-I) Avail: CHARLES R. BAUGHER, ed. Washington Aug. 1990 669 p

CASI HC A04 Workshop held in Guntersville, AL, 11-14 Aug. 1986; sponsored

Abstracts are provided for 154 patents and patent applications by Teledyne Brown Engineering

entered into the NASA scientific and technical information systems (NAS8-36122)

during the period Jan. 1991 through Jun. 1991. Each entry consists (NASA-CP-3088; M-639; NAS 1-55:3088) Avail: CASI HC

of a citation, an abstract, and in most cases, a key illustration A99/MF A06

selected from the patent or patent application. Author ACCELERATION (PHYSICSý, ACCELEROMETERS.

CONFERENCES. REDUCED GRAVITY, SPACE COMMERN91-29088 National Aeronautics and Space Administration, CIALIZATION, SPACE PROCESSING, SPACE STATIONS.

Washington, DC. SPACECRAFT ENVIRONMENTS, SPACELAB. SPACELAB

NASA PATENT ABSTRACTS BIBLIOGRAPHY: A CONTINUING PAYLOADS

BIBLIOGRAPHY. SECTION 2: INDEXES (SUPPLEMENT 39)

Jul. 1991 553 p N91-14897"# National Aeronautics and Space Administration.

(NASA-SP-7039(39)-SECT-2; NAS 1.21:7039(39)-SECT-2) Avail: Ames Research Center, Moffett Field, CA.

CASI HC A24 INTERSTELLAR DUST: CONTRIBUTED PAPERS

A subject index is provided for over 5000 patents and patent ALEXANDER G_ G. M. TIELENS, ed. and LOUIS J.

applications for the period May 1969 through June 1991. Additional ALLAMANDOLA, ed. Dec. 1989 512 p Symposium held in

indexes list personal authors, corporate authors, contract numbers, Santa Clara, CA, 26-30 Jul. 1988; sponsored by NASA. Ames

NASA case numbers, U.S. patent class numbers, U.S. patent Research Center, NSF, and the International Astronomical Union

numbers, and NASA accession numbers. Author (NASA-CP-3036; A-89050; NAS 1.55:3036) Avail: CASI HC

A22/MF A04

N92-22508° National Aeronautics and Space Administration, ASTRONOMICAL MODELS, CONFERENCES, COSMIC DUST.

Washington, DC. INFRARED ASTRONOMY, INFRARED RADI,\TION,

NASA PATENT ABSTRACTS BIBLIOGRAPHY: A CONTINUING INTERSTELLAR EXTINCTION, INTERSTELLAR MATTER,

BIBLIOGRAPHY. SECTION 1: ABSTRACTS (SUPPLEMENT 40) MOLECULAR CLOUDS, STAR FORMATION

Jan. 1992 81 p

(NASA-SP-7039(40)-SECT-1; NAS 1.21:7039(40)-SECT-I) Avail: N91-15930*# National Aeronautics and Space Administration.

CASI HC A05 Marshall Space Flight Center, Huntsville, AL.

Abstracts are provided for 181 patents and patent applications SPACE STATION FREEDOM TOXIC AND REACTIVE

entered into the NASA scientific and technical information system MATERIALS HANDLING

during the period July 1991 through December 1991. Each entry CHARLES R. BAUGHER, ed. Washington Jul. 1990 703 p

consists of a citation, an abstract, and in most cases, a key Workshop held in Huntsville, AL. 29 Nov. - 1 Dec. 1988; sponsored

illustration selected from the patent or patent application. Author by Teledyne Brown Engineering

(NAS8-36122)

N92-27081 National Aeronautics and Space Administration, (NASA-CP-3085; M-638; NAS 1.55:3085) Avail: CASI HC

Washington, DC. A99/MF A06

NASA PATENT ABSTRACTS BIBLIOGRAPHY: A CONTINUING CONFERENCES, HAZARDS, MATERIALS HANDLING,

BIBLIOGRAPHY. SECTION 2: INDEXES (SUPPLEMENT 40) MICROGRAVITY APPLICATIONS, SPACE PROCESSING. SPACE

Jan. 1992 564 p STATION FREEDOM, SPACE STATION PAYLOADS, TOXICITY

(NASA-SP-7039(40)-SECT-2; NAS 1.21:7039(40)-SECT-2) Avail:

CASI HC A24 N92-11930"# National Aeronautics and Space Administration.

A subject index is provided for over 5100 patents and patent Lyndon B. Johnson Space Center, Houston, TX.

applications for the period May 1969 through December 1991. THE MICROGRAVITY ENVIRONMENT OF THE SPACE

Additional indexes list personal authors, corporate authors, contract SHUTTLE COLUMBIA MIDDECK DURING STS-32

numbers, NASA case numbers, U.S. patent class numbers, U.S. BONNIE J. DUNBAR, DONALD A. THOMAS, and JEFF N.

patent numbers, and NASA accession numbers. Author SCHOESS (Honeywell, Inc., Bloomington, MN.) Washington Nov.

48
91 LUNAR AND PLANETARY EXPLORATION

1991 59 p 90

(NASA-TP-3140; S-640; NAS 1.60:3140) Avail: CASI HC

A04/MF A01 ASTROPHYSICS

ACCELERATION (PHYSICS), ACCELEROMETERS, COLUMBIA

(ORBITER), REDUCED GRAVITY, SPACE SHUTTLE PAYLOADS,

SPACEBORNE EXPERIMENTS Includes cosmology, celestial mechanics; space plasmas; and

interstellar and interplanetary gases and dust.

N91-14100"# National Aeronautics and Space Administration.

Ames Research Center, Moffett Field, CA.

N92-11931"# National Aeronautics and Space Administration. THE INTERSTELLAR MEDIUM IN EXTERNAL GALAXIES:

Lyndon B. Johnson Space Center, Houston, TX. SUMMARIES OF CONTRIBUTED PAPERS

THE MICROGRAVITY ENVIRONMENT OF THE SPACE DAVID J. HOLLENBACH, ed. (National Aeronautics and Space

SHUTTLE COLUMBIA PAYLOAD BAY DURING STS-32 Administration. Ames Research Center, Moffett Field, CA.) and

BONIE J. DUNBAR, ROBERT L. GIESECKE, and DONALD A. HARLEY A. THRONSON, JR., ed. (Wyoming Univ., Laramie.)

THuMAS Washington Nov. 1991 51 p Washington Jul. 1990 431 p Second conference held in the

(NASA-TP-3141; S-641; NAS 1.60:3141) Avail: CASI HC Grand Teton National Park, WY, 3-7 Jul. 1989; sponsored by NASA.

A04/MF A01 NSF, and Wyoming Univ.

ACCELERATION (PHYSICS), ACCELEROMETERS, BAYS (RTOP 188-44-53)

(STRUCTURAL UNITS), COLUMBIA (ORBITER), GRAVITATIONAL (NASA-CP-3084; A-90075; NAS 1.55:3084) Avail: CASI HC

EFFECTS, REDUCED GRAVITY, SPACE SHUTTLE MISSION 61-C, A19/MF A04

SPACE SHUTTLE PAYLOADS, SPACEBORNE EXPERIMENTS CARBON MONOXIDE, CONFERENCES, COSMIC DUST,

GALAXIES, INTERSTELLAR MATTER, RADIO ASTRONOMY,

RADIO EMISSION, STAR FORMATION

N91-16858"# National Aeronautics and Space Administration.

N92-33478"# National Aeronautics and Space Administration. Marshall Space Flight Center, Huntsville, AL.

Lyndon B. Johnson Space Center, Houston, TX. PAIRED AND INTERACTING GALAXIES: INTERNATIONAL

ORBITAL DEBRIS: TECHNICAL ISSUES AND FUTURE ASTRONOMICAL UNION COLLOQUIUM NO. 124

DIRECTIONS JACK W. SULENTIC, ed. (Alabama Univ., Tuscaloosa.), WILLIAM

ANDREW POTTER, ed. Sep. 1992 316 p Proceedings held C. KEEL, ed. (Alabama Univ., Tuscaloosa.), and C. M. TELESCO,

in Baltimore, MD, 16-19 Apr. 1990; sponsored by AIAA and DOD ed. Nov. 1990 738 p Colloquium held in Tusczloosa, AL, 4-7

(NASA-CP-10077; S-637; NAS 1.55:10077) Avail: CASI HC Dec. 1989; sponsored by NASA, the International Astronomical

A14/MF A03 Union, and Alabama Univ., Tuscaloosa

COLLISIONS, CONFERENCES, EARTH ORBITAL (NASA-CP-3098; M-652; NAS 1-55:3098) Avail: CASt HC

ENVIRONMENTS, HYPERVELOCITY IMPACT, IMPACT DAMAGE, A99/MF A06

SPACE DEBRIS, SPACECRAFT SHIELDING ACTIVE GALACTIC NUCLEI, ASTRONOMY, COLLISIONS, CONFERENCES, GALACTIC CLUSTERS, GALACTIC

STRUCTURE, INTERACTING GALAXIES, RADIO ASTRONOMY,

STAR FORMATION, STARBURST GALAXIES

N92-21874*# National Aeronautics and Space Administration.

Goddard Space Flight Center, Greenbelt, MD.

THE COMPTON OBSERVATORY SCIENCE WORKSHOP

CHRIS R. SHRADER, ed. (Computer Sciences Corp., Beltsville,

MD.), NEIL GEHRELS, ed., and BRIAN DENNIS, ed.

Washington Feb. 1992 552 p Workshop held in Annapolis, 89 MD, 23-25 Sep. 1991

(NASA-CP-3137; REPT-92B00035; NAS 1.55:3137) Avail: CASI

ASTRONOMY HC A24/MF A04

ASTRONOMICAL SPECTROSCOPY, ASTROPHYSICS,

Includes radio, gamma-ray, and infrared astronomy; and CONFERENCES, GAMMA RAY ASTRONOMY, GAMMA RAY

BURSTS, GAMMA RAY OBSERVATORY, GAMMA RAY

astrometry. TELESCOPES

N91-32006*# National Aeronautics and Space Administration.

Marshall Space Flight Center, Huntsville, AL. 91

DEVELOPMENT OF THE BURST AND TRANSIENT SOURCE

EXPERIMENT (BATSE)

J. M. HORACK Sep. 1991 322 p LUNAR AND PLANETARY EXPLORATION

(NASA-RP-1268; M-668; NAS 1.61-1268) Avail: CASI HC

A14/MF A03 Includes planetology; and manned and unmanned flights.

The Burst and Transient Source Experiment (BATSE), one of

four instruments on the Gamma Ray Observatory, consists of eight

identical detector modules mounted on the corners of the N91-24965* National Aeronautics And Space Administration,

spacecraft. Developed at MSFC, BATSE is the most sensitive Washington, DC.

gamma ray burst detector flown to date. Details of the assembly INTERNATIONAL EXPLORATION OF MARS. A SPECIAL

and test phase of the flight hardware development are presented. BIBLIOGRAPHY

Results and descriptions of calibrations performed at MSFC, TRW, Jun. 1991 66 p

and KSC are documented extensively. With the presentation of (NASA-SP-7091; NAS 1.21:7091) Avail: CASI HC A04

each calibration results, the reader is provided with the means to This bibliography lists 173 reports, articles, and other documents

access raw calibration data for further review or analysis. Author introduced into the NASA Scientific and Technical Information

49
91 LUNAR AND PLANETARY EXPLORATION

Database on the exploration of Mars. Historical references are 92

cited for background. The bibliography was created for the 1991

session of the International Space University. Author SOLAR PHYSICS

Includes solar activity, solar flares, solar radiation and sunspots.

N91-27057*# National Aeronautics and Space Administration. N91-12456"# National Aeronautics and Space Administration

Ames Research Center, Moffett Field, CA. Goddard Space Flight Center, Greenbelt, MD.

SAND AND DUST ON MARS CLIMATE IMPACT OF SOLAR VARIABILITY

RONALD GREELEY (Arizona State Univ., Tempe.) and ROBERT KENNETH H. SCHATTEN, ed. and ALBERT ARKING, ed

M. HABERLE May 1991 65 p Workshop held in Tempe, AZ, Washington Aug. 1990 367 p Conference held in Greenbelt,

4-5 Feb. 1991 MD, 24-27 Apr. 1990

(NCC2-346; RTOP 151-01-60-03) (NASA-CP-3086; REPT-90B00129; NAS 1.55:3086) Avail: CASI

(NASA-CP-10074; A-91130; NAS 1.55:10074) Avail: CASI HC HC A16/MF A01

A04/MF A01 CLIMATE, CLIMATE CHANGE, CLIMATOLOGY,

CHEMICAL PROPERTIES, DUST, DUST STORMS, CONFERENCES, ENVIRONMENT EFFECTS, GREENHOUSE

ELECTROSTATICS, MARS SURFACE, MINERALOGY, SANDS, EFFECT, LUMINOSITY, MAN ENVIRONMENT INTERACTIONS,

WIND TUNNEL TESTS SOLAR ACTIVITY EFFECTS, SOLAR RADIATION, SUN

N91-31061V# National Aeronautics and Space Administration.

Lyndon B. Johnson Space Center, Houston, TX.

ANALYSES OF RISKS ASSOCIATED WITH RADIATION

EXPOSURE FROM PAST MAJOR SOLAR PARTICLE EVENTS

N92-28345*# National Aeronautics and Space Administration, MARK D. WEYLAND (Rockwell International Corp., Houston, TX.),

Washington, DC. WILLIAM ATWELL (Rockwell International Corp., Houston, TX.),

PLANETARY GEOSCIENCES, 1989-1990 FRANCIS A. CUCINOTTA (National Aeronautics and Space

MARIA T. ZUBER, ed. (Natioral Aeronautics and Space Administration. Langley Research Center, Hampton, VA.), JOHN

Administration. Goddard Space Flight Center, Greenbelt, MD.), W. WILSON (National Ae-onautics and Space Administration.

ODETTE B. JAMES, ed. (Geological Survey, Washington, DC.), Langley Research Center, Hampton, VA.), and ALVA C. HARDY

JONATHAN I. LUNINE, ed. (Arizona Univ., Tucson.), GLENN J. Aug. 1991 37 p

MACPHE3SON, ed. (Smithsonian Institution, Washington, DC.), and (NASA-TP-3137; S-639; NAS 1.60:3137) Avail: CASI HC

ROGER J. PHILLIPS, ed. (Southern Methodist Univ., Dallas, TX.) A03/MF A01

1992 81 p LIMITED REPRODUCIBILITY: More than 20% of AEROSPACE ENVIRONMENTS, COMPUTERIZED SIMUthis document may be affected by color photographs Original LATION. HEMATOPOIETIC SYSTEM, RADIATION DOSAGE.

contains color illustrations RADIATION HAZARDS. RADIATION SHIELDING, SOLAR

(NASA-SP-508; NAS 1.21:508; LC-91-33408; CORPUSCULAR RADIATION

ISBN-0-16-036173-7)

NASA's Planetary Geosciences Programs (the Planetary

Geology and Geophysics and the Planetary Material and 93

Geochemistry Programs) provide support and an organizational

framework for scientific research on solid bodies of the solar

system. These research and analysis programs support scientific SPACE RADIATION

research aimed at increasing our understanding of the physical,

chemical, and dynamic nature of the solid bodies of the solar Includes cosmic radiation; and inner and outer earth's radiation

system: the Moon, the terrestrial planets, the satellites of the outer belts.

planets, the rings, the asteroids, and the comets. This research is

conducted using a variety of methods: laboratory experiments,

theoretical approaches, data analysis, and Earth analog techniques. N91-16981"# National Aeronautics and Space Administration.

Through research supported by these programs, we are expanding Langley Research Center, Hampton, VA.

our understanding of the origin and evolution of the solar system. CELLULAR TRACK MODEL OF BIOLOGICAL DAMAGE TO

This document is intended to provide an overview of the more MAMMALIAN CELL CULTURES FROM GALACTIC COSMIC

significant scientific findings and discoveries made this year by RAYS

scientists supported by the Planetary Geosciences Program. To a FRANCIS A. CUCINOTTA (Rockwell International Corp, Houston,

large degree, these results and discoveries are the measure of TX.), ROBERT KATZ (Nebraska Univ., Lincoln.). JOHN W. WILSON

success of the programs. Author (National Aeronautics and Space Administration. Langley Research

Center, Hampton, VA.), LAWRENCE W. TOWNSEND (National

Aeronautics and Space Administration. Langley Research Center,

Hampton, VA.), JOHN E. NEALY (National Aeronautics and Space

Administration. Langley Research Center, Hampton, VA.), and

JUDY L. SHINN Washington Feb. 1991 13 p

N92-30302"# National Aeronautics and Space Administration. (RTOP 199-04-16-11)

Lewis Research Center, Cleveland, OH. (NASA-TP-3055; L-16831; NAS 1.60:3055) Avail: CASI HC

ELECTRICAL AND CHEMICAL INTERACTIONS AT MARS A03/MF A01

WORKSHOP, PART 1 Final Report BIOLOGICAL MODELS (MATHEMATICS), CELLS (BIOLOGY),

1992 31 p Workshop held in Cleveland, OH, 19-20 Nov. 1991 DAMAGE ASSESSMENT, GALACTIC COSMIC RAYS, HEAVY

(RTOP 506-41-41) IONS, RADIATION DAMAGE, RADIATION PROTECTION,

(NASA-CP-10093; E-7016-1; NAS 1.55:10093) Avail: CASI HC RELATIVE BIOLOGICAL EFFECTIVENESS (RBE)

A03/MF A01

AEROSPACE ENVIRONMENTS, CHEMICAL COMPOSITION, N91-17999*# National Aeronautics and Space Administration.

CONFERENCES, ELECTRICAL PROPERTIES, ENVIRONMENT Langley Research Center, Hampton, VA.

MODELS, INTERACTIONS, MARS SURFACE, SPACE RADIATION PROTECTION FOR HUMAN MISSIONS TO THE

EXPLORATION MOON AND MARS

50
99 GENERAL

LISA C. SIMONSEN and JOHN E. NEALY Washington Feb to obtain relevant interaction cross sections with extensive

1991 27 p comparison with experiments. Solution techniotus for the

(RTOP 326-83-10-50) Boltzmann equations are discussed in detail. Transr,.<,t computer

(NASA-TP-3079; L-16892; NAS 1.60:3079) Avail: CASI HC code validation is discussed through analytical benchmarking,

A03/MF A01 comparison with other codes, comparison with laboratory

GALACTIC COSMIC RAYS, LUNAR SURFACE, MARS experiments and measurements in space. Applications to lunar

SURFACE, NUCLEONS, RADIATION PROTECTION, RADIATION and Mars missions are discussed. Author

SHIELDING, SPACE STATIONS

N92-15959"# National Aeronautics and Space Administration.

N91-23017*# National Aeronautics and Space Administration. Langley Research Center, Hampton, VA.

Langley Research Center, Hampton, VA. HZETRN: A HEAVY ION/NUCLEON TRANSPORT CODE FOR

IMPROVEMENTS IN COMPUTATIONAL ACCURACY OF SPACE RADIATIONS

BRYNTRN (A BARYON TRANSPORT CODE) JOHN W. WILSON (Old Dominion Univ., Norfolk, VA.), SANG Y.

JUDY L. SHINN (National Aeronautics and Space Administration. CHUN (Old Dominion Univ., Norfolk, VA.), FOROOZ F. BADAVI,

Langley Research Center, Hampton, VA.), JOHN W. WILSON LAWRENCE W. TOWNSEND, and STANLEY L. LAMKIN (Analytical

(National Aeronautics and Space Administration. Langley Research Services and Materials, Inc.. Hampton, VA.) Dec. 1991 47 p

Center, Hampton, VA.), MARK WEYLAND (National Aeronautics (RTOP 593-42-11-01)

and Space Administration. Lyndon B. Johnson Space Center, (NASA-TP-3146; L-16952; NAS 1.60:3146) Avail: CASI HC

Houston, TX.), and FRANCIS A. CUCINOTTA (Rockwell A03/MF A01

International Corp., Houston, TX.) Washington May 1991 COMPUTER PROGRAMS, HEAVY IONS, NUCLEONS,

37 p PARTICLE INTERACTIONS, RADIATION SHIELDING,

(RTOP 199-04-16-11) SPACECRAFT SHIELDING

(NASA-TP-3093; L-16898; NAS 1.60:3093) Avail: CASI HC

A03/MF A01 N92-22218"# National Aeronautics and Space Administration.

ALGORITHMS, BARYONS, COMPUTER PROGRAMS, Langley Research Center, Hampton, VA.

EXTRATERRESTRIAL RADIATION, RADIATION COUNTERS, AN EFFICIENT HZETRN (A GALACTIC COSMIC RAY

RADIATION DOSAGE, RADIATION SHIELDING, RADIATION TRANSPORT CODE)

TRANSPORT JUDY L. SHINN and JOHN W. WILSON Apr. 1992 17 p

(RTOP 593-42-21)

N91-26107*# National Aeronautics and Space Administration. (NASA-TP-3147; L-16954; NAS 1.60:3147) Avail: CASI HC

Langley Research Cqnter, Hampton, VA. A03/MF A01

RADIATION RISK PREDICTIONS FOR SPACE STATION COMPUTER PROGRAMS, ENERGETIC PARTICLES,

FREEDOM ORBITS GALACTIC COSMiC RAYS, GRID GENERATION

FRANCIS A. CUCINOTTA (Rockwell International Corp., Houston, (MATHEMATICS), INTERPOLATION, MATHEMATICAL MODELS,

TX.), WILLIAM ATWELL (Rockwell International Corp., Houston, RADIATION SHIELDING, SPATIAL MARCHING. TRANSPORT

TX.), MARK WEYLAND (Rockwell International Corp., Houston, THEORY

TX.), ALVA C. HARDY (National Aeronautics and Space

Administration. Lyndon B. Johnson Space Center, Houston, TX.), N92-25100*# National Aeronautics and Space Administration.

JOHN W. WILSON (National Aeronautics and Space Administration. Langley Research Center, Hampton, VA.

Langley Research Center, Hampton, VA.), LAWRENCE W. MIRACAL: A MISSION RADIATION CALCULATION PROGRAM

TOWNSEND (National Aeronautics and Space Administration. FOR ANALYSIS OF LUNAR AND INTERPLANETARY

Langley Research Center, Hampton, VA.), JUDY L. SHINN (National MISSIONS

Aeronautics and Space Administration. Langley Research Center, JOHN E. NEALY, SCOTT A. STRIEPE, and LISA C. SIMONSEN

Hampton, VA.), and ROBERT KATZ (Nebraska Univ., Lincoln.) Washington May 1992 16 p

Washington Jun. 1991 22 p (RTOP 593-42-31-01)

(RTOP 199-04-16-11) (NASA-TP-3211; L-17044; NAS 1.60:3211) Avail: CASI HC

(NASA-TP-3098; L-16903; NAS 1.60:3098) Avail: CASI HC A03/MF A01

A03/MF A01 COMPUTER PROGRAMS, MANNED SPACE FLIGHT,

BIOLOGICAL MODELS (MATHEMATICS), CELLS (BIOLOGY), MATHEMATICAL MODELS, RADIATION DOSAGE, RADIATION

IRRADIATION, PHYSIOLOGICAL EFFECTS, RADIATION TOLERANCE, SPACE EXPLORATION

EFFECTS, RADIATION HAZARDS, SPACE STATION FREEDOM,

SPACGt STATIONS

N92-15956"# National Aeronautics and Space Administration. 99

Langley Research Center, Hampton, VA.

TRANSPORT METHODS AND INTERACTIONS FOR SPACE GENERAL

RADIATIONS

JOHN W. WILSON (California Univ., Berkeley. Lawrence Berkeley

Lab.), LAWRENCE W. TOWNSEND (Old Dominion Univ., Norfolk,

VA.), WALTER S. SCHIMMERLING (Old Dominion Univ., Norfolk,

VA.), GOVIND S. KHANDELWAL, FERDOUS S. KHAN, JOHN E. N91-15975"# National Aeronautics and Space Administration.

NEALY, FRANCIS A. CUCINOTTA, LISA C. SIMONSEN, JUDY L. Washington, DC.

SHINN, and JOHN W. NORBURY (Rider Coil., Lawrenceville, NJ.) ENGINES AND INNOVATION: LEWIS LABORATORY AND

Washington Dec. 1991 615 p AMERICAN PROPULSION TECHNOLOGY

(RTOP 199-04-16-11) VIRGINIA PARKER DAWSON 1991 277 p

(NASA-RP-1257; L-16882; NAS 1.61:1257) Avail: CASI HC (NASA-SP-4306; NAS 1.21:4306; LC-90-20747) Avail: CASI HC

A99/MF A06 A13/MF A03

A review of the program in space radiation protection at the This book is an institutional history of the NASA Lewis Research

Langley Research Center is given. The relevant Boltzmann Center, located in Cleveland, Ohio, from 1940, when Congress

equations are given with a discussion of approximation procedures authorized funding for a third laboratory for the National Advisory

for space applications. The interaction coefficients are related to Committee for Aeronautics, through the 1980s. The history of the

solution of the many-body Schroedinger equation with nuclear and laboratory is discussed in relation to the development of American

electromagnetic forces, Various solution techniques are discussed propulsion technology, with particular focus on the transition in

51
99 GENERAL

the 1940s from the use of piston engines in airplanes to jet (NASA-CP-3136-VOL-2; NAS 1.55:3136-VOL-2) Avail: CASt HC

propulsion and that from air-breathing engines to rocket technology A22/MF A04

when the National Aeronautics and Space Administration was GOVERNMENT/INDUSTRY RELATIONS, MANUFACTURING.

established in 1958. The personalities and research philosophies ROBOTICS, TECHNOLOGY TRANSFER

of the people who shaped the history of the laboratory are discussed, as is the relationship of Lewis Research Center to the N92-23280*# National Aeronautics and Space Administration.

Case Institute of Technology. Author Langley Research Center, Hampton, VA.

LOEF: 69 MONTHS IN SPACE. FIRST POST-RETRIEVAL

N91-23021*# National Aeronautics and Space Administration, SYMPOSIUM, PART 1

Washington, DC. ARLENE S. LEVINE, ed. Washington Jan. 1992 603 p

TECHNOLOGY 2000, VOLUME 1 Symposium held in Kissimmee, FL, 2-8 Jun. 1991; sponsored by

Mar. 1991 416 p Conference held in Washington, DC, 27-28 NASA, Washington Original contains color illustrations

Nov. 1990 (RTOP 196.88-00-03)

(NASA-CP-3109-VOL-1; NAS 1.55:3109-VOL-1) Avail: CASI HC (NASA-CP-3134-PT-t; L-17042-PT-1; NAS 1.55:3134-PT-1)

A18/MF A04 CONFERENCES, LONG DURATION EXPOSURE FACILITY,

ARTIFICIAL INTELLIGENCE, COMPUTER PROGRAMS, POSTFLIGHT ANALYSIS, SPACEBORNE EXPERIMENTS

COMPUTER SYSTEMS DESIGN, ROBOTICS, TECHNOLOGY

UTILIZATION N92-24806'# National Aeronautics and Space Administration

Langley Research Center, Hampton, VA.

N91-24041*# Washington, National Aeronautics and Space Administration, LDEF: 69 MONTHS IN SPACE. FIRST POST-RETRIEVAL DC. SYMPOSIUM, PART 2

TECHNOLOGY 2000, VOLUME 2 ARLENE S. LEVINE, ed. Jan. 1992 588 p Symposium held

TECNOOG 2in 200,VOUM Kissimmee, FL, 2-8 Jun. 1991; sponsored by NASA,

1991 369 p Conference held in Washington, DC, 27-28 Nov. in Original contains color stons

1990 Washington Original contains color illustrations

(NASA-CP-3109.VOL-2; NAS 1.55:3109-VOL-2) Avail: CASI HC (RTOP 196-88-00-03)

A16/MF A03 (NASA-CP.3134-PT-2; L-17042-PT-2; NAS 1.55:3134-PT-2)

CONFERENCES, INFORMATION DISSEMINATION, NASA LIFE SCIENCES, LONG DURATION EXPOSURE FACILITY,

PROGRAMS, PRODUCT DEVELOPMENT, TECHNOLOGY RADIATION EFFECTS, SPACEBORNE EXPERIMENTS

TRANSFER, TECHNOLOGY UTILIZATION N92-24987"# National Aeronautics and Space Administration,

Washington, DC.

N91-24972"# National Aeronautics and Space Administration. THE FEDERAL CONFERENCE ON INTELLIGENT PROCESSING

Langley Research Center, Hampton, VA. EQUIPMENT

FIRST LDEF POST-RETRIEVAL SYMPOSIUM ABSTRACTS Apr. 1992 205 p Conference held in San Jose, CA, 3-5 Dec.

ARLENE S. LEVINE, comp. Jun. 1991 145 p Symposium 1991

held in Kissimmee, FL, 2-8 Jun. 1991 (NASA-CP-3138; NAS 1.55:3138) Avail: CASI HC A10/MF A03

(RTOP 196-88-00-03) ARTIFICIAL INTELLIGENCE, COMPUTER AIDED

(NASA-CP-10072; NAS 1.55:10072) Avail: CASI HC A07/MF MANUFACTURING, CONFERENCES, CONTROL EQUIPMENT,

A02 GOVERNMENTS, MATERIALS SCIENCE, PROCESS CONTROL

ATMOSPHERIC EFFECTS, EXTRATERRESTRIAL RADIATION, (INDUSTRY), RESEARCH AND DEVELOPMENT, ROBOT

LONG DURATION EXPOSURE FACILITY, LONG TERM EFFECTS, CONTROL, UNITED STATES

RADIATION DOSAGE

N92-27083*# National Aeronautics and Space Administration. N91-28060*# National Aeronautics and Space Administration, Langley Research Center, Hampton, VA.

Washington, DC. LDEF: 69 MONTHS IN SPACE. FIRST POST-RETRIEVAL

FIRST AMONG EQUALS: THE SELECTION OF NASA SPACE SYMPOSIUM, PART 3

SCIENCE EXPERIMENTS ARLENE S. LEVINE, ed. Washington Jan. 1992 485 p

JOHN E. NAUGLE 1990 145 p Symposium held in Kissimmee, FL, 2-8 Jun. 1991; sponsored by (NASA-SP-4215; NAS 1.21:4215) Avail: CAS HC A07/MF A02 NASA, Washington Original contains color illustrations

The process ib recounted by which NASA and the scientific (RTOP 196-88-00-03)

community have, since 1958, selected individual experiments for (NASA-CP-3134-PT-3; L-17042-PT-3; NAS 1.55:3134-PT-3)

NASA space missions. It explores the scientific and organizational Avail: CASI HC A21 /MF A04; 1 functional color page issues involved in the selection process and discusses the CONFERENCES, LIFE SCIENCES, LONG DURATION

significance of the process in the character and accomplishments EXPOSURE FACILITY, PROPULSION, SATELLITE

of U.S. space activities. Author TEMPERATURE, TEMPERATURE CONTROL, THERMAL

CONTROL COATINGS

N92-22423*# National Aeronautics and Space Administration,

Washington, DC N92-27218"# National Aeronautics and Space Administration.

TECHNOLOGY 2001: THE SECOND NATIONAL TECHNOLOGY Langley Research Center, Hampton, VA.

TRANSFER CONFERENCE AND EXPOSITION, VOLUME I SECOND LDEF POST-RETRIEVAL SYMPOSIUM ABSTRACTS

Dec. 1991 527 p Conference held in San Jose, CA, 3-5 Dec. Abstracts Only

1991 ARLENE S. LEVINE, comp. Jun. 1992 133 p Symposium

(NASA-CP-3136-VOL-1; NAS 1.55:3136-VOL-1; Avail: CASI HC held in San Diego, CA, 1-5 Jun. 1992; sponsored by NASA,

A23/MF A04 Washington and AIAA

ARTIFICIAL INTELLIGENCE, BIOTECHNOLOGY, CON- (RTOP 196-88-00-03)

FERENCES. MANUFACTURING, ROBOTICS, TECHNOLOGY (NASA-CP-10097; NAS 1.55:10097) Avail: CASI HC A07/MF

TRANSFER A02

EXTRATERRESTRIAL ENVIRONMENTS, LONG DURATION

N92-22676"# National Aeronautics and Space Administration, EXPOSURE FACILITY, RADIATION EFFECTS, SPACEBORNE

Washington, DC. EXPERIMENTS

TECHNOLOGY 2001: THE SECOND NATIONAL TECHNOLOGY

TRANSFER CONFERENCE AND EXPOSITION, VOLUME 2 N92-28344"# National Aeronautics and Space Administration.

Dec. 1991 518 p Conference held in San Jose, CA, 3-5 Dec. Washington, DC.

1991 NASA ENGINEERS AND THE AGE OF APOLLO

52
99 GENERAL

SYLVIA DOUGHTY FRIES 1992 232 p

(NASA-SP-4104; NAS 1.21:4104; LC-90-39761;

ISBNo0-16-036174-5) Avail: CASI HC Alt/MF A03

A historical account of NASA's Apollo era engineers is

presented. This book is based on interviews that were conducted

with fifty-one 'typical' engineers. Author

53
SUBJECT INDEX

NASA Scientific and Technical Publications 1991-1992

Ti~icl ubec Ide LstngThe miCrogravity environment of the Space Shuttle Aeroacoustics of flight vehicles: Theory arid practice Columbia payload bay dunring STS-32 volume 1, Noime sources (NASA-TP-3141 ) p 49 N92-11931 (NASA-RP-'?ý5410-O-l I p 45 N92-10590

The High Resolution Accelerometer Package lHiRAP) Aeroaccu- s of flight vehicles: Theory and practice. SBETHAIGflight experiment summary for the first 10 flights Volume 2: Noise control

N D [TE NASA-RP-t12671 p 3 N92-22506 [NASA-RP-125V0- L-2I p 45 N92-14779 ACCEPTABILITY Fourth Aircraft Intenoir No*@e Workshop The effects of video compression on acceptability of INASA-CP-10103) p 45 N92-32948

ACCELERATED LIFE TESTS images5 for monitoring flfe sciences experiments AEAOASSIIST

Long-term fife testing of Geostationary Operational (NASA-TP-32391 p 16 N492-33933 Stimulation of real-gas effects on pressure distributions

Environmental Satellite (GOES) encoder lamps ACUTCfUT or aroasaist flighlt expeniment vehicle and conmparaisn INýASA-RP- 1273) p 23 N92-20063 Monograph on propagation of sound waves in curved withi prdction ducts

(NASA-RP-1248) p 44 N91.15$4$ (NASA-TP-3157 j p 27 N92-20677

ACOUSTIC EXCITATION Stagnation -point heat-transfer rate predictions at

TITLE RPR UME1UBR PAE ACCESSION NME1NS Flow-induced P302 resonance of screen-covered 2 9-59 cavities aerinrt NS-P301l pc7nNitions

ACOUSTIC MEASUREMENT AERODYNAMIC CHARACTERISTIC

Fourth International Symposium on Long-Range Sound Large-scale aeroacoustic research feasirbility and

Propaationconceptual design of lest-section inserts for the Ames 80-

[NASA-CP-31011 p 44 N91-16682 by 120-toot wind tunnel

The subject heading is a key to Ithe subject content Second Conference on NOE for Aerospace (NASA-TP-3020] p 45 N91.19624

of the document. The title is used to provide a descrip- Reqtutrements Transonic Symposium: Theory, Application and

tion of the subjectnmatter Mhan the title is insufficiently I NASA-CP-30911 p 18 N91-18189 Experiment, volume 2

Large-scale aeroacoustic research feasibility and INASA-CP-3020-VOL-21 p 5 N91-24132 descriptive of document content, a title extension is conceptual design of terst-section inserts for the Ames S0- Low-speed, powered ground effects of a generc.

added, separated from the title by three hyphens. The by 120-foot wind tunnel hypersoni configuration

accession number and the page number are included I NASA-TP-30201 p45 N91-191124 (NASA-TP-30921 p 5 N91-25103

in each entry to assist the user in locating the abstract ACOUSTI1C PROPAGATION Aeroacoustic and aerodynamic applications of the theory Monograph on propagation of sound waves in curved of nonequilitnum therniodynarracs in the abstract section. If applicable, a report number ducts INASA-TP-31 18) p 26 N491-25352

is also included as an aid in identifying the document. [NASA-RP-12481 p44 N91-15848 Wind tuninel investigation of the interaction and

Under any one subject heading, the accession num- Fourth Intemnational Symposium on Long-Range Sound breakdown characteristics of slender wing vortices at

bers are arranged in sequence. Propagat~ion N-182 subsonic, transonic. and supersonic speeds

Aeroacoustics of flight vehicles: Theory and practice. (AAT-11!p 9-29

Volume 2: Noise control The High Resolution Accelerometer Packgel (HiRAP)

[NASA-RP-12WeVOL-21 4 9-47 flight experiment summary for the first 10 flights

ACOUSTIC PROPERTIES p 5N2179 INASA-RP-12671 p 3 N92-22505

Large-Scale aeroacoustic research feasibility and The natural flow wing-design concept

conceptual design of test-section inserts for the Ames 80 I NASA-TP-31931 p 7 N92-25202

by 120-foot wind tunnel Two-dimensional aeodynamic characteristics of several A [NASA-TP-30201 p 45 N91-19824 polygon-shaped cross-sreclionall models applicable to

ACOUSTICS helicopter fuselages

ABSORPTIVIT'Y Wind turbine acoustics I NASA-TP-32331 p 8 N92-30394

Optical measurements on solid specimerisof solidrockret (NASA-TP-30571 p44 N9-1,1679 Lewis icing research tunnel test of the aerodynamic

motor exhaust and solid rocket motor slag ACTIVATION ENERGY effects of aircraft ground deecing/anti-icing fluids

[ NASA-TP-31771 p 20 N92-20949 Two-dimensional stability of laminar flames f NASA-TP-32361 p 10 N92-30395

ABSTRACTS INASA-TP-3131] p 7 N92-17131 Wind tunnell aerodynamic characteristics of a Large space structures and systems in the apace Station ACTIVE GALACTIC NUCLEI transportl-type salad in a Simulated heavy rain era: A bibliography with indexes Paired and Interacting Galaxies: International environment

(NASA-SP-7085(01)3 p 17 N91-18199 Astronomical Union Colloquium No. 124 [ NA5A.TP-31941 p08 N92-31532

Large space structures and systems in the space station I NASA-CP-30981 p 49 N91-16858 Effect of afterbody geometry on aerodynamic era A bibliography with indexes ACTUATORS characteristics of isolated nonaxisymmetric afterbodies at

I NASA-SP-7085(02)) p 18 N491-281 9The 25th Aerospace Mechanisms Symrposium transonic Mach numbers

Earth observations and global change decision making: I NASA-CP-31131 p 30 NOI-24603 I NASA-TP-32361 p 9 N92-337D6

A special bibliography, 1991 The 26th Aerospace Mechanisms Symposium AERODYNAMIC COEFFICIENTS

[NASA-SP-70921 p p32 N9t -30508 I NASA-CP-3147) p 30 N92-25067 Parametric study of afterbody/nozzle drag on twin

Lag pc tutrsad" m ntesaesain ADAPTERS two-dimensional convergent-divergent nozzles at Mach

Lar&Abbigerapace s itrutue andssemes iSplmn th spcesato Graphite/epoxy composite adapters for the Space numbers from 0.60 to 1-20

era NASbiligrphy with3 idxssuplemeNt20 3 17 Shuttle/Centaur vehicle I NASA-TP-2640) p4 N91-14316

IACCLEATED7080LIF p18T [9-21 INASA-TP-30141 p 15 N92-31251 Physically weighed approximations of unsteady

Long-term life testing of Geostationary Operational ADAPTIVE CONTROL

Environmental Satellite (GOES) encoder lamps Development of an adaptive failure detection and aerodynamic forces using the mintimum-stale method

INASA-TP-302S I p 4 N91-18031

[NASA-AP-12731 p 23 N92-20063 identification system for detecting aircvall control element Pamercivsgtonfsnl-xpso-ap

ACCELERATION (PHYSICS) failuresPaaercivsitonf ng-xpno-am

Measurement and Characterization of the Acceleration [NASA-TP-3051 p p12 N91-25151 nozzles at Mach numbers from 0.60 to 1.20

Environment on Board the Space Station Ongoing Progress in Spacecraft Controls I NASA-TP-32401 p 9 N92-34193

NASA-~-00 p4[9-20 NASA-CP-100991 p 19 N92-28730 AERODYNAMIC CONFIGURATIONS

The microgravity environment of the Space Shuttle AEROACOUSTICS A mto o einn lne igbd

Columbia middleck during STS-32 Flow-Widuced resonance of screen-covered cavities configuration' for low wave drag p8N2346 INASA-TP-32 118N2.28 I NASA-TP-3140t p 48 N92-1 1930 (NASA-TP-3052) p 25 N91-15499 AERODYNAMIC DRAG

The microgravity, environment of the Space Shuttle Large-scale aeroacoustic research feasibility and Applications of a direct/literative design method to

Columbia payload bay during STS-32 conceptual design of test-section inserts for the Ames SO1- complex tranisonic configuirations

(NASA-TP-3141 p p49 N92-1 1931 by 120-foot wind tunnel I NASA-TP-32341 p 8 N92-33484 ACCELEROMETERS I NASA-TP-3020) p45 N91-19824 Parametric investigation of stingle-expfansion-ramp, Measurement and Characterization of the Acceleration Acoustic and aerodynamic study of a pusher-propeller nozzles at Mach numbers from 086010o 1.20

Environment on Board the Space Station aircraft model [NASA-TP-3240) p 9 N92-34 193

[NASA-CP-304801 p48 NQ1-12401 I NASA-TP-30401 p 45 N91-21828 AERODYNAMIC FORCES

The microgravity environment of the Space Shuttle Aeroacoustic and aerodynamic applications of the theory Payload bay doors and radiator panels familianzation

Columbia middeclr during STS-32 of nonequilibnium thermodynamics handbook

(NASA.TP-314111 p 48 N92-11930 INASA-TP-31181 p26 N91-25352 [NASA-TM-1077931 p 15 N92.20676

A-i
AERODYNAMIC HEATING SLIBJECT/NOEX

AERODYNAMIC HEATING Aeronautical engineering. A continuing bibliography with Aeronautical engineering A continuing biliography with

A simplified methodfor thermnal analysis ofa cowl leading indexes (supplement 269) indexes (supplement 273)

edge subject to intense local shock-wave-intertererice I NASA-SP-70371269)) p 2 N92-10974 [NASA-SP.7037(273)1 p 3 N92-21 729

heating Aeronautical engineering: A continuing bibliography with Aeronautical engineering A continuing bibliography with

INASA-TP-3-671I p 27 N92-24797 indexes (supplement 271) indexes (supplement 272)

AERODYNAMIC INTERFERENCE JNASA-SP-7037J271)) p 2 N92-14957 INASA-SP-7037)272)( p3 N92-41844

Effect of location of aft-mounted nacelles on the Aeronautical engineering: A continuing bibliography with Aeronautical enigineering A continuing tbiblography with

longitudinal aerodynamic charactenistics of a tsgh-wing indexes (supplement 273) indexes (xupplement 277)

transport airplane (NASA-SP-7031(273)1 p 3 N92-21729 11NASA.SP-7037(277)1 p 3 N92-27929

I NASA-TP-30471 p 4 N91 -13402 Aeoatclegneigt otnigbbiga hy Aeronautical engineering, A continuing bibliography with

Wal-rtefernc asesmet ndcorecios or indexes (supplei-,inl 272) indexes (supplement 278)

transonic NACA 0012 airfoil data trom various wind )NS-P73(7tIp 9-14 NASA.SP-7037(278)1 p 3 N,92-28677

tunnels INS-P73(71p3N2184 Aeronautical engineering: A Continuing bibliography with

[NASA-TP-3070 ( p 5 N491-20043 Aeronautical engineering. 91, continuing bibliography with idxs(upeet25

installation effects of wing-mounted turbofan indexes (supplement 277) inAexs (supplement275) 9-8

nacelle-pylons on a 1/17-scale, twin-engine, low-wing pNS-P73(7) p3 N92-27929 Aeronautical engineering: A continuing bibliography with

transport model Aeronautical engineering: A continuing bibliography with indexes (supplement 280)

1 NASA-TP-31681 p 7 N92-19002 indexes (supplement 278) INASA-SP-7037(260)) p 3 N92-31456

Comparison of a two-dimensional adaptive-wall INASA-SP-7037(278) ( p 3 N492-28677 AERONAUTICS

technique with analytical watt interference correction Aeronautical engineering: A continuing bibliography with Aeronautical engineenring A continuing bibliography with

techniques indexes (supplement 275) indexes (supplement 278) )NASA-TP-3132J p 7 N92-20494 I NASA-SP-7037(275)] p 3 N92-28679 (NASA-SP-7037(278)1 p 3 N92-28677

A simiplified meithod for thermal analysis o1 a cowl leading Aeronautical engineering: A continuing bibliography with AEROSOLS

edge subject to intense local shock-wave-interference indexes (supplement 280) SAM 2 measurements of the polar stratospheric aerosol.

heating (NASA-SP-7037(280)) p 3 N492-31456 Volume 9: October 1982 - Apnl 1983

[ NASA-TP-31671 p 27 N492-24797 AEROELASTICe RESEARCH WINIGS, INASA-SP-12441 p33 14191-i18505

AERODYNAMIC LOADS Deaign 0f control laws for flutter suppression based on Volcanism-Climeate Interactions

A method for the design of transonic flexible wings the aerodynamic energy concept and comparisons with (NASA.CP-100621 p34 Ng 11-21641

1 NASA-TP-30451 p 10 N491-14323 other design methods International Workshop on Stratospheric Aerosols:

AERODYNAMIC NOISE I NASA-TP-30561 p 29 N491-10328 Measurements. Properties. and Effects

Aefroacoustics of ftight vehicles: Theory and practice. AEROELASTICITY [ NASA-CP-3114) p 32 N491-32528

Volume 1: Noise sources A method for the design of transonic flexible wings SAGE 1 data user's guide

I NASA-RP-1258-VOL--l I p 45 N492-10598 I NASA-TP-30451 p t0 N491-14323 [NASA-RP-12751 p 34 N492-33097

Annoyance caused by advanced turboprop aircraft Development ot an integrated aeroseivoelasfti analysis AEROSPACE ENGINEERING

flyover noise: Comparison of different propeller program and correilaition with test data NASA Patent abstracts bibliography: A continuing

configurations [NASA-TP-31 20) p 2 N91 -26113 bibliography. Section 1: Abstracts (supplement 38)

f NASA-TP-31041 p 45 N492-11758 Longitudinal aerodynamic characteristics of a subsonic. I NASA-SP-7039(38)-SECT- I I p 47 N491-17833

Fourth Aircraft Interior Noise iiJortishop energy-efficient transport configuration in the National NASA patent abstracts bibliography. A continuing

I NASA-CP- 101031 p 45 N92-32948 Transonic Facility bibliography. Section 2: indexes (supplemnent 38) AERODYNAMIC STABILITY [ NASA-TP-29221 p 6 N491-28143 I NASA-SP-7039(38)-SECT-2I p 47 N491-1 7834

Flight characteristics of a modified Schweizer SGSi -36 Planforrn curvature effects on tlutter characteristics ot Aerospace Applications of Magnetic Suspension

sailplane at tow and very high angles of attack a wing with 56 deg leading-edge sweep and panet aspect Technology, part 1

I NASA-TP-3022) p 12 N91-10079 ratio of 1, 14 (NASA-CP-10066-PT-l( p 17 N91-21188

Wind-tunnel static and free-flight investigation of [ NASA-TP-31 16] p 11 N492-13054 The 25th Aerospace Mechanisms Symposium high-angle-of-attack stability and control characteristics of AEROMIANEUVERING [ NASA-CP-31 13] p 30 N491-24603 a model of the EA-68 airplane HypermelocitV atmospheric flight: Rteal gas flow fietds NASA patent abstracts bibliography: A continuing

I NASA-TP-31941 p 7 N492-25276 (NASA-AP-12491 ~26 N91-20418 bibliography. Sectior' 1: Abstracts (supplement 39) AERODYNAMICS AERONAUJTICAL ENGINEERING [NASA-SP-7039(39)-t:rECT-i I p 48 N91-28042

Aeronautical engineering: A continuing bibliography with Aeronautical engineerng:. A continuing bibliogrcaphy writh NASA, patent abstracts bibliography: A continuing indexes (supplement 256) indexes (supplement 258) bibliography. Section 2: Indexes (supplement 39) (NASA-SP-7037(256)] p 1 N491-10002 [NASA-SP-7037(256)J p 1 N91-10002 I NASA-SP-7039(39)-SECT-21 p 48 N91-2906

Aeronauticat engineering: A continuing bibliography with Aeronautical engineering: A continuing bibliography with Beyond the Baseline 1991: Proceedings of the Space indexes (supplement 257) indexes (supplement 257) Station Evolution Symposium. Volume 2- Space Station

I NASA -SP-7037(257)1 p 1 NQI-12589 [NASA-SP-7037(257)) p 1 1,191-12589 Freedom, part 1

Aeronautical engineering: A continuing bibliography with Aeronautical engineering: A contintuing bibliography with NASA-OP- 1 0083-VOL-2-PT- I1) p 18 N92- 177688

indexes (supplement 258) indexes (Supplement 258) NS aetasrcsbbigah:Acniun

)NAA-P-737258) 1 911339 NASA-SP-7037(258)1 p 1 N91-13399 bibliography. Section 1: Abstracts (supplement 40) Aeronautical engineering: A continuing bibliography with Aeronautical engineening: A continuing bibliography with (NASA-SP-7039(40)- SECT. I I p 48 N492-22508

indexes (supplement 260) indexes (supplement 260)Th192GdadCnenconSceApitos INASA-SP-7037(?60)1 p 1 N491-15978 (NASA-SP-7037(260i) p 1 N91-15978 h 92GdadCneec nSaeApiain

Aeronautical engineening: A continuing bibliography with Aeoatclegneig otnig~igah ih of Artificial intelligence

indexes (supplement 259) indexes (supplement 259) (AAC- 4)p4 9-35

INASA-SP-7037(259)) p 1 1491-15979 [NASA-SP.7037(259)1 p 1 N491-15979 The 261h Aerospace Mechanisms Symposium

Flight Mechanics/Estimation Theory Symposium, 1990 Aeronautical engineering: A cumulative index to a [NASA-CP-31471 p 30 N492-25067

[NASA-CP-31021 p 14 N91-17073 continuing bibliography (supplement 261) NASA patent abstracts bibliography: A continuing

Aeronautical engineering: A cumulative index to a [NASA-SP-7037(261)) p I1491-23073 bbiliography. Section 2: indexes (supplement 40)

continuing bibliography (supplement 261) Aeronautical engineening: A continuing bibliography with I NASA-SP-7039(40)-SECTý21 p 48 N92-27081

JNASA-SP-7037(261)] p 1 N491-23073 indexes (supplement 262) The 1990 NASA Aerospace Battery Workshop

Aeronautical engineering A continuing bibliography with (NASA-SP-7037(262)1 p I N91-23074 INASA-CP-31191 p 20 N492-21130

indexes (supplement 262) Aeronautical engineering: A continuing bibliography with NASA patent abstracts bibliography: A continuing I NASA-SP- 7037(262)1 p I N91-23074 indexes (supplement 265) bibliography Section 2: Indexes (supplement 41) Aeronautical engineering: A continruing bibliography with I NASA-SP-7037(265)] P2 N91-24095 I NASA-SP- 7039(41 I-SECT-21 p 48 N492-31455

indexes (supplement 265) Aeronautical engineering: A continuing bibliography with AEROSPACE ENVIRONMENTS

[NASA-SP-7037(265)1 p 2 N91-24095 indexes (supplement 2631 Space Photovoltaic Research and Technology Aeronautical engineering: A continuing bibliography with I NASA-SP.7037(263)) p 2 N91 -24096 Conterence

indexes (supplement 263) Aeronautical engineering: A continuing bibliography with [NASA-CP-31211 p 19 N91-30203

INASA-SP-7037(263) I p 2 N491-24096 indexes (supplement 264) Analyses of risks associated with radiation exposure Aeronautical engineering: A continuing bibliog~aphy with INASA-SP-7037f 264)) p2 N91-24097 from past major solar particle events

indexes (supplement 264) Aeronautical eingineering: A continuing bibliography with INASA-TP-31 371 p 50 N91 -31061

[NASA-SP-7037)26411 p 2 N491-24097 indexes (supplement 286) Eetia n hmclitrcin tMr okhp Airborne Wind Shear Detection and Warning Systems: (NASA-SP.7037(266)1 p2 N91-27122 Eetia n hmclitrcin tMr okhp Thir ad Tchnoogits'part Cobine Maufacures' 1 Thid Maufctrer ombne ad Tcholoiss' Aeronautical engineering: A continuing bibliography with (NASA-CP-`100931 p 50 N492-30302 Conlerence. pairt i indexes (supplement 260)

1 NASA-CP- I0060-PT-lI1 p9 N491-24166 )NASA-SP-7037(268)1 p2 1491-310077 AEROSPACE MEDICINE

Aeronautical engineering: A continuing bibliography with Aeronauticai engineering: A continuing bibliography with Aerospace medicine and biology: A continuing

indexes (supplemrent 266) indexes (supplement 267) btibiographly with indexes (supplement 341)

[NASA-SP-7037(266)1 p 2 N91-27122 I NASA-SP-7037(267)] p 2 N92-10001 )NASA-SP-7011(341)) p 37 N91-10594

Aeronautical engiineering: A continuing bibliography with Aeronautical engineering: A continuing bibliography with Aerospace medicine and biology. A continuing

indexes (,supplement 288) indexes (supplement 270) bibliography with indexes (supplement 342)

fNASA-SP-7037(268)] p 2 -N91-30077 (NASA-SP-7037(270)f p 2 N92-10J973 I NASA SP.7011(3A2)1 p 37 N491-13063

Aeronautical engineering A continuing bibliography with Aeronautical engineering: A continuing bibliography with Aerospace medicine ind biology A continuing

indexes (supplement 267) indexes (supplement 269) bibliography with indexes (supplement 343)

1NASA-SP-7037(2r37)) p2 1492-10001 (NASA-SP-7037(269)1 p 2 N492-10974 I NASA -SP- 7011(343)1 p 37 N491-147111

Aeronautical engineering A continuing bibliography with Aeronautical engineering. A continuing bibliography with Aerospace medicine and biology A continuing indexes (supplement 2702) indexes (supplement 271) bibliography with indexes (supplement 344)

I NASA-SP-7037(270)1 p 2 N92-102973 I NASA -SP-7037127 1)) p 2 N492-14967 I NASA-SP-701 1(34411 p 37 N491-14712

A-2
SUBJECT INDEX AIRCRAFT HAZARDS

Aerospace medicine and biology- A cumulative index AEROTHERMODYNAMICS Effect of alterbody geometry on aerodynamic

to a continuing bibliography (supplement 345) Advanced Hypervelocity Aerophysics Facility characteristics of isolated nonaxisymmetric aftebodies at

I NASA-SP-7011(345)1 p37 N91.16547 Workshop transonic Mach numbers

Aerospace medicine and biology: A continuing (NASA-CP-t00311 p13 N91-24211 (NASA-TP-3236] p9 N92-33706

bibliography with indexes (supplement 346) AFTERBODIES AIRCRAFT CONSTRUCTION MATERIALS

FNASA-SP-7011(346)1 p 37 N91-23700 Parametric study of atterbody/nozzle drag on twin Eighth DOD/NASA/FAA Conh, ence on Fibrous

Aerospace medicine and biology: A continuing two-dimensional convergent-divergeni nozzles at Mach Composites in Structural Design. part 2

bilbography with indexes (supplement 347) numbers from 0.60 to 1.20 [NASA.CP-3087-PT-21 p 22 N92-32574

INASA-SP.7011(347)) 137 N91-23701 fNASA-TP-2640! p4 N91-14316 AIRCRAFT CONTROL

Aerospace medicine and biology A continuing Effect of afterbody geometry on aerodynamic A controls engi-'senng approach for analyzing airplane

bibliography with indexes (supplement 348) characteristics of i3solted nonaxisymmetric afterbodes at input-output characteristics

(NASA.SP.7011(348)1 p 37 N9t-23702 transonic Mach numbers (NASA-TP-30"21 p 12 N91-20128

Aerospace medicne and biology A continuing J(NASA-TP-32361 p 9 N92-33706 Fourth NASA Workshop on Computational Control of bibliogrospae weitindes (sdublement 349) coti AGING (MATERIALS) Flexile Aerospace Systems, pe - 2 biblography with idexes (supplement 349) Long-term life testing of Geostationary Operational A erospa 06P2 S 2

[NASA-SP-70t1(349)) p 37 N91-24731 Environmental Satellite (GOES) encoder lamps {NASA-CP-10065-PT-21 p17 N91.22331

Aerospace medicine and biology: A continuing ]NASA.RP-1273] p 23 N92-20063 Development of an adaptive failure detection and

bibliography with indexes (supplement 350) The 1991 International Conference on Aging Aircraft and identification system for detecting aircraft conto 4 element

[NASA.SP.7011(350)] p 38 N91-25600 Structural Airworntiness failures

Aerospace medicine and biology: A continuing (NASA CP-31601 p 31 N92-30106 (NASA.TP-3051) p 12 N91-25,51

bibliography with indexes (supplement 351) AIR Application -"id flight test of linearizing transformations

[NASA-SP-7011(351)] p 38 N91-27756 Calculations and curve fits of thermodynamic and using measurement feedback to the nonlinear corn.,u;

Aerospace medicine and biology: A continuing transport properties for equilibrium air to 30000 K problem

bibliography with indexes (supplement 352) [NASA-RP-1260) p 26 N92-11285 INASA.TP.3154) p 12 N91-30154

[NASA.SP-701 1(352)] p 38 N91-28729 AIR BREATHING ENGINES Visually GuiOed Control of Movement

Aerospace medicine and biology: A continuing Aeropropilsion 1991 (NASA-CP-31 18) p 39 N92-21467

bibliography with indexes (supplement 353) (NASA-CP-100631 p 12 N91-20086 Wind-tur. el static and free-flight investigation of

fNASA-SP-7011(353)] p 38 N91-31760 AIR JETS high.angle-o track stability and control characteristics of

Aerospace medicine and biology: A continuing Venturi air-jet vacuum eeftors for high-volume a model of the EA-68 airplane

bibliography with indexes (supplement 354) atmospheenc sampling on aircraft platforms I NASA-TP-3194) p 7 N92-25276

INASA-SP-7011(354)) p38 N92-12404 [NASA.TP.31831 p 11 N92-20546 AIRCRAFT DESIGN Aerospace medicine and biology: A continuing AIR POLLUTION Effect of location of alt-mounted nacelles on the bibliography with indexes (supplement 355) The atmospheric effects of stratosphenc aircraft: A first longitudinal aerodynamic characteristics of a high-wing

INASA-SP-7011(355)) p 38 N92-12412 program report transport airplane a NASA-RP-12721 p 33 N92-19121 [NASA-TP-30471 p 4 N91-13402 Aerospace medicine and biology: A continuing AIR SAMPLING A method for the design of transoric flexible wings

bibliography with indexes (supplement 356) Venturi air-jet vacuum electors for high-volume [NASA-TP-3045h p t0 N9t-14323

NASA-SP-7011(356)) p 38 N92-15538 atmospheric sampling on aircraft platforms Proceedings of the X-15 First Flight 30th Annrversary

Aerospace medicine and biology: A continuing I NASA-TP-31831 I tI N92-20546 Celebrto

bibliography with indexes (supplement 357) AIR TRAFFIC CONTROL

S NASA-SP-7011(357)I p 39 N92-21714 Aviation Safety/Automation Program Conference (NASA-CP-3105 p t10 N91-20071

Aerospace medicine and biology: A continuing INASA-CP-30901 p9 N91-10936 Aeropropulsion 1991

bibliography with indexes (supplement 359) Report of the workshop on Aviation Safety/Automation (NASA-CP-l00631 p 12 N91-20086

[NASA-SP-7011(359)] p 39 N92-21715 Program Transonic Symposium: Theory, Application and

Aerospace medicine and biology: A cumulative index (NASA-CP.10054] p9 N91-15141 Experiment, volume 2

to a conbnuing bibliography (supplement 358) Flight tests with a data link used for air traffic control INASA-CP-3020-VOL-2] p 5 N91-24132

[NASA-SP-70 1(358)) p 39 N92-22026 information exchange Evaluation of cloud detection instruments and

Fifth Annual Workshop on Space Operations INASA-TP-31351 p 11 N91-31143 performance of laminar-flow leading-edge test articles

Applications and Research (SOAR 1991). volume 2 Flight deck benefits of integrated data link during NASA Leading-Edge Flight-Test Program

[NASA-CP-3127-VOL-21 p41 N92-22324 communication INASA-TP-2888I p 11 N91.24199

Aerospace medicine and biology: A continuing INASA-TP-32191 p 10 N92-21459 The natural flow wing-design concept

bibliography with indexes (supplement 362) AIR TRAFFIC CONTROLLERS (PERSONNEL) INASA-TP-3193i pa7 N92S25202

NASA-SP-7011(362)] p 39 N92-27068 Report of the workshop o0 i Aviation Safety.'Automation CP mputational Structures Technelmgy for AsYtames and

Aerospace medicine and biology: A continuing Program Propulspion Systems

bibliography with indexes (supplement 361) INASA-CP_100541 p 9 N91-15141 NASA-CP-31421 p 31 N92-25911

[NASA-SP-7011(361) Ip39 N92-27433 IRASPORTATIO Aeronautical engineering: A continuing bibliography with Aerospace medicine and biology: A continuing AIR TRANSPORTATION indexes (suoplement 278)

bibliography with indexes (supplement 363) Joint University Program for Air Transportation NASA-SP-7037(278) ( p 3 N92-28677

[NASA-SP-7011(363)) p 39 N92-30987 Research. 1989-1990 Aeronautical engineering: A corntinuing bibliography with

AEROSPACE PLANES INASA-CP-30951 p 1 N91-19024 indexes (supplement 275)

Rocket-Based Combined-Cycle (ROCC) Propulsion Joint University Program for Air Transportation [NASA-SP-7037(275)1 p 3 N92-28679

Technology Workshop Tutorial session Research, 1990-1991 A method for daesiging blended wing-body

(NASA-CP-100901 p 20 N92-21517 INASA-CP-3131 I p 3 N92-17984 configurations for low wave drag

AEROSPACE SCIENCES AIR WATER INTERACTIONS INASA-TP-3261 I p 8 N92-32480

NASA Thesaurus supplement: A four part cumulative NASA Wallops Flight Facility Air-Sea Interaction Eighth DOD/NASA/FAA Conference on Fibrous

supplement to the 1988 edition of the NASA Thesaurus Research Facility Composites in Structural Design, part 1

(supplement 4) (NASA-RP-12771 p36 N92.25981 NASA-CP-3087-PT-1I p22 N92-32513

INASA-SP.Y064-SUPPL-41 p47 N91-10804 AIRB3ORNE EQUIPMENT Applications of a direct/iteratlive design method to

NASA scientific and Technical publications. A catalog Airborne Wind Shear Detection and Warning Systems complex transonic configurations

of special pubhcations, reference publications. conference Second Combined Manufacturers' and Technologists' INASA-TP-32341 p 8 N92-33484

publications, and technical papers, 1989 Conference, part 1 Survey and analysis of research on supersonic

INASA-SP-7063(04)) p47 N91-13374 INASA-CP-10050-PT 11 p9 N91-11682 drag-due-to-lift minimization with recommendations for

NASA Thesaurus supplement: A four part cumulative Airborne Wind Shear Detection and Warning Systems: wing design

supplement to the 1988 edition of the NASA Thesaurus Third Combined Manufacturers' and Technologists' [NASA-TP-32021 p 9 N92-33656

(supplement ill Conference, part 2 AIRCRAFT ENGINES

INASA SP-7064-wuPPL-51 p 47 N91-19962 (NASA-CP-10060-PT.21 p 9 N91.24140 Aeropropulsion 1991

NASA scientific and technical publications A catalog Venturi air-let vacuum electors for high-volume [NASA.CP.100631 p 12 N91-20086

of special publications, reference publications, conference atmospheric sampling on aircraft platforms Aeronautical engineering: A continuing bibliography with

publications, and technical papers. 1987-1990 INASA-TP-31831 p 11 N92-20546 indexes (supplement 267)

(NASA-SP-7063(05)1 p47 N91-24939 AIRCRAFT COMMUNICATION INASA-SP-7037(267)1 p2 N92-10001

AEROSPACE SYSTEMS Flight deck oenefits of integrated data link Aeropropulsion 1987

Second Conference on NOE for Aerospace co)munication ]NASA-CP-30491 p 12 N92-22510

Requirements cNASA-TP-32191 p 10 N92-21459 AIRCRAFT EQUIPMENT

[NASA-CP-30911 p 16 N91-18189 Aeronautical engineering: A continuing bibliography with

Fourth NASA Workshop on Computational Control of AIRCRAFT CONFIGURATIONS indexes (supplement 267)

Flexible Aerospace Systems, part I Span reduction effects on the flutter characteristics of (NASA-SP-7037(267)1 p 2 N92-10001

I NASA-CP- 10065-PT- tI p I I N9t-22307 arrow-wing supersonic transport configurations AIRCRAFT GUIDANCE

Fourth NASA Workshop on Computational Control of fNASA.TP.30771 p 11 N91-21 127 Airborne Wind Shear Detection and Warning Systems

Flexible Aerospace Systems, part 2 Static internal performance of ventral and rear nozzle Second Combined Manufacturers' and Technologists'

I NASA-CP-10065-PT-2} p 1;f N91-22331 concepts for short-takeoff and vertical-landing aircraft Conference, part 2

Methods of applied dynamics [NASA.TP-3t031 p 6 N92-10975 [NASA-CP-10050-PT-21 p 9 N91-11695

I NASA-RP-12621 p24 N91-25303 The natural flow wing-design concept AIRCRAFT HAZARDS

AEROSPACE VEHICLES {NASA-TP-31931 p 7 N92-25202 Airborne Wind Shear Detection and Warning Systems

The 1991 International Aerospace and Ground Applications of a direct/iterative design method to Second Combined Manufacturers' and Technologisls'

Conference on Lightning and Static Electricity, volume 1 complex transonic configurations Conference, part I

INASA.CP-3106-VOL- II p 35 N91 32599 (NASA-TP-32343 p 8 N92-33484 I NASA-CP-t0OSO-PT.-1] p9 N91-11682

A-3
AIRCRAFT INDUSTRY SUBJECT INDEX

The 1991 International Aerospace and Ground AIRCRAFT WAKES ALUMINIDES

conference on Lightning and Static Electricity, volume I Acoustic and aerodynamic study of a pusher-c opeller Oxidat ion characteristics of T,25Ai-1ONti-3V-1M0

INASA-CP-31I06-VOL-t p 1 35 N9 1-32599 aircraft model inlerrnetallic alloy AIRCRAFT INDUSTRY I NASA-TP-3040 I p 45 N91-21828 I NASA-TP-30441 p 22 N91-13522

The I 911 International Conference on Aging Aircraft and AIRFOIL PROFILES ALUMINUM AL'_S -"S

Structural Airworthiness Calibration of the 13- by 13-inch adaptive wall test Surface effects on hydrogen permeation through [NASA-CP-31601 p 31 N92-30106 section for the Langley 0 3-meter trarisonic cryogenic Ti-t14AI-21 Nb alloy

AIRCRAFT MAINTENANCE tunnel JNASA-7P-31091 P 23 N9t1-20266

The 1991 International Conference on Aging Aircraft and I NASA-TP-30491 p 13 N91-1 3461 ANECHOIC CHAMSERS

Structural Airworthiness A method for the design of transonic flexible Wings Annoyance Caused by aircraft en route noise

I NASA-CP-31 60) p 31 N92-301106 I NASA-TP-30-451 p t0 N91-14323 [NASA-TP-31651 p 45 N92-20-479

AIRCRAFT MANEUVERS Wall-interference assessment and corrections for ANGLE OF ATTACK

Control integration concept for hypersonic cruise-turn transonic NACA 0012 airfoil data from various wind Flight characteristics of a modified Schweizer SGSt 136 maneuvers funnels sailplane at low and very high angles of attack

I NASA-TP-31361 p 13 N92-20195 (NASA-TP-30701 p5 N91-20043 ?,IASA-TP-3022j p 12 N91-10079

AIRCRAFT MODELS Full-scale semispan tests of 5 busineSS-ist Wing with a Transonic and supersonic Euler computations of

A controls engineering approach for analyzing airplane natural laminar flow airfoil vortex-dominated flow fields about a generic tighter in'put-output characteristics I NASA-TP-31331 p 6 N91-30099 [NASA-TP.3t561 p6 N92-10011I

INASA.TP-30721 p 12 N91-20128 tInfluence of airfoil geometry on delta Wing leading-edge Wind-tu~nnel static and free-flight investigalton o1

Acoustic and aerodynamic study of a pusher-propeller vortices and vortex-induced aerodynamics at supersonic high-angte-ot-attack stability anid control characteristics of

aircraft model speeds a model Of the EA-6B airplane

INASA-TP-30401 p 4 5 N91-21828 INASA-TP-31051 p 7 N92-20038 INASA-TP-31941 p 7 N92-25276

Low-speed, powered ground effects of a generic. AIRFOILS ANGULAR DISTRIBUTION

hypersorsc configuration Numerical study of the aerodynamic effectsa of using Inclusive inelastic scattering of heavy ions and nucear I NASA-TP-30921 p 5 N91-25103 sulfur hesafluoritte assa test gas in wind tunnels Correlations

Two-dimensional aerodynamic characteristics of several JNASA-TP-30861 p 5 N91-22070 I NASA-TP-30261 p46 N91-t13985

polygon-shaped cross-sectinal models applicable to Comparison of a two-dimensional adaptive-wall ANGULAR VELOCITY

helicopter fuselages technique With analytical wall interference cOrrec'., ' A nonlinear estimator for reconstructing the angular

I NASA.TP-32331 p 8 N92-30394 techniques velocity of a spacecraft without rate gyros Effect of atterbody geometry on aerodynamic INASA.TP-31321 p7 N92-20494 (NASA-TP-31761 p 24 N92-13343

characteristics of isolated nonasisymmetric afferbodies at Wind funnel aerodynamic characteristics of a ANISOTROPIC PLATES

transonic Mach numbers transport-type airfoil in a eimulated heavy rain Buckling behavir of long symmetrically laminated Plates

INASA-TP-32361 p 9 N92-33706 environment subjected to combined loadings AIRCRAFT NOISE fNASA-TP-31841 p 8 N92-31532 I NASA-TP-31951 p 22 N92-25160

Fourth international Symposium or' Long-Range Sound AIRFRAMES ANNUAL VARIATIONIS

Propagation Computational Structures Technology for Airframes and Atlas of the Earth's radiation budget as measured by

(NASA-CP-3101 I p44 N91-1662 Propulsion Systems Nimbus-7: May 1979 to May 1980

Aeroacousfics of flight vehicles: Theory and Practice, [ NASA-CP-31421 p 31 N92-25911 [NASA-RP-1263] p 35 N91-24720

volume 1. Noise sources AIRLINE OPERATIONS ANNULAR FLOW

INASA-RP-I 258-VOL-tiJ p 45 N92-10598 Evaluation of cloud detection instruments and Three-component laser anemometer measurertent

Annoyance caused by advanced turboprop aircraft performance of laminar-flow leading-edge test articles systems flyover noiase Comparison of difefernt propeller during NASA Leading-Edge, Flight-Test Program [ NASA-TP-30801 p 5 N91-19057

configurations J NASA-TP-28881 pit1 N91-2419g Laser anemometer measurements and computations in

INASA-TP-31041 p 45 N92-11758 ALBEDO an annular cascade of high turning core turbine vanes Annoyance caused by aircraft en route noise User's guide Nirnbus-7 Earth radiation budget [NASA-TP-32521 p8 NhZ ',Q80

I NASA-TP-31651 p 45 N92-20479 narrow-field-of-view products. Scene radiance tape ANOMALIES Fourth Aircraft Interior Noise Workshop products, sorting info angular bins Products, and maximum J-85 jet engine noise measured in the ONERA St IWind [NASA-CP-101031 p 45 N92-32948 likelihood cloud estimation products tunnel and extrapolated to tar field

AIRCRAFT PERFORMANCE (NASA-RP-1246) p34 N91-t3043 (NASA-TP-3531 p 45 N91-19823

Joint University Program for Air Transportattion ALIGAF ANTARCTIC REGIONS Research. 1989-1990 Controlled Ecological Life Supper, Lyslems: Natural arid SAM 2 measurements of the polar st ratosphleric aerosol (NASA-CP-30951 p 1 N91-19024 Aniiticial Ecosystems Volume 9: October 1982 - April 1983 Axirorne Wind Shear Detectio and Warning Systems INASA-CP-t0040] p 40 N91-24744 INASA-RP-t12441 p 33 N91-18505 Third Combined Manufacturers' and Technologists' ALGORITHMS West Antarctic lce Sheet Initiative. Volume 1, Science Conference. part 1 NASA Computational Fluid Dynamics Conference, and implementation Plan I NAS, -,P- 1008-PT p9 N91-24166 Volume 2: Sessions 7-12 1 NASA-CP-3t15-VOL-tI] p 32 N91-20541 Control integration concept for hypersonic crulse-tun INASA-CP-1I0038-VOL-2] p 4 N91-10866 etAtrtcIeSetIiitv.Vlm .Dsiln maneuvers ~~~~~~~~~User's guide: Nimbus-7 Earth radiation budget Ws naci c he ntaie oueZDsiln

fNASA-TP.31361 p 13 N92-20195 narrow-fielId-of(-view products, Se-radiance tae Reviews

The 199 1 International Conference on Aging Aircraft and products, sorting into angular bins products, and maximum [NASA-CP-315-VOL-2j p32 N91-26573

Structural Airworthiness likelihood cloud estimation products Nimbus-7 TOMS Antarctic ozone atlas. August -

fNASA-CP-31601 p 31 N92-30106 INASA-RP-12461 p34 N91-13043 December 1990

AIRCRIAFT RELIABILITY An explicit upwind algorithm for solving the parabolized INASA-RP-12641 p 35 N91-26651

The 1991 International Conference on Aging Aircraft and Navie-Stokes equations ANTENNHA DESIGN

Structural Airworthiness fNASA-rf'-30501 p4 N91-18032 On-orbit structural dynamic perormance of a 15-mester

I NASA-CP-31601 p 31 N92-30106 An upwind-biased space marching algorithm for microwave iadiometer antenna

AIRCRAFT SAFETY supersonic viscous tlow fNASA-TP-304t j p 16 N91.171 14

Aviation Saety/Automation Program Conference [NASA-TP-31368I p 26 N91-18381 A new fabrication method for precision antenna

I NASA-CP-30901 p9 N91-10936 Improvements in computational accuracy of BRYNTRN reflectors for space flight and ground test

Joint University Program for Air Transportation (a baryon transport code) !NASA-TP-30781 p 17 N91-21 185

Research. 1990-1991 1 NASA-TP-30931 p 51 N91-23017 ANTI4ROPOMETRY

INASA-CP-31311 p 3 N92,17984 Guidance, navigation. and control subsaystem equipment Responses of women to orthostatic and exercise

The development of the iqASA aviation safety reporting selection algorithm using expert system methods stresses

system INASA-TP-30621 p 42 N91-25624 fNASA.TP-3043) p37 N91 -19711

1 NASA-RP- 11141 p 10 N91 -70436 A comparison of airborne wake vortex detection ANTICYCLONES AIRCRAFT STABILITY measurements with values predicted from potential Inertial oscillation of a vertical rotating draft with Aeronautical engineering A continuing bibliography with theory application 10 a supercell storm indexes Isupplement 2751 INASA-TP-31251 p 10 N92-10994 fNASA-TP-32301 p 36 Nri2-33482

(NASA -SP-703 7(275)1 p 3 N92-28679 Space Network Control Conference on Resource APOLLO PROJECT AIRCRAFT STRUCTURES Allocation Concepts and Approaches NS nier n h g fAol Failure behavior of generic metallic arid composite I NASA-CP-3124 J p 16 N92-f 1039 (NASA-S-4 enier and the2ge2f8Aoll aircraft structur'r components under crash loads A generalized method~ for multiple robtotic nianipulator IAAS-14 5 9-64

INASA-RP-12391 p29 N91 -t3751 programming applied to vertical-up welding APPLICATIONS PROGRAMS (COMPUTERS)

Computational Structures Teclinology for Airframes, and INASA.TP-3t831 p 24 N92-t11215 A method for determining spiral-bevel gear tooth

Propulsion Systems Computational FtIu, Dynamics --- numerical methods geometry for finite element analysis

INASA-CP-31421 p 31 N92-259t1I and algorithm development I NASA-TP-30961 p 28 N92-t0195

The 1991 International Conference on Aging Aircraft and INASA-CP-100781 p 12 N92-25808 ARCHITECTURE (COMPUTERS)

Structural Airworthiness Experimental validation of Clock :,vnchmonization GuIi~nce, navigation, and control subsystem equipment

I NASA-CP-31601 p31 N92-3Ot06 algorithms siec~ion algorithm using expert system methods

AIRCRAFT TIRES I NASA.TP-3209j p 42 N92-27589 I NASA-TP-30821 p42 N91-25624

Static footprint focal forces, areas, and aspect ratios The effects of video compression on acceptability of Control Center Technology Conference Proceedings for three typ 7 aircraft tires images for monitoring life sciences experiments I NASA-CP- 1008 11 p 14 N92t12010

INASA-TP-2983l p t0 N91 17014 1NASA. 1'P32391 p 16 N92-33933 Destination-directed, packet-switchinig architecture for

Computational methods for frictionless contact wit h ALLOYS 3(. 20 -GI-z FDMA/TDM geoStalionary commumications

applicaton to Space Shuttle Orbiter nose-gear tires The interaction of hydrogen with metal alloys satellite network

(NASA-TP-30731 p 30 N91-22576 I NASA -TP 31261 p 23 N91-29318 INiASA-TP-32011I p 16 N92-19762

A-4
SUBJECT INDEX BENDING

ARCTIC REGIONS The atmrosipherrC effects of stratospherci aircraft A AUTONOMY

SAM 2 measwreaments Pt te polar stratosphreric aerosol current consensus Automrating a spacecraft electric fi p43~er Sy-stem ,slnrg

Volume 9~ October 1982 -Apr-il 1983 tilA - 1-2511 p 33 N91-16467 ""pr-I system~s

[NASA-RP-12441 p 33 N91-19505 Fr-at LOEF PosI-Retri-eval Symrposium abstracts INASA-YTP-3161 p?0 N49? 120152

AREA I 1 100~tO721 p 52 N91 249!2 AVIATION METEOROLOGY

Static footprint local forces. areas. and aspect ratios The atmosphteric etects of Stratospheric aircraft A trtSt Thre 1991 International Aerospacer &r-r Wiond-C

tor three type 7 aircr-aft fires program report CU00ren.1a rn L drfrn ar StdI., -r , ,r)'.r'Te

1 NASA-TP-29831 p 10 N91-t7014 I NASA RP-12721 p 33 N92,19121 NASA CP-3106-VOL 1 p3- N91 :32599

ARROW WINGS Sixteenth inrternrational Laser Radar Cotrter-ence Parr AVIONICS

Spai reduction etlects. on thre flutter ctraracteristics oft Aviation' Satety, A.4romatior P~oqrarr Confterence

arraw-*rtr((supersornic transport configurtirons I NASA.CP-3158-PT. It p 28 N92-2922k3 I NASA CP 30940 P9 .49r 1043,af

INASA-TP 30771 p I N9t 2112?7 Hlgh-Speed Researchr Son< Boom volume 1 Space Transportlation Av~onvcs T

ec norog Syposlurn

ARTIFICIAL GRAVITY INASA CP 3 1721 p tI IN92-33874 vo~lume 2 Contererse Pr~oCeedrrgs

Ben-efits troml synrlegies an-d advanced technologies to, ATMOSPHERIC MODELS 1NASA CP-3081 IVOL?2 p I I N91 172,

art advanced-tectrrrology space statiorn The atmospheric effects of stratospheric aircraft A NASA For-mat Melrrads vilorlssrop 1990

I NASA-TP-30671 p 14 N91-201t7

7 current consensus 'NASA-CP 100521 p-4? N49 " 751,9

ARTIFICIAL INTELLIGENCE ;NASA RP-12511 p 33 N9ti~b 147 joitLneriy Progearr for Air Tiar~ponarrorThe191 Cofeene odar rSpae ppictins NASAIMSFC Fy90 Grotar Scale AlmospheriC Research 1989 1990

The Atifcalitellgoentocolrneo paeApcto Processes Research Prog~ram Revre* I NASA CP 30951, p 14N9,1r9024 at nl~rallltllgelce 4912279 NASA-CP-3093! p3 N491-16500 AE RFRNELNS

t NASA-CP 31t0 t43 -~ý6 Vorcanrisr-Climate trrreractions AXE nor-lFearN sINES)c rr~ri~rrr 1- rga

Technology 2000 volume INASA-CP-100621 p34 1491-21641 Aetorlb aa, estacematrt etor~ rare ang

!NAA-P-t0-2L- P? 91232t Inertial osciliaton ot a vertical rotatinlg dratt -1r, ;NASA YP 3r781 p 24 N92 13343 Technology 2001 The Second National Technology applicatiorn to a superel storm.h Video SQpperrel nto AXIAL COMPRESSION LOADS Transfer Conference an-d Exposition volume I NASA TechnCal Paper 3230 -- crrresr eh-a.or ort 9raph-re Mlernopras~r and NASA CP-3136-VOILI p 52 N492-22423 lNASATP-32,30-ViDEO SUPP I p 36 N92-34246 qirapr-rrr epoxy- pane~s -111 i-crclar holes orm~c

The 1992 Godldard Contereonce on Space Applications ATMOSPHERIC MOISTURE lagt of Ant~cial intlelligence The role ot waler vapor in cimate A Str~eyterc rsarch -NASA TP 30'1 2' N9y r 82 1 1,

rN ASA-:P 31411 p 43 N92-23356 plan for the proposed GEWEX water vapor, projerct AXA LOD

The Feder-I Cantererice aon Ir-telligent Processingq fGvaP Pil ar,1 tl wc1-wlic hyvtP5 -,tiesr 

EQorprtent jNASA-CP-31t201 p) 35 N91 251516 frater.al srItsr ~ notcl

1 NASA-CP 3r38 l p52 N492-24987 ATMOSPHERIC PHYSICS NAS _P u-ý i-i N9116Ar

ASPECT RATIO NASA/MSFC Fy90 Global Scat, Atnmospnnr--c NS F0"r .1-

Staroc footprint local ýorces areas, and aspect raIrOS Processes Research Progitra Rev-erat

tor rr~ee type 7 arCratt tires ;NASA-CP-3393i p 3ý. 149. P61l3P B t NASA- TP-2983. p tONi 19- 1 70 14 NASA-MVSFf- FY91 Global Scare Almroiipr-urC

ASTRONAUT PERFORMANCE .Processes Research Progaram Rev era SACKSCArTERING

Rorab-,:Iv of- a Ssvtrle reaction tbmp N IASA CP 3r26! p325 N19 2261, Svryentri r-e'':-4,rrrr 5 -ann-rrn pa-

'NS P3t7 0N2152 application r0a uprIC" S str NAýA ,:P 3r,-ý I" PT9 2q21- ASTRONAUTICS NASA-7TP32301 p36 r492 12462 SANOPASS FILTERS

Ae-nal..le.~eln Acn~ugbt!gatwt ATMOSPHERIC RADIATION A rcnIfr lo, larýD ass lil--b'ring 1-'I- Ilderds 5- ucverý'! 2'e, L-no-dar-henr-q functions as Ilervel trorrr 4lo 'arr n!es-Iale11 t-~rr 4v rpon P0 "IK~l~ 

NIASA-So P0'2i, l N9-8 i pelratlori of lIre EPEE6 scanrning ranlomiqwrs 1

r, AugWs n-i,;w

enqaA4 rqer-Irrr A Car-ri rrung Irogvaphy Arit I985, NA rA Tl P -j 42 N4 r

PIrC Pp r-cr27,-NASA-PP 1243- p .4 -i41 6 H1-r BANDWIDTH

.So rP-A7l2`5; 3 142867Ar kilss~on ilesr-rpton ar-d inr-lgir oae~ab1315 -,f I-dkr 'lrll-0 . 7 5 p,---r p'-r-- r.

ASTRONAUTS -,stsr-onets or, ERRS andNt-iAA 9 r Nacl o-rrn~r~tr ý-I 47

r~r~-~I - r--r Sprcr-r Sldt-On P7r-doe 1114 Ja'vary 195-6 N.ASA I' 1,

-10*.. -i-i#59~%A1A PP 1256 -m,:-'5I-I

-,4,A o 40 9 16i ATMOSPHERIC SOUNDING -,-

ASTRONOMICAL MODELS NASA y A...rr

P~oýis~~s nP'o'a-BARYONS

ASTRONOMICAL SPECTJROSCOPY ATMOSPHERIC TURBULENCE .

4 37t '1 rP BASE PRESSURE

ASTRONOMY

P 1 5,5P %

ASTROPHY'SICS ATOMIC CLOCKS SAYS iSTRUCTURAL UNITS)

ATM OSPHERIC CiIEMlqTRI aY II1-*

ATTF14UATORS......

BEAMS ISUPPORTS),

ATTITUDE rlNtA INATIOHIy,

AT MOSPASfý((C CIRICUk-ATIONA

ATTI'TUDE GYROS BED REST

I ~ ~ ~ ~ AUIJITORY STIMULI -,r-

- I - rl-. SEND TESTS

- I I r A AUTOCLAVES --

AMIVOrPIIE IC COMPOS11"ON AIITOMATII. CONTROL SENDING

A, F1, OurI"r 1RI kF 14

A-5
BIBLIOGRAPHIES 

SUBJECT r NoE(

influence of mass moment of inertia on norma~l modes Large space strUCtureS and Systems In the space station SIOASTRONAIJTlCS

of preloaded solar array mast wer A bsbocgiaphyi with) indexes Aerospace medicine *nd biologry A Continuioig

(NASA.TP-3273 j p 31 N92-33476 jNASA-SP.7085(021) p 18 N91-28191 bibliography with indexes (suppiement 34 1)

SILIORPI16 Aropae edcieand Doiolgy A Ccohtnuing I NASASP-701113411)] p 37 N9 1 10594

Aeronautical engineenring. A continuing bibliography with bibliography with indexes (Supplement 352)1 Aerospace meichinees a$pInd bilgy42) m tnun

indexes (supplement 256) INASA-SP-701 1(352)] p 38 N91-218729 bibrogaSPl wi1(,4th indis Ispp91en 3412)

(NASA-SP-7037(256)] p t

i N91-10002 NASA patent abstract' bibliographly A cortinuing NAAerspacemedcin an bilog p37 Ng.10n" .

Aerospace medicine and biology A continuing bibliography Section 2 Indexies (supplement 39) Aeros~ac meichindex aspind biloyA431 en iun

bibliogiraphy with indexes (supplement 341) INASA.SP.70391391.SECT- 2 1 p 48 N91-2908 bIbigah SP- wiSA. xe (7011ement p37N9 14711

[NS-P71(4) 7N1154Aeronautical engineenng A continuing ~ e bibliography s ~ t2 with Aerospace medicine and biology, A Conmtiieiini

Arnuiaeniern:Acniun 25)(AAS.07 (supplement *ahy-nindexes 268)l 2 9-307 ogrpiy with indexes (suppleinierit 3441

indexsA(supplement25 7

)( p1 N91-P-70 728) p)5893 (NASA.SP-701t1(344)1 p 3"* NjS!1 4712l

INSASP707(5)1p N1-259 Earthi observation$ and global change decision making Aerospace medicine and biolog A ciirrriiatie 'idex

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sp NAS cia ntubic atind reernicel publicationsA canferenc bilography with indexes (supplement 153) bibliography with indexes (suppieelnet 346)

ospublicatins endltechiicslpapers.c 1989caios cofrne NASA.SP70 11(353)1 p 38 N91-31760 (NASA SP 701 1(346(1 p 37 NSA 23700

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Aeronautical engineeenng: A continuing bibliography with indexes (supplemient 267) b"*logrphy with indexes (supplement 34 7)

indexes (supplement 258) (NASA- SP.7037(267)1 p 2 I-A00 NASA- SP,7011(34 7)I p37 N91 23701

[NASA.SP-7037(258) ( p 1 N91 -13399 Aeronautical engineening, A continuing tbiblogaphy with Aerospace medicine and biology A contnining

Aerospace medicine and tiology: A continuing indexes (supplement 270) bibliography with indexes lsuppleiiient 3481

bbidgraphy with indexes (supplement 343) [NASA.-SP. 1037(270)1 p 2 N92-10973 (NASA- SP-70t1t(34811 p 3? N91-23102

(NASA-SP 401 1(343)) p 37 N91-14711 Aeronautical enrgineenng A continuing bibliography with Aerospace medicine anid biology A continuing

Aerospace medicine and biology: A Continuing indexes (supplement 269) bibliography with indexeS (Supplement 349)

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(NASA-SP-70t11(344)) p 37 N91-14712 Aerospace medicine and biology A continuinmg Aerospace medicine &nd biologry A continuing

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Aeronautical engineenng: A continuing bibliography with bibliography with indexes (supplement 355) bibliogiraph with indexes (supplement 3511

indexes (supplement 2591 1 NASA.SP701 1(355)] p 38 N92-12412 tNASA.SP-701 113511) p 38 N91-2'756

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Aerospace medicine and bioogy: A cumulative index indexes (supplement 271) biblography with indexes (supplremen 3521

to a continuing bibliography (supplemeint 345) (NASA-SP.7037(2 7 111 p 2 N92-14967 INASA.SP4OI 1(352)) p 38 N91-28729

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NASA patent abstracts bibliography. A continuing bibliography with indexes (supplement 356) bbigali ihidxs(upeet33

bibliography- Section 1: Abstracts (supplement 381 INASA-SP.7011(356)) p 38 N492-15538 (NASA.SPl701t(353), p 38 N491-31760

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Aeronautical engineenring A continuing bibliography with Indexes (supplement 2721 NS-P37) Aeopc n 40g puci A 42 16562u~n

indexes (supplement 262) [NASA-SP-7037(272)1 p 3 N492-21844 Aebiorospace meicindees andu blogyn A3o5in)n

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[NASA.SP.70t1(346)1 p 37 N491-23700 Large space structures and systems in the Space station bibliography with indexes (supplement 359)

Aerospace medicine and biOlg A continuing era A bibliography with indexes (supplement 03) 1 NASA-SP-101 1(359)1 p 39 N92-21715

bibliography with indexes (supplement 347) (NASA-SP-7085(03)] p 18 N492-22317 Aerospace medicine and biology A Cumnulative rindes

(NAA-P-013p) p37 N491-23701 NASA patent abstracts bibliography: A continuing to a continuing bibliography Isupplement 3581

Aerospace medicine and biology: A Continuing bibliography Section I Abstracts (supplement 401(4SS7I(5) 3 4222

bibliography with indexes (supplement 348) 1 NASA-SPx.7039140)-SECT-1 I( p 48 N9,2-22508 Aerospace medicine and boiogy, A continuing

[NASA.SP.701I(348)] p 37 N91-23702 Continuous improvement. A bibliography with indexes, bibliography with indexes Isu~plement 362)

Aeronautical engineening. A continuing bibliography with 1989-1991 tINASA-SP.,Ott(362() p 39 N492-27068

indexes (supplement 2651 INASA-SP-70971 p 47 N492-22665 Aerospace medicine and biology. A continuing

(14ASA-SP7037(265)1 p2 1,191-24095 Aerospace medicine arnd biology A continuing bibliography with indexes (supplement 361i

Aeronautical engineering: A continuing bibliography with bibliography with indexes (supplement 382) 1 NASA-SP-101 11361)H p 39 N92-27433

indexes~~~~~~~~ (upeet23 NSSP71(2)p39 N92-27068 Aerospace medicine and biloogy A continuing

INASA-P-703(263p p2 N91-24096 Management, A bibliography for NASA managers bibliography with indexes (supmet33

Aeronautical engineening: A continuing bibliography with I NASA-SP.750(3026( p 47 N92-78 AAS'0 161 919-06

indees 64)NASA Suplemnt patent abstracts bibliography A continuing BVODYI4AtICS

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Aerospace medicine and biology. A continuing INASA-SP.7039(401.SECT-21 p 48 N492-27081 joint strength fronm lean body mass

bibliography with indexes (supplement 349) Aerospace medicine and biology A continuing I NASA-TP-3207 I p 40 1492 26682

)NASA-SP.7011(349)) p37 N491-24731 bibliography with indexes (su)pplement 361) BIOLOGICAL EFFECTS dbogy Acniug

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INASA-SP-7500)25)l p46 N91-24936 Aeronautical engineering A continuing bibliography with bibliography with indexes ISulmet41

NASA scientific and technical publications: A catalog indexes (supplement 2771 1 NASA-SP. 701 1134Ill p 37 N91-1059A

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A-6
SUBJEC T INDEX CARBON FIBERS

Aerospace medicine and biology A continuing Two-dimensional aerodynamic characteristics W Save, al BOUNDARY LAYERS

bibliography with indexes (Supplement 348) polygon-shaped cross-Sectional models applicable to Evaluation of a Technique to generate artificially

I NASA-SP-7011f348)) p 37 N91-23702 helicopter fuselages thick~ne boundary layers in supersonric and ntypersonic

Aerospace medicine and biology A continuing INASA-TP-32331 p 8 N92-30394 flows

bibliographty with indexes (Supplement 3.49) BOATTAI IS INASA-TP-31421 p 6 N91-28136

[NASA -SP- 7011(349)1 p 37 N91 -24731 Effect of afterbody geometry on aerodynamic Calculation of unsteady transonic flows with mild

Aer'space m'edicicne and biology A continuing characteristics of isolafexi nonixisymmetric alteri-odies Pf sepieatratc t' . tc-- r nterac'4cbibliography wifth indeses (supplement 350) transoni Mach numbers INASA-TP-31 971 p 7 N9?-2S477

I NASA-SP-701 ff350)) p 38 Ng 1-25600 INASA-TP-32361 p 9 N92-33706 Validation of three-dimenirsional irrcompressitile spatial

Aerospace medicine and biology A continuing DWYWIG CONFIGURATIONS direct numerical simulation code A comparison with linear

bibliography with indeixes (supplement 351) Transonic Symposium Theory. Application anid stability and parabolic stability equation trieories for

[NASA-SP-70t11)351)) p 38 N91-27756 Esperiment, volume 2 onayterrnsinonaftple

Aerospace medicine [NASA-CP-3020-VOL-21 p 5 N91-24 132 boil TP325 y trasiioo3a0la9p5t py and biology A continuing TNAansonic05 and sueronc-309omuttinso

bibliography with indexies (Supplement 352) Toran~omnicand sup ferdsaonic Euleeri computaton of RAXES (FOR ARRESTING MOTION)

I NASA-SP-70t1t(35211 38 N9128729 vorAtex-domiate flo fild aou ageerc igte Determination of the flight hardware configuration oflan

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INASA-TP-31241 p 42 N92-t11885 drag-due-to-lifI minimization with recommendations tor eirpertin se spaerf lcrclpwrsse sn

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bibliography with indexes (supplement 354) 1 NASA-TP-3202 t p 9 N92-33656 I NASA -TP- 31611 p20 N492-12052

)NASA-SP-70t1)(354)1 p 38 N92-1 2404 BOEING AIRCRAFT SUCKLING

Aerospace medicine and biology A continuing Lewis icing research tunnel test of the aerodynamic Research in Structures, Structural Dynamics and

bibliography with indexes (supplement 355) effects of aircraft ground deocing/anti-cn fluids Matenials. 1990

[NASA-SP.7011(355)) p 38 N92-12412 I NASA-TP-3238) p t0 N92-30395 [NASA-CP-30641 p 29 N491L 10301

Aerospace medicine and biology, A continuing BOILER PLATE Suckling and vibration analysis of a simply supported

bibliography with indexes (supplement 356) Long-term orbital lifetime predictions column with a piecewvise constant cross section

I NASA-.SP_7011(356)1 p 38 N92-15538 I NASA-TP-30581 p 13 N491-10092 INASA-TP-30901 p 29 N491-20503

Aerospace medicine and biology A continuing BOME DEMINERALIZATION Effect of low-sPeed impact damage and damage location

bibliography with indexes (supplement 357) Workshop on Exercise Prescription for Long-Duration on behavior of composite panels

(NASA-SP-7011(357)] p 39 N492-21714 Space Flight tNASA-TP-3t961 p 22 N192-23981

Aerospace medicne and biology: A continuing INASA-CP.30511 p36 N91-10574 Buckling behavior of long symmetrically laminiated plates

bibliography with rndeses (supplement 359) Techniques for determination of impact forces during subtecfed to combined loadings

[NASA-SP-70t11359)1 p 39 N92-21715 walking and running in a zero-G environment )NASA.TP-31951 p 22 N492-25160

Aerospace medicine and biology A cumulative index [ NASA-TP-3 159) p 38 N92- 17022 BYPASS RATIO

oacotnigbbigah(splmn35)BOOSTER ROCKET ENGINES installation effects of wing-mounted tfurtioan

to NaS-P71 cotnun 1 (suppemen0326 39logah Parametnic trade studies on a Shuttle 2 launch system nacelle-pylons on a 1/17-scale, twin-engine. low-wing )NSASP70 t35))p3 1922226 architecture transport model Nutritional Requirements for Space Station Freedom [NASA-TP-30591 p 14 N491-18180 INASA-TP-31681 p 7 N492-19002 Crews

INASA-CP-31 461 p 40 N492-25961 Space Transportation Propulsion Technology BYPASSES Symposium Volume 1. Executive summary Modeling of the heat transfer in bypass transitional Aerospace medicine and biology A continuing I)NASA-CP-31121 p 19 N491-25176 boundary-layer flows bibliography wit h indexes (supplement 362)BONAISIAA.P371p2 N2129

I NAA-S-701(36)1 p39 92-2068 Validation of three-dimensional incompressible spatial Aerospace medicine and biology. A continuing direct mimencal simulation code A comparison with linear bibliography with indexes (supplement 361) C )NAS-SP-d~t~6t)(p39boundary-layer transition on a flat plate

Aerospace meiieadbooyAcontinuing ) NASA-TP-32051 p 8 N492-30295 CABLES (ROPES) bibliography with indexes (Supplement 363) Applications 0f FEM and BEM in Iwo-dimensional Cable compliance

[NASA-SP-7011(363)1 p39 N492-30987 fracture mechanics problems INASA.TP-32t6 p 24 1492ý30378

Track structure model of cell damage in space flight I NASA-TP-32771 p31 1492-3t280 CALIBRATING I NASA-TP-32351 p39 N492-34154 BOUNDARY CONDITIONS User's guide Nimbus-7 Earth radiation budget

BIOLOGICAL EVOLUTfON Panel methods An introduction narrow- field-of-view products Scene radiance tape Fourth Symposium on Chemical Evolution and the Origin INASA-TP-29951 p5 N491-19058 Products. soiting into angular bins Products. and maximum and Evolutioni of Life Validation of three-dimensional incompressible spatial likelihood cloud estimation products

fNASA-CP-3t 29) p A i 92-1 3588 direct numerical simulation code. A comparison with linear (NASA-RP-1246] p 34 N491-13043

BIOLOGICAL MODELS (MATHEMATICS) stabi'ity and parabolic stability equation theories for Calibration of the 13- by 13-inch adaptive wail test

Cellular track model o1 biological damage to mammalian boundary-layer transition on a flat plate Section for the Langley 0 3-meter transonic cryogenic cell cultures from galactic cosmic rays ) NASA-TP-32051 p 8 N92-30295 tunnel I NASA-TP-30551 P 50 N491-16981 BOUNDARY ELEMENT METHOD I NASA-TP-30491 p 13 N91-13461

Radiation risk predictions for Space Station Freedom Analysis and prediction of Multiple-Site Damage (MSDf Nimbus-i TOMS Antarctic ozone atlas August -

orbits ftgecakgot eebr19

9.60 )NS-P391PS NASA-TP-32311 p 31 N92-31279 INASA-RP-1264( p 35 N491-26651 BIOMEDICAL DATA Applications of FEM and BEM in two-dimensional Development of the Burst and Transinl Source Eva luation 0f nonlnivasive cardiac output methods during fracture mechanics problems Experiment (BATSE)

exercise I NASA-TP-32771 p 31 N492-31280 I)NASA-RP- 12681 p 4

9 N491-320306 INASA-TP-31 741 p 38 N92-16553 BOUNDARY LAYER CONTROL CALORIC REGUIREMENTS

SIOREACTORS Evaluation of cloud detection instruments and Fuel utilization during exercise after 7 days of bed rest

Experimental measurement of the orbital paths of performance ot laminar-flow leadling~edge test articles I)NASA-TP-31751 p 38 N92-16554

particles Sedimenintrg within a rotating viscous fluid as during NASA Leading-Edge Flight-Test Program CAMBERED WINGS

inflluericedi by gravity iNASA-TP-20881 pit 14,91-24199J Survey and analysis of research on supersonic

INASA-TP-32001 p 40 N92-28l897 BOUJNDARY LAYER FLOW drag -due-to -lift minimization with recommendations for

BioloialieSuprtTcnooieRomeca Wall -interferen ce assessment and corrections for wing design Bilgia upotTeholge if Cmeril transonic NACA 0012 airfoil data from various wind CAINASA -TP-32021 p 9 N492-33656 Opportunities tunnels CPACITANCE

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BIOTECHNOLOGY mea1surements

Technology 21101 The Second National Technology Modeling of th eltase nbps rnrifa NS-P17)p819-73 Transfer Conference and Exposition. volume 1 boundary-layer flows CARBOHYDRATE METABOLISM

I NASA-CP-3t36-VOL-1 I p 52 N92-22423 I NASA-TP-31701 p 27 N492-11299 Fuel utilization during exercise after 7 days of bed rest

BLADE TfIPS BOUNDARY LAYER TRANSITION INASA.TP 31751 p 38 N492-16554

Wake geometry effects on rotor blade-vortex interaction Longitudinal aerodynamic characteristics of a subsonic. CARBON DIOXIDE

noise ditectivity energy -efficient transport contiguratic~n in the National Evaluation of nonlnvasive cardiac output methods during

I NASAýTP-301 51 p44 N91-12315 Transonic Facility exercise

BLADE-VORTEX INTERACTION fNASA-TP-29221 p6 N91-28143 INASA-TP-31741 p 38 N492-16553 Wake geometry effects on rotor blade-vortex interaction Modeling of the heat transfer in bypass transitional CARBON FIBER REINFORCED PLASTICS

noise directivity boundary-layer flows A statistical comparison of two carbon fiber/epoxy

INASA TP 30 151 p 44 14111-12315 ;NASA-TP-31701 p27 1492-11299 fabricationltechniques

BLUNT BODIES Validation of three-dimensional incompressible spatial I NASA-TP-31 791 p 22 N92-20950

Siuaino elgselcso rsuedsrbtos direct numerical simulation code A comparison with linear CARBON FIBERS

for iferoas5it flightl riperi~imln vehicle and comparison stability and parabolic stability equation theorieS for A statistical comparison of two carbon fiber/epoxy withi prediction boundary-layer transit ion on a fiat plate fabrication techniques

INASA TP-3t157) p 27 N492-20677 iNASA-TP-32051 p 0 N92-30295 INASA-TP-31 791 p 22 N492-20950

A-7
CARBON MONOXIDE SL/BJECr INDEX

CARBON MONOXIDE CHEMICAL EVOL.UTION CODING

The Interstellar Medium in External Galaxies Summaries Fourth Symposium on Chemical Evolution and the Origin Advanced Modulation and Codding Technology

of contributed papersa anid Evolution of Life Conf erence I NASA-CP-30S41 p 49 N91-14100 I NASA-CP-3129j p 41 N92-13588 (NASA-CP-100531 p 16 N492-22001 CARDIAC OUTPUT CHEMICAL PROPERTIES COHESION

Evaluation of noninvasive cardiac output methods durnog Sand and Dust on Mars Equivalent crystal tiesory of alloys exercise ( NASA-CP- 100741 p 50 N91-27057 INASA-TP-3155J p23 N91-30318l

I NASA-TP-31741 p 38 N92-16553 CHEMICAL PROPULSION COLLISIONS

CARDIOVASCULAR SYSTEM Lunar missions using chemical propulsion System Paerid and interacting Galaxies International

Workshop on Exercise Prescription for Long-Duration design issues Astronlomiical Union Colloquium No 124

Space Flight I NASA-TP-303651 p 19 N91-15308 INASA.CP-30981 p 4

9 NOI-16858

JNASA.CP.3051 I p 38 N91-10574 Orbital detrirs Technical issues and future directions

CARTS CIRRUS CLOUDS NS-Pt07p4 N934a

Determtination of the flight hardware configuration of an FIRE Science Results 1988 COLUMBA-P1 7 p(O9BITER347

energy absorbing attenuator for the proposed Space INS-P38!p4N1148 The microgravity environment of the Space Shuttle

Station cre* and equipment transltation axd can? CIVIL AVIATION Clmi Kdc uigSS3 [NS-P381p 29 N91-21 558 Flight tests with a data link used for air traffic control ColmbASAT.1 midc duin NSTS1-93

CNASCADEP.FLOW information exchange The microgravity environment of the Space Shuttle

Laser anemometer measurements and computations in INASA-TP-3 1351j p 11 N491-31143 Coblumbia payload bay during STS-32 an annular cascade of high turning core turbine vanes Computational Structures Technology tor Airframnes and (NASA-TP.3141 f p 49 N92-1 1921

I NASA-TP-32521 p 8 N92_28980 Propulsion Systems COLUMNS (SUPPORTS)

CATALOGS (PUBLICATIONS) INASA-CP-31421 p 31 N92-2591 1 Buckling and vibration analysis of a simply supported NASA scientific and technical publications: A catalog CLIMATE column with a piecewise constant cross section

of special publications, reference publications, conference Climate Impact of Solar Variability INASA TP-3090 J p 29 N9 120503

publications, and technical papers, 1989 1 NASA-CP-30861 p560 N491-12456 Determiniation of the flight hardware configuration of an I NASA.SP-7063(04)] p 47 N491-13374 Volcanism-Climate Interactions energy absorbing attenuator for the proposed Space NASA scientific and technical publications: A catalog INASA-CP-100621 p 34 N91-21641 Station crew and equipment translation aid cart

of special publications, reference publications, conference The role of water vapor in climate A strategic research INASA-TP-30841 p 29 N49121 558

publications, arid technical papers, 1987-1990 plan for the proposed GEWEX water vapor protect COMBUSTIBLE FLOW

[NASA-SP.7063(OS)! p 47 N91-24939 (GVaP) Computational Fluid Dynamics Symposium on CAVITIES I NASA-CP-31 201 p 35 N91 -25E56 Aeropropulsion

Flow-induced resonance of screen-covered cavities CLIMATE CHANGE I NASA-CP-30781j p 5 N91 -21062

(NASA-TP-30521 p 25 N91-15499 Climate Impact of Solar Variability COMBUSTION CHAMBERS

Expenimental investigation of porous-floor effects on !NASA-CP-30861 p 50 N91-12456 Computational Fluid Dynamics Symposium on cavity flow fields at supersonic speeds West Antarctic Ice Sheet Initiative. Volume 1 * Science Aeropl-opulsion !NASA-TP-3032 ] p5 N91-19042 and Implementation Plan INASA-CP-30781 p 5 N91421062

Effects of yaw angle and Reynolds number on [NASA-CP-3115-V0L-l I p 32 N91-20541 High-temperaturei durability considerations for HSCT

rectangular-box cavities at subsonic and transonic combustor

sped The role of water vapor in climate. A strategic research fNASA-TP-3162) p 23 N92t17070

I NASA-TP-30991 p5 N91-27124 plan for the proposed GEWEX water vapor protect An analysis of combustion studies in shock expansion Measurements of forces, moments, and pressures on (GVaP)tunlanreecdshktnes agenenri store separating from a box cavity at supersonic I NASA-CP-31201 p 35 N91-25556 tunnesAJý2 an relete Nhock2unnel

speedts Sixteenth International Laser Radar Conference, part COMBUSTION CHEMISTRY

[ NASA-TP-31 10) p 6 N92-10005 ITodmninlsaiiyo amrfae

CAVITY FLOW [ NASA-CP-3 i58-PT-1 i p 28 N492-29228 (A -Two-dimnsina stbpt 07 laminaflame

Experimental investigation of porous-floor effects on SAGE I data user's guide An analysis of combustion studies in shock expansion cavity flow fields at supersonic speeds INASA-RP-12751 p 34 N492-33097 tunnels and reflected shock tunnels

( NASA-TP-30321 p 5 N91-19042 CLIMATOLOGY NS-P321p2 9-87 CELL DIVISION FIRE Science Results 1988NA -T324Ip2N9?37 Multiple lesion track structuire, model INASA.CP-30831 p 34 N91-10448 COMBUS"TION PHtYSICS

NASATP-3851An analysis of combustion studies in shock expansion !NSATP315jp 39 N92-22186 Climate Impact of Solar Variability tunnels and reflected shock tunnels CELLS (BIOLOGY) (NASA-CP-30861 p 50 N91-12456 I NASA.TP-3224j p 22 N92-28374 Cellular track model of bioloical damage to mamnmalian The atmospheric effects of stratospheric aircraft: A COMBUSTION PRODUCTS cell Cultures from galactic cosmic rays topical reviewOtiamesrensnsodspcesofsldoke

!NSATP305!p5 N1-69 I NASA-RP-12501 p 33 N91-16466 Motor exhaust and solid rocket motor slag Radiation nisk predictions for Space Station Freedom West Antarctic Ice Sheet Initiative. Volume 2 Discipline (NASA.TP.31771 p 20 N92-20949 orbifReiew

(NASA-TP-3098 j p 5t N91-26107 r~vesCOMMERCIAL AIRCRAFT

Cellular repair/misrepair track modet INASA-CP-3115-VOL-21 p 32 N491-26573 Annoyance caused by aircraft en ro~ute noise

[NASA-TP-31241 p 42 N92-11685 International Workshop on Stratospheric Aerosols: INASA.rP.3165! 0)45 N492-20479

Muffiple lesion track structure model Measurements, Properties, and Effects COMMUNICATION NETWORKS

(NASA-TP-31851 p39 0492-22i86 I NASA-CP-31 14! p 32 N91-32528 Structural factonring approach for analyzing stochastic

Experimental measurement of the orbital paths of CLOCKS networks

particles sedimenting within a rotating viscous fluid as Experimental validation of clock synchronization (NASA.TP.3069j p43 N91-18753

influenced by gravity algorithms Control Center Technology Conflerence Pioceedings

(NASA-TP-32001 p 40 N92-28897 INASA-TP-32091 p 42 N92ý27589 [NASA-CP-10081] p 14 N952-12010

Track structure model of cell damage in space flight CLOSED ECOLOGICAL SYSTEMS Space Communications Technology Conference

(NASA-TP-32351 p 39 N492-34154 Biological Life Support Technologies Commercial Onboard Processing and Switching

CENTAUR LAUNCH VEHICLE OpportunitiesI A ZP321p5N2140 Graphite/epoiry composite adapters for the Space [NASA-CP-30941 p 36 N91-13842 ProagatioCP.31321 r an mo satelltesytem 25l 

Shuttle/'Centaur vehicle Controlled Ecological Life Support Systems: Natural and Overview of experimental and modeling results

tNASA-TP-30141 p 15 N492-31251 Artificial Ecosystems I NASA-RP-12741 p 25 N492 20404

CERAMIC COATINGS INASA-CP-ID0401 p 40 N491-24744 COMMUNICATION SATELLITES Gibbs free energy of reactions involving itiC. Si304. H2. CLOOD PHYSICS A new fabrication method for precision antenna end H20 as a tunctiorn of temperature and pressure Volcanism-Climate Interactions reflectors for space flight and ground lest INASA-TP-32751 p 23 N492-31278 INASA-CP-100621 p3-f N491-21641 I NASA-TP-30781! p 17 N91.21165

CERAMIC MATRIX COMPOSITES CLOUDS Sae Cmuiain ehooy Cneec

High-temperature durability considerations for HSCT Evaluation of cloud detection instruments and Space Proesningatind SwTching lg oneec

Combustor performance of laminar-flow leading-edge test articles !NASA-CP.3 132! p 25 N492-14202 (NASA-TP-31621 p 23 0492-17070 during NASA Leading-Edge Flight-Test Program CHANNEL FLOW INASA-TP-28688p It N91-24199 Destination-directed, packret. switchinig arcriitecture for

A weakly nonlineair theory for wave-vortex interactions CLOUDS (METEOROLOGY) 30120-GHz FOMA/TOM geostationary communications

in curved channiell flow Atlias of the Earth's radiation budget at measured by satellite network

(NASA-TP-3t581 p 7 N92-19175 Nimbus-7 May 1979 to May 1980 (NASA.TP 32011 0 16 N492-19762

CHAOS INASA-PP- 1263! p 35 N491-24720 COMPLEX SYSTEMS

Steady induction effects in geomagnetism Part IA: COBALT Model reduction by trimming for a class of sem-Markov

Steady motionalt induction of geomagnetic chaos The 23 to 300 C demagnetization resistance of reliaoitity, models and the corresponding error bound

I NASA TP-3272-PT- IA! p 34 N492-32655 samarium cobalt permanent magnets I NASA TP-30691 p43 N9`1.25741

CHARGED PARTICLES INASA-TP-31 191 p 25 N92-11252 COMPONENT RELIABILITY Transrtilii methods and interactions for space COCKPITS Reliability of a Shuttle reaction timer radiations Aviation Safety/Automation Program Conference I NASA-TP L3176! p 40 N492 16562 [NASA.RP-12671 p 5I N92-15956l INASA-CP-30901 p 9 N491 10936 COMPOSITE MATERIALS

CHEMICAL COMPOSITION CODERS National Educators Workshop update 1991 Standard

Electrical and chemical interactions at Mars Workshop. Long-term tile testing of Geostationary Operational Experim-ents in Engineering kialeriais. Sciencri and part I Environmental Satellite (GOES) encoder lamps Technology

I NASA-CP-100931 p 50 N92-30302 I NASA RP-12731 p 23 N492-20063 I NASA.CP.31511 p 24 N92 30263

A-8
SUBJECT INDEX CONFERENCES

COMPOSITE STRUCTURES Workishop on Gnid Generation and Related Areas MIRACAL A mrsasion radiation calculation program for

Structural properties of laminated Douglas fir/epoxy INASA-CP-10089] p 12 N92-25712 analysis of lunar arnd interpianetary miraaaons

composite material Trajectory fitting in function space with application to INASA-TP-32111 p 5t N92-25t00

INASA-RP-1236 I p 20 N91 .10127 analytic modeling of Surfaces COMPUTER SYSTEMS DESIGN

Research in Structures. Structural Dynamics and (NASA.TP.32321 p 8 N92-30747 Technology 2000. volume I

Materials, 1990 Direct simulation of high-speed mixing layers INASA-CP-3109-VOL-1 Ij p 52 N91-23021

INASA-CP-30641 p 29 N91-10301 INASA.TP-3186) p 8 N92-30909 NASA-LaRc Flight-Criical Digital Systems Technology Free vibrations of thin-walled semicircular A method for designing blended wing-body Wokso

graphite-epoxy composite frames configurations for low wave drag INASA.CP-10028) p 11 N91-24200

INASA-TP-30101 p 29 N91-13750 I NASA- TP-3261 Jp 8 N92-32480 COMPUTER SYSTEMS PERFORMANCE

NASA workshop on impact damage to composites COMPUTER strutura DESINaipeorncofa1-tr Advanced techniques in reliability model representation

INASA-CP-100751 p 21 N91-29240 Onobtsrcua yai efrac fa1-itr and solution

Optimization of composite sandwich cover panels microwave (NASA-TP-304t1 radiometer antennaINS-P321p4 N9348 p16 NSI1-71t NSAT-22)p34B 38 subjected to compressive loadings Guidance, navigation. and control subsystem equipment COMPUTER TECHNIQUES

INASA-TP-3173J p 21 N92-20679 selection algorithm using expert System methods Report of the workshop on Aviation Safety/Autornationr

Graphrite/epoxy composite adapters for the Space INASA-TP30821 p 42 N91 -25624 Program

Shuttle/Centaur vehicle A method for determining spiral-bevel gear tooth INASA-CP-100541 p 9 N91-15141

I NASA-TP-30141 p 15 N92-3t2511 geometry for finite element anvalysis Technique to etiminate computational instability in

Eighth DOD/NASA/FAA Conference on Fibrous [NASA.TP-30961 p 28 N92-10195 multibody Simulations employing the Lagrange multiplie

Composites in Structural Design, pert I Second CLIPS Conference Proceedings, volume 1 (NASA-TP-32201 p 42 N92-23432

I NASA-CP-3087-PT-t I p 22 N92-32513 I NASA-CP-10085-VOL-1 p 42 N92-16W4 COMPUTER VISION

Eighth DOD/NASA/FAA Conference on Fibrous Software Surface Modeling and Grid Generation The 1 991 Goddard Conterence on Space Applications

Composites in Structural Design. part 2 Steenring Committee of Artificial Int elfligence

(NASA-CP-3087-PT-21 p 22 1N92-32574 INASA-CP-31431 p 42 N92-24397 [NASA-CP-31 t01 P4 3 N9t-22169

COMPRESSIBLE FL~OW Computational Structures Technology for Airframes and COMPUTERIZED SIMULATION

Evaluation of a technique to generate artificialty Propulsion Systems A scheme for biandpass; filtering magnetometer

thickened boundary layers in supersonic and hypersonic I NASA-CP-31 421 p 31 N92-259t i measurements to reconstruct tethered satellite sliprope

flows COMPUTER AIDED MANUFACTURING motion

(NASA-TP-3142I p 6 N91-28136 The Federal Conference on Intelligent Processing INASA-TP-31231 p 42 N91-25629

COMPRESSION LOADS Equipment Analyses of risks associated with radiatin exposure Optimization of composite sandwich cover panels (NASA-CP-31381 p 52 N92-24987 from past maior Solar a vents

subjected to compressive loadings COMPUTER AIDED TOMOGRAPHY [NASA-TP-31371 p 50 N91-3106t

I NASA-TP-31731 p 21 N92-M079 Second Conference on NOS for Aerospace Modeling of the heat transfer in bypass transitional

COMPRESSION TESTS Requirements boundary-layer flows

Properties of three graphite/toughened resin INASA-CP-3091 p 16 N91-18199 INASA-TP-3170] p 27 N92-1 1299

composites COMPUTER INFORMATION SECURITY Human Machine Interfaces for Teleoperators and Valua

INASA-TP-3t021 p 21 N92-t0067 Proceedings of the Sejcond Annuat NASA Science Environments Conference

Experimental behavior of graphite-epoxy Y-stiffened Internet User Working Group Conference INASA-CP-10071 p p40 N92-1 1638

specimens loaded in compresson [NASA-CP-31 171 p 48 N9 1-27009 Flight deck benefits of integrated data link

INASA-TP-3171 1 p 30 N92-23115 COMPUTER NETWORKS communication

COMPRESSIVE STRENGTH Proceedings of the Second Annual NASA Science INASA-TP-3219) p t0 N92-21459

A statistical comparison of two carbon fiber/epoxy Internet User Working Group Conference Fault tolerance of artificial neural networks with

fabrication techniques I NASA-CP-3t1171 p48 N91-27009 applications in critical systems [NASA-TP-3t791 p 22 N92-20950 Control Center Technology Conference Proceedings [NASA-TP-31871 p 42 N92-22285

COMPUTATION I NASA-CP.1008 11 p 14 N92-12010 Technique to eliminate computational instability in

Computational methods for finctionless contact with COMPUTER PROGRAMMING multibody simulations employing the Lagrange mulitiplier

applicat ion to Space Shuttle Orbiter nose-gear tires Space Transportation Avionics Technology Symposium [ NASA-TP-32201 p 42 N92-23432

tNASA-TP-30731 p 30 N91-22576 Volume 2: Conference Proceedings Vatidation of thiree-dwimensioriat incompressible Spatial COMPUTATIONAL FLUID DYNAMICS I NASA-CP-308 I -VOL-2 p P I1 N91 -17020 direct numerical simulation codea A comparison with lnintear

NASA Computationat Fluid Dynamics Conference. COMPUTER PROGRAMS stability and parabolic stability equation theonies for

volume I Sessions 1-6 Transonic flow analysis for rotors, Peat 3 boundsry-layer transition on a flat plate [NASA-CP- 10038-VOL- 1 p4 N91.10839 Three-dimensional, quasi-steady. Euler calculation INASA-TP-32051 p 8 N92-30295

NASA Computational Fluid Dynamics Conference 1NASA-TP-23751 p3 N91-10007 Direct simulation of high-speed mixing Layers

Volume 2 Sessions 7-12 Prediction of effects of wing contour modifications on (NASA-TP-3186J p 8 N92-30909

I NASA-CP- 10038-VOL-21 p 4 N91-10868 low-speed maximum lilt and transonic performance for the Advanced techniques in reliability model representation Computationiaf Fluid Dynamics Sympoxium on EA-68 aircraft and solution

Aeropropulsion I NASA-TP-30461 p 4 N91-10902 [NASA-TP-32421 p 43 N92-33A83

I NASA-CP-30781 p 5 N91-21062 Navier-Stokes and Eufer solutions for lee-side flows over Reconfiguring the RUM experiment to test circular

Transonic Symposium Theory. Application and supersonic delta wings A correlation with experiment scanning withl rotating unbalanced-mass devices on

Experiment, volume 2 1 NASA-TP-3035) p 4 N91-134011 gimbaled payloads (NASA-CP.3020-VOL-2) p 5 N91-24132 Physically weighted approximations of unsteady I NASA-TP-32821 p 25 N92-33601

Advanced Hlypervelocity Aerophysics Facility aerodynamic forces using the minimum-state method tInertial oscillation of a vertical rotating draft with

Workshop [NASA-TP-3025) p4 N9t-18031 application to a supercetl storm: Video supplement to

JNASA-CP-tCO3t I p 13 N91-24211t Panel methods- An introduction NASA Technical Paper 3230

Shock wave interaction with an abrupt area change INASA-TP-29951I p 5 N91 -19058 I NASA-TP-3230-VIDEO-SUPPL I p 36 N92-34246

I NASA-TP-3113; p86 N91-27140 State estimation applications in aircraft flight-data CONFERENCES

Seals Flow Code Development analysis, A user's manual for SMACK Research in Structures. Structural Dynamics and

INASA-CP-t00701 p 15 N92-15082 INASA-RP-12521 p 10 N91-19082 Materials, 1990

Software Surface Modeling and Gnid C. -neration Aeropropufsion 1991 iNASA-CP-30641 p29 NSI-10301

Steering Committee INASA-CP-100631 p 12 N9 1-20086 FIRE Science Results 1980

1NASA-CP-31431 p 42 N92-24397 Improvements in computational accuracy of BRYNTRN [NASA-CP-30831 p34 N91-10448

Workshop on Engineering Turbulence Modeling (s baryon transport code) NASA Computational Fluid Dynamics Conference,

(NASA-CP-100881 p 27 N92-24514 (NASA-TP-30931 p 5I N91-23017 Volume 1: Sessions 1-6

Computational Fluid Dynamnics -- numerical methods Technology 2000, volume 1 1 NASA-CP-t10038-VOL-1 I p4t N91.10839

and algorithm development I NASA-CP-3109-VOL- I I p52 N91-.23021 NASA Computational Fluid Dynamics Conference,

I NASA-CP- 100781 p 12 N92-25808 Development of an integrated aeroservoelasfic analysis Volumne 2 Sessions 7-12

NASA Workshop on future directions in surface modeling program and correlation with lest data I NAS-P-t10038VOL-21 p4 N91 10868

and grid generation (NASA-TP-31201 p 2 N91-261 13 Aviation Saffety/Automration Program Conference

I NASA-CP-100921 p 8 N92-29625 A three-dimensional finite-element thermal/mechanical INASA-CP-30901 pg Net-10936

Stagnation-point heal-transfer rate predictions at anltcltcnqefrhg-effac rvln ae Twenty-Second Annuel NASA Supply and Eqiupmi'ent

aeroassist flight conditions anlticltcnquboeihpefracsraeigwv Management Conference

I NASA-TP-32081 p 27 N92-31281 INSTP381p 25 N91-27436 INASA-CP-100421 p46 N91-t 1591

Tenth Workshop for Computational Fluid Dynamic INS-P381Airborne Wind Sheat Detection and Warning Systems

Applicatiuris in Rocket Propulsion, part 2 HZETRN Aheavy ion/nucleon transport code for space Second Combined Manufacturers' and Technofogists'

1 NASA-CP-3163-PT-21 p 27 N92-32245 rxdiations Cofrne.pr Tenth Workshop for Computational Fluid Dynamic NASA-TP-31461 p 5t N92-15959 Conference, 00pat. 1 9N9- 8

Appl~cations in R-ktie Propulsion, part t Optimization of composite sandwich cover panels Airborne Wind Shear Detlection and Warning Systerns I NASA-CP 3163-PT-tI p 27 N92 32278 subjected to compressive loadings Second Combined Manufacturers' and Technologists* COMPUTATIONAL GRIDS ( NASA-TP-3t731 p 21 N92-20679 Conference, pert 2

NASA Computational Fluid Dynamics Conference An efficient HZETRN (s galactic cosmic ray transport (NASA-CP-10050-PT-21 p9 N91-1 1695

volume I Sessions t -6 code) Measurement and Characterization of the Acceleration

I NASA-CP. 1 0038 VOL.-I I p 4 N91,10839 INASA-TP-31471 p 51 N92-22218 Environment on Board the Space Station

Relative efficiency and accuracy of Iwo Navier-Slokes Improved accuracy for finite element structural analysis [NASA-CP-30881 p 48 N91-12401

codes for simulating attached transonic flow over wings via a new integrated force method Climate Impact of Solar Variability

INASA-TP-30611 p26 N91-i73t0 I NASA-TP-32041 p 30 N92-22227 INASA-CP-30661 p 50 N91-12456

A-9
CONNECTORS SU8JECT INDEX

The Interstellar Mediumin Ealernal Galaxies. Summaries NASA workshop on impact damage to composites National Educators' Workshop Update 1991 Standard

of contributed papers I NASA-CP-100751 p 21 N91-29240 Experiments in Engineering Materials Science and

INASA.CP-30841 p49 N491 14100 Space Photovoltaic Research arid Technology Technology

Interstellar Dust: Contributed Papers Conference I NASA-CP-3151 I p 24 N92-30263

INASA-CP-3036) p 48 N91-14897 INASA-CP-31211I p 19 Ntll-30203 Electrical and chemiucalmIneractions at Mars Workshop. Report of the workshop on Aviation Safety /Automation The 1991 International Aerospace and Ground part 1

pogram Conference on Lightning arid Static Electricity, volume 1 INASA-CP-1009fll p 50 N92-30302

I NASA-CP- 100541 p 9 N91-15141 [NASA-CP-3106-VOL-I j p 3 N91-32599 Sixteenth International Lase( Radar Conference part Space Station Freedom Toxic and Reactive Materials Magnatoplasmadynamric Thruster Workshop 2NS-P35-t.)p8N2t1 Handling [AACA04 0N2104 [AAC-18P-1p2 9-11

[NASA-CP-30851 p48 N9t-15930 AACPt84p2 N9l)04 Tenth Workshop for Computational Fluid Dynamic Fourth International Symposium on Long-Range Sound Control Center Technologyr Conference Proceedings Apiplictions in Rocket PropulSion, pai 2

Propagation INASA-CP-100811 p 14 N92-12010 INASACP-3I63-PT-2 p 27 N92-32245

(NASA-CP-31011 p 44 N9 I-ý16682 Fourth Symposium on Chemical Evolution and the Origin Tenth Workrshop for Computational Fluid Dynamic Paired and Interacting Galaxies: International and Evolution of Life Applications in Rocket Propulsion. part 1

Astronomical Union Colloquium No. 124 1 NASA-CP.31291 p 41 N92-13588 (NASA-CP-3163-PT-1 I p 27 N92-3227o

I NASA-CP.30981 p49 N91.16856 Space Communications Technology Conterence Eighth DOD/NASA/FAA Conterence on Fibrous

Space Transportation Avionics Technology Symposium Oinboard Processing and Switching Composites in Structural Desin, part 1

Volume 2: Conterence Proceedings INASA-CP.31321 p 25 N92114202 fNASA-CP-3087-PT-1I I p 22 N92-325 13

INASA-CP-3081 -VOL-21 p 11 N9t1A7020 Rotordynmic Instability Problems in High-Perlfomance Eighth DOD/NASA/FAA Conference on Fibrous

Flight Mechanics/Estimnation Theory Symposium, 1990 Turbomachinery. 1990 Composites in Structural Design. parn 2

1 NASA-CP.31021 p 14 N91-17073 I NASA-CP-31221 p 28 N92-14346 INASA-CP-3087-PT-2j p 22 N92-32574

NASA Formal Methods Workshop, 1990 Second CLIPS Conference Proceedings, volume 1 Fourth Aircraft Interior Noise Workshop

INASA-CP-100521 p 42 N91-17559 I NASA-CP- I0085-VOL-tII p 42 N92-16568 (NASA-CP-101031 p 45 N92-32948

Current Collection from Space Plasmais Second CLIPS Conference Proceedings, volume 2 Proceedings 0f the 23rd Annual Precise Time arid Time

I NASA-CP-30891 p 46 N91-17713 I NASA-CP- 10085-VOL-21 p 42 N92-16590 Interval (P~tT) Applications and Planning Meeting Second Cornference on HOE for Aerospace Beyond the Baseline 1991: Proceedings of the Space INASA-CP-31591 p 44 N92-33350

Requirements Station Evolution Symposium Volumne 2 Space Station Orbital debris Technical issues anid futule drrrztions

INASA-CP-3091 Ip 16 N91-18189 Freedom. part 2 INASA-CP-10077J p 49 N92-33478

The 5th Annual NASA Spacecraft Control Laboratory I NASA-CP- 10083-VOL-2-PT-21 p 18 N92-17348 CONNECTORS

Experiment (SCOLE) Workshop, part 2 Beyond the Baseline 1991, Proceedings of the Space The 26th Aerospace Mechanisms Symposium [ NASA-CP-t10057-PT.21 p 17 N91-19122 Station Evolution Symposium. Volume 1 Space Station fNASA.CP-31471 p 30 N92-25067

Sixteenth Space Simulation Conference Confirming Freedom, part 2 CONSTRAINTS

Spaceworthiness Into the Next Millennium [NASA-CP.10083-VOL-1-PT-21 p te N92-17409 The effect of acceleration versus displacement metriods

I NASA-CP-30961 p 17 N91-19126 Beyond the Baseline 1991 Proceedings of the Space on ateady~state boundary forces

Space Photovoltaic Research and Technology, 1989 Station Evolution Symposium. Volume 2- Space Station (NASA-TP-32181 p 30 N92-21457

INASA-CP-31071 p 19 N91-1 9182 Freedom. part 1CONSTRUCTION

Proceedings of the X-15 First Flight 30th Anniversary INASA-CP.10083-VOL-2.PT-tI] p 18 N92-17768 A self-zeroing capacitance probe for water wave Celebration Visually Guided Control of Movement measurements

INASA-CP.3105J pt10 N91-20071 INASA-CP-31t81 p 39 N92-21467 INASA-RP-12781 p 36 N92-27930

National Educators' Workshop: Update 1988. Standard The Cornpton Observatory Science Workshop Software design tor automated assembly of truss

Eaperimenta in Engineering Materials Science and [NASA-CP-31371 p 49 N92-21874 structures

Technology Advanced Modulation and Coding Technology 1 NASA-TP.3198j p 43 N92-28375

(NASA-CP-30601 p 20 N91-20207 Conference CONTACT LENSES

Nineteenth NASTRAN (R) Users' Colloquium I NASA-CP- 100531 p1t6 N92-22001 An investigation of microstructural characteristics ol

I NASA-CP-31 11] p 29 N91-20506 Workshop on Squeezed States and Uncertainty contact-lens polymers Fourth Annual Workshop on Space Operations Relations [ NASA-TP-3034) p 2t N91-13492

Appilications and Research (SOAR 90) NASA-CP-31 351 p46 N92-22045 CONTAMINATION

I NASA-CP.3103-VOL'l IJ p 41 N9t1-20641 Fifth Annual Workshop on Space Operations Payload bay doors and radiator panels familiarization

Fourth Annual Workshop on Space Operations Applications and Research (SOAR 1991), volume 2 handbook

Applications and Research (SOAR 90) [NASA-CP-3127-VOL-21 p 41 N92-22324 [NASA-TM-1077931 p 15 N492ý20676 [NASA-CP-3103-VOL-2J p 41 N91-20702 Technology 2001- The Second National Tbchnology CONTOURS

Proceedings of the Second Joint Technology Workshop Transfer Conference and Exposition. volume IPrediction of effects of wing contour modifications on on Neural Networks and Fuzzy Logic, volume 2 (NASA.CP-3136-VOL-1 p p52 N92-22423 low-speed maximum lift arid transonic performance for the

)NASA-CP.10061 -VOL-21 p 43 Ng91-20811 Aeropropulsion 1987 EA-68 aircraft

Computational Fluid Dynamics Symposium on [NASA-CP.30491 p 12 N92-22510 [NASA-TP-30461 p 4 N91-10902

Aeropropulsion The 1991 NASA Aerospace Battery Workshop CONTROL EOUIPMENT

[ NASA-CP-30781 p 5 N91-21 062 (NASA-CP-31401 p 33 N92-22740 The Federal Conference on Intelligent Processing Volcanism-Climate Interactions LOEF: 69 Months in Space. First Post-Retrieval Equipment

j NASA-CP- 100621 p34 N91-2164i Symposium, part I (NASA-CP-3138j p 52 N92-24987

Proceedings of the Second Joint Technology Workshop IHASA-CP.3t34-PT-t p 52 N92-23200 International Symposium on Magnetic Suspension on Neural Networks and Fuzzy Logic, volume I Software Surface Modeling and Grid Generation Technology, part 1

(NASA-CP- 10061 -VOL- I I p 43 N91-21778 Steering Committee INASA-CP-3152.PT-i I p 18 N92 27721

Vision-21: Space Travel for the Next Millennium I NASA-CP-31431 p 42 N92-24397 CONTROL STA31IUTY

(NASA-CP-100591 p 13 N91-22139 Workshop on Engineering Turbulence Modeling A methodology toy computing uncertainty bounds o1

Fourth NASA Workshop on Computational Control of [NASA-CP-10088J p 27 N92-24514 multrearrable systems based on sector stability theory Flexible Aerospace Systems, part 2 The Federal Conference on Intelligent Processing concepts

INASA-CP-10065-PT-21 p 17 N91-22331 Equipment I NASA-TP31661 p 13 N92-21410

The 1991 Goddard Conference on Space Applications [NASA-CP-3138j p 52 N92-24987 CONTROL SYSTEMS DESIGN

of Artificil Intelligence The 26th Aerospace Mechanisms Symposium Research in Structures, Structural Dynamics and

[NASA-CP-31 101 p 43 N91-22769 JNASA-CP-31471 p 30 N92-25067 Materials, 1990

Technology 2000, volume 2 Workshop on Grid Generation and Related Areas (NASA.CP.3D641 p 29 N91-t1l3Oi

[NASA-CP-3109-VOL-21 p 52 N91-24041 INASA-CP. 100691 po 12 N92-25712 Design of control laws for flutter suppression based on

Airborne Wind Shear Detection and Warning Systems: Computational Structures Technology for Airframes and the aerodynamic energy concept and comparisons with

Third Combined Manufacturers' and Technologists' Propulsion Systems other design methods

Conference, part 2 [ NASA-CP-31421 p 31 N92-25911 INASA'TP'30561 p 29 N91-10328

[NASA-CP-10060-PT-2] p 9 N91-24140 LOEF: 69 Months in Space. First Post-Retrieval NASA Formal Methods Workshop. 1990

Structural Integrity, and Durability of Reusable Space Symposium, part 3 1 NASA-CP- 100521 p 42 N91It17559

Propulsion Systems )HASA-CP.3134-PT-31 po52 N92-27083 The 5th1 Annual NASA Spacecraft Control Laboratory [NASA-CP.100301 p 19 N91.24307 The f1990 NASA Aerospace Battery Workshop Expriment (SCOLE) Workshop, part I

The 25th Aerospace Mechanisms Symposium INASA-CP-31191 p 2

0 N92-27130 I NASA-CP-10057-PT-1 I p 16 N91-18186

I NASA-CP-31 13]j p30 N91-24603 Internationat Symposium on Magnetic Suspension The 5th Annual NASA Spacecraft Control Laboratory

Proceedings of the Second Annual NASA Science Tecnologypar12t- I p1 9-72 Experiment ($COLE) Workshop, part 2 I AS-C-35-P-1p 8N9-272 NASA-CP-10057-PT'21 p 17 N91 -19122 Internet User Working Group Conference International Workshop on Vibration Isolation Aeorplin19 rNASA-CP-31 17) p 48 N91-27009 Technology for Mcicogravity Science Applications eorplin19

Technology for the Future. In-Space Technology I NASA-CP- 100941 p 24 N92-28436 INASA-CP-100631 p Q1,191-200861

Experiments Program, part 1 Types and Characteristics of Data for Geomagnetic Field A controls engineering approach for analyzing airplane I NASA-CP. 10073-PT-1I) p 14 N91-27177 Modeling input-output characteristics

Technology for the Future: In-Space Technology I NASA -CP-31531 p 31 N92-28620 INASA-TP-30721 p 12 N9t-20128

Experiments Program, part 2 NASA Workshop on future directions in surface modeling Aerospace Applications of Magnetic Suspension INASA-CP-10073-PT-21 p 14 N91-27178 and grid generation Technology. part 2

spni-e Transportation Propulsion Technology [NASA-CP-100921 p 8 N92-29625 INASA-CP-10066-PT-21 p 17 N91-21203

Sympoeium Volume 3: Panel Session Summaries and The t9"1 International Conference on Aging Aircraft and Rigid-body-control subsystem sizing for an Earth science

Presentations Structural Airworthiness geostatlonary platform

(NASA-CP-3112-VOL-31 p 19 N91-20235 INASA-CP-31601 p 31 N92-30106 [NASA'TP-30871 p1I? N91-22302

A- 10
SUBJECT INDEX DATA UNKS

Fourth NASA Workshop on conmputational Control of CORIOLIS EFFECT CRYSTALLOGRAPHY

Flexible Aerospace Systems, parl I Inertial oscillation of a vertical rotating draft with, Stiffness and strength Tailoring in unfliorm spoace-tiling

NASA-CP-10065-PT-1 I p 17 N91,-22307 application to a supercell storm truss structures

Guidance, navigation, and control subsystem equipment I NASA-TP-32301 p 36 N92-33482 I NASA-TP-321 01 p 30 N92-24546

selection algorithm using axpert system methods CORRECTION CULTURE TECHNIOUES

I NASA-TP-30821 p 42 N91-25624 Comparison of a two-dimensional adaptive-wall Analysis ot gravity-inducted particle motion and fluid

Application and flight test of linearizing transformations technique with analytical wall interference correction perfusion flow in th. NASA-designed rotating

using measurement feedback to the nonlinear control techniques zero-head-space tissue culture vessel

problem INASA-TP31321 p 7 N92-20494 INASA-TP31431 p 24 N92-13340

[NASA-TP-31541 p 12 N91-30154 CORROSION Experimental measurement of the orbital paths O1

On the formulation of a minimal uncertainty model for Electrochemical studies of corrosion inhibitors particlas sadimrooieting within a rotating viscous fluid as

robust control with structured uncertainty (NASA.TPR30661 p22 N9t -17208 influenced by gravity

JNASA-TP-30941 p 13 N92-10027 CORROSION PREVENTION [NASA-TP-32001 p 4

0 N92-28897

Multidisciplinary optimization of controlled space Electrochemical studies of corrosion inhibitors CORING

structures with global sensitivity equations (NASA-TP-30661 p 22 N91-17208 A statistical comparison of two carbon fiber/epoxy

(NASA.TP-31301 p 18 N92-1 1087 COSMIC DUST fabrication techniques International Symposium on Magnetic Suspension The Interstellar Medium in External Galaxies Summaries INASA.TP-31t791 p 22 N92-2D950

Technology, part 2 ot contributed papers CURVATURE

[NASA-CP-3152-PT-21 p 18 N92-27788 [NASA-CP.3084] p 49 N91 14100 Plonformi curvature effects on flutter characteristics of Ongoing Progress in Spacecraft Controls Interstellar Oust Contnbuited Papers a wing with 56 deg leading-edge sweep anid panel aspect

INASA-CP- 100991 p 19 N92-28730 INASA-CP-30361 p 48 N91-14897 ratio 0f1114 CONTROL THEORY Fourth Symposium on Chemical Evolution and the Origin [ NASA.TP-3t18)1 p~t N92t 3054 Design of control laws for flutter suppression based On and Evolution of Life CURVE FITTING the aerodynamiwc energy concept and comparisons with tNASA-CP 3129) p 41 N92-13W8 Calculations and curve fits of thermodynamic and other design methods

(NASA-TP-30561 p 29 N91-10328 COST ANALYSIS transpor properties for equilibrium air to 30000 l(

Joint University Program for Air Transportation Resource envelope concepts for mission planning INASA-RP-12601 p 26 N92-1 1285

Research, 1989-1990 INASA-TP-31391 p 15 N91.29209 Trajectory fitting in function space with application to

I NASA-CP-30951 p 1 N91-19024 COUPLED MODES analytic modeling of surfaces

Aerospace Applications of Magnetic Suspension The effect of acceleration versus displacement methods INASA-TP-32321I p 8 N92-30747

Technology. part 2 on steady-state boundary forces CURVES

I NASA-CP-1006ro-PT-21 p 17 N91-21203 [NASA.TP-32181 p 3 0 N92-21457 Monograph on propagation of sound waves in curved Fourth NASA Workshop on Computational Control of COWILINGS ducts

Flexible Aerospace Systems, partI A Simplified method tor thermal analysis of scowl leading (NASA-RP-12481 p 44 N91-1584

[NASA-CP-10065-PT-1 Ip 17 N91-22307 edge subtect to intense local shock-wave-interference

The 1991 Goddard Conference on Space Applications heating

of Artificial Intelligence I NASA-TP-31671 p 27 N92-24797 D INASA-CP.311101 p 43 N91-22769 CRACK PROPAGATION

A methodology for computing uncertainty bounds of Analysis end prediction of Multiple-Site Damage (MSD) DAMAGE

muttirvanable systems based on Sector stability theory fatigue crack growth An examination of the damage tolerance enhancement

concepts I NASA-TP-3231 Ip31 N92-31279 of carbon/epoiry using an outer lemmna of spectra ( A)

(NASA-TP-31661 p 13 N92-21410 CRACK TIPS INASA-TP-31601 p 21 N92-11142

Visually Guided Control of Movement Applications of FEM and OEM in two-dimensional Analysis and prediction ofi,.~fl Damage (MSO)

I NASA-CP-3t1181 p 39 ff92.2 1467 fracture mechanics problems fatigue crack growth

CONTROLLERS INASA.TP-3277] p 31 N92-31280 INASA-TP-32311 p31 p N92-31279

Proceedings of Ihe Second Joint Technology Workshop CRACKING (FRACTURING) DAMAGE ASSESSMENT

on Neural Networks and Fuzzy Logic, volume 2 Analysis and prediction of Multiple-Site Damage (USD) Cellular track model of biological damage to mammalian INASA-CP- 10061 -VOL-21 p 43 N91-2081 1 fatigue crack growth cell cultures from galactic cosmic rays

Application and flight test of linearizing Transformations I NASA-TP-3231 I p 31 N92-31279 (NASA-TP-30551 p50 N91-1698i using measurement feedback to the nonlinear control CRASHES DATA ACQUISITION

problem Effect of crash puise shape on seal Stroke requirements Coulgassing data for selecting spacecraft materials. I NASA-TP-31 541 p 12 N91-30154 for limiting loads on occupants of aircraft revision 2 inlernational Workshop on Vibration Isolation (NASA-TP-3I26 p 30 N92-18053 [NASA -RP-1 124-REV-2] p21 N914t4437 Technology for Microgravity Science Applications . CAHOTIESMtioreDt nerw nRmt esn [NASA-CP- 10094) p 24 N92-284t36 CAHOTIESMlioreDt nerto nRmt esn

CONVECTION Failure behavior of generic metallic and composite [NASA-CP-30991 p32 N91-15615

Direct simulation of high-speed mixing layers aircraft structural components under crash loads Three-dimensional laster window formation

INASA-TP-31861 p 8 N92-30909 J NASA-IIP-12391 p 29 N91-13751 INASA-RP-12801 p 14 N92-30307

CONVECTIVE HEAT TRANSFER Effect of crash pulse shape on seal stroke requirements DATA BASES

Numerical studies of convective cooling for a locally for limiting loads on occupants of aircraft Responses of women to orthostatic and exercise

heated sktin I NASA-TP-31261 p 30 N92-18053 stresses

INASA-TP-31001 p 26 N91-22509 CREW PROCEDURES (INFLIGHT) INASA-TP-30431 p 37 N91-19711

CONVERGENT NOZZLES Mission dlescnoption and in-Ifight operations of ERBE International exploration of Mars A special

Paramnetric investigation of single -ex pa nsion-ramp instruments on EROIS and NOAA 9 spacecraft, November bibliography

nozzles at Mach numbers from 0860 to 1 20 1984 - January 1986 INASA-SP-70911I p49 N91-24965

INASA-TP-32401 p 9 N92-34193 I NASA-RP-1 2561 p 32 N92-10208 Earth observations and global change decision making

CONVERGENT-DIVERGENT NOZZLES CRITICAL PATH METHOD A special bibliography. 1991

Parametric study of afterbody /nozzle drag on twin Structural factoring approach for analyzing stochastic JNASA.SP-70921 p 32 N91-30588

Iwo-di~mensional convergent-dlivergentl nozzles at Mach networks Continuous improvement A bibliography with indexes.

numbers from 086010o 1 20 1 NASA-TP-3069] p 43 N91-18753 1989-1991

[NASA-TP-26401 p4 N,91-14316 CRITICAL VELOCITY INASA-SP-70971 p 47 N92-22665

Static thrusltiiectoning performance of ncaxisymirretnic Laser anemometer measurements anid computations in The development of the NASA aviation safety reporting

convergent-divergent nozzles with post-exit yaw vanes an annular cascade of high turning core Turbine vanes system

I NASA-TP-30851 p 5 N91-21059 [ NASA-TP-32521 p 8 N92-28980 I NASA.RP- 11141 p 10 N91-70436

Aeropropulsive characteristics of canted twin CROSS SECTIONS DATA COMPRESSION

pitch-vectonng nozzles at Mach 0 20 to 1 20 Two-dimensional aerodynamic characteristics of several High Resolution. High Frame Rate Video Technology

I NASA-TP-30601 p 5 N91-22069 polygon-shaped cross-sectional models applicable to INASA.CP-30801 p27 1,91-114574

Static performance of a crciform nozzle with multiaxis helicopter fuselages Space and Earth Science Data Compression

thrust-yectoring and reverse-thrust capabilities I NASA-TP-32331 p 8 N92-30394 Workishop

i NASA.TP-3t 881 p97 N92-23095 CRYOGENICS INASA-CP-31301 p 41 N92-12425

Parametric investigationl of son le-expsnsion-ramp The 25th1 Aerospace Mechanisms Symposium The effects of video compression on acceptabiity of

nozzles at Mach numbers from 0 600 to 20 NASA-CP-31 131 p30 N91-24603 images tor monitoning life sciences experiments

I NASA.TP,32401 p91. N92-34193 CRSA[EET NASA-TP-32391 p 16 N92-33933

COOLANTSCRSADECT Numerical studies of convective cooling for a locally Equivalent crystal theory of alloys DATA INTEGRATION

neldsi NAvA.TP-355p23N1i01 Multisource Data integration in Remote Sensing

nested si INASA-CP-30991 p32 N,91-15615

INASA-TP.31001 p26 N91-22509 CRYSTAL GROWTH DATA LINKS

COOLING Long-term life testing of Geoslationary Operational Structural factoring approach for analyzing stochastic in-vestigation of microstruclural changes in Environmental Satellite (GOES) encoder lamps networks

polyiltheirethe, -ketone films at cryogenic temperatures by I NASA-RP-12731 p 23 N92-20063 [NASA-TP-30691 p 43 N91-18753

positron lifetime spectroscopy CRYSTAL LATTICES Flight tests with a data link used for air traffi control

(NASA. TP306.4 p 21 N9 1-18216 Equivalent crystal theory o1 alloys information exchange

CORE FLOW I NASA-TP-11 551 p23 1,91-30318 INASA-TP-3i351 p ItI N9 1-31143

Steadjy induction effects in geomaqnelisrn Part I A CRYSTAL StRUCTURE Space Network Control Conference on Resource

Steady motional induction of qeomragnelic chaos Equivalent crystal theory of alloys Allocation Concepts and Approaches

!NASA 7P 3272PT 1A1 p lit N92-326551 I NASA TP-31551 p 23 N91t303 18 INASA-CP-3t241 p 16 N92 11039

A-il1
DATA MANAGEMENT SUBJECT INDEX

Flight dock benefits of integrated data link Fundarentrals of fluid lubrication Sialoerrth Inrternational Laser R'adar Conference parn

communication I NASA-AP-12655 p 28 N91-30531 2

INASA.TP.32191 p 10 N92-21459 Orgurintation of composite sandwichý cover panels tNASA-CP-31r38.PT-2j P26 N1392310113

DATA MANAGEMENT subjected to compressive loadings DRP MEASUREMENT

Flight dock benefits of integrated data link INASA-TP-31 731 p 21 N92-20679 Parmerir$0C study .2 afterbodylliozzle drag on twin

communication DETECTION two-dimenlsionlal corrvefgent-divergent nozzles at Mach

JNASA-TP'32191 p 10 N92-21459 Airborne Wind Sheat Detection arid Warning Systems numbers from 0 60 to t 20

SAGE 1 data user's guide Second Combined Manufacturers' end Technologists' [NASA-TP-2640) p 4 N491-14316

1 NASA-RP- 12751 p 34 N92 >33097 Conference. panrt IDRAG REDUCTION

DATA PROCESSING (NASA-CP.10050-PT- I I p9 1`491-11682 A method for designing blended wing-body

NASA/MSFC FY91 Global Scale Atmospheric Airborne Wind Shear Defection and Warning Systems configurations for low wave drag

Processes Research Program Review Seond Combined Manufacturers' and Technologists' NASA-TP-326 I[ p 8 N492-32480

INASA-CP.31261 p35 N9t-32660 Conference. part 2 Applications of a ditrect/iteratrve design method to

Mission description and in-ftight operations of ERBE [NASA-CP 10050PT 21 p 9 N9t-1 1695 complex transonic configurations

instruments on ERBS and NOAA 9 spacecraft, November INASA-TP-3234[ p 8 N92,33a48

1984 -January 1986 Evaluation of cloud detection instruments and DUCTS

I NASA-RIP-12561 p 32 N492-10208 performance of laminar-flow leading-edge test articles Effect of type of load on stress analysis of thin-wailed

DATA REDUCTION during NASA Leading-Edge Flight-Teat Program ducts

Types and Characteristics of Data for Geomalgnetic Field [NASA-TP-28881 pr 11 tN91-'24199 [ NASA-TP-324.[ p 31 1492-25669

Modeling DIFFUSION DUST

INASA-CP-3f 531 p 31 N92-28620 Saturation point model for the tormation of metal nitrate Sand and Dust on Mars

Mission descniption and in-flight operations of ERBE in nitrogen ifetroxide oxidizer [ NASA-CP. 100 741 p 50 N91 -27057

instruments on ERBS. NOAA 9. and NOAA t0 INASA-TP-31071 p 26 N91-24542 DUST STORMS

spacecraft Analysis of gravity-induced particle motion and fluid Sand and Dust on Mars

[NASA-RP.1 791 p 32 N492-32127 perfusion flow in the NASA-designed rotating INASA-CP-soola1 050 N1 49-7057

DATA SMOOTHING zero-head-space tissue culture vessel DYNAMIC CHARACTERISTICS

State estimation appficatrons in aircraft flight-data INASA-TP-3143[ p 24 N492-13340 finfluence of mass moment of ineria on normal modes

analysis. A user's manual for SMACK Design and performance of controlled-diffusion stator of preloaded solar array mast

(NASA-RP,12521 p 10 N91-19082 compared with original doubte-circular-aic stator [ NASA-TP-32 73) p 3t N492-334 76

DATA SYSTEMS INASA-TP-28521I p 12 N492-22863 DYNAMIC CONTROL

Small Exrplorer Data System Ml l-STD-`1773 fiber optic DIGITAL DATA Large space structures and systems in the space station

bus Flight deck benefits of integrated data link era A bibliography with inderes (supplement 031

1 NASA-TP-32271 p 16 N492-26667 communication INASA-SP 7085(03 11 p 18 1492 22317

DATA TRANSMISSION I NASA -TP-32t91 p 10 N92-21 459 DYNAMIC MODELS

H-figh Resolution, High Frame Rate Video Technology DIGITAL SYSTEMS Correlation and prediction of dynamiic thuman 'soared

I NASA-CP-30801 p 27 N91,14574 NASA Formal Methods Workshop. 1990 joint strength from lean bcody mass

Flight deck benefits of integrated data link INASA-CP-10052[ p42 N91-17559 [ NASA-TP-3207 i p 

4 0 N92-2668-2

communication. NASA-LaRc Flight-Critical Digital Systems Technology DYNAMICPRESSURE

[NASA-TP 3219) p t0 N492-21459 Workshop Span reduction effects on the fliutter characteristi-s of

Large space structures end systems inI the space station I NASA-CP-t10028[ p 1 1 N91-2420t0 arnow-wing supe5rsoic rarspori coot gu',ations

era A bibliography with indexes (supplement 031 NASA-TP-3077! p I10,9 r'2rr2 7

1 NASA-SP-7085(03l) p18 N92-22317 DIRECTIONAL STABILITY DYNAMI CRESPONSE

DECISION MAKING Wind-tunnel static and free-tlight investigation of Research in Strictures Structural Dynariris and

Proceedings of the Second Joint Technology Workshop high-angle-ol-attacir stability and control characteristics of Matea ies 1990

on Neural Networks and Fuzzy Logic, volume 2 a model of the EA-613 airplane 'NASA CP 3064: r29 N591

I NASA-CP- 1006, -VOL-2; p 43 N91-20811 fNASA-TP-31941 P 7 N92-2527on Deueioprenr or a"- integarwed aeioseivoeiasrc ainal-Oss

Proceedings of the Second Jorint Techniology Workshop DISCHARGE COEFFICIENT program and coireial~on !jh rest rilar

on Neurat Networks anid Fuzzy' Logic, volume I A nozzle internal performance prediction method -sA5A-TP-12C~, ip2 N9157261 tJ

[ NASA-CP-10,061-VOL- p 43 1,91-217,78 1NASA.TP 32211 p 8 V-3,1 DYNAMIC STABILITY

DECONDITIONING. DISPLAY DEVICES A Icheiie -ii !-5iidoiksin le-,I i ýjwiic-ne.e

Workshop on Exercise Prelscirption for Long-Duration Effect of shor-t trm exposurre to stereoscopic rriý,iinn its- 7-n'ruct iiir.rele_ -ie iiCS prnopi

Space ;flight thmefe-flimrnesiciral Hlight, distrlays on real-worcl deursth rro

[NASA CP -3051 ip36 N91-iO574 perception INASA-TIP:3r2i

DEFLECTION [NASA-TO?: tý7[ pt 5192 13065 alnod-tunnel sta ui- free -g usrig

Effect of tenmperarture aria gap opening rate or, the DISTORTION hign~angieoflatrac,,.,1.,tir-l~' ~iiS'~ li

resiliency of candidate solid rocket booster C-ring Tfrerma-disioirion analysis ot a spacecraft riox truss in a model Of th. [Ari a

materails geostarionary orbit !NASA-TP 3194 Nd,

[NASA-TP-32261 p 23 N492-271 94 INASA. TP.30541 It 16 N91t-ifT41 DYNAMIC STRUCTURAL ANALYSIS

DEICING DfSTRIBUTED PARAMETER SYSTEMS Rpsearrh -Siir,_~n tfSiq:ýa

Lewis icing research tuirnel rest of the aerolýynamnic Beyond the Baseline 1991 Proceedings of tie Space Mater~als 'hOG)

effects of aircraft ground deicing /anti-icing fluids Station Evolution Symposii~m Volumea 2 Space Station 'NASA-CP 0i-64,2, 4,

[ NASA-TP-3238![ pl10 N92-30195 iwFreedom oars rtu~m'ei sr-i- a- a4i 7 s oi 'iiiai- -,

DELTA WINGS NASAl fiP 10083 VOL-2-PT Ii[ p 18 92-17766 roCket troosre fiti-!-

Navier- Stokes and Ew~er solutions forf~ee-side flows over DISTRIBUTED PROCESSING NASA 7P-jL:; v- N'4 '4tisupersonic delta wingn~i A ;orrolation with' enperimer-: Fault ltolrance ril artificial r'eiral networks woln WhiT fu1icin daoouslC

i NASA-TP-3(35-1: p-4 N91-124'31 ahlicatroo-nl c'-r.cTal sy~lenis -NASA TP 30i~ht 4t-au !iDetailed flow-f-otld niieasuir'renots over a 75 deg swept NASA-TP 3il7 ie pa 42 52 122815 Tie LIP1 Ar-iiu4, NASA i ~ 4 r -r-'

delta wing Adtvanceif techiri~iqus in, 'elability model riPiresontation- Ex-oe"irneri (SCIOLE) 'iCi-? 3

[NASA TP-29971 pa4 N91 'P030 ano sciution INS-, ,Xý'P

fid unnel ir-yeetgatior of the -nteraction anid ! NASA-TP 3242 - p 43 N9l2-334f11:r 2,-ckiing and vih-r:to- analysis Li -ibreakdown characteristics of Slender wing vortices at DtURNAL VARIATIONS c~unwitt a _-staep:5W- -iiSs Sý2CL'

subsonic transoniic, arid sijucoer,,c speeds Atlas of rhe F aoirs radiationr brirgaf as meas,,ed by NASA-TP-3,54r,,

NASA-TP-3114 t 06 N92-129914 NimbuS-i May '91-1 to May 1980 on NAS, iorlsr--p or,

linfluenui of , i geornetr-r n delta wing leading-edge 1NASA R P- 1i p 35 N91l 24,120 1(i vNin A-3spaii Svt, pair

vorf ices an,; vortey-irrduced aerorlynarnrcs at supersonic DCMNSNASA CFP ý ),--

speeds Large space StfUCtrirIS a'--d SySI~r'mh Is) heý spacef slr411 Sti,uctial !n3io-ty .3nC ..,-i- ity

JNASA-TP-3105[ p? 2-03 era A oiblioiqaphv wirfh -1nitens r~oiplJsl5O nSvse- pNASA 220038 N SP 5(A P 1 Nd-81- NASA-CP rri ii N"1 4ii DEMAGNETIZATIONIirnioa enialo fMr A spca ehrsIviid--nii

The 23 to 300 C 'Iemagqr-tuza1rro resistance of bibliornainiepoainoaphy A NASA-al ,-D 26ho Ip'

sananrum-cobalt permaneint r-aqnels ilogahh NASA~o73loi h-dii fnRnlPm 121. i i ,fi e4si - -

NASA-TP-31 r9[ p2`5 Nif2 11r252 Eatobrviof-anglra-:agdcio-mkn prriiadlr-i '

DESIY IS~fU~ONA special tiibliocIfaphy. 991 Sit ;rSA7D110 Simulation cif real-gas flrift7 rotrun pressure dis~triburtions NASA-SO- 7092! p 12 1491 .1iif)5 NS-.

for aeroasist flight etoer-nrilit vehicle and comparison Aero~naut~ical engineerring A c(~i~tihuinq biNoircriihy vniir

with preadiction inderes siupplementf 2771 or, slireach sta f' i, -- firdA'

[NASA TP-3t571 p2 NS-P73iffi( iN2?5 :-07 NASAN 21i-I>nl 4'-

DPHDO0RS Ongoing Progress in tl-i,

Effect of short -trm (vritrurn ro stereoscopic Payload hay doors air adialfo, anuviO<r 'lcrl NASA C-OP flo)lr4il ~2;7 w 

three-dimensional flighl displays on real-world depth handbook n-flierre 'f -nas, 'riO-o~r-i fi'0Oh r,'i '~--

perception NASA-f M 10 77931 N15-2 20refi ofrreloarler-4 s-ati ar-ar 4at

[NASA-IP-3t171 o 11 N92-t3065 DOPPLER RADAR NASA TP '32:i '' iii-4:i 4

DESIGN ANALYSIS Airborne A-ir'tj Shear [etrxol nt ivii Wiiriir SysfirmS DYNAMIC TESTS

A new fabrication nirilhil-, for precision antenna 'i lntritManrfactir,rrr and "echnrioioists Ef'ro rs u ilp i07S~i i~ - i

reflectors for space hi~ghi anrd girund test ý,onferenco priart for iim-t-ng boail- cirr oPi iaht ofaici

[NASA TP-3078[ p 17 N91-2118 ;Nt ASA C.P r)fl'rO frT 21 ofl) '49 24140i NASA-O I 'C I - l
SU&/ECT INVEX ESTIMATES

DYNAMICAL SYSTEMS EIGEN VALUES ENERGY DISSIPATION

Technirwue to eliminate computational instability in Identificationi of linear systems by ari asymptotically Aeroacoustrc arid aerodynamic applications ofthe theor-y

multibody simulations employing the Lagrange multiplier stable observer of nonesquilirbnum thermodynamics

I NASA-TP-32201 p 42 N92-23432 J NASA-TP-3164] p 31 N92-26537 (NASA.TP-31181 p 26 N91-25352

EJECTORS ENERGY METHODS

Venturi air-jet vacuum electors for high-votume Design ot control laws for Itutter suppression based on' E atmospheric sampling on aircraft platforms the aerodynamic energy concept and comparisons with

INASA-TP-31 831 p I1I N92-20546 other design methods

EARTH (PLANET) ELASTIC PLATES I NASA-TP-30561 p 29 N91-10328

Earth ob~servations and global change decision making: Applications of FEM and BEM in Iwo-dimensional ENERGY OF FORMATION

A special bibliography, 1991 fracture mechanics problems Equivalent crystal theory of alloys

[NASA-SP-7092] p32 N91-30568 [ NASA-TP-32771 p 31 N92-31280 [NASATP-31551 p 23 N91-3031 8

EARTH ATMOSPHERE ELASTOHYDROCYNAMICS, NIEARRM NERTO NASA/ MSFC FY90 Global Scale Atmospheric Fundamentals of fluid lubtrication ENIEffc AIfRM loaiono f-ontedGRATlesOth

Processes Research Program Review [NASA.RP-12551 p 28 N91-30531 lonigituudinal aerodynamic characteristics 0f a hugh-wing

I NASA-CP-30931 p35 N91-116500 ELASTOMERS transport airplane

NASA/MSFC, FY91 Global Scale Atmospheric Effect of temperature and gap opening rate on the INASATP-3071 p4 N91-1 3402

Processes Research Program Review resiliency of candidate solid rocket booster 0-nag ENGINE DESIGN

(NASA-CP-31261 p 35 N91-32660 materialsAeooulon17 I NASA-TP-32261 p 23 N92-217194 eorplon18 EARTH OBSERVATIONS (FROM SPACE) ELECTRA AIRCRAF*T I NASA-CP-30491 p 12 N92-22510

NASA/MSFC FY91 Global Scale Atmospheric Venturi air-jet vacuum ejectors for high-volume ENGtNE NOISE

Processes Research Program Review atmospheric sampling on aircraft Platforms J-85 tat engine noise measured in the ONERA SI wind

INASA-CP-31261 p35 N91-32660 (NASA-TP-31631 p 11 N92-211546 tunnel and estrapolated to far hield

Space and Earth Science Data Compression ELECTRIC BATTERIES [NASA-TP-30531 p 45 N91-19823

Workshop Space Electrochemical Research and Technology ENGINE PARTS

( NASA-CP-31301 p 41 N92-12425 (NASA-CP-31251 p 33 N91-32549 Rocket-Based Combined-Cycle IROCCI Propulsion

EARTH ORBITAL ENVIRONMENTS The 1991 NASA Aerospace Batter Workshop Technology Workshop Tutorial session

Orityal debris: Technical issues and future directions (NASA-CP-31401 p 33 N92-22740 (NASA-CP-100901 p 20 N92-21517

I NASA-CP-10077' p 49 N92-33478 ELECTRIC POTENTIAL ENGINEERING MANAGEMENT

EARTH ORBITS Long-term life testing of Geostationary Operational NASA engineears and the age of Apollo

Metallized propellentls for the human exploration of Environmental Satellite (GOES) encoder lamps I NASA-SP--41041I p 52 N92,28344

Mars [NASA-RP-12731 p 23 N92-20063 ENTHALPY

(NASA-TP-3062) p19 N91-1 1800 ELECTRIC ROCKET ENGINES Calculations and curve fits of thermodynamic arid

Current Collection from Space Plsms Magnet oplaismadynamic Thruster Workshop transport properties for equilibrium air to 30000 K

INASA-CP-30891 p 46 N91-17713 INASA-CP-100041 p 20 N92-10044 (NASA-RP-t2601 p26 N92-ii285

EARTH RADIATION BUDGET ELECTRICAL PROPERTIES ENTROPY

User's guide: Nimbus-? Earth radiation budget Electrical and chemical interactions at Mars Workshop. Aeroacoustic and aerodynamic applications of the theory

narrow-field-of-view products. Scene radiance tape pert I of nonequilibrium thermodynamics

products, sorting into angular bins products. and maximum INASA-CP-100931 p 50 N92-30302 [ NASA-TP-31 IS) p 26 N91-25352

likelihood cloud estimation products ELECTROCHEMISTRY ENVIRONMENT EFFECTS

INASA-RP-12461 p 34 N91 -13043 Electrochermical studies of corrosion inhibitors Climate Impact of Solar Variability

Limb-darkening functions as derived from along-track [ NASA-TP-30661 p22 N91,17208 (NASA-CP-30861 p50 N91-12456

operation of the ERBE scanning radiometers for August Space Electrochemical Research and Technology Teamshrcefcs0 ta~pei icat

1985 1 NASA-CP-31251 p 33 N91-32549 Topicalmshei review trtspei arrat

INASA-RP-12431 p34 N91-14683 ELECTROMAGNETIC COUPLING tpclrve

The 1991 International Aerospace and Ground fNASA-FIP-12501 p 33 N91-16466

Atlas of wide-field-oif-view outgoing Iongwave radiation Conference on Lightning and Static Electricity, volume 2 Wind tunnel aerodynamic characteristics of a derived from Nimbus 7 Earth radiation budget data set. [ NASA-CP-3106-VOL-21 p 36 N91 -32693 transport-type airtfoil in a simulated heavy rain

November 1985 to October 1987 ELECTROMAGNETIC PULSES environment

INASA-RP-12611 p p35 N91-24719 The 1991 International Aerospace and Ground [NASA-TP-31841 p 8 N92-31532

Atlas of the Earth's radiation budget as measured by Conference on Lightrsng and Static Electricity, volume 2 ENVIRONMENT MODELS

Nimbus-i: May 197910o May 1980 [NASA-CP-3f06-VOL-21 p 36 N91-32693 Electrical and chemical interactions at Mars Workshop. [NASA-RP-12631 p 35 N91-24720 ELECTRON IRRADIATION part I

Mission description and in-flight operations of ERBE Space Photovoltaic Research arid Technology INASA-CP-100931 p 50 N92-30302

instruments on ERBS. NOAA 9, and NOAA 10 Conference ENVIRONMENT SIMULATION

spacecraft [NASA-CP.31211 p 19 N91-30203 Shortcomings in ground testing, environment

INASA-RP-1279j p 32 N92-32127 ELECTROSTATIC PROBES simulations, and performance predictions for space

EARTH RADIATION BUDGET EXPERIMENT A self-zeroing capacitance probe for water wave applications

Limb-darkening functions as derived from aloig~track measurements (NASA-TP-32171 p 23 N92-22593

operation of the ERBE scanning radiometers for August [NASA-RP-1278) p 36 N92-27930 Wind tunnel aerodynamic characteristics 0f a 1985 ELECTROSTATICS transport-type airfoil in a simulated heavy rain

INASA.RP-12431 p 34 N91-14683 Sand and Dust on Mars environment

Atlas of wide-field-of-view outgoing longwave radiation INASA-CP-100741 p 50 N91-27057 INASA-TP-31841 p 8 N92-31 532

derived from Nimbus 7 Earth radiation budget data set, The 1991 International Aerospace and Ground ENVIRONMENTAL ENGINEERING

November 1985 to October 1987 Conference on Lightniing and Static Electricity, volume 1 Biological Life Support Technologies Commercial

INASA-RP-1261 J p 35 N91-24719 [ NASA-CP-3106-VOL-1 IJ p35 N91-32599 Opportunities

Mission description and in-flight operations of ERSE ELEVATION INASA-CP-30941I p 36 N9 1-13842

instruments on EROS and NOAA 9 spacecraft. November A self-zeroing capacitance probe for water wave ENVIRONMENTAL SURVEYS

1984 - January 1986 measurements The atmospheric effects of stratospheric aircraft A

INASA-PP-12561 p 32 N92-10208 (NASA-RP-12781 p 36 N92-27930 topical review

Mission description and in-flight operations 0f EREE ENERGETIC PARTICLES (NASA-RP-1250] p 33 N91-16466

instruments on EROS. NOAA 9. and NOAA 10 An efficient HZETRN (a gacici cosmic ray transport EPOXY MATRIX COMPOSITES

spacecraft code) An exatmnation of the damage tolerance enhancement

jNASA-RP-12791 p 32 N92-32127 jNASA-TP-31471 p 51 N92-22218 of carbon/epc'-y using an outer lamine of spectra (R)

EARTH SCIENCES ENERGY ABSORPTION [NASA-TP-3i6o) p 21 N92-1 1142

Rigid-body-control subsystem sizing for an Earth science Failure behavior of generic metallic arid composite fAbricationteclchniquesooftocrnfielpx

geostalionary platform aircraft structural components under crash loads fabriation 79ecp2nNiques5

[NASA-TP-30871 p 17 N91-22302 [NASA-RP-12391 p29 N91-13751 EPOXY RESINS-295 P-379 

Launch vehicle integration options for a large Earth ENERGY BUDGETS Structural properties of laminated Douglas fir/epoxy sri-'- s geostationary platform concept Limb-darkening functions as derived from along-track composite material

(NibA-TP-30831 p 15 N91-27180 operation of the ERBE scanning radiometers for August INASA-RP-12361 p 20 N91-10127

ECOSYSTEMS 1985 EUTOSO TT Controlled Ecological Life Support Systems Natural and )NASA.RPI1243I p 34 N91-14683 EQUATIeoNS OF t STATEel oshei a fo fed

Artificial Ecosystems Atlas of the Earth's radiation budget as measured by (NASA-RP-12491 p26 N91-204118

[ NASA-CP-I100401 p 40 N91-24744 Nimbus-i May 19791to May 1980 EQUIPMENT SPECIFICATIONS

EDUCATION [NASA-RP-12631 p 35 N91-24720 Exobiology on Mars

National Educators' Workshop Update 1988 Standard The role of water vapor in climate. A strategic research (NASA-CP-100551 p AlI N91-t15691

Experiments in Engineering Materials Science and plan for the proposed GEWEX water vapor project ERROR ANALYSIS

Technology (GVap) Model reduction by trimming for a class of serm-Markov

INASA-CP-30801 p 20 N91-20207 )NASA-CP-3120j p 3 5 N91 -25556 relialblity models and the corresponding error bound

National Educators' Workshop Update 1991 Standard ENERGY CONVERSION EFFICIENCY I NASA-TP-3089) p 43 N91 -25741

Experiments in Engineering Materials Science and Design and performance of controlled-diffusion stator ESTIMATES

Technology compared with original double-circular-arc stator Flight Mechanics/Estimation Theory Symposium. 1990

INASA-CP-31511 p p24 N92-30263 (NASA-TP*28521 p 12 N92-22863 I NASA-CP-311021 p 14 N91-17073

A- 13
ESTIMATORS SUBJECT INDEX

ESTIMATORS Aerospace medicine and biology A continuing EXTRATERRESTRIAL ENVIRONMENTS

A nonlinear estimator for reconstructing the angular bibliography with indexes (supplement 352) Second LDEF Post-Retneval; Symposium abstracts

velocity of a spacecraft without rate gyros INASA-SP-7011(352)1 p38 N91-28729 I NASA-CP-100971 p 52 N92-27218

I NASA-TP.31781 p 24 N92-13343 Aerospace niedicine and biology: A continuing EXTRATERRESTRIAL RADIATION

EULER EQUATIONS OF MOTION bibliography with indexes (supplement 353) Improvements in computational accuracy of BRYNTRN Transonic flow analysis for rotors, Part 3. [NASA-SP-7011(353)1 p 38 N91-31760 (a baryon transport code)

Three-dimensional. quasi-steady, Euler calculation Aerospace medicine and biology- A continuing INASA-TP-30931 p 51 N91 23017

INASA-TP-23751 p 3 N91-10007 bibliography with indexes (supplement 354) First LDEF Post-Relrieval SymKosium abstracts

Navier-StofesandEutler solutionsfor lee-sideflows over INASA-SP-7011(354)1 p 38 N92-12404 INASA-CP.10072I p 52 N91.24972

supersonic delta wings. A correlation with experiment Aerospace medicine and biolOgy: A continuing Transport methods and interactions for space

INASA-TP-30351 p4 N91-13401 bibliography with indexes (supplement 355) radiations

Shock wave interaction with an abrupt area change INASA-SP-7011(355)) p 38 N92.12412 INASA.RP-12571 p 5 N92-15956

I Trans 13i puaons-1 Fourth SymposiumNonTChemicalEvoluionand the Oig Track structure model of cell damage in space flight Transomic and supe about ener i fonputigh ofte and Evolution of Life [NASA-TP-3235) p 39 N92-34154

ortex-dominated flow fields abou a genec ighter NASA-CP-3129 p41 9213568 EXTRAVEHICULAR ACTIVITY NASA-TP-356 p N92-10011 p41N92A method of evaluating efficiency during space-suiled EVOLUTION (DEVELOPMENT) Aerospace medicine and biology: A continuing w in a neutral buoyancy environment

Beyond the Baseline 1991: Proceedings of the Space bibliography with indexes (supplement 356)

Station Evolution Symposium Volume 2: Space Station INASA-SP-7011(356)1 p38 N92-15538 [NASA.TP-3153] p40 N92-19772

Freedom. art 2 Aerospace medicine and biology: A continuing Large space structures and systems in the space station

1NASA-CP-10083.VOL-2-PT-21 p 18 N92-17348 bibliography with indexes (supplement 357) era. A bibligraphy with indexes (supplemnt 03)

EXERCISE PHYSIOLOGY INASA-SP-7011(357)) p 39 N92-21714 INASA-SP-7085(03)1 p 18 N92-22317

Workshop on Exercise Prescription for Long-Duration Aerospace medicine and biology: A continuing

Space Flight bibliography with indexes (supplement 359) F

INASA-CP-3051) p 36 N91-10574 INASA-SP-701f(359)] p 39 N92-21715

EXHAUST EMISSION Aerospace medicine and biology: A cumulative index F-15 AIRCRAFT

The atmospheric effects of stratospheric aircraft: A to a continuing bibliography (supplement 358) Application and flight test of lineanrizng transformations

current consensus INASA-SP-7011(358)) p 39 N92-22026 using measurement feedback to the nonlinear control

[NASA-RP-12511 p33 N91-16467 Aerospace medicine and biology. A continuing problem

Optical measurements on solid specimens of sold rocket bibliography with indexes (supplement 362) 1NASA-TP-3154) p 12 N91-30154

motor exhaust and solid rocket motor slag I NASA-SP.7011(362)1 p 39 N92.27068 F-18 AIRCRAFT

INASA-TP-3177) p 20 N92-20949 Aerospace medicine and biology: A continuing Wind tunnel investigation of vortex flows on F/A-18

EXHAUST FLOW SIMULATION bibliography with indexes (supplement 361) configuration at subsonic through transonic speed

A parametric experimental investigation of a scram)et [NASA-SP-7011(361)1 p 39 N92-27433 INASA-TP-31 1 1) p6 N92-14968

nozzle at Mach 6 with Freon and argon or air used for Aerospace medicine and biology: A continuing FABRICATION

exhaust simulation

[NASA-TP-30481 p 4 N91-16990 bibliography with indexes (supplement 363) Structural properties of laminated Douglas fir/epoxy

EXHAUST GASES P NASA-SP-7011)363)) p 39 N92-30987 composite material

A parametric experimental investigation of a scramlet EXPERIMENT DESIGN (NASA-RP-12361 p 20 N91-10t27

nozzle at Mach 6 with Freon and argon or air used for Exobiology on Mars A new fabrication melhod for precision antenna

exhaust simulation INASA-CP-100551 p 41 N91-15691 reflectors for space flight and ground test

[NASA-TP-30481 pi4 N91-16990 Definition and design of an experiment to test raster INASA-TP-30780 p 17 N91-21185

EXHAUST NOZZLES scannig with rotating unbalanced-mass devices on FAILURE

A parametric experimental investigation of a scramjal gimbaled payloads Reliability training

nozzle at Mach 6 with Freon and argon or air used for f NASA-TP.32491 p 24 N92-29677 [NASA-RP-12531 p 15 N92-32456

exhaust simulation EXPERIMENTATION FAILURE ANALYSIS

INASA-TP-3048) p 4 N91-16990 National Educators' Workshop: Update 1988 Standard Failure behavior of generic metallic and composite

Static internal performance of ventral and rear nozzle Experiments in Engineering Materials Science and aircraft structural components under crash luads

concepts for short-takeoff and vertical-landing aircraft Technology INASA-RP-12391 p29 N91.13751

INASA-TP-3103) p 6 N92-10975 INASA-CP-3060) p20 N91-20207 Development of an adaptive failure detection and

EXHAUST SYSTEMS National Educators' Workshop: Update 1991. Standard identification system for detecting aircraft control element

Static internal performance of ventral and rear nozzle Experiments in Engineering Materials Science and failures

concepts for short-takeoff and vertical-landing aircraft Technology [NASA-TP-30511 p 12 N91-25151

INASA-TP-31031 p 6 N92-10975 INASA.CP-3151I p 24 N92-30263 A three-dimensional finite-element thermal/mechanical

EXOBIOLOGY EXPERT SYSTEMS analytical technique for high-performance traveling wave

Aerospace medicine and biology- A continuing Joint University Program for Air Transportation tubes

bibliography with indexes (supplement 341) Research, 1989-1990 tNASA-TP-3081) p25 N91-27436

[NASA-SP-7011(341)] p 37 N91-10594 INASA-CP-30951 p 1 N91-19024 The 3ol 1o f in Nginerig 6

Aerospace medicine and biology' A continuing Fourth Annual Workshop on Space Operations The role of failure/probtenesc i esnsieerlng A

bibtiography with indexes (supplement 342) Applications and Research (SOAR 90) commentary of failues experienced - lessons learned

[NASA-SP.7011(342)) p 37 N91-13063 [NASA-CP-3103-VOL-2) p41 N91-20702 I NASA-TP-32131 p 24 N92-22235

Aerospace medicine and biology: A continuing Proceedings of the Second Joint Technology Workshop ReliabAlty training

bibliography with indexes (supplement 343) on Neural Networks and Fuzzy Logic. volume I (NASA-RP-12531 p 15 N92,32456

[NASA-SP-7011(343) p 37 N91-14711 )NASA.CP,10061-VOL-t I p 43 N91-21778 Advanced techniques in reliabi•ity model representation

Aerospace medicine and biology- A continuing Guidance. navigation, and control subsystem equipment and solution

bibliography with indexes (supplement 344) selection algorithm using expert system methods I NASA-TP-32421 p 43 N92-33483

|NASA-SP-7011(344)( p 37 N91-14712 )NASA-TP-30821 p 42 N91-25624 FAILURE MODES

ExobiolOgy in Earth orbit: The results of science Aiomnating a spacecraft elec•rical power system using Experimental validation of clock synchronization

workshops held at NASA. Ames Research Center expert systems algorithms

[NASA-SP-5001 p4f N91-14725 INASA-TP-31611 p 20 N92-12052 INASA-TP-32091 p 42 N92-27589

Exobiology on Mars Second CLIPS Conference Proceedings, volume 1 Reliability training

INASA-CP.100551 p 41 ff91-15691 1NASA-CP-10085-VOL- - p 42 N92-16568 [NASA.RP-12531 p 15 N92-32456

Aerospace medicine and biology A cumulative index Second CLIPS Conference Proceedings. 4olume 2 Advanced techniques in reliability model representation

fo a continuing bibliography (supplement 345) [NASA-CP-10085-VOL-21 p 42 N92-16590 and solution

INASA-SP-7011(345)) p 37 N91-16547 Beyond the Baseline 1991ý Proceedings of the Space [NASA-TP-3242) p 43 N92-33483

Microbiology on Space Station Freedom Station Evolution Symposium, Volume 1: Space Station FAIRINGS

(NASA-CP-31081 p 37 N91-18573 Freedom, part 2 Payload bay doors and radiator panels familiarization

Aerospace medicine and biology: A continuing (NASA-CP-10083-VOL-1-PT-21 p 18 N92-17409 handbook

bibliography with indexes (supplement 346) Fifth Annual Workshop on Space Operations I NASA-TM-1077931 p 15 N92-20676

INASA-SP-7011(346)) p 37 N91-23700 Applications and Research (SOAR 1991). volume 2

INASA-CP-3127-VOL.21 p 41 N9222324 FAN BLADES Aerospace medicine and biology A continuing EXPLORER SATELLITES Design and performance of controlled-diffusion stator bibliogaphy 0134) (supplement pndexes 3

4 7 bIoorby wAS ) S xcompared with original doublo-circular-arc stator ?011 h exes) psplm 347)N1230 Small Explorer Data System MIL-STO-1 773 fiber optic INASA-TP-28521 p 12 N92-22863 AASP0t34) 37N-27f bus N A-P85)pI N9-86

Aerospace medicine and biology A continuing b NASA.TP-3227, p 16 N92-26667 FAR FIELDS

bibliography with indexes (supplement 348) EXPOSURE J-85 let engine noise measured in the ONERA St wind

I NASA-SP-7011)348)) p 37 N91-23702 Space Photovoltaic Research and Technology tunnel and extrapolated to far held

Aerospace medicine and biology A continuing Conference I NASA-TP-30531 p 45 N91-19823

bibliography with indexes (supplement 349) 1 NASA-CP.31211 p 19 N91-30203 FASTENERS

I NASA.SP-7011(349)1 p3 7 . N91-24731 Track structure model of cell damage in space flight Development of a truss loint fot robotic assembly of

Aerospace medicine and biology: A continuing INASA-TP-3235) p 39 N92-34154 space structures

bibliography with indexes (supplement 350) EXTERNAL STORE SEPARATION INASA.TP-3214] p 31 N92.27974

NASA-SP.7011(350)) p38 N91,25600 Measurements of forces, moments, and pressures on FATIGUE (MATERIALS)

Aerospace medicine and biology A continuing a generic store separating from a box cavity at supersonic Analysis and prediction of Multiple-Site Damage (MSD)

bibliography with indexes (supplement 351) speeds fatigue crack growth

INASA-SP-7011(351() p 38 N91-27756 INASA.TP-31 10) p 6 N92-10005 fNASA-TP-3231) o 31 N92-31279

A-14
SUBJECT INDEX FLOW DISTRIBUTION

FATIGUE TESTS Improved accuracy for finite element structural analysis Advanced techniques in reliability model representation

A method of evaluating efficiency during space-suited via a new integrated force method and solution

work in a neutral buoyancy environment (NASA-TP-3204) p 30 N92-22227 I NASA-TP-32421 p 43 N92-33483

INASA-TP-31531 p 40 N92-19772 Twentieth NASTRAN (R) Users' Colloquium FLIGHT HAZARDS

FAULT TOLERANCE I NASA-CP-31451 p 30 N92-24324 Airborne Wind Shear Detection and Warning Systems

NASA Formal Methods Workshop, 1990 Stress concentrations for straight-shank and Third Combined Manufacturers' and Technologists

INASA-CP.t00521 p42 N91-17559 countersunk holes n plates subjected to tension. bending, Conference, pail I

Development of an adaptive failure detection and and pin loading NASA-CP-10060-PT- A p 9 N91-24166

identification system for detecting aircraft control element I NASA-TP-31921 p 31 N92-25997 The 1991 International Aerospace and Ground

failures Applications of FEM and OEM in two-dimensional Conference on Lightning and Static Electricity. volume I

INASA.TP-3051 I p 12 N91-25t51 fracture mechanics problems INASA-CP-3106.VOL.-1 p 35 N9t.32599

Fault tolerance of artificial neural networks with INASA-TP-32771 p 31 N92-31280 FLfGHT INSTRUMENTS

applications in cntical systems Eighth DOD/NASA/FAA Conference on Fibrous Effect of ~hoi.term exposure to stereoscopic

I NASA-TP-31871 p 42 N92-22285 Composites in Structural Design, part three-dimensional flight displays on real-world depth I NASA-CP-3087-PT-1 I pI2N2-21 ther-cptionsioa lgtdsly nra-ol et

The 1992 Goddard Conference on Space Applications FINITE VOLUME METHOD p N 2 2 N92-325t3 perception

ofArtificial Intelligence FIIT VOUEMTONASATP-311 71 p t 1 N92-13065 I A-CP34 pn43N92-3356 Trensonic flow analysis for rotors Part 3 FLIGHT MANAGEMENT SYSTEMS I NASA-CP-3t41 p43 N92-23356 Th- ie-dimensional. quasi-steady. Euler calculation

Advanced techniques in reliabihty model representation INASA-TP-23751 p 3 N91-10007 Report of the workshop on Aviation Safety Automation

and Solution FIRE (CLIMATOLOGY) Program

INASA-TP-32421 p 43 N92-33483 FIRE Science Results 1988 INASA-CP-100541 p9 N91-15141

FEASIBILITY ANALYSIS [NASA-CP-30831 p 34 N91-10448 Airborne Wind Shear Detection and Warning Systems

Feasibility study of a low-energy gamma ray system for FLAME STABILITY Third Combined Manufacturers' and Technologists'

measunog quantity and flow rate of slush hydrogen Two-dimensional stability of laminar flames Conference, part 1

INASA-TP-3150) p19 N92-25147 [NASA.TP-31311 p7 N92-17131 [NASA-CP-10060-PT-t p9 N91-24166

Definition and design of an experiment to test raster FLAPPING FLIGHT MECHANICS

scanning with rotating unbalanced-mass devices on Full-scale semispan tests of a business-let wing with a Flight Mechanics/Estimation Theory Symposium. 1990

gimbaled payloads natural laminar flow airfol (NASA-CP-31021 p 14 N91-17073

I NASA-TP-3249j p 24 N92.29677 I NASA-TP-31331 p 6 N9t-30098 FLIGHT OPERATIONS

FEEDBACK CONTROL FLAPS (CONTROL SURFACES) Flight tests with a data link used for air traffic control

Application and flight test of linearizing transformations Aeropropulsive characterstics of canted twin information exchange

usng measurement feedback to the nonlinear control pitch-vectoring nozzles at Mach 0,20 to 1.20 INASA-TP-31351 p 11 N91-31143

problem INASA-TP-30601 p 5 N91-22069 FLIGHT SAFETY

INASA-TP-31541 p 12 N91-30154 FLAT PLATES A comparison of airborne wake vortex detection

The effect of bandwidth on telerobot system Measurements of forces, moments. and pressures on measurements with values predicted from potential

performance a genenc store separating from a box cavity at supersonic theory

INASA-TP-31521 p 28 N91-30540 speeds INASA-TP-31251 p 10 N92-10994

On the formulation of a minimal uncertainty model for INASA.TP-3t 101 p 6 N92-t0005 FLIGHT SIMULATION

robust control with structured uncertainty Validation of three-dimensional incompressible spatial Evaluation of cloud detection instruments and

I NASA-TP-3094 1 p 13 N92-10027 direct numerical simulation code A comparison with linear performance of arnminar-flow leading-edge test articles

FEMALES stability and parabolic stability equation theones for during NASA Leading-Edge Flight-Test Program

Responses of women to orthostatic and exercise boundary-layer transition on a flat plate I NASA-TP-28881 p It N91-24199

stresses I NASA-TP-3205) p 8 N92-30295 Human Machine Interfaces for Teleoperafors and Virtual

INASA-TP-30431 p 37 N91-19711 FLEXIBILITY Environments Conference

FIBER COMPOSITES Calibration of the 13- by 13-inch adaptive wall test INASA-CP-t00711 p40 N92-11638

Eighth DOD/NASA/FAA Conference on Fibrous section for the Langley 0 3-meter transonic cryogenic FLIGHT TESTS

Composites in Structural Design, part 1 tunnel Transonic Symposium Theory, Application and

INASA-CP-3087-PT-1 I p 22 N92-32513 INASA-TP-30491 p 13 N91-13461 Experiment, volume 2

Eighth DOD/NASA/FAA Conference on Fibrous FLEXIBLE BODIES INASA-CP-3020-VOL-21 p 5 N91-24132

Composites in Structural Design, part 2 lechnique to eliminate computational instability in Airborne Wind Shear Oefection and Warning Systems

(NASA-CP.3087-PT-21 p 22 N92-32574 multibody simulations employing the Lagrange multiplier Third Combined Manufacturers' and Technologists,

FIBER OPTICS [NASA-TP-32201 p 42 N92-23432 Conference, part 1

Small Explorer Data System MIL-STD-1773 fiber optic FLEXIBLE SPACECRAFT I NASA-CP-10060-PT-1t p 9 N91-24166

bus The 5th Annual NASA Spacecraft Control Laboratory Flght tests wih a data hnk used for air traffic control { NASA-TP-3227 J p 16 N92-26667 Experiment (SCOLE) Workshop, part 2 Foigato testswih andtge ue o artafioto

FIELD THEORY (PHYSICS) INASA-CP-10057.PT-21 p 17 N91.19122 information exchange

Workshop on Squeezed States and Uncertainty Fourth NASA Workshop on Computational Control of I NASA-T ER1 CN91-3S43

Relations Flexible Aerospace Systems, pail 1 OW CHARATERISTICS

INASA-CP-31351 p 46 N92-22045 INASA-CP-10065-PT-1 p 17 N91-22307 ircSilTi. s fhh6rmixing layers

FIGHTER AIRCRAFT I NASA p17 N91-22307aINASAoTP-3t6al p8 N92-30909

Transonic and supersonic Euler computations of Fourth NASA Workshop on Computational Control of FLOW DISTRIBUTION

vortex-dominated flow fields about a generic fighter Flexible Aerospace Systems, part 2 Navier-Stokes and Euler solutions for tee-side flows over

INASA-TP-31561 p6 N92-10011 (NASA-CP-10065-PT-21 p 17 N91-22331 supersonic delta wings A correlation with experiment

Static internal performance of ventral and rear nozzle FLEXIBLE WINGS INASA.TP-30351 p 4 N91.13401

concepts for short-takeoff and verlical-landing aircraft A method for the design of transonic flexible wings Calibration of the 13. by 13-inch adaptive wall test

INASA-TP-3t031 p 6 N92-10975 (NASA-TP-30451 p 10 N91-14323 section for the Langley 03-meter transonic cryogenic

Effect of afterbody geometry on aerodynamic Fourth NASA Workshop on Computational Control of tunnel

ciharactearsfis of isolated nonaxisymmetric afterbodies at Flexible Aerospace Systems, part 2 1 NASA-i P-30491 p 13 N91-13461

transonic Mach numbers INASA-CP-10065-PT-21 p 17 N91-22331 A parametric experimental investigation of a scramlet

I NASA-TP-32361 p 9 N92-33706 FLIGHT CHARACTERISTICS nozzle at Mach 6 with Freon and argon or air used for

FILM THICKNESS Flight characteristics of a modified Schweizer SGS1-36 exhaust simulation

Low-energy positron flux generator for microstructural sailplane at low and very high angles of attack I NASA-TP-3048 p 4 N91-16990

characterization of thin films INASA.TP-3022] p 12 N91-10079 Relative effticency and accuracy of two Navier-Stokes

INASA-TP-30741 p 27 N91-22538 FLIGHT CONDITIONS codes for simulating attached transonic flow over wings

FINITE DIFFERENCE THEORY Stagnation-point heat-transfer rate predictions at INASA-TP-3061 p 26 N91-17310

Validation of three-dimensional incompressible spatial aeroassist flight uonditions Detailed flow-field measurements over a 75 deg swept

direct numerical simulation code A comparison with linear I NASA-TP-32081 p 27 N92-3128t delta wing

stability and parabolic stability equation theories for FLIGHT CONTROL INASA-TP-29971 p4 N91-18030

boundary-layer transition on a flat plate NASA Formal Methods Workshop. 1990 An explicit upwind algorithm for solving the parabolized

INASA-TP-32051 p 8 N92-30295 INASA-CP-100521 p42 N91-17559 Navier-Stlokes equations

FINITE ELEMENT METHOD NASA-LaRc Fhght-Cntical Digial Systems Technology INASA-TP-30501 p 4 N91.18032

Nineteenth NASTRAN (R) Users' Colloquium Workshop An upwind-biased space marching algorithm for

I NASA-CP-31 I I p 29 N91-20506 (NASA-CP-100281 p 11 N91t24200 supersonic viscous flow

Computational methods for frictionless contact with INASA-TP-30681 p 26 N91-18381

application to Space Shuttle Orbiter nose-gear tires Development of an integrated aeroservoelastic analysis Experimental investigation of porous-floor effects on

INASA-TP-30731 p 30 N91-22576 program and correlation with test data cavity flow fields at supersonic speeds

Development of an integrated aeroservoelasttc analysis INASA.TP.31201 p 2 N91-26113 I NASA-TP-30321 p 5 N91-19042

program and correlation with test data Application and flight test of linearizing transformations Hypervelocity atmospheric flight Real gas flow fields

INASA-TP-3120j p2 N91-26113 using measurement feedback to the nonlinear control INASA-RP-12491 p26 N91-20418

A three-dimensional finite-element thermal/mechancal problem Aeropropulsive characteristics of canted twin

analytical technique for high-performance traveling wave INASA-TP-31541 p 12 N91-30154 pitch-vectoring nozzles at Mach 0 20 to 1 20

tubes Confrol Center Technology Conference Proceedings INASA-TP-30601 p 5 N91-22069

iNASA-TP-308 1I p25 N91-27436 [NASA-CP-100811 p 14 N92-12010 Effects of yaw angle and Reynolds number on

A method for determining sp-alibevel gear tooth Control integration concept for hypersonic Cruise-turn rectangular-box cavities at subsonic and transonic

geometry for finite element analysis maneuvers speeds

INASA-TP.30961 p 28 N92-10t95 INASA-TP-31361 p 13 N92-20195 (NASA-TP-3099i p5 N91-27124

A-15
FLOW EQUATIONS SUBJECT INDEX

Measurements of forces, moments, and pressures on FOREBODIES Proceedings of the Second Joint Technology Workshop

a generic store separating from a box cavity at supersonic Wind tunnel investigation of vortex flows on F/A-I8 on Neural Networks and Fuzzy Logic, volume I

speeds configuration at subsonic through transonic speed INASA-CP-1006t-VOL-1 J p 43 N91-21778

(NASA-TP-311t0 p 6 N92-10005 INASA-TP-31111 p 6 N92-14968 FUZZY•SYSTEMS

Transonic and supersonic Euler computations of Simulation of real-gas effects on pressure distributions Proceedings of the Second Joint Technology Worksnop

vortex-dominated flow fields about a generic fighter for aeroassist flight experiment vehicle and comparison on Neural Networks and Fuzzy Logic, volume I

INASA-TP-31561 p 6 N92-10011 with prediction INASA-CP-10061-VOL-1 I p 43 N91-21778

Numerical analysis and simulation of an assured crew INASA-TP-31571 p 27 N92-20677 return vehicle flow field FOURIER SERIES

I NASA-TP-3i0t I p 26 N92-10161 Validation of three-dimensional incompressible spatial G

A comparison of airborne wake vortex detection direct numerical simulation code: A comparison with linear measurements with values predicted from potential stability and parabolic stCbility equation theories for GAACI CLUSTERS

theory boundary-layer transition on a flat plate Airen Unteracting d G s n a a

INASA-TP-31251 p 10 N92-10994 j NASA-TP-32051 p8 -30295 Astronomical Union Colloquium No 124

Calculations and curve fits of thermodynamic and FRACTURE MECHANICS GNASA-CP-3098J p49 N91-16C58

transpotapoetiens and qilbim i o 00 GALACTIC COSMIC RAYS transport properties for equilibrium air to 30000 K National Educators' Workshop: Update 1986. Standard Cellular track model of biological damage to mammalian

iNASA-RP-t260i Wind p 26 N92-11285 Experiments in Engineering Materals Science and cell cultures from galactic cosmic rays tunnel investigation of the interaction and Technology [NASA-TP-30551 p5$0 N9t-t698t

breakdown characteristics of slender wing vortices at TnoAogy 2 NAS-T0355 R p c for u

subsonic, transonic, and supersonic speeds INASA-CP-3060] p 20 N91-20207 Radiation protctin for human missions to the Moon

INASA-TP-31 14t p 6 N92-12994 National Educators' Workshop: Update 1991. Standard and Mais

The naturil flow wing-design concept Experiments in Engineering Materials Science and [NASA-TP-3o7g9 p 50 N91-17999

I NASA-TP-31931 p 7 N92-25202 Technology Benchmark solutions for the galactic heavy-on transport

Computational Fluid Dynamics --- numerical methods I NASA-CP-3151 ] p 24 N92-30263 equations with energy and spatial coupling

and algorithm development Applications of FEM and BEM in two-dimensional INASA-TP-3i 121 p 44 N92-13756

[NASA-CP-t00781 p 12 N92-25808 fracture mechanics problems An efficient HZETRN (a galactic cosmic ray transport

Calculation of unsteady transonic flows with mild INASA-TP-32771 p 31 N92-31280 code)

separation by viscous-inviscid interaction FRACTURING [NASA-TP-31471 p 51 N92-22218

(NASA-TP-31971 p 7 N92-28477 National Educators' Workshop: Update 1988. Standard GALACTIC STRUCTURE

A nozzle internal performance prediction method Experiments in Engineering Materials Science and Paired and Interacting Galaxies: inlernational

INASA-TP-3221 p 8 N92-33625 Technology Astronomical Union Colloquium No. 124

FLOW EOUATIONS [NASA-CP-30601 p 20 N91-20207 INASA-CP-3098) p49 N91-16858

Calculation of unsteady transonic flows with mild FRAMES GALAXIES

separation by viscous-inviscid interaction Free vibrations of thIn-walled semicircular The Interstellar Medium in External Galaxies. Summaries

I NASA-TP-3197) p 7 N92-28477 graphite-epoxy composite frames of contributed papers

FLOW MEASUREMENT [NASA-TP-3010) p 29 N91-13750 INASA-CP-3084] p 49 N91-14100

Three-dimensional laser window formation FRAMES (DATA PROCESSING) GAMMA RAY ASTRONOMY

[NASA.RP-1280] p 14 N92-30307 High Resolution. High Frame Rate Video Technology The Compton Observatory Science Workshop

FLOW STABILITY INASA-CP-30801 p27 N91-14574 INASA-CP-31371 p 49 N92-21874

Aeroscoustic and aerodynamic applications of the theory FREE FLIGHT GAMMA RAY BURSTS

of noriequilibrium thermodynamics Wind-tunnel static and free-flight investigation of Development of the Burst and Transient Source

INASA-TP-3t 181 p26 N91-25352 high-angle-of-attack stability and control characteristics of Experiment (BATSE)

FLOW VELOCITY a model of the EA-6B airplant TNASA-RP-1268t pb49 NWs -32006

Analysis of gravity-induced particle motion and fluid I NASA-TP-3194] p 7 N92-25276 The Compton Observatory Science Workshop

perfusion flow in the NASA-designed rotating FREE FLOW INAS. -CP-3137] p 49 N92.21874

zero-head-space tissue cu•lture vesset Detailed flow-field measurements over a 75 deg swept GAMMA 1AY OBSERVATORY

[NASA-TP-31431 p 24 N92-13340 delta wing Development of the Burst and Transient Source

Feasibility study of a tow-energy gamma ray system for I NASA-TP-29971 p 4 N91-18030 Experiment (BATSE)

measuring quantity and flow rate of slush hydrogen FREE WING AIRCRAFT [NASA-RP-1268J p 49 N91-32006

(NASA-TP-31501 p 1

9 N92-25147 DiTrect simulation ot high-speed mixing layers The Compton Observatory Science Workshop

FLOW VISUALIZATION INASA-TP-3186J p8 N92-30909 {NASA-CP-C137j p49 N92-21874

Detailed flow-field measurements over a 75 deg swept FREQUENCY DIVISION MULTIPLEXING GAMMA RAY TELESCOPES

delta wing Destination-directed. packet-switching architecture for The Compton Observatory Science Workshop

[NASA-TP-29971 p 4 N91-18030 30/20-GHz FDMA/TDM geostationary communications (NASA-CP-31371 p49 N92-2187A

FLUID DYNAMICS satellite network GAMMA RAYS

A weakly nonlinear theory for wave-vortex interactions INASA-TP-3201i p 16 N92-19762 Development of the Burst and Transient Source

in curved channel flow FREQUENCY SHIFT KEYING Experiment (BATSE)

INASA.TP-31581 p 7 N92-19175 Advanced Modulation and Coding Technology FNASA-RP-1268i p 49 N91-32006

Aeronautical engineering: A continuing bibliography with Conference Feasibility study of a low-energy gamma ray system for

indexes (supplement 277) INASA&CP-100531 p 16 N92-2200t measuring quantity and flow rate of slush hydrogen

[NASA-SP-7037(277)J p 3 N92-27929 FREQUENCY STANDARDS INASA-TP-31501 p 19 N9P :5147

Validation of three-dimensional incompressible spatial The 22nd Annual Precise Time and Time Interval (PT-rt GAS FLOW

direct numerical simulation code: A comparison with linear Applications end Planning Meeting An explicit upwind algorithm for solving the parabolized

stability and parabolic stability equation theories for [NASA-CP-31161 p44 N91-25755 Navier-Stokes equations

boundary-layer transition on a flat plate Proceedings of the 23rd Annual Precise Trime and Time INASA-TP-30501 p4 N91-18032

[NASA-TP-32051 p 8 N92-30295 Interval (PTTI) Applications and Planning Meeting Hypervelocity atmospheric flight Real gas flow helds

FLUID FILMS [NASA-CP-31591 p 44 N92-33350 INASA-RP-12491 p26 N91-20418 Fundamentals of fluid lubrication FRICTIONLESS ENVIRONMENTS GAS-METAL INTERACTIONS

INASA-RP-1255j p 28 N91-30531 Computational methods for frictionless contact with The interactin of hydrogen with metal alloys

FLUID MECHANICS application to Space Shuttle Orbiter nose-gear tires NASA-TP-31281 p 23 N91-29318

Aeroptopusiorn 1991 [NASA.TP-30731 p 30 N91-22576 GASEOUS DIFFUSION

(NASA-CP-10063] p 12 N91-20086 FUEL CELLS An investigation of microstructural characteristics of

Analysis of gravity-induced particle motion and fluid Space Electrochemical Research and Technology contact-lens polymers

perfusion flow in the NASA-designed rotating [NASA-CP-31251 p 33 N91-32549 INASA-TP-30341 p 21 N91-13492

zero-head-space tissue culture vessel FULL SCALE TESTS The interaction of hydrogen with metal alloys

INASA-TP-3143J p 24 N92-13340 Full-scale semispan tests of a business-jet wing with a NASA-TP-31281 p23 N91-29318

FLUITER natural laminar flow airfoil GEAR TEETH

Fourth NASA Workshop on Computational Control of INASA-TP-31331 p 6 N91-30098 A method for determining spiral-bevel gear tooth

Flexible Aerospace Systems, part 2 FUNCTION SPACE geometry for finite element analysis

JNASA-CP-10065-PT-21 p 17 N91-22331 Trajectory fitting in function space with application to tNASA-TP-30961 p 28 N92-10195

FLUTTER ANALYSIS analytic modeling of surfaces GEARS

Design of control laws for flutter suppression based on [NASA-TP-3232J p 8 N92.30747 Development of a full-Scale transmission testing

the aerody'amic energy concept and comparisons with FUNCTIONAL DESIGN SPECIFICATIONS procedure to evaluate aidvanced lubricants

other design methods Beyond the Baseline 1991. Proceedings of the Space INASA-TP-32651 p 28 N92-30396

I NASA-TP-30561 p29 N91-10328 Station Evolution Symposium. Volume 2: Space Station GELLED PROPELLANTS

Span reduction effects on the flutter characteristics of Freedom, part 1 Upper stages using liquid propulsion and metallized

arrow-wing supersonic transport configurations INASA-CP-I0083-VOL-2-PT- I p 18 N92-17768 propellants

INASA-TP-30771 pit N91-21127 FUSELAGES INASA-TP-31911 p20 N92-17151

Planform curvature effects on flutter characteristics of Two-dimensional aerodynamic characteristics of several GENERAL AVIATION AIRCRAFT

a wing with 56 deg leading-edge sweep and panel aspect polygon-shaped cross-sectional models applicable to Effect of crash pulse shape on seal stroke requirements

ratio of t 14 helicopter fuselages for limiting loads on occupants of aircraft

INASA-TP-31161 p I t N92-13054 INASA-TP-32331 p 8 N92-30394 INASA.TP-31261 p30 N92-08053 FLYING PLATFORMS FUZZY SETS GEOCHEMISTRY

Venturi air-jot vacuum ejectors for high-volume Proceedings of the Second Joint Technology Workshop Fourth Symposium on Chemical Evolution and the Origin

atmospheric sampling on aircraft platforms on Neural Networks and Fuzzy Logic, volume 2 and Evolution of Life

INASA-TP-31831 p 11 N92-20546 INASA-CP-10061-VOL-2J p43 N91-20811 [NASA-CP-31291 p41 N92.13588

A-16
SUBJECT INDEX HOLE DISTRIBUTION (MECHANICS)

planetary geoscrences, 1989-1990 GRAVITATIONAL PHYSIOLOGY Tenth Workshop for Computational Fluid Dynamic

INASA-SP-5081 Ip 50 N92-28345 Techniques f or determination of impact forces during Applications in Rocket Propulsion, part I

GODEoSY walking and running in a zero-G environment INASA-CP-3 163-PT p 27 N92-32278

Types and Characteristics of Data for Geomagnetic Field INASA-TP.3 1591 p 38 N92- 17022 HEAT TREATMENT

Modeling GREENHOUSE EFFECT Outgassing data for selecting spacecraft materials.

INASA-CP-31531 p 31 N92-28620 Climate impact of Solar Variability revision 2

GEOLOGY INASA-CP-30861 p 50 N91-12456 INASA-RP-1 124.RIEV-21 p 21 N91-14437

Volcartism-Climate Interactions GRID GENERATION (MATHEMATICS) HEAVY IONS

[NASA-CP-10062] p 34 N91-21641 NASA Computational Fluid Dynamics Conference fInclusive inelastic scattrling of hieavy ions and nuclear

Planetary geosciences, 1989-1990 Volumle 1 Sessions 1-6 correlations

INASA-SP-5081 po50 N92-28345 [NASA-CP-1I0038-VOL- II p 4 N91-10839 I NASA-TP-30261 p 46 N91-13905 Computational Fluid Dynamics Symposium on Cellular track model of biological damage to mammalian GEOMAGNETISM Aeropropulsion cell cultures fronm galactic cosmic r~j% Types and Characteristics of Data for Geomagneltic Field INASA-CP-30781 p 5 N91-21062 INASA.TP-30551 p 50 -.91-16981 ModelingAnefcetHEA (aglcicomcrytasot BnhakSltosfrteglcihev-otrspt I AAC.13 1N2260 code) equations with energy and spatial coupling Steady induction effects in geolmegnetism Part 1A INASA-TP-31471 p 51 N92-22218 [NASA.TP-31 121 p 44 N92-13756 Steady motional induction of geomagnetic chaos Software Surface Modeling and Grid Generation HZETF1N A heavy ion/nucleon, transport code fir space (NASA-TP-3272-PT-1A1 p 34 N92-32655 Steering Comnmittee radiations

GEOPHYSICS tNASA-CP-31431 If42 N92-24397 INASA-TP-31461 p 51 N92-15959 Planetary geosciences. 1989-1990 Workshop on Grid Generatin and Related Areas Multiple lesion track structure modcel

INASA-SP-5081 p 50 N92-28345 I NASA.CP. 100691 p 12 N92-25712 I NASA-TP-31851 p 39 N92-22186

Types and Characteristics of Data for Geomagnetic Field NASA Workshop on future directions in surface modeling HEISENBERG THEORY

Modeling and grid generation Workshop on Squeezed States and Uncertainty

INASA-CP-31531 p 31 N92-28620 I NASA-CP- 100921 p 8 N92-29625 Relations

GEOSYNCHRONOUS ORBITS Trajectory titling in function space with application to [ NASA-CP-31351 p 46 N92-22045

Thermal-distortion analysis 0f a spacecraft box truss in analytic modeling 0f surfaces HELICOPTER PROPELLER DRIVE

geoslationary orbit INASA-TP-32321 p 8 N92-30747 Experimental and analytical evaluation 0f efficiency 0f

[NASA-TP-30541 p 16 N9 I- 11041 Tenth Workshop tor Computational Fluid Dynamic helicopter planetary stage

On-orbit struc'jiral dynamic performance 0f a 15-meter Applications in Rocket Propulsion, part I I NASA-TP-3063 j p 28 N9 1-12956

microwave ractroineter antenna I NASA-CP-3163-PT-l p 27 N92-32278 Development of a tub-ýscale transnissin testing

I NASA-TP-30411 p p16 N91-171 14 GROUND BASED CONTROL procedure to evaluate advanced lubricants

Launch vehicle integration options for a large Earth Control Center Technology Conference Proceedings I NASA-TP-32651 p 28 N92-30396

sciences geostationary platform concept N9-78 Is NASA-CP- 1006 11 p 14 N92-12010 HELICOPTERS

INASA-TP-30831 p 5N1210 GROUND EFFECT (AERODYNAMICS) Expenrimental and analytical evaluation of efficiency 0f Low-speed, powered ground effects of a generic, helicopter planetary stage Packaging. developmient. and on-orbit assembly options hypersonic configuration INASA-TP-30631 p 28 N91-12956 for large geostalionaly spacecraft tNASA-TP.3092J p 5 N91-25103 Two-dimensional aerodynamic characterislicSof several I NASA-TP-30881 p 17 Ng 1-27182 GROUND SUPPORT EQUIPMENT potygon-shap'd cross-sectional models applicable to GIBBS FREE ENERGY The 25th Aerospace Mechanisms Symposium helicopter fuselages Gibbs tree energy 0f reactions involving SiC. Si3N4. H2, (NASA-CP-31131 p 30 N91-24603 [(NASA-TP-3233 p p8 N92-30394 and H20 as a function 01 temperature and pressure Control Center Technology Conference Proceedings HELIUM INASA-TP-3275J p 23 N92-31278 [NASA-CP-10081 I p 14 N92-12010 The interaction 0f hydrogen with metal alloys

GLASS GROUND SUPPORT SYSTEMS INASA-TP-31281 p 23 N91 29316 Three-dimensional laser window formation Control Center Technology Conference Proceedings HEMATOPOIETIC SYSTEM

fNASA-RP-12801 p 14 N92-30307 I NASA-CP-10081 Jp 14 N92-1 2010 Analyses of risks associated with radiation exposure

GOiDERS GROUND TESTS from past major solar particle even~s Flight characteristics of a modified Schweizer SGSI1-36 Shortcomings in ground testing, environment (NASA.TP-31371 p50 1,191-310615

sailplane at low and very high angles of attack simulations. and performance predictions tor space HIGH FREQUENCIES

I NASA-TP-30221 p 12 N91-10079 applications Time-frequency representation olea highly norstalionary

GLOBAL ATMOSPHERIC RESEARCH PROGRAM I NASA-TP-321 71 p 23 N92-22593 signal via the modified Wigner distribution

NASA/MSFC FY90 Global Scale Atmospheric GROUND-AIR-GROUND COMMUNICATION I NASA-TP-32151 p 25 N92-20492

Processes Research Program Review Flight deck benefits 0f integrated data link HIGH RESOLUTION

I NASA-CP-30931 p 35 N91-16500 communication High Resolution. High Frame Rate Video Technoogy

GOVERNMENT/INDUSTRY RELATIONS I NASA-TP-32191 p1o N92-21459 INASA-CP-30801 p2 7 N91-1 4574

Space Transportation Materials and Structures GROUP THEORY The High Resolution Acceleromrreter Package Il-IRAPI

Technology Workshop Volume I Esecutmve Summary Workshop on Squeezed Stales and Uncertainty tlight experiment summary for the tirst t0 flights

I NASA-rP-3t48-VOL- 11 p 15 N92-22660 Relations INASA-RP-12671 3 N92-22505

Technology 2001 The Second National Technology I NASA-CP-31351 p 46 N92-22G45 HIGH REYNOLDS NUMBEP

Transfer Conference and Exposition. volume 2 GUIDANCE (MOTION) Effects ot yaw angle and Reynolds number on

INASA-CP-3136-VOL-21 p 52 N92-22676 Joint University Program for Air Transportation rectanigular-box cavities at subsonic and transonic

GOVRNMNTSResearch. 1909-1990 speeds ThVERNET FeeI olrneo tlietPoesn NASA-CP-30951 p I N91-19024 (NASA-TP-30991 p 5 N9 1-ý27124 ThipentdrlCneeneo nelgetPoesn HIGH TEMPERATURE SUPERCONDUCTORS

Eqi NS-pme 18n5tN2248 National Educators' Workshop Update 1908 Standard GRNAAPHT-EPOXY38 COMPOSITES87 Experiments In Engineering Materials Science and

Free vibrations of thin-walled semicircular TeMNISNAAChnology20N9220 graphite-epoxy composite framesHAMNC[AA-P36120N 220

I NASA-TP-30 101 p29 N91-13750 Wind turbine acoustics AMSAHTS 1990 Advances in Materials Science and

Comresionbeavir o gaphte-heropastc ad NASA-TP-3057; p 44 N91-16679 Applications 0f High Temperature Supercond.,ctors

graphite-epoxy panels with circular holes or impact HAZARDS N A--30Ip2 N9-10

Space Station Freedom Toxic and Reactive Materials HIGH TEMPERATURE TESTS

damage EadigHigh-temperature durability considerations for HSCT

NASA-TP-30711 p 1N9-81 NASA-CP-30851 Ip 48 N9 1-15930 combustor Properties of three graphite /toughened resin HAEINASA-TP-31621 p 23 N-2.17070

composites HAraZEdsrcurltssofRn 1 oecm INASA-TP-31021 o021 N92-10067 Evaluation 0f cloud detection instruments ,and ThraansrutaletsoRna4hnycm

Exprimnta 0 grphie-eoxyY-sitfned beavir performance of lampinar-Ilow leading-edge test articles integral-tank concept for future space transporation

sxpeimensa eairo rpil-px -tfee during NASA Leading-Edge Flight-Test Program systems seiesloaded in compression IN ASA- TP-28881 p I¶I N9 1 .24199 [NASA-TP-31451 p 30 N92 24205 INASA-TP-3171 J p 30 N92-23115 HISTORIES

Effect of low-speed impact damage and damage location HEALTH Egnsadinvto ei aoaoyadAeia on behaio of cmpositepanelsMicrobiology on Space Station Freedom Enginm echndinovatongy i abrtrndAeia onAAT-96 p22vo Nof28 [NAmAposite p3nel N91-18573 prplso technologyp51N9-197 NAAA-TPP31961 22N9298 PS (AS-5 308 p3

Graphite/epoxy composite adaptars for the Space HEAT AFFECTED ZONE Responses of women to orthostatic ai'd exercise

Shuttle/Centaur vehicle A simolified method for thermal analysisof a cowl leading stresses

I NASA-TP-30141 p 15 N92-31251 edge subject 10 intense local shock-wave-interefeence I NASA-TP-30431 p3 7 N91-19711 GRAVITATIONAL EFFECTS heating Proceedings Of the X-15 First Flight 30th Anniversary

The microgravity environment of the Space Shuttle [NASA-1P.3l871 p 2

7 N92 24797 Celebration

Columbia payload bay during STS-32 HEAT FLUX fNASA-CP-3f051 p 1 Nttl.2DO71

INASA-TP-3141 p p 4

9 N92-1 1931 Thermal-distortion analysis 0f a spacecraft box truss ini NASA engineers and the age of Apollo

Analysis of gravity-induced particle motion and fluid geostatronary Orbit fNASA-SP-41041 p 52 N92?28-144

perfu-ion flow in the NASA-desgiged rotating [NASA-TP-3054I p 16 N9t1-t11041 HOLE DISTRIBUTION (MECHANICS)

zero-head-space tissue culture vessel HEAT TRANSFER Compression behaviror of graphte-thermopiastic and

I NASA-TP-31431 p 24 N92-13340 Modeling of the heat transfer in bypass transitional graphite-epoxy panels with circular holes or impact

Fuel vitilization during exercise after 7 days of be rest boujndary layer flows damage

I NASATP-31 751 p 38 N92-16554 [NASA.TP-31701 p27 N92-tt299 (NASA TP-30711 p 21 N9t1 18215

A- 17
HOLES (MECHANICS) SUBJECT INDEX

HOLES (MECHANICS) H4YPERSONIC FLIGHT IMAGING TECHNIQUES

Stress concentrations for straight-shank and Proceedings ot the X1-15 First Flight 30th Anniversary High Resolution, High Frame hate Video Tecrinology

counltersunktl holes in plates subjected to tension, bending, Celebration I NASA-CP-30801 p 27 N91-14674

and pin loading I NASA-CP-31051 p tO N91-20071 Sixteenth international Lser Radar Conterence, part

I NASA-TP-31921I p 31 N92-25997 Hypervelocity atmospheric flight Real gas flow fields 1

HONEYCOMB CORES (NASA.RP-1249j p26 N91-20418 I NASA-CP.3158 P T -t p 28 N92-29228

A novel method of testing the siiear strength of thick Control integration concept f of hyperxanic, crui-tel Sixteenth international Laser Radar Conterence part

honeycomb composites maneuvers 2

1 NASA-TP-31081 p 2l N,9t-21242 [NASA-TP-31361 p 13 N92-20195 tNASA-CP-3158-PT-21 p 28 N92.310t3

NONE YCOIIB STRUCTURES Roijet-Based Combined-Cycle (R8CC) Propulsion IMPACT DAMAGE

A novel method of testing the shear strength of thick Technology Workshop Tutorial session Compression behavior of graphite-thermoplastic and

honeycomb composites (NASA-CP 100901 p 20 N92-21517 graphite-epoxy panels with circular Poles or impact

I NASA-TP-3td1 0)p 21 N91-21242 An analysis of combustion studies in Shock expansion damage

Determination of the flight hardware configuration oflan tunnels and fefleced shc tunnels INASA-TP-307t11 p 2t N,9t-182115

energy absorbing attenuator far the proposed Spate INASA-TP-3224) p 22 N92-28374 A navel method at testing the sheet strength of thcick

Station crew and equipment translation aid can HYPERSONIC FLOW honeycomb composites

INASA-TP-30841 p 29 N91 -21558 An expliCit upwind algorithrn fi sovn the parabolized I NASA-TP-31081 p 21 N91 21242

Evaluation of a technique to generate artificially Navier Stjokes equations NASA workshop on impact damage to composites

thickened bonaylayers in supersonic and hyesoi I NAAT-00 9-83 ) NASA-CP-ID0751 p 21 N91-29240

flNwsA-P341p ~-8 Evaluation of a technique to generate artificially Prptis o the ahle/ugnd rsn

IAAThermal and srcuatetofhn41oNe1-comb 1 thickened boundary layers in supersonic end hypersonic composites foraladstutra ftrest sa ee tra hnsportaib p6ow INASA-TP.3t021 p 21 1-t0067 integral-tank concept (oIuuesae rnprain NASA-tP-3t421 p6N9f1-28136 Effectoat low-speed impact damage and damagri location

systems Nueia nlssadsmlto fa sue rw on behavior of composite panels

I NASA-TP-31451 p 30 N92-24205 Neumn ericale anlysisead siuainOtnasrdce NASA-TP.31961 p22 N92.2398t

HUBBLE SPACE TELESCOPE reunA veil -T311 flo field0t~ Orbital debris Technical issues end future directions

The role ot failure/problems in engineering. A (NStgA-tP-310 rt ha-rnfrrt p26dictio-s0t6 INASA-CP-100771 p 49 592ý33478

commentary of failures experienced - lessons lertrned tagnoat fighn-ondintihattrnsfe aepeitos IMPACT LOADS

tNASA-TP-32131 p 24 N92-22235 Ieoss fliATP-ht8 Conditions8 Failure behavior of generic metallic and composite

HUMAN BEINGS (NPASA-T-3C HE2T NT2ANSFER aircraft structural components under crash loads

Correlation and prediction of dynamic human Isolated HVPERS tonIC HEAT in TRASF tanfe e prdciosa NASA-RP-12391 p 29 N9t-i375t

joint strength tram leer body mass iagnoass lgtiononinhetitrnsfe aepeitos Properties of three graphitle/toughened resin

INASA-TP-32071 p 40 N92-26682 I NASA-TP-32081 p 27 N92-3128i composites

HUMAN FACTORS ENGINEERINGHYESNCSED(A .T312 21N-06

Avitin Sfey Prgrm /Auomaio Cnfrene imulation of real-gas effects on pressure distributions Techniques tor determination ot Impact forces during

I NASA-CP-30901 p 9 N91-109313 for aia,'rassi- ':.ght experiment vehicle and companison walking and running in a zero-G environment

Manual Control Aspects of Orbital Flight J NASA-TP-31591 p 38 N9? 170i22 (NASACP-10561p 13N91-0147 with peau~ction )NASA-CP-t0056I p1 9-04 NASA-TP-31IS71 2 9-07 IMPACT TESTS Fourth Annual Workshop on Space Operations HYPERSONIC VEHICLES p 7N2267 A novel method at testing the shear strength of thick

NApplications Resarc -t] (StOAR90) Control integration concept for hypersonic cruise-turn honeycomb composites

I App li -cPtion an h VO L r rI SOA 41 N190)1 m ne v r I NASA- TP .3t 108 1 p 2 1 N91-21 242 Fourth Annual Workshop on Space Operations tNASAýTP-3t361 p 13 N92-20t95 Properties of three graphite/toughened resin Apiainan eelClIAR9)HYPERSONICS composites I NASA-CP-3103-VOL~-21 p 41 N91-20702 NASA Computational Fluid Dynamics Conference I NASA-TP-3102j pt21 N92-10067

Effect of short-ter- exposure to stereoscopic Volume 2 Sessions 7-12 An examination of thei damage tolerance enhancement

three-dimensional flight displays on teal-world depth [NASA CP 10038 vOL 21 p

4 5149110868 of carbon/epoxy using an outer lamina ot spectra (R)

perception HYPERVELOCITY FLOW [NASA-TP-3160) ip21 N92-t11142

I NASA-TP-31 171 p ftI N92-13065 Hypervelocity atmospheric fligh't Real gas flow fields Effect of low-speed impact damage and damage location

Fifth Annua Workshop on Space Operations (N SA.-RP- 12a( 0ý2`6 NSA-24141 a n behavior of composite panels

Applications and Research (SOAR 1991), volume 2 Advanced Hypervelocity Aerophysics Facility IMPACATP-OLERANCES98 6 

NASA-CP 3127-VOL 21 pt 41592-22324 WorkshopIMATOLRNE

Cable compliance INASA-OP-I 00311 p 13 N91-24211 A novel method at testing the shear strength of thick

[NASA.TP-32t61 p 24 N92-30378 HYPER VELOCITY IMPACT honeycomb composites

HUMAN PERFORMANCE Orbital debris Technical issues and future directions IN-FLIGTP-t8 021NI9O2124 Ecce,itric and concentric muscle per' - mance following I NASA-CP-f1007 71 p 49 N92-33478 I LGTMNTRN 7 das a Simlatd wightessessA comparison of u.rborne wale vortex detection

I dAySA TP3f siulte 2 -er3h92e17645 measurements with values predicted trom potential

NASATP-382( 3592- 76.5 Itheory The validation ofla human lar:e model to predict dynamic [NASA-TP-31251 p 10 N92r10994

forces resulting from multi-taint niofions ICE INCOMPRESSIBLE FLOW INASA-TP-32061 p 40 N92-26538 West Antarctic ice Sheet Initiative Volume r Science Validationf three-dimensional Incompressible spatial

HYDRAZINES and Implementation Plan direct numerical Simulation code A comparison with lin6ie

Lunar missions using chemical propu~sion System I NASA-CP 3115-VOlL I I p32 N91-20541 stability andparabolic stability equation theories far

design Issues West Antarctic Ice Sheet Initiative Volume 2 Discipline boundary-layer !,ansflion on a flat plate

I NASA-TP-3065( p 19 N91-15308 Reviews I NASA-TP-32051 p 8 N92-30295

HYDRODYNAMIC EQUATIONS I NASA-CP-31t15-VOL-21 p32 N9t-26573 INDEXES (DOCUMENTATION)

Hyperselocity, atmospheric flight Real gas flow fields ICE CLOUDS Aeronauticai engineering A continuing bibliogiaphy with

I NASA-hP-12491 p 26 W~ -2041k b international Workshop on Stratospheric Aerosols indexes (supplement 256)

HYDROGEN Measurements, Properties. and Effects I NASA-SP-7037(256) I pi 1N91.10002

Surface effects on hydrogen permeation through IfvASA-CP-3t 14) p 32 N91-32528 Aerospace medicine and biology A continuing

T, 14A1-2: Nb alloy ICE ENVIRONMENTS bicliography with indexes ISuopp ament 34 1)

INASA-TP-31091 p 23 N91-20266 West Antarctic Ice Shiee' Initiative Volume I Science IlNAS ASOS 7011(34t1(jI p37 N9 1.10594

The interaction of hydrogen with) metal alloys and Implementation Plan NASA Thesaurus supplement A four part cumulative

I NASA-T4'-31281 p23 N91-29318 INASA-CP 3tt5-VOL-tI) p 32 591 20541 -3plemenf to the 198t1 edition of the NASA Thesaurus

Gibbs free energy of reactions involving SiC 5i354, H2. ICE FORMATION Isupplement 4)

anld H420 a-, function ot temperature and pressure Lewis icing research tunnel text of the aerodynamic I NASA-SP-706-4-SUPPL-4 j p 4. N91-10804

I NASA.TP 37751 p23 1492.31278 effects of aircraft ground decicrr:,isnti-icing fluids Aeronautical engineering A crnstlnuing bibliography with

HYDROGEN EMBRITTLEMENT [NASA TP-32381 p r0 N92-30395 indexes (supplement 257)

The inleraction. of hydrogen with meral alloys IMAGE ANALYSIS (NASA-SP-7037f257l1 p f N91-12589

[NASA TO 31281 p 23 N91 29318 Multisaurce Data Integration in Remote Sensing Aerospace medicine and biology A canti-ruing INASA OP-30991 p32 N91-15615 bibliography with indexes (supplement 3421 HYDROGEN MASERS IMAGE PROCESSING I NASA -SP- 7011(342)) p 37 N91 13063 The 22nd Aninuai Preci- v T

ime and Time interval (PT111 High Resoulutoir. Ifigh Fiqarne Rate Video Technology NSAsinfcadtchcl ibcein Acalo Applic;atiOns and Planning Meeting iNASA CP '30101 p027 N91-14574 of specal S pblicatinsd rteren~ce publications Aonflerenc

I NASA-OP-311 tf p 44 N91-25755 Multisource Date Integration in Remote Sensing o pca ulctos eeec ulctosýofrrc

HYDROGEN OXYGEN ENGINES I NASA CP,30991 p 32 N91-t15r'i publications, and fechnical papers. 1989

Tenth Workishop for C;omputational Fiuid Dynamic Pfrioedings, of the Second Joint Technology Workshop I uli'm SP-7063(04)) p 47 N91.i3374

Appiications, in, Roceet Propulsion, part 2 on Neural Nerwcurlr and Fiuzzy Logic volume 2 Aeronautical engineering A continuing bibliography with ;NASA CP.3r63 PT 2! p 7 9232 (NSOPtOtVl.1435t0rr Indexes (supplement 25S)

HYPERSONIC AIRCRAFT Space and Earth Science Data Compression I NASA-SP-703 7t258)] of N 91 '3299

Adivanced Hybervetocity Aerophysics Facility workshop AerospaIce medicine and biology A cc tin, iq

Workshop I NASA-CP 313101 p - * 92-12425 bibliography with indexes (supplemenit 344)

1 NASA CPt10011 p 13 N91-24211 IMAGE RESOLUTION I(NASA SP-7Dlt1(344)i p 37 N91 -4712

Low speed clowered qrmind etfec.n of a generic. The effects of video compiession on acceptabiliry of Aeronautical engineering A contirnuing bibliography with

hýyperno,,Ic confliquiration image% fo monitoarin litfe sciences experiment-, nr~ones ISupplement 260',

!NASA TP 10921 ph 5N41 25103 1NASA rP 32391 p 16 592-339133 NASA. SP 703 7(260)1 pf tN91 15976

A-l8
SUBJEC T INDEX ION SCATTERING

Aeronautical engineering A continuing bibliography with Aerospace medicine and biology A Cmulative indle, INHIIBITORIS

indexes (supplement 259) to a continuing bibliography (supplrrement 358, Electrocriemica stucies of COrrosion irhbitors

I NASA SP-7037l259I ý p I N91 15979 1INASA SP-7011t1356) l p 391 N92 22026 NASA-TP 30661 p 22 N91 17208

Aerospace medicine and biology A cumulative index NASA patent abstracts bibfiOgrapny A corq.nurrg INSERIS

to a Continuing bibliogralphy (supplement 345) bibliography Sectior,2 Indexes (supplement 407) Large scale aeroacokisric research feasib'ily arid

I NASA-SP-701t1J345)1 p37 N91-16547 I NASA-SP 7039(40l-SECr-21 p48 N92 27081 conceptual design of tesi-sixxCtiorr inserts for the Ames 80-

Large siace structures and systems in the Space station Aeronautical engineering A contrinuing bibliography i~ eth by 120-tool wind tunnel

era A biblciograptill with indeies indexes (supplement 2717 1 NASA TP-30201 p4a5 N9! il)824

INASA.SP-7085(01f( p 1 N91-t8199 JNASAýSP.7037J277j] p 3 N92 27929 INSPECTION

NASA Thesaurus supplement A four part Cumulative Aeronautical engineering A cont~nuing biblogriiphy with Second Conference on NOlE I i, Aeriospace

supplement to 'he 1988 edition ot the NASA Thesaurus indexes (Supplement 278) Rleluiremenits

(supplement 5) NASA-SP-7037(278)1 p 3 N92 28677 1 NASA CPý309t( p 16 N9t 1ftt89

)NASA.SP-7064-SUPPL-51 p 47 N9t1-9962 Aeronautical engineering A contrining bibliography with National Educators' Workshop Update taaa Standard

Aeronautical~ eniern Aeonutcl cmltv ndxt iexes (Supplement 2751 Experiments in Engnee~nsg Materials Science anid ngnerngAcuultvendxtoa `ASA-SP 703 7)275) j p 3 N92-28679 rechnology continuing bib' jgraphy (supplement 2611 NASA patent abstracts cibl~ogiaphy A conitinuing NASA CP 3060 1 p 20 N91 20207 INASA-SP-70371261fl Pt

I N91-23073 bibliography Section 2 indexes lhuppljieneit 41) INSTALLING Aeronautical engineering A continuing bibliography with INASA-SPi7039(41 t SECT-2) p 48 N92-3 1465 Large. Scale aeroacoustic research teasibiity and indexes (supplement 2621 Aeronautical engineering A continuing bibliography with conceptual design of test section inserts for the Ames 80- INASA-SP-7037(262l( p I N9t1-23074 indexes (supplement 2801 by t?0-tooi wind tunnel

Aerospace medicine anld biology. A continuing INASA-SP 7037(2800) p 3 N92-31456 1 NASA.TP-3020i p 4! N91-!9824 bilbliography with indexes (supplement 346) INDUCED DRAG INSTRUMENTS I NASA.SP.701t)346(( p 37 N91-23700 Applications of a ditecI/ iterative design method to NASA Wallops Flightr Facility Air*Sea inteiacrCin

Aerospace medicine and biology A continuing Complex transonic configurations Research Pacility

bibliography with indexes (supplement 347) [NASA-TP. 32341 p 8 N92-33484 I NASA-SPý 12 77 p 36 N92 25981 1 NASA-SP-701 t(347( ( p 37 N,9t1-23701 INDUSTRIES INSULATORS

Aerospace medicine and biology A continuing Technology for the Future In-Spacef Technology Low-energy positron tlux generator for microstructral

bibliography with indexes (supplement 3481 Experiments Program, part 1 characterization of thin film$

1 NASA-SP-7Ott(348)1 p 37 N91-23702 (NASA-CP-t0073-PT-1 j pt14 N91t27177 1NASA-TP-30741 p 27 N9t 22538

Aeronautical engineering A continuing bibliography with Technology tor the Future In-Space Technology INTEGRATED MISSION CONTROL CENTER

indexes (supplement 265) Experimentls Program, part 2 Control Center Technology Conference Proceedtings

( NASA SP-703712 p 2 N9t-24095 I NASA-CP-10073-PT-21 p ta N9t-27178 I NASA-CP-t1008t 11 p 14 N92.!2010

Aeronautical engineering A continuing bibliography with INELASTIC SCATTERING INTERACTING GALAXIES

indexes (supplement 263) Inciusive inelastic scattering of heavy ions and nuclear Paired and Interacting Galaxies internationaI NASA-SP.7037(263)1 p 2 N91-24096 correlations Astronomical Union Colcoquium No i 24

Aeronautical engineering A continuing bibliography with INASA-TP-30261 p

4 6 N9t-1t3995 I NASA-CP j.098 I p 49 Ngi-16858

ircdexes Isopplement 264) INERTIA INTERACTIONAL AERODYNAMICS

1 NASA-SP-7037(26.4) p 2 N91-24097 Inertial oscillation of a vertical rotating draft with Wake geometry effects on rotorbae-cre nrcto

Aerospace medicine and biology A continuing application to a supercell Stormi noise directlrety

bibliography with indexesl (Supplement 349) 1 NASA.TP.32301 p 36 N92-33482 INASA-TP-30t5i p 44 N91 12315

1 NASA SP-7011(349l 1 p 37 N91-24731 INERTIAL UPPER STAGE Acolustic and aerodynamic studty Onra pusher-propeller

NASA scientrfic and technical publications. A catalog Upper stages using liquid propulsion and metallilec! aircraft model

of special publications, reference publications, conference propellants I NASA.TP-30401 p 45 N91-21828 publications, and technical papers. 1987.t990 [NASA.TP-31it p p20 N92-17151 Wind tunnel investigation of vortex flows on, F/At 8

I NASA -SP. 70601( p 47 N9t-24939 INFORMATION DISSEMINATION configuration at subsonic through transonic speed

Aerospace medicine and biology A continuing Large space structures and systems in the space Station (NASA. TP-311 t 1)p 6 N92 14968

bibliography with indexes (supplement 3501 era A bibliography with indexes instaallaion effects of wing-moluntedo turboran

(NASA&-SP-70t11(350)) p38 N91-25600 I NASA -SP- 7085(0t1)1 p 17 N9t-t8i199 nacelle-pylons on a '1t7.icale. twinr-enigne. low-wing

Aeronautical engineening A continuing r ibitography willf Technology 2000. volume 2 transport model

indexes (supplemnent 286) 1NASA-CP-310gVOL-21 p 52 N91-24041 I NASA-TP-3t66; p 7 N92-19002

INASA-SP-7037(266)1 p2 N91t27122 Large space structures and Systems in the space station Effect of aftertiody geometry on aerodynamic

Aerospace medicine and biology A continuing era. A bibliography with indexes characteristics of isolated nonlaxisymmetric afferbode at

bibliography with indexes (supplement 351) [ NASA-SP.7085102(( p t8 N9t-20191 transonic Mach numbers

NASA- SP4Ot t (35t If p38 N9t-27756 The develrpment of the NASA aviation safety reporting I NASA-TP-3236 l p9 N92.33706

Large space structures Ind systems in the space station system INTERACTIONS

era A bibliography with indexes y AAFP 14 0N1746 Eetia adcecliealosa asWtita

(NASA-SP-7085(02)1 p18 N91t.28t91 INFORA--TION ~ 59NA0436N paecrct IneatostMr ndeca okro

Aerospace medicine and biology- A continuing INOMTO MANGEEN CP 091t45 9 0C

bibliography with indexes (supplement 352) The t9at Goddard Conference on Space Applications INTERFERENCE DRAG I NASA-SP.7011(352)) p 38 NY91-28729 of Artificial Irrelligence Applicats--ris of a direct/ iterative design method to NASA patent abstracts bibliography A continuing NASA-CP.31 10) p 43 N91-22769 complex transonic configurations

bibliography Section 2 Indexes (supplement 39) The development of the NASA aviation safety reporting fNASA TP-32341I p 8 N9? 33484

1NASA-SP- 7039(391.SECT-21 p 48 N9r-29088 system INTERPOLATION

Aeronautical engineenig. A ontinuing bibliography with I NASA-RPP 11 t 1~ P1 i0 N9 1 70436 An efficient HZE TPN (a galactic Cosmic a,, iranispnnr

indexes (supplement 2681 INFORMATION RETRIEVAL code)

INASA- SP- 703 7(268)1 p 2 N91-30077 NASA Thesaurus supplement A tour part cumulative I NASA TP 3 4 71 p hI N92-2?218

Earth observations and global change decision making supplement to the 1988 edition of the NASA Thesa~urus INTERSTELLAR EXTINCTION

A special bibliography 1991 (supplement 4) interstellar Dust Contributed Paper

[NASA-SP-70921 p 32 N9t-305138 I NASA-SP.7064-SUPPL. 41 p 47 N91 10804 ltiNASA CP 30361 p 48 N91 1489?,

Aerinspace medicine and biolo>gy A continuing NASA Thesaurus supplement A tour part Cumulative INTERSTELLAR MATTER

bibliography with indexes (supplement 353; supplement IC the 1988 edition of the NASA Inesaurus The interstellar Med~u; ihxiernai Galax-es Summaries

i NASA SP. 7011(353)1 p 38 N91 31 7610 fsupplement 5) Of contributed pac'e's

Aeronautical ingineernng A continuing bibliography with NASA-SP- 7064 SUPPIL.51 p 47 N91-19%,? 1 NASA-CP 308A P p 49 N9i r4100

,indeves Isupplement 270) The development of the NASA aviation Iatety reporting Interstellar Dust Gontrributled 0 Prce(I

iNASA SP-7037(270)) p 2 N92?tO973 system IENASA.CP 3036! P 48 N9r 148q',

Aeronautical engineerinq A contInuii.g bitliorapry with INASA-PP- It 14 pto0 N9t-T04,36 INVENTORIES

indexes lsupplement 289) INFORMATION SYSTEMS Twenty-Second Annuai NAS1A S,,tof)v aridF rtjipment

I NIASA-SP- 7037(269)1 p 2 N92 1 t0974 Aeronautical engineering A continuing tbibioraphy witlh Management Conferencp

Aetrospace medicine and biology A continuing indexes (supplement 267) NAýSA (-P I OrA21 p46 Nht I 591

bibliography with indexes (supplement 354) 'NASA SP 70371f267)) p 2 N92 I")1 I NVERSE KINEMATICS

INASA-SP 7t1t(35411 p 38 N92 12404 Spc and Earith Science Data "lmrs~n Tie-.a aflynmnrnnvoors-~ namic

Aero)space medicine and biology A continuing ores Crsn ins~itn from n..i, n -ictions

bibliogtraphy with indexes lbSupplemnent 3551 ) N?22 NASA 793/Fp/ 9?~f

NlASA SP>'D rt)35511 p 18 N9212.r4r2 Cotnu mrvmn ~;orpywt ie INVISCID FLOW

Aeronautical eingineering A contiiiuing bibliograpily with. Cnisu mrvmn iigah i nee Panxii -nerlnxt Ainvciv

rideren tsuppiemerir 2 7t 11989-th9iNAAP qlN4 wp jNASA.SP 7037fill~i p 2 N92 t47*7 !NASA SP. 1097: oaT 4 92 22661, aAnp~q- 5 (,

Aerospace mredicine and bology A cont~inuing Th eenmero n AS vt ilt iohin i eailuiyoil , a., a riusi /y5 Ii~ i 

iblu;r,,raphy with. indexes Sueet35".1 System NA-iA -V 3086 5

1NASA S9 701t 11356H p '18 N492 I Slif4 NASA RP-t t is n 1' I 7raiF 04 Ni' anakysstOS'-it-i i44 -iv1-i

Aeronaurcal enigivarrg A ýorntiwnq bibliography w1it- INFRARED ASTRONOMY let"" ,riiri 11w 7

,nirr5isupylemhnen 2731 litersTellar Dust Ocr irtiurvi PAtx?'s NASA 'Ii OFi , ~ xs~ i

NIASA-SP 07231 3 Nh? 2r.21 77 NASA (,P 03 p 411 N4! 1Ai tON SCATTERING

AnrriiilcairgnurinoA Otiuig Ouigvbhvwii INFRARED RADIATION ii.v iva Siuiiri'if> 54/tiie

NASA !5P 'QIIt.?1.i212 p 3 NW922144 N A SAi(P 373 v 48f N9r41 4' NAiSA TP 3025)6 as Ns. 14

A- 19
IONIC COLLISIONS SUBJECT 7INDEX

IONIC COLLISIONS LAMINAR FLOW Womisttor on Squeezed ijtaftes and Uncertainry

Inclusive inelastic scattering of heavy ions and nucle-i Two-dimensisonal stability of laminar flames Relations

correlatioins I NASA.TP-313t1 p 7 N92-17131 JNASA-CP-$t351 p 46 N92 2204,

1 NASA-TP-3026] p 46 N91- -185 LAMINAR FLOW AIRFOILS Sixteenth i SeinatiOnal Laser Radar Conference, part

IRRADIATION Full-scale semi~span tests of a busriness-jet wing witth a 2

Radiation risk predictions for Space Station Freedom natural laminar flow airfoil I NASA.CP-3i50PT 21 p 28 N92-31013

orbits I NASA-TP-31331 p6 N91-30098 LATCHES

(NASA-TP.30981 p 51 N9t1-26107 LAMINATES The 25th Aarospace Mechanisms Symrposium

Structural properties of laminated Douglas fir/epoxy I NASA-CP-31 t31 P30 Nr91-24603

composite material The 26th Aerospace Metchanusmrs Symposium

I NASA-RP-t1236] p20 N91 lt2t? (NASA-CP-3147) p 30 N92-25067

J-6S ENGINE Free vibrations Of thin-walled semicircular LATTICE PARAMETERS

J-85 let engine noise measured in the ONERA Si winld graphite-epoxy composite frames Equivalent crystal theory of alloys

tunnel and extrapolated to far field (NASA-TP-30101 p 29 N95113750 I NASA-TP-3t155j p23 N9t-30318 (NAS-TP3051 95 N1-t823 ompesson ehaiorof raphte-heiriolasic rid LAUNCH VEHICLE CONFIGURATIONS

(NASA-P-3053 p 45 91-1983 Compessionbehavir of gaphitParametricp Itrade ndtudiestrionraaeSrid-ttonea2Sutale claunc syste JET AIRCRAFT graphirte-epoxy panefs with circular holes or impact architecture Full-scale semnispan tests of a business-let wing with a damage (NASA-TP-3059; p 4 N9t*18160 natural laminar flow airfoil (NASA-1P-30711 ti~ N9t-182t5 Graphite/epoxy composite adapters for thie Space

I NASA-TP-31 33 p 6 Ng91-30098 Properties of three graphite/toughened resin Shuttle/Centaur vehicle JET AIRCRAFT NOISE composites (NASA-TP.30i41 p 15 Nf92 31251 Aeroxcoustics of flight vehicles Theory and practice INASA-TP-31021 p 21 Nf9210D067 LAUNCH VEHICLES Volume 2: Noise control Effect of low-speed impact damage arnd damage location Launch vehficle integration options for a large Earth

I NASA-RP-1258-VOL-21 p 45 N92-14779 on behavior of composite panels sciences geostationary Platform concept JET FLOW I NASA-TP-31961 p 2

2 N92-23981 INASA-TP-30831 p5 14 91 27180 Detailed flow-field measurements over a 75 deg swept suckfing behavior of long symmetrically laminated plates Packaging, development, and oln-rbit assembly options delta wing subjected to combined loadings tor large geost1aflionary spacecraft

[ NASA-TP-29971 p 4 N9f-t8030 (NASA-TP-3i951 p 22 N92-25160 I NASA-TP-30881 P 17 N91 27182 JET PROPULSION LAND MOBILE SATELLITE SERVICE Uipper stages using liquid Propulsion and rmetallized

Engines and innovation. Lewis Labtoratoryi and American Propagation effects for land mobile satellite systems propellants

propulsion technology Overview of experimental arid modeling results [NASA.TP-3t911 p 20 Nf92 t17151

(NASA-SP-43061 pSi N9t-t5975 (NASA-RP-t2741 p 25 ff92-20404 LAUNCHING JET VANES

Static thrust-vectoring performance of rionaxisyrnmetnc LANDING GEAR Metallized propellants for the human exploitation of

conveirgent-divergent nozzles with post-exit yaw vanes Computational methods for frictionless contact with Mars

I NASA-TP-30851 p 5 N91t-21059 application to Space Shuttle Orbiter nose-gear tires (NASA-TP-30621 p 19 N9f-I1600

JOINTS (ANATOMY) I NASA-TP-30731 p 30 N91-22576 LEADING EDGE SWEEP

Correlation and prediction of dynamic human isolated LARGE SPACE STRUCTURES Plantorri urvature effects on flutter characteristics of

joint strength from lean body mass The Sih Annual NASA Spacecraft Control Laboratory a wing with t)6 deg leading-edge sweep and pante aspect

INASA-TP-32071I p 40 N92-26682 Experiment (SCOLE) Workshop, part I ratio of t 14

JONT (UNTON) NAACP1057P-1I 1 911886 INASA-TP-3116; p ft IN92 13054

JOINS (UNCION) IASACP-0057PT- I 16ff9-f t66 LEADING EDGES

Axisymmetnc snell analysis of the space shuffle solid Large space structures and systems in the space station Evaluation of cloud detlection instruments ania rocket booster Ifield joint era. A bibliography with indexes performance of laminar-flow leading-edge test articies

tNASA-TP-30331 p 28 N91-14618 (NASA-SP-7085(Ot)l p 17 1,9t-t18t99 during NAS3A Leading-Edge Flight-Test Program Cable compliance The 5f f Annual NASA Spacecraft Control Laboratory (NASA-TP-28a8j p t I N91-24t99

I NASA-TP-3216] p 24 N92-30378 Expenimentl (SCOLE) Workshop, part 2 Modeling ot the heat transfer in bypass lransifionai JUDGMENTS [NASA-CP-t0057-PT-21 p 17 N91-19122 boundry-tyer flows Annoyance caused by aircraft en route noise Fourth NASA Workshop on Computational Control of INASA-TP-31 701 p 27 ff92-f1299 [NASA-1P-3t651 p 45 Nf92-20479 Flexible Aerospace Systems, part 2 Wind tunnel investigation of the interaction and [NASA-CP-t0065-PT-21 p 17 N91-22331 breakdown characteristics of slender wing vortices at

Packaging, development. and on-orbit assembly options subsonic, transonic, and supersonic speeds K for large geostationaty spaceciatt I NASA-TP-3t 14) to6 ff92-17994

K-ESION URULECEMODL NASA-TP-30688 p 17 Nf91-27182 Wind funnel investigation of vortex flowvs on FIA-18 K-PSLO TRBLECEMOELLarge space structures and systems in the space slat ion configuration at subsonic through transonic speed Modeling 0f the heat transfer in bypass transitionaf era A bibliography with indexes tNASA-TP-3t1t 1 p 6 ff92-1 4968 boundary-layer flows [NASA-SP-7085(0211 p 18 N91-281911 Influence of airfoil geometry on delta wing leadrig-edge INASA-TP-31701 p 27 Nf92-11t299 Multidisciplinary optimization of controlled space vortices arid vorte-induced aerodynamics at supersonic

KALMAN FILTERS structures with global sensitivity equations speeds

A nonlinear estimator for reconstructing the erigutar INASA-TP-3130I p 18 N92-tt087 I NASA-TP-31051 p 7 N92-20038

velocity of a spacecraft without rate gyros Large space st ruct urns and systems in the space station A simplified method for thenrmtal analysis of a cowl leading

I NASA-TP-31 781 p24 ff92-13343 era A bibliography with indexes (supplement 03) edge subject to intense local shock -wave.intesrlererice

KINEMATICS I NASA-SP- 7085(03)1 p 18 N92-22317 heating

State estimation applications in aircraft flight-data The 26th Aerospace Mechanisms Symposium I NASA-TP-31671 P27 ff9224797

analysis A user's manual for SMACK INASA.-e-P-3t 471 p 30 ff92-2506? The natural flow wing-design concept

INASA-RP-12521 p 10 ff91-19082 Automation and Robotics for Space-Based Systems, I NASA-TP-31931 p 7 Nf92-25202

Methods of applied dynamics 1991 LEAST SQUARES METHOD

INASA-RP-1 2621 p 24 N91 -25303 I NASA-CP- 100961 p 43 Nf92-27763 Physicalfy weighted approximations o. unsteady

Steady induction effects in geomagnetisirr Part 1 A: Development of a truss joint for robotic assembly of aerodynamic forces using the minimum-state me-thod

Steady mrotional induction of geomagnetic chaos space structures I NASA-TP-3025) p 4 N91r 16031

1INASA-TP-3272-PTIA I p 34 N92-32655 INASA.TP-32141 p 31 N92-27974 Correlation and prediction of dynamic human isolatedl

KINETICS LASER ANEMOMETERS joint strenlgth from lean body mass

Cellular reparir/rrsrepair track model Three-component laser anesmometer measurement I NASA-TP-32071 p 40 ff92-26682

I NASA-TP-3124J p 4

2 ff92-f 165 systems LESIONS

KNOWLEDGE BASES (ARTIFICIAL INTELLIGENCE) I NASA-TP-30801 pS 1491f-19057 Multiple lesion track structure model

Se%,ond CLIPS Conference Proceedings, volume?2 Laser anemometer measurements and computations in INASA-TP-31851 p 39 ff92221 86

1INASA -CP- 10085-VOL-21 p 42 ff92A6590 an annular cascade of high turning core turbine vanes LETHALITY

KNOWLEDGE REPRESENTATION INASA-TP-32521 p8 ff92-28980 Cellular reparrlmisrepair track modlel The 191 Gdda n Spae Aplicaions LASER APPLICATIONS [AAt-14 2N21l8 ohe At-fc9lItellGeda-orni nSaeApiain Three-dimensional laser window formation LEINS-P324 pN2UMBERS68 ofAJiil nelg NASA-RP-t2801 p 14 N92-30307 LEWIS NME imnso stblyofimn lare 1NASA-CP3t t10 p43 N91t-22769 LASER DOPPLER VELOCIMETERS Two-dimensional stblt o7 lamna 1ames Second CLIPS Conference Proceedings, volume I Three-component later anemometer measurement IAAT-ttI7 N~~~ I NASA-CP-t10y85-VOL- I p 42 Nf92,16568 systems LIFE (DURABILITY'1

I NASA-TP-30801 p 5 N91-19057 Structural Integrity and Durvability, or Reusable Space

L ~~~~LASER INTERFEROMETRY anmmtrmaueef Propulsion, Systerris

systems LIFE SCIENCES

LAGRANGE MULTIPLIERS INASA-TP-30801 p5 ff91.19057 Fourth Annuai Workshop on Space Operations

Technique to eliminate computaliinal instability in LASER WINDOWS Applications and Research (SOAR 901

niulfibody simulations employing the Lagrange multiplier Three-dimensional laser window formation INASAýCP 3103-VOL-1Il p 41 ff91 7iti$.u fNASA TP 32201 p 42 Nf92-23432 I NASA-RPt12801 p 14 ff92 30307' Aerospace medicine and biology A coctnturig

LAMINAR BOUNDARY LAYER LASERS bibliography with mnexes, (supplement 37)~

Evaiuation of cloud detectiorn instruments and Wind tunnel investigation of the interacllont and I NASA-SP-7011(35 71 p39 N92 217'4

pqrr-iomsnce of laminar-floI- leading edgie test articles trealdown, chalacerisfics of slender wing vortices at Aerospace medicine and biology A conri~nuing

during NASA Leading Edge F light-Test Program subsonic transonic and supersonic speeds bibliography with inde~xes tsuppiemerit 359i

I NASArP 2e888 p ftI N91-24t199 1INASATP 31141 p6 Nf9212994 1 NASA SP 71otI3S9)l 0 39 NW 172715

A-20
SU&IECT INDEX MAN-COMPUTER INTERFACE

Fifth Annual Workshop on Space Operatioins The effect of acceleration versus displacement methods LUNAR BASES

Appiltions and Research (SOAR 1991). volume 2 on steady-state boundary forces Lunar missions using chemical propulsion System

1NASA-CP-3l27-VOL-21 P 41 N92-22324 INASA-TP-32181 p 30 N92-21457 design isuess

LOEF: 69 Months in Space. First Post-Retrieval Stiffness and strength tailoring in uniform space-filling (NASA-TP.30651 p19 N91-15"0

Symposium, part 2 truss strujctures5 LUNAR SURFACE

(NASA.CP-3134-PT-21 p 52 N92-24808 [NASA.TP.32101 p 30 N92424546 Radiation protection for human mnissions to the, Moon

Aerospace medicine and bioog A continuing Suckling behavior of long symmetriclly larmeated plates and Mara

bibliography with indexes (suppternent 362) subjfected to comriiuied loadings I NASA-TP-30791 p 50 N9 1-17999

INASA-SP-70 11(362)l p 39 N92-27068 I NASA-TP-31951 p,22 N92-25160

LOEF 69 Months in Space First Post-Retrieval Effect of typ of load on stress analysis of thin-walledM

Symposium. par 3 duicts

JNASA-CP-3134-PT-31 p 52 N92-27M6 INASA.TP-32461 p 31 N92-26669

Aerospace medicins and biology: A continuing LCaIC CIRCUITS MACH NUMBER

bibliography with indeses (supplement 361) Proceeding~s of the Second Joint Technology Workshop Expenimental inviestigation of porous-floor aftectIs on [NASA-SP-701I)361)) p 39 N92-27433 on Neural Networks and Fuzzy Logic, volume I cavity, flow fields at supnersonic speeds Aeronautical engineering: A continuing bibiliogralphy with (NASA-CP.10061-VOL-1 I p 43 N91-2i178 fNASA.TP.30321 pS N91-19042

indees (upplmen 275 LOGC DEIGNEffects of yaw angle anid Reynolds number on (NASA-SP-7037(275)1 p,3 P492-28679 NASA Formal Methods Workshop, 199 rectangular-box cavitie at subsonic and tcainaolr

Aerospace medicine anid biolog: A continuing INASA-CP-100521 p 42 N91-17559 speeds bibliography with indexes (supplement 363) LOGISTICS I NASA-TP-30991 p 5 N91-27124

INASA-SP-7011(363)) p 39 N92-30987 Twenty-Second Annual NASA Supply and Equi~pment Parametric investigation of single-expainsion-ramp The effects of video compression on acceptability of Management Conterence I19 oze tMOnmesfo o12 images for mnonitonrig tile sciences expeniments I NASA-CP-100421 p 46 N9I-51 (nozlSAT320 at Mac numer2fom3401932 : NASA-TP-32391 p 16 N92-33933 LONG DURATION EXPOSURE FACILITY )AAT-2Ip9N23 9

LliS SUPPORT SYSTEMS Long-term orbital lifetime predictions MAGNETIC BEARINGS

Aeorospace medicine and bioog A continuing [NASA-TP-30581 p 13 N91-t0092 Aerospace Applications of Magnetic Suspension

bibliography with indexes (supplement 343) First LOEF Post-Retrieval Symposium abstracts Technology, par 2

(NASA-SP-7011(343)1 p 37 NSI-14711 INASA-CP. 100721 p 52 N91-24972 (NASA-CP-1006-PIT-2( p 17 N91-21203

LIFTING REENTRY VEHICLES LOEF- 69 Months in Space. First Pott-Retneval International Symposium oni Magnetic Suspension

Numenicel analysis and simulation of an assured crew Symposium, part ITechnology, part I

return veti ie flow hield I NASA.CP.3134-PT-1 I p 52 N92-23280 I NASA-CP.3152-PT-1 I p 18 N92-27721

[ NASA-TP-3 10 1 p,26 N92-10161 LDCF 69 Months in Space First Post-Retrieval International Symposium on Magnetic Suspensilon

LIFTING ROTORS Symposium, part?2 Techniology. par 2

Transonic flow analysis for rotors. Pert 3, [NASA-CP-3134-PT-21 p 52 N92-24806 [NASA-CP-3152.PT-21 p 16 N92-27788

Three-dimeinsional, quasi-steady. Euler calculation LOEF: 69 Months in Space First Post-Retrieival MAGNETIC CONTROL

I NASA-TP-23751 p3 NOI-10007 Symposium, part 3 International Symposium on Magnetic Suspension

LIGHTNHING (NASA-CP-3134-PT-31 p 52 N92-2,383 Tecfrrioogy. pWr I

The 1991 International Aerospace and Ground Second LOEF Post-Rftrieval Symposium abstracts (NASA.CP.3t 52-PT-1I) p 18 N92-27721

Conference on Lightning and Static Electricity, volume I INASA-CP-10097) p 52 N92-27218 MAGNETIC EFFECTS

fNASA-CP-3106-VOL-1 I p 35 N91-32599 LONG DURATION SPACE FLIGHT Steady induction effects in geomagnietism Part IA

The 1991 International Aerospace and Ground Workshop on Exercise Prescription tor Long-Duration Steady motional induction of geomagnetfic caosci

Conference on Lightning and Static Electricty, volume 2 Space Flight (NASA- W-3272-P3T-I1AI p 34 N92-32655

[ NASA-CP-3106-VOL-21 p 36 N91-32693 (NASA-CP-3051 p p36 N91-10574 MAGNETIC FLUX

LIGHTNING SUPPRESSION LONG TERM EFFECTS Steady induction effects in geomagnetisin Part 1 A

The 1991 International Aerospace and Ground Long-taerm orbital lifetime predictions Steady motional inuction of geomragnetic chaos

Conference on Lighltning and Static Electricity, volume 1 INAS/-TP-3058) p t3 N91-10092 I NASA-TP-3272-PT- IAjI p 14 N92-32655

I NASA-CP-3106-VOL-1 I p 35 N91-32699 First LDEF Poal-Retneval Symposium abstracts MAGNETIC INDUCTION

LIMB DARKENING I NASA-CP- 100721 p52 N91-24972 Steady induction effects in geormagnetism. Pert IA

Limb-darkening functions as derived firm along-track L0NGITU0II4AL ST4SIuTY Steady motional induction of geomagnetic: chaos

operation of the ERBE scanning radiometers for August Longitudinal aerodynamic charactenistics of a subsonic, I NASA- TP-3272-PYT- IA I p 34 N92-32655

1985 energly-efficient transport configuration in the National MAGNETIC LEVITATION VEHICLES [NASA-RP-12431 p134 N91-1 4663 Transonic Facility Inentoa Symposium on Magnetic Suspension LINEAR ENERGY TRANSFER (LET) [ NASA-TP-29221 p6 N91.28143 Technology, par I Track structure model of cell damage in space flight LOUDNESS [NASA-CP-3152-PT-11 p 18 N92-27721

LINEARSYSTEM51p39N2-45 A loudness calculation procedure applied to shpe MAGNETIC MEASUREMENT LNAR mYSEthdoog frcmui ucranybndof sonic booms A schema for benldpeass tiltaring magnetometer Ametiharioleosytm base ooptng setrstaility thedsory [NASA-TP-31 341 p 45 N92-1 1765 measurements to reconstruct teteed satellite skipiope

concepts LWSEDmto

I NASA-TP-31661 p 13 1492-21410 Low-speed, powered ground elfecit of a generic. INASA-TP-31231 p 42 NSI-25M2

Identification of linear systems by an asymptotically hypersonic configuration MAGNETIC SUSPENSION

stable obsre [NASA-TP-30921 p 5 N91-25103 Aerospace Applications of Magnetic Suspension

[NASA-TP-3 164) p 31 N92-26537 Full-scale sensspsn tests o1 a business-jte wing with a Technology, per I

LININGS natural laminar flow airfoil (NASA-CPD-1006ilPT-I p 17 Ng1-.21188

Large-scale aeroacoustic research feasibility and (NASA-TP.3133) p 6 N91-30098 Aerospace Applications of Magnetic Susenio

conceptual design of test-section inserts for the Armex so- NACA 0015 wing pressure and Iraifn vortex Technology. part 2

by 120-foot wind tunnel measurements (NASA-Ci--10066-PT-21 p 17 N9t1-21203

[NASA-TP.30201 p 45 N91-19824 [NASA.TP-3t511 p 6 N92-10981 fInternational Symposium on Magnetic Suspenscion

Higf-temperature durability considerations for HSCT Effectof low-speed impact damage and damage location Technology, per 1

combustor on behavior of composite panels I NASA-CP-3152-PT- I I p 18 N92-27721

INASA-TP-3t621 p 23 N92,17070 INASA-TP-31961 p 22 N92-23981 International Symposium on Magnetic Suspension

'LIQUID CRYSTALS LOW THRUST PROPULSION Technology. par 2

Positron lifelime measurements in chiral nemnalic liquid Magnetuplassmadynemic Thruster Workshop fNASA-CP-3152-PT-21 p 18 N92-27766

crystals [NASA-CP-100841 p 20 N92-10044 MAGNETOPLASMADYNAMICS

INASA-TP-31221 p 4

6 N92-10677 LUBRICANT TESTS Megnestoplasimadnmir Thrsuter Workshop

LIQUID PROPELLANT ROCKET ENGINES Development of a full-scale transmission testing I NASA-CP-I 0004) p 20 N92-1004-

Tenth Workshop tor Computational Flitd Dynamic procedure to evaluate ad~anced lubricants MAINTENANCE

Applications in Rocket Propulsion, part? 2 NASA-TP-32651 p 28 N92-30396 Structural properie of laminated Douglas firlepoxy

[NASA-CP.3163-PT-21 p 27 N92-32245 LUBRICATING OILS composite malarial

Tenth Workshop for Computational Fluid Dynamic Development of a lull-scale transmission testing )NASA-RP-t2361 1120 N91-10127

Applications in Rockiet Propulsion, pert I1rcdr oeaut dacdlbiat Reliability traininig

[NASA-CP,3163-PT-1 J p 27 N92-32278 procedure265 to evlut advanced6 Iurc~NASA-RP-1253) p 15 N92-32456 LITHIUM SULFUR BATTERIES )NS-P36)p8N2336 MAN ENVIRONMENT INTERACTIONS

rhe 1990 NASA Aerospace Battery Workshop LUBRICATION CiaeIpc fSia aiblt

I NASA -CP-3 t191 p 20) N92-27 130 Fundamentals ot fluid lubnicationl [A -Climate Imac f So9arVanai45t

LOAD DISTRIBUTION (FORCES) INASA-PP-12551 p28 N91-30531 MAN MACHINE SYSTEMS

Static footprint local forces. areas, and aspect ratios Development of a full-scale trasmirnssion testing Aviation Safety/Autorneltion Program Conference tor thr~ee type 7 aircrahttirss procedure to evaluate advanced lubricantls (NASA-CP-30901 p9 N9I-10936

I NASA-TP.29831 plo0 N91-17014 [NASA-TP-32651 p 28 N92-30396 Cbecmlac

LOADS (FORCES) LUMINAIRES I NASA-TP-32161 p 2

4 N92 30378

Research in Structures. Structural Dynamics and Long-term life testing ot GeostationarY Operational MAN-COMPUTR INTERFACE

Malw'ails. ~ Envitonmrentlal Satellite tGOF-S) encoder snipe Aviation Safety/ Automation Program Conference

INASA CP 3%)641 p29 N9t-10301 INASA-RP-t2731 p?23 N92-20063 INASA-CP-30901 p9 N91-10936

Effect of crash pulse shape on spol stroke requirements LUMINOSITY Fourth Annual Workshop on Specep Operations

tor limiting loads on occupants of aircraft Climate Impact of Solar Variability Applications and Research (SOAR 90) NASA-T P 31261 p 30 N92 18053 (NASA-CP-30566 pt50 N91-12456 INASA-CP-3103-VOL-2) p 41 N91-20702

A-21
MANAGEMENT SUSJIECT INDEX

Human machine Interfaces for Teleoperators and Vvirual MATERIALS HANDLING MECHANICAL PROPERTIES

Environments Conference Space Station Freedom Toxic and Reactive Materials Eighth DOO)NASAiFAA Gonleerh'co 0on FLo~s

INASA-CP-100711 p 4

0 N92-1 1638 Handling Composites in Struetweal Design part I

MANAGEMENT I NASA-CP-30851 p 48 N9I-15930 1 NASA.CP.308?.PT-1.l p 22 N92 52513

Management. A bibliography for NASA managers MATERIALS SCIENCE MESOSPHERE

I NASA-SP-7500(25)I p 46 N9t-24936 The Federal Conference on Intelligent Processing S~ixteenth lintent~inonal Laser Radar Confrrience parl

Management A bibliography for NASA managers Equipment 2

1 NASA-SP-7500(26fl p 47 N92-27080 I NASA-CP-31381 p 52 N92-24987 I NASA-CP-3158-PT 21 p?8 N92 31013 MANAGEMENT METHODS MATHEMATICAL MODELS METAL AIR BATTERIES

Twenty-Second Annual NASA Supply and Equipment Structural properties 0f laminated Douglas firiepoxy The 1991 NASA Aerospace Battery 8korohhop

Managerment Conference composite material INASA-CP-31401 r 33 N92 22740

INASA-CP-100421 p 46 N91-11591 (NASA-RP-12361 p 20 N91-10127 METAL HYDRIDES

Issues in NASA program and project management NASA Computational Fluid Dynamics Conference The interaction ot hydrogen with, metal ailcys

[NASA-SP.6101(03)1 p46 N911-13347 Volume I Sessions 1.6 INASA.TP-31281 p23 N91 29:31,8

Management A bibliography for NASA managers (NASA -CP-1I0038-VOL- 11 p 4 N91 .10839 METAL PROPELLANTS

JNAS'h-SP-7500(251J p

48 N9i-24936 Failure behavior of generic metallic and composite Metallized propellants lor tme humnan expiorat~or of Proceedings of the Second Annual NASA Science aircraft struictural components under crash loads Mars Inrternet User Working Group Conference INASA-RP-12391 p 29 1,91-137S1 I NASA-TP.30621 pi t 9 119r80y0

[NASA-CP-31171 p 48 N91,27009 The 5th Annual NASA Spacecraft Control Laboratory Lunat missio'ns using cnemical propuisoon System Issues in NASA program and project management Expeniment (SCOI.EI Workshop. part 1 design issue INASA-SP-6t0t(04)1 p 46 N91-28026 I NASA-CP. 1OS7-PT- I I p16 N91-18186 I NASATP-30651 p 19 N91 15306 Management: A bibliography for NASA managers The 5th Annual NASA Spacecraft Control Laboratory Uprsae sn iudpouso n eaic

I AS-S-7002)Jp4 N2-700 Expeniment (SCOLE) Workshop, part 2prelat Issues in NASA program and project management [NASA-CP-10057.PT-2] p 17 N91-19t22 (rNpeSAnTPs11Ip2 9 75 1 NASA-SP-6101(05)1 p 47 N92-27609 Numenical studies of convective cooling for a locaily MTLUG MANAGEMENT PLANNING heated skin MTLUG

Management A bibliography for NASA managers [NASA.TP-3t001 p 26 N91-22509 Natronal Educators Workshop update 199 1 Standard

I NASA. SP- 7500(25)) p 4

6 N91-24936 Model reduction by trimming for a class of semi-Markov Expenments in Engineering Matrirais Scoence and

Management. A bibliography for NASA managers reliability models and the corresponding ertor bound 'Technology

INASA-SP-7500(26)i p 47 N92-27080 I NASA.TP-30891 p 43 N91-25741 I NASA-CP.3151 1 24 N92? 302t3

MANEUVERABILITY Development of an integrated aeroservoelastic analysis METALS

Prediction of eff ects of wing contour modifications on program and correlation with test data Structural deterministic safety fac:tors selectior criteria

low-speed maximum lift and fransonic performance for the (NASA-TP-31t201 Ilp 2 N91t 261 13 and verification

EA-6B aircraft Shock wave interaction with an abrupt area change (NASA.TP-32031 p K0 N2- !931t;

[NASA-TP-30461 p4l N911-109402 I NASA-TP-3113J p 6 N91-271 40 METEOROLOGICAL PARAMETERS

MANIPULATORS A method for determining spiral-bevel gear tooth West Antarctic ice Sheet initiative volume I Scýencp

A generalized method for multiple robotic manipulator geometry for finite element anatysis and implementation Plan

programming applied to vertical-up welding I NASA-TP-30961 p 28 N92-10195 I NASA-CP-31 15-VDL-II P32 N91 2051i4

[NASA-rP-31631 p 24 N92-11218 Seals Flow Code Development NASAIMSFC FY91 Cilota. Scale Atrrosphieric

MANNED MARS MISSIONS INASA-CP-100701 p 15 N92-1 5082 Processes Research Ptogramr Review Metallized propellants for tne human exploration of Multiple lesion track structure model (NASA-CP.31261 P 35 N91 -32660I Mars INASA-TP-31851 p 39 N92-22t58 METEOROLOGICAL RADAR I NASA-TP-30621 p 19 N91 -1 1800 An efficient HZETRN (a galactic cosmic ray transport Airborne Wind Shear Detection and warning Systems International exploration of Mars- A special codef Third Combined Manufacturers 30d Technoiogsiss

bibliography [NASA-TP,31471 p SI N92-22218 Conference, part?2

(NASA-SP-70911 p 49 N91-24965 Improved accuracy for finite element structuraf analysis I NASA-CP-10060-PT-21 p 9 N91-24r40I Dngoing Progress in Spacecraft Controls via a new integrated torce Method METEOROLOGY [NASA.CP-10099] p 19 N92-28730 INASA.TP-32041 p 30 N92-22227 NASA/MSFC FY90 Global Scane Afmospheric MANNED SPACE FLIGHT The High Resolution Accelerometer Package (HiRAP) Processes Research Program Review MIRACAL. A mission radiation calculation program for flight experiment summary for the first 10 flights [NASA-CP-30931 p 35 N91 86500 analysis of lunar and interplanetary missions JNASA-PP-i 2671 p 3 N92-22505 Te2n nulPes ieadTm nevlITi

(NAA-T-31 1p~iN9-2500 Software Surface Modeling and Grid Generation Applications and Plarnniig meeting MANNED SPACECRAFT Steering Committee A -P316p4Nt275

Ongoing Progress in Spacecraft Controls I NASA-CP-3143] p 42 N92-24397 JNASAMSFC FY91 Sca plpa 4 Almopheric

[NASA-CP-10099] p 19 N92-28730 MIRACAL A missin radiation calculation program for ProcsAses Resarc Program Review Amspe

MANUAL CONTROL anatysis of lunar and interplanetary missionsPrcseRsachpoamevw

Manual Control Aspects of Orbital Flight f NASA-TP-3211 1 p 51 N92-25100 [NASA-CP-31261 p35 N91-326601

JNASA-CP-100561 p 13 N91t-2014 7 Computational Fluid Dynamics --- numerical methods MICROBIOLOGY

MANUFACTURING and alginythmi development Microbiology on Space Station Freedom

Technology 2001, The Second National Technology INASA-CP-100781 p 12 N92-25808 INASA-CP.31081 p37' N91 18573

Transfer Conference and Exposition. volume 1 Calculation of unsteady transonic flows with mild MICR013URSTS (METEOROLOGY)

[NASA-CP-3136-VOL- I p 52 N92-22423 separation by viscous-inviscid interaction Airborne Wind Shear Detection and Warning Systems

Technology 2001. The Second National Technology INASA-TP-31971 p 7 N92-2F477 Second Combined Manufacturers and Technologists

Transfer Conference and Exposition. volume 2 Trajectory fitting in function Space wilth application to Conference, part 2

INASA-CP-3136.VOL-21 p 52 N92-22676 analy-tic modeling of surfaces fNASA-CP-10050.PT -21 p9 N91-. 1695

MARINE METEOROLOGY (NASA-TP-32321 p 8 N92-30747 Airborne Wind Shear Detection and Warning Systems FIRE Science Results 1988 Eighth D)OD/NASA/F SA Conference on Fibrous Third Combined Manufacturers and Technologists,

NASA-CP-30831 p 34 N91-10448 Composites in Structural Design, pant I Conference, part 2

MARIKOV PROCESSES INASA-CP-3087-PT-1I p p22 N92-32513 JNASA-CP.i0060-PT 21 p9 N91-241AO

Model reduction by tnrnmming for a class of semi-Markov Inertial oscillation of a vertical rotating draft with Airborne Wind Shear Detection and Wartsng Systems

reliability models and the corresponding error bound application to a superceit sform Third Combined Manufacturers' and Tectinolcgisls

[NASA-TP-30891 p 43 N91-25741 I NASA-TP-32301 p 36 N92-33482 Conference, part 1

Identrfication of linear systems by an asymptotically Advanced' techriques in reliability model representation I NASA-CP-10060.T-1 I p 9 N9t -241t66

stable observer and solution IMICROGRAVITY APPLICATIONS

rNASA-TP-3164J p 3 1 N92-26537 INASA-TP-32421 945 N92-33483 Space Station Freedom Toxic and Reactive MateriaiS

MARS (PLANET) Inertial oscillation of a vertical rotating draft with Handling

Evobiology on Mars application to a supercell storm. Video supplement to INASA-CR-3o851 p 48 N91 r5930

I NASA-CP-t00551 pat1 N9t 15691 NASA Technical Paper 3230 MICROORGANISMS

MARS ATMOSPHERE I NASA-TP-3230-VIDEO.SUPPLI p 36 N92-34246 M~crobiotogy, on Space Station Freedom

international exploration of Mars A spezial MATRICES (MATHEMATICS)1AAP310 p3 N9187

bibliography Physically weighted approximations of unsteady NACRSA.UCP-10103'NRIt8

INASA-SP-70911 1p49f N91-249'5 aerodynamic forces using the minimum-state method MCRScUTR

MAS NIRNEN(NASA.TP-30251 p4 N91.18031 An investigation of mtcrosstructrual characieristcs 01

MAioRSaEVIONEN On the tormulation of a mifnimal uncertainty model for *-nfact-lens polymers

Inte--iational exploration of Mars A special robust control with structured uncertainty I NASA. IP-30341I p 21 N91 134-492 bibliogrphy'9 p[ INASA-TP-30941 p 13 N92 10021' investigation of incrosiruclural changes in NAAS701p49N91 -24965 MAXIMUM LlKELIHf)OD ESTIMATES polyetherelhvr-ketono films at cryogenic temperatures by

MARS SURFACE User's guide Nimbus.? Earth radiation Ibuigel positron litetme speciroscolpy,

Radiation protection for human missions to the Moon narrow-field-of viey prottucts Scene radiance tape I NASA TP-306d I p 21, N91 -Ih2rf.

and Mars products, sorting into angular bins products, and mavimum Low-energy positron flow generator for microslructirja !NASA- TP-30791 Ip 50 N9t -17999 lik-ilihood cloud estimation products characterization of ti~n lrins

Sand and Dust on) Mats INASA-ftP 12461 p 34 N9t-1Q043 !NASA TP-301'4! p 27 Nd9t 22115A

'N4ASA CP- 100741 p p50 N91-27057 MEASURE AND INTEGRATION MICROWAVE RADIOMETERS

Electrical and chemical interactions at Mars Workshop, Impfoved accuracy for finite element tructufai analysis On-oriti slrsctciai dynamic periroim4'rý -ii a i S wei,i

part I via a new integrated force mrethodl microwave iadiorntWer anteinnua

'NASA -,P- 10093 i p 50 N92-30302 I NASA-TP-32041 p 30) N92-22P27 INASA.TP -1.i0r 1 p ir. N91 71 '

A-22
SUBJECT INDEX NITROGEN TETROX IDE

MAIMO (CONTROL SYSTEMS) Eccentric and concentric muscle Performarnce following NAVIGATION

A methodology for computing uncertainty bounds of 7 days of simulated weightlessness Joint University Program ltr Air Transportation

multivariable systems based on si3ctor stability theory INASA-TP-31821 p 39 N,92-t 7645 Research, 1989-1990

concepts I NASA-CP -JOSSI p1I N91-19024

(NASA-TP-31661 p 13 N92-21410 NJoint ]riversity Program for Air Transportaton

MINERALOGY NResearch. 1990.1991

Sand and Dust on Mars NAELE NASA-CP-3t31 I p 3 N92 17984

MISIN PLANNING4105 91275 Applications of a direct/ iteratlive design method to NAVIGATION SATELLITES

MISS liO ed pLANNI lntsfrtehmnepoaino complex transornic configurations Proceedings of the 23(d Annual PreciSe Tsme "nd sime

Mears zdpoelnslxth ua alrln0 [NASA-TP-32341 p 8 N92-33484 Interval (PT-TI) Applications and Planning Meeting

MNarSAT30 NASA PROGRAMS NASA-CPý31591 p 44 N92 33350

NAS-T-3021p 19 N91-1 1800 Issues in NASA program and project management NEAR WAKES

Exiobiology on Mars INASA-SP.6101(03)) P46 1,91-13347 A companison of airborne wake xortex detection

INASA-CP.100551 p 41 N91-15691 Engines and innovation Lewis Laboratory and Amtericanl measurements with valves predicted from potential

Vision-21 Space Travel for theo Next Millennium propulsion technology the"rt

1 NASA-CP- 100591 p 13 N91-22t39 I NASA-SP-43061 p 51 N91-15975 INASA-TP-3t251 p t0 N92-10994

First among equals The selection of NASA space NASA patent abstracts bibliography A continuing NETWORK( CONTROL

science experiments bibliography Section 1 Abstracts (supplement 38) Space Netiw'ork Control Conterence on Resource

INASA-SP-421 51 p 52 N91 2606;) (NASA-SP-7039(38)-SECT. I I p 47 N9 1-17833 Allocation Concepts and Approaches

Resource envelope concepts for mission planning NASA Patent abstracts bibliography A continuing (NASA-CP-31241 p 16 N92-11039

I NASA-TP-31391 p 15 N91 .29209 bibliography Section 2 indexes (supplement 38) Space Communications Technology Conferensce

Flight Mechanics/Estimation Theory Symposium,' 1991 1NASA-SP-7039(381-SECT-21 p 47 N91- 17834 Onboard Processing arid Switching

INASA-CP-31231 p 14 N92-14070 Proceedings ot the X.15 First Flight 30th Anniversary INASA-CP-31321 p 25 N92-14202

Beyond the Baseline 1991- Proceedings of the Space Celebration NEURAL NETS

Station Evolution Symposium. Volume 2 Space Station (NASA CP-31051 p 10 N91-203071 Proceedrngs of the Seconi Jorint ITechnology Workishop

Freedom, pat Technology 2000, volume 2 on Neural Networks and Fuzzy Logic. rolume* 2

JNASA-CP.10083.VOL-2-PT.11 I P 18 N92-17768 NASA-CP-3109-VOL-21 p 52 N91-24041 I NASA-CP-tOO061-VOIL-21 043 1,91-20811

MIXING LAYERS (FLUIDS) Issues in NASA program and protect management Proceedings ot the Second Joint Technology Workshop

Direct simulation 0f high-speed mixing layers I NASA-SP-6101 104)1 p 46 N91 -28026 on Neural Networks and Fuzzy Logic. voiume I

(NASATP-386) p N923090 NASA patent abstracts bibliography A continuing sAP-otvLIp4 N1278

MODAL RESPONSE bilorpyScin1AsrcsIupeet3)The 1991 Goddard Conference on Space Applications

On-orbit structural dynamic Performxance of a 15-meter I NASA-SP-7039t391- SECT -tI) p 48 N91-28042 of Artrhcial Intelligence

microwave radiometer antenna NASA patent abstracts bibliography A Continuing I NASA-CP-31 101 p 43 N91-22769

* NASA-TP-304t) p 16 N91-171 14 bibliography Section I Abstracts (supplement 40)_ antlrneo ntca er)ntoswt

A controls engineering approach Ior anatyzing airplane INASA-SP- 7039(40)- SECT-lII p 48 N92 22508 Futtlrne~ riiilnuh ewrswt

inpu-ouputchaactrisicsNASA Wallops Flight Facility Air-Sea Interaction apptlications in cinticel syrstems

NASA-TP-30721 p 12 N91-20128 Research Facility IAAr-t7 4 9-28

The efflet of acceleration versus displacement methods INASA-AP-12771 p 36 N92-25981 The 1992 Goddard Contererice on Space Applications

on steady-state boundary forces NASA patent abstracts bibliography A continuing 0f Artfitcial Intelligence

[NASA-TP-32181 p 30 N92-21457 bibliography, Section 2- indexes (supplement 40) fNASA-CP-3t41 p p43 N92-23356

MODELS I NASA-SP- 7039(40)- SECT .21 p 4e N92-27081 NEUTRAL B3UOYANCY SIMULATION

Compansoin of a two-dimensional adaptive-wall Issues in NASA program and project management A method 0f evaluating efficiency duning space-suited

technique with analytical wall interference correction (NASA-SP-6101(05I) p 47 N92-27609 work in a neutral buoyancy environment

techniques NASA Workshop on tuturedinections in surface modeling (NASA-TP-3 1531 p 40 N92- 19772

(NASA-TP-31321 p 7 N92-20494 and grid generation NEUTRONS

MODULATION INASA-CP-100921 p 8 N92-29625 Benchmark solutions for the galactic heavy-ion transport

Advanced Modulation and Coding T Iechnology NASA patent abstracts bibliography A continuing equations with energy and spatial couplin

Conference bibliography. Section 2. Indexes (supplement 4 1) 1 NASA-TP-31 12) p 44 1`92,13756

INASA-CP-100531 p 16 N192-22001 I NASA-SP-7039(41)-SECT-21 p 48 N92-31455 NEWTONIAN FLUIDS

MOLECULAR CLOUDS The development of the NASA aviation safety reporting Lewis icing research tunnel test 01 the aerodynamic

Interstellar Dust. Contributed Papers systemefetofaratgoudelnaiiin lis

I NASA-CP-30361 p48 N91-14897 AINASA-RP-11141 p 10 N91-ý70436 eectSA 01 Tircaf grun de2cingpntiicing 30395

MOMENTS NASA SPACE PROGRAMS NICKEL CADMIUM BATTERIES

Measurements 01 forces, moments, and pressures on Exobiologyr on Mars The 11991 NASA Aerospace Battery Worktshop

a generic store separating from a box cavity at supersonic INASA-CP-10055) p 41 N191-15691 INASA-CP-31401 p 33 N92-22740

speeds Technology tot the Future- In-Space Technology The 1990 NASA Aerospace Battery Workshop

INASA-TP-31 101 PIS 8192-10005 Experiments Program. part I I NASA.CP-31 191 p)20 N92-27130

MOMENTS OF INERTIA I NASA-CP-10073-PT-1 I p 14 N191-27177 NCE YfOE ATRE

Influence of mass moment of inertia on normal modes Technology for the Future: In-Space Technology NIhEL 1991OGNAS BATERosaESBteyWrso

a --reloaded solar array mast Experiments Program, part 2 Te19 AAArsaeBteyWrso

I NASA-TP-32731 p 31 N9:2-33476 tNASA-CP-10073-PT-21 p 14 N91-27178 [NASA-CP-3140) p 33 N192-22740

MOMENTUM TRANSFER First among equals The selection of NASA space The 1990 NASA Aerospace Battery Workshop

Inclusive inelastic scattering 0f heavy ions and nuclear science expenments, I NASA-CP-31 191 p20 N192-27 130

Correlations I NASA-SP-42151 p 52 N191-28060 NIMBUS 7 SATELLITE

[NASA- TP-3026; p 46 N191 -13985 Ongoing Progress in Spacecraft Controls User's guide Nimbus-? Earth radiation budget

MULTIGRID METHODS f NASA-CP- 100991 p 19 N92-28730 ilarrow-tield-ot-view products Scene radiance tape

Workshop on Grid Generation and Related Areas NASTRAN products, Sorting info angular bins products. and maximum

INASA-CP- 100891 p 12 N92-25712 Nineteenth NASTRAN (R) Users'Col[loquium likelihood Cloud estimation products

MULTISENSOR APPLICATIONS J NASA-CP-31 111 p29 N191-20506 INASA-RP-1246I P 34 8191-130.43

Multisource Data Integration in Remote Setsing Twentieth NASTFIAN (R) Users' Colloquium Nimbus-7 TOMS Antarctic ozone atlas AugustI NASA-CP-3099~ Jp32 N191-15615 INASA-CP-31451 p 30 N192-24324 December 1990

MULTI VARIABLE CONTROL NATIONAL AEROSPACE PLANE PROGRAM [ NASA-RP- 12641 p 35 N191.26651

A methodology for computing uncertainty bounds of Numerical studies of convective cooling for a locally NIOBIUM ALLOYS

muttivariable systems based on sector stability theory heated skin Surface effects on hydrogen permeation through

concepts I NASA-TP-31001 p 26 N191-22509 Ti-14AI-2lNb alloy

[NASA TP-3 1661 p 13 N192-21410 NATIONAL AIRSPACE SYSTEM I NASA-TP-3109t p23 8191-202?66

MUSCLES Joint University Program tar Air Transportation NTAE

Eccentric and concentric muscle performance following Research, 1990-1991 Saturation point model for the formation of metal nitrate

7 days 0f Simulated weightlessness JNASA-CP-31311 p 3 N952-17984 in nitrogen testrosicle oxidizer

I NASA-TP-31821 p 39 N192-17645 NAVIER-STOKES EQUATION tNASA-TP,3107I 0)26 N91-24542

MUSCULAR FUNCTfON Naviefr-Stokes and Euler solutions lox lee-side flowsoe NITROGEN

EccentrIc and concentric muscle Performance following suesoi detoigv oreainwt u enrn Calculations and curve fits of thermodynamic and

N AySA, 0 siuae 1 -vergrtl'r30351 p4 N9 1-13401 transport properties lox equilitinum air to 30000 Kt

ttAS-iP-t82 p39 N192-l17645 )NS-P33)INASA-AP-12601 P26 N192-1 1285

MUSCULAR STRENGTH Relative efficiency and accuracy of two Nev~er-Stokes NITROGEN DIOXIDE Thealdaloptahumn ore mde lor~itl dna~c codes tor simulating attached transonic flow over wings SAGE I data user's guide foresaiisuring riomalruma wtorcmoleiopredctyn f NASA-TP 3061 1 p 26 8151 17310 1INASA-RP-t1275) p 34 1492 310T97

iNASA !P.-12G6 1 P 40 N192-26538 An explicit upwind algorithm for solving the parabolized NITROGEN OXIDES

MUSCULOSI(ELETAL SYSTEM Nauier-Stokes equations The atmospheric effects ot stratospheric aircraft A

WorkshpD )nr Fver'ý,iw Prescription lor LongqDuration I NASA- TP-30501 p 4 N191-18032 Current consensus

Spa-e FI'qWi Stagnation-point heat-transler rate predictions at JNASA-RP-i 251 tp 33 8191 16467

iNASA CP '305,1 p 36 N191 1057'4 seroassist flight coriditions NITROGEN TETROXIDE ~nhrie o eemio fnpc ocsrlnn AAT-?8P27 8152 31261 Saltuation point model lox the formation of metal nitrate

siall-uii sait runninq in a zro G environment A nozzle internal perlorman~ri prediction method in nitrogen tetroxide oxidizer

NtASA TP~ll 'JIý1p 18 N192 17022 NASA T P32211 p 8 N92 336f25 )NASA TP-31071 0 26 Ng91 245412

A-23
NOAA 10 SATELLITE SUBJECT INDEX

NOAA 10 SATELLITE A nozzle internal performiance prediction method OPTICAL MEASUREMENT

Mission description and in-f light operations ot EFIBE I NASA-7P-322t I p 8 N92-33625 Optical measurements on solid specimens of Sowlidocket

instruments on ERaS and NOAA 9 spacecraft, November Parametric investigation of sing le-ex pansion-ramp motor exhaust and Solid rocket Motor Slag

1984 ,-January 1986 nozzles at Mach numbers from 0 60 to 1 20 1 NASA-TP-3 t771 p 20 N92 20949

[NASA-RP-12561 p 32 N92-10208 INASA-TP-32401 p 9 N92ý34193 rliree-drmensiornal laser window formation

Mission description and in-flight operations of ERBE NOZZLE GEOMETRY I NASA-RP-12801 p 14 N92 30307

instrumentls on ERBS, NOAA 9, and NOAA 10 Statrc thruaf -vectoring performance of rinaxnsxymmetr.C OPTICAL RADAR

spacecraft conyergent-drvergenf nozzles with post-exit yaw vanes Airborne Wind Shear Detection anid Warning Systems

INASARP-1279j p 32 N92-32127 ]NASA.TP.30851 p5 1,91-21059 Third Combined Manufacturers and Technr-ologists

Misson dAEscLpIonadTE lgtoprtos~EB Aeroviropulsive characteristics of canted twin Conference, pant 2

MinstrumentsonptioS and in-fAAh 9opaecraftion November Pitch-vectoring nozzles at Mach 0 20 to 120 (NASA-CP-10060-PT 21 p 9 N91-24 140

19srum4 t oJnur 1986 an NOA9saerf.Nvme NASA-TP-3060 I p5~ N9 122069 Sivteenth International Laser Radar Conference part

[NASA-RP-t2561 p 32 N92-10208 NOZZLE THRUST COEFFICIENTS I NASA-CP.3158-PT-1I p 28 N92-29228

Mission description and rn-flight operations of ERBE A nozzle internal performance prediction method SivteenthC International Laser Radar Conference. pant

instruments on ERBS, NOAA 9. and NOAA 10 1INASA.TP-32211 p 8 N92-33625 2

spacecraft NUCLEAR ENGINE FOR ROCKET VEHICLES I NASA-CP,3158-PT.21 p 28 N92-31013

I NASA-RP- 12791 p 32 N92-32127 Nuclear Thermal Propulsion A Joint NASA/OOE/DOO OPTICAL TRACKING

NOISE GENERATORS Workishop Proceedings of the 23rd Annual Precise Time and Time

Aeroacoustics of flight vheicles Theory and practice I NASA-CP- 10791 p 20 N92-1 1088 Interval (PTTIf Applications and Planning Meeting

Volume 1: Noise sources NUCLEAR INTERACTIONS (NASA-CP-3t 59i p 44 N92 33350

INASA-RP-1258-VOL-) p p45 N92-10598 Benchmark solutions for the galactic heavy.,on transpoyt OPTIMAL CONTROL

NOISE INTENSITY equations with energy and spatral coupling Fourth NASA Workshoip On Compurational Control or

Fourth International Symposium on Long-Range Sound I NASA-TP.31 112] p 44 N92- 13756 Flexible Aerospace Systems, part 2 Propagation NUCLEAR PROPULSION INS--.06-T2P1 9-23 INASACP-3101 1 p 44 N91-116682 Vision-?t Space Travel for the Next Millennium OPIMIAS TION05P-I r7NP-23 NOISE MEASUREMENT J NASA-CP- 100591 p 13 N191-22139 OTMuts tnr opiizationofcnrie spe Wind turbine acoustics Nuclear Thermal Propulsion. A Joint NASA/DOE/DOD structures With global sensitivity equations

INASA-TP-30571 p44 1,191-16679 Workshop INASA-TP-31301 p 18 N92-11087 Fourth Aircraft Interior Noise Workshop INASA-CP-100791 p 20 N192-11088 Opizaon1cmostsndchCerpel

]NAS-CP10t31 p5 N2-3949 NUCLEAR REACTORS subjected to compressive loadings NOISE POLLUTION Visin-21- Sipace Travel for the Nest Millennium INASA-TP-3173) p 21 N192-20679 The atmospherrc effects of stratospheric aircraft: A first I NASA-CP- 10059) p 13 N91 .22139 ORTCA UL IN program report NUCLECACULTIS

[NASA-AP- 12721 p 3 92-19121 NULOSFlight Mechanics/Estimation Theory Symposium. 1991 NOIE REDCTON 33Radiation protection for human missions to the Moon I NASA-CP-31231 p 14 N192- 14070 NOISEPREDITIONand Mars Aeroacouslics of flight veh;cles Theory and practice. I NASA-TP-30791 p 50 N191-1 7999 ORBIT DECAY

Volume 2: Noise control Flight Mechanics IEstimation Theory Symposium 1991

[NASA-RP-1258-VOL-21 p 45 N92-14779 HZETAN: A heavy ion/nucleon transport Code for Space (NASA-P-31231 p 14 N192- 14070

Fourth Aircraft Interior Noise Workshop radiationsORITANFRVHCE

[NAS-CP10101 p45 N2-3948 1 NAA.T-3141 p51 N2-1959 Hypervelocity, atmospheric flight Real gas flow fields

NOISE PROPAGATION NUMERICAL ANALYSIS INASA-RP-12491 p26 5191-20418)

Aeroacoustics of flight vehicles. Theory and practice Shock wave interaction with an abrupt area change Launch vericle integration options for a large Earth

Volume 2: Noise control I NASA-TP-31 131 p 6 N191-27 140 sciences geosrationary platform concept

[NASA-RP-1258.VOL.21 p 45 N92-14779 Computational Fluid Dynamics -- numerencal methods I NASA-TP-30831 p 15 5191-27180

NOIS REDUCTION and algorithm development Simulation of real-gas effects on pressure distributions Aeroacoustics of flight vehicles: Theory and practice. INASA-CP-1 00781 p 12 N92-25808 for aeroessit r fight experiment vehicle and comparison

Volume 1: Noise sources NUMERICAL CONTROL with prediction

INASA-RP- I258-VOL-l I Ip 45 N92-10598 A generalized metlhod for nnaltrtle robmtc mani1putlaor INASA-TP-3157I p 2

7 N92 206777 Aeroitcoustics of flight vehicles: Theory and practice programming applied to vertical-up welding ORBITAL ASSEMBLY Volume 2: Noise control INASA-TP-31631 Ill24 N92.112t8 Launch vehicle integration options for a large Earth [NASA-RP-1258-VOL-21 p 45 N192-14779 NUMERICAL STABI1LITY sciences geostationary platform c-ocept Fourth Aircraft Interior Noise Workshop Identification of linear systems by an asympfotically I NASA-TP30831 p 15 N91-27180 fNASA-CP-10103J p 45 N92-32948 stable observer Pcaig eeomnadoobrasml pin

NONADIABATIC CONDITIONS I NASA-TP-31641 p 31 N92-26537 forclarige g eeotlonrspaecr.afto~rf ssml pin

Logiudnl erdyaicchratnsic o sbsni. NUMERICAL WEATHER FORESCASTING I NASA-TP-30881 p 17 N191 27182 energy-efficient transport configuration in the National NASA/MSFC FY90 Global Scale AtmosphenrAimco n Pblc o pceOsdSses Transonic Facility Processes Research Program RevrewAuoainndP tlsfrSceBedytm,

(NASA-TP-2922J p8 6N91-28143 [ NASACP-30931 p 35 N91-16500 1991

NONDESTRUCTIVE TESTS NUTRITIONAL REOUIREMENTS DeveloCpment9 of3 aNrus9ontr,2obtc7s6mly0

Second Conference on NOE for Aerospace Nutritional Reqtuirements for Space Station Freedom spaceslopmetures rusjit oobtcasebyo

Requirements crews saesrcue

[NASA-CP-30911 p 16 N9t-f8189 INASA-CP-3161 40 5192-25961 I NASA-TP-321A I p 31 N192-27974

The 1991 International Conference on Aging Aircraft and 1)-Software design for automated assembly of truss

Structur~al Airworthiness structures

INASA-CP-3160) p 31 N92-30106 [NASA-TP-31961 p43 N192-28375

NONEQUILIBRIUM THERMODYNAMICS 0ORBITAL LIFETIME

Aeroacoustic and aerodynamicaplctosoththoyLn-emobalifieprdtos

of nonequililbrium throy appicaton ofteter RING SEALS Ln-emobtllftm rdcin

I NASA-TP-31 IS] p 26 N191-25352 Asisymmetric shell analysis of the space shuttle solid INASA-TP-303581 P 13 N91 10092

NONLINEAR SYSTEMS rocket booster field loint ORBITAL MANEUVERS

Application and flight test of linearizing transformations [NASA-TP-30331 p28 N,91-14618 Manual Control Aspects of Orbital Flight

using measurement feedback to the nonlinear control Effect of ter.pierature and gap opening rsle on the INASA-CP-100561 p 13 N191-201,67

problem resiliency of candidate solid rocker booster 0-nng OSCILLATIONS

(NASA-TP-31541 p 12 N9t-30154 rnatenials Inertial oscillation of a vertical rotating draft with

A nonlinear estimator for reconstructing the angular [NASA-TP-32261 p 23 N92-27194 application to a supercelt tirorm

velocity of a spacecraft without rate gyros OCEAN SURFACE I NASA-TP-3230i p 36 N192-33482

INASA-TP-3t781 p 24 N92,13,343 A self-zeroing capacitance probe for waler wave Inerfial oscillation of a vertical rotating draft with

NONLINEARITY measurements application to a supercell storm Video supplementh tor

A weakly nonlinear theory for wave-vortex Interactions INASA.RP-t 278] p 36 N92-27930 NASA Technical Paper 3230

in curved channel flow ONBOARD DATA PROCESSING I NASA- TP. 3230-VIDEO-SUPPL I p 36 N92 34246

t NASA -TP-31561 p 7 N192-19175 Space Communications Technology Conference OUTGASSING

NOZZLE DESIGN Onboard Processing and Switching Oulgassing data for selecting spacecraft materials

A no7'le internal performance preoiction method I NASA-CP.3 1321 p 25 N192-14202 revision 2

(NASA-TP-32211 p 8 N92-33625 OPERATIONS RESEARCH (NASA-RP-1 124-REV-21 p2l N191-14437

Parametric investigation of Single -espansion -ramp Fourth Annual Workshop on Space Operations OXIDATION

nozzles at Mach numbers from 0860 to1020 Applications and Research (SOAR 90) Oxidation characteristics of Tr-25AI I ONb.3V IlMo

INASA-TP-32401 pg 5N92-34193 I NASA-CP-3103-VOL-tI I p 41 N91-20641 intermetallic alloy

NOZZLE EFFICIENCY OPERATORS (PERSONNEL) I NASA TP-30441 op22 N191-13S2,'

A nozzle internal performance prediction method Human Machine Interfaces for Teleoperalors and Virtual Fourth Annual Workshop on Space Ophiatrons

INASA-TP-32211 p p8 N92-33625 Environments Conference Applications and Research ISOAR 901,

NOZZLE FLOW I NASA -CP. 100711 p 40 N92 11638 1 NASA-CP.3t03-VOI-.21 pa 41N91 20702

A parametric experimental ivsgaonof a scramletl OPTICAL ACTIVITY OXIDES

nozzle at Mach 6 with Freon and argon or air used for Positron lifetime measurements in chiral nematic liquid AMSAHTS 1990 Advances in Materals Science an~d

exhaust simulation crystals Applications of High Temperature Superconductors

I NASA-TP-30481 p 4 5191-16990 tNASA-TP-31221 p 46 N92-10677 I NASA.CP-3 1001 p 22 510? 2160)5

A-24
SUBJEC r NDEX POINTING CONTROL SYSTEMS

OXIDIZERS PATENT POLICY PHASE SHIFT KEYING Saturation point model tar the lormiation of metal nitrate NASA patent abstracts bibliography A continuing Advanced Modulation and Coding Tecrinology

in nitrogen tetroxide oxidizer bibliography. Section 1: Abstracts (supplement 38) Conference

INASA-TP-31071 p 26 N91-24542 (NASA-SP-7039(38)-SECT- Ij p 47 N91-17833 I NASA-CP- 100531 p 16 N92-22001 OXYGEN NASA patent abstracts bibliography. A continuing PHOTOVOLTAIC CELLS

Calculations and curve fits of thermodynamic and bibliography Section? 2:Indexest (supplement 38) Space Phtioovoltaic Research and Technology. 1989

transport properties for equilibrium air to 30000 K I NASA-SP-7039(38)-SECT-21 p47 N91-17034 I NASA.CP-3107 j p 19 NOt-19182

INASA-RP-12601 p 26 N92-11285 NASA patent abstracts bibliography, A continuing PHOTDVOLTA- CONVERSION

OXYGENATION bibliography Section 1 Abstracts (supplement 39) Space Photovoltaic Research and Technology. 1989

Electrochemical studies of corrosion inhibitors I NASA-SP-7039(3g)-SECT-t I p48 N91-280-42 JNASA-CP-31071 p 19 N91,19182

INASA-TP-30661 P 22 N91-17208 NASA patent abstracts bibliography A continuing Space Photovoltaic Research and Technology OZONE iblography. Section I : Abstracts (Supplement 40) conterence OZOE atIphn efcsostaopeiarrftA NASASP- 7039(40).SECT.tI p 48 N92-22W0 [ NASA-CP-3121 I p 19 N91-30203 Topicalmshei review trtspei arrat NASA patent abstracts bibliography. A continuing PHYSICAL EXERCISE toicalAR-20 p33eview4 bibliography. Section 2 Indexes (supplement 41) Workshop on Exercise Prescription far Long-Duration TheARP120 atopei effct staopei N9o146 aicat NASA-SP-7039(4i)-SECT-2j p 48 N92-31455 Space Flight Th topei fet fsrtshrcarrf:A PATENTS I NASA-CP-3051 I p36 N91-t 0574 currant consensus NASA patent abstracts bibliography: A continuing Responses of woman to orihostatic and exercise INASA-RP-1251 J p33 N91-16467 bibliography, Section 2: Indeses (supplement 39) stresses

Nimbus*7 TOMS Antarctic ozone atlias: August )NASA-SP-7039139)-SECT-21 p 48 N91-29088 INASA-TP-30431 p 37 91-19711 December 1990 NASA patentf abstracts bibliography. A continuing Fuet utilization during exercise after %a st bed rest INASA-AP-1264) p 35 N91-26651 bibliography. Section 2: Indeses (supplament 40) [NASA-TP-31 75) p 38 N92,16554 Sixteenth International Laser Radar Conference, part I NASA-SP17039(40)-SECT-2J p 48 N92-27081 A method of evaluating efficiency during space-suited 2 PATT'ERN4 RECOGNITION work in a neutral buoyancy envionment

I NASA.CP-3158-PT-21 p 28 N92-31013 Proceedings of the Second Joint Technology Workshop INASA-TP-31 531 p 40 N92-19772

SAGE I data user's guide on Neural Networks and Fuzzy Logic, volume 2 PHYSICAL FITNESS

(NASA-RP-12751 p 34 N92-33097 [NASA-CP.10061-VOL-21 p 43 N91-20811 Foel utilization during exercise after 7 days of bed rest OZONE DEPLETION PAYLOAD INTEGRATION INASA.TP.31751 p 38 N92-16554

Nirnbus-7 TOMS Antarctic ozone atlas: August - Launch vehicle integration options for a large Earth PHYSICS

December 1990 sciences geostationary platform concept Aeronautical engineening. A continuing biblioglraphy with

I NASA-RP-1264) p 35 N91-26651 )NASA-TP-30831 p 15 N91-27180 indexes (supplement 275)

The atmospheric affects of stratospheric aircraft: A first Packaging, development, and On-orbit assembly options I NASA-SP-7037(275)1 p 3 N92-28679

program report for large geocstationary spacecraft PHYSIOLOGICAL EFFECTS

I NASA-RP.1272) p 33 N92-19121 I NASA-TP-30881 p 17 N91-27182 Radiation niski predictions for Space Station Freedom

PAYLOADS Orbits

Metallized propellants for the human exploration of I NASA-TP-30981 p 51 N91-26107 P Mars PHYSIOLOGY

f NASA-TP-3062J p19 N91-t 1800 Responses of women to orthostatic and exercise

PACKET SWITCHING Lunar missions using chemical propulsion: System stresses

Destinatin-dirrected. packet-switching architecture for desigrn issues I NASA-TP-3043j p 37 N91-19711

30/20-GHz FOMA/TDM geostationary communications )NASA-TP-30651 p 19 N91-15308 PILOT PERFORMANCE

satellite network Payload bay doors and radiator panels famirliarization Flight characteristics of a modified Schrweizer 5SfS -36

[NASA-TP.32011 p 16 N92-1 5762 handbook sailplane at low and very high angles of attack

PALEOMAGNETISM I NASA-TM-1077931 p 15 N92-20676 (NASA.TP.30221 p 12 N91-10079

Steady induction effects in geomnagnetism. Part 1A- Definition and design of an experiment to test raster Effect of short-farm exposure to stereoscopic Steady motional induction of geomagnetic chaos scanning with rotating unbalanced-mass devices on three-dimensional flight displays on real-world depth jNASAj-TP3272.PT-tA) p 34 N92-32655 gimbaled payloads perception PANEL METHOD (FLUID DYNAMICS) INASA-TP-32491 p 24 N92-29677 [ NASA-TP-31 171 p 1t N92-13065

Prediction of effects of wing contour modifications on PEEK PIPES (TUBES) low-speed maximum lift and transoric performance for the Investigation of microstructural changes in Eftect of type of load on stress analysis of Itin-walled

EA-68 aircraft pofyatherether-ketone films at cryogenic temperatures by ducts

I NASA-TP-30461 p 4 N91-10902 positron lifetime spectroscopy [NASA-TP-32481 p 31 P92-26689

Panel methods: An introduction [ NASA-TP-3064 ] p 21 N91-182l6 PITCHING MOMENTS

INASA-TP-29951 p 5 N91 -19058 PERFORMANCE PREDICTION A nozzle internal performance prediction method

PANELS Long-term orbital lifetime predictions [NASA.TP-322t) p 8 N92-33625

Payload bay doors and radiator panels familiarization (NASA-TP.30581 p 13 N91-10092 PLANE STRAIN

handbook Prediction of effects Of wing contour modlifications, on Applications of FEM and SEM in two-dimensional

I NASA-TM-107793 j p 15 N92-20676 low-speed maximum lift and transonic performance for the fracture mechanics Problems

PARABOLIC DIFFERENTIAL EOUATIONS EA-68 aircraft [NASA-TP-32771 p 31 N92-31280

An explicit upwind algorithm for solving the parabolized tNASA.TP.30461 p 4 N91-10902 PLANETARY GEOLOGY

Navier-Stokes equations Shortcomings in ground testing, environment Planetary geosciences. 1989-1990

INASA-TP-3050) p 4 N91-18032 simulations, and performance predictions for space I NASA-SP-5081 p 50 N92-48345 PARALLEL PROCESSING (COMPUTERS) applications PLANFORMS

Advanced techniques in reliability model representation I NASA-TP-32171 p 23 N92-22593 Plantorm curvature effects on flutter characteristics of and solution Wind tunnel aerodynamic charactenistics of a a wing with 56 deg leading-edge Sweep and panel aspect 1 NASA.TP-32421 p 43 N92-33483 transport-type airfoil in a simulated heavy rain ratio oft1 14

PARAMETER IDENTIFICATION environment INASA.TP-31 16) p 11 N92-13054

Flight characteristics of a modified Schweizer SGSI-36 INASA-TP-31841 p 8 N92-31532 PLASMA ARC WELDING

sailplane al low and very high angles Of attack A nozzle internal performance prediction method A generalized method for multiple robotic manipulator

[NASA-TP-30221 p 12 N91-10079 (NASA-TP-3221 p p8 N92-33625 programrming applied to vertical-up welding

PARAME7ERIZATIOS4 PERFORMANCE TESTS I NASA-TP-31631 p 24 N92-t11218

FIRE Science Results 1988 Fault tolerance of artificial neural networks with PLASMA PHYSICS

I NASA-CP-30831 p 34 N91-10448 applications in critical systems Current Collection from Space Plasmnas Parame'iic study of afferbody/nozzle drag on twin I NASA-TP-3t871 p 42 N92-22285 I NASA-CP-3l89 J p 46 N91-17713

two-dimensional convergerlf-divergent nozzles at Mach Static performance of a crucilfom nozzle with multiaxis PLASMA PROBES

numbers from 0 80 to 1 20 thrust-vectoring and reverse-thrust capabilities Current Collection from Space Plasmas

JNASA-TP-26401 p4 Ngt-14316 INASA-TP-31881 p 7 N92-23095 NASA-CP-30091 p 46 N91-17713 PARTICLE INTERACTIONS PERMANENT MAGNETS PLASMA PROPULSION

HZETRN A heavy ion/nucleon transport code for space The 23 to 300 C demagnetization resistance of Magnetoplasmedynamnic Thruster Workshop

rNadia-tions 65 N9.15 samarum-cobalt permanent magnets INASA-CP-100841 p 201 N92-10044

PNARATICLE MO5 4 N2t19N INmASA-TP-31 191 p25 N92-1 1252 PLATES (STRUCTURAL MEMBERS) PAnaILysi ogrvt-nuepaileMOTIONanfli An examination of the damage tolerance enhancement Aayiofgaiyidcdprilmoinadfud PERMEABILITY ot carbon/epoxy using an outer lamine of spectra (RI pefso in te lw NS-eige oaig An investigation of microstructural Characteristics Of (NASA-TP-3 i601 p 2t N92-1l 142

zero-head-space tissue culture vessel cnatln oyesPUE

I NAA-T-3131 p24 92-334 (NAA-T-3041 pl N1-1492 Comparison of let plume shape predictions and plume

PARTICLE SIZE DISTRIBUTION Surface effects on hydrogen permeation through influence on sonic boom signature

Volcanism-Climate interactions Ti-1 4A1-2l1Nb alloy I NASA-TP-31 721 p 7 N92-ZS1 33

I NASA.CP-100621 p 34 N91-21641 INASA-TP-31091 p 23 N91-20266 POINCA.RE PROBLEM PATENT APPLICATIONS PERMEATING Workshop on Squeezed States and Uncertainly

NASA patent abstracts bibliography A continuing Surface effects on hydrogen permeation through Relations

bibliography Section?2 Indexes IsucPplement 39t Ti-14AI-2lNb alloy INASA-CP-31351 p 46 N92-22045 I NASA SP 7039f3g1.SECT.2 I p 48 N91 -29088 I NASA-TP-3i09 I p 23 N91 -20266 POINTING CONTROL SYSTEMS

NASA. patent abstracts bibliography A continuing PERSONNEL Thermal-distortion analysis Of a spacecraft box truss in

bibliography Section 2 Indexes (supplement 40) NASA engineers and the age of Apollo geoslationary orbit

INASA SP.7019(40)-SECT.21 p 4

8 N92 27081 1INASA-SP-41041 p 52 N92-2834l4 INASA.TP-305-41 p 18 N91-1 1041

A-25
POLAR METEOROLOGY SUBJECT INDEX

Aerospace Applications of magnetic Suspension PRESSURE DEPENDENCE PROPELLERS

Technology, part 2 Gibbs free energy of reactions involving S#C. Si3N4. H2. Structural properties of lamirnated Douglas firtapoxy

LNASA-CPD-i006&-PT-21 p 17 N491-21203 and H20 as a function of temperature and pressure composite Malaonal

Rigid-body-control subsystem sizing for an Earth science I NASA-TP-32751j p 23 N92-3 1278 (NASA-RP- 12361 p20 N91-110127

geostationary platform PRESSURE DISTRIBUTION Annoyance caused by advanced turboprop aircraft

INASA-TP-30871 p 17 N91,22302 Reflative efficiency and accuracy of two Navief-Stokes 1lyover noise Compareson of different propellef POLAR METEOROLOGY codes for Simulating attached transonic flow over wings configurations

SAM 2 measurements of the polar stratospheric aerosol JNASA-TP-30611 p 26 N91-1 7310 I NASA-TP.31041 p 45 N92- 11758

Volume 9- October 1982 -April 1983 Effects of yaw angle and Reynolds number on PROPULSION

1NASA-RP-12441 p 33 N91-185035 rectangular-box cavities at subsonic and lransonic Space Transportation Propulsion Technology

International Workishop on Stratospheric Aerosols: sed Symposium Volume I Executive summary

Measuremenfta. Properties, and Effects INASA-TP-30991 p 5 N91-27124 I NASA-CP-3t 121 p 19 N91-25 176

[NASA-CP-3tt41 p 32 N91-32528 Transonic and supersonic Euler computations of Large space structures and systemsin the space Station

POLICIES vortex-dominated flow fields about a generic fighter era A bibliography with indexes (supplement 03)

Proceedings of the Second Annual NASA Science INASAýTP-3156 p 6 N92- 10011 INASA-SP-7085(031 p p18 N92-22317

Internal User Working Group Conference Simulat ion of real-gas effects on pressure disriuon Workshop on Engineering Turbulence Modeling

[NASA-CP-3t11?) p 48 N91-27009 aeositfih xetn eil n oprislons I NASA-CP-100881 P 27 N92-24514

POLYETHYLENES for arassflgteprmnveiladco aionDEF 69 Months in Space First Posi-Retrieval

An examination of the damage tolerance enhancement I NASA-TP-3157j ~ 27 N92-20677 NSym Cposium, par 32N2-76 Tofcrolpx sn notrlemina of spectra tR PRESSURE MEASUREMENT INS-P3 4P-lp5 9-76 of carbon/eporrp usin oute2 N9n PROPULSION SYSTEM CONFIGURATIONS (NAS.TP3t6I p1 N2-1t42 Measurements of torces, moments, and pressures on Lunar missions using chemical propulsion System

TwLYO-dmNSioa eoyai hrc rsso eea a generic store separating from a box cavity at supersonic design issues Twhewa eoyaihrceitc fsvrl spewds I NASA-TP.-30651 p 19 N9 1-15306 polygon-shaped cross-sectional models applicable to I NASA-TPý31101 p 6 N92-10005 Parametri trade studies on a Shuttle 2 launch system helicopter fuselages NACA 0015 wing pressure and trailing vortex architecture [NASA-TP-3233] p 8 N92-30394 measurements I NASA-TP-30591 p 14 N91-18180

POLYMER MATRIX COMPOSITES I NASA-TP-31 511 p 6 N92-10981 Aeropropulsion 1991 NASA workshop on impact damage to composites PRESSURE OSCILLATIONS I NASA-CP-1I00631 p 12 N91.20086 INASA-CP-ID0751 p 21 N91-29240 Flow-induced resonance of screen-covered cavities Structural Integrity and Durability 01 Reusable Space

POROSITY [NASA-TP-30521 p 25 N91I-1 5499 Propulsion Systems

Experimental investigation of porous-floor effects on PROBABILITY THEORY I NASA-CP- 100301 p 19 N91-.24307

cavity flow fields al supersonic speeds Strutural deterministic Safety factors selection criteria Space Transportation Propulsion Tecinoloy

( NASA-TP-30321 p 5 N91-19042 and venification Symposium Volume 1 Executive summary

POSITRON ANNIHILATION I NASA-TP-32031 p30 N92-19355 INASA-CP.31 121 p 19 N91-25176

Investigat ion of microstructural changes in PROCESS CONTROL (INDUSTRY) Space Transportation Propulsion Technology

polyefherether-kertone films at cryogenic temperatures by The Federal Conference on Intelligent Processing Symposium, Volume 2 Symposium Proceedings

positron lifetime spectroscopy Equiment I NASA-CP-3112-VOL-2) p 19 N91-28193

INASA-TP-3064 ] p 2

1 N91-18216 I NASA-CP-31381 p 52 N92-24987 Space Transportation Propulsion Technology

Low-energy position flux generator for microstructural PRCODUCT DEVELOPMENT Symposium Volume 3- Panel Session Summanies and

charactenriation of thin films ecnlg200voue2Presentations

INS-P374 2 9-22538 (NASA-CP-3t09-VOL-21 p 52 N91-24041 [NASA-CP-3112-VOL-31 p 19 N91 29235

Positron lifetime measurements in chiral inrtiesaic liquid PROJECT MANAGEMENT Static internal performance of ventral and rear nozzle

crystals NAAconcepts for short-takeoff and vertical-landing aircraft

INASATP-31221 p46 N92-10677 TwentySeon Annual NAASup~py and Equipment I NASA-TP-31031 p 6 N92-10975

POSITRONS, Management Conference Nuclear Thermal Propulsion A Joint NASA/DOE/DOD

Positron lifetime measurements in chiral nemati liquid [NASA-CP-100A21 p 46 N91 -1 1591 Workshop

crystals Issues in NASA program and project management 1NASA-CP-i00791 p20 N92-11088

INASA-TP-31221 p 4 6 N92-10677 [NASA-SP-6101(03)1 p 46 N91-13347 Aerapropulsion 1967

POSTFLIGHT ANALYSIS Issues in NASA program and project management [NASA-CP-3G491 p 12 N92-22510

State estimation applications in aircraft ffighl-t-dta I NASA.SP-6101(OAII pi46 11,91-28026 Computational Structures Technology for Airframes and

analysis: A user's manual for SMACK Nuclear Thermal Propulsion A Joint NASA/DOE/DOD Propulsion Systems

INASA-RP-12521 prO0 N91-19082 Workshop fNASA-CP-31421 p 31 N92-25911

LOEFi 69 Months in Space First Post-Relneval J NASA-CP- 100791 p 20 N92-1 1068 Supersonic Througtrllow rarn Text Facility at NASA

Symposium, part 1 Issues in NASA program and project management Lewis Research Center

I NASA-CP-3134-PT-t I p 52 N92-23280 P.1NASA-SP-6101(05)I p 47 N92-27609 (NASA TP 3036) p 13 N92-31640

POTE4TIAL Space Travel forLANNxtNileniu Tenth workshop for Computational Fluid Dynamic

Panel methods: An introduction NAsAo-CP100Spacp frteNxMilnnium 13ve 13 Applications in Rocket Propulsion, part?2

INAS-TP2991 p N9-1958 NASACP.1009 tp 13N9`-2239 NASA-CP-3163-PT-21 p 17 N92-32245

POWRALSS-P2g1p 9-95 Nuclear Thermal Propulsion. A Joint NASA/DOE/DOD PROPULSION SYSTEM PERFORMANCE POWERLOSSWorkshop

Experimental and analytical evaluation of efficiency of INASA-CP-i0079I p20 N'921 188 Lunar missions using chemical propulsi~ri System

helicopter planetary stage Beyond the Baseline 1991. Proceedings of the Space design issues

INASA-TP-30631 p28 N91 12956 Station Evolution Symposium Volume 2: Space Station N AT-351p1 Nf1130

PRECIPITATION (METEOROLOGY) Freedom. part 2 Computationial Fluid Dynamics Symposium on

The role of water vapor in climate. A strategic research I NASA-CP-10083-VOL 2-PT-21 p 18 N92-17348 Aeropropulsion

plan for the proposed GEWEX water vapor project Beyond the Baseline 1991. Proceedings of the Space INASA-CP-30781 p 5 N91.21062

IGVapI Station Evolution Symposium Volume 2 Space Station Space Transportation Propulsion technology

(NASA-GP-31201 p35 N911-25556 Freedom. part t Symposium Volume?2 Symposium proceedings

PREDICTION ANALYSIS TECHNIGUES (NASA-CP-10083-VOL.2-PT-1 I p 16 N92-17768 I NASA -CP-311t2.VOL-21 p 19 N91.28193

Wind turbine acoustics PROP-FAN TECHNOLOGY Nuclear Thermal Propulsion A Joint NASA IDOE iDOD)

INASA-TP-3057) p 44 N91-16679 Annoyance caused by aircraft en route noise Workshop

West Antarctic ice Sheet initiative Volume 1 Science NASA-TP-316S] p 4

5 N92-20479 INASA-GP.10079i p 20 N92 t 1088

and Implementation Plan PROPELLANT ADDITIVES Aeropropulsion 1987

1 NASA-CP-31 I5-VOL~- I p32 N91-20541 Lunar missions using chemical propulsion System [NASA-CP-30491 p 12 N92 22510O

Structural Integrity and Durability of Reusable Space design issues Supersonic Througritlow Van Test Facilty at NASA

Propulsion Systems [NASA-TP-30651 p 19 49 1-15308 Lewrs Research Center

I NASA-CP- 100301 p 19 N91424307 Upper stages using liquid propulsion and metallized INASA-TP-30381 p 13 N92 3111AO

Modeling of the heat transfer in bypass transitional propellants Prmti netgto fsnl xaso an

boundary-layer flows INASA-TP-31911 p 20 N92-17f51 Parlesamtriach invmertiton 016 tigeeo 1 20 ~ am

1NASA-TP-31 70) p 27 N92-1 1299 PROPELLANT COMBUSTION Ioze NA A-TP-20 Mac n9br o9206304192

Correlation and predictior of dynamic human isolated Tenth Workshop for Computational Fluid Dynamic PR ULIEFICNC

Applications in Rocket Propulsion, part IPR ULIEFICNY joint fitrengir, from leen body mass (NASA-CP-3163-PT-1 I p 27 N92-27 Aerooropulsive characteirlics of canted tw-n

I NASA-TP-32071 p 41' N92-26682 PROPELLER BLADES 2378 pItch-vectoring nozzles at Mach 0 20 to 1 20

PREDICTIONS Acoustic and aerodynamic study of a pusher-propeller I NASA TP-30601 p 5 Nql -.22069C

Comnpanison of jet plume Shape predictions and plume aircraft model PROSTHETIC DEVICES

'intluence on sonic boom signature INASA-TP.30401 p 45 N91-2t1828 Cable compliance

I NASA-TP 31721 p 7 1492-25133 PROPELLER NOISE I NASA-TnP 32161 0 24 N92 303781

PREMIXED FLAMES Acoustic and aerodynamic study of a pusher -propeller PROTEINS

Two-dimensional stability of laminar ilames aircraft model Fuel utilization during nmiri~sr afteir 7 day,; of bpo pen?

INASA-TP-3t311 p 7 N92-17t111 I NASA-TP.30401 p 45 N91 211128 1 NASA TP 31751 p 311 N51? iriuiS4

PRESSES Annoyance caisped by advanced turboprop aircraft PROTON IRRADIATION

A statistical comparison of two carbon liber/epoxy flyover noise Comparison of differentl propeler Space Photosolta~c Peiitarch and rxi,h~o1ioQ

fabrication techniques contigurations Confeeirncr

I NASA-TP 1-791 p 22 N492-20950 I NASA-T P 3104tl p 45 N49? 1158 [NASA C-P 3121, p P 1 N-i'10 .;0' 1

A-26
SUBJECTINOEX REFLECTOR ANTENNAS

PSYCI40ACOUSTICS LOEF, 69 Months in Space First Post-Retneval Wind tunnel aerodynamic characteristics of a

Annoyance caused by advanced turboprop aircraft Symposium, part 2 tfanspoit-type airfoi in a Simulated hieavy rain

flyover noise: Comparison of different propeller (NASA-CP-3t34-PT-21 p 52 N92-24806 environment

configurations Second LDEF Post-Retrieval Symposium abstracts I NASA TP-31841 p 8 N92-31 532

(NASA-TP-31041 p 45 N92-11758 INASA-CP-100971 p 52 N92-272ili RASTER SCANNING

PULSE COMMUNICATION RADIATION HAZARDS Definition and design of an experiment to rest raster

Flight deck benefits af integrated data link Radiation risk predictions for Space Station Freedom Scanning with rotating uncalaic ed -mass devices on communication orbits gimbiater payloads

INASA.TP.32t91 p 10 N92-2t459 (NASA-TP-30981 p51 N91-26107 I NASA-TP-32491 p 24 N92,29677

The effects of video compression on acceptability of Analyses of risks associated with radiation exposure REACTING FLOW

images for monitoring life sciences 3xpertments from past major solar particle events Stagnation-point heat-transter rate predictions at

I NASA -TP-32391 p 16 N92-33933 INASA.TP-31371 p50 N91-31061 aferoassist flight conditions

PUMP SEALS RADIATION PROTECTION INASA-TP-32GBI p 27 N92 31281

Seats Flow Code Development Cellular track modet of biological damage to mammalian REACTION KINETICS

JNASA-CP-100701 p 15 N92-t 5082 Cell I NASA-TP-30551 cultures fronm galactic cosmic rays p 50 N91-t6981 Oiaincaatrsiso Oiaincaatrsiso ,5I i2A-Ob3-~ ~-1ýIM

Radiation protection tor human missions to the Moon inteninetallic alloy

and Mars INASA-TP-30441 p 22 N91-13522

INASA-TP-3079]J p 50 N91-17999 AMSAHTS 1990 Advances in Materials Science and

QULIYCOTRLTransport methods and interactions for space Applications ot High Temperature Superconductors

QUALITY COTRLh-rtclDgtlSsesThnoy a radiations (NASA-CP-31001 p 22 N92-21605

WorsAhoap FihCrtclDgtlSsesTcnly NASA.RP-12571 p 5t N92-15956 An analysis of combustion studies in shock expansion

(NASA-CP-100281 piti N9t-24200 RADIATION SHIELDING tunnels and reflected shock tunnels

QUANTUM MECHANICS Radiation protection for human missions to the Moon INASATP-32241 p 22 N92-28374

Wrso onSuee SttsadUcrany and Mars REACTION TIME

Weatorkshpo SueedSae an Uneait (NASA TP-30791 p50 N91-1 7999 Reliabitity of a Shuttle reaction timer

I NASA-CP-31 351 p 46 N92-22045 improvements in computational accuracy at BRYNTRN INASA-TP-3t 761 p 40 N92-16562

QUANTUM OPTICS fa baryon transport code) REACTION WHEELS

Workshop on Squeezed States and Uncertainty [NASA-TP-30931 p p51 N91 -23017 Rigid-body-control subsystem sizing for an Earth science

Relations Analyses of risks associated with radiation exposure geostationary platform

I NASA-CP-3 1351 p 46 N92-22045 tram past major sotar particle events I NASA-TP-30871 p 17 N9 122302

QUANTUM THEORY [NASA-TP-31t371 p 50 N91t-31061 REACTOR DESIGN

Workshop on Squeezed States and Uncertainty Benchmark solutions for the gatactic heavy-ion transport Vision-2 I Space Travel for the Next Millennium

Relations equations with energy and spatial coupting INASA-CP-100591 p 13 N91-22139

INS-P331p 46 N92-22045 [NASA-TP-31121 p 44 N92-13756 Nuclear Thermral Propulsion A Joint NASA /DOE /DOD I NSA-P-335 f-ZETRN: A heavy ron/nucleton transport code f or space Workshop

radiations [NASA-CP-100791 p 20 N92-1 1088 R INASA-TP-31461 p 5t N92-15959 REACTOR TECHNOLOGY An efficient HZETFIN (a galactic cosmic ray transport Vision-21.ý Space Travel for the Nest Millennium RADAR DETECTION code) IAAC-051p1 9-23 Airborne Wind Shear Detection and Warning Systems: INASA-TP-31471 p St N92-22218 [N A-P059p1 Nt-23

Third Combined Manufacturers' and Technologists' RADIATION TOLERANCE Nuclear Thermal Propulsion A Joint NASA/DOE/DOD

Conference. part 2 MIRACAL: A rirission radiation catcutation program for Workshop

INASA-CP-t0060-PT-21 p 9 N91-24140 analysis of tunar and interplanetary missions [NASA-CP-100791 t20 Ng?-t 11088

RADAR MEASUREMENT INASA-TP-32111I p 5t N92-25t00 REAL GASES

Sixteenth International Laser Radar Conference, part RADIATION TRANSPORT Hypervelocity atmospheric flight Real gas flow fields

1 Improvements in computational accuracy of BRYNTRN INASA-RP- t2491 p26 N9 1-20418

(NASA-CP-31 58-PT-I I p 28 "492-29228 (a baryon transport code) Simulation of real-gas effects on pressure distributions

RADIATION COUNTERS INASA-TP.30931 p 51 N91-23017 for aefroessist flight experiment vehicle and companison

Improvenients in computational accuracy of BRYNTRIN RADIATIVE HEAT TRANSFER with prediction

Is baryon transport code) Stagnation-point heat-transfer rate predictions at INASA-TP-31571 p 27 N92-20677

I NASA-TP-30931I p 51 N91t-2301t7 aeroassist flight conditions Computational Fluid Dynamics --- numerical methods

Development of the Burst and Transient Source I NASA-TP-32081I p 27 N92-3128t and algorithm development

Experiment (BATSE) RADIO ASTRONOMY INASA-CP-t00781 p 12 N92-25808

INASA-RP-12681 p 49 N91-32006 The Interstellar Medium in External Galaxies. Suimmanies REAL TIME OPERATION

RADIATION DAMAGE of contributed Papers Fautt tolerance of artificial neural networks with

Cellular track model of bilogical damage to mammalian f NASA.CP-30841 p 49 N91-14100 applications in critical systems

cell cultures from galactic cosmic rays Paired and Interacting Galaxies international [NASA-TP-3t871 p 42 N92-22285

INASA-TP-30551 p50 1,91-16981 Astronomical Union Coltoqurlum, No. 124 REESREATHING

Space Photovoltaic Research and Technol:)gy I NASA-CP-30961 p 49 N91-16858 Evaluation of noninvasive cardiac output methods during Conference RADIO EMISSION exercise

I NASA-CP-3121 It p19 N91-30203 The Interstellar Mediuimi External Galaxies. Summaries INASA-TP-3t74I p 38 N92-16553

Multiple lesion track structure model of contributed papers REDUCED GRAVITY

I NASA.TP-3185j p 39 N92-22186 tNASA-CP-3084 I p 49 1,91-14100 Meassurnment and Characferization of the Acceleration

Shortcomings in ground testing, environment RADIO FREQUENCIES Environment on Board the Space Station

simulations. and performance predictions for space Flighf tests with a data link used for air traffic control INASA-CP-308131 p48 N91 -12401

applications information exchange Responses of women to orthostatic and exercise

I NASA-TP-32 171 p 23 N92-22593 I NASA-TP-3 1351 p 11 N9 1-31t143 stresses Track structure model ot Cell damage ini space flight RADIO WAVES INASA-TP-30431 p 37 N9 1.19711

INASA-TP-32351 p 39 N92-34154 Propagation e"Itcs for land mobile satellite systems Aerospace Applications of Magnetic Suspension RADIATlION DOSAGE Overview of experimental and modeling results Technology, part 1

Improvemerits in computational accuracy of BRYNTRN [NASA-RP-1 274) p 25 N92-20404 I NASA-CP-tI0066-PT- I1I p 17 N91 -21188

(a baryon transport code) RADIOGRAPHY The microgravity environment of the Space Shuttle I NASA-TP-30931 p 51 N91-23017 National Educators' Workshop Update 1968. Standard Columbia middeck during STS-32 First LDEF Post-Retrieval Symposium abstracts Euperimlents in Engineering Materials Science and [NASA.TP-31 40) p48 N92-119Z,0

!NASA-CP.100721 p52 N91-24972 Technology The microgravify environment of the Space Shuttle

Analyses of risks associated with radiation exposure I NASA-CP-3060 I p 20 N9 i -20207 Columbia payload bay during STS-32

from past major Solar particle events RADIOMETERS INASA-TP-31411 p 49 N92-t11931

I NASA-TP-31371 p 50 N91-31G61 Limb-darkrening functions as derived trom along-track Analysis of gravity-induced particle motion and fluid

Benichmarki solutions for the galactic heavy-ion transport operation of the ERBE scanning radiometers for August pertusion flow in the NASA-designed rotating

equations with energy and spatial coupling 1985 rero-head-space tissue culture vessel

INASA TP-31 121 p 44 N92-13756 I NASA-RP-12431 p 34 N91-14683 I NASA-TP-31431 p 24 N92-13340

MIRACAL A mission radiation calcuiation program for Mission description and in-flight operations of ERBE Techniques for deterimnation of impact forces during

analysis of lunar and interplanetaty missions instrumentls on EROS, NOAA 9. and NOAA 10 walking and running in a zero-G environment

I NASA-TP-32t11 p51 N92-?StOO spacecraft I NASA-TP-31591 p 38 N92-17022 RADIATION EFFECTS lNASA-RP-t2791 p 32 N92-32127 International Wcrkshop on Vibration Isolation

Radiation rtsk prediction-, for Space Station Freedom RAIL TRANSPORTATION ýechnology for Microgravity Science Applications

orb-its Determination of the flight hardware configuration of an I NASA-CP-100941 p 24 N92-28436

INASA VP 30981 p 5t N9t-ý26t07 energy absorbing attenuslor for the proposed Space Experimental measurement of the orbital paths of Crful~iar rirpair/misrepair track model Station crew and equipment translation aret Cart particles sedtimenting within a rotating viscous fluid as

!NASA TP 31241 p 42 N92. 11685 1INASA.TP-3084I 1 ig N91-21556 influenced by gravity

Transport. mirtnoiiv ani ritreactions for space RAtN f NASA-1P-32001 p 40 N92-28897 radiatoins Airborne Wind Shear Detection and Warning Systems REFLECTOR ANTENNAS

INASA lRP 12571 p 51 N92-1591r6 Third Combined Manulacturers' and Technologists A new fabrication method for precsion antenna

Muiripie lesion track stricurwe modeol Conference, part I reflectors for space flight and ground test

NASA-VP 3195 1 p 39 N92,22186 I NASA-CP-t10060 PT I I p 9 Ni9l-24166 INASA-TP-30781 p 17 N91g 21185

A-27
REFLECTORS SUBJECT INDEX

REFLECTORS NASA scientific and technical publications A catalog Automation and Robotics for Space-Based Systems. A new fabrication method tor precision antenna of special publications, reference publications, conference 1991

reflectors for space flight arid ground last publications, and technical papers. 1987-1990 INASA-CP-100981 p 43 N92-27763

INASA-TP-30781 p 17 N91-21185 INASA-SP.70631051) p 4

7 N91-24939 ROBOT DYNAMICS

REFRACTORY MATERIALS RESCUE OPERATION4S A generalized method for muiltiple robotic manipulator High-temperature durability considerations for HSCT Numerical analysis and simulation of an assured crew programming applied to vertical-up welding combustor return vehicle flow field [NASA-TP-31631 to24 N92-11218

I NASA-TP-31621 p 23 N92-17070 fNASA-TP-3101 p p26 N92-10161 ROBOTICS

REGENERATION (PHYSIOLOGY) RESEARCH AND DEVELOPMEN4T Faiv.tn Annual Workshiop on Space Operations Biological Life Support Technologies: Commercial Microbiology on Space Station Freedom Applications and Research (SOAP 90) opportunities I NASA-CP-31 081 p 37 N91-18573 INASA-CP-3103-VOL.A I p 41 N91-20641

[NASA-CP.30941 p 36 N9t-13842 Proceedings of the X.15 First Flight 30th Anniversary Fourtfh NASA Workshop on Computational Control of

Controlled Ecological Life Support Systems: Natural and Celebration Flexible Aerospace Systems, pan 2

Autl,i', Ecosystems I NASA-CP-31 051 p 10 N91-20071 INASA-CP-tO0eS-PT-21 p 17 N91-22331

[NA,-ý IP-100401 p 40 N91-24744 National Educators' Workshop.ý Update 1988. Standard The 1991 Goddard Conference on Space Applications

REGRESSION ANALYSIS Experiments in Engineering Materials Science and of Artficical intelligence

Correlation and prediction of dynamic human isolated Technology (NASA-CP-31101 p 43 N91-22769

joint strength from lean body mass [NASA-CP-30601 p 20 N91-20207 Technology 2000. volume 1

1NASA-TP-3207 j p 40 N-92-26682 The Federal Conference on Intelligent Processing INASA-CP-3109-VOL-tI p 52 N91-23021

REGULATIONS Equipment The 25th, Aerospace Mechanisms Symposium

Twenty-Second Annual NASA Supply and Equipment [NASA-CP-31381 p 52 N92-24987 I NASA-CP-311t31 p 30 N9t-24C603

Management Conference Computational Fluid Dynamics --- numriecal methods Large space structures and systems in the Space station

[NASA-CP-100421 p 46 N91-111591 arid algorithm development aera A bibliography with indexes (supplement 031

REINFORCED PLATES I NASA.CP- 100781 pt 12 N92-25808 [NASA-SP-7086103) p p18 N92-22317

Experimental behavior of graphite-epoxy Y-stiffened RESEARCH FACILITES Fifth Annual Workshop on Space Operations

specimrens loaded in compression Engines and innovation Lewis Laboratory and American Applications and Research (SOAR 1991). volume 2

[NASA-TP-31711 p 30 N92-23115 Propulsion techno0logy INASA-CP-3127-VOL-2) p 41 N92-22324

RELATIVE BIOLOGICAL EFFECTIVENESS (ROE) [ NASA-SP-43061 p 51 N91-15975 Technology 2001. The Second National Technology

Cellular track model of biological damage to mammalian NASA Wallops Flight Facility Air-See Interaction Transfer Conference and Exposition. volumeI

cell cultures from galactic corsmic rays Research Facility I NASA-CP-3I36VOL. I I p 52 N92-22423

(NASA-TP-3055] p 50 N91-16981 I NASA-RP-12771 p 36 N92-25981 Technology 2001 The Second Nationul Technology

Cellular repairlmiarepair track model Sixteenth international Laser Radar Conference, part Transfer Conference and Exposition, volume 2 1 (NASA-CP.3t36-VOL-21 p 62 N92-22676 If.NASA-TP-3t124) p 42 N92-1 1685 )NASA-CP-3t58-PT-1) p 28 N92-29228 Automation and Robotics for Space-Based Systems, Track structure model of cell damage in space flight RESEARCH PROJECTS 1991

1 NASA-TP-32351 p 39 N92-34154 Nuclear Thermal Propulsion. A Joint NASAIDOEI000 INASA-CP-100981 p 43 N92-27763

RELATIVISTIC PARTICLES Workshop Ongoing Progress in Spacecraft Controls

Inclusive inelastic scattering of heavy ions and nuclear [NASA-CP-10079j P20 N92-11088 [NASA-CP,100991 po 19 N92-28730

correlations RESIDUAL STRENGTH Cable compliance [ NASA-TP-30261 p 46 N91-13985 An examination of the damage tolerance enhancement INASA-TP-32161 p 24 N92-30378

RELIABILITY of carbon/epoxy using an outer lamina of spectra (R) ROBOTS

Reliability training [NASA-TP-31601 p21 N92ý11142 Automation and Robotics for Space-Based Systems. [NASA-RP-12531 p 15 N92-32456 RESILIENCE 1991

RELIABILITY ANALYSIS Effect of temperature and gap opening rate on the I NASA-CP- 10098 1 p 43 N92-27763 Model reduction by trimming for a class of semi-Markov resiliency of candidate solid locket booster O-orig Development of a truss joint for robotic assembly o1

reliability models and the corresponding error bound matenials saesrcue [NASA-TP-30891 p 43 N91-25741 fNASA-TP.3226J p 23 N92-27194 spc N SATructures1N9-297

Structural deterministic safety factors selection critenia RESONANT VIBRATION ROBUSTNESS (MATNEMATICSI and verfifcation Flow-induced resonance of screen-covered cavities On the formulation of a minimal uncertainty model for

I NASA-TP-32031 p 30 1192-19355 [NASA-,TP-30521 p25 %SI-15499 robust control wifh structured uncertainty

Advanced techniques in reliability model representation RESOURCE ALLOCATION I NASA-TP-3094 I p 13 N92- 10027

and solution Space Network Control Conference on Resource ROCKET ENGINE DESIGN [NASA-TP-32421 p 43 N92-33483 Allocation Concepts arid Approaches

RELIABILITY ENIERNNASA-CP-31241 p 16 N92-11039 Nuclear Thermal Propulsion. A Joint NASA/DOE'DOO

RELABI-LTY FNGIgh-NEER INGitlSsesTcnt RESOURCES MANAGEMENT Workshop

NAALacFlgtCrtca iitlSytm Tcnooy Resource envelope concepts for mission planning INASA-CP-10079) p 20 N92-1 1088

[orkshop-02j N140 I NASA-TP-3139) p 15 N91-29209 Rocket-Based Combined-Cycle IRBCC) Propulsion NAAC-108 1N1220 REUSABLE ROCKET ENGINES Technology Workshop Tutorial session Fault tolerance of artificial neural networks with Structural Integrity and Durability of Reusable Space INASA-CP-100901 p 20 N92-21517

applications in critical systems Propulsion Systems Tenth Workshop for Computational Fluid Dynamic INASA-TP-31871 p 42 N92-22285 (NASA-CP-100301 p 19 N91-24307 Applications in Rocket Propulsion, part 2

RELIEF MAPS REYNOLDS NUMBER INASA-CP-3163-PT.21 p 27 N92-32245

Atlas of wide-field-of-view outgoing longwave radiation Companison of a two-dimensional adaptive-wall ROCKET ENGINES

deried from Nimbus 7 Earth radiation budget data set, technique with analytical wall interference correction Rocket-Based Combined-Cycle IRBCCI Propulsion November 1985 to October 1987 techniques Techriology Workshop Tutorial session

(NASA-RP-12611 p 35 N91-24719 I NASA-TP-31321 p 7 N92-20494 [NASA-CP-100901 p 20 N92-21517

REMOTE MANIPULATOR SYSTEM RHEOLOGY ROCKET EXHAUST

Automation and Robotics for Space-Based Systems, Lewis icing research tunnel test of the aerodynamic Optical measuremenets on solid specimens of solid rocket

1991 effects of aircraft ground deicing/anti-icing fluids motor exhaust and solid rocket motoi slag )NASA-CP-100981 p 43 N92-27763 (NASA-TP.A2381 p 10 N92-30395 (NASA-TP-31771 p 20 N92-20949

REMOTE SENSING RIGID STRUCTURES ROCKET NOSE CONES

Mulfisource Data In-tegration in Remote Sensing Rigid-body-control subsystem sizing for an Earth science Comnputational methods for frictionless contact winr

[NASA-CP-3099j p 32 N9t-15615 geostationary platform application to Space Shuttle Orbiter nose-gear tires

NASA/MSFC FY90 Global Scale Atmospheric INASA-TP-30871 p 17 N91-22302 INASA-TP-30731 p 30 N9t-22576

Processes Research Program Revienw ROBOT ARMS ROLLING CONTACT LOADS

INASA-CP-30931 p35 1,91-16500 A generalized method for multiple robotic manipulator Computational methods lot frictionless contact with

Sixteenth international Laser Radar Conference, part programming applied to vertical-up welding application to Space Shuttle Orbiter nose-gear tires

1 I NASA-TP-31631 p 2

4 N92112`18 IAAT-03 3 ~.27

I NASA-CP-3158-PT-t Ij p 28 N192-29228 Auoato adRbtcfoSpe-sdSyem. OLLING MOMENTS

Sixteenth~~~~~~~ ItrainlLsrRdrCneecpi NASA-GP- 100981 p 43 N92-27763 A nozzle internal performance prediction method

2 Cable compliance I NASA-TP 32211 ti 8 N192-33625

INASA-CP-3158-PT-21 p 28 N92-31013 INASA-TP-32161 p 2

4 N92-30378 ROTARY WINGS

REMOTE SE.NSORS ROBOT CONTROL Development 0f a full-scale transmission testing Multisource Data integration in Remote Sensing Fourth NASA Workshop on Computational Control of procedure to evaluate advanced iibricants

1 NASA-CP-30991 p 32 N91-15515 Flexible Aerospace Systems. part I INASASTP-32651 pi 28 N92ý30396

RENE 41 1INASA-CP-10065-PT- I p 17 N91-22307 ROTATING BODIES

thermal and structural tests of Rene 41 honeycomb The effect of bandwidth on lelerobot system Definition and design of an expernment to te,,t raster

integral-tank concept for future space transportation performance scanning with rotatin-g viitinahance3mass devices on

systems I NASA-TP-31521 p 28 N91.30540 gimbaled payloads INASA.TP-it 45) p 30 N92-24205 A generalized method for miiltiple robotic manipulator I NASA TP 3249 ) p 24 N92 2967 7

REPORTS programming applied to vertical-up welding ROTATING FLUIDS

NASA scientific and technical publications A catalog I NASA-TP-31631 p 24 N92- t1218 Experimental measuremnent of the o'brxa paths ofi

of special publications, reference publications. conference The Federal Conference on Intelligent Processing parlisles sedimenting within a rotattng vtscoriIiiis ld as

publications, and technical papers 1969 Equipment influenced tiy gravity

I NASA-SP-706.1(04)] p 4 7 N91-13374 jNASA-CP-3i38j p 52 N92-24987 I NASA.TP 3200 1 p04() N92 298I47

A-28
SUBJECTINDEX SHORT TAKEOFF AIRCRAFT

ROTATION SATELLITE CONTROL SEDIMENTS Reconfiguring the RUM experiment to test circular A scheme for bandpass filtering magnetometer Experimental measurement of the orbital paths of

scanning with rotating unbalanced-mass devices on measurements to reconstruct tethered satellite skiprope particles sedimenting wihin a rotating viscous fluid as

gimbaled payloads motion influenced by gravity

INASA-TP-32821 p 25 N92-33601 [NASA.TP-31231 p42 N91-25629 INASA-TP-3200l p 40 N92-28897

Inertial oscillation of a vertical rotating draft with SATELLITE INSTRUMENTS SELECTION

application to a supercelt storm. Video supplement to The 22nd Annual Precise Time and Time Interval (PTTI) First among equals The selection of NASA space

NASA Technical Paper 3230 Applications and Planning Meeting science experiments

INASA-TP-3230-VIOEO-SUPPLp p 36 N92-34246 INASA-CP-31161 p 44 N91-25755 (NASA-SP421t5J p 52 N91 28060

ROTOR AERODYNAMICS Advanced Modulation and Coding Technology SEMISPAN MODELS

Transonic flow analysis for rotors Part 3: Conference Full-scale semispan tests of a business-let wing with a

Three-dimensional, quasi-sxe¢dy, Euler calculation JNASA-CP-100531 p 16 N92,22001 naturat laminar flow airfoil

INASA-TP-2375| p 3 N91-10007 SAGE 1 data user's guide INASA-TP-3133] p 6 N91-30098

ROTOR DYNAMICS (NASA.RP-12751 p 34 N92-33097 NACA 0015 wing pressure and trailing vortex

Limit cycle vibrations in turbomachmery Proceedings of the 23rd Annual Precise Time and Time measurements

[NASA-TP-3151 I p 6 N92-t0981

NASA-TP-31811 p 20 N92-14108 Interval (PTTI) Applications and Planning Meeting NSORY PERCEPION

[NASA-CP-31591 p 44 N92-33350 SENSORY PERCE fTION Rotordynamic Instability Problems in High-Performance Human Machine interfaces for Teleoperatorsand Vrtual

Turbomachinery. 1990 SATELLITE NETWORKS Environments Conference

INASA-CP-3122J p 28 N92-14346 Space Communications Technology Conference. [NASA-CP-100711 p 40 N92-11638 ROTORS Onboard Processing and Switching ROTORS-332 pI5N2-40 SERVICE LIFE LNASA-CP-3132a p 25 N92-14202 Long-term life testing of Geostationary Operational

UNA 

Limit cycle vibrations in tupbomachinery Destination-directed, packet-switching architecture for Environmental Satellite (GOES) encoder lamps A-T 8 I p 20 N92-14108 30/20-GHz FDMA/TDM geostationary communications INASA-RP-12731 p 23 N92-20063 RUNGE-KU"TA METHOD satellite network Reliability training Validation of three-dimensional incompressible spatial INASA-TP-3201] p 16 N92-19762 INASA-RP-12531 p 15 N92-32456

direct numerical simulation code A comparison with fneear SATELLITE OBSERVATION SEAVOCONTROL

stability and parabolic stability equation theories Jr FIRE Science Results 1988 Development of an integrated aeroservoelastic analysis

boundary-layer transition on a flat plate I NASA-CP-3083] p 34 N91-10448 program and correlation with test datl

INASA-TP.32051 p 8 N92-30295 Atlas of wide-field-of-view outgoing longwave radiation INASA-TP-31201 p2 N91-261 i3

derived from Nimbus 7 Earth radiation budget data set, SERVOMECHANISMS

S November 1985 to October 1987 Definition and design of an experiment to lest raster INASA-RP-1261] p35 N91-24719 scanning with rotating unbalanced-mass devices on Atlas of the Earth's radiation budget as measured by gimbaled payloads SAFETY Nimbus-7- May 1979 to May 1980 [NASA-TP-32491 p 24 N92 29677

Twenty-Second Annual NASA Supply and Equipment [NASA-RP-12631 p35 N91.24720 Reconfigurting the RUM experiment to test circular

Management Conference

{NASA-CP-10042) p 46 N91-11591 NASA/MSFC FYg1 Global Scale Atmospheric scanning with rotating unbalanced-mass devices on

SAFETY FACTORS Processes Research Program Review gimbaled payloads INASA-CP-31261 p35 N91-32660 INASA-TP-32821 p25 N92-33601 Plate and butt-weld stresses beyond elastic limit, SATELLITE TEMPERATURE SERVOMOTORS

material and structural modeling SATEnLtTE TdMPnRATURE

INASA.TP-30751 p29 N91-16413 LDEF 69 Months in Space First Post-Retrieval Deinition and design ot an expeimen to test raster

Symposium, part 3 scanning with rotating unbalanced-mass devices on

Flight tests with a data link used lor air traffic control I NASA-CP-3134-PT-3] p 52 N92-27083 g9mbaled payloads

information exchange INASA.TP-32491 P24 N92-29677

[NASA.TP-3135] p 11 N91-31143 SATELLITES Reconfiguring the RUM f cml to test circular

Structural deterministic Shortcomings in ground testing, environment scanning with rotating unbalanced-mass devices on

and verificat3on 

safety factors selection crtena simulations, and performance predictions for space gimbalad payloads applications [NASAFTP-3203Y INASA-TP-32821 p 25 N92-33601 p30 N92-19355 INASA-TP-3217] p 23 N92-22593 SET THEORY SAFETY MANAGEMENT SATURATION (CHEMISTRY) Proceedings of the Second Joint Technology Worisrop The development 14ation of the NASA safety reporting Saeurat-on point model for the formation of metal nitrate on Neural Networks and Fuzzy Logic. volume 2 system pn ni(roqan tetroxide oxidizer I NASA-CP.1006-tVOL.2! p43 N91-20811 ISNASA-RP-TL1141 p 10 N91-70436 NASA-TP-3107] p 26 N91-24542 SHAPES SAGE SATELLITE SATURN 5 LAUNCH VEHICLES Effect of crash pulse shape on seat stroke requirements SA-RPE 1 data user's gu3de The role of failure/problems in engineering- A for limiting loads on occupants of aircraft NASA-RP,12751 p 34 N92-33097 commentary of failures experienced - lessons learned INASA-TP-3126] p 30 N92-18053 SAMARIUM [NASA-TP-32131 p 24 N92,22235 Comparison of let plume shape predictions and piume

The 23 to 300 C demagnetization resistance of SCALE MODELS influence on sonic boom signature

samanum-cobalt permanent mregnets Low-speed, powered ground effects of a generic, (NASA-TP-31721 p 7 N92-25133

[NASA-TP-3t 19] p25 N92-11252 hypersonic configuration SHEAR STRENGTH

SANDS INASA.TP-30921 p 5 N91-25103 A novel method of testing the shear strength of thick

Sand and Dust on Mars Wind tunnel aerodynamic characteristics of a honeycomb composites

INASA-CP-100741 p 50 N91-27057 transport-type airfoil in a simulated heavy rai [NASA-TP-31081 p21 N91-21242

SANDWICH STRUCTURES environment SHOCK ABSORBERS

Optimization of composite sandwich cover panels tNASA-TP-31B4 p 8 N92-31532 Determination of the flight hardware configuration of an subjected to compressive loadings SCANNERS energy absorbng anfenuator for the proposed Space

[NASA-TP-31731 p 21 N92-20679 Reconfiguring the RUM experiment to test circular Station crew and equlpment translation aid cart

Thermal and structural tests of Rene 41 honeycomb scanning with rotating unbalanced-mass devices on INASA-TP-30841 p 29 N91-21556

mtegral-tank concept for future space transportation gimbaled payloads SHOCK LAYERS

systems [NASA-TP-32821 p 25 N92-33601 Stagnation-pomt heal-transfer rate predictions at (NASA-TP-31451 p 30 N92-24205 aeroassist flight conditions SCANNING (NASA-TP-32081 p 27 N92-31281 SATELLITE ANTENNAS Re-onfiguring the RUM experiment to test circular A new fabrication method for precision antenna scanning with rotating unbalanced-mass devices on SHOCK TUNNELS

reflectors for space flight and ground test gmaled payload- An analysis of combustion studies in shock expansion

NASA-TP-3078 p17 N9-285 IaTP-3282 p 25 N92-33601 tunnels and reflected shock tunnels

SATELLITE ATTITUDE CONTROL INASA-TP-32241 p 22 N92-28374

Flight Mechanics/Estimation Theory Symposium, 1990 SCIENTISTS SHOCK WAVE INTERACTION [NASA-CP-31021 p 14 N91-17073 NASA engineers and the age of Apollo Shock wave interaction with an abrupt area change [NASA-SP-4t041 pI52 N92-28344 INASA.TP.31131 p6 N91-27140 Rigid-body-control subsystem sizing tor an Earth science SOKWV RPGTO

geostationary platform SCREENS SHOCK WAVE PROPAGATION

[NASA-TP-30871 p 17 N91 -22302 Flow-induced resonance of screen-covered cavities High-Speed Research Sonic Boom. volume

A nonlinear estimator for reconstructing the angular INASA-TP-30521 p25 N91-t5499 INASA-CP-31721 p 1I N92-33874

velocity of a spacecraft without rate gyros SEA LEVEL SHOCK WAVES J NASA-TP-3178I p 24 N92,13343 West Antarctic Ice Sheet Initiative Volume 2 Discipline Shock wave interaction with an abrupt area change

SATELLITE COMMUNICATION Reviews INASA-TP-31131 p6 N91.27140

Space Communications Technology Conference I NASA-CP-31 15-VOL-2i p 32 N91-26573 A simplified method for thermal analysis of a cowl leading edge subject to intense loral shock-wave-inieffefence

Onboard Processing and Swtching SEALING headang INASA-CP.31321 p 25 N92-14202 Effect of temperature and gap opening rate on the (NASA-TP-3167] p 27 N92-24797

Destinaeon-directed, packet-switching architecture for resiliency of candidate solid rocket booster 0-ring SHORT TAKEOFF AIRCRAFT

30/20-GHz FOMAITDM geostafonary communications materials NASA Computational Fluid Dynamics Conference

satellite network INASA-TP.32261 p 23 N92 27194 Volume 2 Sessions 7-12 (NASA-TP-32011 p 16 N92-19762 SEATS INASA-CP-10038-VOL 21 p 4 N91-1081,8

Advanced Modulation and Coding Technology Effect of crash pulse shape on seat stroke requirements Static internal performance of ventral and rear nozzle

Conference for limiting loads on occupants of aircraft concepts for short-takeoff and vertical-landing aircraft

INASA.CP-100531 p 16 N92-22001 INASA-TP-3126J p 30 N92-18053 1NASA-TP 31031 p 6 N92?10975

A-29
SHOULDERS SUBJECT INDEX

SHOULDERS SOFTWARE TOOLS Biological Life Support Technologies Commercial The validation of a human force model to predict dynamic Second CLIPS Conference Proceedings, volume 2 Opportunities

forces resulting from multi-j

oint motions I NASA-CP-10085-VOL-21 p 42 N92-16590 INASA-CP-30941 p 36 N91-13842

(NASA.TP-32061 p 40 N92-26538 Advanced techniques in reliability model representation Large space structures and systems in the space station

SIGNAL ANALYSIS and solution era A bibliography with indexes (supplement 03)

Time-frequency representation of a highly nonstationary INASA-TP-3242] p 4 3 N92-33483 ItlASA-SP-7085(03)1 p 18 N92-22317

signal via the modified Wigner distribution SOLAR ACTIVITY EFFECTS Development of a truss joint for robotic assembly of

[NASA-TP-3215] p 25 N92-20492 Climate Impact of Solar Variability space structures

SIGNAL PROCESSING (NASA-CP-30861 p 50 N91-12456 INASA-TP-32141 p 31 N92-27974 Proceedings of the Second Joint Technology Workshop SOLAR ARRAYS SPACE COMMUNICATION

on Neural Networks and Fuzzy Logic, volume I Space Photovoltaic Research and Technology. 1989 Space Network Control Conference on Resource

[NASA.CP-10061-VOL- I] p 43 N91-21778 INASA-CP-31071 p 19 N91-19182 Allocation Concepts and Approaches

Space and Earth Science Data Compression I NASA-CP-3124) p 16 N92-t 1039

Workshop MILSTAR's flexible substrata solar array Lessons Space Communications Technology Conference

[NASA-CP-31301 p 41 N92-12425 learned, addendum Onboard Processing and Switching

Time-frequency representation of ahighly nonstationary NASA-CP-3147-ADD] p 33 N92-26895 INASA-CP.31321 p 25 N92-14202

signal via the modified Wigner distribution Influence of mass moment of inertia on normal modes SPACE DEBRIS

I NASA-TP-3215j p 25 N92-20492 of preloaded solar array mast Optical measurementson solid specimensof solid rocket

SIGNATURES [NASA-TP-32731 p 31 N92-33476 motor exhaust and solid rocket motor slag

Comparison of let plume shape predictions and plume SOLAR CELLS I NASA-TP311771 p 20 N92-20949 influence on sonic boom signature Space Photovoltaic Research and Technology. 1989 Fifth Annual Workshop on Space Operations

INASA-TP-31721 p 7 N92-25133 NASA-CP.3107j p 19 N91-19182 Applications and Research (SOAR 1991), volume 2 SILICON CARBIDES Space Photovoltaic Research and Technology INASA-CP-3127-VOL-2J p 41 N92-22324

Gibbs free energy of reactions involving SiC, Si3N4. H2. Conference Orbital debris Technical issues and future directions

and H20 as a function of temperature and pressure [NASA-CP.31211 p 19 N91-30203 [NASA-CP-10077j p 49 N92-33478

INASA.TP-32751 p 23 N92-31278 SOLAR CORPUSCULAR RADIATION SPACE ENVIRONMENT SIMULATION

SILICON NITRIDES Analyses of risks associated with radiation exposure Sixteenth Space Simulation Conference Confirming

Gibbs free energ, of reactions involving StC, Si3N4, H2, from past major solar particle events Spaceworthiness into the Next Millennium

and H20 as a funcd, n of temperature and pressure [NASA-TP-3137J p 50 N91-31061 INASA.CP-3096] p 17 N91-19126 INASA-TP-32751 p 23 N92-31278 SOLAR RADIATION SPACE ERECTABLE STRUCTURES

SILVER ZINC BATTERIES Climate Impact of Solar Variability Launch vehicle integration options for a large Eartn

The 1991 NASA Aerospace Battery Workshop [NASA-CP-30861 p50 N91-12456 sciences geostationary platform concept

[NASA-CP-31401 p 33 N92-22740 SOLAR SYSTEM INASA-TP.3083] p 15 N91-27180

The t990 NASA Aerospace Batlery Workshop Planetary geosciences, 1989-1990 Packaging. development, and on-orbit assembly options

INASA-CP-31191 p 20 N92-27130 INASA-SP-508) p 50 N92-28345 tor large geostationary spacecraft

SIMULATION SOLID MECHANICS I NASA-TP-30881 p 17 N91-27182

NASA Computational Fluid Dynamics Conference Improved accuracy for finite element structural analysis Development of a truss joint for robotic assembly of

Volume I Sessions 1-6 via a new integrated force method space structures INASA-CP-10038-VOL-1I p 4 N91-10839 INASA.TP.3204) p 30 N92-22227 INASA-TP-32141 p 31 N92-27974

Simulation of real-gas effects on pressure distributions SOLID PROPELLANT ROCKET ENGINES Software design for automated assembly of truss

for aeroassist flight expenment vehicle and companson Axssymmetnc shell analysis of the space shuttle solid stnuctures

with prediction rocket booster field toint INASA-TP-3198] p 43 N92-28375

INASA.TP-31571 p27 N92-20677 INASA-TP-30331 p28 N91-14618 SPACE EXPLORATION

SINGLE EVENT UPSETS Optical measurements on solid specimens of solid rocket Evobiology on Mars

Shortcomings in ground testing, environment motor exhaust and solid rocket motor slag [NASA-CP-10055) p 41 N91-1569i

simulations, and performance predictions for space [NASA-TP-31771 p 20 N92-20949 Vision-21 Space Travel for the Next Millennium

applications Tenth Workshop for Computational Fluid Dynamic (NASA-CP-10059j p 13 N91-22139

I NASA-TP-3217] p 23 N92-22593 Applications in Rocket Propulsion. part 2 International exploration of Mars A specia; SKIN TEMPERATURE (NON-BIOLOGICAL) (NASA-CP.3163-PT-2, p 27 N92-32245 bibliography

Numerical studies of convective cooling for a locally Tenth Workshop for Computafional Fluid Dynamic [NASA.SP-7091 I p 49 N91-24965

heated skin Applications in Rocket Propulsion, part 1 MIRACAL A mission radiation calculation program for INASA TP-3 1I(On p 26 N91-22509 INASA-CP-3163-PT-t11 p 27 N92-32278 analysis of lunar and interplanetary missions

SLAGS SOLID ROCKET PROPELLANTS I NASA.TP-321ft p 51 N92-25100

Optical measurements on solid specimens of solid rocket Optical measurements on solid specimens of solid rocket Ongoing Progress in Spacecraft Controls

"no!3r eulidi &xno SOlic rocket motor Slag motor exhaust and solid rocket motor slag :NASA-CP-100991 p 19 N92-28730

fNASA-TP-31 771 p 20 N92-20949 {NASA-TP-31771 p 20 N92-20949 Electrical and chemical interactions at Mars Workshop,

SLENDER WINGS SONIC BOOMS part I Wind tunnel investigation of the interactinn and A loudness calculation procedure applied to shaped [NASA-CP-10093] p 50 N92-30302

breakdown characteristics of slender wing vortices at sonic booms SPACE FLIGHT

subsonic transonic, and supersonic Speeds INASA.TP-3134J p45 N92-11765 Proceedings of the X-15 First Flight 30th Anniversary

]NASA-TP-31141 p6 N92-12994 The atmospheric effects of stratosphenc aircraft, A first Celebration

The natural flow wing-design concept program report INASA-CP-31051 p 10 N91-20071

I NASA-TP-3193J p 7 N92-25202 [NASA-RP-12721 p 33 N92-19121 SPACE FLIGHT FEEDING

SLUSH HYDROGEN Comparison of let plume shape predictions and plume Nutritional Requirements for Space Station Freedom

Feasibility study of a low-energy gamma ray system for influence on sonic boom signature Crews

measuring quantity and flow rate of slush hydrogen INASA-TP-31 72; p 7 N92-25133 ]NASA-CP-3146j p 40 N92-25961 INASA.TP-31501 p 19 N92-25147 High-Speed Research Sonic Boom, volume 1 SPACE LABORATORIES

SMALL SCIENTIFIC SATELLITES J NASA-CP.31 721 p 11 N92-33874 Exotbiofogy in Earth orbit The results of science

Small Explorer Data System MIL-STO-1773 fiber optic SOOT workshops held at NASA, Ames Research Center

bus International Workshop on Stratospheric Aerosols: [NASA-SP.500I p 41 N91-14725 1 NASA-TP-32271 p 16 N92-26667 Measurements, Properties. and Effects SPACE MANUFACTURING

SMOOTHING INASA-CP-31141 p 32 N91-32528 Internahonal Workshop on Vibration isolaton

Trajectory titting in function space with application to SOUND FIELDS Technology for Microgravity Science Applications

analytic modeling of surfaces J-85 let engne noise measured in the ONERA S1 wind NASA-CP.100941 p 24 N92-28436 I NASA.TP-32321 p 8 N92-30747 tunnel and extrapolated to far field SPACE MISSIONS

SODIUM SULFUR BATTERIES [NASA-TP-3053J p 45 N91-19823 Upper stages using iqutd propulsion and metallized

The 1991 NASA Aerospace Battery Workshop SOUND PROPAGATION propellants

fNASA.CP-3t40 p 33 N92-22740 Monograph on propagation of sound waves in curved INASA-TP-3191i p 20 N92-1715t

SOFTWARE ENGINEERING ducts SPACE OBSERVATIONS (FROM EARTH)

Space Transportation Avionics Technology Symposium I NASAnRP 12481 r p 44 N91-1584y Space and Earth Science Data Compression

Volume 2 Conference Proceedings Fourth Intana 'al Symposium on Long-Range Sound Workshop

INASA-CP-3081 -VOL-21 p11 N91i.17020 Propagation -NASACP1334 pat1 N92-12425

Proceedings of the Second Annual NASA Science IUNASA-CP-3tVES 44 N91-16682 SPACE PERCEPTION

Internet User WorkingJ GrOup p46ferenc00 Monograph on propagation of sound waves in curved Effect of short-term exposure to stereoscopic INASA.CP-3117j p48 N91.27009 ducts three-dimensional flight displays on real world depth

Beyond the Baseline 1991 Proceedings of the Space INASA-RP-12481 p 44 N91.15848 perception

Station Evolution Symposium Volume 2 Space Station Wind turbine acoustics INASA-TP-3t 171 p 1 t N92. 13065 Freedom. part 2 I NASA.TP-30571 p44 N91-!6679 Visually Guided Control of Movement

INASA-CP-t0083 VOL-2.PT-2) p 18 N92-17348 SPACE CH ,RGE [NASA-CP-31181 p 39 N92-21467

Software Surface Modeling and Grid Generation Current Collection from Space Plasmas SPACE PLASMAS

Steering Committee INASA-CP-30891 p 46 N91.17713 Current Collection from Space Plasmas iNASA-CP-3t431 p 4

2 N92-24397 SPACE COMMERCIALIZATION INASA-CP-30891 p 4P N91.17713

Software design for automated assembly of truss Measurement and Characterization of the Acceleration Fifth Annual Workshop on Space Operations structures Environment on Board the Space Station Applications and Research (SOAR 1991). volume ;

(NASA TP.31981 p 43 N92 28375 INASA-CP-30881 p 48 N9t-12AOt (NASA-CP-3127-VOL. I p 41 N92.ý232,

A-30
SUBJECTINOEX SPACECRAFT CONTAMINATION

SPACE PROCESSING Beyond the Baseline 1991: Proceedings ot the Space SPACE TRANSPORTATION SYSTEM

Measurement and Characterization of the Acceleration Station Evolution Symposium Volume I Space Station Space Transportation Avionics Technology Symposium

Environment on Board the Space Station Freedom, part 2 Volume 2 Cotiference Proceedings

INASA-CP-30881 p48) N91-124011 INASA-CP-10083-VOL-1-PT.21 p 18 N92-17409 tNASA-CP-3061-VOL-21 p 11 N91-170ZO

Space Station Freedom Toxic and Reactive Materials Beyond the Baseline 1991. Proceedings of the Space Manual Control Aspects o1 Orbital Flight

H-andling Station Evolution Symposium Volume 2- Space Station INASA-CP-100561 p 13 N91 202147

JNASA-CP-3085 p 48 N91-1 5930 Freedom. part 1Space Transportation Propulsion Technology

SPACE SHUTTLE BOOSTERS I NASA-CP-10083-VOL-2-PT-t I p 18 N92-17768 Symposium Volume I Executive summary

Aursynimetric shell analysis 0f the space shuttle solid Nutritional Requirements for Space Station Freedom I NASA-CP-311 12)j p 19 N91-.25176

rocket booster field joint Crews Sae Tasotto rplin Tcnlg

INASA-TP-30331 p 28 N91-1 4618 I NASA-CP-31461 p 40 N92-2596t Sypaceu TrnVorlati2Smon Propusn iu echnolog

Optical measurements on solid specimens ofsolid rocket MILSTAR's ftexible substrate solar array Lessons NSymposium Volume2. Sypsu 19roceed8ngs

motor exhaust and solid rocket motor stag learned, addendum IAAPt1-O-Ip1 9-89

tNASA.TP.31 771 p 20 N92-20949 INASA-CP-3147-ADDI p 33 N92-26895 Space Transportation Propulsion Technology

International Workshop on Vibration Isolation Symposium Volume 3- Panel Session Summaries anx The role of failure/problems in engineering: A Technology for MicrOgravity Science Applications Presentations

commentary 0f failures experienced - lessons learned [ NASA.CP- 100941 p 24 N92-28436 (NASA-CPý3t 12-VOL-31 p 19 N91-28235

[NASA-TP-32131 p 24 N92-22235 SPACE STATION PAYLOADS Upper stages using liqu - propulsion and metallized

SPACE SHUTTLE MAIN ENGINL Space Station Freedom Tosic and Reactive Materials propellants

Limit cycle vibrations in Iurbomachineryi Handling INASA-TP-3191 I p 20 N92-17151

[NASA.TP-3181) p20 N92-14108 I NASA-CP-30051 p48 591A15930 The High Resolution Accelerometer Package (HiRAPI

Time-frequency representation of a highly nonstationery SPACE STATIONS flighlt expeniment summary for the first 10 flights

signal via the moditied Wigner distribution Measurement and Characterization of the Acceleration INASA-RP-12671 p 3 N92-22505

[NASA-TP-32151 p 25 N92-20492 Environment on Board the Space Station SPACEBORN4E EXPERIMEN4TS

The role 0f failure/problems in engineering: A [NASA-CP-30881 p48 N91-12401 Exotbiology in Earth orbit The results of science

commentary 0f tailures experienced -lessons learned Radiation protection for human missions to the Moon workshops hetd at NASA, Ames Research Cente

INASA-TP-32131 p 24 N92-22235 and Mars [ NASA-SP.5001 p41 N91-14725

Effect of type 01 toad on stress analysis 01 thin-walled f NASA-TP-30791 p 50 N91-17999 First among equals The selection 0f NASA space

ducts Large space structures and syr'ams in the space station science experiments

[NASA-TP-3248 I p 31 N92-26669 era. A bibliography with indexes INASA-SP-42151i p 52 N91 -28060

Tenth Workshop for Computational Fluid Dynamic [NASA-SP47085(01)I p 17 N91-18199 Development 0f the Burst and Transient Source

Applications in Rocket Propulsion, part 2 Microbiology on Space Station Freedom Esperiment (BATSE)

[NASA-CP.3163-PT-21 p 27 N92-32245 (NASA-CP-3 108 1 p37 N91-18573 (NASA-RP-12681 p 49 N91-32006

SPACE SHUTTLE MISSION 61-C Manual Control Aspects of Orbital Flight The microgravity, environment of the Space Shuttle

The microgravity environment 0f the Space Shuttle I NASA.CP. 100561 p 13 N91-20147 Columbia middeck dunng STS-32

Columbia payioed bay during STS-32 Benefits from synergies and advanced technologies for NASA.TP-31401 p 48 N92-1 1930

INASA-TP-31411 p 49 N92-11 931 an advanced-technology space stationThmcrgaiyevonnt0teSpeSutl (NASA-TP-30671 p 14 N91-20177 Th irgaiyevonntfteSpcSutl SPACE SHUTTLE ORBITERS Fourth Annual Workshop on Space Operations Columbia payload bay during STS-32

Fourth Annual Workshop on Space Operations Applicetions and Research (SOAR 90) [ NASA-TP-3141 Ip 49 N92-11931

Applications and Research (SOAR 90 (NASA-CP-3103-VOL-21 p 41 N91-20702 IDEF 89 Months in Space First Post-Retrieval

(NASA-CP-3103-VOL-21 p41 N91-20702 Determination 0f the flight hardware configuration of an Symposium, pert 1

Computational methods for frictionless contact with energy absorbing attenuator for the proposed Space f NASA-CP-3134-PTt p 52 N92-23280

application to Space Shuttle Orbiter nose-gear tires Station crew and equipment translation aid cart LOEF. 69 Months in Space First Post-Retneval

INASA-TP-30731 p 30 N91-22578 I NASA.TP.30841 p 29 N91-21556 Symposium, part 2

SPACE SHUTTLE PAYLOADS Radiation risk predictions lor Space Station Freedom INASA-CP-313A-PT-21 p 52 592-24806

The microgravity environment of the Space Shuttte orbits Second LDEF Post-Relneval Symposium abstracts

Columbia iniddeck during STS-32 INASA-TP-30981 pSI N91-26107 INASA.CP-ID0971 p 52 N92-27218 fNASA TI- :ý401 p 48 N92-11930 Technology for the Future: In-Space Technology SPACEBORNE TELESCOPES

The mic- ogravity environment 01 the Space Shuttle Experiments Program, part 1 Eirobiology, in Earth orbit The results of science

Columbia payload bay during STS-32 I NASA-CP- 10073-PT-1 I p 14 N91-27177 workshops held at NASA. Ames Research Center

(NASA.TP-3141 p p49 N92-11931 Technology for the Future tn-Space Technology INASA-SP-5001 p 41 N91-14725

Graphite/epoxy composite adapters for the Space Expeniments Program, part 2 SPACECRAFT

Shuttle/Centaur vehicle [NASA-CP-10073.PT-21 p 14 N91-27178 Shortcomings in ground testing, environment

I NASA-TP-30141 p 15 N92-31251 Launch vehicle integration options for a large Earth simulatitcis. and performance predictions for space

SPACE SHUTTLES sciences geostationary platform concept ipplications

Reliability of a Shuttle reaction timer I NASA-TP-30831I p 15 N491I-2-i'- Jii NASA-TP-321 71 p 23 N92-22593

INASA.TP-31761 p 40 N92-16562 Large space structures and systems in the space station SPACECRAFT ANTENNAS

Payload bay doors and radiator panels familiarization era- A bibliography with indexes Influence of mass moment 0f inertia on normal modes

handbook I NASA-SP-7085(02)) p 18 N91-28191 of preloaded solar array mast

INASA-TM. 1077931 p 15 N92-20676 Resource envelope concepts for mission planning INASA-TP-32731 p 31 N92-33476

Theroe lilreprbles 1 n ngleeng A INASA.TP-31391 p 15 N91-29209 SPACECRAFT CABINS

comentryl of failures/eperieceble ssonngnseearined Large space structures and systems in the space station Benefits from synergies and advanced technologies for commen-3tary fiueexeind-lsonsl-arned p24 era: A bibliography with indexes (supplement 03) an advanced-technology space station I AAT-23 p2 9-23 NASA-SP-7085(03fl p 18 N92-22317 I NASA-TP-30671 p 14 N91-20177 Fihth Annual Workshop on Space Operations Filth Annual Workshop on Space Operations SPACECRAFT CHARGING

Applications and Research (SOAR 1991). volume 2 Applications and Research (SOAR 1991). volume 2 Current Collection from Space Plasmas I NASA -CP-3127 -VOL-2j p 41 N92-22324 INASA-CP.3127-VOL-21 p 41 N92-22324 (NASA-CP-30891 p 4

6 N91-17713

International Workshop on Vibration Isolation SPACE SUITS SPACECRAFT CONFIGURATIONS

Technology for Microgravity Science Applications A method of evaluating efficiency during space-suited Parametnic trade studies on a Shuttik 2 launch system I NASA-CP 100941 p 24 N92-28436 work in a neutral buoyancy environment architecture

SPACE STATION FREEDOM INASA-TP-31531 p 40 N92-19772 [NASA-TP-30591 p 14 N91-18180

Space Station Freedom Toxic and Reactive Materials SPACE TRANSPORTATION Benefits from synergies and advanced technologies for

Handling Metallized propellants for the human exploration of an advanced-techniology space nlation [NASA-CP.30851 p48 1,91-15930 Mars INASA-TP-30671 p 14 N9t-20177

Microbiology on Space Station Freedom INASA-TP-30621 p 19 N91-Il1800 Beyond the Baseline 1991 Proceedings of the Space

I NASA -CP-31081 p 37 N91-18573 Lunar missions using chemical propulsion: System Station Evolution Symposiumn Volume 1 Space Staition

Radiation risk predictions for Space Station Freedom design issues Freedom, part 1

orbits INASA-TP-30651 p 19 Ng91-15308 [ NASA-CP-tI0083-VOL-tI-PT-I I p 18 N92.17098

H ASP TP-30981 p51 N91-2610? Space Transportation Propulsion Technology SPACECRAFT CONSTRUCTION MATERIALS

Resource ervelope concepts for mission planning Sypsium. Volume I Executive summary Oulgassing data for selecting spacecraft materials,

(NASA-TP.31391 0p 15 N91-29209 INSym CPo 311p1 N1217 revision 2 Numerical analysis112 siultin-f2nasurd7re6 pn9 NASA-RP-1 124-REV-21 p 21 N91-14437 ehcl anar lys iseadsiuainoanaurdce Space Transportation Propulsion Technology Fourth Annual Workshop on Space Operations

INASA-TP-3101 p p26 ff92-10161 Symposium. Volume 2: Symposium proceedings ;'.iplications and Research (SOAR 90)

Automating a spacecraft electrical power system using [NASA-CP-31 12-VOL-21 p 19 N91-28i93 (NASA-CP-3103-VOL-21 941 N9,-20702

expert systems - Space Transportation Propulsion Technology Space Transportation Materials and Structures

I ASA-TP-3116t p20 N92-I 2052 Symposium Volume I Panel Session Summaries and Technology Workshop Volume 1 Executive Summary

Beyond the Baseline 1991. Proceedings of the Space Presentations -NASA.-CP.3148-VOL I I p 115 N92-22WEf

Station Evolution Symposium Volume 1 Space Station INASA.CP-3112-VOL-31 1 19 N91-28235 Graphite/epoxy composite adapters for the Space

Freedom, parn I Upper Stages using liquid propulsion and metallized Shuttle/Centaur vehicle

I NASA-CP-tI0081-VOL-It-PT- I I p l8 N92-17098 propellants INASA-TP-30141 p1 9 15 Beyond the Baseline 1991: Proceedings of the Space I NASA.TP.3 1911 p 20 N92-1 11St SPACECRAFT CONTAMINATION

Station Evolufion Symposium Volume 2 Space Station Space Transportation Materials and Structures Sixteenlth Space Simulation Conference Confirming

Freedom, part 2 Technology Workshop Volume I Executive summary Spaceworthiness into the Next Millennium

I NASA-CP-t0083-VOL-2-PT 21 p t1t N92-17348 (NASA-CP-3t48-VOL-I I p I5 N92-2266 I NASA-CP-30961 p 17 Ng I -V'126

A-31
SPACECRAFT CONTROL SUBJEC T INDEX

SPACECRAFT CONTROL The 1990 NASA Aerospace Battery Workshop STAP FORMATION

The 51h Annual NASA Spacecraft Control Laboratory I NASA -CP-3t 191 p 20 N92-27 130 the interstellar Medium in External Gatiaares Summaries

Experiment (SCOLE) Workshop. part 1 SPACECRAFT PROPULSION of contributed papers

INASA.CP-10057-PT-1I p 16 N91- 18186 Engines and innovation Lewis Laboratory and American I NASA-CP-30841 p 49 N91 -14100

The 5th Annual NASA Spacecraft Control Laboratory Propulsion technology Interstellar Du~st Contributedi Papers

Experiment ISCOLE) Workshop, part2 1 NASA SP-43061 p5 1,191-15975 1ASA-CP.30361 p48 N91 14897

[NASA.CP-10057-PT-21 p 17 N91-19122 Vision-211 Space Travel for the Next Millennium Ph ýed and interacting Gale, es. international R igid-body-control subsystem sizing for an Earth science I NASA-CP-t100591 p 13 N91.22139 Astronnica Union Colloquium No 124

geostationary platform Space Transportation Propulsion Technology [NASA-CP,30961 p49 N91- 16858

[NASA.TP.30671 p 17 N91-22302 STARBURST GALAXIES

Fourth NASA Workshop on Computational Control of oymposium Volume 3 Panel Session Summaries and Pie n neatn aae nentoa

FlxbeArsaeSses atIPresentationsPard ad Itrcig Gixe inraiol Feible AerCpace065Systes I p17t 9-2 INASA-CP-31t12-VOL.31 p 19 N91-28235 Astronomical Union Colloquium No 124 INS-C-065P- Ip17N1220 NASA-CP-30981 p 49 N91-16658

Multidisciplinary optimization of controlled space Upper Stages using liquid propulsion ,'d metallized STATE ESTIMATION

structures With global sensitivity equations propellants State estimation applications in aircraft flighit-data

I NASA-TP.3130j p 18 N92-11087 INASA-TP-319t1 p,10 N92-i7151 analyis A user's manual for SMACK

Fifth Annual Workshop on Space Operations Tenth Workshop for Computational Fluid Dynamic iNASA-RP-t12521 p 10 1,91-19082

Applications and Research (SOAR 199 1). volume 2 Applications in Rocket Propulsion. part 2 STATIC ELECTRICITY

INASA.CP-3127-VOL-21 p 41 N92-22324 (NASA.CP-3163-PT-21 p 27 N92-32245 The 1991 International Aerospace and Ground

Ongoing Pirogressmi Spacecraft Controls Tenth Workshop for Computational Fluid Dynamic Conference on Lightning and Static Electricity volume 1

[NASA-CP 10099) p 19 N92-28730 Applications in Rocket Propulsion, Part I I NASA-CP-3t06.VOL. 1 1 p 35 N91-32599

SPACECRAFT DESIGN I NASA-CP-3163-PT- 1 p 027 N92-32278 The 1991 international Aerospace and Ground

NASA Computational Fluid Dynamics Conference SPACECRAFT SHIELDING Conference on Lightning and Static Electricity volume 2

Volume 2 Sessions 7-12 HZETPN A heavy ion/nucleon transport codetfor space (NASA-CP.3106.VOL-2, p36 N91-32693

I NASA-CP-10038-VOL-21 p 4 N91-10866 radiations STATIC TESTS

Parametric trade studies on a Shuttle 2 launch system I NASA-TP-31 46; p 5t N92- 15959 Static thrust vectoring performance of noneaxSymromti-ic

architecture Orbital debris Technicai issues and future directions convergent -divergent nozzles with pos' exit yaw vanet

I NASA.TP.30591 p 14 N91-181 80 (NASA-CP-100771 p 49 N92-33478 I NASA-TP-3085I p 5 N91.2t059

Guidance, navigation. and control subsystem equipment SPACECRAFT STRUCTURES Wind-tunnel static and tree-f lght investigation of

selection algorithm using expert system methods Multidisciplinary optimization Of controlled space higho-angle-ot-a'iack stability and control characteristics of

[NASA-T'P-30821 p 42 N91-25624 structures with global sensitivity equations a model of the EA-6B airplane

Packaging, development, and on-orbit assembly options fNASA-TP-31 10] p 18 Nq2-t11087 [NASA-TP-3t941 p 7 N92-2527'6

for iarge geostatic'ary spacecraft Spa~e Transportation Materials and Structures STATIC THRUST

!NASA-TP-30881 p 17 N91-27182 Technology Workshop Volume I Executive summary Static thrust-vectoring prlxrrmarce of non'xisymmetric

Multidisciplinary Optimization of controlled space [NAlFA-CP-3148-VOL-1 I p 15 N92-22660 convergent-dvergent nozzles witi post-eelt yaw vanes

structures with global sensitivity equations INASA-TP-30851 p N91-2105ý

INASA.TP-31301 p 18 N92-11087 Stiffness a.,d strength tailoring in uniform space-fibring STATISTICAL CORRELATION

Beyond the Baseline 1991 Poednsof the Space truss structures Rsosso onr oatotlcadeecs

Station Evolution Symposium. Volume 1 Space Station NA -T320p30 92456 stresses

Freedom, part 1 Computational Strictures Technology for Aintrames and I(NASA- TP-30431 p3 7 N9t-1971 1

INASA-CP-t0083.VOL.I-PT.11 p 18 N92-17098 Propulsion Systems Correlatior and Prediction of dynamic huiman isolated

Beyond the Baseline 1991 Proceedings of the Space (NASA-CP-31421 p 31 N92-2591 1 joint strength from lean body mass

Station Evolution S npoosium Volume 2 Space Stsition Graphite/epoxy composite adapters for the Space (NASA-TP-32-- p p40 N92-26682

Freedom. part t Shuttle/Centaur vehicle STATOR BLADES

tNASA-CP-10083-VOL-2-PT-1 I p 16 N92-17768 I NASA-TP-30141 p 15 N92-31251 Design arid perlormance of contiolled -ditfuSion Stator

Cromputational Structures Technology for Airframes and Influence ot mass moment of inertia on normal modes compared withi original double-circular-arc Stator

Propulsion Systems of preloaded solar array mast I NASA-TP-28521 p 12 N92-22863

[NASA-CP-31421 p 31 N92-25911 I NASA-TP-32731 p 31 N92-33476 STATORS

Graphite/epoxy composite adapters for the Space SPACECRAFT TRAJEC1_!.;ES Design and performance 01 controlled-diftfusion Stator

Shuhtle'Centaur vehicle Flight Mechancs'Fstimation Theory Syninosium, 1990 compared with original double-circular-arc stator

tNASA-TP-30141 p 15 N92-31251 I NASA-CP-3t021 p) 14 N91-17073 INASA-TP-285e] p 12 N92-22863

SPACECRAFT ENVIRONMENTS SPACECREWS STEADY STATE

Measurement and Characterization of the Acceleration Microbiology on Space Station Freedom The effect of acceleration versus displacement methods

Environment on Board the Space Station I NASA-CP-31 081 p37 N91-1 8573 on steady-state boundary forces

I NASA-CP-3088] p48 N91-t2401 SPACELAB (NASA-TP-32101 p 30 N92-21457

SPACECRAFT EO~~tPMENT Measurement and Characterization of the Acceleration STROCPC ISN

Small Explorer Data System MILt-STD-11773 fiber optic Environment on Board the Space Station Effect of short~tetrn exposure In stereoscopic

bus I NASA-CP-30881 p 48 N91-12401 three-dimensional flight diospk /s on reali-world depth

!NASA-TP.32271 p 16 N92-26667 SPACELAB PAYLOADS perception

SPACECRAFT INSTRUMENTS Measurement and Charact rizafion of the Acceleration [NASA-TP-31 171 p I1 IN2-13065

Guidance, navigation, and conttrol subsystem equipment Environment on Board the Space Station STIFFENING

selection algonithim using expei. system methods INASA.CP-30881 p 48 N91-1 2401 Experinienta, behavior 01 graphite-epcvy Y-stiffened

J NASA TP-3082 j f, 42 N91 -25624 SPATIAL MARCHING specimens loaded in compression

Mission description and in-flight opera 01 ERBE An upwind-biased space marching algorithm for [NASA-TP-3 171 p p 30 N92-23t1t5

instruments on ERBS, NOAA 9. and NOAA t0 supersonic viscous flow STIFFNESS

spacecraft I NASA-TP-30681 p26 N91-18361 Stifl.ess and strength tailoring in uniform space filinig

[NASA RP-12791 p 32 N92-32t27 An efficient HZETRN is galactic cosmic ray transport truss structures

SPACECRAFT LAUNCHING code) INASA.TP-32101 p 30 N92-245456

Launch vehicie integration options tor a large Earth INASA-TP-3t47[ p 5t N92-22218 buckling behavior of Ilong symvmetrically laminated plates

sciences geostat-onoary platform concept SPECTRA subjected to combined ioad-ni;

I NASA-TP-30831 p15 N91 -27t180 Wind turbine acoustics I NASA.TP.3 1951 p 22 N92-251603

SPACECRAFT MOTION [NASA-TP-30571 p 44 N9t-16679 STOCHASTIC PROCESSES

A scheme to' bandoass filtering magneitnmeter SPECTROSCOPY Structural factoring approach tot analyzing stochastic

measurements to reconstruct tethered satellite skiprope Investigation of inicrostrluctural changes in networks

motion polyetherether-ketone films at Cryogenic temperatures by INASA-TP-30691 p 43 N9t1-t87,53

1 NASA-TP.I31231 p42 N91 -25629 positron lifetimne spectroscopy STRAIN MiEASUREMENT

SPACECRAFT ORBITS INASA-rP-30641 p 21 N9tI-t18216 Thermal and structural tests of Rene 41 nioneycorrb

Flinhiti Merna,-ir-siEstimation Theory Symposium, 1990 Low-energy positron flux generator tor microstructural integral-tank concept !or future soace tranisportation

[NASA CP-3102[ p 14 N91-17073 characterizatiron 0f thin films systems

SPACECRAFT POWER SUPPLIES INASA-TP-30741 p 27 N91-22538 I NASA-TP-3t4S I p 30 N92-24205

Space P;-otovolf arc Reseairch and Technology. 1989 SPEECH RECOGNITION STRATOCUMULUS CLOUDS

P3107[1 .AA p 19 N9t-i91s? Proceedings of the Second Joint Technology Worksnhop FR ceie is 8

space Transportation Propulsion Technology on Neural Networks and Fuzzy Logic, volume 2 1 NASA-CP-308J! p 34 N9t -10448

Symposium Volume 2 Symposium proceedings INASA-CP-10061-VOL-2[ p 43 N91-20811 STRATOSPHERE

I NASA-CP.3112 VOL 21 p 19 N91-28193 SQUEEZED STATES (QUANTUM THEORY) The atmosphieric effects of svratosr-ier: aircraft A

Space Photovoltaic Research and Technology Workshop on Squeezed States and Uncertainty tpclrve

Conference Relations iNASA-RP-12501 r33 N91-16466

lNASA CP 312t1 ip 19 N91-30203 f NASA-CP-31351 p 46 N92-22045 The atmospheric ~flects o1 strato ,,herc aircraft A

Automating a spacecrah electrical power system using STAGNATION POtINT current conosensus,

expert systems Stagnation-pointl heat-transfer rate predictions at INASA PIP-t1251 p 13~ N9t 16467'

NASA TP-316i p 20 N92-12052 aeroassist flight conditions SAM i eaguremrertS of ther polar %fiatoSpheirT r.osolr

I arigisoace structures and systems in the space station I NASA-TP-32081 p?27 N92,31281 Volume 9 Onlotyer 1982 -April 19A3

eria A bibliography with indexes (supplement 03) STANDARD DEVIATION 1 NASARP- 1244; jp 33 N4! Au,05

t NASA SP. 08510311 0 18 N92 22317 Strucrirgai deteirsinislic, %rfervo fatitors serfipcoo crilera irtenr-alronal Wvorksh~r [. 'irxlspsieii( Aeroso,

The 1991 NASA Aerospace Biane Workrshop and verification Meas,-rrreii~s Piripriti, 5,1iir

PINASA CP 314.211 p33 N92-2"140 INASA TP 320t yp 3 N92 19`1)"i3 NASA(-P" fi14 tP' 12 N9i 1 31r,'2P

A-32
SUBVEMrNDEX SURFACE PROPERTIES

The atmospheric effects of stratospheric aircraft A first Eighth D00/NASA/FAA Conference on Fribrous SUPERCRIT)CAL WINGS

Program report Composites in Structural Design paW 2 Lodgiudinal aerodynamic criaracleristicsi of a subsonic,

INASA-RP-127?I p 33 N92-19121 [NASA-CP-3087-PT-21 p 22 N92-32574 enegy-afficienit trnspiort configuration 4ni t,* National

Sixteenth International Laser Rladar Conference. part STRUCTURAL DESIGN CRITERIA Tranuonic Facilty

IStiffness and strength tailoring in uniform apace-tilling I NASA-TP-29221 P 6 N9 1 28143

t NASA-CP-3 ISO-PT- I I p 28 N92-29228 truss structures Installatiicn effeets of 9iti-mourned turofn

SAGE I data users guvie I NASA-TP-32101 p 30 N92-24546 nacelle-pylons oni a 1/I 7acals. twieinergwvs, lo-ing

INASA-FIP-12751 p 34 N92-33097 STRUCTURAL ENGINEERING transport model

STRESS ANALYSIS Spt Transportation Materials and Structures INASA-TP-3t6sl p 7N92. 19002

Plate and butt-weld stresses beyond elastic limit. Technioloigy Workshop Volume I Execuveo summary SUPERSONIC AIRCRAFT arrf

material and structural rcxjuling tNASA-CP.314e-VOtL-1 Ip 15 N92-22660 The atmospheric effectsOfsaOShrcjiatA

INASA-TP-30751 p 29 N91-16413 STRUCTURAL FAILURE current consensus A three-dimensionat filnile-elenient tyiermal/tiecttaticat t NASA-RP-1251t p 33 N91 1648? Developmen of nnegs aeroservoelssllc analysis analytical techniique tot higtt-peormance traveling wave A mebthod lr(r designing blended wing-body

program and correlation e-th test data '-waedg

NAA-P310 p 912tt NASA-TP-30611 p 25 N91-27436 (IOASA.TP-32611 p68 N92- 32480

Structural deterministic safety factors selectionr critena Structural deterministic safety factors selection criteria Survey and snalysis of research on suersonic

an cAa.tio201p3 and verificationi drag-due-to -lift mrrrintuatoon with recon-mendatons for NAA.P-23Ip3 92-19355 [NASA-TP-32031 p 30 N92-19355 wing design

Thermal and structural tests of Rene 41 honeycomb STRUCTURAL RELIABILITY (NASA-TP-320?J P 9 N92-33656 integral-tank concept for future space transportation Structural determnirsatic safely factors selection criteria SUPERSONIC COMBUSTION RAMAET ENGINES

systems and verification A parametric exiperrimenrtall inwasigation of a sciamWe

JNASATPý31451 p 30 N92-24205 INASA-TP-32031 p30 N92-i9355 nowxe at Mach 6 with Vraoi an argon Of ax used fot

Effect of type of load on stress analysis of thin-walled STRUCTURAL STABILITY exhaust sinsilation

ducts Suckling and vilbration anatysis of a simply suppore INASA-TP-30481 p4

l NSI-t699

INASA-TP-32481j p 31 N92-26669 column with a pweewise constant cross section SUPERSONIC DRAG

STRESS CONCENTRATION INASA.TP-30901 P29 N91-20503 Survey an analysis of reseatrch on suersonic

Stress concentrations tor straight-shank and STRUCTURAL VIBRATION drag-due-to-fllt mnimiza~tioin with recommendats ion s for

countersunk holes in plates subjected to tension, bending. Free vibirations o1 thin-wetted semicircular win design*

andS-P39 pi pl31ading9 graphllteepoxy composite frames I NASA-TP-32021 p 9 N92-33656

STES INTES ITY-392 pACTORS299 I NASA-TP-30 0o p29 N91-1 3750 SUPERSONIC FLOW

STRES INENSIY FATORSNavier-Stokas; and Euler solutions tot leie-aide flows over Analysis and prediction of Muhfipte-Site Damage (MSD) Buckling and vikiattori analysi of a simlply supre supersoni defta wings A correlation with experimerr

tat igue crack growth column with a piecewise constant cross section I NASA-TP.30351 p 4 N9l -i 340t

[NASA-TP-3231 p p31 N92-31279 INASA.TP-30901 p 29 N91-20503 An upwindl-buased space marching algorithm for

Apiplications of FEM and SEM in two-dimensiornal Rotordyriarric Instability Problems in High-Performance supersonic viscous flow

fracture mechanics problems Turboirnachwiney. 19 (NASA-TP-30681 p 26 N91 -111381

[NASA-TO-32771 p 31 N92-31280 I NASA-CP-31221 p 28 N92-14346 Evaluation of a techrelue to generate artilicially

STRESS-STRfAIN RELATIONSHIPS SUBDVISIONS thickiened boundary layers in supersonic anid hypersonic

Plate and butt-weld stresses beyond elastic limit, Earth observations and global change decision making flow

malenal and structural modeling A special bibliography. 1991 INASA-TP-31421 p 6 N91-26136

NASA-TP-30751 p 29 N91-16413 [NASA-SP-70921 p 32 N91-30586 The natural flow wing-desig concept

Improved accuracy tor finite element structural analysis SUBSONIC FLOW INASA-TP-31931 p 7 N92-25202

via a new integrated torce method J-85 pet engine noise measured in Itie ONERA StI wind Supersonic Throughtlow Fan Test Facillity, at NASA

I NASA-TP-32041 p 30 N92-22227 tunnel and extrapolated to for field Lewis Reselarch Center

STRUCTURAL ANALYSIS I NASA-TP-30531 p45 N91-19823 INASA-TP.30381 p 13 N92-3i6-a0

Free vilbrations ofthi~n-walled semicircular Numerical study 0f the aerodynamic effecs of using SUPERSONIC SPEED

graphite-epoxy composite frames sulfur hexaftuonde as a test gas in wind tunnels Experimental investigattion of porous-Iboor effects on

INASA-TP-30101 p 29 N91-13750 [NASA-TP-30861 p 5 N91-22070 cavity ftow fields at Supersonic speeds

Plate and butt-weld stresses beyond elastic limit, Effects 0f yaw angle and Reynolds number on I NASA-TP-3032I JP5 N911t9D42

material and structural modeling rectangular-box cavities at subsonic and Itranscinic Paelo methods An introduction

INASA-TP-30751 p29 N91-16413 spesINASA-TP-29951 p5 N91.19058

Nineteenth. NASTRAN (R) Users'Colloqium [NASA.TP-3099j p 5 N91-27124 Measurements of forces, moments. end pressures on

1 NASA-CP-31 it I Ip 29 N91-2056 SUBSONIC SPEED a generic store separatin from a box cavity at supersonic Improved accuracy for finite element structural analysis Panel methods An introduction speeds "va a new integrated force method I AAT-95 SNi106 INASA-TP-31t01 p 6 N92-10005

I NASA-TP-3204 I p 30 N92-22227 NST-29JP N1-1 Influence of atiroil geometr on delt "in eadcing-edge

Twentieth NASTRAN (Rf Users Colloquium Longitudinal aerodynamic characteristics of a subsonic, vrices and roles-finduced aerodynamics at supersonic

I NASA-CP-31 451 p, 30 N92-24324 energy -efficient transport configuration in the Nationial Speed

Ouckling behavior of long symmetrically laminated plates Transonic Facility IAspeeds 01 N2203

subjected to combined loadings INASA-TP-29221 p 6 N9t-28143 Supersonic Throughitjow Fan Test Facility at NASA

!NASA-TP-3t951 p 22 N92-25160 SULFUR FLUORIDES LwsResearch Center

Computational Structures Technoliogy to( Airframnes and Numerical study 0f the aefrodynamioc effects 0f using I NASA- TP-30381 p 13 N92 31t640

Propulsion Systems sulfur heasalucirctri as a test gas in wind tunnels SUPERSONIC TEST APPARATUS

INASA-CP-31421 p 31 N92-25911I INASA-TP-30861 p5 N91-22070 Supersonic Throughflow Fan Test Facility at NASA National Educators' Workshop Update 1991 Standard SUN Lewis Research Center

Experiments in Engineering Matenials Science anid Climate Impact of Solar Variability I NASA-TP-30381 IP 13 N92-3 1640

Technology I NASA-CP-3086 I p 50 N91 -12456 SUPERSONIC TRANSPORTS

I NASA-CP-3151 Ip 24 N92-30263 Atlas of the Earth's radiation budget as measured by The atmospheric effects of stratospheric aircraft A

Graphite/epoxy composite adapters for theo Space Nimbus-?. May 1979 to May 1960 topical review

Shuttle/Centaur vehicle INASA-RP-12631 p 35 N91-24720 I NASA RP.-1250) p 33 N91-16a6%

I NASA-TP-3014 ] p 15 N92-31251t SUPERCOMPUTERS Span reduction eoffects on the "autte charactenistics of

Eighth 000/NASA/FAA Conference on Fibrous NASA Computational Fluid Dynamics Conference arrow-wing Supersonic transport configurations

Composites in Structural Desin, part 2 Volume I Sessions 1-6 INASA.TP-30771 Pt t N91-2t 127

INASA-CP-30S7-PT-2I p 22 N92-32574 I NASA-CP- 10038-VOL-1I I p 4 N91-t0839 A loudnvess calculation procedure applied to shaped

STRUCTURAL DESIGN NASA Computational Fluid Dynamics Conference sonic boom$

Or,-0rbit structural dyranaic perfomance of a t 5-meter Volume 2. Sessions 7-t2 1 NASA -TP-31341 p 45 N92t11765

microaveradiomete anen p (N1111 NASA-CP-t0038-VOL-21 p4 Ngt 1086 Computational Structures Technology tor Airfirsams end

IAAeroProp041or p 6 91 771 SUPERCONDUCTING MAGN4ETS Propulsion Systems erpouso191international Symposium on Magnetic Suspension I NASA CP-31421 p 31 N92-259i I pNS-PiO3 12 N9t-20086 Tehooy atISUPERSONIC TURBINES

Optimization of composite sandwich cover panels (NASA-CP-3t52-PT-t I p IS N92-2772t Supersonic Throughllow Fan Test Facility at NASA

subjected to compresarve loadingsLeiRsarhCnl

INASA-TP.31731 p)21 N92-20679 International Symposium on Magnetic Suspension LeIs Research338 Center-3t

Large Space structures and systems in the space statio Techniology part 2 SUPERSONIC33 WIN pT1UNNELS64 era A bibliography with indexes (supplement 03) 1INASA-CP-3t52-PT-21 p 18 N92-27788 SUESupronic WINOuhfo TUNN stELSh t AS

tNASA-SP-7085(03)1 p 18 N92-22317 SUPERCONDUCTIVITY Lawis Research Center

Stiffness and strength tailoring in uniform space-filling Aerospace Applications 0f Magnetic Suspension INASA.TP-30301 p 13 N92-31640

truss structures Technology, part I SURFACE GEOMETRY

INASA-TP-32t01 p 30 N92424546 (NASA-CP-10066-PT-1 I p 17 N91-21 188 A method for determining spiral-bevel gear tooth

Computational Structures Technology for Airframes. and Aerospace Applications of Magnetic Suspension geometry for finite element analysis

Propulsion Systems Technology. part? 21NASA.TP-30961 p 20 N92-t0195

[NASA-CP-31421 p 31 N92-25911 INASA-CP-t0066-PT-2I p 17 N9 1-21203 SURFACE PROPERTIES

Eighth DOD)/NASA/FAA Conference on Fibrous International Symposium on Magnetic Suspension Software Suirface Modieling and Grnd Generation

Coimposirtes in Structural Design, part I Technology, part 2 Steernog Commnittee

I NASA-CP-3087-PT-1 I p 22 N92,32513 (NASA-CP-3152-PT-21 p tO N92-27788 INASA-CP-31431 P 4

2 N92-24397

A-33
SURFACE REACTIONS SUBJECT INDEX

SURFACE REACTIONS SYSTEMS STABILITY TENSILE TESTS

AMSAHTS 1990 Advances in Materials Science and A methodology tot computing uncertainty bounds of Stress concentrations tof straight shnk, and

Applications of High Temperature Superconductors murltivariable systems based on sector stability theory Coririteruns holes in pistes subj~ected to tensiori bendhing

INASA-CP-31001 p 22 N92-21605 concepts and pin ioading

Gibbs free energy ofreactions involvingSiC.S61,N4, H2, INASA-TP-31661 p 13 N92-21410 INASA TP-31921 p 31 N92 ?5i997

and M20 as a function of temperature and Pressure TERMINOLOGY

INASA-TP-32751 P 23 N92-31278 NASA Thesaurus supplementl A tour part cumulative

SURFACE WAVES T Supplement to the 1968 edition of the NASA I hesaurus.

Diffracted and head waves associated with waves on (supplement 41

noriseparable surfaces TAL NASA-SP.7064 SUPPL-4) pal N9itOOO0A

(NASA-TP.31691 p 7 N92-20545 T LES (DATA)NAATearsuperetAfrprtcmlie

SURFACES SAGE 1 data user's guid NSuplmn Tohesa 90u 8edition ol A oth NaSA cTnsmatius

Workishop on Grid Generation and Related Areas (NASA-RP-1275j p 34 N92-33097 (Supplement toteI5) eiinofteNS hsuu

[NASA-CP-t 00891 p 12 N92,25712 TAKEOFF I NASA-SP-7064,SUPPL-51 p4 7 N91 19%2

SURVEYS Annoyance caused by aircraft en route noise TEST FACILITIES

Survey and analysis of research on supersonic [NASA-TP-31651 p 45 N92-?0479 Aviaton Safety'iAutomation Program Conlferece

drag-due-to-lift mininization with recommendations tor TAPERING INASA-CP,30901 p 9 N91-10936r

wing design Buckling and vibration anatysis ot a simply supported TEST STANDS

INASA-TP.32021 p 9 N92,33656 column with e piecewise constant cross section Development of a lullscale transmission testing

SURVIVAL INASA-TP.30901 p 29 N91 .20503 Procedure to evaluate advanced lubricantS

Track structure model of cull damage in space ftight TECHNOLOGIES I NASA-TP-32651 p 28 N92 30396

[NASA.TP.3235J p 39 N92-34154 Nationat Educators' Workshop, Update 1980 Standard TESTS

SWEPT WINGS Experiments in Engineering Materials Science and NASA Wallops Flight Facility Air-Sea Interaction

Detailed flow-field measurements over a 75 deg swept Technotog Research Facility

delta wing I NASA-CP.30601 p20 N91-20707 INASA-AP-12771 p 36 N92 25981

(NASA.TP.29971 p4 N91-t8030 TECHNOLOGY ASSESSMENT THERMAL ANALYSIS

Planform curvature effects on flutter ctiaractenistics of NASA-LaRc Flight-Critical Digitall Systems Technology Thermal-distortion analysis of a spacecraft bcx truss n

awring with 56 deg leading-edge sweep and panel aspect Workshop geostalionary orbit

ratioof 1 14 NASA-TP021P1 9-40 AAP-30541 p 1b N9t1t'C041 rati of1.14NAS-CP-0021 P 1 91 2200 A ihrea-dirimensional tinite-elernent thenrnalmechsriicai

I NASA-TP-31161 p 11 N92-13054 Advanced Hypervelocity Aerophysics Facility analytical technique for high performance traveling wave

The natural flow wing-dlesign concept Workshop tbes (NASA-TP-31931 p 7 N92-25202 [NASA-CP-100311 p 13 N91-24211 INAAT-01I U-73 2 

SWITCHES The 1990 NASA Aerospace Battety Workshop Thermal and Structural tests of Rene 4t nlorreycomb

Reliability of a Shuttte reaction timer I NASA-CP-31191 p 20 N92-27130 integral-tank concept tor future space transportation

[NASA-TP-31761 p 40 N92-16562 TECHNOLOGY TRANSFER systems

SWITCHING Technology 2000 volume 2 JNASA-TP-31451 P3 9-40

Space Communications Technology Conference: [NASA-CP-3109-VOL-21 p 52 N91-24041 A simplified method tot thermal analysis of a cow leading

Onboard Processing and Switching Technology 2001 The Second National Technology edge Subject to intense local Shock-wave-interference

(NASA-CP-31321 p 25 N92-14202 Transfer Conference and Exposition,. volume 1 heating

SYNCHRONISM [ NASA-CP-3 i36-VOL 1)I p 52 N92-22423 (NASA-TP-31671 p27 N9224797

Experimental validation of clock synchronization Technology 2001 The Second National Technology THERMAL CONDUCTIVITY

algorithms Transfer Conference and Exposition. volume 2 CalCute' 7Its and curve fits of thermodynamic and

( NASA-TP-32091 p4A2 N92-27589 I NASA-CP-3136-VOL-21 p 52 N92-22676 transport properis for equilibrium air to30000 K

SYNCHRONOUS PLATFORMS TECHNOLOGY UTILIZATION )NASA-AP-1260) P 26 N92-1 1285

Thermal-distortion analysis of a spacecraft box truss in Aerospace Applictions of Megnetic Suspension THERMAL CONTROL COATINGS

geostationiary orbit Technology, part I LOEF 69 Months in Space First Post Retrieval

INASA-TP-30541 p 16 N91-11041 (NASA-CP-t0066-PT-1 I p 17 Ng 1-21 188 Symposium, pent 3

On-orbi structurall dynamic performance of a I15-meter Technology 2000, volume I NASA-CP-3134-PT-3i p 52 N92-27083

microwave radiometer antenna I NASA-CP-3109-VOL- I I p 52 N91-23021 THERMAL EMI3SION

tNASA-TP-3041J P 16 N91-1 7114 Technology 2000. volume 2 Optical measuremtents on soliospecimensof solidrocket

Rigid-body-control subsystem sizing for an Earth science (NASA-CP-3t09-VOL-21 p2N1401 motor exhau';t and solid rocket motor slag

geostattoriary platform TELECOMMUNICATION THERMAL PROTECTION

I NASA-TP-30871I p 17 N9t -22302 The 22nd Annual Precise Time and Time interval (PiTt) Numerical studies of convective cooling tor a locally

Launch vehicle integration options for a large Earth Applications and Planning Meeting heated skin

sciences georstationary platform concept INASA-CP-31 161 p44 N91 -25755 (NASA-TP.3100I p 26 N91-22509

[NASA.TP-30831 p 15 N91-27180 TELEOPERATORS, Payload bay doors and radiator panels famikiarization

SYNCHRONOUS SATELLUTES Human Machine Interlaces for Teteoperators and Virtual handbook

packaging, development, and on-orbitl assembly options Environments Conference I NASA-TM-t07?93; p 15 N92 20676

for large geoxtationary spacecraft JNASA-CP-1100711 p 40 N92-11638 THERMAL SIMULATION

)NASA-TP-30881 P 17 N91-27182 TELER0O30TICS Sixteenth Space Simulation Conterence Confirming

SYSTEM EFFECTIVENESS The effect of bandwidth on teterobot System Spaceworthiness into the Next Millennium

Experimental and analytical evaluation of efficwncy of Performance JNASA-CP-30961 p 17 N91-19126

helicopter ptanetary stage JNASA-TP-31521 p28 N9t-30540 THERMAL STABILITY

INASA-TP-30631 p28 N91-t2956 Automation and Robotics for Space-Based Systems. High -temperature durability considerations try HSCT

SYSTEM IDENTIFICATION 1991 comrbustor

Identification of linear systems by an asymptotically [ NASA-CP- 100981 p 43 N92-27763 I NASA-TP-31621 p 23 N92 17070

stable observer TEMPERATURE CONTROL THERMODYNAMIC EQUILIBRIUM

[NASA-TP.31641 p 31 N91-26537 LDEF: 69 Months in Space First Post-Retrieval Aeroacoustic anidaerodtynamic applications of the t"er

SYSTEMS ANALYSIS Symposium, part 3 Of nOn~equikbinum thermodynamics

Benefits fromt synergies and advanced techniologies for I NASA-CP-3134-PT-31 p 52 N92-27083 I NASA-TP-31 181 p 26 N91-25352

an advanced-technology space statin TEMPERATURE DEPENDENCE Calculations and curve fits ot thermodynamic and

I NASA-TP-30671 p 14 N91-20177 Gibbs tree energy of reactions involving SiC, S6144, H2, transpor properties for equilrbnum air to 30000 K

SYSTEMS EN4GINEERING and H20 as a function of temperature and pressure I NASA-Rp-t12601 p 26 N92-1 1285

Space Transport ationi Avionics Technology Symposium, fNASA-TP-3275 I p 23 N92-31 278 THERMODYNAMIC PROPERTIES

Volume 2. Conference Proceedings TEMPERATURE EFFECTS Electrochemical studies of corrosior inhibitors

INASA-CP-3081-VOL-21 pit N91-17020 Oxidation characteristics of Ti-25AI-tONb-3V-lMo INASA-TP-30661 p22 1491,1t7208

The 1991 Goddard Conference on Space Applications intermetaltic, alloy AMISAHTS 1990 Advances in Matenials Science and

of Artificial Intelligence INASA-TP-30441 p 22 N91-13522 Applications of High Temperature Superconductors

INASA-CP-31 101 p 43 N91-22769 Investigation of microstructural changes in INASA-CP-31001 p 22 N92-21605i

NASA LaRc Fltight-Critical Digital Systems Technology polyethefelher- ketone films at cryogenic temperatures by THERMODYNAMICS

Works~hop positron lifetime spectroscopy Gibbs free energy of reactions involving StC. Si3N4. H2.

I NASA.CP- 100281 pI it 1'1-24200 1NASA-TP-30641 p2l N91-18216 and H20 assa function of temperature and pressure

Flight tests with a data link used for air traffic control The 23 to 300 C deomagnetization resistance of I NASA-TP-3275) p 23 N92-31 278

information exchange samarium-cobalt permanent magnets THERMOPLASTIC RESINS

I NASA-TP-31351 p 11 N9 1-31143 1 NASA-TP-31191 p 25 N92-11252 Compression behavior of graphite-thermocplastic and

Beyond the Baseline 1991.ý Proceedings 01 the Space Effect of temperature and gap opening rate on the graphite-epoxy panels with circular holes or impact

Station Evolution Symposium. Volume 2: Space Station resiliency of candidate solid rocket booster 0-ring damage

FreedOmr. part 2 materials (NASA-TP.30711 p 21 N91-t8Z 15

1 NASA-CP- 10083-VOL-2-PT -21 p 18 N92-17348 INASA-TP-32261 p 23 N92-27194 THESAURI

SYSTEMS INTEGIPATtON TEMPERATURE PROFILES NASA Thesaurus supplemrent A tour part cumulative

Space Transportation Aviontics Technology Symposium SAM 2 measurements of the polar stratosphenc aerosol supplement t0 the 1988 edition of the NASA Thesauru

Volume 2. Conference Proceedings Volume 9 October 1982 - April 1983 (supplement 4)

INASA-CP-3081-VOL-21 pit N91-t7020 JNASA-RP-112441 p 33 N9t-18505 I NASA- SP- 7064- SUPPL-41 p 47 N91-ý10804

A-34
SUBJECT INDEX TURBINE PUMPS

NASA Thesaurus supplement A four pait cumulative Experimental measurement of th~e orbital paths of Effects of yaw angle and Rleynolds niimpe on

supplement to the 1988 edit ion of the NASA Thesaurus particles secimenting within a rotai-ng viscous fluid as rect-angularibox cavities at subsonic an tiansornic

(supplement 5) influenced by gravity speeds

I NASA-SP-7064-SUPPL-5l p 47 N91-19962 [NASA-TP-32001 p 40 N92-28897 I NASA.T P30g99 p 5 N9t-27124

THIN FILMS TITANIUM ALLOYS Calculat~on of unsteady transonic flows wmrlr uid

Low-energy positron flux generator for mcrostructural Oxidation characteristics of T-25Af1-tNb-3V tMo soetatiaon by viscousrinvsc~d ,rieractkon

cheracterizafion of thin films intermetlaffic alloy INASA-TP-31971 p 7 N92 2BA77

I NASA.TP-3074 J p 27 N91-22538 INASA.TP-30441 p22 N9irt3522 TRANSONIC FLUTTER

THIN WALLED SHELLS Surface effects on hydrogen permeation through Span reduction effects on the flutter craacferstics of

Diffracted and head waves associated with waves on Trl I4Al 21Nb alloy arrow-*ing supersonic transport configufrationis

nonseparable surfaces I NASA-TP-3091 p23 N91ý20?656 I NASA TP 30771 p1If N91 211??

I NASA.TP-3t691 p 7 N92-20545 TOLERANCES IMECHANICS) Pafr uvtr fet nfutcaarsiso

THIN ViLL An examinatin of the damage tolerance enhrancement Pa wngtoim 56rva"ur leffngeteswe ond nrce;raspct potfr o

Effect of type of load on stress analysis of thin-walled of carbon/eporxy using an outer lamina of specfra (R)( fal wif wit 56dglaigdesepaidpnlapc

ducts I NASA-TP-31601 p 21 N92-1t142 iNafioof 14N2135 316 p 

1 NASA-TP-32481 p 3t N92-28669 TOLLUIEN-SCHLICHTING WAVES (AAT-16 i 9 35

THRE DMESIOALBODESA weakily nonlinear theory tor wave-vortes interactions TRANSONIC SPEED

Three-iesoa DlESO aLe BO ndIES omaio in curved channel flow A method for the dlesign of transonic flexible wings

Thre-imnsona lse wndo frmtin NASA-TP-31581 p 7 N92-19175 (NASA-TP 30451 p 10 N91-t4323

INASA-RP-12801 p 14 N92-30307 TORQUE TRANSONIC WIND TUNNELS

THREE DIMENSIONAL FLOW The validation of a human force model to predict dynamic Comparison of a two-dimensional attaptive-wali

Three-component laser anemometer measurement forces resulting from multi-1otrnt motions technique with analytical wall inerference correction

systems I NASA-TP-32061( p 40 N92-26538 techniques

I NASA-TP.30801 p5 N9t-19057 Correlatin and Prediction of dynamic human isolated (NASATP 31321 p 7 1492.20494

Calculation of unsteady transonic flows with mild joint strength from lean body mass TRANSPORT AIRCRAFT

separation by viscous-inviscid interaction JNASA-TP-32071 p 40 N492-26682 Eftect of location of alt-mourted nacelles on the

1 1 SA-TP-319 71 p 7 N492-28477 TOTAL OZONE MAPPING SPECTROMETER tongifudinall aarodyn~arnic: characteristics of 8 nig-wing

THREE DIMENSIONAL MODELS Nimbus.? TOMS Antarctic ozone atlas August - transport airplane

A three-dimensional finite-element thermal /mechanical December 1990 [ NASA-TP-3C471 p 4 N49113402

analytical technique for htgh-performancii traveling wave INASA-RP- 126.41 p 35 N9 1-26651 The aitmosphenic effects of stratospheinc aicraff A first

tubes TOTAL QUALITY MANAGEMENT program report

[NASA-TP-3081 p p25 N491-27436 The role of failure/Problems in engineer~ig A I NASA-RP-12721 p 33 N492.19121

A method for determining spiral-bevel gear tooth commentary of failures experienced t essons opined Applications of a direculterative design method to

geomefr for finite element analysis I NASA-TP-32131 p 24 N492-22235 complex transonic configurations

I NASA-TP.3096 ] p28 N192-10195 TOXICITY INASA-TP-32341 p 8 N92-33484

Stress concentrations for straight-shank and Space Station Freedom Toxic and Reactive Materials TRANSPORT PROPERTIES

countersunk holes in plates subjgected to tension bending. Handling Calculations and curve fits of okermodynamic and

and pin loading [NASA-CP-30851 p48l N91- 15930 transport Properties for equilibnium fi - 'o 30000 K

I NASA-TP.31921 pt 31N92-25997 TRACKING NETWORKS (NASA-RP-12601 26 N492-11f285

THRUST REVERSAL Proceedings of the 23rd Annual Precise Tine and Time TRANSPORT THEORY

Static performance of a cruciform nozzle with muttiaxis Intrval (PTIt) Appfications and Planning Meeting Berichiarfi solutions for the galactic heavy-ion transport

thrust-vectoring and reverse-thrust capabiltities I NASA-CP.31ISP p 44 N492-3331 0 equations with energy anid spatial coupling INASA-TP-31881 p 7 N92-23095 TRAILING EDGES INASA.TP-31t21 p 44 1492 13756

TRSVETRCNRLNACA 0015 wing pressure and trailing vorte Tasotmtosaditrcin o pc

TRSVETRCN OLmeasurements Tasotmtosaditrcin o pc

Static thruat-vectoning performance of nonairisymmefnic INASA.TP-3151 ( p86 N92,10981 radiations

convergent-divergent nozzles with post-exit yaw vanes TRJCOISIAAR-15(p119-55

I~~~ NAAT-05 5 N491-21 059 Trajectory titting in function space with application to An efficient HZETRN (a galactic cosmic ray transport

Aeropropulsive characteristics of canted twi anallytic modeling of surfaces corlel

pitch-vectoring nozzles at Mach 0 20 to 1 20 1 NASA-TP-32321 p 8 N492-30747 INASA-TP-31471 p 51 N492-22218

INASA-TP-30601 p 5 N91-22069 TRAJECTORY CONTROL TRAPPED PARTICLES

Static Performance of a cruciform nozzle with multiasis Applicatiton and flight test of linearizing transformations Proceedings of the 23rd Annual Precise Time and Time

thnust-veclonng and reverse-thrust capabilities using measurement feedback to the nonlinear control Interval IP771) Applications and Planning Meeting

INASA.TP-31881 p 7 N92-23095 problem I NASA-CP-31591 p 4A N92-33350

THRUST-WEIGHT RATIO I NASA-TP-3t54) p 12 N91-30154 TRAVELING WAVE TUBES

Parametrnc trade studies on a Shuttle 2 launch system TRANSFER FUNCTIONS A three-dimensioinal finite-element thermalirnechanica

architecture On the formulation of a minimal uncertainty model for anafytical technique for high-performance traveling wave

(14ASA-TP-3059) p 14 N491-18180 robust control with structured uncertainty tubes

THUNDERSTORMS I NASA-TP-3094 ] p 13 N492-10027 I NASA-TP-308t1 p 25 N491-27436

Inertial oscillation of a vertical rotating draft with TRANSITION FLOW TRIB3OLOGY

application to a supercell storm Modeling of the heat transfer in bypass transitional The 25th Aerospace Mechanisms Symposium

[NASA-TP-32301 p 36 N92-331482 boundary-layer fltows I NASA-CP-31 t31 p 30 N491-.24603

Inertial oscillation of a vertical rotating draft with IHASA-TP-3I701 p27 N492-11t299 Fundamentals of fluid lubricatior

application to a supercell storm: Video supplement to TRANSMISSIONS (MACHINE ELEMENTS) INASA-RP-12551 p2 ?8 491-30531

NASA Technical Paper 3230 Expenimental and analytical evaluation of efficiency of TROPOSPHERE

(NASA-TP-3230-VIDEO-SUPPLI p 36 N92-34246 helicopter planetary stage Sixteenth international Laser Radar Conference, part

TIME INASA-TP-30631 p28 1491-12956 2

The 22nd Annual Precise Time and Time Interval (PTTI) Development of a full-scale transmission testing [NASA-CP-3158-PT-21 p 28 N92-3101 3

Atppitcations and Planning Meeting procedure to evaluate advanced lubricants TRUNCATION ERRORS

INASA-CP-31 161 p 44 N491-25755 (NASA-TP-32651 p 28 N492-30396 The effect of acceleration versus displacement methods

TIME DIVISION MULTIPLEXING TRANSMITTERS on steady -state boundary forces

Dearination-direcled, packet-switching architecture for Propagation effects for land mobile satellite systems INASA-TP-32181 p 30 N492-21457

30/20-GHz FDMA/TDM geostationary communications Overview of expeninenta) and modeling results TRUSSES

satellite network INASA-PP-12741 p 25 N492-20404 Thermal-distortion analysis of a spacecraft boo, !nisI NASA-TP-3201 I p 16 N492-19762 TRANSONIC FLOW geostalionary orbit

TIME MEASUREMENT Transonic flow analysis for rotors. Part 3 1 NASA-TP-30541 p 16 N149ff l41

The 22nd Annual Precise Time and Time itlerval (PTTI) Three-dimensional, quasi-steady, Euler calculation Stiffness and strength tailoring in uniform space-filling

Appfications and Planning Meeting NS-P271p3 9-007 tustrcre

I AAC~ 11p1 9415 Prediction of effects of wing contour modifications on (NASA-TP-321 01 p 30 N492-24546

Positron lifetime measurements in chiral nemtatic liquid low-speed maximum lift and transonic performance for the Development of a truss joint for robotic assembly of

crystals E-1 icatsaesrcue

I NASA-TP-31 22) p46 1492ý10677 ENAA-68 airraf 306 space90 [N sAtP-1ctures9-297

Experimental validation of clock synchronization p4ig [autoTmated SoftwTPare6 for-190 assmbl of9-russ

algorithms Relative efficiency and accuracy of two Navier-Stokes sotwactres dsg o uoae sebyo rs

I NASA-TP-32091 p 42 N92-27589 codes for simulating attached transonic flow over wings struc.tures 1p43N2-87

Proceedings of the 23rd Annual Precise Time and Time (NASA-T-P3061 ( p26 N1.9f-7310 TUNASATEN18 4 19-8

Interval (PTTI) Applications and Planning Meeting Wall -interference assessment and corrections for Low-energy positron flux generator for microstructural

(NASA-CP-3159( p 44 N492-33350 transonic NACA 0012 airfoil data from various wind characterization of thin films

TIMING DEVICES tunnels I NASA-TP-30741I p 27 N491-22538

Reliability of a Shuttle reaction timer I NASA.TP-30701 p 5 N91-20043 TURBINE BLADES

I NASA-TP-31 761 p 40 1492-16562 Numerical study of the aerodynamic effects of using Laser anemometer measurements and computations in

TISSUES (BIOLOGY) sulfur hesaffuoride as a leaf gas in wind tunnels an annular cascade of high turning core turbine vanes

Anairq of qm"vulnduced pirrtlcle molion and fluid I NASA-TP-10818 ni ;NIi22070 INASA TF-321,- p 8 N92-28980

perfusion flow in the ffASA-deSignpd rotating Transonic Symposium' Theory. Application and TURBINE PUMPS

zero-head-space tissue culture vessel Experiment. volume 2 Limit cycle vibrations in turbomachinery

fNASA-TP-31431 p 24 N492-13340] (NASA-CP-3020-VOL-21 p 5 N91-24132 I NASA-TP-318ti I p20 N492,14108

A-35
TURBOCFAN AIRCRAFT SUBJECT INDEX

TURBOFAN AIRCRAFT ULTRAHIGH FREQUENCIES VENTURI TUBES

Annoyance caused by advanced lurbprop aircraft Propagation effects for land mobile satellite systems Venturi air10 rill-oaurnm ejectors for high- Vovrine

flyover noise Comparison of different propeller Oveirview ofI experimental and modelling results atmsospheric samping on aircraft platforms

configurations (NASA-RP- 1274j p 25 N92-20404 INASA- TP 3 1831 p11 N92 20546

INASA.TP-31041 p 45 N92-1 1758 ULTRAMIGH VACUUM VERTICAL AIR CURRENTS

Annoyance caused by aircraft en route noise Surface effects on hydrogen permeation through Inaiblt~ oiscillation of a veritcal iotal-lig dirol wxith

[NASA.TP-3t651 p 45 N92-20479 T.-14Al-21f~b alloy applicationi to a superceri storm V'ideo sjippeiemni to

TURBOFAN EN4GINES I NASA-TP.3t09] p23 N91-20266 AAlcnclPpr33

Installation effects o1 wing-mounted turbofan ULTRASONIC FLAW DETECTION tNASA- I P-3230-V;DEO-SUPPI. p 36 1,92342415

nacelle-pylons on a 1/17-scale, twinn-engine. lo*-wing Second Conference on NDE for Aerosace VERTICAL LANDING

transport model Requirements Static internal performance it ~erilfal and reai nozzle

INASA-TP-31681 p 7 N92-19002 INASA-CP.309t I p 16 N91-18169 conrcepts for short taireori and ,,enCsl landing airciat

TURBOFANS efcs fwn-ontd troa UNIQUENESS THEOREM I NASA-TP-31031 p N92-t097?5

insalltio o efort wig-muntd lrboan Shock wave interaction with en abrupt ares change VIBRATION

nacelle-py~ons on a 1/17-scale. twin-engine, low-wing INASA-P3 313 1 p 6 N91-27140 Lim~it Cycle vibrSatos in. tirbomachinery

transport model UIEST ESI NASA-TP-3 1811 p20 N92-t4105

JNAAýT-3661p TN9-1902 The Federal Conference on Intelligent Processing VIBRATION DAMPING

Supersonic Throughtlow Fan rest racility at NASA EquipmentDeinocntllasfrluerupesonbedn

LNawsAT-3 pes13rch2Centel INASA-CP-31381 p 52 N92-24987 thre aerodynamic energy concept and comparisons with

TURASOA-T-339N13N9R364 UNIVERSITY PROGRAM other design methods TUSMCIEYJoint University Program for Air Transportation I NASA TP,30561 p 29 N9t-10328

Three-component laser anemometer measurement Research. 189ý990 Fourth NASA Worathop on __.riputational Control or

sysA-tems 0 9 o ( NASA-CPA3O51 P7 1 N9t- 19024 Flexible Aerospace Systems, lonr 2

CompuA-tionAl lud Dyamc Syp5su N11on Technology for the Future In-Space Technology [NASA-CP.t0065.PT 2] p 17 fv91-22331

Aeopropulatoa lid DnmciSmoimon Experiment s Program, part 1 A Scheme Ifor baindpass fittering magnetomelef ]ASA-CP-3078]i pI N~-16 NASA-CP- I0073-PTt p t 14 N91-27177 measurements to reconstruct tethered satellite sorupý* INAA-P-071 S 912162 Technoiogy for the Future in-Space Technology motion

Limit cycle vtbrations in turbomachniery Experiments Program, part 2 1NASA TP-31231 p 42 N9r-25629

INASA-7P-3181 1 p20 N92-14108 JAAC107-T2 14N1778 Rocordynamric Instability, Proý.emns in High%-Perofomance

Tulrionsa tchInstablit Prbes nHghProtac Joint University, Program lot Air Transportation Turbornacturinery, 1990 TubrahnrIMReseoarch 1490-149i J1A~5'' -:' p1 e N92 14346

(NASA-CP-31221 p 28 N92-14346 fNASA-CP,3t311 p3 N92-17984 VIBRATION EFFECTS

Laser anemometer measurements and computations in UNSTEADY AERODYNAMICS Free vibrations of thin-wailed semicrcular

an annular cascade of high turning core turbine vanes Physically weighted approximations of1 unsteadty graphite-epoxy composite frames

INASA-TP-32521 p 8 N92-28980 aerodynamic forces using the minimum-stale method INASA-TP-30101 p29 Nrt 13750

Tenth Workshop yor Computational Fluid Dynamic INASA-TP-30251 p 4 N9t-t803t VIBRATION ISOLATORS

Applications in Rocket Propulsion, part 1 UNSTEADY FLOW International Workshop oil Vibration Isolation

I NASA-CP-3t63.PT-tIl p 27 N92-32278 Calculation of unsteady transonic flows with mild T echnology tor Microgravity Science Applications

TURBOPROP AIRCRAFT separation by viscous-inviSCid interaction [NASA-CP- 10094] p 24 N92 28436

Annoyance caused by advanced turborprop aircraft I NASATP-3197]) p 7 N92-25477 VIBRATION MODE

flyover noise: Comparison of different propeller UPPER ATMOSPHERE influence 0f mass moment of inertia on normal modes

configurations The High Resolution Accelerometer Package JHlRAP) of preloaded solar array mast

INASA-TP-31041 p 45 N92-11758 flight expeniment summary for the first 10 ftighls I NASA- TP-32 731 p 31 N92-33476

Annoyance caused by aircraft en route noise[ A -R 161p3N2205 VDOAT

TURBULENCE 1 45N9 UPPER STAGE ROCKET ENGINES High Resolution, High Frame Rate Video Technology

TUBUENEGraphifi/lepoxy composite adapters for the Space (NASA-CP-30801 p 2

7 N9t-14574

State estimation applications in aircraft flight-data Shuttle/Centau.r vehicle The effects of video compression on acceptability 0f

analsi:A-Ruser's maua for-SMACK INASA-TP-30141 p 15 N92-3125i iages for monitoring life sciences experiments IAAP-22p10N1902 USER MANUALS (COMPUltR PROGRAMS) [NASA-TP-3239) P 16 N92-33933

Workshop on Engineering Turbulence Modeling State estimation applications in aircraft flight-dlatao viscous FLOW

INASA-CP- 10088] p 27 N92-24514 analyis. A user's manual for SMACK Flow-induced resonance o1 sceen-covered cavities

Laser anemometer measurements and computations in INASA-RP-12521 p 10 N91-19002 INASA-TP-30521 925 N91-15499

an annular cascade of high turning core tubne vanes USE REQUIREMENTS An upwind-biased space marching algorithm tot I NASA.TP-32521 tp8 N92-28980 Beyond the Baseline 1991: Proceedings of the Space supesonic viscous flow

Direct simultafion of high-speed reixtin layers station Evolution symposium Volume 1 Space Station (NASA-TP-30681 D 26 N9t -M138

[NASA-TP.31861 p C~ N92-30909 Freedom. panr I Aeroacoustic;and aerodynamic applications ofthe theor-y

TURB3ULENCE EFFECTS I NASA-CP-10083.VOL-1 .PT-1 I p 18 N92-17098 of nonequilitinum thermodynamics

High-Speed Research. Sonic Boom, volume 1 Beyond the Baseline I991 Proceedings of the Space lNASA-TP-31 181 p 26 N91-25352

JNASA-CP-31 721 p 11 N92-33874 Station Evolution Symposium Volume 2 Space Station Calculation of unsteady transonic flows with mild

TURBULENCE MODELS Freedom. cart I separation by viscous-inviscidminteraction,

NASA Computational Fluid Dynamics Conference. fNASA-CP-t0083-VOL-2-PT-tl j p 10192-17768 [NASA-TP-3t971 p)7 N92-285?'7

Volume, I -sessions t -8 Stag nationýpo int heat-transfer rate predictions at

INASA-CP-10038-VOL-1 I p 4 N9t-10839 aefoassist flight conditions

Computational Ftuid Dynamics Symposium on V (NASA-TP-32081 p 27 N92-11281

Aerinpropulsion VISCOUS FLUIDS

INASA-CP-30781 p5 1,91-21062 VACUUM Experimental measurement of the orbital paths of

Workshop on Engineering Turbulence Modeling The 25th Aerospace Mechanisms Symposium particles sedimenting within a rotating viscous fluid as

INASA-CP.10088] p 27 N92-24514 I NASACP.3t 13] p30 N9i-4403 influenced by gravity

TURBULENT BOUNDARY LAYER VACUUM PUMPS I NASA-TP-3200] p 40 N92-28897

Evaluation of a technique to generate artificially Venturi air-tel vacuum electors for i~ -oue VISUAL CONTROL

thickened boundary layers in supersonic and hypersonic atmospherrc sampling on aircraft platforms Visually Guided Control of Movement

flows I NASA-TP-3183] p I I N92-20546 I NASA-CP -3t11 itIp39 N92 21467

]HASA-TP-311421 p6 N91-28136 VACUUM TESTS VISUAL PERCEPTION

TURBULENT FLOW Oulgassing data for selecting spacecraft materials, Visually Guided Control of Movement

Numerical study of the aerodynamic effects of using revision 2 1 NASA -CP-31 181 p 39 N92-21467

sulfur hexafluonde as a lest gas in wind tunnels INASA-RP-t l2is.REV.21 p 21 N91-14437 VISUAL STIMULI

INASA-tP.3086] p 5 N91-22070 VANES Reliability of a Shuttle reaction timer

Laser anemometer measurements and computations in Laser anemometer measurements and computations in INASA-TP-31761 p 40 N92-f 6562

an annular cascade of high turning core furbine vanes an annular cascade of high turning core turbine vanes VOICE COMMUNICATION

1 NASA-TP-3252 I p 8 N92-28980 I NASA-TP-32521 p 8 N92-28980 Flight tests with a data link used tot air traffic control

TWISTED WINGS VARIATIONAL PRINCIPLES information exchange

Survey and analysis of research on supersonic Computational methods for frictionless contact with INASA-TP-31351 p 11 N91.31143

dralt-dlue-to-Itil minimization with recommendations for application to Space Shuttle Orbiter nose-gear tires VOLCANOES

wing design INASA-TP.30731 p 30 N9t-22576 International Workshop on Stratospheric Aerosols

I NASA-IP-32021 p 9 N92-33656 VEHICULAR TRACKS Measurements, Properties. and Elffects

TWO DIMENSIONAL FLOW Static footprint local forces, areas, and aspect ratios I NASACP.31 14][ p 32 N91-32528

Static performance of a cruciform nozzle with multraxis for three type 7 aircraft tires Sixteenth International Laser Radar Conference. panM

thrusf -vectoring and reverse-thrust capabilities INASA-TP-2983) p 10 Ng1-170il t

I NA SA- TP-31881 p 7 N92-23095 VELOCITY MEASUREMENT I NASA-CP-31 58-PT-I I p 28 N92-292281

NACA 0015 wing pressure and trailing vortex VOLCANOLOGY

measurements Volcanism-Climate fInteractions

U (N4ASA- TP-3151 j p 6 N92-10981 ]NASA.CP.100621 p 34 N91 21641

VENTS VOLUME

U.S.SR. SPACE PROGRAM Experimental investigation of porous-floor effects on An investigation of microSlructutatl characteristics, of

Exoibology on Mars cavity flow fields at supersonic speeds contact-lens. polymers

JNASA-CP-101055 p 41 N91-15691 [NASA-TP-3032] p 5 N91-19042 1 NASA-TP-30341 021 N~i 13491^

A-36
SUBJECT INDEX WINO TUNNEL TESTS

VORTEX BREAKDOWN WATER VAPOR WIND TUNNEL APPARATUS

Wind tunnel investigation of vorteri flows on F/A-18 The role of water vapor in climate A strategic research Large-scale aferoacoustic research teasrioitti and

configuration at subsonic through transonic speed plan for the proposed GEWEX water vapor project conceptual design of testisection inseris for the Ames 80

I NASA-TP-311t 11v6 N92-14966 IGVaP) by 120-foot wind tunnel

VORTEX SH4EDDING JNASA-CP 31201 p 35 N91 25556 [NASA TP 30201 p 41, N91 19824

Flow-induced resonance of screen-coverea cavities WATER WAVES WINO TUNNEL DRIVES

NASA-TP-30521 p 25 N91-15499 A self-zeroing capacitance probe for water wave Supersonic Througriflo* Fan Test Faciliy at NASA

VORTICES measurements Lewis Research Center

Detailed Ilow-field measurements over a 75 deg swept INASA.RP-t2781 p 36 N92-27930 ( NASA, TP 30381 p 13 N92 3!640

delta wing WAVE DIFFRACTION WINO TUNNEL MODELS

INASA-TP-29971 p 4 N91-18030 Diffracted and head waves associated with waves on Experimental investigation o1 poroustfloor affects cii

NACA 0015 wing pressure and trailing vortex nonseparable surfaces Cavity flow fieiis at Supersonic speeds

measurements INASA-TP-31691 p 7 N92-2054S tNASA-TP-30321 p 5 N91 ',904?

1NASA-TP-3t51 p6 N92-1 0981 WAVE DRAG Evaluation or a technique to generate artifcially

A comparison of airborne wakie vortex detectiion A met hod for designing blended winxg-booy thiickene boundary layers in superoic and hypersonic

measuremrents with values predicted from potential configurations for low wave dragflw

theory ~~~I NASA-TP-3261t p 8 N92,32480 IlowSAT312p6Ni60 theory -325 p 10 N92-10994 WAVE EQUATIONS NST~4jp ~-83

Wind funnel investigation of the interaction and Monegraph on propagation of sound waves in curved Pmanform curvature effects on flutter characteristics of

breakidown characteristics of slender wing vortices at ductsawigit56ce sin-d wepndaelset

subsonic, transonic, and supersonic speeds I NASA-RP. 12481 p 44 N91 -15848 ratio of 1 14

NASA-TP-31it41 p 6 N92- 12994 WAVE PROPAGATIONI AAT-16pIIN9135

Wind tunnel investigation of vortex flows on F/A-tB Propagation effecs for land mobtle satellite systems Effect ot afterbodli geometry on aerodynamic

configuration at subsonic through transonic speed Overview of experimental and modeling results Characteristics of isolated nonaxtsyrrirnil afteriodres at

I NASA-TP-3ttj 6 92t46 INASA-RI'.12741 p 25 N92-20404 transonic Mach numbers

A~~~~ nnierterfowaevtxiNteration we6l WAVE REFLECTION I NASA- TP-32361 p 9 N92-3370b

in curedkl chaninelr thlow yfrwv-otxitrcin Validation of three-dimensional incompressible spatial WIND TUNNEL TESTS

[NASA.TP-31581 p7 N92-191175 direct numenical simulation code A comparison with linear Prediction of effects of wIns; -intour modif ca* :ns on

Infuene eoetr f arfil ondeta in ledig-ege stability and parabolic stability equation theories for low-speed maximum lrthand transonic perfoirmancetfor tihe

vrinlces aidvrfoxidugeometryodndlamwing o ltsueadingidg boundary-layer transition on a flaf plate EA-68 aircraft

votiees advre-nueaeoyaisasuroic I NASA.-P-32O5 I p 8 N92-30295 I NASA-TP-30461 p 4 N9 1-1t0902?

JNspeeds 5 p7N9.001 WEAR TESTS Wake geometry ettlects on rotor tirade-vortexinteraction

INAA-T-3t5I N9-2038 Development of a full-scale transmission testing noise dlrectivity

procedure to evaluate advanced lubricants I NASA-TP-30151 p)44 N9tI-r 2315

W I NASA-TP-32651 p 28 N92-30396 J-85 jet engine noise Measured in the ONERA S1 wind WEATHER tunnel and extrapolated to far field

WAKES NASA/MSFC FY91) Global Scale Atmospheric IN,,3A-TP-30531 p 45 N91,19823

wake geometry effects on rotor blade-vortex interaction Processes Research Program Review Large-scale aeroacoustic research feasibility arid

noise directIviry I NASA-CP-30931 p 35 N91-116,0= conceptual design ui test-section inserts lor the Ames 80.

I NASA-TP-30151 p 44 N91-12315 WEATHER FORECASTING by 120-toot wind tunnel A comparison of airborne wake vortex detection NASA/MSFC FY91 Global Scale Atmospheric I NASA-TP-30201 p 45 N91-1 9824 measurements with values predicted from potential Processes Research Program Review Span reduction effects on the flutter characteristics of theory INASA-CP-31261 p 35 N91-32660 arrow-wing supersonic transport configurations INASA-TP-31251 p 10 N92-10994 The 1991 International Aerospace and Ground 'NASA.TP 3077' ItI NC' 21127 WALKING Conference on Lightning and Static Electricity, volume 2

Techniquex (fo Jeteir~nation of impact forces dunring [NASA-CP-3106-VOL-21 p36 N91-32693 Numerical study of the aerodynamic effects of using

walking and running in a zero-G environment WEBSS(SUPPORTS) sulfur hexaftuoride as a test gas in wind tunnels

INASA-TP-31591 p 38 N92-17022 Experimenfal behavior of graphite-eposy V-stiffened I NASA-TP-30861 p 5 1,91-22070

WALL FLOW specimens loaded in compression Transoitic Symposium Theory. Aplcation and

Wall-interference assessment arid corrections for [NASA-TP-31711 p30 N92-23t 15 Experiment, ,otume 2

transonic NACA 0012 airfoil data from various wind WEDGES [AAC-00VL2 9ý43

tunnels Large-scale aeroacoustic research feasibility and Low-speed, powered ground effects of a generic,

INASA-TP-30701 p 5 N91-20043 conceptual design of test-section inserts for the Ames 80- hypersonic: configuration

Comparison of a two-dimensional adaptive-wall by 120-foot wind tunnel I NASA.TP-3092) p 5 N91-25103

technique with analytical wall interference correction INASA-TP-30201 pt45 N91-19824 Sand and Dust on Mars

techniques WEIGHT REDUCTION INASA-CP-t00741 p 50 N9t-27057

INASA-TP-31321 p 7 N92-20494 Multidisciplinary optimization of controlled space Full-scale semnispan tests of a business-lel wing wifh a WALL TEMPERATURE structures with global sensitivity equations natural laminar flow airfoil

Longitudinal aerodynamic characteristics of a subsonic. I NASA-TP-31301 p 18 N92-1 1087 I NASA-TP-31331 p 6 N91-30098

energy-efficient transport configuration in the Nationlal WEIGHTLESSNESS Planform curvature effects .7n flutter characteristics of

Transonic Facility Workshop on Exercise Prescription for Long-Duration a wing with 56 deg leading-edge sweep and panel aspect

I NASA-TP-29221 p 6 N91-28143 Space Flight ratio of 1 14

WALLOPS ISLAND I NASA-CP-30511 p 36 N91-10574 I NASA-TP-31161 pItI N92-13054

NASA Wallops Flight Facility Air-Sea Interaction WEIGHTLESSNESS SIMULATION Wind tunnel investigation of v~~rex flows on F/A-IS

Research Facility Techniques for determinaftion of impact forces dunring configuration at subsonic through transonic speed I NASA-RP-12771 p 31. N92-25981 walking and running in a zero-G environment INASA-TP-31 ItI D6 N92-1 4968 WALLS (NASA-TP-311591 p 38 N92-1 7022 Ifuneo ifi emtyo et iglaigeg

Large-scale aeroacoustic research feasibility and Eccentric arid concentric muscle performance following vortices nd otidce d etryondyntamwics afarolgo atsupersonic

concentual design ot test-section inserts for the Ames 60- 7 days of simulated weightlessness vrie n otxidcdardnmc tsproi

'1, 12' , I ý,t wind tunnel I NASA-TP-31821 p39 N92-117645 speeds

I NASA-TP 30201 p 45 N91-f 9824 WELDED JOINTS INASA-TP-3t05J p 7 N92-20038

WARNING SYSTEMS Plate and butt-weld sfresses beyond elastic mint. Static performance of a cruciformi nozzle with multiaxis

Airborne Wind Shear Detection and Warning Systems material and structural modeling thrust-vectoring and reverse-thrust capabilities

Second Combined Manufacturers' and Technologists' INASA-TP-30751 p29 N91-16413 I NASA-TP-31881 pt 7 N92-23095

Conference, part t WIND SHEAR Wrnd-tunnel Static and free-flight investigatio of

NASA CP-10050-PT-1 I p 9 N91-1 1682 Airborne Wind Shear Defection and Warning Systems high-angle-ot-attack stability and control characteristics of

Airborne Wind Shear Detection and Warning Systems Second Combined Manufacturers' and Technologists' a Model of the EA-68 airplane

Second Combined Manufacfurers' and Technologists' Conference, part I INASA-TP-31941 p 7 N92-25276

Conference, part? 2 NASA-CP-t0050-PT-1 I p 9 N91-t11682 Two-dimensional aerodynarrvic Characteristics of Several

I NASA-CP-10050-PT-21 p9 N91-t 1695 Airborne Wind Shear Detection and Warning Sysfems Polygon-shaped cross-secfional models applicable to

Airborne Wind Shear Detection and Warning Sysftems Second Combined Manufacturers' and Technologists' helicopter fuselages

Third Combined Manufacturers* and Technologists' Conference, part? 2 NASA-TP-32331 p 8 N92-30394

Conference, part 2 1NASA-CP. 10050PT-2 p 9 N9t1-11695 Lewis icing research tunnel test of the aerodynamic

I NASA CP-10060-PT-21 p 9 N91-24140 Wind turbine acoustics effects of aircraft ground dercing/anii-icing fluids Airborne Wind Shear Detection and Warning Systems INASA-TP-30571 p 44 N91-16679 [NASA-TP-3238I p 10 N92-303145

Third Combined Manufacturers* and Technologists' Airborne Wind Shear Detection and Warning Systems Wind tunnel aerodynamic characteristics of a Conference, part IThird Combined Manufacturers* and Technologists' transport-type airfloil in a simulated heavy rain

INASA CP- 10060-PTtI I p 9 N9t-24166 Conference, part?2 environment

WASTE TREATMENT I NASA-CPt10060-PT-2J p9 N91-24140 INASA-TP-3104) p 8 N92-3t532

Cocntrolled Ecological Lite Support Systems Natural and Airborne Wind Shear Detection and Warning Systems Effect of afterbody, geometry on aerodynamic Artificial Ecosystems Third Combined Manufacturers' and Technologists' characteristics of isolaftad nonaxisymmetnc aft rtciis at

I NASA CP-t00401 p 40 N91-24744 Conference, part t transonic Mach numbers WATER [NASA-CP-10060.PT-1 I p9 1491.24166 INASA-TP-32361 p 9 N92-33706

Gibbs free energy of reactions involving SK, Si3N4f-H2, inertial oscillation of a vertical rotating draft with Parametric investigation of single -expansion -ramp

and H20 as a function of temperature and pressure application to a supercell storm nozzles at Mach numbers from 0 60 to 1 20

1 NASA-TP-32751 p 23 N92 31278 I NASA-TP-32301 p 36 N92-33482 I NASA-TP-32401 p 9 N92-34193

A-37
WIND TUNNEL WALLS SUBJECT INDEX

WIND TUNNEL WALLS Effects of yaw angle and Reynolds number on

Calibration of the 13- by 13-tinch adaptive wall test rectangular-box cavities at subsonic and transonic

section for the Langley 0.3-meter tranisonic cryogenic speedsl

tunnel (NASA-TP-3099j p 5 N91-27 124

I NASA-TP-30491 p 13 N91-13461 YAWING MOMrENTS

Wall-interference assessment and corrections for A nozzle infernal pcrformance prediction method

transonic NACA 0012 airfoil data from various wind [NASA-TP-32211 p 8 N92-33625

funnels

JNASA-TP-30701 p 5 N91-20043

Comparison of a two-dimensional adaptive-walt 

Z

technique with analytical wall inferference correction

techniques ZINC-OXYGEN BATTERI ES

t NASA-TP-31321 p 7 N92-20494 The 1991 NASA Aerospace Battery Workshop

WIND TURBINES [NASA-CP-3f401 p 33 N92-22740

Wind turbine acoustics

[NASA-TP-30571 p44 1%91-116679

WING NACELLE CONFIGURATIONS

Effect of location of aft-mounted nacelles on the

longitudinel aerodynamic charactenastics of a high-wing

transport earplarne

[NASA-TP-3047) p4f N91.13-402

installation effects of wing-mounted turbofan

nacelle-pylons on a 1ill-scale, twin-engine, tow-wing

transport model

( NASA-TP-31681 p 7 N92-19002

WING PANELS

Optimization of composite sandiwich coverr panels

subtected to compressive loadings

I NASA-TP-31731 p 21 N92-20679

WING PROFILES

Prediction of effects of wing contour modifications on

low-speed maximum fill and transonic performance for the

EA-6B aircraft

I NASA-TP-3046] p 4 N91-10902

Relative efficiency and accuracy of two Navier-Stokers

codes for simulating attached transonic flow over wings;

(NASA-TP-3061 p p26 N91-17310

WING SPAN

Span reductioin effects on the flutter characteristics3 of

arrow-wing supeirsonic transport configurations

INASA-TP-307'7] p 11 N91-21127

WING TIIPS

NACA 0015 wing pressure and trailing vortex

measurements

tNASA-TP-31!51 I p 6 N92-10981

WINGS

NACA 0015 wing pressure and trailing vortex

measurements

[NASA-TrP-31511 p 6 N92-10981t

Wind tunnel investigation of vortex flows on F/A-is8

configuration at subsonic through transonic speed

[NASA-TP-311 11 p 6 N92-1496e

Survey and analysis of research on supersonic

drag-dlue-to-lift minimization with recommendations for

wing design

[NASA.TP-3202j pg9 N92-33656

WOOD

Structural properties of laminated Douglas fir/epoxy

composite material

[NASA-RP-1238) p20 N91-10127

WORK CAPACITY

A method of evaluating efficincy during space-suited

work( in a neutral buoyas" environment

[ NASA-TP-31531 p 40 N92-19772

WORKSTATIONS

Report of the workishop on Aviation Safety/ Automation

Program

[NASA-CP-100641 p9 N911-15141

WRIST

The validation of a human force model to predict dynamic

forces resulting trom mutti-lomrrt motions

[NASA-TP-32061 p 40 N92-26538 x

X RAYS

Multiple lesion track stri.turs molell

[NAsA-TP-31851 p 39 N92-22186

Feasibility study of a low-energy gamma ray system for

meassuring quantity anid flow rate of slush hydrogen

fNASA-TP-3150j p 19 N92-25147

X-16 AI RCRAFT

Proceedings of the X-15 First Flight 30th Anniversary

Celebration

(NASA-CP-31051 pl 10 ,19-20071 V

YAW

Static thrust-vectoin Performance of ntonaxisymmetric

convergent-divergent nozzles with post-exit yaw vanes

(NASA.TP-3085) p 5 N91-21059

A-38
PERSONAL AUTHOR INDEX

NASA Scientific and Trechnical Publications 1991-1992

Typical Personal Author

Index Listing

Software design to, automated -isembly of truss BAKER, J. T.

structures Responses of women to orthostattic and exercise

[NASA.TP-31981 p 43 N92-26375 strenses

PESNLUHRALLISON. DENNISO0. (NASA.TP-30431 p37 Ki9t-19711 ~NA AUHORPrediction of effects of wing contour modifications on BALDWIN, R. T_

low-speed maximum fitl and transonic performance for the Types and Characteristics of Data for Geomnagnetic Field

EA-6B aircraft Modeling

ALRDE .I N NASA-TP-30461 pi4 N9i-t0902 . NASA-CP-31531 p 31 N92-28620

ALOIDG. AN ~ANDERSEN. 0. BNOERT, LINDA S.

The validation ofa humantforce modello predicOdynam. Exob~iology on Mars Effect of afterbody geometry on aerodynamic forces resulting from multi-joint motions (NASA-CP-10D055] p 41 N91-15691 charactenistics of isolated nonaxisymmetnic aftaxtiodies at

INASA-TP-3206i p 40 N92-26538 ANDERSEN. DALE Tr. transonic Mach numbers

Fourth Symposium on Chemical Evolution and the Origin I NASA-TP-32361 p 9 N92-33706

and Evolution of Life BARBER. FRANK iTILE RPOT PAE ACCESSION tINASA-CP.31291 p 41 N92-13588 Reliability training

NUBR NME NUMBER ADREN, KRISTINN (NASA-RP- 12531 p 15 N92-32456

A generalized method for multiple robotic manipulator BARE. E. ANN

programming applied to vertical-up welding Parametric stud of afterbody/ nozzle drag on twin

I(NASA-TP-31631 p 24 N92-t 121 8 two-dimensional convergent-divergent nozzies at Mach

ANDERSON4, MELVIN S. nliernumbers from 0.60 to 1 20

"-,innts inl this index are arranged alphabetically Asisymmetric shell analysis of the space shuttie solid (NASA-TP.26401 p4t N91-114316

by p i<-'-thor- The title ot the document pro- rocket booster tield joint r'aramethic investigation of single-expansion -ramp

vids wiria he ~etdecritin se o te sbjct NASA-TP-3033 p p28 N91 -14618B nozzles at Mach numbers from 0.60 to 1 20 viisteue iha,'fdsrpino h ujc NESNW. KYLE I NASA-TP-3240) p9 N92-34193

matter. The report number nalps to indicate the Numerical study of the aerodynamic effects of using BARGER, RAYMOND L

type of document listed (e.g., NASA rport. trains- sulfur hesalluoride assa teat gas in wind tunnels Diffracted and head waves associated with waves on

lation, NASA contractor report). The page and ac- I NASA-TP-3G861 p 5 N91-22070 nonseparables surfaces

cession numbers are located beneath and to the ANTONIEWICZ. ROBERT F. I NASA-TP-31691 p 7 N92-20545

Application and flight test of linearizing transformations Companison of let plume shape predictions and plume right of the title. Under any one author's name the uigmaue ntfdbctoheolnarotol nleceon sonic boom signature

accession numbers are arranged in sequence. problem (NASA.IP-31721 p 7 N92-25133

I NASA-TP-31541 p 1.2 1491-30154 Trajectory ftiting in function space wilth application

ARBUJCKLE, P. DOUGLAS analytic modeling of surfaces

A controls engineering approach for analyzing airplane [NASA-TP-32321 p 8 N92-30747 A input-output characteristics A methiod for designing blended wing-body [ NASA-TP-30721 p t2 Ng 1-20128 configurations for low wave drag

ABEYOUNIS, WILLIAM K. ARKING, ALBERT I NASA-TP-3261 I p 8 N92-32480

Effect of location of aft-mounted nacetles on the Climate Impact of Solar Variability BARINA. FRANK J.

longitudinal aerodynamic characteristics of a high-wing INASA-CP-30861 p5O N91-12456 Reliability training

transport airplane ARMA4I0, SASAN C. INASA-RP-i2531 p 15 N92-32456

INASA-TP-30471 p4 N91-1 3402 Influence of mass moment of inertia on normal modes BARNETT, ROBERT JOEL

ADDY, HAROLD E., JR. of preloaded Solar array mast A generalized method for multiple robotic manipulator

Lewis icing research tunnel test of the aerodynamic INASA-TP-32731 pt31 N92-33476 programming applied to vertical-up welding

effects of aircraft ground deticmglanti-cing fluids ARRAS. MICHAEL K. INASA-TP-31931 p 24 N92-1 1218

INASA-TP-32381 p t0 N92-30395 Fault tolerance of aitifiial neural networks with BARRETT. M.

AGGARWAL P. K. applications in critical systema The High Resolution Acceierometer Package (HiRAP)

Effect of type of load on stress analysis of thin-walled INASA-TP-31871 p 4 2 N92-22285 flight expeniment summary for the first 10 flights

ducts ASBURY, SCOTT C. I NASA-RP-1 2671 p 3 N92-22505

INASA-TP-32481 p 31 N92-26669 Static performance of a cruciform nozzle with multiaxsi BARROWS, LINDA H.

AIELLO, ROBERT A. thrust-vectoring and reverse-thrust capabilities Evaluation of nioninvacive cardiac output methods during Improved accuracy tor finite element structural analysis INASA-TP-31881 p 7 N92-23M9 exercise

via a new integrated force method ATENClO, ADOLPH, JR. I NASA-TP-31741 p 38 N92-16553

INASA.TP-32041 p 30 N92-22227 J-85 jet engine noise measured in the ONERA St wind Fuel utilization during exercise after I days of bed rest

ALDRIDGE. ANN M. tunnel and extrapolated to for field (NASA-TP-3175) p 36 N92-16554

The validationi ofta human force model to predict dynamic [NASA-TP-30531 p45 1,91-19823 Eccentric and concentric muscle pedtirmarce followting

torces resulting from ri'ulti-jo-11 motions ATWELL, WILLIAM 7 (ays of simulated weightlessness

I NASA-TP-32061 p 40 N92-26538 Radiation risk predictions for Space Stationt Freedom JNASA-TP-31821 p 39 N92-17645

Correlation and prediction of dynamic human isolated orbits BARTHELEMY, JEAN-FRANCOIS M.

jointt strength from lean body mass I NASA-TP-30981 p 51 N91-26107 Research in Structures, Structural Dynamics and

I NASA-TP-32071 Ip 40 N92-26682 Analyses of risks associated with radiation exposure Materials, 1990

ALHORN, D. C. from past major solar particle events I NASA-CP-3064 I p 29 N91-10301

Definition anid design of an experiment to test raster I NASA-TP-31371I p 50 N91 -31061 BARTOS. KAREN F.

scanning with rotating unbalanced-mass devices on AVIS, LEE M. A three-dimensional finite-element thermal/mechanitcall

gimbaled payloads Limb-darkening functions as derived from along-track analytical technique for high-performance traveling wave

I NASA-TP-32&91 p 24 N92-29677 operation of the ERBE scanning radiometers for August tubes

Reconfiguring the RUM experiment to test circular 1985 INASA-TP-30811 p p25 N91-27436

scanning with rotating unbalanced-mass devices on INASA-RP-12431 p 34 N91-1 4683 BAUER, STEVEN X. S.

gimbaled payloads The natural flow -wing-design concept

INASA -P-32821 p025 N92-33601 INASA-TP-31931 p 7 N92-25202

ALI. MICHAEL S. B SAUGHER, CHARLES R.

The effect of bandwidth on telerobot system Measurement and Characterization of the Acceleration

performance Environment on Board the Space Station

I NASA-TP-3152 f p28 N91-30540 BACH. RALPH E., JR. I NASA-CP-30e8 I p 48 N9t-12401

ALLAMANDOLA, LOUI3 J. State estimation applications in aircraft ftight-data Space Station Freedom Toxic and Reactive Materials

Interstellar Oust Contributed Papers analysis. A user's manual for SMACK< Handling

INASA CP-30361 p48 N91-14897 JNASA-RIP-12521 p 10 N91-t9082 I NASA-CP-30851 p48 N91-15930

ALLEN. CHERYL L, BACAVI, POROOZ F. BECK. SHERWIN M.

Guidance, navigation, and control subsystem equipment HZE TFN. A heavy ion/Inucleon transport code for space Technology for the Future in-Space Technology

Selection algorithm using expert system methods radiations Experiments Program, pairt I

[NASA.TP-30821 p4 2 N91-25624 JNASA-TP-3t461 p51t N92-15959 INASACP-t10073-PT-ttI p 14 N91-27177

B-i
BELCASTRO, CHRISTINE M. PERSONAL AU THOR INDEX

Technology for the Future ln-Space Technology BREWER, JEFFREY C. C

Experiments Program, pert 2 The 1991 NASA Aerospace Battery Workshop

(NASA-CP.10073-PT-21 p 14 N91-27178 I NASA-CP-31401 p 33 N92-22740 CAMARDA, CHARLES J.

BELCASTRO. CHRISTINE M. BRITCHER. COLIN P. A simplified method for thermal analysis o1 a CowileWading

On the formulation of a minimal uncertainty model for Aerospace Applications ot Magnetic Suspension edge subject to intense local shocti-waxa-intearteence

robust control witlh structured uncertainty Technology, pat heating

JNASA-TP-30941 p 13 N92-10027 (NASA-CP-t0066-PT-1 I Ip 17 N91-2t1188 INASA.TP-31671 p27 N92-24797

BENNETT, LARRY H. CAMPBELL, RICtHARD L

AMSAHTS 1990: Advances in Materials Science and Aerospace Applications 0f Magnetic Suspension AmeodIrtedegn1tannileiiawns

Applications of High Temperature Superconductors Technology. part 2 NAAT met04d desig po 10e 14tanoicfe 23eig

[NASA.CP-3t001 p 22 N92-21605 [NASA-CP-10066-P1'-21 * 7 Ng 1 -21203 Applications of a direct/ iterative design method to

BERKE. LDSZLO International Symposium on Magnetic St.spension complex lowaivorimc Configurations

Improved accuracy for tinite element structural analysis T echnology, part 1 1NASA- TP-32341 p 8 N92- 33454

via a new integrated force method I NASA-CP.3152-PT-1 I p 18 N92-27721 CAMPBELL. WILLIAM A.. JR.

LNASA-TP-32041 p 30 N92-22227 international Symposium on Magnetic Suspension Outgassing data for selecting spacecraft materials

BESS. T'. DALE 7echnology. pert 2 revision 2

Atlias 01 wide-iteld-ot-view, outgoing longwave radiation (NASA-CP-3152-Pr-21 p 18 N92-27788 I NASA-RP-Il124-REV.21 P 21 N91-t4437

derived from Nimbus 7 Earth radiation budget data set BRODY, ADAM R. CAPON4E, FRANCIS J,

November 1965 to October 1987 Manual Control Aspects 0f Orbital Flight Aeroptroyulsiva characteristics of canted twin

INASA-RP-12611 p i 35 N91-24719 INASA-CP-100561 p 13 N91-20147 pitch-vectoring nozzles at Macno0 200 to 21)

KZOS. GAUDY M. I NASA-TP-30601 P5 1491-22069

Wind tunnel aerodynamic characteristics of a BROWN. JEFFREY C. Parametric investigationl 0f single -expansoon-ranW

transpori-type airfoil in a simulated heavy rain Supersonic Throughtlow Fan Test Facility at NASA nozzles at Mach numbers from 0 60 to 1 20

environment Lewis Research Center tAAT-20 9-49

[NASA-TP-31841 p 8 N92-31532 INASA.TP-30381 p 13 N5,c-3i,640 CARDSN.T320 HU9 N0-3t

BILLINGS. C. E. BROWNLEE, 0. Free vibrations 0f thin-walled semicircular

The development of the NASA aviation salaty reporting Eirobiology in Earth orbit The results of science graphite-epoxy composite frames

system workshops held at NASA. Ames Research Center INASA-TP-30101 p 29 N491-13750

1 NASA-RP- 11141 p 10 N91-70436 [NASA.SP-5001 p 41 N91-t4725 Failure behavior of generic metallic and composite

BINDSCHADLER. ROBERT A. BRUCKER. 0. J. aircraft structural Components under crash loads

West Antarctic ice Sheet initiative Volume V- Science Shortcomings in ground testing, environment I NASA-RP- 12391 p29 N91, 13751

and Implementation Plan simutations, and performance predictions lor space Effect of Crash Pulse shape on seat stroke requirements

[NASA.CP.31 t5-VOL. I p 32 1491-20541 applications for limiuting loads on occupants of aircraft

West Antarctic Ice Sheet Initiative. Volume 2: Disciptine INASA-TP-32171 p 23 N92-22593 I NASA.TP-31261 p 30 N92.18053

ReviewsCALOHRYW

J NASA.CP-31t5-VOL-21 p 32 N91-26573 BRYSON. CRAIG C.CRSNARYW

BIACKELDAW, L 0. Second Conference on NDE for Aerospace Survgdeytantd mnizalyisonfit resachommndatipons b

NASA Workshop on future directions in surface modeling Requirements wing-cu~ designonwthrcomndton f o

and grid generation I NASA-CP301 I p 16 N491-18189 wingS-P.2 p9 49.365

[NASA-CP-100921 p 8 N92-29625 BULLOCK, ELLEN PARKER CARLSON,. "ON R.

BISHOP. PHILLIP Span reduction effects on the flutter characteristics of A nozzle internal performance prediction method

Techniques for determination of impact forces dunring arrow-wing Supersonic franspori configurations INASA-TP-3221 r p 8 N92-33625

walking and running in a zercl-G environment [NASA-TP-30771 p 11 N91-21 127 CARPENTER, M. H.

I NASA-TP-3159 J p 38 N492-17022 BUNDICK. W. THOMAS Direct simulation of high-Speed mixing layers

BLAIR. A. B., JR. Development of an adaptive failure detection and I NASATP-31861 p 8 N92-30909

Evaluation 01 a technique to generate artificially identification system for detecting aircraft control element CARROLL, Mi. A.

thickened boundary layers in supersonic and hypersonic failures The atmospheric effects of stratospheric aircraft A

flows INASA-TP-30511 p 12 N9t-2515i current consensus

INASA.TP-3t4Z[ p 6 N91-28136 BURKHARDT, R. INAZA.RP-125t I p 33 N491 1646?7

BLANCHARD. ROBERT C. Cable compliance CARSON, GEORGE T., JR.

The High Resolution Accelerometer Package (HiRAP) (NASA-TP-32161 p 24 N92-30378 Aeropropulsive characteristics of canted twin

flight experiment summary for the first 10 flights ic-etngozlsaMch02to10

[NAS.RP1261 p3 N9-2205 URLY, JMESR.,11 NASA.TP-30601 p5 N491-22069 SOHON, HERMAN L Parametric st udy ot after' ody /nozzle drag on twin Static internal performance of ventral and rear nozzle Eighth 'I)D/NASA/FAA Conference on Fibrous two-dimensional convergent-divergent nozzles at Mpch concepts ton short-takeoff and vertical- landing aircraft

Composites in Structural Design. part1 numbers from 0 60 to 1 20 INASA-TP-31031 p 6 N92.10975

I NASA-CP-3081-PT- I p 22 N92-32513 [NASA-TP-2r>401 p 4 N91-14316 Effect of aflerbody geometry on aerodynamic

Eighth DOD/NASAIFAA Conference on Fibrous BURNEY, LEWIS G. characteristics of isolated nonaxirymnmetric atterbodies atI

Composites in Structural Design, part 2 Ventun air-jet Vacuum etectors for high-volumne transonic Mach numbers

(NASA.CP.3087-PT-21 p 22 N492-32574 artmospheric sampling on aircraft platforms tNASA-TP-32361 P 9 N92-33706

BONHAIJS, DARYL. L [NASA.TP.31831 p 11 N92-20546 CAZIER, F. W.. JR.

Retative efficiency And accuracy of two Navier-Slokes BURNS, KAREN S. Space Transportation Materialt and Structures

codes for simrulating attached transonic flow over wings An investigation of microstructural characteristics of Technology Workshop Volume 1 Executive summary

INASA-TP-30611 p 26 N91-17310 contact- lens polymers I NASA -CP- 3148 -VO.IA p 15 N92-2Z660

BOWLES, ROLAND L. [NASA-TP-30341 p 21 N91- 13492 CHAMIS. CHRISTOS C.

Airborne Wind Shear Detection and Warning Systems BUSH. KATHRYN A. Computational Structures Technology for Airhtames and

Second Combined Manufacturers' and Technologists' Mission description and ..i-llightl operations of EASE Propulsion Systems

Conference, part 1 instruments on ERRS and NOAA 9 spacecraft. November I NASA-CP.31421 p 31 N92-2591 1

[NASA-CP- IO005-PT -1I p9 N491-11682 1984 - January 1986 CHANG, 5.-C.

Airborne Wind Shear Detection and Warning Systems I NASA.RPI 2561 p 32 N92-10208 On the formulation of a minimal uncertainty model for

Second Combined Manufacturers' and Technologists' Mission description end in-flight operations of EASE robust control with structured uncertainty

Conference, part 2 instruments on ERRS. NOAA 9. and NOAA 10 1 NASA-TP-30941 p 13 N92-1 0027

[NASA-CP-10050'PT-2j p 9 N491-11695 spacecraft CHANG, CHAU-LYAN

Airborne Wind Sheer Defection and Warning Systems. (NASA-RP-12791 p 32 N492-32127 Validation of three-dimensional incompressible spatial Third Combined Manufacturers' and Technologists' BUSOUETS, ANTHONY M. direct numerical simulation code A comparison with linear

Conference, part 2 Effect of short-term exposure to stereoscopic stability and parabolic stability equationr theories fon

I NASA-CP- 10060.-PT .21 p 9 N91-24 140 three-dimensional flight displays on real-world depth boundary-layer transition on a flar Plate

Airborne Wind Shear Detection and Warning Systems percepton [NASA-1'P-32051 p 8 N492-30295

Third Combined Manufacturers' and Technologists' INASA-TP-31171 p 11 N92-13065 CHANG. I-CHUNG

Conference, pert 1 BUTLER, RICKY W. Transor-c flow analysis for rotors Part 3

1 NASA-CP- 10060-PT-1I I p9 N91.241ffi NASA Formal Methods Workshop. 1990 Three-dimensional. quasi steadty. Euler calci~ation

DOZZOLO. GUILLERMO [ NASA-CP- 100521 p 42 N491-17559 I NASA-TP-23751 p3 N91 10007

Equirvalent crystal theory of alloys BUTTERFIELD, ANSEL J. CHEANEY, E. S. I NASA.TP-3155) p23 N491-30318 Benefits from synergies and advanced technologies for The development of the NASA aviation salety reporting

BRECKENRIDGE. ROGER A. an advanced-technology space station system

Technology for the Future. tn-Space Technology [ NASA-TP-30671 p 14 N9t-20177 (NASA RP-t 11141 p t0 N491 70436

Experiments Program, pert I BYRD. JAMES E. CHOO. Y. K.

fNASA-CP-1I0073-PT - 1 Ip 14 N491-27177 Influence of airfoil geometry on delta wing leading-edge NASA Workshop on futuredirections in surface modelino

Technology for the Future In-Space Technology vortices and vortex-induced aerodynamics at supersonic and grid generation

Experiments Program. pert?2 speeds (NASA-CP 100921 p8 N92 2()625

1 NASA-CP- 10073-PT-21 p 14 N149-717e I NASA-TP-31051 p 7 N492-20038 CHU. JULIO

BRENN4ER. M. J. BIlK, SARA E. Effects of yaw angle and Reynolds numher on

Development of an integrated aeroservoelastic analysis Fourth Symposium or Chemical Evolution and the Origin rectangularibox ca'~ties at suivo~rir Arid Iansoi~c

Program and correlation wtith leaf dale and Evolution of Lila speeds INASA-TP-31201 p2 N91-26113 INASA-CP-31291 p41 N492-03588 I NASA rP 3099a1 p 5 149 1 2771ý4

B-2
PERSONAL AUTHOR INDEX FASANELLA, EDWIN L.

CHU, WILUAM P. Multiple lesion track structure model DOW. MARVIN B.

SAGE I data user's guide INASA-TP-31851 p039 N92,22,86 Properties of throe grapinitetyouighoerd rosin

INASA-RP-12751 p 34 N92-33097 Track structure model of cell damage in spaeC fqlh Composites

CHUANG, SHERRY L INASA-TV-323151 p 39 N92-3415-s INASA-TP-31021 p 21 N92 10067

The eftects of vide compression on acceptability 0f CULBERT, CHRISTOPHER J. DREHER, P. E.

images for monitoring life sciences experiments Second CLIPS Conference Proceedings, volume I Long-term Orbtal irfetirfed Predictions

INASA.TP-32391 p 1

6 N92-33933 INASA-CPlOOOS-VOL-l p 42 N92-16%68 INASA-TP-30581 p 13 N91-10092

CHUN, SANG Y. Second CLIPS Contfernce Proc~eedngS, volume 2 ORMMO00D J. PHILIP

HZETRN A heavy ionirnucleon trarnsport Code lor Space INASA-CP-1008-VOL-2 p 42 N92-16590 Two-dimensionial stability of lamrinar flames

radiations CUNNAN, WALTER S. I NASA-TP-31311I p 7 N92,17t3l

I NASA.TP-3146! p 5 N92-15959 Supersoric Throughtlow Fan Test Facility at NASA Direct swlaorn of i h-peed mixing layers

CLARK, JOHN S. Lewis Reserch Center JNASA.TP318161 p 8 N92-30"0

Nuclear Thermal PrropulsiOri A Joint NASA/DOE/DOD [NASA.TP-30381 p 13 N92,31640 DUKE, EUGENE L

Work~shop Application and flightl test of lineaising transformnations

I NASA-CP- 100791 020 N92-1 1088 D using mfeasuremen~ft feedback to trhe nonlinear control

CLARK, LEN WOCO G. problem

Technology for the Future In-Space Technology OANFORO, M. o. INASA.TP-3t5.41 p 12 N91t30154

Experirments Programt. part 1 Electrochemnical studies of corrosion inhibitors DUNBAR. BONNIE J.

INASA.CP.10073-PT- I p 14 N91-27177 INASA-TP-30661 p 22 N91-17208 The mnicrograity, environment of the Space Shuttle

Technology for the Future In-Space Technology The interaction of hydrogen with metal alloys Columbia msddecli during STS-32

Experiments Program. part 2 (NASA-TP.312el 0)23 N91-29318 INASA-TP-31401 p 48 N92-11930

INASA.CP.10073.PT-21 p 14 N97-271 78 DARDEN, CHRISTINE M. The nlicrogravity environment of the Space Shuttle

CLARK, RONALD K. High-Speed Research Sonic Boom, volume I Columbia payload bay during STS-32

Oxidation characteristics of Ti-25A1-tONb-3V-1Mo INASA-CP-31721 pit1 N92-33874 INASA-TP-31411 p 49 N92-1193,

intermneelglic alloy DAVIS. 0. 0. DUNHAM, J. R.

[NASA-TP-30441 p 22 N91-13522 Evaluation of a technique to generate artificially NASA-LaRc Flight-Cntlical Digital Systems Technoliogy

Surface effects on hydrogen permeation through thickened boundary layers in Supersonic and hyperSonic Workishop

Ti- I4AI-2tINb alloy flows [NASA-CP.100281 pI I N91 .242f00

1 NASA-TP-31091 p 23 N91-20266 INASA-TP.31421 p6 N91-20136 DUNHAM, At. EARL. JR.

DAVIS. RICHARD E. Wind tunnel aerodynamic Characteristics Of 8

COLLIER, LISA D. Evaluation of clood defection instruments and transportl-ype airfoi n a simulated heavy rain

Technology (of the Future in-Space Technology performance of lamninar-Ilow, leading-edge test articles environment

ExeimentsCProgram.Part I p1 ~-77 duning NASA Leading-Edge Flight-Test Program 1NASA-TP-31B41 p 8 N92-31532

TeSAchnology fo PT- th In-Space7 1uur Teholg NASA-TP-28881 p 11 N91-24199 DURICY, JAMES A. ETecnoelots Program theFtre inSaeTcnlg DAVIS. WILLIAM T. Rigid-body-control subsystem sizing lor an Earth science

ExeimentsCProgramT- p 142t-77 Packagin~g, evelopment, and on-orbit assembly optionts geostationary platform

COK GEORGEP E07-T2. 1 9-77 for large geostalionary spacecraft [NASA-TP.30871 p 17 Ngi-22302

A generalized method for multiple robotic manipulator DAIC NAAT-0. , pS.Nt-78

programming applied to vertical-up welding DAnalCsis an. peiton Multiple-Site Damage (MS0I E

I NASA-TP-31631 p 24 N92-1 1218 fatigue crack growth COSGROVE, PATRICK A. INASA-TP-3231 j p 31 N92-31279 EFTEKHARI, ABE

Themriral-distortion analysis of a spacecraft box truss in DAWSON, RON4ALD A. An investigation of mrCrostructural characteristics of

geootationrray orbit Supersonic Throughtlow Fan Test Facility at NASA contact-lenaf polymers

INASA-TP-305-41 p16 N91-1 1041 Lewis Research Center I NASA-TP-30341 p 21 N91-13492

Inertial ROBcRTat C. a etclrttigdatwt NASA-TP-30381 p 13 N92-31640 Investigation of rnicrostructural changes in

appltical onctllato superc vertorm roaigrftwt DAWSON, VIRGINIA PARKER polyetherettier-kalone hMMs at cryogenic tempertures by

NASha-tP-32 to p 36erel N92-34 Engines and Innovation: Lewis Laboratory and American poaitron lafeti" spectroscopy

InerAtial osilto 30 Of 59-38 vetiaortaigurltwihidon Technology INASA-TP-30641 p 21 N91-18216

aneplicationclltio ofa e vue rstorm l riotsupplement Ifwto INASA-SP-43061 p 51 N91-15975 Low-entergy, positron flux generator for frucrOStruCturaI

NaSApTchtinioal Paporer 3230 ie splmet DECKER, HARRY J, characterization of thin films

NAA ecnialPaer320 evlometof a full-scale transmissoion testing INASA.TP.30741 osrio p 27 1`91-22538

INASA.TP-3230-ViDEO-SUPPLI p3 N92446 procedure to evaluate advanced lubricants Psto eieI ncrl oochfs

CRIM. G. INASA-TP-32651 p 28 N92-30396 crystals

NASA-LaRc Flight-Cnilical Digital Systems Technology DEFREES 0. (NASA-TP-3122J p 46 N92-10677

WoAsA-op-128p11N1240 Exobiofogy in Earth orbit: The results ot science EKLUNO. W.

INASALL.CYNTIA08 A.N1240 workishops held at NASA. Amnes Research Center Cable compliance

TRWELiLn, CYTIAA naardnmccaatntiafeaa NASA-SP-00I p 41 N91-14725 I NASA-TP-32161 p 24 N92-30378

polyo-dmn-shapedcerodysetinai mhaadelistapicsserable to EGNAN, KEITH T. EWlS. STEPHEN R.

helicopte tselagedrssscinlmdsapiabet Mission description and in-flight operations of ERBE Manual Control Aspects of Orbital Flight

heicpe fAuselages 8 92309 instruments on ERBS. NOAA 9. and NOAA 10 INASA-CP. 10561 p 13 N91-20147

CRUZS.CHITOP HER3 I9-09 p spacecraft ERICKSON, GARY E.

PCRameri CHITradeR stuie on i[t2arc -oe NAftA RP-12791 o32 NQ7'i-7127 Wind tunnel investigation of the interaction) and

Parchiteic ture d tde naSwt-2tuc )ýe DEWMOE. W.O6. oieaiidowoi Characteristics 01 sOrnde, wrirQ uthI44ir at

arhietueThe atmospheric effects of stratospheric aircraft: A subsonic, transonic. and suptersonic speeds

INASA- TP-3059 p fit N911-18180 cretonnssINASA-TP-31141 p 6 N92-129194

CRU7'JUJAN R. INASA-RP-12511 p 33 N91-16467 Widtne vsigtooforxflwonF-1 Oiptimization of composite sandwich cover panels DENNIS, BRIAN4 configuration at subsonic Ithrough transonic speed

Nsubjeted37 comresiveloaing pto The Compton Observatory Science Workshop (NASA-TP-31 I1I1 p 6 N92-14968

I AAT-371p2 N2269 INASA-CP-31371 p 49 N92-21874 ERICKSON. LARRY L.

CUSBAGE, JAMES U. DESILVA. SHANAKA Panel methods An introduction

A parametric ewpe~iiiitýai inrue irIiui Of - ýC:.amjel Volcanismn Climate lI-teractimris INASA-TP-2995 I p5 N91-19058

nozzle at Mach 6 with Freon and argon or air used for (NASA-CP- 100621 p34 N91-21641 ERLEOACHER, GORDON

exhaustP-08 p4imulation DEVINCENZI, 0. L A weakly nonineaisr theory fO, wa~o v010tN ,r!0P*Ctionix

CUCNOAA.T-08 A.-199 pRACI Exobiology on Mars in curved Channel flow

Icrr ielat atc cteig fhayionsannulr DILLARD, RICHARD S. ESGAR. JACK 9.

correa-tions 1p6 ~-t9 Reliability training Structural properties of laminated Douglas tv/epoxy

Cellular track model of biological damage to mammalian D ASAGETT, 253LIA p. isS-P-26 compsi maen p20345 

cell cultures from galactic cosmic rays DoftEare W eiLLIA fo. aNutomated36 pssmbl Noftruss

INASA-TP-305C, p 50 N16l1-16981 SotaedsgfoaumtdasmbyotrsF

Improvements in computational accuracy of SRVNTRN s3ructures7F

(a baryon transport cod~e) (NASA-TP-31981 p4 9,87

fNASATP-3093I p 51 N91-230t7 DOIRON. SCOTT 0- FARMER. JEFFERY T.

Radiation risk predictions for Space Station Freedom Nimbus-7 TOMS Antarctic ozone atlas August - Thermal-ditstortio analysias of a spacecraft box truss in

orbits December 1990 geosfationery orbit

ýNASA.TP-30981 p 51 N91-26107 tNASA-ltP-12641 p35 N91-26651 I NASA-TP-305-41 p16 N91-11041

Analyses of risks associated with radiation exposure DOUGLAS&. A. R. On-~orbit structural dynamic per-formance of a IS-meter

from past malor solar particle events The atmospheric effects of stratospheric aircraft A microwave radiometer antenna

I NASA.TP 31371 p 50 N91-31061 currentf consensus INASA-TP-30411 p 16 N91-17114

Cellular repair/misrepair track model INASA-RP-12511 p 33 N9`1-16847 FASANELLA EDWIN L

I NASATP 31241 p 42 N92-1 16M DOUGLASS, ANNE R. Determination of the nlight hardware configuratio of an

Trasnport methods anid interactions tor space The atmospheric effects of stratosphenic aircraft A first energy absorbn attenuator for the Proposed Space

radiations program report Station crew and equipment translation aid cart

I NASA RP 12571 p 51 N92-15956 [NASA-RPt12721 p 33 N92-19121 INASA-TP-306-41 p 29 N91-.21556

8-3
FEREBEE, MELVIN J., JR. PERSONAL A UTHOR INDEX

FEREBEE. MELVIN J5.. JR, GARRISON. JAMES L GREELEY, RONALD

Benefits from synergies arid advanced technologies for Launch vehicle integration options t

o, a large Earth Sand arid Dust on Mars

an advanced-technology space station sciences geostationai'y Platfo~rm concept jNASA-CF 10074 p S N 9 2 10 a4

JNASA.TP-306-1 p 14 N91 20177 tNASA-TP 30831 0 15 N91 27180 GREEN. LAWRENCE L

FERNANDEZ. KENNETH R. GARY, J. PATRICK Wall-Initerferenice assessmnent arid coliect,ons 10i

A generalized method for multiple robotic manipulator Proceedings ot the Second Annrual NASA Science tiansonic NACA 0012 aafoli dalei ton v'arious wind

pirogramming applied to vertical-up welding Internet use( vvorflnig Gt-ip ;Ao-.ýi,,w lfl.Si 101*

1NASA.TP-31631 p 24 N92.11218 INASA-CF 31171 p 48 N`9i-27009 [NASA tP 3070j i Pi N9it 20)04 3

FERRAINOLO. JOH4N J. GARZON. SHERRYA. GREENE. FRANCIS A.

Large space structures slid systems in the space station Eighth DODINASAIFAA Conflererice on i-brous An upwind-biased space marchriNi hagiolfittfiii

era A bibliography with indexes Composites in Structural Design, part I spersoniic viscous flow

t NASA -SP- 7085(0 111 p 17 1,91-118199 (NASA -C P-308 ?-PT-Il p 22 N92 32513 jNASA, T P 3068.ý 216 N9! 1838 t

uerge space structures and systems in the space station Eighth DOD/NASA/FAA Conlfernce on Fotous Nun'enal analysis and simulation of an assurea cifr.

era A bibliography with indexes Composites in Structural Design pan 2 return vehicle flow field

INASA-SP. 7085(02)] p 18 N91-28191 [NASA.CP-3087-PT-?I p 22 N92-3;!574 [NASA TP 3101! p 26 N92 r10161

FERRANTE, JOHN GATLIN. GREGORY M. GREENISEN. MICHAEL

Equivalent crystal the"r of alloys Lo0w-speed. powered ground effects of a generic Techniques for determinantion, ot irmpact forces during

tNASA-TP-31551 p23 N91-30318 hypersonic cornfiguration walking anid running in a zero G ernvironmnent

FIELDS, ROGER A- INASA.TP-30921 p 5 N9t 25103 ýNASA-fll-3i591 A3 N92 70-22

Thermal and structural tests ofl Rene 41 honeycomb GENRELS. NEIL GREENISEN. MICHAEL C.

integral-tank concept for future space transporltaiori The Compton Observa~tory Science Workishop A mnathod 0f evaluating efficiency during spae s,,ited

systems INASA-CP-31371 p 49 N92 21874 work in a neutral buoyancy envuoiimentl

tNASA-TP3145j p 30 N92-24205 GELDER, THOMAS F. [NASA TP 3153; p 40 N92 197'2

FISCIIL. ROBERT Design and performance o1 conritoltd-diflusion stalo.l GROOM. NELSON J.

On the f ormiulation of a minimal uncertainty model fix compared with original double-circular arc stator Aerospace Applicatins of Magnetic Su"speson

robust control with structured uncertainty I NASA-TP-28521 p 12 N92-22863 Technology. part I

NASA-TP-30941 p 13 N92-10027 GENTRY. GARL L, JR. jNASA-CF 10066 PtI ;r p 17 N91 ?I'M9

FISHER. DAVID F. Wind tunnel aerodynamic characteristics of a Aerospace Applications of Magnetic Suspenfsion

Evaluation 0f cloud detection instruments and transport-type airfoil in a simulated heavy rain, Technology part 2

perfoain ice of lamirtiar-tiow leading-edoge test articles environment [ NASA-CP 10066-PT 2 p t7 N9¶-212C3

during NASA Leading-Edge Flight-Test Program I NASA-rP-31841 p 8 N92 31532 interrnationa~l Symposium on Magretic SsnsensoiI NASA -TP-28881 p I11 N9t1-24 199 ONOSH. DAVE Technology part I

FITE. E. BRIAN Ongoing Progress in Spacecraft Corrirois INASA-CP-3t52.P' I 1 18 N9? 27721

A three-dimensional tinite-lement thermiali mechanical (NASA-CP-t00991 P t9 N92-28730 International S~mposuvm on Magnetic S,,spension

arnalytical technique loin high-performance traveling wave GIARRATANO, JOSEPH Technology part? tubas Second CLIPS Conference Proceedings. volumie I I NASA-CP-3t 52-PT 21 P 18 N92-T6

INASA-TP-30811 p 25 N91-27436 1NASA-CP-10085-VOL I Ip 42 N92-16568 GROVEMAN. MRAN

FLANEGAN, MARK Second CLIPS Conference Proceedings, volume?2 Users guide Nimbus 7 Earth iadiatronr Oudgii!

Small Explorer Data System MIL-STD-t1773 fiber optic (NASA-CP-10085-VOL-21 p 42 N92-16590 nalrtoei-ieidof vi-ew products Scene radiance tapeo

bus 01mB. JOHN4 products. sorting into angular bins ofrouctrs anid rlaxnimum

[ NASA-TP-32271 p 16 N92-26667 MILSTAR's flexible substrate solar array Lessons likelihood clouid estimation products

FLOM1, URY learned, addendum I NASA-AP-12461 r 34 N9' 1304 3 AMSAHTS 1990 Aidvances in Materials Science and I NASA-CP 3147-ADD I p 33 N92-26895 GUIMARASS. PATRICIA T. Applications of High Temperature Superconiductors GIESECKE, ROBERT L Nimbus-? TOMS Antarctic ozone atlias August

[ NASA-CP-31DOI p 22 N92-21605 The microgravity enviroriment of the Space Shuttle December 1990 FOLEY, ROBERT J. Columbia payload bay duning STS-32 INASA RP 126-41 ) j1 N9r 2665! Static thrust-vectoring performnance ofnonexlisymmetnic INASA-TP-31411 p49 N92-t 1931 GUPTA, K. K. convergent-diverglent nozzles with post-exrit yaw vanes GILBERT, JOHN H. Development of anminegratedt aefose~voeiaslrc anatirvs

(NASA-TP-30851 p5 8591-21059 A method of evaluating afficiency during space-suited program anm corelatron with test dale FORREST. DANA K. worklin a neutral buoyancy environment I NASA, TP 3120! o2 N91 26 * t3 Measuremients of lorceils. moments, and pressures on fNASA-TP-31531 p 40 N92-19772 GPA OPN

a generi store separating from a box cavity at supersonic GLOSS. BLAIR B. GPA OPN

speeds Longitudinal aerodynamic characteristics of a subsonic. Calculations and curve cils of theirnodvnamric and

[NASA-TP-31 101 p 6 N92-1t0005 energy-etifictent transport configuration in the National transport properties lor equlubriurn a-i to 30000) K

FOUGHINER, JEROME T.. JR. Transonic Faciuliy NASA -RP-t12601 P .6 N92 ' 12AS

Transonic Symposium Theory Applicafion and I NASA- TP-29221 p 6 N91-28143 Stagnation-point heat-transfer 'ate predictions at

Experiment. volume 2 GODBOLD, JO0HN A. aeroasist hlight conditions

tNASA-CP-3020-VOL-21 p5 N91-24132 Payload bay doors and radiator panels familiarization I NASA-T P 3208 j p 27 N92 31281

FREY. RICHARD handbook

User's guide Nimbus-i Earth radiation budget [ NASA-TM-t1077931 p 15 N92-20676

narrow -field -of -view products Scene radiance tape GOLDHIRSH, JULIUS H

products, sorting into angular bins products, and maximum Propagation effects tor land mobile satellite system's

likelihood cloud estimation products Overview of expenmental and modeling results I4ABERLIE. ROBERT M.

INASA-AP.12461 p 3A N91-t3043 [NASA-RP-12741 p 25 N92-20404 Sand and Dust on Mars

FRIES, SYLVIA DOUGHITYs GOLDMAN. LOUIS J5. I NASA-CP- I100741 p 50 N91 27057

NASA engineers and the age of Apollo Three-component laser anemometer measurement HAHNE, DAVID E.

;NASA-SP-41041 p 52 N92-28344 systems Full scale semispan tests oi a business let wing with a

FROINEK. DENNIS L [NASA.TP.211-l p 5 N91,19057 natural laminfir flow airfoil

Supersonic Throughtflow Fan Test Facility at NASA Laser anemometer measurenielis enid computations in I NASA-TP-3 133 i p 6 N931300981

Lewis Research Center art annular cascade of high turning core turbine vanes Wind-tunnel static and freetflight nvestigalion of

I NASA.TP-30381 p 13 N92 31640 1NASA-TP-32521 p 8 N92-289f0 high-angle-of -attack stability and control charactens~tics of

GONG, LESLIE a mocdel of the EA-68 airplane

Gintegral-tank GThermal and structural tests of Rane 41 honeycomb INASA-TP-31941 p 7 N92-25216 concept for future Space transportation HIAINES, RICHARD F.

01AAOBRYMsystems The effects nii voideocompression orn acceptability of

Benchmark solutionslforthe galactic heavy-ron transport QSLAAU -34)pP0N-3?05 I NASA. iaesfr3oiorn9fl1 cice opet6 N92-33z5 3

equations with energy and spatial couplingGODELAAM.INS-P391b6N?333

1 NASA-TP-31 121 p 44 N592-13756 Transonic arid supersonic Euler computations of HAUROCIS. BERNARD .J_

GARDNER. J5. E. vorter-dominated flow fields about a generic fighter Fundamentals 0f fluid lubrication

Space Transportation Materials and Structures I NASA-TP-31561 p 6 N92-10011 I NASA.RP 12551 pi 28 Nitt 305 11 TecnoogyWolisio Voum V veutio ummry GOUGEON. MEADIE HNDE Technlogy Volme orkshp I xecutve sumary Structural proplerties of laminatrid Douglas fir/epoxy HNDEO

I NASA-CP-3148-VOL-t I I IS1 N92-22660 composite material Works~hop oin Squeezed States anid Uncertintyih

GARDNER, JAMES E.I AAP-131p2 N9107 Reain

National Educators' Worfkshop- Update 1988 Standard GRAHAMR.-26 p2NN 1012?-335 I9 pRelations,1

Expemantsin ngneeingMatrils ciece nd Experimental validation of clock synchronization HANDSCHU54. ROBERT F.

Technofogy aloihsA method for determining spiral-bevepl geet tooth

INASA-CP-30601I p20 N91-20207 INS-P32091 p 42 N92-275819 geometry for finite element analysis

National Educators* Workishop- Update 1991 Standard GRANTHAM, CAROLYN I NASA TP-30961 o281 N92 10195

Experiments in Engineeenng Materials Science and Software design for automated assembly of truss HARDY. ALVA CTchrsotogy structures Radiation risk predictions tor Space Station Freedom

fNASA-CP-315t 1 p 24 N92-30263 JNASA.TP-3198I p43 N592-28375 orbits

GARRETT, L BERNARD GRAVES. PHILIP C. (NASA-TP-309E1 p o t N91 2610 7

Benefits trom synergies and advanced technologies tot Multidisciplinary optimizatIori ot controlled space Analyses of risks associated with radiation exposure

an adnianced-tatchnoflogy space station structures with global sensitivity equations from past mator solar particle events

JNASA.TP-30671 pt 14 N91.20177 [NASA-TP 31301 p 18 N592-11087 INASA.TP-31371 p 50 8591 3 104)1

S-4
PERSONAL A UTHOR INDEX JONG, J,

HARDY. R. HOL.TON, J. A. IVANCIC. WILLIAM 0,

The development of the NASA aviltion safety reporting The atmospheric effects ot strittospohenc aircraft A Destination-airected. pacirel-switching architecture for

system currenlt Consensus 30/ 20-iGHz FDMA/ TOf geostatroinary communications

INASA-RP-ttt141 p 10 N91-70a36 JNASA-RP-12St)I p33 N91-iii,,67 satellite network

HARRIS, BERNARD A. HOPKINS, DALE A. I NASA TP-32011 p 16 N920 9762

Fuet utiltization durnfg exercise after 7 days of bed rest Irrproved accuracy for tinite, element structural analysis

iNASA-TP-31751 p 38 N92-16554 "isa anew integrated force methiod

Eccentric and concentr-ic muscle performance following I NASA-TP-32041 p 30 N92??22227

7 deys of simulated weightlessness Computational Structures Technology for Aarfrar'-ý nid

INASA-TP-3le2i p 39 N92-17645 Propulsion Systems .rACHIMOWSEI, CASIMIR J.

HARRIS,~ . R SENR NASA-CP 31421 p 31 1 e-25911 An Analysis of combustion Studies in shock expansion

Workshop on Exercise Prescription for Long-Duration HORACK, J. Mt. ~adrfetdso unl

Space Flight Development of "h Burst a- ,/tient Source INASA TP-32241 p 22 N92-26374

jNASA-CP.30511 p36 N91-10574 Experiment (SATSE) JACKSON, CHERYL C,

HARRIS. HARLES E. NASA-RP.12681 p 49 N91-32006 Rigid-body-control subsystemsizing floran Earth scinc

The 1991 International Corifetrunce on Aging Aircraft and HORNE, W. CLIFTON geostationsry platform

Structural Airworthiness Acoustic and ae&WOnriamc Study Of a Puspheir-prOPeIeR1 INASA-TP-30871 p 17 N9 122302

INASA-CP-31W01 p 31 N92-30 106 aircraft model JACKSON, KAREN E.

HARMIS, CHRIS J, NASA-TP-301401 p 45 N91-21628 Determination Of the fliht hardware configuration of an

Mission descniption and in-flighlt operations of ERBE Aeroac:..tic and aerodynarricapplictionsofthetheor energy absorbing eltenuator for the proposed Space

instruments on ERSS and NOAA 9 spacecraft. November of , ,-uimhbnurn thermiodirnam-cs Station crew and equipmrent translation aiid cart

1984 -January 1986 IN.. -rP-31t81 p 26 N91-25352 [NASA-TP-3084j p?29 N91-21556

INASA.RP-12561 p 32 N92-10206 HORTA, LUCAS G. JACKSON. LENORE A.

HASSON. SCOTT M. identification 01 linear systems by an asymptotically Prceig of the Second Annual NASA Science

The validation of a human force model to predict dynamic stable observer Internet User Working Group Conference

iorcos resulting trom mutt.i-ysnt mhotions INASA-TP-31641 p 31 N92-26537 INSA-CP.31171 p 48 N91-27009

tNASA.TP-32061 p 40 N92-26538 HOUSNER. JERROLD it. JACKSON. U.MI.

Correlation end prediction of dynamic human isolated Comnputationial Structures Technology for Awirframes and Responses ot women to orlthostatic and exercise

pint strength from lean body mass Propulsion Systems straisses

INASATP-3207t p 40 N92-26682 (NASAr-CP-31421 p 31 N92-25911 INASA-TP.30431 p 37 N91-1971i

HATHAWAY. MICHAEL 0. HOWE. JOHN T. JACOBS, JAMES A.

Design and performance of coritrollWdffusion stator Hyper-velocity atmosphenic #flight Real gas flow folds National Educators' Workshop Update 198a Standard

compared with original douible-zircular-src Stator I NASA.RP- 12491 p 26 N91-204tIS Expenierimets in Engineering Matenials Science arid

INASA-TP-28521 p 12 N92-22863 HOWELL. WILLIAM E. TeSAcP-0nologyN 1.220 HAYES, JUDITM C. Static footprint local forces, areas, and aspect ratios IAS.P300 90N1-00

Eccentnic and concentnic muscle performnance followin for three type 7 aircraft tres National Educators' Workshop Update 1991 Standard

7 days of simulated weightlessness (NASA-TP-29931 p tO N91-17014 Espenriments in Erngineening Mallenats Scoence and

jNASA-TP-31S2j p 39 N92.t17646 HOWERTON. CLAYTON E. Technology

HAYHURAST. KELLY J. Mission descnption and in-flight operations of ERSE !AAC35 t2 9-08

Structural factoring approach tor analyzing stochastic instruments on ERSS and NOAA 9 spacecraft, November JACOBS, PETER F.

networks t 984 - January t 986 Longitudinal aeodynarmic charersiianstics of a substonic

INASA-TP-30691 p 43 N91-18753 INASA-RP-i2581 p 32 N92-10208 eflergifefficieflt transport configuration in the National

HAYS, RUSSELL 0. Aission descnption and in-flight operations of ERaE Transonic Facility

Reliability ofta Shuttle reaction timeir instruments on ER8S. NOAA 9, and NOAA t0 INSATP-2922! p8 N91-28143

INASA-TP.3t761 p 40 N92 16562 spacecraft JACOBSON. NATHAN S,

HERSTROU, CATHERINE L INASA-RP-12791 p 32 N92-32127 High-temperature durabilit considerations for HSCT combtustor Softwere design for automated assembly 01 truss HOWL.ETT,.JAMES T. fNASA-TP-3162) p 23 N92-17070 structures Calculation of unsteady tran sonic flows with mild JAE, BN.JAMIN 8. [NASA-TP-3i98j p 43 N92-28375 separation by viatcous-tinviecd interaction Muliscplinary optimiation of controlled space

HILL, ACOUILLA S. INASA-TP-31971 p 7 N92-28477 structuires with olobal sensitivity equations

Calibration ot the 13- by 13-sinch adaptive watt test HUBBARD. HARVEY H. INASA-TP-31301 p 18 NB? 11087

section for the Langley 0 3-meter transonic cryogenic Wind turbinie acoustic JAMES, ODETTE 1. tunnel INASA-TP-30571 p44 N9 1-16679 Ptrtr geocieriones. 1999- 1 99W

[NASA-TP-30491 p 13 Ng I- 13461 Aeroecoustics of flight vehicles Theory and practice. NASA-SP-5081 p SO N92-28345

HILL. EUGENE G. Volume 1. Noise sources JIEOLEY. DAWN C.

Lewis icing research tunnel test of the aerodynamic I NASA-RP-1258-VOL-i I p45 N92-IOS98 Compression behavior of graphie-thierrnopiastic and

effecis of aircraft ground deicing/anti-icing fluids Aeroacoustics of flight vehicles Theory and practice graphite-epoxy panels With circular holes or Wnpect

1NASA-TP.3236 I p 10 N92-30395 Volume 2 Noise control damage

HILL, GERALD F. tNASA-AP-125S-V0L.-2I p 45 N92-14779 INASA-TP-30711 p21 N91-t82 IS Ventun air lt vacuum electors for high-volumne HUCEK. RICHARD R. Effect oflow-speed impact damage and damnage IOU *n

atmosfihenic sampling on aircraft platforms User's guide Nimbus-? Earth radiation budget on behavior of composite panes

INASA-TP-31831 p I

t N92-20546 narrow -field -of-view products Scene radiance tape [NASA-TP-3t961 p 22 N92-23961

HINGST. W. A- products, sorting into angular bins products, and maximum JOHNISON R. L

Evaluation of a technique to generate artificialty likelihood cloud estimation products Responses of women to orthostalic: and exercise

thicktened boundary laties in supersonic and hypersonic [NASA-RP-12461 p 34 N9. '3043 stresses flows Atlas of the Earth's radiation budget as measilwfed by fNAS-TP-3OA3 p 37 N491,19711

I NASA-TP 31421 p8 N91-281315 Nimbus-?7 May 1979 to May 1980 JOHNSON, WALTER WHOADLEY, SHERWOOD TIFFANY [NASA-RP-12631 p 35 N91-24720 Vissially Guided Control of Movement

Physically weighted approximations 0f unsteady [NASA-CP.31 181 p39 N92-21ASI`

aerodynamic forces using the mrinimum-sltae method JOHNSTON, H. S&

INAS-TP302I p4N91t801 IThe atmospheric effects of stratospheric isicrfti A INASAN. TPRANCIS T4.1ý83 current consensus

issues in NASA program and project management INASA-RP-12511 p33 N91.16467

INAA-P-60t031 p6 Nt-33 BR1AHIM, K. Y- JOHNSTON, HAROLD S. INsAsues in~ NAS (0 prora adpoem Nagement 7 Resource envelope co.'ces'ts for mission planning The atmospiheric effct of statospheric aircraft A iAsAsues NASA82 0(01 prgaIn rtetmngmnNASA-TP pi6 31391 p 15 N91-29209 topicat review I AAS-110) 6N1206 INGRAL01, ANTHONY M. I NASA.RP. 12501 p 33 1491 16466 Issues in NASA Program and project management Installation eftects of wing-mounteid turbofan JONES. ,J. H. I NASA.SP-6t01(05)1 p 47 N92-27809 nacelle-pylons on F. 1/17-scale, hein-enIne, low-wing Twiime-frequencyrimpresaertation of ahighfy nionstationary

HODGE. A. J. transport model signal via the modified Wigner distribution

A novel method 01 testing the sheer strength of thick INASA-TP.3t681 p 7 N92-t9002 INASA-TP.32151 p 25 N492,20492

honeycomb composites IRIE ,JONES, JIM J.

(NAA-T-3081p~lN9-2142 Excbiology in Earth Orbit The results O 09hscine Stagnation-point heatl-tratnafar rate predictions at A statistical compripeson of two carbon fiber/epioxy workishops held at NASA. Ameos Research Center OW055515 flight conditions

fabrication techniques NS-P50p41N1175 (AAT3M p2 N2326

I NASA.TP-11 79f p 22 N492-20950 9tti~ JONES,500 N SATP28 LI p2E.2-16

HOFFLER. 0. W. ISAXSEN, 1. S. A. Deterimination of the flighit hardware configuration of an

Responses 0f women to orthostalic and exercise The atmospheric effects of stratospheric aircraft A energy, absorbing attenuator foi the proposed Space

stresses current consensus Station crew and equipment translation aid cairt

(NASA-TP-30431 o37 N91-19711 INASA-RP-12511 p33 N491-16467 I NASA-TP,30641 p29 N491-21556

HOLLENUACH. DAVID J. ISHAM, M. A. JONG. J.

The Interstellar Mediummi External Galaxies Summaries Gibbs tree energy of reactions involing SiC, S3N-4. H42, Time-frequenrcy representation of a highly nonstationsity

ot contrnbuted papers and H420 as a function of temperature and pressure signet vie the modiie Wigrle distributlion

INASA-CP 30841 p49 1N9t-t4l00 1 NASA.TP-32751 p 23 N492-31278 I NASA.TP-32i5) p 25 N492-20492

8-5
JORDAN, FRANK L., JR. PERSONALt A U THOR /NDEA

JORDAN, FRANK L.. JR. KIM, KYUN 0. LANCE, 0. G.

Full-scale sarrsspan tests of a business-tel wing withl a COmputatiortaf methlods tot fr-clrorrress contact ewitr An examination of thre damage l,ýoance enhrancement

natural laminar lo BIO rf N application to Space Shruttle Orbirter nose gear fiees of carbe n~epoxy using an outr zam~na of sptel a Rt

!NASA TP-3 i331 p 6 N9 i 30098 1NASA TP 30731 p 310 N91 22576 NASA Tl'i6 110 p2 14 92 !.r42

Wind-tunfnel static and free-llrghl investigation of KIM, Y_ S. LANDIS, GEOFFREY A

high-argie-ol-aftaCk stability and control characteristics of Workshop on Squeezed States and Uncetamnty Vision- 21 Space Travel for the Nlext Mll-ienr,,,m

a mode? of the f.A-6 airplane Relations jNASA-CF- 10059i p 13 N491 22111V

!NASA T F 31941 p 7 N92 25276 [NASA-CF-3 1351 p 46 N92 22045 LANE. HELEN W.

JOSLIN, RONALD 0, KING. CHARLES 8,NwinlRfieeS.frSaeSac ,oo

Validation of three-drmensional incomtpressible Spatial Packaging developmntel and on -drbll assemrbly options Crews

direct n,,menrcal simulation-Icode A comnparison with hnear for large geostalronary spaclicraft NASA.CP.3t461 P 40 Nl2.25-961

stalt),ly and parabolrc ssaba145 eq~uation theories lor I NASA T P )08S p l7 N491-27182 LANGEL. Rt. A.

boundary layer l'anSrtron o1' a fl15 plate KJELGAARO. SCOTT 0. Types and Characlrerstrcs of Data ory Geloragrret,c rI d

I NAAFP32051 p 8 1492-30295 Detailed flow-field measurements over a 75 deg swept Modeling

JUANG. JER-NAN della wing I NASA CP-31S31 p3'ý N92 286;,

identifcatinon of linear systems bry an asymptlpotcalyp INASA.TP.?9971 p 4 N491 18030 LANTZ, RICHARD L.

stable Obsorvier KLEIN, H. Supersonic Throuightlow Fan' Tesl t FCIlr 4 1atNSAs

JNASA TPF31641 P31 N492-26537 Enobiroqlog n Earth olorit The results of Scence LowAsA-P33 Centel peeac 314

JULIENNE. ALAIN work~shops held; at NASA, Ames Research Cene L ARKSAVI T E0.;p1 9?-A

J-85 le engine noise measured in te ONERA Si wind jNASA-SP-SO00 1p)41 N491 147725 Nmu OSA~cr zn la 4.s tunnel and extrapolated 10 far field KNOX, CHARLES E. December 19GOO NASA TP.3053ý p a5 N491-19823 Firghrt tests with a data sink Used for air traffic COntll INA SA -RP- 126-a1 p 3`5 N14f 2661'.r

.pnfn-slvor exchrange LARMAN, K. T.

KKO, INASA.TP 31351 p I! N491-311,13 The Hilghr Resolution Acceerromaele Pack~age i-'RAPI W. K. W. ft'ght Gerpemerrt Summary, %' mre !irst 10 flirghts The atmospheric effects of stratospherlc aircraft A i NASA.RP 12157 ) p3 N962-225012

KAISER. MARY K. current consensus LAWRENCE, UEORGE F,

Visually Gurded Control of Movement I NASA.RP- 1251 1 p 33 1491 16467 Large space structures and syslemsnt ine spacesao I NASA CP .3t 181 p 39 N492-21467 KO. MALCOLM K. W. era A toibolrarphry wrill noexes

KARAMNCETI. KRISHNAMURTY The atrmosphereic effects of stratospheric arrcraft A first ;NASA-SP-7085(02) p 18 Ncri 216,14

Aerocacroosticand aerodynarmicapplications offthe theory program report LEA, ROBERT N.

of nonequllrbrum thermnodynamics !NASA.RP 12721 p 33 N492-19121 Proceedings ot the Second Join! Technology Work~shop !NASA.TP.31181 p 28 N91-25352 KORITE. JOHN J. on Neural Networks and Fuzzy L09,C. volume 2

KARIYA, TIMMY T. An explicit upwind aigor~thm 10r Solving the paratbofrued 1NASA.CP 10061- OIL-2, jP43 N491 208'11

Installation effects of wing. nounted turbofan Na,.er-Slorres equat0Ios Priickneqsgf of the Zwurr(j j ,oint Technolokgy yironkshoo

nacelle pylons oin a 1, 17 scale hoarr-n~erl~ . low-wing JNASA TP.30501 p 14N91 '8032 on Neural Nehvorks and Fulzy Log<c volume I

transpiort model KRANTZ, TIMOTHY L I NASA-CP 1 W61 -VOLI-t I(V43 N149 217.?y

1NASA.TP-31681 p 7 N492 19002 Experimental and analytical evaluatron of efllcrency of LEE. KAU.PUI

KARPEL. MOROIECHAY helicopter planetary stage CalculatIons and curve Itjs -I tnerrnodnam~c anld

Physically weigr tefd approximations of unsteady NASA.TP.30631 p 28 N9t 1 12958 transport Propeoltes try Oquillbrur air to 301300 K

aerodynamic forces using the minmumv-state method KRISHEN. KUMAR i NASA-RP- 12W0 p v26 N492I 1181,

jNASA TPF30251 p4 N491 IOC31 Fifth Annual Workshop on Space Operatriors LEFSCH. ROGER A.

KASPER. HAROLD J. Applications and Research (SOAR 19911ý volume 2 Paramelnc trade strrdres on a Sh~tlfe 2 launcf' sys!,ol'

Graiphrfeievooay Cioniposte adapters for the Space I NA-A-CP.3127 VOL-21 p) 4t N92-22324 architecture ShurttfeiCenlaur vehncl KRUEGER, ARLIN J. NASA-TP.30591 j 4 N91 ' 8817

1NASA.FF.30141 p 15 N492-31251 Nrmbus.? TOMS Antarctic ozone atltas August . LESLIE. FRED W.

KATZ. ROBERT December 1990 NASAMSFC Fn90 Global Scale Atmospriec

Celfuluar track modell of bkological damage to mammalian I NASARP- 1264 jp 35 N1-9 26651 Processes Research Program Review

Iceil cultujres from galactic cosmic rays KUMAR. AJAY INASA CF 30931 035 1491.165(00

I NASA-TP-30551 p 50 N491 16981 Direct simulation ot high-speed mixing layers NASAIMSFC trY9 Global Scale Atmospheprrc

Radiation nsa Predictions for Space Station Freedom INASA-TP-31861 p8 6N92-30909 Processes Research Program. Resrew

04,its KYLE. H. LEE I NASA CP .3t261 p 35 1,5 326.;

INASA. TP 3098; 51 1491 Z8t07 Users guide Njmbus-7 Earth radiation tirjdgef LEVINE. ARLENE S.

Track stnructure model of cell damage in~ Space flrghtf narrow -field-of -view products Scene radiance tape :irst k.0FF Posf.Relrleval Sympodsrurm abstracrs

iNASA-TP 32351 p 39 N92-34 154 products, sorting info angular bins prodoct5. and maximum fNASA-OF- 10072! p 52 N491 249'2

KEEL. WILLIAM C. lrkefrtlood cloud estimation products LOEF 69 Months in Space First Posrtlletlreval

Paeffd arnd interacting Galaxies lniterniatlonal INASA-RP-12461 p 3

4 N91-t 3043 Sympcs~um panrt

Astronomircal Uniron Colloqurum Nol 124 Atlas of the Earith re tlatkon budget as measured by INASACP.3134-PT ! p 52 N492 23260

1NASA-CP-30" I p 4

9 N91 16858 NMmbus-7 May t979 to May t980 LDEF 69 Months in Space l'rst Post Retrieval

KELLER. DONALD F. NASA-RP- 12631 p 35 N491-24720 Symposium. Part 2

Span reduction effects on the flutter characteristics of(AA01-1A-T2 p5 9 4

artow-wtng supiersionrc: transport configurations LOEF 69 Mornths in Space Frst Post Rer~rena

INASA-TP.30771 pI I N9t- 2112 7 L Symnposium, part 3

Ptanfiorm curvature effrscfs on flutter charactenistics of I NASA -CP.3t34.F- 1 PT 5 N492 270$3

a winmg with 56 deg leading-edge sweep and panel aspect LABEL, KEN Second LOEF Post.Reitrieval Symposiumn abstracts

ratio ott 1 1 Small Explorer Data System MIL-STOt1773 fiber optrc ;NASA-CF. 100971 p 5' 149227218

TNASA-TF-3t 161 p) It N92-13054 bus LEWICKI. DAVID G.

KELLEY, HENRY L INASA-TP-32271 p 18 N92-2W67 Developmnent Of a furl Scalp transmihssion, letinlg

Two-dirnensicinat aerodynamic characteriatics of several LACK, CYNTHIA L procedure to evaluate advanced iubrlcwin'5

polygon shaped cross -sectional models applicable to Effect of temperature and gap opening late 00 the I NASA-TP-32651 0)28 N492 30396

helefcootf or fuselages resiliency of candellate solid rocket booster 0 ring LIGHTSEY. W. 0).

I NASA TP-32331 p 8 N492 30394 materials A nlonlinear estimator fry reconstructing the arngular

KENNEDY, LEWIS w. (NASA-TP-32261 p 23 N492-27194 velocity of a spacecraft wttlhoult rate gyros The 1990 NASA Aerospace Battery, Workshop LAKE. MARK S. I NASA-TP-3t 781 p 24 1492 13343

1 NASA-CP- 31 t91 pt20 1492.27130 Buckig and vibration analysins 01 a simply supported Definition and design of an experriment 10 lest raster KERLEY, J. clmwihaprecewtse consftant Cross sect ion

Cable compliance I NASA-TP-30901 p 29 N91-20503 scmafedgit payotads gublacdmsdvcso

I NASA-TP-32161 p 24 N92-30376 Stiffness and strength tailoring inl uniform space-fillIing giNASo a- yl-ads9

KETELSEN. DEAN A. truss structures (NS.P341p24 N4922967'

A nw arralorlme~o fr NASA-TP-3210 I p 30 N92-24546 LIN. PAUL Anwfbelo endfrprecision antenna fALVNETI nfluence of mass moment of rnertia on normal modes

relcosfSaeflighrt adgroudts Reliabininty training ot prefoaded solar array mast

I NASA-TP-30781 p 17 N91-21185 I NASA-RP-1 2531 po tS N92-32456 (NASA-FP-32731 p 3t N92-33476

KHAN, FIERDOUS S. LALLMAN, FREDERICK J. LIOU, W. W. Transport methods and interactions fory space Control integrat ion concept for hypersontc cruise-turn Workrshop on Errgineerrng Turbutence Modelling

tadtatorr maneuvers I NASA-CP- 00881 5 27 1492 24514

I NASA RP-1257) p 51 N492-15956 INASA-TP-31361 p %3 N492-20195 LITVIN. FAYDOR L

KHANOIELWAL. QOVIND S, LAMKIN. STANLEY L A method for determining sp~rfarbevei gear tooth Incltuaf inelasfic scattering of heavy ions and nucl ear Berrcfhmartk Sotlutiorns fry the galactic heavy-on transport geomefry tory fInute element analysis

correlations equations wifth ertergy and spatial coupling INASA-FF-30961 P 28 N92-10195

[NASA.TP-30261 p46 N491-13985 INASA-TP-31 121 p 44 N492-13756 LOLLAR, L FV

Transpoi efhiods and interactions tor space HZETFIN A heavy ott/nucleorn transport code for space Automratrng a spacecraft efelctrnali power system using

radialliorts radiationsa export systemns

[NASA-FtP 12S71 p 51 N492-15956 I NASA-TP-3I461 p 51 N92 15,05t, I NASA-TP-31611I p 20 N49? I120,
PE- 1A L A UTHOR INDEX NEWMAN, 4. C., JR.

I.Olqi) * EN R, MCCUROY. DAVIV A- MOE. KAREN L.

N Wallops Flight Factiiy Air-Sea interaction Annoyance caused by advanced turtboprop aircraft Space Network Control Conference on Reource

* ~ Facility I"yve noise Comparison of *"gfrant propae.e Allocation Concepts and Approaches

P-12771 p 36 N92-2596i configurations INASA-CP-31241 1. 6 N917 11039

zeroing capacitance probe for water ways [NASA-TP-31041 p 45 N92-1 1758 MONTA. WILLIAM .1.

flients Annoyance caused by aircraft to route noiae A prmatrnic *sperenpental rivwsbigatbon of & ec~reile

P-12781 p 36 N92-27930 INASA-TP.31651 p 46 N92-20479 nozzle at Mach 6 witth Freon e" argon or ao uwae tor

LOGARICHARD W. MCDOO4GAL.. DAVID S. exhaust~ simejaltton

mtoun Of linear systems by an asymptotically FIRE Science, Reaufts 1980 p 4N1-04 NASA-TP.30481 04 NO' 1699

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9 .31641 p 31 N92-26537 MACOHEE.O0. & The inrction of hydrogenr with meta "coy.

LUBiu i, JOSEPH V. The effect of accelerationvrsu adisplacemnent methods INASA-TP-31261 P 23 N91 29318

sonal Workishop on vibration Islation oel steady-state boundary forces MOORE, ALAN 0.

gy for Microgiravily Science Aprplecations LNASA-TP-321 81 p 30 N92-21457 Evaluation of nonmnvasive cardia OeVW mrethode durng

a.'-,00941 p 24 N92- 28436 MCGINNIS, MICHAEL R. 0etci50

LUNN )NATHAN 1. Microbiology on Space Station Freedom )NASA.TP.3174 1 P 38 N92-16553 tr esineL18.19 NASA-CP-31061 p 37 N9t-t8573 Fuel u110117txon dluirng exerciae affaer 7daysaof bed real

Ly-l "! p 50 Nlý235 A qimplee imethod tor thermiat analyaia ofla cowl leading [NS-P, 5 PK3IN92I655

LY - m ria lieiri ~ rdý .~ edge subject to intense local shock-wave-inteeterenie AMSOtANI,S tg dane MaeaaScec n rm orbital predictionshealing lifeime SAT19 AdacsiMtealSwvan

'1-3058) p 13 N91-10092 INS.P36jp7N2277 Applications of High Temperature Superconductors

MCMASATPR. 7 p 27 N9-477 INASA -CP-3 100) P22 N92-2t135

SAM2r*aS~en~n30th~0Ir talsphnciarOS4 MOREUO. SAMUEL A.

M ~~~~~strtsh eoo Aviation Safety/ Automation Programr Conrternce

MACE * V. ROBERT 0. NASA-RP-12441 p 33 1,91-18505 Repout 01 the. orkariop on Ariation Safety/ Automnation

ife if Sppot Eolgicl ysem Naurl nd MCMASTER. LEONARD R.Prga 4ed coloicalLifeSuport ystes Nauraland SAGE 1 data user'a guide rga A cosystems [NASA-RPP12751 p 4N2.39 )NASA-CP-100!,41 p9 N91 l5t4"

.4 P-10040 i p40 14,91.247'44 MCUILUMN S. NAOMIfp3 N2- MORRELL. FRIEDERIC R.

M A P 3M, LEN J.Naver-liaesan Eu soutins or ee-tcl ifJoint Unrversty Program lot Air Transportation MA~" 344.GLNN 5. aver-toks ad Ele soutins orleesid fows ove ReseachI. 11969-1990 iry geoscienCe. 19119- 1990 supersonic defta wings A correlation with expenrnrent I NASA-CP-30951 p I N9 1-19024 a-SO I-08 p 50 N92-28345 J NASA.TP-30351 p 4 N91-13-401 Joint Univer0sitly Program tar Air Tranaportation

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ion of cloud oetection instrumnents and NASA-LaRc Flight-4:ntica Digital Systems Technology INASA-CP-31311 p 3 NO2-17984 inca o at sninar-llow leading-edge test articles Workshiop liSALeaingEdg Fliht-estProram NAS-CP1008J p11 912200 MORRIS. W. DOUGLAS %SA rogam eadng-dgeFlthl-Tst NAS-CP-002) p11 91-42M Parametric rade0 Studier on a Shuttle 2 launch System 0 -2888ji p ItI N91-24199 MEILFI. S. HARVEY architlectune

MAiCi. WES C. The role of water vapor in climate A strategic researchl INASA-TP-30691 P 14 N97I lf80

.dationofeahuman force model to predticdynamic: Plan for the proposed GEWEX water vapor protect MIJKUNOA. H. S. * ulting front multi-Koint motions (GVaP) w-iesoastblyofam rras

a. -32061 p I N92-26538 INASAr-CP-31201 p35 N9V 25556 (A -Twodienina1 I sablt y laminar2f71es

boil and Prediction of dynamic riuman isolated MELSON, N. DUANEDietsuaioolhg-pdnliglars

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MA ANY A. INS-i-12 7N22t3 Ninneir-Stoies and Euler soutilons for le-so flow over

4vy training MELSON, W. EDWARD. JR. Sproi et ig orlto ihepnnn Wind tunnel aerodynamic charactenistics 0of 'NSA.TP-3035 ig ACfwW pet ith N91.13401 P. 1253) p 15 N92-32456 aNs91.13fd eay0ai8easottV 'NASrtoi'35 pn 

M~lv 0.environment PIAIVIDD 

arliening functions is derived from alo-ig-track I NASA-TP-318-41 p08 N92-31 532 N of0 the ERBE scanning radiometers for August MELTON, JOH4N E.

1241 p4 O I-1Transonic and supersonic Euler computations 0f NAFIEL..J. CH4RISTOPHER P 14,p34N1163 vortexi-dominated flow fiels about a generric fighter Perenalet-. trade studies on a Shuttle 2 launch system

MA,0'- " AEL J. JNASA-TP-3tt61 p 6 N92-10011 architecture and analyses of research on supersonic MENON, P. K. A. (NASA-TP-30591 P 14 Not-Ifi1SO 10 t-lif" minminzation with recommendations for Application and fliht test of minanziing tiansformations, NAUGLE. JOHN E. gnl using measurement feedbaclr to the nonlinear control First among @equas The selection of NASA apace -- P-32021 p) 9 N92-33656 problem science expenme~nts

MAPl' 4, MICHAEL A. [NASA.TP-315-4) 12 N91-30154l INASA-SP-42151 p 52 N91-2806

?eomnetry effects on rotor blade-vortex interactioni .. iAKE-LYE, RICHARD C. MEALY. JOHN E.

act"tt The atmospheric effects 0f Stratospheric sircraft A first Cellular track model of biologicial damage -o nmammalin

-- P-301t51 p 44 N,191-12315 Program report cell cultures from galactic cosmic rays

MA-- L, J, R. (NASA-AP-12721 p 33 N92-19t21 JNASA-TP-3055i P50 N91-16981

logy on Masr' MICOL. JOHN R. Radiation protection for humnan missions to the moper

- P 10055) p 41 N91-15691 Simulation 0f real-gas effects on pressure distributions and Mars

MA; '- 1. M. for aeroasWSit flight experiment vehicle and compripason [NASA-TP.30791 P50 N91-I 7999

5eomelry effects on rolor bladfe-vortex interaction with prediction Transport methods and interactions; for space

Icr'vrty [NASA.TP-31571 p 27 N92-20677 radiations

P-3015) p44 N91-12315 MIILS ATI . R NASA.RP-12571 p 51 N92-15956

MAS Nr 1i ARY L Buckling and vltiratioet analysis of a simply supported MIRACAL A mission radition calculation program for

Opulsive Characteristics of canted twin column with a piecewise constant cross section analysis of lunar and interplanetary missions

Zornqnozzlesat Mach 020 to 1 20 (NASA-TP-30901 p 29 N91-20503 )AAT-21 S O-50

P-30601 p 5 N91-22069 NI.J ELSON. MARK

M J- , UGSTS .Effect of type of load on stress analysis of then-walled Biological Life Support Technologies Commercial

M A. y AU of huSttle recin. ie ducts Opprtunitres -St eatin ~ aShffe imr NASA-TP-32481 p 31 N92-26669 INASA-CP-30941 p36 Ngi-i16842 P P31761 p 4 0 N92 -$6562 Applications of FEM and OEM in two-dimensional NEMETH. MICHAEL P.

'ic and concentric muscle pertormance following fracture mechanics problems Axisymmetric Shell analysi Of the space shufttl SOli Isimulatedl weightlessness (NASA-TP-32771 p 31 N92-31 280 rocket booster field joint - P-31e21 P 39 N92-17645 MtNECK. RAYMOND E. I NASA-TP-30331 p28 N191.14618

MCA R. K_ W Calibration of the 13- by 13-inch adaptive wall test Buckling behavior of ong symmetricallfy arnwalod plates

0)015 wing pressuire and trailing vortex section f a' the Langley 0 3-mefer transonic cryogenic subleced to combined loadings nents tunnel INASA-TP-3195) p 22 N192-251W0 N P.3tsl1I p ft N92-10901 I NASA.TP-3049) p 13 5191-13461 NETTLE&. A. T.

Mf W; J0OHN.J. Compoansoin of a two-dimensional attaptive-wall A novel method ol fasting the shear strengtht of thick

f simulated weightlessness lectiniques INASA-TP-31081 p?1 N191-21242

- P-31621 N 592-176-45 I NASA-TP-31321 I N92-204h14 An eamarinetiari of the damage tolerance enhancement

Mr C' 114i. CK. M. PATRICK MINIS. IOANNIS Of carbon/epoiry usin an outert lamina of spectra ffR)

'ltt Internationial Laser Radar Conference. part The effeet of bandwidth on ferlerobot system INASA-TP-31601 Ip 21 tN92-l1t142 performance NEWMAN. J. C.. JR.

;P 31 56-PT I) IP28 N192-29228 INASA-TP.31521 p 28 N9 1-305-40 Stress concen1trations for straighl.shank arid

-- nth international Lase Radar Conference. pert MISHIIA, S. K. counitersuink holes in plates subtected to tension, bending

Mirobiolog~y on, Space Station Freedom and pin loain

N 'P-3t58,PI-21 P 28 N192-31013 )IiASA.CP.31081 p37 N914t8573 I)NAt3A-TP-31921 p 31 N192-25997

8-7
NEWMAN, PERRY A. PERSONAL A UTHOR INDEX

Analysis and prediction of Multiple-Site, Damage (MSDI PANDYA. ASHILASH K. PORRO. A, R,

tat"gu crack growth The validation of a huma~n force model t0 p18-lict dynamic Evaluatilon 01 a tocrnioule to generale anoic~aily

(NASA.TP.3231 1 p 31 N492-31279 forces resulting trom mulli-point motions thickened boundary layers in bupffrsonic arid hyperrorvc

NEWMAN, PERRY A. I NASA-TP- 3206! p 40 N492-26538 flows

Wail-interference assessment and correctionis for Correlation and predictton of dynamic human isolated I NASA TP-:314Z! 06N9Iý8!6

transonic NACA 0012 airfoil data from various "rind point strength from lean bodzy mass POTTER, ANDREW funnels I NASA-TP-32071I p 40 N492286682 Orbital delofs Technical i5s%,$ arid future 0riect.ns INAS.TP-0701PS N1-2043INASA-CP 10071 v049 N492 33478

INEW ATON, REDEIC p51412. PARMA. GEORGE F, POVINELLI, LOUIS A.

A mediodfa evaluating aftficiency during space-suited Developmentt of a truss paint tar robotic assembly o1 Workshrop on Engineering T .rtulence Modeling

work in a neutral buoyancy environment spce structures N1ASA-CP- 10081I p27 141224514

(NASA.TP.31531 p 40 N492-19772 NAAP324p119-274 POWFLl.. K. A.

-:GO, DUC M. PARMAR, DEVENDRA S. SAM 2 measurements of the polar stratospleric aeoroso Track structure model of cell damage in space tlight Positron lirtetime measuremeintsrin chiral neinetic liquid Volume 9 October 198? April 1983

JNASA-TP-32351 p 39 1492-3415.4 crystals I NASA-RIP-12441 p33 N149r1t50t5

NICOL, DAVID M. [NASA.TP.31221 p 46 N492- 10617 POWERS. CHARLES E_

Advanced techniques in reliability model representation PARRISH, RUSSELL V. Long-term tile testing of Geostationary Opeiatlorai

and solution Effect at snort-term exposure to stereoscopic Environmental Satellite IGOESI encoder tamps

INASA-TP-32421 p43 N92-37-.t3 three-dimrensionael flight displays on real-world depth INASA-RP- 12 731 p 23 -N92 20j63

NIEDRA, JANIS M. perception PRATH4ER. M. J.

The 23 to 300 C demagnetization resistance 0f I NASA-TP-31171 pIt I1N92-13065 The atmospheric efttacs of stratospheric aircraft A

samanum-cobalt permanent magnets PATNAIK. SURYA N. topical review

INASA.TP-31191 p25 1492.11252 cuayfr tieeeetsrutrlasyi Impoe ASA-RP-12501 o033 Ng i 16466

NISSIM. ELI vi iteracytar accu finite meteethtutuaonayi PRATHER, MICHAEL J.

Design of control laws tor flutteir suppression based on vIaSAT-24 a new integrated methodcefcs Tohc fsrtopei acii is

the aerodynamic energy concept and cornparisons with AA-T-20 p3 The Vam-222 atos~rrecefas0 taoliecaril

other design methods PATTERSON, JAMES C., JR. Iga NAArePoi221p33N292

[NASA-TP-30561 p 29 N491-10328 Effect of location of ett-mounted nacelles on the PROTZEL. PETER W,

NOOR. AHMED K. longitudinal aerodynamic characteristics at a high-wing Fault tolerance ot artiticial neural neteorkst with)

Research in Structures. Structural Dynamics and transport airplane applications in Critical systems

Matenats, 1990 (NASA-TP.30471 p 4 N91-13402 IlNASA.TP-3187! p 4

2 N492-222185

INASA-CP-30641 p 29 N491-10301 PIENDERORAFT. ODIS C., JR. P5JESCHEL. RUDOLF F.

Free vibrations at thin-walled semicircular Paraetriec study of afterbody/nozzle drag on twin Internalitionall Workshop on Stratosphrtiec Aerosols

graphte-epoxy composite frames twc -dimensional convergent-drivergent nozzles at Mach Measurements, Properties, arid Eftects

INASA.TP.3010; p 29 N491-13750 numbers tram 061) to 1 20 INASA-CP,31141 p 32 N491-32528

Computational methods for finctionless contact with INRSA.TP.26401 p

4

l 1,19114316

application to Space Shuttle Orbiter nose-gear tieas Static thrust-vectoning pertonmance of niontaxisymmetnic

I N4ASA-TP-30731 p 30 N491-22576 convergent-drivergent nozzles with post-evil yaw vanes

Conmputational Structures Technology for Airframess and 1 NASA-TP,30e5 p 5 Ng491-21059 OUEIJO, MANUEL J.

Propulsion Systems Installation effects ot winng-mouinted turbofan Benefits trom synergies and advanced technologies for

INASA-CP-3142j p 31 N492-25911 nracelle-pylons one a /17.scals, twirn-engine, t ow-wing an advanced. technology space station

NOREURY. JOHN W. transport model NS-PD61p4NR207

Transport methods and irnteractions for space (NASA-TP-31681 p 7 1492-19002 NAAT301P14 41-17

radiations PENN, LANNINO M.

IN4ASA-RP-12571 p51 N492-15956 Nimbus-7 TOMS Antarctic ozone atlas: August - R

December 1990

(NASA-RP.12641 p35 N491-26651 RANEYDAVID L

0 PEREZ. SHARON E. Control integration concept lta hypersonsic cruise-turn

Static tootprint local forces, areas. and aspect ratilos maneuver-s

OLSEN, LARRY E. for three "yp 7 aircraf twres INASA-TP-31361 P 13 N492-20195

Large-scale aeroacouslic reseatch feasibility and I NASA-TP-29631 pl 10491-17014 RASH, JAMES L

Conceptual design 0f test-sectioin inserts tar thle AMeS S0- PETERS. JEANNE M. The 1991 Godd..-'t Conference on Space Applications,

by 120-toot wind tunnel Free vibration$ of thin-walled semicircular of Artificial Intelligence

I NASA-TP-30201 p45 N491.19824 graphirte-epxty composite frames ( NASA-CP-3t 101 1)43 1491 22769

OUTLAW, RONALD A. I NASA- TP-301 0 p 29 N491-13750 The 1992 Goddard Conference on Space Applications

Surface effects on hydrogen permeation through PHAN, MINHI 0. of Artificial Intelligence

Ti-14AI-2lifb altoy Identification ot linear systems by an asymptotically INASA-CP.3141 p p4

3 14923356

INASA-TP-31091 p 23 N91-20266 stable observer RASHID, MICHAEL

OVERTON, ERIC [NASA-TP-31i'iI p 31 N492-26537 Evaluation of nonmirivsi cardiac output methods during

The 23 to 300 C demagnetization resistance of PHILLIPS. ROGER J, exercise

samairium-cobalt permanent magnets Planetary geosciences. 1989-1990 ( NASA-TP-31 741 p 38 N492-16553

INASA-TP-31 19) p 25 N492-11252 I14ASA-SP-508, p 50 N492-28345 Reliability of e Shuttle reaction timer

PIERSON. DUANE L INASA-TP-31761 p 40 1492 16562

Microbiology on Space Station Freedom RE. RICHARD J.

P NASA-CP-311081 p 37 N491-18573 Static internal performance 01 ventral and rear nozzle

PINKERTON. THERESA L Concepts tar short-takeoff and vertical-landifng aircraft

PAOULA. SHARON L Planform, curvature effects on ftutter characteristisc at INASA.TP-31031 p 6 N492-10975

Multidisciplinary OptimnizatiOn of controlled space a wing with 56 deg leading-edge sweep and panel aspect Installation effects of winrg-mounted turbofan

structures; with global sensitivty equations ratio ot 1. 14 nacelte-pylons on a 1/11-scaleL hntw-in-egine, low-win

(NASA-TP-31301 p 18 N492-11087 JNASA-TP-31161 p It IN92-1305-4 transport model

PALASZEWSKII BRYAN PLENTOVICHi. E.S0. [NASA-TP-3t661 p 7 N492-19002

Lunar missions using chemical propulsion: System Effects of yaw angle and Reynolds number on Parametric investigation ot single-expanison-ramp design issues rectangular-box cavities at subsonic and transonic nozzles at Mach numbers tram 0 60 to 1 20

(NASA-TP.30651 p 19 N491-15308 speeds I NASA-TP-32401 P 9 N492-34193

PALASZEWSKI. BRYAN A. I NASA-TP-30991 p 5 N491-27124 REARDON, LAWRENCE F.

Metallized propellants tar the human exploration ot POE (-, C.. JR. Thermal and structural tests at Rene 41 honeycomb Mars NASA woritahop on impact damae" to composites integral-lank concept for future space transportation 114ASA-TP-30621 p 19 N149-11600 INASA-CP-100751 p 21 N491-29240 systems

Upper stages using 'luid propulsion and metallized POLITES, M. E. (NASA-TP-31451 p 30 1492-24205

Propellants A scheme for banidpass filtering magnetometer REYNARD,11W. 0-0

I14ASA-TP-31911 p 20 1492-17151 measunfrements to reconstruct tethered satellite sk'prope The development at the NASA avition safety reporting PALUMBO, DANIEL L motion system

Model reduction by trmmingfor a class of serm-Marltav (NASA-TP-31231 p42 N491-256.29 I NASA-RP-I1t141 pl 10491-70436

reliability models anid the corresponding error bound A nonlinear estimator ota reconstructing the angular RI4EINFURTN, U. . - I NASA-TP-30891I p 43 N491-25741 velocity ot a spacecraft without rate gyros Methods of applied dynamics

Fault tolerance ot artificial neural networks with INASA-TP-31781 p 24 N492-13343 I14ASA.RP-126?I p?24 149125303

applicartilons in critical systems Definition and design of an expeniment to test raster RICE. BARBARA L.

INASA-TP-31871 p 42 N492-22285 scanning with rotatinig unbalanced-mass delvicest on Nutritional Requirements for Space Station Freedom

Experimental validation ot clock synchronization gimnbaled payloads Crews"

algorithms INASA-TP-32491 p 24 N492-29677 [NASA-CP-31461 pC 140 92-25961

I14ASA.TP-32091 p 42 N492-27589 Recontiguring the RUM experiment to lest circular RING, DARRYL S.

Advanced techniqu~es in reliability model representation scanning with rotating unbalanced-mass devices on Graphitefepany composite adapters tar the Space

and solution gimbaled payloads Shuttle/Centaur vehicle

I NASA-TP-32421 p 4 3 1492-3348.3 INASA-TP-32821 p 25 N492-33601 I NASA.TP-30141 p 15 1492-31251
PERSONAL A UTHOR INDEX SINGER, BART A.

ROBERTS, F. E.. fIt# SCHIMMERLING. WALTER S. A trveed lmnanal intrue oainemer thermal, qinecrharca,

Optical measurements ont solid specimens of solid rocket Transport methods and interactions for space analytical technique for irgti Pertormiance travelin wae"

motor exhaust and solid rocket motor slag radiations tubes

I NASA-TP-31771 p 20 N92-20949 I NASA-AP-125,71 p 5 N92 15956 1 ASATP 30811 p 25 N91 27436

ROBINSON, MARTHA P. SCHLICKENMAIER. H4ERBERT SHEN. CHIN-4ING

Failure behavior, of generic metallic and Composite Airborne Wind Shear Detection and Warring Systems Flealiblijity, Study Of a Ow energy gammra Fay system 10,

aircraft structural componentjs under Crash l0oads Second Combined Manufacturers and Technoiogists Measuring quantity and flow tate of Slush hydrogen

I NASA-RP-12391 p29 N91-t375t Conference, part I INASATPar15o p 19 N92-2514a7

Computational methods for frictionless contact with I NASA-CP-tOOSO5-PT-t 1 p 9 N91 11682 SHEPHERD. KEVIN P.

application to Space Shuttle Orbiter noega two Airborne Wind Shear Detection and Warning Systems Wind turbine acoustics

I NASA-TP-30731 p 30 N91-22576 Second Combined Manufacturers' and Techrnologists, I NASA.rP-30571 P44 N149 16679

ROCHELLE, WILLIAM C. Conference, part 2 A loudness calculation procditiore applied to shaped

Stagnation -point heat-transfer rate predictions at JNASA-CP-tOOSO-PT-21 P9 N91-It695 sonic booms ar , 3sst flight conditions Airborne Wind Shear Detection and Warning Systems I NASA-TP-31341 0 45 N492 1176

INASA-TP-32081 p 27 N492-31281 Third Combined Manufacturers and Technologists' SIEE .O4 Conference. part 2 SIEEJH

ROPER. MARY L 1NASA-CP-10060-PT.2] p 9 N91-24140 Thermal and structural tests of Poe@ie it honeiycomb Eccentric and concentric muscle Performance following AiIreWn ha eeto n ann ytems integral-tank concept ice futuure space lrarsrioftaticrr

7 days ofemlatdeihtlsses Third Combined Manutacturers' and Technologists systems

INSAPp12 p39 N92-176.45 Conference, part i NASA-TP-31451 p 30 N492 24205

ROSSONI. P. iNASA.CP.10060-PT-1 I p 9 N91-24166 SHIER. DOUGLAS R.

Cable compliance SCHMELTEKOPF, ARTH4UR L Structural factoring approachn lor analyi stochastic

INASA-TP-32t61 p 24 N492-30378 The atmospheric effects of stratospheric aircraft A first nerworkis

ROSTAFINSKI, WOJCtECH Program report INASA.TP-3091 p 43 N91 18753

Monograph on propagation 01 sound eaves in curved [NASA.RP.12721 P 33 N92-19121 SHIM. T4.-H

ducts SCHMIDT. JAMES F. Workshop2 on Engineering Turbulence Modelin

INASA-RP-12481 p 44 N91-15848 Design and perlorance of controlled-diftfusion stator I NASA-CP-t100881 P 27 N92 24514

ROWELL. LAWRE ACE F. compared with original double-circular-arc; stator SNIMSKI. JOHN T.

Thermal-distontion linaltysis of a spacecraft box truss in (NASA-TP-28521 p 12 N492-22663 Development of a lull scale transmission testiN

geostationary orbit SCHOESS, JEFF N. procedure to evaluate advanced lubricants

I NASA-TP-30541 p 16 N91-11041 The microgravity environment of the Space Shuttle I NASA-TP-3265i p 28 N492-30396

Launch vehicle integration options for a large Earth Columbia middelck during STS-32 SIINN. JUDY L

sciences gelostationary platform concept I NASA-TP-3 140) p 48 N492-11930 Cellular track model ot bioilogicall damage to mammairan

I NASA-TP-30831 p 15 N491-27180 SCHULTZ. K.-J. cell cultures from galactic cosmic rays

ROWLAND, MICHAEL W. Wakte geometry effects on rotor blade-vortex interaction [NASA-TP-30551 p50 N491.16981

SAGE 1 data user's guide noise directivity Improvements in computational accuracy of BRYNTAN

INASA-RP-1275J p 34 N492-33097 I NASA-TP-30151 p44 N491-12315 (a baryon transport code)

RUMMEL. JOHN D. SCHWARZ. RAY P. INASA-TP-30931 pl Nt191.23017

Fourth Symposium on Chemical Evolution and the Origin Analysis of gravity-induced Particle motion and fluid Radiation nisk Predictions for Space Station Freedom

and Evolution of Lila perfusion flow in the NASA-designed rotating orblt5

(NASA-CP-312g) p 41 N92-13588 zero-head-space tissue culture vesselI NASA-TP-30981 pS N1191 -26107

RUNYAN, L JAMES I NASA-TP-31431 p 24 N92-13340 Transport methiods and interactions for space

Lewtis icing research tunnel test of the aerodynamic Experimental measurement of the orbital paths 0f radiations

effects of aircraft ground dieicing/anti-ifcing fluids Particles sedirmenting wrthn a rotating viscous fluid as INASA-RP-12571 p 51 N492 15956

1 NASA-TP-32381 p t0 N92-30395 influenced by gravity Multiple lesion track structure model

RYAN. R. S. JNASA-TP-32001 p 40 N492-28897 (NASA-TP,31851 p 39 N492 221866

The role 0f failure/problems in ertgineening: A SCIALDONE, JOH4N J. An efhvcrent H-ZETRN (a gatactic cosmic ray traensport

commentary of failures experienced - lessons learned Oulgassing data for setileciting speciat~at rmatenials, code)

INASA-TP-.32131 p 24 N492-22235 revision 2 INASA-TP-31471 p51 N492-22218

RYAN, S. G I NASA-RP-1 124-REV-21 p 21 N91-14437 Track structure model of call damage in space Ilightl

Limit cyc~e vibrations in turbomnachinery SCO`TT. A. DON I14ASA-TP-32351 p 39 N492-34154

(14ASA-TP-3i61 I p 20 N92-14108 Rigid-body-control subsystem sizing for an Earth science SHIVFAKUMAR, K. N.

geosatioaryplatormStress concentrations for straight-shank and

geI NS- aioir Platform7N9-230 countersunk holes in Plates subjected to tension. bending, (NAS-TP3067 p 7 141-2302 and Pon loading S SCOTT, COURTNEY J1. [ NASA-TP-31921 p 31 N492-25997

Nimbus-7 TOMS Antarctic ozone atlias August - SHRADER. CHRIS R.

SACHSE, GLEN December 1990 The Compton Observatory Science Workshop Venturi air-p~i vacuum electors for high-volume (NASA-RP-i2641 p 35 N91-26651 fNASA-CP-3t371 p 49 N492-21874

atmospheric sz D 'ng on aircraft platforms SCOTTI. STEPHEN J. SHUART, MARK J.1

[ NASA-TP-3183 p I1I N92-20546 Numerical studies of convective cooling for a locally Experimental behavior of graphite-epoxy Y-sltl"ened

SALAS, MANUEL L healed skrin specimriens loaded in compression Shock wave in riction with an abrupt area change INASA-TP-31001 p 26 N491-22"0 (NASA-TP-317i I p 30 N492-23115

INASA-7P-31131 p6 N91-27140 A simplified method forlthermal analysis ofa co-wlleading SICONOLFI. STEVEN F.

SANDFORD, MAYNA, , C. edge subject to intense local shock-wave-interference Evaluation of noninvasive cardiac output methods duning Plenform curvature :'facts on flutter characteonslics, of heating exercise

a wing wrh 56deg I" ng-edge sweep and paneltaspect (NASA-TP-3167) p 2? N92-24797 (NASA-TP.3t741 p 38 N492-16553 ratio 0f11. 14 SEASHOLTZ. RICHARD 0.. Fuel utilization during exercise after 7 days ot bied rest

INASA-TP-31 161 p I I N92-13054 Laser anemometer measurements and Computations in IHASA-TP-3175) p 38 1492- 16554

SANKARAN. SANOARA N. an annular cascade of high turning Core turbine vanes Reliability of a Shuttle reaction ntmer

Surface effects on hydrogen permeation through INASA-TP-32521 p 8 N92-28980 (NASA-TP-31761 p 40 N492- 16562

T-t.4Al-2114L alloy SEKAR, B. Eccenti. and concentric muscle Perto mance toltowiing

(NASA-TP-31091 p23 N491-20266 Direct simulation of high-speed mixing layers 7 days of simulated weightlessness

SANKARAN, SANkARA N. (NASA.TP-31861 p 8 N92-30909 INASA-TP-31821 p 39 N492-17645

Oxidation characteristics of Ti-25A1-tONb-3V-1Mo SELLERS, WILLIAM L. III SIM, ALEX G.

intermetallic alloy Detailed tlow-ftield measurements over a 75 de wp Flight characteristics of a modtified Schweizer SGS 1 -36

[NAS-TP3044 p2 N911352 deta ingsailplagne at low and very high angles of ettack

SAVELY, ROBERT T. INASA.TP-29971 pit N491-18030 SIMON.SA-RED30R21 12NF.-10

Fourth Annual Workshop on Space Operations SHASSIR, A.SIOFE RCK.

Appticaw'~ns and Research (SOAR 90) Worlishop on Engineering Turbulence Modeling Modeling of the heal transfer in bypass transitional

I NASA-CP-3103-VOL-1 I p 41 N491-20641 I NASA-CP- 10088) p 2? N92-24514 boundary-layer flows I NASA-TP-31701 p 27 N492-11299 Fourth Annual Workshop on Space Operations SI4ALKHAUSER, KURT A. SIMONSEN. LISA C. Applications and Research (SOAR 90) A three-dimensional linite-lement theffrmal/mechanicatl Radiation protection for human missions to the Moon

I NASA-CP-3103-VOL-21 p 41 N491-20702 analytical technique for high-performance traveling wave and Mars

SCALLION, WILLIAM 1. lubes I NASA-TP-30791 p50 1491-17999

Advanced Hypervefocify, Aerophysics Facility INASA-TP-3081 p 25 N491-27436 Transport methods and interactions for space Workshop SHALKHAUSERt, MARY JO radiations

I NASA.CP ,J 3 p 13 N9 1-24211 Destination-directed, packet-swirtchin architecture for (NASA-RP- 1257) p 51 N92- 15956

SCANLON, , IARILES H. 30/20-GHz FDMA/TDM geostationary communications MIRACAL A mission radiation calculation program for

Flight teats with a data link used for air traffic control satellite network analysis of lunair and intearplaeary missions

information exchange INASA-TP-32011 p 16 N492-19762 INASA-TP-32111 IpSI N92-25100

JNASA-TP-3t35j pit N91-31,143 SHARP, G. RICH4ARD SINGER. BART A.

SCHATTEN. KENNETH H. A new fabrication method for precision antenna A weakly nonlinear thefory fon wave-vorltex interactions

Climate Impac of Solar Variabillityi reflectors for space flight and ground fest in curved channel flow

INASA-CP-3086l p50 N491-12456 INASA-TP-30781 p 17 N491-21 185 INASA-TP-31581 p 7 N92-19175
SINGH, JAG J. PERSONALI A UTHOR IN'DEX

SINGH, JAG J. SPRINKLE. DANNY R. STONE,, NOGlE H.

An investigation of mrcrostructural characteristics of investigation of microstructural Changas in cuoient Goiieciion lhorn Space Platirras

contact-lons polymerse polyetherether-lrelonb films at cryogeiiic temperatures by NASA CP 3089 jp46 fN91 1~17,3

(NASA-TP-3034 P p21 N91-)13492 positron lifetime spectroscopy STREET?, CRAIG L

investigation Ot mictrostructural changes in [NASA TP 30641 p 21 N91 18L216 validation of three dime ascnal rincompressible iiPA14

polyetherether-ketors il rms at crogenic temperatures by Feasibility study of a low-energy gamma ray system lot direct numerical simulatio code A comipafisorinl'ira

positron lifetime spectroscopy mreasurin-g quanrtity arr. flow tate ot slush hydrogen stability arrd parabolic stabotfy eq-,al~oi frieoires 1ci

I NASA-TP-30641 p 21 N91 18216 INASA.TP.3t501 p 19 N92 25147 boundanyiayoer tranrsitiorn on a tuft plate

Low-energy positron tiux generator for mtcrostruCtural SQUIRES, WILLIAM I NASA-TP 32051 p 8 N92 30295

ctharacterization ot thin tilms Techrniques ota d"tarmination at impact torces durnirg STRIEPE, SCOTT A.

I NASA-TP-30?4 I p 27 N91t 22538 walking and runninrg ir a zero.G environment MIRACAL A mission radiattcn Calcuilation programn lo

Positron lirtetimne measurements rn chiral nernaltr liquid I NASA-TP-3t591 p 38 N92 17022 analysis of lunar srid interplanetary missions

crystals SQUIRES. WILLIAM G. I NASATP3?t tl p 5! Ng?-25rbC

I NASA.TP-3t221 p 4 6 N92 10677 A method ot evaluating etficrency during space suited SUDER. KENNETH L

Feasibility study of a low-energy gamma ray system tOe' worli in a neutral buoyancy environment Design and perormance at conilroliied dift,-ion Valaor

measuring quantrty and tlow rate of slush hydrogen INASA-TP-31531I p40 N92 '9772 compared with orrginal doutble-circular-arc stailor

JNASA-TP-3150ý p 1

9 N92-2514 7 ST.CtAtR, TERRY L INASA TP 28521 p 12 N92 22663

SINGH, NAGENDRA Investigairon ot microstructural changes in SULENTtC, JACK W,

Current Coltactro,, from Space Plasmas potyetherether-ketone films at cryogenic temperatures by Paired and Iriteractinig Galiaxes IiteornaliorIa

[NASA-CP-30891 p 46 N91-t7713 positron itetirhe spectroscopy Astronomical Union Coibr:uium No 124

SLEIGHT, DAVID W. JNASA-TP-30654) p 2

1 N91 t8216 1 NASA-CP-30981 p 49 N91 16856,

On-orbrt structural dynamic Performance Of a 15-melte Low-energy positron tlux generator for micr~ostrucltural SULLIVAN. BRENDA M,

microwave radiometer antenna characterization of thrrr films A loudness caiculatron Procedure applied 10 shaped

tlNASA-TP-3041 IPIS N91t171t4 INASA-TP-30741 p?27 N91-22538 sonic booms

SMITH, CHARLES A. STALLINGS, ROBERT L. JR. I NASA-TP-3 134! p 45 N92 I''765

Aeroacoustrc and aerodynamic applications of the theory Measurements of torces, moments, and Pressures on SWANSON, G. R.

at nonetu~ifibnum thermodynamics a generic store separating tram a box Cavrry at supersonic Applications ot FEll and B3EM in. two~d-inens~onal

I!NASA.TP-31 101 p 26 N91-25352 speeds fracture mechanics Problem's

SMITH, DONALD L [NASA.TP-31 101 p6 N92-iO005 INASA-TP-32771 p 31 N92 31260

Properties of three graphite/ toughened resin STANLEY, DOUGLAS 0, SYDNOR, RICHARD L.

composites Parametric trade Studies on a Shuttle 2 launch system The 22nd Annual Pirecise Time and T ime interval IPTTt)

[NASA TP-3t0?j p 21 N92-10067 architecture Applications and Planning Meeting

SMITH. G. LOUIS [NASA-TP-30591 p 14 N9t-taraO [NASA CP-31161 p 44 N91-25 755

Limb-dlarliening functions as derived trom along-track STARNES, JAMES H., JR. Proceeings of the 23rd Annual Precise 'ime and Time

operation of the ERBE scanning radiometers tor August Computational Structures Technology tor Arirtrarnes and interval IPTTII Applications and Planning Meeting

1985 Propulsion Systems [NASA-CP.3159' 0 44 N92-373350

1NASA-FlP- 12431I p 34 N91-14683 [NASA-CP.31421 p 31 N92-2591 I SYDOW. P. DANIEL

Atlas ot wide-tireld-of -view outgoing torxgwave radiation Eighth 000/NASA/FMA Conference on Fibrous Experimental behavior 0

of grapriite-eipoty Y slititned

derived from Nimbus 7 Earth radiation budget data Set. Composites in Structural Design, part I specimens loaded in compreswion

November 1985 to Octobrer 1987 1 NASA.CP-3087.PT-tlI p2 2 l"92-32513 INASA-TP-3t71, 030 N92.23ni5

1NASA RP- 12611I p35 N91-24719 Eighth 000/NASA/FAA Conference on Fibrous

SMITH, LEIGH ANN Compositesoi Structural Design. Part 2

A method tar the design of transonic flexible wings INASA-CP-3087-PT-21 p22 N92-32574 T

j NASA-TP-30451 p 10 N91 14321 STARR,0. OC.

Applications ot a direct/ierative design method To The role of water vapor in climate A strategic research TAKAHASHI. R. K.

complex transonic conftigurations plan for the proposed GEWEII water vapor project NACA 0)015 wing pressure and trailing voirlex

INASA- TP-323-41 p 8 N92-33484 IOVaPI measurements

SMTH R-ENASA.CP-31201 p 35 N91.25556 1 NASA-TP-315t p 6 N92 1,981

NASA Workshop ontfuture directionis insurface modeling STSI OLShotoig in grud tsig enromt TALAY, THEODORE A.

and grid generation Socoig in gon teig, nvrmnt Parametric trade studies on a Shuhle 2 launch system,

INASA-GP-100921 p 8 N92-?9625 simulations. lar~d performance predictions for space architecture

SMIH.ROBRTE.applications INASA-TP-3059i p 14 N91 18180-

Software Surtace Modeling and Grid Generation NASA.T.32t, JO2EP L.2-III TANNER, JOHN A.

Steernog Committee STExHeR.t JSEpHc L. uato Cofrnc ofimn Computational methods ton trictionless contact itrI NASA-CP-31431 pa?2 N92-24397 Sixteewrhnth Sptace SimeltMiolnCnieeneCofrmn application to Spiace Shuttle Olrbiter nose-gear tires

SMITH, ROBERT E., JR. hINASA-CP-30961 7N1 92 T AA-RTE. 307J.p3 91257

Numerical analysis and simulation of an assured crew STEE YE.s. E. TREJ

return vehicle flow field Applications at FEll and BEMl in two-dimensicval Exobiology in Earth orbit The results of Science

I NASA TP-3101 p 26 N92 10161 fracture mechanics problems workshops held at NASA Amen Research Center

SODERMAN. PAUL T. fNASA.TP-32771 p 3t N92-3!280 I NASA.SP 500 1 p4r N9t 147?'5

Flow-induced resonance of sceen-covered cavities STENGLE. THOMAS TATRO. 0.

I NASA.TP-30521 p 25 N91-15499 Flight Mechanics/ Estimation Theory Symposium 1990 Responses 01 women to orlhostatic and exercrse

J-85 let engine noise measured in the ONERA St wind 1 NASA CP-31021 p 14 Ny91 .17073 stresses

tunnel and extrapolated 0o0 fa feld Flight Mechanics/ Estimation Theory Symposium 1991 [NASA.TP-30431 o 31 N91 19711

(NASA TP-30531 p 45 N91-19823 I NASA-CP-31231 pt4 N92-14070 TAYLOR, LAWRENCE W.. JR.

Large-scale aeroacoustic research feasibility and STEPHENS. CRAIG A. The 51h Annual NASA Spacecraft Control Laboratory

conceptual design of test-section inserts for the Ames 80- Modeling Ot the heat transfer in bypass transitional Experiment (SCOIE) Wsorkrshop, pail 1

by 120-toot wind tunnel boundary-layer flows INASA.CP.10057-PT1: p 16 Nol1 18186

1INASA TP-30201 p45 N91-t9824 INASA-TP-3t701 p 2

7 Ny92 11299 The 5th Annual NASA Spacecraft Control Laboratory

Acoustic and aerodynamic study 01 a pusher-Propeller STEPHENS. DAVID G. Expenrtent ISCOLE) Workshop. parr?2

aircraft model Fourth Aircraft Infenor Noise Workshop I NASA CP-10057-PT-21 p 17 N91rI9t22

1 NASA, TP-30401 p45 N,19-21828 fNASA-CP-10t031 p 45 N92-32948 Fourth NASA Workshop on Computatronai Control of

SOFEN.GERLDSTEWART. DONALD F. Flexible Aerospace Systema, part I Biologica GRLifD upr ehooisCmeca Workshop on Exercise Prescription for Long-Duration [NASA-CP.10065-PT-t p 17 N9t -22307 BooiaLieSpotTcnlgeComril Space Flight Fourth NASA Workshop on Computational Control of

Opportunitie94 p 36 N91-13842 SI NASA-CP-305t1 1,p36 N91-10574 Flexible Aerospace Syslrnms. part?2

NSAP-0-ISEWART, ERIC C.INS-P105P-1p1 9 Z3

SPADY, AMOS A.. JR. A companison of airborne wake vortex detection N AC-00-T-lPr Nr233

Airborne Wind Shear Dritection and Warning Systems measurements with values predicted trom potential TELESCO. C. M.

Second Combined Manutacturers' and Technologists' theor Paired and interacting Galaxies International

Conference, p-11 INS-P321pt 9-09 Astronomical Union Colloqtuium No t24

NA1-P t p0 t -t12NASA-CP-30981 NASA-T0-1T- N9N999 p49 N91-1685i8 I Airborn Wind0 Shea Deeto an WaNig Systems2 STIEGLER, JAMES 0.TER

Airorn her Dtetio wnd an Wrnig ystms National Educators' We sthop- Update t991 Standard TEE.JOHN E., JR.

Second Combined M~anufacturers' and Technologists' Experiments in Engineering materials Science and Determination ot the flight hardware conirgurkc'on ot an

Conference part? 2Technology energy absorbing attenuator for the proposed Space

I NASA-CPt1005()PT.21 p9 N9t-11695 INASA.CP.3tstl p 24 N92-30263 Station crew and equipment translation aid cart

SPERA. DAVID A. STOCK. LARRY V. INASA-TP-30841 p29 fy91 21556

Structural properties of laminated Douglas lir/ePoxy Inertial oscillation ot a vertical rotating dratt with THOMAS, DONALD A.

composite material application to a iupercell storm i he micragravity ervironmrent at the Space Shuttle

INASA RP-t12361 p 20 N91-t012 7 [NASA-TP-32301 p 36 N92-33402 Columbia middclck dluring STS.32

SPLETTSTOESSER, W. R. Inertial oscillation at a vertical rotating draft with I NAS-A-TP-31401 p 48 N92.1r9,10

Wake geometry eftects on rotor blade-vOrtex interaction apptication to a supercell alarm Vtdeo supplerment 10 The mricrograviry, environment of the Space Shuilflf

i-.ise ilirectivity, NASA Technical Paper 3230 Columbia payload Day during STS-32

1, ASA-TP-30151 p 44 N91-1231-5 INASA.TP,3230-VIDEO-SIJPPL 1 p36 N92-345246 1INASA.-TP-314, p 049 N92 triIl1t

8-10
PERSONAL AUTHOR INDEX WILLIAMS, R. W,

THOMAS, JAMES L V WALTER, LOUIS S.

Navier-Stokeis and Euler solutions for lee-side flows over VO)canism-Climate interactions

supersonic delta wings A correlation withi experiment VALLETTE. BRENDA J. INASA.CP 10062! p 34 N91 ?1641

1 NASA-TP-30351 p 4 N91-13401 Atlas 0f the Earth~s radiation budget as measured tiy WALTON, MARLEI

THOMPSON, BRAD a. Nimbus- 7 May 1979 to May t980 Technrou~es to(r detwiamiruiaor of mpacl forces doring

Controlled Ecological Lifa Support Systems Natural and INASA-RP-12631 p 35 N91 24 7202 walking arid running in a zero-G environment

Artiticial Ecosystems VANDALS~EM. W. A. I NASA TP-31591 p 3 8 N92 17022

INASA-CP-100401 p40 N9i-24744 NASA Workishop on future directions in surface modeling WANHAINEN. JOYCE S.

THOMPSON, RICHARD A. and grid generation A new labocati~on metriod lor precision aintenna

Calculations and curve fits of thertmodynaimic and INASA-CP-100921 p 8 N92-29625 reflectors for space flight arid ground test

transport properties for equilibrium air to 30000 K VERDERAlIME, V. I NASA TP-30781 p 17 N491-21185

INASA-RP-12601 p 26 N92-1 1285 Plate end butt-weld stresses beyond elastic limit, WASZAX, MARTIN R.

THRONSON. HARLEY A.. JR. material and structural modeling A methodology for computin uncertainty bounds of

The Interstellar Medium in External Galaxies Summaries [NASA.TP.30751 p2 141161 multivariable systems based oil sector stability thaoi-y

of contnbuted papers Structural deterministic safety factors selection criteria cnet

(NASA-CP.30841 p 49 N91,14100 and verification INASA-TP-31661 p 13 N492-2!410

TIBSITYS. THEODORE W. I NASA.TP.32031 p 30 N492-19355 WATSON, A. T. VERHOFF. VINCENET G. Controlled Ecological Life Support Systems Natural and Three-dimensional laser window formation The atmosphieric effects of stratospheric arcraft A Artificial Ecosyistems (NASA-RP-t2801 p 14 N492-30307 topical review

([NASA.CP. 100401 p 40 N491.24744 VICROY. DAN 0. INASA ARP12501 p 33 N91 Itr466

TIELENS. ALEXANDER 0. 0. 111 Airborne Wind Shear Detection end Warning Systems WATTS. G.

Interstellar Dust. Contributed Papers TIhird Combined Manufacturers' and Techinologists' Tecthnique to eliminate computational instability in

INASA-CP-30361 p 48 N91-14897 Conference, part 2 multitody simulations employing ther Lagrange multiplier

TILTON. JAMES C. INASA-CP-10060-PT-2j p 9 149124140 INASA-TP-32201 lp42 N492-23432

Multisource Data Integration in Remote Sensing Airborne Wind Shear Detection and Warning Systems WEAVER, WILLIAM L

I NASA-CP,30991 p 32 N491-15615 Third Combined Manufacturers' and Technologists' Mission description arid 0 flight operations of ERSE

Space arid Earth Science Data Compression Conference, part I instruments on ERBS and NOAA 9 spacecraft. November

Workshop INASA.CP.10060.PT-) p p9 N491.24166 198.4 - January 1986

1NASA-CP-31301 p 41 N92-12425 VILLARREAL, JAMES I NASA-RP-t12561 p 32 192-10206

TOKAZ, J. C. Proceedings of the Second Joint Technology Workshop Mission description and in-filgit operationa of ERBE Resource envelope concepts forn isstooi planning on Neural Networks and Fuzzy Logic, volume t instruments on EROS NOAA 9. and N40AA 10

INASA-TP.31391 p 15 N491-29209 I NASA-CP. 10061 -VOL- 11 p 43 N491-21778 spacecraft

TOLSON, CAROL J. VILLARREAI. JAMES A. INASA-RP-12791 p32 149232127

Mission descnipfion and in-~flight operations of EREE Proceedings of the Second Joint Technology Workishop WEILER, J.30.

instruments on ERBS and NOAA 9 spacecraft. November on Neural Networks and Fuzzy Logic, volume 2 Resource envelope concepts for mission planning

1984 -January 1986 (NASA-CP-10061-VOL-21 pf43 N491-20811 I NASA-TP-3t391 p 15 N91-29209

I NASA.RP- 12561 p 32 N492-10208 VOIELKER. L S. WEILMUENSTER. K. JAMES

Mission description and in-flight operations of ERBE Developrmenf of an integrated aeroservoelastic analysis Numerical analysis and simulation of an assured crew

instruments on ERBS. NOAA 9. and NOAA 10 program and correlation with test data return veficle flow field

spacecraft I NASA-TP-31201 p 2 Ng 1 26113 JNASAýTP.310h1 p26 N492t0161i

I NASA-RP- 2 791 p 32 N142 32127 VOGEL. A. A- WESOKY. HOWARD L

TORRANCE. PAUL R. NASA Workshop on future directions in surface modeling The atmospheric effecfts of stratospheric aircraft A first

Saturation point model for the formation of metal nitrate and gnid geneation program report

in nitrogen tetroside oxidizer (NASA-CP.100921 p 8 N92-29625 J NASA-RP-t12721 p 33 N492-19121

(NASA-TP-3 1071 p 26 N491-24542 VOELEWLFARELM~I ANN, GARY F. TOWNSEND. ~ ~ ~~ VOEL LAWRENCE PoaaineecsfrlnmoieatltestmsrInfluence J. of airfoil geometry on delta wing leading-edge TOWNEND LARENE W.Proagaioneffcts or andmoble stelitesysems vortices and vortex-induced aerodynamics at supersonic Inclusive inelastic scattering of heavy ions and nuclear Overview of experimental arid modeling results sed

correlations [NASA-RP-12741 p 25 N92-20404 INspeed 15sp 7 19220

I NASA.TP-3026] p 46 N491-13985 VOGLER, WILLIAM A. WEST, PHILLIP

Cellular track model of biological damage to mammalian Sfatic tootpririt local forces, areas, and aspect ratios A method of evaluating efficiency during space-sunaed cell cultures from galactic cosmic rays for three type 7 aircraft tires work in a neutral buoyancy environment 1 NASA-TP-30551 p 50 N491-16981 tNASA-TP-29831 pl 10491-17014 [NASA-TP.3153) If40 N492-19772

Radiation risk predictions for Space Station Freedom YOLK, TYLER WEYLAND. MARK

orbits Controlled Ecological Life Support Systems Natural and Improvements in computational accuracy 01 BRYNTAN

i NASA-TP-30981 p 5t N91-26107 Artificial Ecosystems (a baryon transport code)

Blenchmark solutions for the galactic hesavy-ion transport INASA-CP-100401 p 40 N491-24744 I NASA-TP-30931 p 51 1491-23017

equations with energy and spatial coupling VOORHIES. COERTE V. Radiation nisk predictions for Space Station Freedom

I NASA .TP-31 121 p 44 N492-13756 Steady induction effects in geomagrietism Part IA orbita

Transport methods and interactions for space Steady motional induction of geomagnetic chaos INASA-TP-30981 p 51 N491-26107

radiations (NASA-TP-3272-PT-lAl p 34 N492-32655 WEYLANO, MARK 0.

I NASA -RP. 125 71 p 51 N492.15956 Analyse of niskrs associated with radiation exposure

HZETRN A heavy ion/nucleon transport code for space wfronm past major Woar particle events

radiations W NASA.TP.31371 p 50) N91-31061

I NASA-TP-3t461 p 51 N92-15959 WHARTON. ROBERT A_. JR.

TRACY, M. &. WADE, LARRY 0. Fourth Symposium on Chemical Evolutio and the Origin

Effects of yaw angle and Reynolds number on Venturi air-lef vacuum electors for high-volume and Evolution of Life

rectangular-box cavities at subsonic and transonic atmospheric sampling on aircraft Platforms [NASA-CP-3i291 p 41 N492-13588

speeds 1NASAýTP.31831 p 11I N92-205-46 WHITE. ALLAN L

I NASA-TP-30991I p 5 N491-27124 WAGGONER. E. G. Model reduction by tnrimmng for a class of semni-Markov

TURCO, RICHARD P. Prediction 0f effects of wing contour modificafions on reliability modela and the corresponding error bound

The atmospheric effects of stratospheric aircraft A first low- speed maximum lift and tranisonic perormance for the I NASA.TP-30891 p 43 N491-25741

program report EA-68 aircraft WIEDEMANN, KARL E.

JNASA-RP-12721 p33 1492-1912i J NASA-TP-30461 p 4 N491-110902 Oxidation characteristics of Ti-25AI-lONb-3V-tMo

WAGNER, N. SCOWT infermetallitc alloy

FIRE Science Results 1988 INASA-TP-30441 p22 N491-13522

U 1 NASA-CP-30831 p 34 N9 1-10448 WILCOX. FLOYDJ.,. JR.

WAGNR. 0.Experimental RCHAR investigation of porous-floor effecta on UEBEL. MAR14 ~WAGEvauaio ofCAR loD. dtcinintuet cavity flow fieds at supersonic speeds UES MRK valaton f couddetcton nstumets nd I NASA.TP-30321 p5N91-194 The effect 0f bandwidth on telerobol system performance of laminar-flow leading-edge test .1arils Measuremrrents of forces. moments. and preasirea on perormvnce during NASA Leading-Edge Flight-Test Program a generic store separating fronm abox cavity at supersonic I NASA.TP-3t521 p 28 1491-30540 (NASA-TP-2888) I tt N14-24199 speeds

UPCHURCH, BILLY T. WAHLS. DEBORAH M. I NASA-TP.31 101 p6 N492-10005

An investigation of rrrcrostructurat characteristics of On-orbit structural dynanic performance of a 15-meter WILL. RALPH W.

contacltlens polymers microwave radiometer antenna Software design for automated assembl of truess !lNASA-TP-30341 p 21 N491-13492 IN4ASA-TP-30411 p 16 N49 1-17114 structures

URASEX. DONALD C. WALLACE, TERRYL A. I NASATP-31981 p 43 N492-28375

Supersonic Trirouglitlow Fan Test Facility at NASA Oxidation characteristics of Ti-25A-1-tNb-3V lMo WILLIAMS, R. W.

Lewis Research Center tintermetaltic alloy Tenth Workshop for Computational Fluid Dynamic

IFNASA-TP-.t0381 p 13 N492-31640 INASATP-30441 D22 N91-13522 Applications in Rocket Propulsion, part2 USHER. 0. WALLER. MARVIN C. JNASA-CP-3i63-PT-21 p 27 N492-32245

Eroibiology in Earth orbit The results of science Flight deck benefits of integrated dale link Tenth Workshop for Computational Fluid Dynarmuc

workshops held at NASA. Ames Research Center communication Applications ill Rocket Propulsion, part I

INASA -SP.500 1 p At N91-14725 INASA-TP-32191 p 10 N492-21459 IfNASA-CP-3163-PT IlI p 27 N92-32270

B-il
WILLIAMS, ROBERT L., 11 PERSONAL AlUrfOR INDEX

WILLIAMS, ROBERT L, 11 WOODARD, STANLEY E.

Automation and Robotics for Soace-8ased Systems. Multidisciplinary optimiziationr of conritolled space

1991 structures with glalis sensiti-it equations

INASA-CP-t00981 p 43 N92 27763 INASA-TP-31301 P IS N92-11087

WILUAMSL STEVEN P. WOODIS. KENNETH W.

Effect of short-term exposure to stereoscopic Second Conference on NOE for Aerospace

three-dimensional flight displays on real -world depth Requirements

perception [NASA-CP-3091) p 16 N91-18189

INASA-TP-31171 p11 N92-13065 WODOLIFOAD,BARBARA J.

WILLS&IIRE. KELLI F. The validation oat human force model to Predict dynamic

Technology for the Future: In-Space Technology torces re~suilting from multi-joint motions

Experiments Program. part I I NASA-TP-32061 p 40 Ni92-26538

[NASA.CP.10073.PT-1 I p 14 N91-27177 Correlation and prediction of dynamic numan isolated

Technology for the Future: In-Space Technology joint strength from lean body mass

Experiments Program. paW 2 I NASA-TP-320-1I p 40 N92-26682

INASA-CP-10073-PT-21 p 14 1491-27178 WORKMAN, GARY L

WILLSMIRE, WILLIAM L, JR. Second Conference on NDE for Aerospace

Fourth International Symnposium on Long-Range Sound Reqlurements

Propagation (NASA-CP-3091J IP16 N91-18189

(NASA-CP-31011 p4-4 N91-16682 WORNOM* STEPHIEN F.

WILSON. H. 8. Relative efficienicy and accuracy of two Navier-Stokes

Methods of applied dynamics codes for srrulating attached transonic flow over wings

I NASA-RP- 12621 p24 N91-25303 [NASA-TP-3061) p26 N91-17310

WILSON, JOHNW c WRIGHT, K. H., JR.

Two-dimensional aerodynamic characteristlics of several Current Collection from Space Pfasmas

polygon-shaped cross-sectional models applicabl to I NASA-CP-30891 p46 N91-17713

helicopter fuselages WUEBaLES, DONALD J..

[ NASA-TP-32331 p 8 N92-30394 The atmospheric effects of stratospheric aircraft A f:rst

WILSON. JOHN W. program report

Inclusive inelastic scattening of heavy ions and nuclear [NASA-RP-i2721 p 33 N92-19121

correlations

(NASA-TP-30261 p 46 N91-13985y

Cellular track modell of biological damage to mammalian

cell cultures from galactic cosmidc rays

(NASA-TP-3055] P 50 N91-16981 YMS JERROLD M.

Improvements in computationall accurac of BIRYNTRN Calculat ions and curve fits of thermodynamic and

(a baryon transpor code) transport properties for equilibrium air to 30000 K

(NASA-TP-30931 p51 N91423017 [NASA-RP-12601 p 26 N92-11285

Radiation risk predictions for Space Station Freedom YONG DOUGLAS C.

oftts Venturi air-jet vacuum ejectors for high-volume

INASA-TP-3098J p 51 N91 -26107 atmospheric sampling; on aircraft platforms

Analyses of risks associated with radiation exposure [NASA-TP-31831 I II N92-20546

firom pest majo aolar particle events YONO RONALD

[NASA-TP-3137J p 50 N91-31061 Evaluation 0f cloud detection instrumrents; and

Cellular repaigr/miarepair track model performance of larminr-flow leading-edge test articles

jNASA-TP-31241 p 42 N92-11685 during NASA Leading-Edge Flight-Test Program

Benchmark solutions for the galactic heavy-ion transport [NASA-TP-208851 p 11 N9t1-241t99

equations with energy and spatial coupling

NASA-TP-31121 p 44 N92-13756

Transpiort methods and interactions for apace

radiationsZCAYW..

JNASA-RP-12571 p 51 N92-15956 WoNrksho W. on ee ttsan netit

HI-ZETRN: A heavy ion/nucleon transport coda for space WReltioslipo qezdSae n netit

(NAbosAT-16 p tN2 J NSA-CP-31351 P 46 N92-22045

(Nul-TP-14e leio trac strutur1moel9 ZANL.; THOMdAS A.

MulSAtiple 8 struturemode pa 39ac A weakly nonlinear theory for wave-vortex interactions fMAS-TP-1861p 3 N922218 incurved channel flow An efficient HZETRN (a galactic cosmic ray transport [NASA-TP-31 581 p 7 N92-19175

[code) 34] S N222t ZEIN-SABATTOU. &ALEN

[AATrack stutr 47 mode fcelamgiN92-2221 A generalized method for multil robotic manipulator Trak srucuremoel f cll am~i n sacefliht programming applied to vertical-up weldn J NASA.TP-32353 p 39 N92-34154 [NASA-TP-3i031 p 24 N92-1121 B

WING, DAVID J. ZETN HMSA

Statc o a prfomane ucdom nzzl wih mttixis Lewis icing research tunnelt tesg of the aerodynamic tttruat-vectoning and reverse-thrust capabilities effects of aircraft ground rteicingtanti-Kicrg fluids

[NASA-TP-3tae) p 7 N92-23095 I NASA-TP-3238) p 1t0 N92-30395

WITCOFSKI, ROBERT D. ZOLADZ. T. F.

Advanced Hfypervelocity Aeropflysics Facility Time-frequency representation of a highly nonstationary

Workshop signal via fth mockbedi Wigner distrib~ution

(NASA-CP-1003t1 p 13 N91-24211 I NASA.TP-3215) p 25 N92-20492

WODGAN CHRIISTINE F. ZUDER, MARIA T.

Microbiology on Space Station Freedom Planetary geosiciences. 19869-1990

(NASA-CP-3t081 p 37 N91-16573 [NASA-SP-Sflj p 50 N92-28345

Nutritional Requirements for Space Station Freedom ZIJTCK, MICH4AEL 0.

Crew" Structuiral properties of lamninated Douglas fir/epoxy

[NASA-CP-31461 p 40 N92-25961 composite material

WOLF, AVID A. INASA-RP-12361 p20 N91-10127

Analysis. of gravity-induced particle motion and fluid

perfusion flow in the NASA-designed rotatin

weo-head-space tissue culture vessel

(NASA-TP-31431 p 24 N92-13340

Experimental measurement of the orbital paths of

particiles aedimer"tn within a rotating viscous fluid as irifluenced by gravity

[NASA-TP-3200] p 40 N92-211897

WON111 KAM L

Reliability trsining

[NASA-AP-12S3] p 15 N92-32456

WOOD. RICHARD M.

Influeince f airoil geometry on delta wing leading-edge

vortices and vortex-induced aerodynamics at supeirsonic

INASA-TP-31051 p I N92-20038

The natural f'low wing~dsg concept

I NASA-TP-31931 p 7 N92-25202

8-12
REPORT NUMBER INDEX

NASA Scientific and Technical Publications 1991-1992

Typical Report Number NASA-CP-10103 p45 N92-32948 NASA-CP-3153 p 31 N92 28620

Index Listing NASA.CP-3020-VOL-2 ... p 5 N91-24132 NASA-CP-3158-PT-1 p 28 N92-29228

NASA-CP-3036 p 48 N91-14897 NASA-CP-3158.PT-2 p 28 N92-31013

NASA-CP-3049 p 12 N92-22510 NASA-CP-3159 p 44 N92-33350

NASA-CP-3051 p36 N91-10574 NASA-CP-3060 ..... ... p 20 N91-20207 NASA-CP-3160 p 31 N92-30106 ACESIO ..... 9r.I001p27 NASASA30-C..... 3.9 N328 REOTACSIN NASA-CP.30154 p 29 N91.10301 NASA-CP-31&3-PT- p27 N92-32278 NUMBER NASA-CP-3078 p5 N91-21062 NASA-CP-3163-PT-2 p27 N92-32245

NASA-CP-3080 p 27 N91-14574 NASA-CPr3172 p 11 N92-33874

45NASA-CP-3081-3 - p341 N91-17020 NASA-RP-1014 p 21 N91,14437 SNASA-CP-3081-VOL-? p 11 N91-17020

NUMPE1 NASA-CP-3083 .. . . p 34 N91-10448 NASA-RP-14 p33 N9121643?

iN gSA- hs nde are ar3ang fp aN umei-3 NASA-CP.3094 p 49 N91.14100 NASA.RP.125014 p 10 N 16-70436

cy r r b m. r pe e NASA-CP-3065 p 48 N91-15930 NASA.RP-1124-REV-2 p 21 N91-14437

NASA-CP-3056 .................. p 50 N91-12456 NASA.RP-1236 p 20 N91-10127

NASA.CP.3087.PT1 ............ p 22 N92-32513 NASA-RP-1239 p 29 N9I1,3751

NASA.CP.30187-PT-2 p 22 N92-32574 NASA-RP-1243 p 34 N91 .14683

NASA-CP-3088 p 43 N91-12401 NASA-RP-1244 p 33 N9-19505

NASA-CP-3089 p 42 N91-17713 NASA-RP-1246 . p 34 N91.13043

NASACP-101 44 91-1682 NASA-RtP-1248VO2 045 W9-15609

NASA-CP-3090 ................. p 9 N91-10936 NASA-RP-1248 p 26 N91-10418 NASA-CP-3091 p 16 N91-18189 NASA-RP-12 . . p35 N91-2418 Listings in this index are arranged aiphanumeri- NASA-CP-3093 .. . p 35 N91-16500 NASA-RP-1250 p 33 N91.16466

Aally by report number. The page number jn•.icates NASA-CP-3094 p 36 N91-113142 NASA-RP-1251 p 33 N91-1647

the page on which the citation i4 Nocated, 9 he ac- NASA-CP-3095 . ... . .p 1 N91.19024 NASA-RP-1252 p 10 N91-19082

cession number denotes the numb-. 9,y which the NASA-CP-3096 .. ........... p 17 N91-19126 NASA-RP-1253 p 15 N92-32456

NASA.CP3A... p 49 N91-168-8 NASApSA.RP.1255 p42 N91-30531

citation IS identified. NASA-CP-3099 p 32 N91.15615 NASA-RP-1256 p 32 N92-10202

NASA-CP-3100 . p.... 22 N92-2105W NASA-RP-1257 . pS3 N92-15956

NASA-CP.3101 ................ ... p 44 N91-16682 NASA-RP-1258-4 L.1 p 25 N92-10598

NASA-CP-10028 p42 N91.24200 NASA.CP-31102 p 14 N91-17073 NASA-RP.125V . 45 N92.14779

NASA-CP-10030 p 19 N91-24307 NASA-CP-3103-vOL- . p p...... 41 N91-20641 NASA.RP-1260 p 26 N92-11285

NAS-CP1054 9 91-5t1 NSACP.11.VO.2p19 N9-2893 NASA-RP- 1261 p 36 N92-24719

NASA-CP-10031 p 13 N91-24211 NASA-CP-3103-VOL-2 ........... p....... p 41 N91.20702 NASA-RP-1262 p 32 N91-25370 NASA-CP.10038-VOL- p14 N91-10639 NASA-CP-3105 ...................... p... 10 N91-20071 NASA-RP-1263 p 35 N91-24703 NASA-CP-10038-VOL-2 ............ p4 N91-10868 NASA-CP-3106.VOL-1 ............. 35 N91-32599 A.4 N92-247

NASA-CP-3106VOL-2 . p 36 N91,32693 NASA-RP- 1264 p 35 N91-2W51

NASA-CP-10040... . p 40 N91-24744 NASA-CP-3107 ..-.- p 19 N91-19182 NASARP.1267.. p 3 N92-22505

NASA-CP-10042 . p 46 N91-11591 NASA-CP-3108 ... p................. 37 N91-18573 NASA-RP-1268 p 49 N9!32006

NASA-CP-10045 ..... p9 N91-2.1.6 NASA..P-31, 1 ... p 4 N91p2 -3021 NASA-RP-1272 p 33 N92-19127

NASA-CP.10050-PT-1 ................ p 9 N91-11642 NASA-CP-3109VOL-2 .p 52 N91-24041 NASA-RP.1273 p 23 N92-20063 NASA.CP.10050-PT-2. p 9 N91-11695 NASA-CP.3118 . p3 N91-22769 NASA-RP-1274 p 25 N92-20404

p4NSAC331 N.-28 .... .... p91-43 N.AS-603 

NASA-CP-10052 ...... .... ....... p 42 N91-17559 NASA-CP-3111 . .............. .. p 29 N91-20506 NASA-RP-1275 p34 N92 8027

NASA-CP-10053 ............. p 16 N92-22001 NASA-CP-3112-VOL-2 NASA-CP-10054 ....... p........... P 9 N91-15141 . 19 N91-28193 NASA-RP-1277.... p47 N92-7! NASA-CP-3112VOL NASA-CP-10055.... . p14 N91-15691 NASA-CP-3112 ..................... .. p p19 19 N91-28235 N91.25176 NASA-RP-1278 NASA.RP.71279. .... p p32 36N9 N92.362"27 21-94

NASA-CP-10056 ... ..... ..... p 13 N911,20147 N..........N....... NASA-CP-3113 .... ....... 30 N91.24603 NASA-RP-1280 .. 4 N92-30307

NASA.OP-10057-PT-1 p 16 N91-18188 NASA-CP.3114 . ............... . p32 N91-3252p NASA-CP-10057-PT-2 ............. p 17 N91-19122 NASA-CP-31152VOL-1 .... ........... 32 N91-20541 NASA.SP-4104 p..............p 52 N92-28344

NASA.CP-10059 p 13 N91-22139 NASA-CP.3115-VOL-2 . 32 N91-26573 NASA-SP-4215 .7......................... p 52 N91 -2816

NASA.CP-10060-PT-1 p 9 N91-24166 NASA-CP-3116 p 44 N91-25755 NASA.SP-4306 ............. p 51 N91-13$975

NASA-CP-10060-PT-2 p2 N9124 NASA-NP-3117-1O24 p41 N92-22324 NASA-SP-500 .1.. ...... P 41 N91-14725

NAS-C-1073PT1 14 912777 NASA-CP-3117. p 41 N9-270098 NASA-SP-50138) p370 N92 2&345

NASA-CP-10061VOL-. . p 43 N91-21778 NASA-CP-3118 .......... p 39 N92-21467 NASA-SP-501 ...49) p37 N92.235 NASA-C 0p -VOL-2 .. 43 N914-20711 NASA-CP-3119 .............. 3 20 N92-27130 NASA-SP-61013;.. p 46 N91-13347

NASA-CP-10062 p23 N91-29640 NASA-CP-3120 .... ...................... p 35 N9I-25556 NASA-SP-6101( p 46 N91-27756

NASA-CP-10063 .. .p 12 N91.20086 NASA-CP-3121 ......................... p19 N91-30203 NASA-SP-7101(05) p 47 N92-28729

NASA-CP-100657PT-l P 17 N91-22307 Np937 NASA.CP.3122 ... ......... ..... 28 N92-14346 NASA-SP-7011(341) N23"1053

NASA-CP-100657PT-2 p 17 N91-22331 NASA-CP-3123 ..... ............. 14 N92,14070 NASA-SP.7011(342) . p37 N91 13063

NASA-CP-10066-PT-1 p 17 N91-21188 NASA-CP-3124 .......................... p 16 N92-11039 NASA-SP.701 1(343) p 37 N91.14711

NASA-CP-10066-PT-2 p 17 N91-21203 NASA-CP-3125 . .................. 4....... 33 N91-32549 NASA-SP.7011(3) . p 37 N91-14712

NASA-CP-10070 .......... p 15 N92-15072 NASA-CP-3126 ... .......... 35 N91-32660 NASA-SP.7011(345) p 37 N92-1'547

NASA-CP-10071..... p 40 N92-11638 NASA.CP-3137.VOL-2 p. 2 N92-22324 NASA-SP-7011(346) ............... p 37 N91.23700

NAACP108-OL2PT1 . 8 9-178 NASA-CP-3137-L2 p 49 N92-22324 NASA-SP.7011(358) p 39 N91237201

NASA-CP.10032-.... . p 52 N91-24972 NASA-CO-3129 p 41 N92.13587 NASA.SP.7011(34 .. p39 N91-23701 NASA-CP-10073-PT-1 p 14 N91-27177 NASA-CP-3130 p 41 N92-12425 NASA-SP-7011(348) p 37 N91.23702

NASA-CP-100O3PT2 . p 14 N91-27178 NASA-CP-3131 p 3 N92-17934 NASA-SP.7011(349) p 3? N91-24731

NASACP-P I0074 .. . p 45 N9:-21057 NASA-CP.3132 ..... ....................... p 25 N92-14202 NASA-SP-7011(350) p 38 N91-30067 NASA-CP. 0075O p 21 N91-29240 NASA-CP-3134-PT-1 .. ...... ...... p.4. 52 N92-23280 NASA-SP.7011(351) ....... p..... 938 N91-27756

NASA-CP-10077 p 49 N92-33478 NASA-CP-3Q4-PT-2 _._.. 52 N92-24832 NASA-SP-7011(352) p 38 N91.26729

NASA-CP-I00078 p 12 N92-2580 NASA-CP.3134.PT-3 ................... p540 N92-27083 NASA-SP-7011(353) p 38 N91.317W0

NASA-CP.10079 p 20 N92-11088 NASA-CP-3135 ... p. 46 N92-22045 NASA-SP.7037(354) p 38 N92-12404

NASA-CP-10081 p 14 N92-12010 NASA-CP-3136-VOL-4 p 52 N92-22423 NASA.SP.70t1(355) .. ......... p 38 N92-12412 NASA-CP-10083-VOL-1.PT.1 .. p 18 N92-17098 NSCP33VO-........ 52N-276 NASA-SP-7011(356) .......... p 38 N92-15S538

NAA-Pl094p4 49-846 NASA-CP-3l48.VOL-2 p 152 N92-22676 NASA-SP-7037)281) p 39 N92-20713

NASA-CP-10083.VOL 1IPT.2 p 18 N92-17409 NASA-CP-3137 ..... .... .......... p p49 N92-21874 NASA-SP-7037) p I N922074 NASA-CP-10083VOL-PT-1 . p 18 N92-17768 NASA-CP-3138 p... 52 N92-24987 NASA-SP-7011(356) ........... p 39 N92-22026 NASA.CP- 10083-VOL-2.PT.2 . 10l N92-17348 NASA.CP.3140 ............ 33 N92-22740 NASA-SP-7011(359) .............. p 39 N92'21 715

NASA-CP- 10084 ... ........ p 20 N92o 10044 NASA.CP-3t41 ............. P 43 N92-2335,6 NASA-SP-7011(361) .... .. .p 39 N92-27433

NASA-CP-10085OL.1 p 42 N92-16568 NASA-CP.3142 ........ .... p 31 N92-25917 NASA-SP-7011(362) p 39 N92'21061

NASA.CP.10085-VOL-2. . p 42 N92-16590 NASA-CP.3143 ................. 42 N92-24397 NASA-SP-7011363) . .p 39 N92.30987 NASA-CP-10088 ...... .p 27 N92-24514 NA AC -15............ 0 N2234NASA-SP-4037(256) . . .... p I N91.10002

NASA-CP-10089 . . . . p 12 N92-2571 NASA-CP-3146 ......... . . 40 N92-25961 NASA-SP-7037(257) p.... I N91.13399 NASA-CP-10090 ... . p 20 N92-2151 7 NASA-CP-3147-ADO ........ p 33 N92-26895 NS-P73(5)......... 9.39 NASA-CP-10092 P 8 N92-29625 NASA-CP-3147 .: p....... 30 N92-25067 NASA-SP-7037(259) ....... p I N91 -15979

NASA-CP- 10093 ,p 50 N92-30302 NASA-SP-7037(260) ......... p 1 N91-15978 NASA-CP-10094 p 24 N92-28436 NASA-CP-3148-VOL-1 .......... p 15 N92-22660 NASA-SP-7037(2681) .......... pi N91-23073

NASA-CP-10097 . .. p 52 N92-27218 NASA-CP-3151 ............. 24 N92-30263 NASA-SP-7037(262) .......... p I N91.23074

NASA-CP-10098 . ... p 43 N92-27763 NASA-CP-3152-PT-1 .. .... ...... . p 18 N92-27721 NASA-SP-7037(2>63) ........ p 2 NO 1-24096

NASA-CP.10099.. ... p 19 N92.28730 NASA-CP-3152.PT-2 ..... ; 18 N92-27788 NASA-SP-7037(264) ....... p 2 N91-24097

C-1
NASA-SP-7037(265) REP•OR T NUMBER .WDEA

NASA-SP-70371265) p 2 N91.24095 NASA-TP-3083 015 N91-27180 NASA TP,3194 7 N92 252765

NASA-SP-70371266) p 2 N91-27122 NASA.TP-3084 p29 N9 1.21556 NASATP.3195 p22 N92 25160

NASA-SP-7037(267) p 2 N92-10001 NASA.TP-3085 p 5. N91.2105.g NASA TP-3196° P 22 R92 23981

NASA-SP-7037(260) p 2 N91.30077 NASA.TP.3086 p 5 N91-22070 NASA TP,3197, p 7 NO? ?84?77

NASA-.SP-7037(20) p 2 N92-10974 NASA-TP,3087 p 17 NO 1.22302 NASA TP.319M P 63 N92.28375

NASA-SP-7037(270) p 2 N92.10973 NASA-TP-3088 p 17 N 1 .21182 NASA-'P-3200 p 4^1 N92 2669,

NASA-SP-7037(2711 p 2 N924149657 NASA, TP-3069 p 43 NO1-25741 NASA TP 3201 p 16 N92.197'62

NASA-SP-7037(2721 p 3 N92.21844 NASA.TP-3090 p 29 Ngi-2'0503 NASA-TP.3202 p 9 N92 33656

NASA-SP-7037(273) ... p 3 N92-21729 NASA-TP-3092 p 5 Ngl1.25.,03 NASA.TP.3203 v 30 N92-19355

NAWSA,S7037(275) p 3 N92-28679 NASA-TP.3093 p 51 N 1 .230! 7 NASA.TP-3204 g) 30 N92 22227

NASA.SP.703742771• p 3 N92-27929 NASA-TP-3094 p 13 N92-10027 NASA TP.3205 p 8 N92 30295

NASA-SP.7037(2781 p 3 N92-28677 NASA.TP-3096 p 28 N92-10195. NASA.TP 3206 p 40 N92• 26$36

NASAýSP.7037(280,! p 3 N92-31456 NASA-TP-3096 51 N91-26107 NASA.TP.3207 p 40 N92..?W2

NASA.SP.7039(38).SECT-I p 47 N91.17833 NASA-TP-309 M 5 N91-27124 NASA TP-320 p 27 N92 31701

NASA.SP-703g(38)-SECT.2 p 47 N9I-17834 NASA-TP-3100 p 26 N91-22509 NASA-TP Mg0 p 412 N92 27569

NASA-SP-7039(39)-SECT-t p 48 W-128042 NASA-TP-3101 p 24_ N92-10161 NASA-TP 3210 p "t0 N92 24SA6

NASA-SP.7039(39)-SECT-2 p 48 N91 .29088 NASATP-3102 p 21 N;ý- 10067 NASA.-TP-3211 P 51 NOR 25 100•

NASA-SP-7039(40)-SECT-1 p 48 N92425.06 NASA-TP-3103 . 6 N92'1097ý NASA TP-3213 r; 24 NW 22235

NASA-SP-7039(40)-SE:CT-2 p 48 N92-27001 NASA-TP-3104 p 45 N92-117,58 NASA-TP-321`1 P 31 N92 27974

NAWASP.7039(41I)- SECT-.2 p 48 N92-31455 NASAJ.TP3105 .. . p 7 N92.20038 NASA. TP-3215S p 25 N92 20492

NASA-SP,7063404) p 47 N91-!3374 NASA-TP-3107 p 26 N91.24542 NASA.TP,3215 p 2& N%:2.303 7

NASA-SP-7063(05) . .... p 47 N91-24939 NASA-TP-3108S p 21 N91.21242 NASATPý3217 p 23 N92,22593

NASA.SP-70s4-SUPPL-4 ... p 47 N91 .10804 NASA-TP-3109 p 23 N91-20266 NASA MP3218 p 3,0 NW•.21Wf7

NASA.SP.70W4SUPPL-5 ..... P47 N91-19W6 NASA.TP-3110 1)6 NSZ. i c'5 NASA.TP.3219 v 10 N92.21459

NASA-SPJ7085{01) . ... p 17 N91-18199 NASA.TM31 11 .p 6 N92.14%S8 NASATP.3220 p 42 N92-23432

NASA.,•o.7005021 ... p IS N91-28191 NASA-TP.3112 p 44 N92.13756 NASATP.3221 p 8 N92.33625

NASA.SP-7085(03) p 18 N92.22•317 NASA-TP-3113 p 6 N91,21140 NASA.TP.3224 0 22 1492 283741

NASA.SP-7091 ... . p 49 N91-24965 NASA-TP.3114 . 6 N92-12M9 NASA"TP-3226 p 23 N92 27I94

NASA-SP-7092 .... p 32 N'91-30.5e$ NASA TP-3116 P 11 Ng2- I V54 NASA.TP.3227 p t6 NgZ 2666 7

NASA-SP-7097 ... p47 N92-22665 NASA-TP-3117 p 11 N92.13065 NASA - P.,3230-VIDE•O-SUPPL p 36 N92 34246

NASA-SP.7500(251 p.. 48 N 1 -24936 NASA-TP-311 I. p 265 N91-25352 NASATP-3230 p 36 N92 334182

NASA.SP- 7500(26) ... p 47 N92-27080 NASA-TP-3119 p 25 N92-11252 NASA. TP. 3231 p 31 N92 V•279

NASA-TP-3120 p 2 N91-26113 NASA-TP-3232 p a N92-30747

NASA.TP-POI3.2 ......... 1 5 N92-20676 NASA-TP-3122 p 46 N92- 1 0677 NASA-TP-3233 0 a N92-30394

NASA-TP.3123 p 42 N91-25629 NASA- MP3234 p 6 N92 33484

NASA-TP.2375 . ....... p 3 N91-10007 NASA-TP-3124 p 42 N92- 11!685 NASA. TP3235 p 39 N92-:34154

NASA.TP.2W4 .. .. p 4 N91.14316 NASA-TP-3125 p 10 N92-10994 NASA.TP.3236 p 9 N92-33706

NASA-TP-2852 .. .. p 12 N92-22863 NASA-TP-3126 p 30 N92-1805.3 NASA-TP.3238 p to N92.30395

NASA.TP.28M8 pi11 N91-24199 NASA-TP-312a p 23 N91-293!8 NASA.TP.3239 p 16 N92.33933

N4ASA-TP-292•2 T).. 6NSI-26143 NASA-TP-3130 p 18 N•2- 11067 NASA, TP-3240 p 9 N92-34193

NASA-TP.2983 .p 10 N91-17014 NASA-TP-3131 p 7 N92.-17131 NASA.TP.3242 p 43 NOZ-33483

NASA.TP-2995 .. . p 5 N91,19058 NASA-TP-3132 . . . p 7 N92_20494 NASA-TP-3248 p 31 N92 2•6%9

NASA-TP-2997 ....... p 4 N91-18030 NASAJTP-3133 ..... p 6 N91-,30096 NASA-TP-3249 P 241 N92.29677

NASA-TP.3C10 ...... 29 N91-13750 NASA-TP.3134 ... . .. p 45 N92. 11765 NASA-TP.3252 p 8 N92 2e980

NASA-TP,30;4 .... . P l N92-31251 NASA-TP.313,5... . p 11 N91 .31143 NASA.TP-3261 p a N92.324180

NASA-TP-301S. ......... p 44 N91-12315 NASA.TP-3136 . .. p 13 N92.201 95 NASA.TP-3265 p 28 N92.30396

NASA-TP-3020 ....... P 45 N91-19824 NASA-TP-3137 ... .p 50 N91 .31061 NASA.TP-3272,PT IA p 34 N92-32655

NASA-TP-3022 .... p 12 N9I1t0079 NASA-TP-3139 p 15 N91 .29209 NASA-TP-3273 p 31 N92-33476

NASA-TP-3025 ..... d 4 N91.16031 NASA-TP-3140 p 48 N92.-11930 NASAJTP.3275 P 23 N92.31278

NASA-TP.3026 . p 46 N91-13985 NASA-TP-3141 p 49 N92 . 11931 NASA.TP.3277 p 3t N9Z 3i2W•

NASA-TP-3032 1rp 5 N91"t- 9042 NASA-TP'3142 p 6 N91".28136 NASA-TP'3282 p 2S N92-33601

NASA.TP-3033 " 28 N91"14618 NASA-TP-3143 p 24 N92"13340

NASA.TP-3034 .P 21 N91.13492 NASA-TP.3145 .p 30 N92-24205

NASA-TP-3035 P 4 N91-13401 NASA-TP-3146 p 51 N92-15959

NASA.TP-3038 p 13 N92.31640 NASA-TP-3147 p 51 N92-22218

NASA-TP-3040 o.. D45 N91-21828 NASA-TP-3150 . ... p 19 N92-25147

NASA-TP-3041 . p 16 N91-17114 NASA-TP-3151 . p.. 6 N92-10981

NASA-TP-3043 .... . p 37 N91-19711 NASA-TP.3152 9 28 N91.30540

NASA-TP-3044 .... .. p 22 N91-13522 NASA.TP-3153 ... p 40 N92.1gT72

NASATP-3045 p 10 N91-ý14323 NASA-TP.3154 .p 12 N91-3015-4

NASA.TP-3046 . .. p 4 N91-10902 N4ASA-TP-3155 .P 23 N91-303 18

NASA-TP.3047 . .. P 4 N91-13402 NASA-TP-31565 p 6 N92.10011

NASA-TP-3048 . p 4 N91-16990 NASA.TP-315.7 . .. p 27 N92-20677

NASA-TP-3049 p 13 N9 1,13461 NASA.TP-3156 p ? N92-1917S

NASA.TP-3050 . ... p 4 Ng I. 18032 NASA-TP-315.9 p 38 N92-17022

NASA-TP-3051 . . p 12 N91-2515.1 NASA-TP,3160 .. .. 21 N92.11142

NASA-TP.3052 ..... p 25 N91-15499 NASA-TP-3161 ... .p 20 N92-12052

NASA.TP.3053 . .. p 45 N91I- 19623 NASA-TP-3162 p 23 N92-17070

NASA-TP-3054 . p 16 N91-11041 NASA-TP,3163 p 24 N92.11216

NASA-TP-305.5 .. ... p $0 N91-16961 NASA-TP,3164 p 31 N92-26537

NASA-TP-30566 ...... p 29 N91-10326 NASA-TP.3165 p 45 N92 204 79

NASA-TP-3057 . p 44 N91-16679 NASA-TP-3166 . p 13 N92-21410

NASA.TP-3058 ....... p 13 N91,10092 NASA-TP.3167 9 27 N92.24797

NASA.TP-305.9 . ... p 14 Ngt-18180 NASA-TP,3166 p 7 N92- Ig900Z

NARA.TP-3060 .. . .p . N91-22069 NASA-TP,3169 p 7 N92,20545

NASA-TP-306i.. p 26 N91.17310 NASA- TP-3 110 p 27 N92-1 Q299

NASA.TP-3062 .... . p 19 N91-11600 NASA-TP,3171 . .. p 30 N92.23i IS

NASA.TP-30)63 .. .. p 28 N91-12956 NASA-TP,3172 p 7 N92-;25133

NASA.TP.3064 .. .. p 21 N91-18216 NASA-TP-3173 p 21 N92-n679

NASA-TP-3065 .. .. p 19 N91.15306 NASA-TP-3174 p 38 N92-16553

NASA-TP-3066 P U2 N91.17208 NASA-TP-3175 p 38 N92.1655A

NASA-TP-3067 . . .. p 14 Ng1-2>0177 NASA.TP.3176 p 40 N92-16562;

NASA-TP-3060 p 26 N91-1638t NASA-TP,3177 .p 20 N92.20949

NASA.TP.3069 p 43 N91.18753 NASATP-3178 p 24 N92-13343

NASATP.3070 . .. p 5 1491-20043 NASA.TP-3179 p 22 N92.20950

NASA.TP.3071 p 2i Not-162f5 NASA- M.31 61 p 20 N92-14108

NASA.TP.3012 p 12 N91.2012e NASA-TP-3182 p 39 N92- 17645

NASA-TP.3073 p 30 Ngi.22576 NASA-TP-31S3 p I1I N92-20546

NASA.TP-3074 .p 21 N 1-.22538 NASA-TP-3184 p 8 N92.31532

NASA.TP-3075 , p 29 N91.16413 NASA-TP-3185 p 39 N22,22186

NASA TP-30}77 pi1 N91.21127 NASA-TP-3186 p 8 N92.30909

NASA-TP-3078 p 17 NOI.21185 NASATP-3187 p 42 N92-22286

NASA.TP-3079 p SO N91-17999 NASA-TP-3188 p 7 N92 23095

NA&A.TP-3080 p 5 N91-19057 NASA.TP-3191 p 20 N92.1715.t

NASA-TP-3001 p 25 Ngf-27436 NASA.TP.3192 p 3t N92.2599?

NASA-TP-3062 ... p 42 N91-25624 NASA-TP-3193 p 7 N92,25202

C-2
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APP-1
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A02 12.50 2500

A03 17.00 34.00

A04-A05 19,00 38W00

A06-A09 26,00 52.00

AIO-A13 35.00 7000

A14-A17 43-00 8600

A18-A21 50.00 10000

A22-A25 59.00 118.00

A99 69.00 13800

MICROFICHE

NORTH

PRICE AMERICAN FOREIGN

CODE PRICE PRICE

A01 $ 9.00 $ 18.00

A02 12.50 25.00

A03 17,00 34.00

A04 19.00 38.00

A06 2600 52.00

A10 35.00 70.00

IMPORTANT NOTICE

CASI Shipping and Handling Charges

U.S. - ADD $3.00 per TOTAL ORDER

Canada and Mexico - ADD $3.50 per TOTAL ORDER

All Other Countries - ADD $7.50 per TOTAL ORDER

Does NOT apply to orders

requesting CASI RUSH HANDLING,

Contact CASI for charge.

APP-2

*U.S. GOVERNMENT PRINTING OFFICE: 1993-728-150/10027
I Report No. 2 Government Accession No. 3 Recipient's Catalog No

NASA SP-7063(06)

4. Title and Subtitle 5 Report Date

NASA Scientific and Technical Publications: A Catalog February 1993

of Special Publications, Reference Publications, 6. Perlorming Organization Code

Conference Publications, and Technical Papers, 1991-1992 JTT

7 Author(s) 8 Performing Organtzation Report No

S .......... 10 Work Unit No.

9 Performing Organization Name and Address

NASA Scientific and Technical Information Program 11 Contract or Grant No

13 Type of Report and Period Covered

12. Sponsoring Agency Name and Address Special Publication

National Aeronautics and Space Administration

Washington, DC 20546 14. Sponsoring Agency Code

15. Supplementary Notes

16 Abstract

This catalog lists 458 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 Information

Database during the accession years 1991 through 1992. 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)) le. Distribution Statement

Catalogs (Publications) Unclassified - Unlimited

Subject Category 82

19. Security Classif (of this report) 20. Security Classif. (of this page) 21No. of Pages 22. Prc~ e

Unclassified Unclassified 120 Free