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t NASA SP-7063(02) 

NASA 

Scientific and Technical 

A cz10g7 publications 

Special Publications, 111 

Reference Publica tions, 

Conference' Publications, and 

Techn ica I Papers 

1987 

[rJSSA-SP-7063 (02) ) NASA SCIENTIFIC AYD ~~1-228 30 

TECHNICAL PUBLICATIONS: A CATALOG OF SPECIAL 

PUBLICATIONS, REFERENCE PUBLICATIONS, 

CONFERENCE PUBLICATIONS, AID TECHNICAL Unclas 

PAPERS, 1987 (NASA) 69 p CSCL OSB 61/82 0141579 
NASA SP-7063(02) 

NASA 

Scientific and Technical 

publications A Catalog 

of 

Special Publications, 

Reference Publications, 

Conference Publications, and 

Tech n ica I Papers 

1987 

Iw\sA Scientific and Technical Information Division 1988 

National Aeronautics and Space Administration 

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

Virginia 22161 as PR 828. 
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, archeologists, aircraft 

engineers, aerospace decision makers, land-use planners, historians, and rescue teams all 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 list of NASA publications from four report series entered into the NASA scientific 

and technical information database during accession year 1987. Records ofAchievement, NASA SP-470 

(accession number N83-33792) and 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) list previous NASA publications not covered by this catalog. 

Two semimonthly abstract journals cover all aspects of aeronautics and space research, NASA and 

non-NASA, nationally and worldwide: STAR (Scientific and TechnicalAerospace Reports), which focuses 

on scientific and technical reports, and IAA (International Aerospace Abstracts), which covers the open 

literature. These are available by subscription from, respectively, the U.S. Government Printing Off ice 

and the American Institute of Aeronautics and Astronautics, Inc., (see below). 

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 technical information derived from NASA programs for audiences of diverse technical 

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 

NASA SP-7037 

NASA SP-7039 

NASA SP-7041 

Aerospace Medicine and Biology: 

A Continuing Bibliography with Indexes 

Aeronautical Engineering: 

A Continuing Bibliography with Indexes 

NASA Pa tent Abstracts Bibliography: 

A Continuing Bibliography 

Section 1 :Abstracts; Section 2: Indexes 

Earth Resources: 

A Continuing Bibliography with Indexes 

Monthly plus 

annual cumulative index 

Monthly plus 

annual cumulative index 

Semiannual 

Quarterly 

iii 
NASA SP-7046 Technology for Large Space Systems: Semiannual 

NASA SP-7056 Space Station Systems: Semiannual 

NASA SP-7500 Management: Annual 

A Bibliography with Indexes 

A Bibliography with Indexes 

A Bibliography for NASA Managers 

Please note that the reports cited in this catalog are available for purchase from the U.S. Government 

Printing Office for a limited time after publication, depending on public demand, and from the National 

Technical Information Service (NTIS) with no time limit. They are also available at any Federal Regional 

Depository Library. Additional availability information follows, including current NTIS price schedules, 

which are keyed to the price code in the citation. 

iv 
TYPICAL CITATION AND ABSTRACT 

NASA SPONSORED 1 I- ON MICROFICHE 

ACCESSION NUMBER -N87-11916'# National Aeronautics and Space Administration. - CORPORATE SOURCE 

Wallops Flight Center, Wallops Island. Va. 

TITLE -PULSE COQE MODULATION (PCM) ENCODER HANDBOOK FOR 

AYDIN VECTOR MMPdOO SERIES SYSTEM 

1986 139 p 

AUTHORS AS. F. CURRIER and W. R. POWELL Washington, D.C. Aug. - PUBLlCATlON DATE 

REPORT NUMBERS-(NASA-RP-1171; NAS 1.61:1171) Avail: NTlS HC A07/MF A01 - PRICE CODE h 

COSATI CODE-^^^^ The hardware and software characteristics of a time division 

multiplex system are described. The system is used to sample 

analog and digital data. The data is merged with synchronization 

information to produce a serial pulse coded modulation (PCM) bit 

stream. Information presented herein is required by users to design 

compatible interfaces and assure effective utilization of this encoder 

system. GSFC/Wallops Flight Facility has flown approximately 50 

of these systems through 1984 on sounding rockets with no inflight 

failures. Aydin Vector manufactures all of the components for these 

systems. Author 

AVAILABILITY SOURCE 

TYPICAL CITATION AND SUBJECT TERMS 

NASA SPONSORED 

ON MICROFICHE 

ACCESSION NUMBER ____c N87-22604'# National Aeronautics and Space Administration. - CORPORATE SOURCE 

Langley Research Center, Hampton, Va. 

RESEARCH, 1984 

held in Hampton, Va., 18 Jan. 1985 

TITLE -JOINT UNIVERSITY PROGRAM FOR AIR TRANSPORTATION 

AUTHOR .-b FREDERICK R. MORRELL, comp. May 1987 165 p Meeting 

REPORT NUMBERS- (NASA-CP-2452; L-16255; NAS 1.55:2452) Avail: NTlS HC 4 AVAILABILITY SOURCE 

PRICE CODE-AOB/MF A01 CSCL 018 COSATI CODE 

AIR TRANSPORTATION, AIRCRAFT CONTROL, AIRCRAFT 

GUIDANCE, AVIONICS, CONTROL THEORY, SURFACE 

NAVIGATION 

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

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Public Collections of NASA Documents 

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

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

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

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

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

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

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For registration information contact: 

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PO. Box 8757 

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vi 
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viii 
NASA Scientific and Technical Publications 1987 

TABLE OF CONTENTS 

AERONAUTICS 

Includes aeronautics (general); aerodynamics: air 

transportation and safety; aircraft communications and 

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

facilities (air). 

For related information see also Astronautics. 

01 AERONAUTICS (GENERAL) 1 

02 AERODYNAMICS 1 

Includes aerodynamics of bodies, combinations, 

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

ducts and turbomachinery. 

For related information see also 34 Fluid Mechanics 

and Heat Transfer 

03 AIR TRANSPORTATION AND SAFETY 

and aircraft accidents. 

tion and 85 Urban Technology and Transportation. 

5 

Includes passenger and cargo air transport operations; 

For related information see also 16 Space Transporta04 AIRCRAFT COMMUNICATIONS AND 

NAVIGATION N.A. 

Includes digital and voice communication with aircraft; 

air navigation systems (satellite and ground based); and 

air traffic control. 

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

05 AIRCRAFT DESIGN, TESTING AND 

PERFORMANCE 5 

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 7 

Includes cockpit and cabin display devices; and flight 

instruments. 

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

07 AIRCRAFT PROPULSION AND POWER 7 

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 

trols; and autopilots. 

Testing and Performance. 

8 

Includes aircraft handling qualities; piloting; flight conFor related information see also 05 Aircraft Design, 

09 RESEARCH AND SUPPORT 

FACILITIES (AIR) 8 

Includes airports, hangars and runways: aircraft repair 

and overhaul facilities; wind tunnels; shock tubes; and 

aircraft engine test stands. 

For related information see also 14 Ground Support 

Systems and Facilities (Space). 

ASTRONAUTICS 

Includes astronautics (general); astrodynamics; 

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

communications, spacecraft communications, command 

and tracking: spacecraft design, testing and performance: 

spacecraft instrumentation; and spacecraft propulsion and 

power. 

For related information see also Aeronautics 

12 ASTRONAUTICS (GENERAL) 9 

For extraterrestrial exploration see 91 Lunar and Planetary Exploration. 

13 ASTRODYNAMICS N.A. 

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

14 GROUND SUPPORT SYSTEMS AND 

FACILITIES (SPACE) N.A. 

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 9 

Includes boosters: operating problems of launch/space 

For related information see also 20 Spacecraft Propulvehicle systems; and reusable vehicles. 

sion and Power: 

16 SPACE TRANSPORTATION 10 

Includes passenger and cargo space transportation, 

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

For related information see also 03 Air Transportation 

and Safety and 18 Spacecraft Design, Testing and Performance. For space suits see 54 Madsystem Technology 

and Life Support. 

17 SPACE COMMUNICATIONS, 

SPACECRAFT COMMUNICATIONS, 

COMMAND AND TRACKING N.A. 

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: 

ix 
18 SPACECRAFT DESIGN, TESTING AND 

PERFORMANCE 10 

Includes satellites; space platforms; space stations; 

spacecraft systems and components such as thermal and 

environmental controls; and attitude controls. 

For life support systems see 54 ManKystem Technology and Life Support. For related information see also 05 

Aircraft Design, Testing and Performance, 39 Structural 

Mechanics, and 16 Space Transportation. 

19 SPACECRAFT INSTRUMENTATION N.A. 

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

20 SPACECRAFT PROPULSION AND 

POWER 10 

Includes main propulsion systems and components, 

e.g. rocket engines; and spacecraft auxiliary power 

sources. 

For related information see also 07Aircraft Propulsion 

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

Ve hicles. 

CHEMISTRY AND MATERIALS 

Includes chemistry and materials (general); composite 

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

materials processing. 

23 CHEMISTRY AND MATERIALS 

(GENERAL) 11 

24 COMPOSITE MATERIALS 11 

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

For ceramic materials see 27 Nonmetallic Materials. 

25 INORGANIC AND PHYSICAL 

CHEMISTRY 12 

Includes chemical analysis, e.g., chromatography; 

combustion theory; electrochemistry; and photochemistry. 

For related information see also 77 Thermodynamics 

and Statistical Physics. 

26 METALLIC MATERIALS 12 

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

27 NONMETALLIC MATERIALS 12 

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 07Aircraft Propulsion 

and Power; 20 Spacecraft Propulsion and Power; and 44 

Energy Production and Conversion. 

29 MATERIALS PROCESSING 13 

Includes space-based development of products and 

processes for commercial application. 

For biological materials see 55 Space 6iology: 

X 

ENGINEERING 

Includes engineering (general); communications and 

radar; electronics and electrical engineering; fluid 

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

assurance and reliability; and structural mechanics. 

For related information see also Physics. 

31 ENGINEERING (GENERAL) 13 

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

32 COMMUNICATIONS AND RADAR 13 

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

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

Spacecraft Communications, Command and Tracking. For 

search and rescue see 03 Air Transportation and Safe& 

and 16 Space Transportation. 

33 ELECTRONICS AND ELECTRICAL 

ENGINEERING 14 

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 14 

Includes boundary Isyers; hydrodynamics; fluidics; 

For related information see also 02 Aerodynamics and 

mass transfer and ablation cooling. 

77 Thermodynamics and Statistical Physics. 

35 INSTRUMENTATION AND 

PHOTOGRAPHY 16 

Includes remote sensors; measuring instruments and 

gages; detectors; cameras and photographic supplies; and 

holography. 

For aerial photography see 43 Earth Resources and 

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

36 LASERS AND MASERS 16 

Includes parametric amplifiers. 

For related information see also 76 Solid-state 

Physics. 

37 MECHANICAL ENGINEERING 16 

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

38 QUALITY ASSURANCE AND 

RELIABILITY 17 

Includes product sampling procedures and techniques; 

and quality control. 

39 STRUCTURAL MECHANICS 17 

Includes structural element design and weight 

analysis; fatigue; and thermal stress. 

For applications see 05 Aircraft Design, Testing and 

Performance and 18 Spacecraft Design, Testing and Performance. 
GEOSCIENCES 

Includes geosciences (general); earth resources and 

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

For related information see also Space Sciences. 

42 GEOSCIENCES (GENERAL) 18 

43 EARTH RESOURCES AND 

REMOTE SENSING 18 

Includes remote sensing of earth resources by aircraft 

For instrumentation see 35 Instrumentation and Phoand spacecraft: photogrammetry; and aerial photography. 

tography 

44 ENERGY PRODUCTION AND 

CONVERSION 19 

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

cells; global sources of energy; geophysical conversion; 

and windpower. 

For related information see also 07Aircraft Propulsion 

and Power; 20 Spacecraft Propulsion and Power; and 28 

Propellants and Fuels. 

45 ENVIRONMENT POLLUTION N.A. 

Includes atmospheric, noise, thermal, and water pollution. 

46 GEOPHYSICS 19 

Includes aeronomy; upper and lower atmosphere 

studies; ionospheric and magnetospheric physics: and 

geomagnetism. 

For space radiation see 93 Space Radiation. 

47 METEOROLOGY AND CLIMATOLOGY 20 

Includes weather forecasting and modification. 

48 OCEANOGRAPHY 21 

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

For related information see also 43 Earth Resources 

and Remote Sensing. 

LIFE SCIENCES 

Includes life sciences (general); aerospace medicine; 

behavioral sciences; manlsystem technology and life support; and space biology. 

51 LIFE SCIENCES (GENERAL) 21 

52 AEROSPACE MEDICINE 21 

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

53 BEHAVIORAL SCIENCES N.A. 

includes psychological factors; individual and group 

behavior; crew training and evaluation; and psychiatric research. 

54 MANBYSTEM TECHNOLOGY AND 

LIFE SUPPORT N.A. 

Includes human engineering: biotechnology; and 

For related information see also 76 Space Transportaspace suits and protective clothing. 

tion. 

55 SPACE BIOLOGY N.A. 

Includes exobiology: planetary biology; and extraterrestrial life. 

MATHEMATICAL AND COMPUTER 

SCIENCES 

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

numerical analysis: statistics and probability: systems 

analysis: and theoretical mathematics. 

59 MATHEMATICAL AND COMPUTER 

SCIENCES (GENERAL) N.A. 

60 COMPUTER OPERATIONS AND 

HARDWARE N.A. 

Includes hardware for computer graphics, firmware, 

For components see 33 Electronics and Electrical Enand data processing. 

gineering. 

61 COMPUTER PROGRAMMING AND 

SOFlWARE 22 

Includes computer programs, routines, algorithms, and 

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

62 COMPUTER SYSTEMS 22 

Includes computer networks and special application 

computer systems. 

63 CYBERNETICS N.A. 

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

For related information see also 54 Man/System 

Technology and Life Support. 

64 NUMERICAL ANALYSIS 22 

Includes iteration, difference equations, and numerical 

approximation. 

65 STATISTICS AND PROBABILITY 23 

Includes data sampling and smoothing: Monte Carlo 

method; and stochastic processes. 

66 SYSTEMS ANALYSIS N.A. 

Includes mathematical modeling; network analysis; 

and operations research. 

67 THEORETICAL MATHEMATICS N.A. 

Includes topology and number theory. 

PHYSICS 

Includes physics (general); acoustics; atomic and 

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

For related information see also Engineering. 

70 PHYSICS (GENERAL) N.A. 

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. 

xi 
71 ACOUSTICS 23 

Includes sound generation, transmission, and attenuation. 

For noise pollution see 45 Environment Pollution. 

N.A. 

Includes atomic structure, electron properties, and 

72 ATOMIC AND MOLECULAR PHYSICS 

molecular spectra. 

73 NUCLEAR AND HIGH-ENERGY 

PHYSICS 24 

Includes elementary and nuclear particles; and reactor 

For space radiation see 93 Space Radiation. 

Includes light phenomena and optical devices. 

For lasers see 36 Lasers and Masers. 

theory. 

74 OPTICS 24 

75 PLASMA PHYSICS 24 

Includes magnetohydrodynamics and plasma fusion. 

For ionospheric plasmas see 46 Geophysics. For 

space plasmas see 90 Astrophysics. 

76 SOLID-STATE PHYSICS N.A. 

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 

For related information see also 25 lnorganicand PhysBose and Fermi statistics. 

ical Chemistryand 34 Fluid Mechanics and Heat Transfel: 

SOCIAL SCIENCES 

Includes social sciences (general); administration and 

management; documentation and information science; 

economics and cost analysis; law, political science, and 

space policy; and urban technology and transportation. 

80 SOCIAL SCIENCES (GENERAL) N.A. 

Includes educational matters. 

81 ADMINISTRATION AND 

MANAGEMENT 24 

Includes management planning and research. 

82 DOCUMENTATION AND 

INFORMATION SCIENCE 24 

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

arts; and micrography. 

For computer documentation see 61 Computer Programming and Software. 

83 ECONOMICS AND COST ANALYSIS 

Includes cost effectiveness studies. 

N.A. 

84 LAW, POLITICAL SCIENCE 

AND SPACE POLICY N.A. 

Includes NASA appropriation hearings; aviation law; 

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

85 URBAN TECHNOLOGY AND 

TRANSPORTATION 25 

Includes applications of space technology to urban 

problems; technology transfer; technology assessment; 

and surface and mass transportation. 

For related information see 03 Air Transportation and 

Safe& 16 Space Transportation, and 44 Energy Production 

and Conversion. 

SPACE SCIENCES 

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

and space radiation. 

For related information see also Geosciences. 

88 SPACE SCIENCES (GENERAL) 25 

89 ASTRONOMY 25 

Includes radio, gamma-ray, and infrared astronomy; 

and astrometry. 

90 ASTROPHYSICS 26 

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 26 

Includes planetology; and manned and unmanned 

For spacecraft design or space stations see 18 Spaceflights. 

craft Design, Testing and Performance. 

92 SOLAR PHYSICS 26 

Includes solar activity, solar flares, solar radiation and 

sunspots. 

For related information see 93 Space Radiation. 

93 SPACE RADIATION 27 

Includes cosmic radiation; and inner and outer earth’s 

radiation belts. 

For biological effects of radiation see 52 Aerospace 

Medicine. For theory see 73 Nuclear and High-Energy 

Physics. 

GENERAL 

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

too broad for categorization; histories or broad overviews 

of NASA programs. 

99 GENERAL 27 

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

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

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

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

xii 
01 

AERONAUTICS (GENERAL) 

N87-18520'# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

JOINT UNIVERSITY PROGRAM FOR AIR TRANSPORTATION 

RESEARCH, 1983 

FREDERICK R. MORRELL, comp. Mar. 1987 80 p Conference 

held in Atlantic City, N.J., 16 Dec. 1983; sponsored by NASA and 

FAA 

(NASA-CP-2451; L-16254; NAS 1.55:2451) Avail: NTlS HC 

A05/MF A01 CSCL 01B 

GUIDANCE, AVIONICS, CONFERENCES, FLIGHT CONTROL 

AIR NAVIGATION, AIR TRANSPORTATION, AIRCRAFT 

N87-22604'# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

JOINT UNIVERSITY PROGRAM FOR AIR TRANSPORTATION 

RESEARCH, 1984 

FREDERICK R. MORRELL, comp. May 1987 165 p Meeting 

held in Hampton, Va., 18 Jan. 1985 

(NASA-CP-2452; L-16255; NAS 1.55:2452) Avail: NTlS HC 

A08/MF A01 CSCL 01B 

AIR TRANSPORTATION, AIRCRAFT CONTROL, AIRCRAFT 

GUIDANCE, AVIONICS, CONTROL THEORY, SURFACE 

NAVIGATION 

N87-25267'# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

WIND SHEAR/TURBULENCE INPUTS TO FLIGHT SIMULATION 

AND SYSTEMS CERTIFICATION 

ROLAND L. BOWLES, ed. and WALTER FROST, ed. (FWG 

Associates, Inc.. Tullahoma, Tenn.) Jul. 1987 272 p Workshop 

held in Hampton, Va., 30 May - 1 Jun. 1984 

(NASA-CP-2474; L-16329; NAS 1.55:2474) Avail: NTIS HC 

A12/MF A01 CSCL 016 

FLIGHT SIMULATION, PILOT PERFORMANCE, WIND SHEAR 

AIRCRAFT PERFORMANCE, AVIONICS, FLIGHT SAFETY, 

N87-27596'# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

JOINT UNIVERSITY PROGRAM FOR AIR TRANSPORTATION 

RESEARCH, 1985 

FREDERICK R. MORRELL, comp. Jul. 1987 100 p Conference 

held in Atlantic City, N.J., 30 Jan. 1986 

(NAS 1.55:2453; NASA-CP-2453) Avail: NTlS HC AO5/MF A01 

CSCL 016 

AIR TRAFFIC CONTROL, AIR TRANSPORTATION, 

CONFERENCES, FAULT TOLERANCE, FLIGHT CONTROL, 

GLOBAL POSITIONING SYSTEM, INERTIAL NAVIGATION 

N87-27613' National Aeronautics and Space Administration, 

Washington, D.C. 

AERONAUTICAL ENGINEERING: A CONTINUING BIBLIOGRAPHY WITH INDEXES (SUPPLEMENT 217) 

Sep. 1987 134 p 

(NASA-SP-7037(217); NAS 1.21:7037(217)) Avail: NTlS HC A07 

CSCL 01 B 

This bibliography lists 450 reports, articles, and other documents 

introduced into the NASA scientific and technical information 

system in August, 1987. Author 

02 

AERODY NAMlCS 

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

control surfaces; and internal flow in ducts and turbomachinery. 

N87-10039'# 

Langley Research Center, Hampton, Va. 

National Aeronautics and Space Administration. 

WIND-TUNNEL INVESTIGATION OFTHE FLIGHT CHARACTERISTICS OF A CANARD GENERAL-AVIATION AIRPLANE CONFIGURATION 

D. R. SATRAN Oct. 1986 60 p 

(NASA-TP-2623; L-15929; NAS 1.60:2623) Avail: NTlS HC 

A04/MF A01 CSCL 01A 

GENERAL AVIATION AIRCRAFT, WIND TUNNEL TESTS 

CANARD CONFIGURATIONS, FLIGHT CHARACTERISTICS, 

N87-10042'# 

Langley Research Center, Hampton, Va. 

FOR HIGH LIFT WITH EXPERIMENTAL VALIDATION 

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

Aerospace Corp., Bethpage, N.Y.) Aug. 1984 221 p 

(NASA-TP-2336 L-15787; NAS 1.60:2336) Avail: NTlS HC 

AlO/MF A01 CSCL 01A 

FLOW, SUPERSONIC AIRFOILS, SUPERSONIC FLOW 

National Aeronautics and Space Administration. 

SUPERSONIC, NONLINEAR, ATTACHED-FLOW WING DESIGN 

CAMBERED WINGS, REATTACHED FLOW, SUPERCRITICAL 

N87-10838'# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

EFFECTS OF TAIL SPAN AND EMPENNAGE ARRANGEMENT 

J. R. BURLEY, II and B. L. BERRIER Sep. 1984 

(NASA-TP-2352 L-15742; NAS 1.60:2352) Avail: NTlS HC 

A07/MF A01 CSCL 01A 

FRICTION, TAIL ASSEMBLIES, TRANSONIC SPEED 

ON DRAG OF A TYPICAL SINGLE-ENGINE FIGHTER AFT END 

136 p 

AERODYNAMIC DRAG, AIRCRAFT CONFIGURATIONS, SKIN 

1 
02 AERODYNAMICS 

N87-10839*# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

RAMP NOZZLES WITH THRUST-VECTORING CAPABILITY UP TO 

60 DEG 

B. L. BERRIER and L. D. LEAVITT Oct. 1984 144 p 

(NASA-TP-2364; L-15766; NAS 1.60:2364) Avail: NTlS HC 

A07/MF A01 CSCL 01A 

CONTROL 

STATIC INTERNAL PERFORMANCE OF SINGLE-EXPANSIONAXISYMMETRIC BODIES, NOZZLE FLOW, THRUST VECTOR 

N87-10841'# National Aeronautics and Space Administration. 

Ames Research Center, Moffett Field, Calif. 

TRANSONIC FLOW ANALYSIS FOR ROTORS. PART 2 

LATION 

I. C. CHANG Jan. 1985 27 p 

(NASA-TP-2375-PT-2; A-9682; NAS 1.60:2375-PT-2) Avail: NTlS 

HC AO3/MF A01 CSCL 01A 

AERODYNAMIC STABILITY, HELICOPTER PERFORMANCE, 

ROTORS, TIP VANES, TRANSONIC FLOW 

THREE-DIMENSIONAL, UNSTEADY, FULL-POTENTIAL CALCUN87-10843'# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

PILOTED SIMULATION STUDY OF THE EFFECTS OF AN 

AUTOMATED TRIM SYSTEM ON FLIGHT CHARACTERISTICS 

INOPERATIVE 

E. C. STEWART, P. W. BROWN, and K. R. YENNI 

41 P 

(NASA-TP-2633; L-16147; NAS 1.60:2633) Avail: NTlS HC 

A03/MF A01 CSCL 01A 

ENGINE FAILURE, LIGHT AIRCRAFT 

OF A LIGHT TWIN-ENGINE AIRPLANE WITH ONE ENGINE 

Nov. 1986 

AERODYNAMIC BALANCE, AUTOMATIC FLIGHT CONTROL, 

N87-11702'# National Aeronautics and Space Administration. 

Langley Research Center, Hampton. Va. 

FORWARDSWEPT WING CONFIGURATION DESIGNED FOR 

HIGH MANEUVERABILITY BY USE OF A TRANSONIC 

COMPUTATIONAL METHOD 

M. J. MANN and C. E. MERCER 

(NASA-TP-2628; L-16120; NAS 1.60:2628) Avail: NTlS HC 

AO9/MF A01 CSCL 01A 

AIRCRAFT, SWEPT FORWARD WINGS, TRANSONIC SPEED 

Nov. 1986 185 p 

AERODYNAMIC CONFIURATIONS, HIGHLY MANEUVERABLE 

N87-12541'# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

EFFECT OF PORT CORNER GEOMETRY ON THE INTERNAL 

REVERSER 

B. L. BERRIER and F. J. CAPONE Dec. 1986 51 p 

(NASA-TP-2624; L-16135; NAS 1.60:2624) Avail: NTlS HC 

A04/MF A01 CSCL 01A 

PERFORMANCE OF A ROTATING-VANE-TYPE THRUST 

CORNER FLOW, NOZZLE GEOMETRY, PORTS (OPENINGS), 

ROTATING BODIES, THRUST REVERSAL, VANES, WIND 

TUNNEL TESTS 

N87-14284*# National Aeronautics and Space Administration. 

Lewis Research Center, Cleveland, Ohio. 

PROPAGATION OF SOUND WAVES IN TUBES OF 

NONCIRCULAR CROSS SECTION 

W. B. RICHARDS (Oberlin Coll., Ohio) Aug. 1986 33 p 

(NASA-TP-2601; E-2690; NAS 1.60:2601) Avail: NTlS HC 

AO3/MF A01 CSCL 01A 

WAVE PROPAGATION 

ELLIPTICAL CYLINDERS, PIPES (TUBES), SOUND WAVES, 

N87-15174'# 

Langley Research Center, Hampton, Va. 

METHODS TO DESIGN AND ANALYSIS OF FLAP SYSTEMS 

AT LOW SPEEDS FOR THIN SWEPT WINGS WITH SHARP 

LEADING EDGES 

HARRY W. CARLSON and CHRISTINE M. DARDEN Jan. 1987 

54 P 

(NASA-TP-2653; L-16151; NAS 1.60:2653) Avail: NTlS HC 

AO4/MF A01 CSCL 01A 

DESIGN ANALYSIS, FLAPS (CONTROL SURFACES), 

LINEARITY, LOW SPEED, SHARP LEADING EDGES, SWEPT 

WINGS, THIN WINGS, VORTEX FLAPS 

National Aeronautics and Space Administration. 

APPLICABILITY OF LINEARIZED-THEORY ATTACHED-FLOW 

N87-15183'# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

EFFICIENT SOLUTIONS TO THE EULER EQUATIONS FOR 

SUPERSONIC FLOW WITH EMBEDDED SUBSONIC REGIONS 

ROBERT W. WALTERS and DOUGLAS L. DWOYER Jan. 1987 

18 P 

(NASA-TP-2523; L-15975; NAS 1.60:2523) Avail: NTlS HC 

A02/MF A01 CSCL 01A 

SOLVING, SUBSONIC FLOW, SUPERSONIC FLOW 

EMBEDDING, EULER EQUATIONS OF MOTION, PROBLEM 

N87-15184'# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

SUBSONIC MANEUVER CAPABILITY OF A SUPERSONIC 

CRUISE FIGHTER WING CONCEPT 

GREGORY D. RlEBE and CHARLES H. FOX, JR. Jan. 1987 

74 P 

(NASA-TP-2642; L-16097; NAS 1.60:2642) Avail: NTlS HC 

A04/MF A01 CSCL 01A 

SUPERSONIC CRUISE AIRCRAFT RESEARCH, WINGS 

FIGHTER AIRCRAFT, MANEUVERS, SUBSONIC SPEED, 

N87-17665'# National Aeronautics and Space Administration. 

Lewis Research Center, Cleveland, Ohio. 

PRELIMINARY DESIGN OF TURBOPUMPS AND RELATED 

MACHINERY 

GEORGE F. WISLICENUS Oct. 1986 397 p 

(NASA-RP-1170; E-7389; NAS 1.61:1170) Avail: NTlS HC 

A17/MF A01 CSCL 01A 

Pumps used in large liquid-fuel rocket engines are examined. 

The term preliminary design denotes the initial, creative phases of 

design, where the general shape and characteristics of the machine 

are determined. This compendium is intended to provide the design 

engineer responsible for these initial phases with a physical 

understanding and background knowledge of the numerous special 

fields involved in the design process. Primary attention is directed 

to the pumping part of the turbopump and hence is concerned 

with essentially incompressible fluids. However, compressible flow 

principles are developed. As much as possible, the simplicity and 

reliability of incompressible flow considerations are retained by 

treating the mechanics of compressible fluids as a departure from 

the theory of incompressible fluids. Five areas are discussed: a 

survey of the field of turbomachinery in dimensionless form; the 

theoretical principles of the hydrodynamic design of turbomachlnery; 

the hydrodynamic and gas dynamic design of axial flow turbomachinery; the hydrodynamic and gas dynamic design of radial and mixed 

flow turbomachinery; and some mechanical design considerations of 

turbomachinery. Theoretical considerations are presented with a relatively elementary mathematical treatment. Author 

(NAS3-13475) 

2 
02 AERODYNAMICS 

N87-17668'# 

Langley Research Center, Hampton, Va. 

A REMOTECONTROLLED CANARD MISSILE WITH A 

A. B. BLAIR, JR. Mar. 1985 38 p 

(NASA-TP-2401; L-15882; NAS 1.60:2401) Avail: NTlS HC 

AO3IMF A01 CSCL 01A 

BRAKING, CANARD CONFIGURATIONS, FINS, MISSILE 

CONFIGURATIONS, REMOTE CONTROL, ROLLING MOMENTS, 

SUPERSONIC SPEED, TAIL ASSEMBLIES, TORQUE, WIND 

TUNNEL TESTS 

National Aeronautics and Space Administration. 

WIND-TUNNEL INVESTIGATION AT SUPERSONIC SPEEDS OF 

FREE-ROLLING-TAIL BRAKE TORQUE SYSTEM 

N87-17669'# National Aeronautics and Space Administration. 

Lewis Research Center, Cleveland, Ohio. 

COMBINED AERODYNAMIC AND STRUCTURAL DYNAMIC 

PROBLEM EMULATING ROUTINES (CASPER): THEORY AND 

IMPLEMENTATION 

WILLIAM H. JONES Feb. 1985 75 p 

(NASA-TP-2418; E-2278; NAS 1.60:2418) Avail: NTlS HC 

A04/MF A01 CSCL 01A 

AERODYNAMIC COEFFICIENTS, COMPUTATIONAL FLUID 

DYNAMICS, COMPUTERIZED SIMULATION, DYNAMIC STRUCTURAL ANALYSIS 

N87-18537"# 

Langley Research Center, Hampton, Va. 

National Aeronautics and Space Administration. 

HELICOPTER BLADE-VORTEX INTERACTION LOCATIONS 

SCALE-MODEL ACOUSTICS AND FREE-WAKE ANALYSIS 

RESULTS 

DANNY R. HOAD Apr. 1987 106 p 

Avail: NTlS HC AO6IMF A01 

HELICOPTERS, ROTORS, VORTICES, WAKES 

(DA PROJ. 1 L1-62209-AH-76-A) 

(NASA-TP-2658; L-16214; AVSCOM-TM-87-B-1; NAS 1.60:2658) 

CSCL 01A 

ACOUSTICS, BLADE-VORTEX INTERACTION, FREE FLOW, 

N87-19351'# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

NUMERICAL SIMULATION OF CHANNEL FLOW TRANSITION, 

RESOLUTION REQUIREMENTS AND STRUCTURE OF THE 

HAIRPIN VORTEX 

STEVEN E. KRlST (Joint Inst. for Advancement of Flight Sciences, 

Hampton, Va.) and THOMAS A. ZANG Apr. 1987 71 p 

(NASA-TP-2667; L-16204; NAS 1.60:2667) Avail: NTlS HC 

A04lMF A01 CSCL 01A 

BOUNDARY LAYER STABILITY,. BOUNDARY LAYER 

TRANSITION, BOUNDARY VALUE PROBLEMS, CHANNEL FLOW, 

COMPUTATIONAL FLUID DYNAMICS, SPECTRAL METHODS 

N87-20233'# 

Langley Research Center, Hampton, Va. 

INVESTIGATION OF LEADING-EDGE FLAP PERFORMANCE ON 

DELTA AND DOUBLE-DELTA WINGS AT SUPERSONIC 

SPEEDS 

PETER F. COVELL, RICHARD M. WOOD, and DAVID S. MILLER 

Apr. 1987 125 p 

(NASA-TP-2656; L-16143; NAS 1.60:2656) Avail: NTlS HC 

AO6IMF A01 CSCL 01A 

FLAPS, SUPERSONIC SPEED 

National Aeronautics and Space Administration. 

DELTA WINGS, EXPERIMENT DESIGN, LEADING EDGE 

N87-20238'# 

Lewis Research Center, Cleveland, Ohio. 

LEWIS INVERSE DESIGN CODE (LINDES): USERS MANUAL 

JOSE M. SANZ Mar. 1987 67 p 

(NASA-TP-2676; E-3221 ; NAS 1.602676) Avail: NTlS HC 

A04lMF A01 CSCL 01A 

AIRFOILS, CODING, DESIGN ANALYSIS, HODOGRAPHS, 

INVERSIONS, TURBINE BLADES, USER MANUALS (COMPUTER 

PROGRAMS) 

National Aeronautics and Space Administration. 

N87-20966'# 

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

COMPARISONS TO PRESSURE DISTRIBUTION AND 

ROBERT R. MEYER, JR. and LISA A. JENNElT Apr. 1985 

27 p Original contains color illustrations 

(NASA-TP-2395; H-1184; NAS 1.60:2395) Avail: NTlS HC 

AO3IMF A01 CSCL 01A 

National Aeronautics and Space Administration. 

IN-FLIGHT SURFACE OIL-FLOW PHOTOGRAPHS WITH 

BOUNDARY-LAYER DATA 

BOUNDARY LAYER FLOW, FLOW VISUALIZATION, 

IN-FLIGHT MONITORING, OILS, PHOTOGRAPHY, PRESSURE 

DISTRIBUTION 

N87-21855'# 

Langley Research Center, Harnpton, Va. 

National Aeronautics and Space Administration. 

WIND-TUNNEL FREE-FLIGHT INVESTIGATION OF A 

0.15-SCALE MODEL OF THE F-106B AIRPLANE WITH VORTEX 

FLAPS 

LONG P. YIP May 1987 46 p 

(NASA-TP-2700; L-16202; NAS 1.60:2700) Avail: NTlS HC 

AO3IMF A01 CSCL 01A 

TUNNEL MODELS, WIND TUNNEL TESTS 

F-106 AIRCRAFT, FREE FLIGHT, VORTEX FLAPS, WIND 

N87-21871*# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

NEW METHODS AND RESULTS FOR QUANTIFICATION OF 

FELIX L. PITTS, LARRY D. LEE, RODNEY A. PERALA, and 

TERENCE H. RUDOLPH (Electro Magnetic Applications, Inc., 

Lakewood. Colo.) Jun. 1987 67 p 

(NASA-TP-2737; L-16281; NAS 1.60:2737) Avail: NTlS HC 

AO4lMF A01 CSCL 01A 

LIGHTNING, RESEARCH AIRCRAFT 

LIGHTNING-AIRCRAFT ELECTRODYNAMICS 

ELECTRODYNAMICS, F-106 AIRCRAFT, FLIGHT TESTS, 

N87-21873'# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

EFFECTS OF AFTERBODY BOATTAIL DESIGN AND 

EMPENNAGE ARRANGEMENT ON AEROPROPULSIVE CHARACTERISTICS OF A TWIN-ENGINE FIGHTER MODEL ATTRANSONlC SPEEDS 

LINDA S. BANGERT, LAURENCE D. LEAVITT, and DAVID E. 

REUBUSH Jun. 1987 134 p 

(NASA-TP-2704; L-16227; NAS 1.60:2704) Avail: NTlS HC 

A07/MF A01 CSCL 01A 

AFTERBODIES, AXSYMMETRIC FLOW, BOATTAILS, DRAG, 

FIGHTER AIRCRAFT, NOZZLES, PROPULSIVE EFFICIENCY, 

TAIL ASSEMBLIES 

N87-22626'# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

EXPERIMENTAL CAVITY PRESSURE DISTRIBUTIONS AT 

SUPERSONIC SPEEDS 

ROBERT L. STALLINGS, JR. and FLOYD J. WILCOX, JR. Jun. 

1987 79 p 

(NASA-TP-2683; L-16215; NAS 1.60:2683) Avail: NTlS HC 

A05/MF A01 CSCL 01A 

SUPERSONIC SPEED 

CAVITIES, FLUID FLOW, PRESSURE DISTRIBUTION, 

N87-23586'# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

ON MINIMIZING THE NUMBER OF CALCULATIONS IN 

RAYMOND L. BARGER and ANUTOSH MOITRA Jun. 1987 

(NASA-TP-2706; L-16226; NAS 1.60:2706) Avail: NTlS HC 

AO2/MF A01 CSCL 01A 

AERODYNAMIC CONFIGURATIONS, APPROXIMATION, 

DESIGN ANALYSIS, NUMERICAL ANALYSIS, PRESSURE 

DISTRIBUTION 

DESIGN-BY-ANALYSIS CODES 

16 P 

3 
02 AERODYNAMICS 

N87-23592'# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

MACH 6 EXPERIMENTAL AND THEORETICAL STABILITY AND 

PERFORMANCE OF A CRUCIFORM MISSILE AT ANGLES OF 

ATTACK UP TO 65 DEGREES 

EDWARD R. HARTMAN (Arnold Engineering Development Center, 

Arnold Air Force Station, Tenn.) and PATRICK J. JOHNSTON 

Jul. 1987 41 p 

(NASA-TP-2733; L-16287; NAS 1.60:2733) Avail: NTlS HC 

AO3/MF A01 CSCL 01A 

TION, HYPERSONIC SPEED, MACH NUMBER, MISSLES 

ANGLE OF ATTACK, CRUCIFORM WINGS, EXPERIMENTAN87-23593'# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

EFFECT OF A TRADE BETWEEN BOATTAIL ANGLE AND 

RIC WEDGE NOZZLE 

GEORGE T. CARSON, JR., E. ANN BARE, and JAMES R. 

BURLEY, II Jul. 1987 67 p 

(NASA-TP-2717; L-16248; NAS 1.60:2717) 

A04/MF A01 CSCL 01A 

PERFORMANCE TESTS, TRADEOFFS, WEDGES 

WEDGE SIZE ON THE PERFORMANCE OF A NONAXISYMMETAvail: NTlS HC 

AXISYMMETRIC BODIES, BOATAILS, NOZZLE GEOMETRY, 

N87-23597*# 

Langley Research Center, Hampton. Va. 

DELTA WINGS AT SUPERSONIC SPEEDS, PART 1 

RICHARD M. WOOD and CAROLYN B. WATSON Jul. 1987 

212 p 

(NASA-TP-2660-PT-1; L-16192; NAS 1.60:2660-PT-l) Avail: 

NTlS HC AlO/MF A01 CSCL 01A 

CONICAL CAMBER, DELTA WINGS, FLOW DISTRIBUTION, 

LEE WAVES, STRUCTURAL DESIGN, SUPERSONIC FLOW, 

VORTICES 

National Aeronautics and Space Administration. 

STUDY OF LEE-SIDE FLOWS OVER CONICALLY CAMBERED 

N87-24410'# National Aeronautics and Space Administration. 

Ames Research Center, Moffett Field, Calif. 

PROCEEDINGS OF THE 1985 NASA AYES RESEARCH 

CENTER'S GROUNPEFFECTS WORKSHOP 

KERRY MITCHELL, ed. Feb. 1987 448 p Workshop held at 

Moffett Field, Calif., 20-21 Aug. 1985 

(NASA-CP-2462; A-86391; NAS 1.552462) Avail: NTlS HC 

A19/MF A01 CSCL 01A 

GROUND EFFECT (AERODYNAMICS), INGESTION (ENGINES), POWERED LIFT AIRCRAFT, V/STOL AIRCRAFT, VERTICAL LANDING 

N87-24432*# 

Langley Research Center, Hampton, Va. 

k. ANN BARE and DAVID E. REUBUSH Jul. 1987 115 p 

(NASA-TP-2721; L-16240; NAS 1.60:2721) Avail: NTlS HC 

AO6/MF A01 CSCL 01A 

THRUST VECTOR CONTROL, TWO DIMENSIONAL FLOW 

National Aeronautics and Space Administration. 

STATIC INTERNAL PERFORMANCE OF A TWO-DIMENSIONAL 

CONVERGENT-DIVERGENT NOZZLE WITH THRUSTVECTORING 

CONVERGENT-DIVERGENT NOZZLES, STATIC TESTS, 

N87-24433'# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

MULTlAXlS CONTROL POWER FROM THRUST VECTORING 

FOR A SUPERSONIC FIGHTER AIRCRAFT MODEL AT MACH 

0.20 TO 2.47 

FRANCIS J. CAPONE and E. ANN BARE 

(NASA-TP-2712; L-16213; NAS 1.60:2712) 

Al2/MF A01 CSCL 01A 

AIRCRAFT RESEARCH, THRUST VECTOR CONTROL 

Jul. 1987 264 p 

Avail: NTlS HC 

FIGHTER AIRCRAFT, MACH NUMBER, SUPERSONIC CRUISE 

N87-25301'# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

STUDY OF LEE-SIDE FLOWS OVER CONICALLY CAMBERED 

DELTA WINGS AT SUPERSONIC SPEEDS, PART 2 

RICHARD M. WOOD and CAROLYN B. WATSON Jul. 1987 

404 p 

(NASA-TP-2660-PT-2; L-16192; NAS 1.60:2660-PT-2) Avail: 

NTlS HC A18/MF A01 CSCL 01A 

FLOW VISUALIZATION, SUPERSONIC FLOW, WING LOADING 

N87-25998'# National Aeronautics and Space Administration. 

Ames Research Center, Moffett Field, Calif. 

SUPERCOMPUTING IN AEROSPACE 

PAUL KUTLER and HELEN YEE Mar. 1987 299 p Symposium 

held at Moffett Field, Calif., 10-12 Mar. 1987 

(NASA-CP-2454; A-87082; NAS 1.55:2454) Avail: NTlS HC 

A13/MF A01 CSCL 01A 

CONICAL CAMBER, DELTA WINGS, FLOW DISTRIBUTION, 

COMPUTATIONAL ASTROPHYSICS, COMPUTATIONAL 

TIONAL GRIDS, COMPUTERIZED SIMULATION, CONFERENCES, 

SUPERCOMPUTERS 

N87-26031*# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

EFFECT OF REYNOLDS NUMBER VARIATION ON 

CONCEPT AT MACH 6 

JIM A. PENLAND and DON C. MARCUM, JR. Aug. 1987 28 p 

(NASA-TP-2728; L-16286; NAS 1.60:2728) Avail: NTlS HC 

AO3/MF A01 CSCL 01A 

AERODYNAMIC CONFIGURATIONS, HYDROGEN FUELS, 

HYPERSONIC AIRCRAFT, MACH NUMBER, REYNOLDS 

NUMBER, TRANSPORT AIRCRAFT 

N87-26032"# National Aeronautics and Space Administration. 

Langley Research Center, Hampton. Va. 

STEADY AND UNSTEADY AERODYNAMIC FORCES FROM THE 

WITH TIP MISSILE AND COMPARISON WITH EXPERIMENT 

AND PANAIR 

HERBERT J. CUNNINGHAM Aug. 1987 29 p 

(NASA-TP-2736; L-16262; NAS 1.60:2736) Avail: NTlS HC 

AO3/MF A01 CSCL 01A 

METHOD (FLUID DYNAMICS), UNSTEADY FLOW, WINGS 

N87-26874'# 

Langley Research Center, Hampton, Va. 

CHEMISTRY, COMPUTATIONAL FLUID DYNAMICS, COMPUTAINTERACTIONAL AERODYNAMICS, NAVIER-STOKES EQUATION, 

AERODYNAMICS OF A HYDROGEN-FUELED TRANSPORT 

SOUSSA SURFACE-PANEL METHOD FOR A FIGHTER WING 

AERODYNAMIC FORCES, FIGHTER AIRCRAFT, PANEL 

National Aeronautics and Space Administration. 

SUBSONIC LONGITUDINAL AND LATERAL-DIRECTIONAL 

CHARACTERISTICS OF A FORWARD-SWEPT-WING FIGHTER 

CONFIGURATION AT ANGLES OF ATTACK UP TO 47 DEG 

MICHAEL J. MANN, JARRETT K. HUFFMAN, and CHARLES H. 

FOX, JR. Sep. 1987 103 p 

(NASA-TP-2727; L-16206; NAS 1.60:2727) Avail: NTlS HC 

AO6/MF A01 CSCL 01A 

AERODYNAMIC CONFIGURATIONS, ANGLE OF ATTACK, 

FIGHTER AIRCRAFT, LATERAL CONTROL, LATERAL STABILITY, 

SUBSONIC AIRCRAFT, SWEPT FORWARD WINGS 

N87-26883'# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

AN EXPERIMENTAL INVESTIGATION OF AN ADVANCED 

TURBOPROP INSTALLATION ON A SWEPT WING AT 

SUBSONIC AND TRANSONIC SPEEDS 

JOHN R. CARLSON and ODlS C. PENDERGRAFT, JR. Sep. 

1987 242 p 

(NASA-TP-2729; L-16043; NAS 1.60:2729) Avail: NTlS HC 

A11/MF A01 CSCL 01A 

AERODYNAMICS, ENGINE AIRFRAME INTEGRATION, 

SUBSONIC SPEED, SWEPT WINGS, TRANSONIC SPEED, 

TURBOPROP ENGINES 

4 
05 AIRCRAFT DESIGN, TESTING AND PERFORMANCE 

N87-27622'# 

Lanalev Research Center. HamDton. Va. 

National Aeronautics and Space Administration. 03 

CALCULATION OF VISCOUS EFFECTS ON TRANSONIC FLOW 

FOR OSCILLATING AIRFOILS AND COMPARISONS WITH AIR TRANSPORTATION AND SAFETY 

Includes passenger and cargo air transport operations; and aircraft 

accidents. 

EXPERIMENT 

JAMES T. HOWLETT and SAMUEL R. BLAND Sep. 1987 

77 .. 0 

INAkA-TP-2731: L-16289: NAS 1.60:2731) Avail: NTlS HC 

N87-10054*# 

Langley Research Center, Hampton, Va. 

DOPPLER RADAR DETECTION OF WIND SHEAR 

National Aeronautics and Space Administration. AO51MF A01 CSCL OlA 

TRANSONIC FLOW, VISCOUS FLOW 

AIRFOILS, COMPARISON, INVISCID FLOW, OSCILLATIONS, 

V. E. DELNORE, Comp. (PRC Kentron, Inc., Hampton, Va.) and 

V. A. MCCLELLAN (Research Triangle Inst., Research Triangle 

Park, N.C.) Sep. 1985 1 18 p Presented at a Meeting, Hampton, 

Va., 24-25 Sep., 1985; sponsored in part by FAA 

N87-27626'# National Aeronautics and Space Administration. (NASA-CP-2435; NAS 1.55:2435; FAA/PM-86/31) Avail: NTlS 

Langley Research Center, Hampton, Va. HC AO6/MF A01 CSCL 01C 

DRAG MEASUREMENTS OF BLUNT STORES TANGENTIALLY AIRCRAFT HAZARDS, CONFERENCES, DOPPLER RADAR, 

MOUNTED ON A FLAT PLATE AT SUPERSONIC SPEEDS 

FLOYD J. WILCOX, JR. Sep. 1987 68 p 

[NASA-TP-2742: L-16284; NAS 1.60:2742) Avail: NTlS HC 

MICROBURSTS, RADAR MEASUREMENT, WIND SHEAR 

A04/MF A01 CSCL 01A N87-22634*# National Aeronautics and Space Administration. 

FLAT PLATES, MOUNTING, SUPERSONIC SPEED, TANGENTS 

AERODYNAMIC DRAG, BLUNT BODIES, EXTERNAL STORES, Ames Research Center, Moffett Field, Calif. 

COCKPIT RESOURCE MANAGEMENT TRAINING 

HARRY W. ORLADY, ed. (Orlady Associates, Inc., Los Gatos, 

Calif.) and H. CLAYTON FOUSHEE, ed. May 1987 308 p 

Workshop held in San Francisco, Calif., 6-8 May 1986; sponsored 

by NASA. Ames Research Center and Air Force Military Airlift 

N87-27643'# National Aeronautics and Space Administration. (NASA-CP-2455; A-87038; NAS 1.55:2455) Avail: NTlS HC 

Langley Research Center, Hampton, Va. A14/MF A01 CSCL 01C 

PRESSURE MEASUREMENTS ON A THICK CAMBERED AND 

TWISTED 58 DEG DELTA WING AT HIGH SUBSONIC SPEEDS 

FLIGHT CREWS, FLIGHT SIMULATION, FLIGHT TRAINING, 

GROUP DYNAMICS, PERSONNEL MANAGEMENT 

JULIO CHU and JOHN E. LAMAR Sep. 1987 233 p 

(NASA-TP-2713; L-16224; NAS 1.60:2713) Avail: NTIS HC 

A1 1 IMF A01 CSCL 01A N87-29469*# National Aeronautics and Space Administration. 

Langley Research Center, Hampton. Va. 

SUBSONIC SPEED, THICKNESS, TWISTED WINGS JET TRANSPORT FLIGHT OPERATIONS USING COCKPIT 

DISPLAY OF TRAFFIC INFORMATION DURING INSTRUMENT 

METEOROLOGICAL CONDITIONS SIMULATION EVALUATION 

DAVID H. WILLIAMS and DOUGLAS C. WELLS May 1986 

50 D 

CAMBER, DELTA WINGS, PRESSURE MEASUREMENT, 

(NASA-TP-2567; L-16091; NAS 1.60:2567) Avail: NTlS HC 

AO3/MF A01 CSCL 01C N87-29432'# National Aeronautics and Space Administration. 

Ames Research Center, Moffett Field, Calif. 

AUTOMATED REDUCTION OF DATA FROM IMAGES AND 

HOLOGRAMS 

G. LEE, ed., JAMES D. TROLINGER, ed. (Spectron Development 

Labs., Inc., Costa Mesa, Calif.), and Y. H. YU, ed. May 1987 

614 p Workshop held at Moffett Field, Calif., 10-11 Jan. 1985 

(NASA-CP-2477; A-87135; NAS 1.55:2477) Avail: NTIS HC 

A99/MF A01 CSCL 01A 

RAPHIC INTERFEROMETRY, IMAGE ANALYSIS, PARTICLE SIZE 

DISTRIBUTION 

AIR TRAFFIC CONTROL, COCKPIT SIMULATORS, DISPLAY 

PORT AIRCRAFT, VIDEO COMMUNICATION, WORKLOADS 

~PSYCHOPHYSIOLOGY) 

DEVICES, INSTRUMENT APPROACH, JET AIRCRAFT, TRANSCOMBUSTIBLE FLOW, DIGITAL TECHNIQUES, HOLOG05 

AIRCRAFT DESIGN, TESTING AND 

PERFORMANCE 

N87-29462'# 

Langley Research Center, Hampton, Va. 

National Aeronautics and Space Administration. 

LOW-SPEED AERODYNAMIC CHARACTERISTICS OF A 

WIN-ENGINE GENERAL AVIATION CONFIGURATION WITH 

AFT-FUSELAGE-MOUNTED PUSHER PROPELLERS 

DANA MORRIS DUNHAM, GARL L. GENTRY, JR., GREGORY S. 

MANUEL, ZACHARY T. APPLIN, and P. FRANK QUINT0 Oct. 

1987 116 p 

(NASA-TP-2763; L-16331; NAS 1.60:2763) Avail: NTlS HC 

AO6/MF A01 CSCL 01A 

AERODYNAMIC CHARACTERISTICS, GENERAL AVIATION 

AIRCRAFT, LOW SPEED, PROPELLERS, PROPULSION SYSTEM 

CONFIGURATIONS, PYLON MOUNTING, TURBOPROP 

ENGINES 

Includes aircraft simulation technology. 

N87-11717'# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

RECENT EXPERIENCES IN MULTIDISCIPLINARY ANALYSIS 

AND OPTIMIZATION, PART 1 

J. SOBIESKI, comp. 1984 517 p Symposium held in Hampton, 

Va., 24-26 Apr. 1984 

(NASA-CP-2327-PT-1; NAS 1.55:2327-PT-l) Avail: NTlS HC 

A221MF A01 CSCL-01C 

AIRCRAFT DESIGN. COMPUTER AIDED DESIGN, CONFERENCES, DESIGN ANALYSIS, OPTIMIZATION, STRUCTURAL DESIGN 

5 
05 AIRCRAFT DESIGN, TESTING AND PERFORMANCE 

N87-11750*# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

RECENT EXPERIENCES IN MULTIDISCIPLINARY ANALYSIS 

AND OPTIMIZATION, PART 2 

J. SOBIESKI, comp. 1984 509 p Symposium held in Hampton, 

Va., 24-26 Apr. 1984 

(NASA-CP-2327-PT-2; L-15830; NAS 1.55:2327-PT-2) Avail: 

NTlS HC A22/MF A01 CSCL 01C 

HELICOPTERS, OPTIMIZATION 

AIRCRAFT DESIGN, COMPUTER AIDED DESIGN, 

N87-15959*# 

Ames Research Center, Moffett Field, Calif. 

National Aeronautics and Space Administration. 

LARGE-SCALE STATIC INVESTIGATION OF CIRCULATIONCONTROL-WING CONCEPTS APPLIED TO UPPER SURFACEBLOWING AIRCRAFT 

M. D. SHOVLIN, R. J. ENGLAR (Naval Ship Research and 

Development Center, Bethesda, Md.), J. C. EPPEL, and J. H. 

NICHOLS, JR. Jan. 1987 65 p 

(NASA-TP-2684; NAS 1.60:2684) 

CSCL 01c 

CIRCULATION CONTROL AIRFOILS, GROUND TESTS, LIFT 

AUGMENTATION, SHORT TAKEOFF AIRCRAFT, STATIC TESTS, 

THRUST CONTROL, TURBOFAN ENGINES, UPPER SURFACE 

BLOWING 

Avail: NTlS HC A04/MF A01 

N87-16815*# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

FLIGHT INVESTIGATION OF THE EFFECT OF TAIL 

CONFIGURATION ON STALL, SPIN, AND RECOVERY 

RESEARCH AIRPLANE 

H. PAUL STOUGH, 111, JAMES M. PATTON. JR.. and STEVEN M. 

SLIWA Feb. 1987 125 p 

(NASA-TP-2644; L-16194; NAS 1.60:2644) Avail: NTlS HC 

AO6/MF A01 CSCL 01C 

CHARACTERISTICS OF A LOW-WING GENERAL AVIATION 

AERODYNAMIC CONFIGURATIONS, AERODYNAMIC STALLING, AIRCRAFT SPIN, GENERAL AVIATION AIRCRAFT, RESEARCH AIRCRAFT, TAIL ASSEMBLIES 

N87-17690'# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

EXPLOITING SYMMETRIES IN THE MODELING AND ANALYSIS 

OF TIRES 

AHMED K. NOOR (Joint Inst. for Advancement of Flight Sciences, 

Hampton, Va.), CARL M. ANDERSEN (College of William and Mary, 

Hampton, Va.), and JOHN A. TANNER Mar. 1987 63 p 

(NASA-TP-2649; L-16185; NAS 1.60:2649) Avail: NTlS HC 

A04lMF A01 CSCL 01C 

SYMMETRY, TIRES 

(NCC1-40) 

FINITE ELEMENT METHOD, MATHEMATICAL MODELS, 

N87-17693'# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

EFFECTS OF EMPENNAGE SURFACE LOCATION ON 

AFTERBODY MODEL WITH NONAXISYMMETRIC NOZZLES 

FRANCIS J. CAPONE and GEORGE T. CARSON, JR. 

1985 79 p 

(NASA-TP-2392; L-15825; NAS 1.60:2392) 

A05/MF A01 CSCL 01C 

AERODYNAMIC CHARACTERISTICS, AERODYNAMIC DRAG, 

AFTERBODIES, AXISYMMETRIC BODIES, FIGHTER AIRCRAFT, 

NOZZLE GEOMETRY, TAIL ASSEMBLIES, TAIL SURFACES 

AERODYNAMIC CHARACTERISTICS OF A TWIN-ENGINE 

Feb. 

Avail: NTlS HC 

N87-20990'# 

Ames Research Center, Moffett Field, Calif. 

SUMMARY OF STUDIES TO REDUCE WING-MOUNTED 

PROPFAN INSTALLATION DRAG ON AN M = 0.8 

TRANSPORT 

RONALD C. SMITH, ALAN D. LEVIN, and RICHARD D. WOOD 

May 1987 29 p 

(NASA-TP-2678; A-86242; NAS 1.60:2678) Avail: NTlS HC 

A03/MF A01 CSCL 01C 

TRANSPORT AIRCRAFT, WIND TUNNEL TESTS 

N87-23614*# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

FLIGHT INVESTIGATION OF THE EFFECTS OF AN OUTBOARD 

National Aeronautics and Space Administration. 

DRAG REDUCTION, HIGH SPEED, PROP-FAN TECHNOLOGY, 

WING-LEADING-EDGE MODIFICATION ON STALLBPIN 

CHARACTERISTICS OF A LOW-WING, SINGLE-ENGINE, T-TAIL 

LIGHT AIRPLANE 

H. PAUL STOUGH, 111, DANIEL J. DICARLO, and JAMES M. 

PATTON, JR. Jul. 1987 117 p 

(NASA-TP-2691; L-16243; NAS 1.60:2691) Avail: NTlS HC 

AO6IMF A01 CSCL 01A 

LEADING EDGES, REVISIONS, SPIN, WINGS 

N87-24458*# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

MEASUREMENTS OF FLOW RATE AND TRAJECTORY OF 

AIRCRAFT TIRE-GENERATED WATER SPRAY 

ROBERT H. DAUGHERTY and SANDY M. STUBBS Jul. 1987 

118 p 

(NASA-TP-2718; L-16195; NAS 1.60:2718) Avail: NTlS HC 

AO6/MF A01 CSCL 01C 

INGESTION (ENGINES), SPLASHING, SPRAYING 

N87-26041'# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

EVALUATION OF INSTALLED PERFORMANCE OF A 

WING 

JAMES C. PATTERSON, JR. and GLYNN R. BARTLETT 

1987 30 p 

(NASA-TP-2739; L-16252; NAS 1.60:2739) Avail: NTlS HC 

A03/MF A01 CSCL 01C 

ENGINES, TURBOPROP ENGINES, WING TIP VORTICES 

AERODYNAMIC STALLING, FLIGHT TESTS, INVESTIGATION, 

AIRCRAFT TIRES, ENGINE INLETS, FLOW VELOCITY, 

WING-TIP-MOUNTED PUSHER TURBOPROP ON A SEMISPAN 

Aug. 

INSTALLING, PROPELLERS, SEMISPAN MODELS, TURBOFAN 

N87-29497*# National Aeronautics and Space Administration. 

Ames Research Center, Moffett Field, Calif. 

QUALITATIVE EVALUATION OF A FLUSH AIR DATA SYSTEM 

AT TRANSONIC SPEEDS AND HIGH ANGLES OF ATTACK 

TERRY J. LARSON, STEPHEN A. WHITMORE, L. J. 

EHERNBERGER. J. BLAIR JOHNSON, and PAUL M. SIEMERS, 

111 Washington NASA Apr. 1987 64 p 

(NASA-TP-2716; H-1277; NAS 1.60:2716) 

A04lMF A01 CSCL 01C 

AIR DATA SYSTEMS, ANGLE OF ATTACK, FLOW 

DISTRIBUTION, ORIFICE FLOW, PITOT TUBES, STAGNATION 

PRESSURE, TRANSONIC SPEED 

N87-29499'# National Aeronautics and Space Administration. 

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

APPLICATION OF PARAMETER ESTIMATION TO AIRCRAFT 

STABILITY AND CONTROL: THE OUTPUT-ERROR APPROACH 

RICHARD E. MAINE and KENNETH W. ILIFF Jun. 1986 

175 p Submitted for publication 

(NASA-RP-1168; H-1299; NAS 1.61:1168) Avail: NTlS HC 

The practical application of parameter estimation methodology 

to the problem of estimating aircraft stability and control derivatives 

from flight test data is examined. The primary purpose of the 

Avail: NTlS HC 

A08lMF A01 CSCL 01c 

6 
07 AIRCRAFT PROPULSION AND POWER 

document is to present a comprehensive and unified picture of 

the entire parameter estimation process and its integration into a 

flight test program. The document concentrates on the output-error 

method to provide a focus for detailed examination and to allow 

us to give specific examples of situations that have arisen. The 

document first derives the aircraft equations of motion in a form 

suitable for application to estimation of stability and control 

derivatives. It then discusses the issues that arise in adapting the 

equations to the limitations of analysis programs, using a specific 

program for an example. The roles and issues relating to mass 

distribution data, preflight predictions, maneuver design, flight 

scheduling, instrumentation sensors, data acquisition systems, and 

data processing are then addressed. Finally, the document 

discusses evaluation and the use of the analysis results. Author 

applications of signal conditioning for the most common flight-test 

data-acquisition systems. A limited amount of theoretical discussion 

is included to assist the reader in a more complete understanding 

of the subject matter. Nonspecific signal conditioning, such as 

amplification, filtering, and multiplexing, is discussed. Signal 

conditioning for various specific transducers and data terminal 

devices is also discussed to illustrate signal conditioning that is 

unique to particular types of transducers. The purpose is to 

delineate for the reader the various signal-conditioning technique 

options, together with tradeoff considerations, for commonly 

encountered flight-test situations. Author 

06 

AIRCRAFT INSTRUMENTATION 

Includes cockpit and cabin display devices; and flight instruments. 

07 

N87-10864'# 

Langley Research Center, Hampton, Va. 

National Aeronautics and Space Administration. 

GROUND-BASED TIME-GUIDANCE ALGORITHM FOR CONTROL OF AIRPLANES IN ATIME-METERED AIRTRAFFIC CONTROL ENVIRONMENT: A PILOTED SIMULATION STUDY 

C. E. KNOX and N. IMBERT (Office National d'Etudes et de 

Recherches Aerospatiales, Toulouse, France) Nov. 1986 36 p 

(NASA-TP-2616; L-16116; NAS 1.60:2616) Avail: NTlS HC 

AO3IMF A01 CSCL 01 D 

AIR TRAFFIC CONTROL, ENERGY CONSERVATION, FLIGHT 

MANAGEMENT SYSTEMS, FLIGHT SIMULATION, FUEL 

CONSUMPTION, PILOTS (PERSONNEL), TIMING DEVICES 

N87-13438'# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

DEVELOPMENT AND EVALUATION OF AN AIRPLANE 

ELECTRONIC DISPLAY FORMAT ALIGNED WITH THE 

INERTIAL VELOCITY VECTOR 

G. G. STEINMETZ Dec. 1986 23 p 

(NASA-TP-2648; L-16168; NAS 1.60:2648) Avail: NTlS HC 

A02/MF A01 CSCL 01D 

ALIGNMENT, DIRECTIONAL CONTROL, DISPLAY DEVICES, 

ELECTRONIC EQUIPMENT, FLIGHT TESTS, INERTIAL 

NAVIGATION, PERFORMANCE TESTS, .VELOCITY 

N87-19393'# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

A SIMULATION EVALUATION OF A PILOT INTERFACE WITH 

AN AUTOMATIC TERMINAL APPROACH SYSTEM 

DAVID A. HINTON Apr. 1987 21 p 

(NASA-TP-2669; L-16222; NAS 1.60:2669) Avail: NTlS HC 

A02/MF A01 CSCL 17G 

APPROACH CONTROL, AUTOMATIC CONTROL, AUTOMATIC 

PILOTS, GENERAL AVIATION AIRCRAFT, MAN MACHINE 

SYSTEMS 

N87-29533'# 

Ames Research Center, Moffett Field, Calif. 

INSTRUMENTATION 

DONALD W. VEATCH and RODNEY K. BOGUE Washington 

NASA Jan. 1986 173 p Presented at the AGARD Flight 

Mechanics Panel, Flight-test Techniques Working Group, 

AGARDograph 160, Flight-Test Instrumentation Series Previously 

announced as N86-29816 

(NASA-RP-1159; H-1191; NAS 1.61 :1159) Avail: NTlS HC 

A08lMF A01 CSCL 01 D 

The application of analog signal conditioning to flight-tests data 

acquisition systems is discussed. Emphasis is placed on practical 

National Aeronautics and Space Administration. 

ANALOG SIGNAL CONDITIONING FOR FLIGHT-TEST 

AIRCRAFT PROPULSION AND POWER 

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

gas turbine engines and compressors; and onboard auxiliary power 

plants for aircraft. 

N87-17699'# 

Lewis Research Center, Cleveland, Ohio. 

COMPRESSOR AND OVERALL PERFORMANCE FOR FIRST 3 

STAGES 

RONALD J. STEINKE May 1986 35 p 

(NASA-TP-2597; E-2589; NAS 1.60:2597) Avail: NTlS HC 

AO3IMF A01 CSCL 21 E 

COMPRESSORS, DESIGN ANALYSIS, FLOW DISTRIBUTION, 

PERFORMANCE TESTS, ROTOR BLADES (TURBOMACHINERY) 

National Aeronautics and Space Administration. 

DESIGN OF 9.271-PRESSURE-RATIO STAGE CORE 

N87-20267'# 

Lewis Research Center, Cleveland, Ohio. 

SYMPOSIUM 

1986 230 p Symposium held in Cleveland, Ohio, 23-27 Sep. 

1985 

(NASA-CP-2433; E-3033; NAS 1.55:2433) Avail: NTlS HC 

A01 IMF A01 CSCL 21 E 

National Aeronautics and Space Administration. 

NASA-CHINESE AERONAUTICAL ESTABLISHMENT (CAE) 

COMBUSTION, FLUID DYNAMICS, THERMODYNAMICS 

N87-24481'# 

Lewis Research Center, Cleveland, Ohio. 

BLADE TIP CLEARANCE MEASUREMENT SYSTEM 

JOHN P. BARRANGER Jul. 1987 16 p 

(NASA-TP-2746; E-3455; NAS 1.60:2746) Avail: NTlS HC 

A02lMF A01 CSCL 21 E 

BLADE TIPS, ERROR ANALYSIS, FREQUENCY 

MODULATION, NONDESTRUCTIVE TESTS, OSCILLATORS, 

ROTOR BLADES (TURBOMACHINERY) 

National Aeronautics and Space Administration. 

LOW-COST FM OSCILLATOR FOR CAPACITANCE TYPE OF 

7 
08 AIRCRAFT STABILITY AND CONTROL 

AIRCRAFT STABILITY AND CONTROL 

Includes aircraft handling qualities; piloting; flight controls; and 

autopilots. 

N87-10103'# 

Ames Research Center, Moffett Field, Calif. 

National Aeronautics and Space Administration. 

IN-FLIGHT TOTAL FORCES, MOMENTS AND STATIC 

AEROELASTIC CHARACTERISTICS OF AN OBLIQUE-WING 

RESEARCH AIRPLANE 

R. E. CURRY and A. G. SIM 

(NASA-TP-2224; H-1181; NAS 1.60:2224) Avail: NTlS HC 

A03fMF A01 CSCL 01C 

AEROELASTIC RESEARCH WINGS, AIRCRAFT DESIGN, 

FLIGHT TESTS, OBLIQUE WINGS, RESEARCH AIRCRAFT, 

STRUCTURAL DESIGN, WIND TUNNEL TESTS 

Oct. 1984 30 p 

N87-10870'# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

INTERFERENCE EFFECTS OF THRUST REVERSING ON 

FIGHTER AIRCRAFT AT MACH NUMBERS FROM 0.15 TO 0.90 

F. J. CAPONE and M. L. MASON Oct. 1984 

(NASA-TP-2350; L-15811; NAS 1.60:2350) 

AO6fMF A01 CSCL 01C 

ASSEMBLIES, THRUST REVERSAL, WIND TUNNEL TESTS 

HORIZONTAL TAIL EFFECTIVENESS OF TWIN-ENGINE 

104 p 

Avail: NTlS HC 

AERODYNAMIC INTERFERENCE, FIGHTER AIRCRAFT, TAIL 

N87-10871'# 

Ames Research Center, Moffett Field, Calif. 

National Aeronautics and Space Administration. 

FLIGHT-DETERMINED AERODYNAMIC DERIVATIVES OF THE 

AD1 OBLIQUE-WING RESEARCH AIRPLANE 

A. G. SIM and R. E. CURRY Oct. 1984 40 p 

(NASA-TP-2222; H-1179; NAS 1.60:2222) Avail: NTlS HC 

A03/MF A01 CSCL 01C 

RESEARCH AIRCRAFT, VARIABLE SWEEP WINGS 

AERODYNAMIC COEFFICIENTS, OBLIQUE WINGS, 

N87-16849'# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

PILOTED SIMULATOR STUDY OF ALLOWABLE TIME DELAYS 

WILLIAM D. GRANTHAM, PAUL M. SMITH (PRC Kentron, Inc., 

Harnpton, Va.). LEE H. PERSON, JR., ROBERT T. MEYER 

(Lockheed-Georgia Co., Marietta), and STEPHEN A. TINGAS Feb. 

1987 69 p 

(NASA-TP-2652; L-16149; NAS 1.60:2652) Avail: NTlS HC 

A04fMF A01 CSCL 01C 

CONTROL SYSTEMS DESIGN, FLIGHT CHARACTERISTICS, 

FLIGHT SIMULATORS, LOW SPEED, TIME LAG, TRANSPORT 

AIRCRAFT 

IN LARGE-AIRPLANE RESPONSE 

N87-18570'# 

Ames Research Center, Moffett Field, Calif. 

FLIGHT CHARACTERISTICS OF THE AD-1 OBLIQUE-WING 

RESEARCH AIRCRAFT 

ALEX G. SIM and ROBERT E. CURRY 

National Aeronautics and Space Administration. 

Mar. 1985 29 D 

(NASA-TP-2223; H-1180; NAS 1.60:2223) Avail: NTlS HC 

A03fMF A01 CSCL 01C 

TICS, LOW SPEED, OBLIQUE WINGS, RESEARCH AIRCRAFT 

AERODYNAMIC CONFIGURATIONS, FLIGHT CHARACTERISN87-25331*# National Aeronautics and Space Administration. 

Lewis Research Center, Cleveland, Ohio. 

ADVANCED DETECTION, ISOLATION AND ACCOMMODATION 

WALTER C. MERRILL, JOHN C. DELAAT, and WILLIAM M. 

BRUTON Jul. 1987 30 p 

(NASA-TP-2740; E-3479; NAS 1.60:2740) Avail: US Patent and 

Trademark Office CSCL 01 C 

ENGINE CONTROL, ENGINE FAILURE, FAULT TOLERANCE, 

REDUNDANCY ENCODING, REMOTE SENSORS, TURBINE 

ENGINES 

N87-26922*# 

Langley Research Center, Hampton, Va. 

OF SENSOR FAILURES REAL-TIME EVALUATION 

National Aeronautics and Space Administration. 

PILOTED-SIMULATION STUDY OF EFFECTS OF VORTEX 

FLAPS ON LOW-SPEED HANDLING QUALITIES OF A 

DELTA-WING AIRPLANE 

JAY M. BRANDON, PHILIP W. BROWN, and ALFRED J. 

WUNSCHEL Sep. 1987 38 p 

(NASA-TP-2747; L-16307; NAS 1.60:2747) Avail: NTlS HC 

AO3fMF A01 CSCL 01C 

LOW SPEED, PILOTS (PERSONNEL), VORTEX FLAPS 

CONTROLLABILITY, DELTA WINGS, FLIGHT SIMULATION, 

09 

RESEARCH AND SUPPORT FACILITIES (AIR) 

Includes airports, hangars and runways; aircraft repair and overhaul 

facilities; wind tunnels; shock tubes; and aircraft engine test 

stands. 

N87-10876'# 

Washington, D.C. 

AERONAUTICAL FACILITIES ASSESSMENT 

F. E. PENARANDA. comp. Nov. 1985 204 p 

(NASA-RP-1146; NAS 1.61:1146) Avail: NTlS HC AlO/MF A01 

CSCL 14B 

A survey of the free world's aeronautical facilities was 

undertaken and an evaluation made on where the relative strengths 

and weaknesses exist. Special emphasis is given to NASA's own 

capabilities and needs. The types of facilities surveyed are: Wind 

Tunnels; Airbreathing Propulsion Facilities; and Flight Simulators 

Author 

National Aeronautics and Space Administration, 

N87-17717'# National Aeronautics and Space Administration. 

Lewis Research Center, Cleveland, Ohio. 

EXPERIMENTAL EVALUATION OF WALL MACH NUMBER 

DISTRIBUTIONS OF THE OCTAGONAL TEST SECTION 

PROPOSED FOR NASA LEWIS RESEARCH CENTER'S 

ALTITUDE WIND TUNNEL 

DOUGLAS E. HARRINGTON, RICHARD R. BURLEY, and ROBERT 

R. CORBAN Nov. 1986 35 p 

(NASA-TP-2666; E-3145; NAS 1.60:2666) Avail: NTlS HC 

AO3/MF A01 CSCL 148 

APPARATUS. WIND TUNNEL WALLS 

FLOW VELOCITY, MACH NUMBER, WIND TUNNEL 

N87-18576'# National Aeronautics and Space Administration. 

Lewis Research Center, Cleveland, Ohio. 

EXPERIMENTAL EVALUATION OF TWO TURNING VANE 

DESIGNS FOR FAN DRIVE CORNER OF 0.1-SCALE MODEL 

OF NASA LEWIS RESEARCH CENTER'S PROPOSED ALTITUDE 

WIND TUNNEL 

DONALD R. BOLDMAN, ROYCE D. MOORE, and RICKEY J. 

SHYNE Mar. 1987 148 p 

(NASA-TP-2646; E-3175; NAS 1.60:2646) 

A07fMF A01 CSCL 148 

TUNNEL DRIVES 

Avail: NTlS HC 

CORNER FLOW, VANES, WIND TUNNEL APPARATUS, WIND 

8 
15 LAUNCH VEHICLES AND SPACE VEHICLES 

N87-20295*# National Aeronautics and Space Administration. 

Lewis Research Center, Cleveland, Ohio. 

DETAILED FLOW SURVEYS OF TURNING VANES DESIGNED 

FOR A 0.1-SCALE MODEL OF NASA LEWIS RESEARCH 

CENTER'S PROPOSED ALTITUDE WIND TUNNEL 

ROYCE D. MOORE, RICKEY J. SHYNE, DONALD R. BOLDMAN, 

and THOMAS F. GELDER Apr. 1987 151 p 

(NASA-TP-2680; E-3294; NAS 1.60:2680) Avail: NTlS HC 

A081MF A01 CSCL 148 

VANES, WIND TUNNEL APPARATUS, WIND TUNNEL DRIVES 

ALTITUDE SIMULATION, FLOW DISTRIBUTION, GUIDE 

N87-22694'# National Aeronautics and Space Administration. 

Lewis Research Center, Cleveland, Ohio. 

EXPERIMENTAL EVALUATION OF BLOCKAGE RATIO AND 

PLENUM EVACUATION SYSTEM FLOW EFFECTS ON 

PRESSURE DISTRIBUTION FOR BODIES OF REVOLUTION IN 

0.1 SCALE MODEL TEST SECTION OF NASA LEWIS 

RESEARCH CENTER'S PROPOSED ALTITUDE WIND TUNNEL 

RICHARD R. BURLEY and DOUGLAS E. HARRINGTON Apr. 

1987 26 p 

(NASA-TP-2702; E-3267; NAS 1.60:2702) Avail: NTlS HC 

A031MF A01 CSCL 14B 

CHAMBERS, WIND TUNNEL MODELS, WIND TUNNEL TESTS 

EVACUATING . (VACUUM), EVALUATION, PLENUM 

N87-23662'# National Aeronautics and Space Administration. 

Lewis Research Center, Cleveland, Ohio. 

EXPERIMENTAL EVALUATION OF HONEYCOMB/SCREEN 

CONFIGURATIONS AND SHORT CONTRACTION SECTION FOR 

NASA LEWIS RESEARCH CENTER'S ALTITUDE WIND 

TUNNEL 

RICHARD R. BURLEY and DOUGLAS E. HARRINGTON May 

1987 30 p 

(NASA-TP-2692; E-3142; NAS 1.60:2692) Avail: NTlS HC 

AOSIMF A01 CSCL 148 

HONEYCOMB STRUCTURES, PRESSURE DISTRIBUTION, 

SCREENS, TURBULENCE EFFECTS, TURBULENT FLOW, WIND 

TUNNEL CALIBRATION 

N87-28570'# 

Langley Research Center, Hampton, Va. 

National Aeronautics and Space Administration. 

EVOLUTION, CALIBRATION, AND OPERATIONAL CHARACTERISTICS OF THE TWO-DIMENSIONAL TEST SECTION OF THE 

LANGLEY 0.3-METER TRANSONIC CRYOGENIC TUNNEL 

CHARLES L. LADSON and EDWARD J. RAY Sep. 1987 

171 p 

(NASA-TP-2749; L-16190; NAS 1.60:2749) Avail: NTlS HC 

AOBIMF A01 CSCL 148 

CRYOGENIC WIND TUNNELS, EVOLUTION (DEVELOPMENT), 

HISTORIES, TRANSONIC WIND TUNNELS, TWO DIMENSIONAL 

FLOW 

N87-29544'# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

LANGLEY AIRCRAFT LANDING DYNAMICS FACILITY 

PAMELA A. DAVIS, SANDY M. STUBBS, and JOHN A. TANNER 

Oct. 1987 35 p 

(NASA-RP-1189; L-16293; NAS 1.61:1189) Avail: NTlS HC 

AOSIMF A01 CSCL 148 

The Langley Research Center has recently upgraded the 

Landing Loads Track (LLT) to improve the capability of low-cost 

testing of conventional and advanced landing gear systems. The 

unique feature of the Langley Aircraft Landing Dynamics Facility 

(ALDF) is the ability to test aircraft landing gear systems on actual 

runway surfaces at operational ground speeds and loading 

conditions. A historical overview of the original LLT is given, 

followed by a detailed description of the new ALDF systems and 

operational capabilities. Author 

12 

ASTRONAUTICS (GENERAL) 

N87-20302'# National Aeronautics and Space Administration. 

Goddard Space Flight Center, Greenbelt, Md. 

THE 1986 GET AWAY SPECIAL EXPERIMENTER'S 

SYMPOSIUM 

LAWRENCE R. THOMAS, ed. and FRANCES L. MOSIER, ed. 

Feb. 1987 236 p Symposium held in Greenbelt, Md., 7-8 Oct. 

1986 

(NASA-CP-2438; NAS 1.55:2438) 

CSCL 22A 

Avail: NTlS HC A1 1 /MF A01 

CONFERENCES, GETAWAY SPECIALS (STS) , GOVERNMENT/ 

INDUSTRY RELATIONS, SPACE SHUTTLE PAYLOADS, UNIVERSITIES 

N87-29576' National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

TECHNOLOGY FOR LARGE SPACE SYSTEMS. A 

BIBLIOGRAPHY WITH INDEXES (SUPPLEMENT 17) 

Oct. 1987 140 p 

(NASA-SP-7046(17); NAS 1.21:7046(17)) Avail: NTlS HC A07 

CSCL 228 

This bibliography lists 51 2 reports, articles, and other documents 

introduced into the NASA scientific and technical information 

system between January 1, 1987 and June 30, 1987. Its purpose 

is to provide helpful information to the researcher, manager, and 

designer in technology development and mission design according 

to system, interactive analysis and design, structural and thermal 

analysis and design, structural concepts and control systems, 

electronics, advanced materials, assembly concepts, propulsion, 

and solar power satellite systems. Author 

15 

LAUNCH VEHICLES AND SPACE VEHICLES 

Includes boosters; operating problems of launchlspace vehicle 

systems; and reusable vehicles. 

N87-12581'# 

Marshall Space Flight Center, Huntsville, Ala. 

SOLAR ARRAY FLIGHT DYNAMIC EXPERIMENT 

R. W. SCHOCK Washington May 1986 27 p 

(NASA-TP-2598; NAS 1.60:2598) Avail: NTlS HC AOSIMF A01 

CSCL 10A 

LARGE SPACE STRUCTURES, LASER APPLICATIONS, 

SOLAR ARRAYS, SPACE SHUTTLE PAYLOADS, TRACKING 

(POSITION) 

National Aeronautics and Space Administration. 

N87-18588*# National Aeronautics and Space Administration. 

Marshall Space Flight Center, Huntsville, Ala. 

SYSTEM STUDY OF THE CARBON DIOXIDE OBSERVATIONAL 

J. BRISCOE STEPHENS and WILBUR E. THOMPSON Mar. 

1987 35 p 

(NASA-TP-2696; NAS 1.60:2696) 

CSCL 228 

SENSING, SPACE PLATFORMS 

PLATFORM SYSTEM (CO-OPS): PROJECT OVERVIEW 

Avail: NTlS HC A03lMF A01 

ATMOSPHERIC COMPOSITION, CARBON DIOXIDE, REMOTE 

9 
15 LAUNCH VEHICLES AND SPACE VEHICLES 

N87-22702'# National Aeronautics and Space Administration. 

Marshall Space Flight Center, Huntsville, Ala. 

STRUCTURAL DYNAMICS AND CONTROL INTERACTION OF 

FLEXIBLE STRUCTURES 

ROBERT S. RYAN, ed. and HAROLD N. SCOFIELD, ed. Apr. 

1987 680 p Workshop held in Huntsville, ALa., 22-24 Apr. 

1986 

(NASA-CP-2467-PT-1; M-554-PT-1; NAS 1.55:2467-PT-l) Avail: 

NTlS HC A99/MF E03 

CONTROL SYSTEMS DESIGN, DYNAMIC STRUCTURAL 

ANALYSIS, FLEXIBLE BODIES, LARGE SPACE STRUCTURES, 

SPACECRAFT CONTROL 

N87-22729'# National Aeronautics and Space Administration. 

Marshall Space Flight Center, Huntsville, Ala. 

STRUCTURAL DYNAMICS AND CONTROL INTERACTION OF 

FLEXIBLE STRUCTURES 

ROBERT S. RYAN, ed. and HAROLD N. SCOFIELD, ed. Apr. 

1987 729 p Workshop held in Huntsville, Ala., 22-24 Apr. 

1986 

(NASA-CP-2467-PT-2; M-554-PT-2; NAS 1.55:2467-PT-2) Avail: 

NTlS HC A99/MF E03 

CONFERENCES, DESIGN ANALYSIS, DYNAMIC STRUCTURAL 

ANALYSIS, FLEXIBLE BODIES, JOINTS (JUNCTIONS), LARGE 

SPACE STRUCTURES, ORBITAL SPACE STATIONS 

CSCL 228 

CSCL 228 

16 

SPACE TRANSPORTATION 

Includes passenger and cargo space transportation, e.g., shuttle 

operations; and space rescue techniques. 

N87-12585'# National Aeronautics and Space Administration. 

Marshall Space Flight Center, Huntsville, Ala. 

DEVELOPMENT TESTING OF LARGE VOLUME WATER 

SPRAYS FOR WARM FOG DISPERSAL 

V. W. KELLER, B. J. ANDERSON, R. A. BURNS, G. G. LALA 

(New York State Univ., Albany), M. B. MEYER, and K. V. BEARD 

(Illinois Univ., Urbana-Champaign) Washington Jun. 1986 

112 p 

(NASA-TP-2607; NAS 1.60:2607) Avail: NTlS HC AO6/MF A01 

CSCL 148 

SPACECRAFT LAUNCHING, SPRAY NOZZLES, WATER 

COALESCING, FOG DISPERSAL, SPACE SHUTTLES, 

18 

SPACECRAFT DESIGN, TESTING AND 

PERFORMANCE 

Includes satellites; space platforms; space stations; spacecraft 

systems and components such as thermal and environmental 

controls; and attitude controls. 

N87-16014'# 

Langley Research Center, Hampton, Va. 

OGY, 1986 

ROBERT L. WRIGHT, comp. Nov. 1986 549 p Conference 

held in Norfolk, Va.. 18-21 Nov. 1986; sponsored by NASA Langley 

Research Center and AFWAL 

Avail: NTlS HC A23/MF A01 

ANTENNAS, CONFERENCES, FLEXIBLE SPACECRAFT, 

LARGE SPACE STRUCTURES, SPACE STATIONS, SPACECRAFT 

National Aeronautics and Space Administration. 

NASNDOD CONTROUSTRUCTURES INTERACTION TECHNOL- 

(NASA-CP-2447-PT-1; L-16242-PT-1; NAS 1.552447-PT-1) 

CSCL 228 

CONTROL, SPACECRAFT DESIGN, SYSTEMS ENGINEERING, 

TRUSSES, VIBRATION DAMPING 

N87-24495'# 

Langley Research Center, Hampton, Va. 

OGY, 1986 

ROBERT L. WRIGHT, comp. Jun. 1987 314 p Conference 

held in Norfolk, Va.. 18-21 Nov. 1986 

Avail: NTlS HC A14/MF A01 

CONTROL STABILITY, CONTROL SYSTEMS DESIGN, 

INTERACTIVE CONTROL, ORBITAL SPACE STATIONS, 

SPACECRAFT CONTROL, VIBRATION DAMPING 

National Aeronautics and Space Administration. 

NASNDOD CONTROUSTRUCTURES INTERACTION TECHNOL- 

(NASA-CP-2447-PT-2; L-16242-PT-2; NAS 1.5512447-PT-2) 

CSCL 228 

N87-26073' National Aeronautics and Space Administration, 

Washington, D.C. 

SPACE STATION SYSTEMS A BIBLIOGRAPHY WITH INDEXES 

(SUPPLEMENT 4) 

May 1987 220 p 

(NASA-SP-7056(04); NAS 1.21 :7056(04)) Avail: NTlS HC A1 0 

CSCL 228 

This bibliography lists 832 reports, articles, and other documents 

introduced into the NASA scientific and technical information 

system between July 1, 1986 and December 31, 1986. Its purpose 

is to provide helpful information to the researcher, manager, and 

designer in technology development and mission design according 

to system, interactive analysis and design, structural and thermal 

analysis and design, structural concepts and control systems, 

electronics, advanced materials, assembly concepts, propulsion, 

and solar power satellite systems. The coverage includes 

documents that define major systems and subsystems, servicing 

and support requirements, procedures and operations, and missions 

for the current and future space station. Author 

20 

SPACECRAFT PROPULSION AND POWER 

Includes main propulsion systems and components, e.g., rocket 

engines; and spacecraft auxiliary power sources. 

N87-20380'# 

Marshall Space Flight Center, Huntsville, Ala. 

TION EXPERIMENT 

LEIGHTON E. YOUNG and HOMER C. PACK, JR. 

72 P 

(NASA-TP-2690; NAS 1.60:2690) Avail: NTlS HC A04/MF A01 

CSCL 10A 

LARGE SPACE STRUCTURES, SOLAR ARRAYS, SOLAR 

DYNAMIC POWER SYSTEMS, SPACE ERECTABLE 

STRUCTURES,SPACE SHUTTLE PAYLOADS 

National Aeronautics and Space Administration. 

SOLAR ARRAY FLIGHT EXPERIMENT/DYNAMIC AUGMENTAFeb. 1987 

N87-20381'# National Aeronautics and Space Administration. 

Lewis Research Center, Cleveland, Ohio. 

EXPERIMENTAL THRUST PERFORMANCE OF A 

ALBERT J. PAVLI, KENNETH J. KACYNSKI, and TAMARA A. 

SMITH Apr. 1987 16 p Presented at the 23rd JANNAF 

Combustion Meeting, Hampton, Va., 20-24 Oct. 1986 

(NASA-TP-2720; E-3236-1 ; NAS 1.60:2720) Avail: NTlS HC 

HIGH-AREA-RATIO ROCKET NOZZLE 

AO2/MF A01 CSCL 21 H 

AREA. NOZZLE GEOMETRY, ROCKET NOZZLES, ROCKET 

THRUST 

10 
24 COMPOSITE MATERIALS 

N87-22766'# National Aeronautics and Space Administration. 

Lewis Research Center, Cleveland, Ohio. 

STRUCTURAL INTEGRITY AND DURABILITY OF REUSABLE 

SPACE PROPULSION SYSTEMS 

1987 205 p Conference held in Cleveland, Ohio, 12-13 May 

1987 

(NASA-CP-2471; E-3512; NAS 1.552471) Avail: NTlS HC 

AlO/MF A01 CSCL 21H 

AEROTHERMODYNAMICS, CONFERENCES, DURABILITY, 

DYNAMIC STRUCTURAL ANALYSIS, FATIGUE (MATERIALS), 

FRACTURE MECHANICS, SPACE SHUTTLE MAIN ENGINE, 

SPACECRAFT PROPULSION, STRUCTURAL RELIABILITY 

N87-25423'# National Aeronautics and Space Administration. 

Lewis Research Center, Cleveland, Ohio. 

COMPARISON OF THEORETICAL AND EXPERIMENTAL 

THRUST PERFORMANCE OF A 10301 AREA RATIO ROCKET 

NOZZLE AT A CHAMBER PRESSURE OF 2413 KN/M2 (350 

PSIA) 

TAMARA A. SMITH, ALBERT J. PAVLI, and KENNETH J. 

KACYNSKI 1987 25 p Presented at the 23rd Joint Propulsion 

Conference, San Diego, Calif., 29 Jun. - 2 Jul. 1987; sponsored 

by AIAA, SAE, ASME and ASEE 

(NASA-TP-2725; E-3523; NAS 1.60:2725; AIAA-87-2069) Avail: 

NTIS HC A02/MF A01 

THRUST 

CSCL 21H 

ENGINE TESTS, PREDICTIONS, ROCKET NOZZLES, ROCKET 

N87-25424'# National Aeronautics and Space Administration. 

Lewis Research Center, Cleveland, Ohio. 

EXPERIMENTAL EVALUATION OF HEAT TRANSFER ON A 

10301 AREA RATIO ROCKET NOZZLE 

KENNETH J. KACYNSKI, ALBERT J. PAVLI, and TAMARA A. 

SMITH Aug. 1987 28 p Presented at the 23rd Joint Propulsion 

Conference, San Diego, Calif., 29 Jun. - 2 Jul. 1987; sponsored 

by AIAA, SAE, ASME and ASEE 

(NASA-TP-2726 E-3558; NAS 1.60:2726; AIAA-87-2070) Avail: 

NTIS HC AOB/MF A01 CSCL 21H 

NOZZLE FLOW, ROCKET NOZZLES, WALL TEMPERATURE 

EXHAUST NOZZLES, HEAT FLUX, HEAT TRANSFER, 

N87-25425'# 

Lewis Research Center, Cleveland, Ohio. 

ROBERT L. ZURAWSKI and DOUGLAS C. RAPP (Sverdrup 

Technology, Inc., Cleveland. Ohio.) Aug. 1987 32 p Presented 

at the 23rd Joint Propulsion Conference, San Diego, Calif. 29 

Jun. - 2 Jul. 1987; sponsored by AIAA, SAE, ASME and ASEE 

(NASA-TP-2751; E-3554; NAS 1.60:2751; AIAA-87-2082) Avail: 

NTlS HC AOWMF A01 CSCL 21 H 

ENGINES, SPACE SHUlTLE BOOSTERS 

National Aeronautics and Space Administration. 

ANALYSIS OF QUASI-HYBRID SOLID ROCKET BOOSTER 

CONCEPTS FOR ADVANCED EARTH-TO-ORBIT VEHICLES 

FEASIBILITY ANALYSIS, HYBRID PROPELLANT ROCKET 

23 

CHEMISTRY AND MATERIALS (GENERAL) 

N87-18611*# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

SPECTROSCOPIC COMPARISON OF EFFECTS OF ELECTRON 

RADIATION ON MECHANICAL PROPERTIES OF TWO 

POLYlMlDES 

EDWARD R. LONG, JR. and SHEILA ANN T. LONG Apr. 1987 

21 P 

(NASA-TP-2663; L-16200; NAS 1.60:2663) 

AOP/MF A01 CSCL 11C 

MARK), RADIATION DAMAGE, TENSILE PROPERTIES 

Avail: NTlS HC 

DURABILITY, ELECTRON RADIATION, KAPTON (TRADE24 

COMPOSITE MATERIALS 

Includes physical, chemical, and mechanical properties of laminates 

and other composite materials. 

N87-10184'# 

Langley Research Center, Hampton, Va. 

FORCED 6061 ALUMINUM 

G. A. DRIES (PRC Kentron, Inc., Hampton, Va.) and S. S. 

TOMPKINS Oct. 1986 29 p 

(NASA-TP-2612; L-16139; NAS 1.60:2612) Avail: NTlS HC 

AOB/MF A01 CSCL 11 D 

ALUMINUM GRAPHITE COMPOSITES, CARBON FIBERS, 

METAL MATRIX COMPOSITES, REINFORCING FIBERS, 

SPACECRAFT STRUCTURES, THERMAL CYCLING TESTS 

National Aeronautics and Space Administration. 

EFFECTS OF THERMAL CYCLING ON GRAPHIE-FIBER-REINN87-25435'# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

PRELIMINARY STRUCTURAL DESIGN OF COMPOSITE MAIN 

ROTOR BLADES FOR MINIMUM WEIGHT 

MARK W. NIXON Jul. 1987 28 p Prepared in cooperation 

with Army Aviation Research and Development Command, 

Hampton, Va. 

Avail: NTlS HC A03/MF A01 

ANALYSIS, HELICOPTERS, ROTORS, WEIGHT REDUCTION 

(DA PROJ. 1 L1-62209-AH-76) 

(NASA-TP-2730; L-16310; NAS 1.60~2730; AVSCOM-TM-87-B-6) 

CSCL 11 D 

BLADES, COMPOSITE MATERIALS, DYNAMIC STRUCTURAL 

N87-29612'# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

THE ACEE PROGRAM AND BASIC COMPOSITES RESEARCH 

AT LANGLEY RESEARCH CENTER (1975 TO 1986): SUMMARY 

AND BIBLIOGRAPHY 

MARVIN B. DOW Oct. 1987 147 p 

(NASA-RP-1177; L-16290; NAS 1.61:1177) Avail: NTlS HC 

A07/MF A01 CSCL 11D 

Composites research conducted at the Langley Research 

Center during the period from 1975 to 1986 is described, and an 

annotated bibliography of over 600 documents (with their abstracts) 

is presented. The research includes Langley basic technology and 

the composite primary structures element of the NASA Aircraft 

Energy Efficiency (ACEE) Program. The basic technology 

documents cited in the bibliography are grouped according to the 

research activity such as design and analysis, fatigue and fracture, 

and damage tolerance. The ACEE documents cover development 

of composite structures for transport aircraft. Author 

11 
25 INORGANIC AND PHYSICAL CHEMISTRY 

INORGANIC AND PHYSICAL CHEMISTRY 

Includes chemical analysis, e.g., chromatography; combustion 

theory; electrochemistry; and photochemistry. 

N87-18629'# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

ELECTRON STIMULATED DESORPTION OF ATOMIC OXYGEN 

FROM SILVER 

R. A. OUTLAW, W. K. PEREGOY, GAR B. HOFLUND (Florida 

Univ., Gainesville), and GREGORY R. CORALLO Apr. 1987 

25 P 

(NASA-TP-2668; L-16225; NAS 1.60:2668) Avail: NTlS HC 

A02/MF A01 CSCL 07D 

OXYGEN, SILVER, STIMULATED EMISSION 

ATOMIC BEAMS, DESORPTION, ELECTRON EMISSION, 

26 

METALLIC MATERIALS 

Includes physical, chemical, and mechanical properties of metals, 

e.g., corrosion; and metallurgy. 

N87-16902'# National Aeronautics and Space Administration. 

Lewis Research Center, Cleveland, Ohio. 

CONVENTIONALLY CAST AND FORGED COPPER ALLOY FOR 

HIGH-HEAT-FLUX THRUST CHAMBERS 

JOHN M. KAZAROFF and GEORGE A. REPAS Feb. 1987 

12 P 

(NASA-TP-2694; E-3304; NAS 1.60:2694) 

A02/MF A01 CSCL 11F 

COMBUSTION CHAMBERS, COPPER ALLOYS, HEAT FLUX, 

HIGH TEMPERATURE, LININGS, SPACE SHUTTLE MAIN 

ENGINE 

Avail: NTlS HC 

N87-18644'# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

EFFECT OF LID (REGISTERED) PROCESSING ON THE 

MICROSTRUCTURE AND MECHANICAL PROPERTIES OF 

MATERIALS 

LINDA B. BALCKBURN Apr. 1987 27 p 

(NASA-TP-2677; L-16098; NAS 1.60:2677) Avail: NTlS HC 

AO3/MF A01 CSCL 11F 

BONDING, DIFFUSION, INTERFACES, LIQUIDS, MECHANICAL 

PROPERTIES, MICROSTRUCTURE, PROTECTIVE COATINGS, 

TITANIUM ALLOYS 

TlbAL-4V AND TlbAL-2SN-4ZR-2MO TITANIUM FOIL-GAUGE 

N87-20407*# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

MATERIAL CHARACTERIZATION OF SUPERPLASTICALLY 

FORMED TITANIUM (TI-6AL-SN-4ZR-2MO) SHEET 

WILLIAM A. OSSA (PRC Kentron, Inc., Hampton, Va.) and DICK 

M. ROYSTER 1987 38 p 

(NASA-TP-2674; L-16115; NAS 1.60:2674) 

A03/MF A01 CSCL 11F 

CREEP, TITANIUM ALLOYS 

Avail: NTlS HC 

AEROSPACE INDUSTRY, SUPERPLASTICITY, TENSILE 

N87-21076"# National Aeronautics and Space Administration. 

Marshall Space Flight Center, Huntsville, Ala. 

THE CORROSION MECHANISMS FOR PRIMER COATED 

2219-T87 ALUMINUM 

MERLIN D. DANFORD and WARD W. KNOCKEMUS (Huntingdon 

Colt., Montgomery. Ala.) Apr. 1987 25 p 

(NASA-TP-2715; M-559; NAS 1.60:2715) Avail: NTlS HC 

A02/MF A01 CSCL 11 F 

(COATINGS), PROTECTIVE COATINGS 

ALUMINUM ALLOYS, CORROSION RESISTANCE, PRIMERS 

N87-25463'# National Aeronautics and Space Administration. 

Marshall Space Flight Center, Huntsville, Ala. 

HYDROGEN TRAPPING AND THE INTERACTION OF 

HYDROGEN WITH METALS 

MERLIN D. DANFORD Jul. 1987 36 p 

(NASA-TP-2744; NAS 1.60:2744) Avail: NTlS HC AO3/MF A01 

CSCL 11F 

GEN, TRAPPING 

CRYSTAL LATTICES, GAS-METAL INTERACTIONS, HYDRON87-27024'# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

PERMEATION OF OXYGEN THROUGH HIGH PURITY, LARGE 

GRAIN SILVER 

R. A. OUTLAW, W. K. PEREGOY, and GAR 6. HOFLUND (Florida 

Univ., Gainesville.) Sep. 1987 19 p 

(NASA-TP-2755; L-16305; NAS 1.60:2755) Avail: NTlS HC 

A02/MF A01 CSCL 11 F 

SILVER 

GRAIN BOUNDARIES, OXYGEN, PERMEATING, PURITY, 

27 

NONMETALLIC MATERIALS 

Includes physical, chemical, and mechanical properties of plastics, 

elastomers, lubricants, polymers, textiles, adhesives, and ceramic 

materials. 

N87-12680'# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

INVESTIGATION OF THE EFFECTS OF COBALT IONS ON 

EPOXY PROPERTIES 

J. J. SlNGH and D. M. STOAKLEY 

(NASA-TP-2639; L-16196; NAS 1.60:2639) 

AO2/MF A01 CSCL 11 G 

MECHANICAL PROPERTIES 

Dec. 1986 16 p 

Avail: NTlS HC 

COBALT, EPOXY RESINS, INVESTIGATION, IONS, 

N87-18666'# National Aeronautics and Space Administration. 

Lewis Research Center, Cleveland, Ohio. 

ESTER OXIDATION ON AN ALUMINUM SURFACE USING 

CHEMILUMINESCENCE 

WILLIAM R. JONES, JR., MICHAEL A. MEADOR, and WILFRED0 

MORALES Jul. 1986 16 p 

(NASA-TP-2611; E-2647; NAS 1.60:2611) Avail: NTlS HC 

AO2IMF A01 CSCL 116 

METAL SURFACES, OXIDATION 

ALUMINUM ALLOYS, CHEMILUMINESCENCE, ESTERS, 

12 
32 COMMUNICATIONS AND RADAR 

N87-20423*# National Aeronautics and Space Administration. 

Marshall Space Flight Center, Huntsville, Ala. 

MICROGRAVITY CRYSTALLIZATION OF MACROMOLECULES 

AN INTERIM REPORT AND PROPOSAL FOR CONTINUED 

RESEARCH 

BENJAMIN E. GOLDBERG Dec. 1986 26 p 

(NASA-TP-2671; NAS 1.60:2671) Avail: NTlS HC A03IMF A01 

CSCL 208 

REDUCED GRAVITY 

MOLECULES, POLYMER CHEMISTRY, RECRYSTALLIZATION, 

29 

MATERIALS PROCESSING 

Includes space-based development of products and processes for 

commercial applications. 

N87-21141'# National Aeronautics and Space Administration. 

Lewis Research Center, Cleveland, Ohio. 

MICROGRAVITY FLUID MANAGEMENT SYMPOSIUM 

Apr. 1987 225 p Symposium held in Cleveland, Ohio, 9-10 

Sep. 1986 

(NASA-CP-2465; E-3386; NAS 1.552465) Avail: NTlS HC 

AlOIMF A01 CSCL 22A 

MANAGEMENT, WEIGHTLESSNESS 

AEROSPACE ENVIRONMENTS, CONFERENCES, FLUID 

31 

ENGINEERING (GENERAL) 

Includes vacuum technology; control engineering; display 

engineering; cryogenics; and fire prevention. 

N87-22870'# 

Marshall Space Flight Center, Huntsville, Ala. 

TERED MEASUREMENTS 

MICHAEL E. POLITES Jun. 1987 23. p 

(NASA-TP-2732; NAS 1.60:2732) Avail: NTlS HC A02IMF A01 

CSCL 13H 

SYSTEMS, STATE VECTORS, SYSTEMS ENGINEERING 

National Aeronautics and Space Administration. 

MODELING DIGITAL CONTROL SYSTEMS WITH MA-PREFILCONTROL SYSTEMS DESIGN, DIGITAL FILTERS, DIGITAL 

N87-24585'# National Aeronautics and Space Administration. 

Marshall Space Flight Center, Huntsville, Ala. 

A NEW APPROACH TO STATE ESTIMATION IN 

DETERMINISTIC DIGITAL CONTROL SYSTEMS 

MICHAEL E. POLITES Jul. 1987 16 p 

(NASA-TP-2745; NAS 1.60:2745) Avail: NTlS HC AO2IMF A01 

CSCL 09B 

ESTIMATION 

CONTROL SYSTEMS DESIGN, DIGITAL SYSTEMS, STATE 

N87-27067'# National Aeronautics and Space Administration. 

Marshall Space Flight Center, Huntsville, Ala. 

EXACT STATE RECONSTRUCTION IN DETERMINISTIC 

DIGITAL CONTROL SYSTEMS 

MICHAEL E. POLITES Aug. 1987 19 p 

(NASA-TP-2757; NAS 1.60:2757) 

CSCL 13H 

VECTORS 

Avail: NTlS HC AO2IMF A01 

DIGITAL COMMAND SYSTEMS, STATE ESTIMATION, STATE 

32 

COMMUNICATIONS AND RADAR 

Includes radar; land and global communications; communications 

theory; and optical communications. 

N87-11916'# National Aeronautics and Space Administration. 

Wallops Flight Center, Wallops Island. Va. 

PULSE CODE MODULATION (PCM) ENCODER HANDBOOK FOR 

S. F. CURRIER and W. R. POWELL Washington, D.C. Aug. 

1986 139 p 

(NASA-RP-1171; NAS 1.61:1171) Avail: NTlS HC A07/MF A01 

CSCL 17B 

The hardware and software characteristics of a time division 

multiplex system are described. The system is used to sample 

analog and digital data. The data is merged with synchronization 

information to produce a serial pulse coded modulation (PCM) bit 

stream. Information presented herein is required by users to design 

compatible interfaces and assure effective utilization of this encoder 

system. GSFC/Wallops Flight Facility has flown approximately 50 

of these systems through 1984 on sounding rockets with no inflight 

failures. Aydin Vector manufactures all of the components for these 

systems. Author 

AYDIN VECTOR MMP-600 SERIES SYSTEM 

N87-12718'# National Aeronautics and Space Administration. 

Wallops Flight Center, Wallops Island, Va. 

PULSE CODE MODULATION (PCM) DATA STORAGE AND 

ANALYSIS USING A MICROCOMPUTER 

D. E. MASSEY Aug. 1986 8 p 

(NASA-TP-2629; REPT-822.3; NAS 1.60:2629) Avail: NTlS HC 

A02IMF A01 CSCL 178 

MICROCOMPUTERS, PULSE CODE MODULATION 

DATA PROCESSING, DATA REDUCTION, DATA STORAGE, 

N87-17971'# 

Lewis Research Center, Cleveland, Ohio. 

TRAVELING WAVE TUBES FOR GROUND-TERMINAL 

APPLICATIONS 

KURT A. SHALKHAUSER and GENE FUJIKAWA Oct. 1986 

16 P 

(NASA-TP-2635; E-2996; NAS 1.60:2635) Avail: NTlS HC 

AO2IMF A01 CSCL 178 

EFFICIENCY, TRAVELING WAVE TUBES 

National Aeronautics and Space Administration. 

BIT-ERROR-RATE TESTING OF HIGH-POWER 30-GHZ 

BIT ERROR RATE, PERFORMANCE TESTS, TRANSMISSION 

N87-20448'# 

Lewis Research Center, Cleveland, Ohio. 

SATELLITE COMMUNICATION SYSTEMS 

MARY JO WINDMILLER Mar. 1987 13 p 

(NASA-TP-2699; E-3322; NAS 1.60:2699) Avail: NTlS HC 

A02lMF A01 CSCL 178 

SATELLITE COMMUNICATION, SYSTEMS ANALYSIS 

National Aeronautics and Space Administration. 

UNIQUE BIT-ERROR-RATE MEASUREMENT SYSTEM FOR 

BIT ERROR RATE, COMMUNICATION NETWORKS, 

N87-24590'# National Aeronautics and Space Administration. 

Wallops Flight Center, Wallops Island, Va. 

A SYNCHRONOUS DATA ANALYZER FOR THE MINIMUM 

DELAY DATA FORMAT (MDDF) AND LAUNCH TRAJECTORY 

ACQUISITION SYSTEM (LTAS) 

ANDREW J. GREEN Jul. 1987 10 p 

(NASA-TP-2743; REPT-822.1; NAS 1.60:2743) Avail: NTlS HC 

AO2IMF A01 CSCL 178 

TRAJECTORY ANALYSIS 

DATA REDUCTION, LAUNCHING, SAMPLING, SYNCHRONISM, 

13 
33 ELECTRONICS AND ELECTRICAL ENGINEERING 

33 N87-22923*# 

Lewis Research Center, Cleveland, Ohio. 

National Aeronautics and Space Administration. 

REVISED NASA AXIALLY SYMMETRIC RING MODEL FOR 

COUPLED-CAVITY TRAVELING-WAVE TUBES ELECTRONICS AND ELECTRICAL ENGINEERING ~~~~ 

JEFFREY D. WILSON Jan. 1987 17 p 

(NASA-TP-2675; E-3220; NAS 1.60:2675) 

A02lMF A01 CSCL 09A 

MODELS, RINGS, TRAVELING WAVE TUBES 

Avail: NTlS HC Includes test equipment and maintainability; components, e.g., 

tunnel diodes and transistors; microminiaturization; and integrated 

circuitry. AXISYMMETRIC BODIES, CAVITIES, COUPLED MODES, 

N87-11072'# National Aeronautics and Space Administration. 

Goddard Space Flight Center, Greenbelt, Md. 

THE 1985 GODDARD SPACE FLIGHT CENTER BATTERY 

WORKSHOP 

G. MORROW, ed. Sep. 1986 427 p Workshop held in 

Greenbelt, Md., 19-21 Nov. 1985 

(NASA-CP-2434; REPT-86B0366; NAS 1 552434) Avail: NTlS 

HC A19/MF A01 CSCL 1OC 

CONFERENCES, ENERGY STORAGE, LITHIUM SULFUR 

BATERIES, NICKEL CADMIUM BATTERIES, NICKEL 

HYDROGEN BATTERIES 

N87-17990*# National Aeronautics and Space Administration. 

Lewis Research Center, Cleveland, Ohio. 

PERFORMANCE OF TEXTURED CARBON ON COPPER 

ELECTRODE MULTISTAGE DEPRESSED COLLECTORS WITH 

PETER RAMINS and ARTHUR N. CURREN Nov. 1986 12 p 

(NASA-TP-2665; E-3143; NAS 1.60:2665) 

AO2IMF A01 CSCL 09A 

ELECTRON EMISSION, TRAVELING WAVE TUBES 

MEDIUM-POWER TRAVELING WAVE TUBES 

Avail: NTlS HC 

ACCUMULATORS, CURRENT DENSITY, ELECTRODES, 

N87-17991'# National Aeronautics and Space Administration. 

Lewis Research Center, Cleveland, Ohio. 

CALCULATION OF SECONDARY ELECTRON TRAJECTORIES 

IN MULTISTAGE DEPRESSED COLLECTORS FOR MICROWAVE 

AMPLIFIERS 

DALE A. FORCE Nov. 1986 7 p 

(NASA-TP-2664; E-3196; NAS 1.60:2664) Avail: NTlS HC 

AO2IMF A01 CSCL 09A 

ACCUMULATORS, ELECTRON EMISSION, MICROWAVE 

AMPLIFIERS, PARTICLE TRAJECTORIES, TRAVELING WAVE 

TUBES 

N87-20474'# National Aeronautics and Space Administration. 

Lewis Research Center, Cleveland, Ohio. 

DESIGN, FABRICATION AND PERFORMANCE OF SMALL 

GRAPHITE ELECTRODE, MULTISTAGE DEPRESSED COLLECTORS WITH 200-W, CW, 8-TO 18-GHZTRAVELING-WAVETUBES 

BEN T. EBIHARA and PETER RAMINS Feb. 1987 22 p 

(NASA-TP-2693; E-3099; NAS 1.60:2693) Avail: NTlS HC 

AO2/MF A01 CSCL 09A 

ACCUMULATORS, DESIGN ANALYSIS, ELECTRODES, 

FABRICATION, PYROLYTIC GRAPHITE, TRAVELING WAVE 

TUBES 

N87-21239'# National Aeronautics and Space Administration. 

Lewis Research Center, Cleveland, Ohio. 

TRAVELING-WAVE-TUBE EFFICIENCY IMPROVEMENT BY A 

LOWCOST TECHNIQUE FOR DEPOSITION OF CARBON ON 

MULTISTAGE DEPRESSED COLLECTOR 

BEN T. EBIHARA, PETER RAMINS, and SHELLY PEET May 1987 14 p 

(NASA-TP-2719; E-3416; NAS 1.60:2719) Avail: NTlS HC 

AO2IMF A01 CSCL 09A 

FILMS, TRAVELING WAVE TUBES 

CARBON, COPPER, DEPOSITION, ELECTRODES, THIN 

N87-25532*# National Aeronautics and Space Administration. 

Lewis Research Center, Cleveland, Ohio. 

ANALYTICAL AND EXPERIMENTAL PERFORMANCE OF A 

DUAL-MODE TRAVELING WAVE TUBE AND MULTISTAGE 

DEPRESSED COLLECTOR 

PETER RAMINS, DALE A. FORCE, and HENRY G. KOSMAHL 

Aug. 1987 29 p 

(NASA-TP-2752; E-3470; NAS 1.60:2752) Avail: NTlS HC 

AO3IMF A01 CSCL 09A 

TUBES 

ACCUMULATORS, ELECTRON BEAMS, TRAVELING WAVE 

34 

FLUID MECHANICS AND HEAT TRANSFER 

Includes boundary layers; hydrodynamics; fluidics; mass transfer; 

and ablation cooling. 

N87-11963*# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

ON THE MAXWELLIAN DISTRIBUTION, SYMMETRIC FORM, 

AND ENTROPY CONSERVATION FOR THE EULER 

EQUATIONS 

S. M. DESHPANDE Nov. 1986 30 p 

(NASA-TP-2583; L-16036; NAS 1.60:2583) Avail: NTlS HC 

A03/MF A01 CSCL 20D 

BOLTZMANN DENSITY FUNCTION 

ENTROPY, EULER EQUATIONS OF MOTION, MAXWELLN87-13664'# 

Langley Research Center, Hampton, Va. 

ANCES ON A FLAT PLATE AT A MACH NUMBER OF 6.5. 

C. E. GLASS and L. R. HUNT Dec. 1986 61 p 

(NASA-TP-2631; L-16160; NAS 1.60:2631) Avail: NTIS HC 

A04IMF A01 CSCL 20D 

NAR BOUNDARY LAYER, PREDICTION ANALYSIS TECHNIQUES, 

LENT BOUNDARY LAYER 

National Aeronautics and Space Administration. 

AEROTHERMAL TESTS OF SPHERICAL DOME PROTUBERAEROTHERMODYNAMICS, HYPERSONIC VEHICLES, LAMIPROTUBERANCES, THERMAL PROTECTION, TILES, TURBUN87-17000'# National Aeronautics and Space Administration. 

Marshall Space Flight Center, Huntsville, Ala. 

SPACE SHUTTLE MAIN ENGINE HIGH PRESSURE FUEL PUMP 

AFT PLATFORM SEAL CAVITY FLOW ANALYSIS 

S. A. LOWRY and L. W. KEETON (CHAM of North America, Inc., 

Huntsville, Ala.) Jan. 1987 134 p 

(NASA-TP-2685; NAS 1.60:2685) Avail: NTlS HC A07/MF A01 

CSCL 20D 

CAVITIES, FUEL PUMPS, HIGH PRESSURE, SEALS 

(STOPPERS), SPACE SHUTTLE MAIN ENGINE, TURBINE 

PUMPS 

14 
34 FLUID MECHANICS AND HEAT TRANSFER 

N87-18034'# National Aeronautics and Space Administration. 

Lewis Research Center, Cleveland, Ohio. 

JET MODEL FOR SLOT FILM COOLING WITH EFFECT OF 

FREE-STREAM AND COOLANT TURBULENCE 

FREDERICK F. SIMON Oct. 1986 21 p 

(NASA-TP-2655; E-2961 ; NAS 1.60:2655) Avail: NTlS HC 

A02/MF A01 CSCL 20D 

NUMERICAL ANALYSIS, TURBULENCE EFFECTS, WALL JETS 

FILM COOLING, FLOW VELOCITY, JET ENGINES, 

N87-18035'# 

Lewis Research Center, Cleveland, Ohio. 

VELOCITY PROFILES IN LAMINAR DIFFUSION FLAMES 

VALERIE J. LYONS and JANICE M. MARGLE (Pennsylvania State 

Univ., Abington) May 1986 13 p Presented at the Combustion 

Inst. Meeting, Cleveland, Ohio, 5-6 May 1986 

(NASA-TP-2596; E-2879; NAS 1.60:2596) Avail: NTlS HC 

A02/MF A01 CSCL 20D 

CYCLOHEXANE, DIFFUSION FLAMES, ETHYL ALCOHOL, 

HEPTANES, LAMINAR FLOW, OCTANES, TEMPERATURE 

PROFILES, VELOCITY MEASUREMENT 

National Aeronautics and Space Administration. 

N87-18782'# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

AEROTHERMAL EVALUATION OF A SPHERICALLY BLUNTED 

BODY WITH A TRAPEZOIDAL CROSS SECTION IN THE 

CINDY W. ALBERTSON Apr. 1987 83 p 

(NASA-TP-2641; L-16096; NAS 1.60:2641) Avail: NTlS HC 

AO5/MF A01 CSCL 20D 

BOUNDARY LAYERS, FLOW DISTRIBUTION, HEAT 

TRANSFER, PREDICTIONS, PRESSURE MEASUREMENT, 

THERMAL PROTECTION 

LANGLEY 8-FOOT HIGH-TEMPERATURE TUNNEL 

N87-18783'# 

Langley Research Center, Hampton, Va. 

METHOD FOR INVISCID COMPRESSIBLE FLOWS 

SURESH M. DESHPANDE Dec. 1986 42 p 

(NASA-TP-2613; L-16050; NAS 1.60:2613) 

AO3/MF A01 CSCL 20D 

BOLTZMANN TRANSPORT EQUATION, EULER EQUATIONS 

OF MOTION, KINETIC THEORY, NUMERICAL ANALYSIS, SHOCK 

WAVE PROPAGATION 

National Aeronautics and Space Administration. 

A SECOND-ORDER ACCURATE KINETIC-THEORY-BASED 

Avail: NTlS HC 

N87-22103'# National Aeronautics and Space Administration. 

Marshall Space Flight Center, Huntsville, Ala. 

SPACELAB 3 MISSION SCIENCE REVIEW 

GEORGE H. FICHTL, ed., JOHN S. THEON, ed. (National 

Aeronautics and Space Administration, Washington, D.C.), 

CHARLES K. HILL, ed., and OTHA H. VAUGHAN, ed. Feb. 

1987 98 p Symposium held in Huntsville, Ala., 4 Dec. 1985 

(NASA-CP-2429 M-547; NAS 1.552429) Avail: NTlS HC 

A05/MF A01 CSCL 22A 

AEROSPACE ENVIRONMENTS, POSTFLIGHT ANALYSIS, 

REDUCED GRAVITY, SPACE COMMERCIALIZATION, SPACE 

SHUTTLES, SPACEBORNE EXPERIMENTS. SPACELAB 

N87-23921'# 

Lewis Research Center, Cleveland, Ohio. 

TURBOMACHINES 

ROBERT C. HENDRICKS Jun. 1987 75 p 

(NASA-TP-1848; E-3186 NAS 1.601848) Avail: NTlS HC 

A04/MF A01 CSCL 20D 

ENGINE, STATIC TESTS, TURBOMACHINERY 

National Aeronautics and Space Administration. 

THREE-STEP LABYRINTH SEAL FOR HIGH-PERFORMANCE 

FUEL PUMPS, LABYRINTH SEALS, SPACE SHUlTLE MAIN 

N87-23936'# 

Lewis Research Center, Cleveland, Ohio. 

TURBOMACHINES 

ROBERT C. HENDRICKS Jun. 1987 76 p 

(NASA-TP-1850; E-31 84; NAS 1.60:1850) Avail: NTlS HC 

A05/MF A01 CSCL 20D 

CYLINDRICAL BODIES, FUEL PUMPS, SEALS (STOPPERS), 

SPACE SHUTTLE MAIN ENGINE, TURBINE PUMPS, 

TURBOMACHINERY 

National Aeronautics and Space Administration. 

STRAIGHT CYLINDRICAL SEAL FOR HIGH-PERFORMANCE 

N87-24639*# 

Lewis Research Center, Cleveland, Ohio. 

TURBOMACHINES 

ROBERT C. HENDRICKS Jun. 1987 79 p 

(NASA-TP-1849; E-31 85; NAS 1.60:1849) Avail: NTlS HC 

A05/MF A01 CSCL 200 

SEALS, SPACE SHUTTLE MAIN ENGINE, TURBINE PUMPS 

National Aeronautics and Space Administration. 

THREE-STEP CYLINDRICAL SEAL FOR HIGH-PERFORMANCE 

DYNAMIC STABILITY, FUEL PUMPS, LEAKAGE, PUMP 

N87-24672'# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

MULTISCALE TURBULENCE EFFECTS IN SUPERSONIC JETS 

EXHAUSTING INTO STILL AIR 

KHALED S. ABDOL-HAMID (Analytical Services and Materials, Inc., 

Hampton, Va.) and RICHARD G. WILMOTH Jul. 1987 38 p 

(NASA-TP-2707; L-16258; NAS 1.60:2707) Avail: NTlS HC 

A03/MF A01 CSCL 200 

AIRCRAFT, TURBULENCE 

JET EXHAUST, NAVIER-STOKES EQUATION, SUPERSONIC 

N87-26309'# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

SIMPLIFIED CURVE FITS FOR THE THERMODYNAMIC 

PROPERTIES OF EQUILIBRIUM AIR 

S. SRINIVASAN, J. C. TANNEHILL (Iowa State Univ. of Science 

and Technology, Ames.), and K. J. WEILMUENSTER Aug. 1987 

(NASA-RP-1181; L-16276; NAS 1.61:1181) Avail: NTlS HC 

A03/MF A01 CSCL 20D 

New, improved curve fits for the thermodynamic properties of 

equilibrium air have been developed. The curve fits are for pressure, 

speed of sound, temperature, entropy, enthalpy, density, and 

internal energy. These curve fits can be readily incorporated into 

new or existing computational fluid dynamics codes if real gas 

effects are desired. The curve fits are constructed from Grabau-type 

transition functions to model the thermodynamic surfaces in a 

piecewise manner. The accuracies and continuity of these curve 

fits are substantially improved over those of previous curve fits. 

These improvements are due to the incorporation of a small number 

of additional terms in the approximating polynomials and careful 

choices of the transition functions. The ranges of validity of the 

new curve fits are temperatures up to 25 000 K and densities 

from 10 to the -7 to 10 to the 3d power amagats. Author 

48 P 

(NAG 1 -3 1 3) 

N87-27161'# National Aeronautics and Space Administration. 

Lewis Research Center, Cleveland, Ohio. 

APPLICATION OF TURBULENCE MODELING TO PREDICT 

SURFACE HEAT TRANSFER IN STAGNATION FLOW REGION 

OF CIRCULAR CYLINDER 

CHI R. WANG and FREDERICK C. YEH Sep. 1987 25 p 

(NASA-TP-2758; E-341 8; NAS 1.60:2758) Avail: NTlS HC 

A02/MF A01 CSCL 20D 

STAGNATION FLOW, SURFACE PROPERTIES, TURBULENCE 

CIRCULAR CYLINDERS, HEAT TRANSFER, MODELS, 

15 
34 FLUID MECHANICS AND HEAT TRANSFER 

N87-29778'# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

DESCRIPTION AND CALIBRATION OF THE LANGLEY 

HYPERSONIC CF4 TUNNEL A FACILITY FOR SIMULATING 

LOW GAMMA FLOW AS OCCURS FOR A REAL GAS 

RAYMOND E. MIDDEN and CHARLES G. MILLER, 111 Mar. 

1985 78 p 

(NASA-TP-2384; L-15798; NAS 1.60:2384) 

A05/MF A01 CSCL 20D 

CALIBRATING, CARBON TETRAFLUORIDE, HYPERSONIC 

WIND TUNNELS, MACH NUMBER, REAL GASES, TEST 

FACILITIES 

Avail: NTlS HC 

N87-29795'# 

Ames Research Center, Moffett Field, Calif. 

SPACE SHUlTLE ORBITER 

WILLIAM L. KO, ROBERT D. QUINN, and LESLIE GONG 

1986 59 p 

(NASA-TP-2657; H-1236; NAS 1.60:2657) Avail: NTlS HC 

A04/MF A01 CSCL 20D 

AERODYNAMIC HEATING, FINITE ELEMENT METHOD, HEAT 

TRANSFER COEFFICIENTS, REENTRY SHIELDING, SPACE 

SHUTTLE ORBITERS, THERMAL ANALYSIS 

National Aeronautics and Space Administration. 

FINITE-ELEMENT REENTRY HEAT-TRANSFER ANALYSIS OF 

Dec. 

35 

INSTRUMENTATION AND PHOTOGRAPHY 

Includes remote sensors; measuring instruments and gages; 

detectors; cameras and photographic supplies; and holography. 

N87-10263'# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

THIRTEENTH INTERNATIONAL LASER RADAR CONFERENCE 

Aug. 1986 335 p Conference held in Toronto, Ontario, 11-15 

Aug. 1986; sponsored by NASA, Washington, D.C., Atmospheric 

Environment Service, and York Univ. 

(NASA-CP-2431; L-16201; NAS 1.552431) 

A15/MF A01 CSCL 20E 

ROLOGICAL PARAMETERS, MIDDLE ATMOSPHERE, OPTICAL 

RADAR, RADAR EQUIPMENT 

Avail: NTlS HC 

CONFERENCES, LASER APPLICATIONS, LASERS, METEON87-13731'# 

Lewis Research Center, Cleveland, Ohio. 

CINEMATOGRAPHY IN A FLUTTER CASCADE 

A. J. DECKER Jul. 1986 33 p 

(NASA-TP-2593; E-2937; NAS 1.60:2593) 

AOWMF A01 CSCL 14E 

CINEMATOGRAPHY, FLOW VISUALIZATION, HOLOGRAPHIC 

INTERFEROMETRY, HOLOGRAPHY, LASER OUTPUTS, THREE 

DIMENSIONAL FLOW 

National Aeronautics and Space Administration. 

EVALUATION OF DIFFUSE-ILLUMINATION HOLOGRAPHIC 

Avail: NTIS HC 

N87-20514'# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

A SIMPLIFIED METHOD FOR DETERMINING HEAT OF 

COMBUSTION OF NATURAL GAS 

JAG J. SINGH, HOSHANG CHEGlNl (Old Dominion Univ., Norfolk, 

Va.), and GERALD H. MALL (Computer Sciences Corp., Hampton, 

Va.) Apr. 1987 15 p 

(NASA-TP-2682; L-16261; NAS 1.60:2682) 

AO2/MF A01 CSCL 148 

OXYGEN SUPPLY EQUIPMENT 

Avail: NTlS HC 

GAS DETECTORS, HEAT OF COMBUSTION, NATURAL GAS, 

36 

LASERS AND MASERS 

Includes parametric amplifiers. 

N87-20522'# 

Langley Research Center, Hampton, Va. 

TECHNOLOGY 

CARMEN E. BATTEN, ed., IRVlN M. MILLER, ed., GEORGE M. 

WOOD, JR., ed., and DAVID V. WILLETTS, ed. (Royal Signals 

and Radar Establishment, Malvern. England.) Apr. 1987 279 p 

Workshop held in Hampton, Va., 10-12 Jun. 1986 

(NASA-CP-2456; L-16271; NAS 1.552456) Avail: NTlS HC 

A1 3/MF A01 CSCL 20E 

STABILITY, RESEARCH MANAGEMENT 

National Aeronautics and Space Administration. 

CLOSED-CYCLE, FREQUENCY-STABLE C02 LASER 

CARBON DIOXIDE LASERS, CLOSED CYCLES, FREQUENCY 

N87-27994'# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

FREQUENCY DOMAIN LASER VELOCIMETER SIGNAL 

PROCESSOR: A NEW SIGNAL PROCESSING SCHEME 

JAMES F. MEYERS and JAMES I. CLEMMONS, JR. Sep. 1987 

38 P 

(NASA-TP-2735; L-16209; NAS 1.60:2735) 

AOWMF A01 CSCL 20E 

ERS, SIGNAL PROCESSING 

Avail: NTlS HC 

DOMAINS, FREQUENCIES, LASER DOPPLER VELOCIMET37 

MECHANICAL ENGINEERING 

Includes auxiliary systems (nonpower); machine elements and 

processes; and mechanical equipment. 

N87-10391'# 

Lewis Research Center, Cleveland, Ohio. 

TESTING OF UH-GOA HELICOPTER TRANSMISSION IN NASA 

LEWIS 2240-KW (3000-HP) FACILITY 

A. M. MITCHELL, F. B. OSWALD, and H. H. COE 

30 P 

(NASA-TP-2626; E-2941; NAS 1.60:2626) Avail: NTlS HC 

AO3/MF A01 CSCL 131 

VIBRATION MEASUREMENT 

N87-18095'# National Aeronautics and Space Administration. 

Lewis Research Center, Cleveland, Ohio. 

PREDICTED EFFECT OF DYNAMIC LOAD ON PllTlNG FATIGUE 

DAVID G. LEWlCKl Jun. 1986 19 p 

AVSCOM-TR-86-C-21) Avail: NTlS HC AO2/MF A01 CSCL 131 

APPLICATIONS PROGRAMS (COMPUTERS), DYNAMIC 

LOADS, FATIGUE (MATERIALS), GEARS, LIFE (DURABILITY), 

PITTING 

National Aeronautics and Space Administration. 

Aug. 1986 

HELICOPTERS, TRANSMISSIONS (MACHINE ELEMENTS), 

LIFE FOR LOW-CONTACT-RATIO SPUR GEARS 

(NASA-TP-2610; E-2989; NAS 1.60:2610; AD-A1 70906; 

N87-18821'# 

Washington, D.C. 

TETHER DYNAMICS SIMULATION 

Feb. 1987 338 p 

1986 

(NASA-CP-2458; NAS 1.55:2458) Avail: NTlS HC A1 5/MF A01 

CSCL 228 

THERED SATELLITES, TETHERLINES 

National Aeronautics and Space Administration, 

Workshop held in Arlington, Va., 16 Sep. 

COMPUTERIZED SIMULATION, ELECTRODYNAMICS, TE16 
39 STRUCTURAL MECHANICS 

N87-20555*# 

Lewis Research Center, Cleveland, Ohio. 

VIBRATION CHARACTERISTICS OF OH-58A HELICOPTER 

MAIN ROTOR TRANSMISSION 

DAVID G. LEWlCKl and JOHN J. COY Apr. 1987 18 p 

AD-A180364) Avail: NTlS HC AOl/MF A01 CSCL 01C 

(MACHINE ELEMENTS), VIBRATION MEASUREMENT 

National Aeronautics and Space Administration. 

(NASA-TP-2705; E-3368; NAS 1.60:2705; AVSCOM-TR-86-C-42; 

HELICOPTERS, ROTOR AERODYNAMICS, TRANSMISSIONS 

N87-22199'# 

Lewis Research Center, Cleveland, Ohio. 

ROTORDYNAMIC INSTABILITY PROBLEMS IN HIGH-PERFORMANCE TURBOMACHINERY, 1986 

Jan. 1987 Workshop held in College Station, Tex., 2-4 

Jun. 1986; sponsored in cooperation with Texas A&M Univ., Army 

Research Office, and Air Force Aeropropulsion Lab. 

(NASA-CP-2443; E-3136; NAS 1.55:2443) Avail: NTlS HC 

A23/MF A01 CSCL 131 

SORS, TURBOMACHINERY 

National Aeronautics and Space Administration. 

548 p 

ROTOR AERODYNAMICS, STABILITY, TURBOCOMPRESN87-22235'# National Aeronautics and Space Administration. 

Lewis Research Center, Cleveland, Ohio. 

GEAR TOOTH STRESS MEASUREMENTS ON THE UH-GOA 

HELICOPTER TRANSMISSION 

FRED B. OSWALD Mar. 1987 17 p 

(NASA-TP-2698; E-3357; NAS 1.60:2698) Avail: NTlS HC 

AO2/MF A01 CSCL 131 

GEAR TEETH, STRESS MEASUREMENT, TRANSMISSIONS 

(MACHINE ELEMENTS), UH-GOA HELICOPTER 

30 

QUALITY ASSURANCE AND RELIABILITY 

Includes product sampling procedures and techniques; and quality 

control. 

N87-27204'# 

Langley Research Center, Hampton, Va. 

OGY 

JOSEPH S. HEYMAN, ed. Aug. 1987 143 p Conference held 

in Hampton, Va., 3-5 Jun. 1986; sponsored by NASA Langley 

Research Center, USAF, National Security Industrial Association, 

and the Aerospace Industry Association 

(NASA-CP-2472; L-16315; NAS 1.552472) Avail: NTlS HC 

A07/MF A01 CSCL 14D 

National Aeronautics and Space Administration. 

ELECTRONICS RELIABILITY AND MEASUREMENT TECHNOLCOMPONENT RELIABILITY, INSPECTION, MICROELECTRONICS, NONDESTRUCTIVETESTS, QUALITY CONTROL, RELIABILITY ENGINEERING 

N87-28025'# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

A TECHNIQUE FOR EVALUATING THE APPLICATION OF THE 

DANIEL L. PALUMBO and GEORGE B. FlNELLl Sep. 1987 

PIN-LEVEL STUCK-AT FAULT MODEL TO VLSl CIRCUITS 

45 D 

(NAkA-TP-2738; L-16269; NAS 1.60:2738) 

AOWMF A01 CSCL 14D 

COMPUTERS, ERROR ANALYSIS, EVALUATION, FAULT 

TOLERANCE, INTEGRATED CIRCUITS, VERY LARGE SCALE 

INTEGRATION 

Avail: NTlS HC 

STRUCTURAL MECHANICS 

Includes structural element design and weight analysis; fatigue; 

and thermal stress. 

N87-11180'# National Aeronautics and Space Administration. 

Lewis Research Center, Cleveland, Ohio. 

TURBINE ENGINE HOT SECTION TECHNOLOGY, 1984 

Oct. 1984 400 p Conference held in Cleveland, Ohio, 23-24 

Oct. 1984 

(NASA-CP-2339; E-2267; NAS 1.55:2339) 

A17/MF A01 CSCL 20K 

AIRCRAFT ENGINES, AIRFOILS, CONFERENCES, LIFE 

(DURABILITY) LININGS, MATHEMATICAL MODELS, PREDICTION 

ANALYSIS TECHNIQUES, ROTOR BLADES (TURBOMACHINERY), 

TURBINE ENGINES 

Avail: NTlS HC 

N87-12921'# National Aeronautics and Space Administration. 

Marshall Space Flight Center, Huntsville, Ala. 

EFFECTS OF VARIABLES UPON PYROTECHNICALLY INDUCED 

SHOCK RESPONSE SPECTRA 

J. L. SMITH May 1986 61 p 

(NASA-TP-2603; NAS 1.60:2603) Avail: NTlS HC A04/MF A01 

CSCL 20K 

VARIABILITY 

PYROTECHNICS, SHOCK LOADS, SHOCK SPECTRA, 

N87-13789'# 

Langley Research Center, Hampton, Va. 

National Aeronautics and Space Administration. 

EFFECTS OF WINGLET ON TRANSONIC FLUTTER CHARACTERISTICS OF A CANTILEVERED TWIN-ENGINE-TRANSPORT 

WING MODEL 

C. L. RUHLIN, K. G. BHATIA (Boeing Commercial Airplane Co., 

Seattle, Wash.), and K. S. NAGARAJA Dec. 1986 77 p 

(NASA-TP-2627; L-16095; NAS 1.60:2627) Avail: NTlS HC 

A05/MF A01 CSCL 20K 

AERODYNAMIC CONFIGURATIONS, FLUTTER, PREDICTION 

ANALYSIS TECHNIQUES, TRANSONIC FLOW, WIND TUNNEL 

TESTS, WINGLETS, WINGS 

N87-16321'# National Aeronautics and Space Administration. 

Lewis Research Center, Cleveland, Ohio. 

THE 20TH AEROSPACE MECHANICS SYMPOSIUM 

May 1986 316 p Symposium held in Cleveland, Ohio, 7-9 May 

1986; sponsored by NASA, the California Inst. of Tech. and 

LMSC 

(NASA-CP-2423-REV; E-2904; NAS 1.55:2423-REV) Avail: NTlS 

HC A14/MF A01 CSCL 20K 

ACTUATORS, CONFERENCES, FLEXIBLE SPACECRAFT, 

IPULATORS, SPACE STATIONS, SPACECRAFT INSTRUMENTS, 

SPUTTERING, TRIBOLOGY 

HYDRAULIC EQUIPMENT, JOINTS (JUNCTIONS), MANN87-18855'# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

SENSITIVITY ANALYSIS IN ENGINEERING 

HOWARD M. ADELMAN, comp. and RAPHAEL T. HAFTKA, comp. 

(Virginia Polytechnic Inst. and State Univ., Blacksburg) Feb. 

1987 369 p Symposium held in Hampton, Va., 25-26 Sep. 

1986 

(NASA-CP-2457; L-16278; NAS 1.55:2457) Avail: NTlS HC 

A16/MF A01 CSCL 20K 

RESPONSE, OPTIMIZATION, SENSITIVITY 

DYNAMIC STRUCTURAL ANALYSIS, EIGENVALUES, MODAL 

17 
39 STRUCTURAL MECHANICS 

N87-20566"# 

Lewis Research Center, Cleveland, Ohio. 

BLADES 

GERALD A. CAREK Apr. 1987 9 p 

(NASA-TP-2711; E-3430; NAS 1.60:2711) Avail: NTlS HC 

AOl/MF A01 CSCL 20K 

TITANIUM ALLOYS, VANADIUM 

National Aeronautics and Space Administration. 

SHOT PEENING FOR TI-6AL-4V ALLOY COMPRESSOR 

ALUMINUM, COMPRESSOR BLADES, SHOT PEENING, 

N87-20567'# National Aeronautics and Space Administration. 

Langley Research Center, Hampton. Va. 

MODELING OF JOINTS FOR THE DYNAMIC ANALYSIS OF 

TRUSS STRUCTURES 

W. KEITH BELVIN May 1987 43 p 

(NASA-TP-2661; L-16163; NAS 1.60:2661) Avail: NTlS HC 

AOS/MF A01 CSCL 20K 

LARGE SPACE STRUCTURES, MODELS, TRUSSES 

DYNAMIC STRUCTURAL ANALYSIS, JOINTS (JUNCTIONS), 

N87-20568'# National Aeronautics and Space Administration. 

Marshall Space Flight Center, Huntsville, Ala. 

SPACE STATION STRUCTURES AND DYNAMICS TEST 

PROGRAM 

CARLETON J. MOORE, JOHN S. TOWNSEND, and EDWARD W. 

IVEY Mar. 1987 47 p 

(NASA-TP-2710; NAS 1.60:2710) Avail: NTlS HC A03/MF A01 

CSCL 20K 

DYNAMIC STRUCTURAL ANALYSIS, DYNAMIC TESTS, 

LARGE SPACE STRUCTURES, SPACE STATION STRUCTURES, 

SPACE STATIONS, SYSTEMS ANALYSIS 

N87-27231'# 

Center, Athens, Ga. 

FIFTEENTH NASTRAN USERS COLLOQUIUM 

Aug. 1987 312 p 

May 1987 

(NASA-CP-2481; NAS 1.55:2481) Avail: NTlS HC A14/MF A01; 

also available from COSMIC, Athens. Ga. 30602 CSCL 20K 

COMPUTER AIDED DESIGN, COMPUTER TECHNIQUES, 

CONFERENCES, FINITE ELEMENT METHOD, NASTRAN, 

STRUCTURAL ANALYSIS, STRUCTURAL VIBRATION 

Computer Software Management and Information 

Colloquium held in Kansas City, Mo., 4-8 

(NASW-3247) 

N87-29858'# National Aeronautics and Space Administration. 

Lyndon B. Johnson Space Center, Houston, Tex. 

THE 21ST AEROSPACE MECHANISMS SYMPOSIUM 

May 1987 Symposium held in Houston, Tex., 29 Apr. - 1 May 1987; sponsored by NASA, California Inst. of Tech., and 

LMSC 

A16/MF A01 CSCL 20K 

ACTUATORS, DEPLOYMENT, LARGE SPACE STRUCTURES, 

MANIPULATORS, ROBOTICS, SPACE ERECTABLE STRUCTURES 

356 p 

(NASA-CP-2470; S-560; NAS 1.55~2470) Avail: NTlS HC 

42 

GEOSCIENCES (GENERAL) 

N87-18139'# National Aeronautics and Space Administration. 

Goddard Space Flight Center, Greenbelt, Md. 

GEOMORPHOLOGY FROM SPACE: A GLOBAL OVERVIEW OF 

REGIONAL LANDFORMS 

NICHOLAS M. SHORT, ed. and ROBERT W. BLAIR, JR., ed. 

(Fort Lewis A&M Coll., Durango, Colo.) 1986 737 p Original 

contains color illustrations 

(NASA-SP-486; NAS 1.21:486; LC-86-17974) Avail: SOD HC 

$41.00 as 033-000-00994-1; NTlS MF E03 CSCL 08E 

This book, Geomorphology from Space: A Global Overview of 

Regional Landforms, was published by NASA STlF as a successor 

to the two earlier works on the same subject: Mission to Earth: 

LANDSAT views the Earth, and ERTS-1: A New Window on Our 

Planet. The purpose of the book is threefold: first, to serve as a 

stimulant in rekindling interest in descriptive geomorphology and 

landforms analysis at the regional scale; second, to introduce the 

community of geologists, geographers, and others who analyze 

the Earth's surficial forms to the practical value of space-acquired 

remotely sensed data in carrying out their research and 

applications; and third, to foster more scientific collaboration 

between geomorphologists who are studying the Earth's landforms 

and astrogeologists who analyze landforms on other planets and 

moons in the solar system, thereby strengthening the growing 

field of comparative planetology. F.M.R. 

43 

EARTH RESOURCES AND REMOTE SENSING 

Includes remote sensing of earth resources by aircraft and 

spacecraft; photogrammetry; and aerial photography. 

N87-22281*# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

SURFACE BIDIRECTIONAL REFLECTANCE PROPERTIES OF 

TWO SOUTHWESTERN ARIZONA DESERTS FOR 

WAVELENGTHS BETWEEN 0.4 AND 2.2 MICROMETERS 

CHARLES H. WHITLOCK, G. CARLTON PURGOLD, and STUART 

R. LECROY (PRC Kentron, Inc., Hampton. Va.) May 1987 

48 P 

(NASA-TP-2643; L-16159; NAS 1.60:2643) Avail: NTlS HC 

AO3/MF A01 CSCL 20F 

DIRECTIVITY, SOLAR POSITION, ZENITH 

ALBEDO, BIDIRECTIONAL REFLECTANCE, DESERTS, 

N87-27315. National Aeronautics and Space Administration, 

Washington, D.C. 

EARTH RESOURCES A CONTINUING BIBLIOGRAPHY WITH 

INDEXES (ISSUE 54) 

Aug. 1987 164 p 

(NASA-SP-7041(54); NAS 1.21:7041(54)) Avail: NTlS HC A08 

CSCL 058 

This bibliography lists 562 reports, articles, and other documents 

introduced into the NASA scientific and technical information 

system between April 1 and June 30, 1987. Emphasis is placed 

on the use of remote sensing and geophysical instrumentation in 

spacecraft and aircraft to survey and inventory natural resources 

and urban areas. Subject matter is grouped according to agriculture 

and forestry, environmental changes and cultural resources, 

geodesy and cartography, geology and mineral resources, 

hydrology and water management, data processing and distribution 

18 
46 GEOPHYSICS 

systems, instrumentation and sensors, and economic analysis. 

Author 

46 

GEOPHYSICS 

N87-28162'# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

EFFECTS OF AEROSOLS AND SURFACE SHADOWING ON 

BIDIRECTIONAL REFLECTANCE MEASUREMENTS OF 

DESERTS 

DAVID E. BOWKER and RICHARD E. DAVIS Sep. 1987 26 p 

(NASA-TP-2756; L-16327; NAS 1.60:2756) Avail: NTlS HC 

AO31MF A01 CSCL 04A 

AEROSOLS, BIDIRECTIONAL REFLECTANCE, DESERTS, 

DUST, REMOTE SENSING, SHADOWS, SURFACE PROPERTIES 

N87-28955"# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

ATLAS OF ABSORPTION LINES FROM 0 TO 17900 CY 

J. H. PARK, L. S. ROTHMAN, C. P. RINSLAND, H. M. PICKETT, 

D. J. RICHARDSON, and J. S. NAMKUNG (ST Systems Corp., 

Hampton, Va.) Sep. 1987 197 p 

(NASA-RP-1188; L-16330; NAS 1.61:1188) Avail: NTlS HC 

AOSIMF A01 CSCL 04A 

Plots of logarithm (base 10) of absorption line strength versus 

wavenumber from 0 to 17900lcm(sup)-1 are shown for the 28 

atmospheric gases (H20, C02, 03, N20, CO, CH4, 02, NO, SO2, 

N02, "3, "03, OH, HF, HCI, HBr, HI, CIO, OCS, H2C0, HOCI, 

N2, HCN, CH3CI, H202, C2H2, C2H6, PH3), which appear in the 

1986 Air Force Geophysics Laboratory high-resolution transmission 

molecular absorption data base (HITRAN) compilation, and for 

O(P-3), 0-18 isotopic ozone, and H02 from the 1984 JPL 

compilation in the 0- to 200/cm(sup)-1 region, and infrared solar 

CO lines at 4500 K. Also shown are plots of logarithm (base 10) 

of approximate infrared absorption cross sections of 11 heavy 

molecules versus wavenumber. The cross-section data cover 700 

to 1800/cm(sup)-l and are included as a separate data file in the 

1986 HITRAN database. Author 

(SUP)-l 

44 

ENERGY PRODUCTION AND CONVERSION 

Includes specific energy conversion systems, e.g., fuel cells; global 

sources of energy; geophysical conversion; and windpower. 

N87-26413'# National Aeronautics and Space Administration. 

Lewis Research Center, Cleveland, Ohio. 

SPACE PHOTOVOLTAIC RESEARCH AND TECHNOLOGY 1986. 

HIGH EFFICIENCY, SPACE ENVIRONMENT, AND ARRAY 

TECHNOLOGY 

Jun. 1987 375 p Conference held in Cleveland, Ohio, 7-9 Oct. 

1986 

(NASA-CP-2475; E-3450; NAS 1.552475) Avail: NTlS HC 

A161MF A01 CSCL 1OB 

CONFERENCES, ENERGY CONVERSION EFFICIENCY, 

PHOTOVOLTAIC CONVERSION, SOLAR CELLS, SPACECRAFT 

POWER SUPPLIES 

N87-29914'# National Aeronautics and Space Administration. 

Lewis Research Center, Cleveland, Ohio. 

SPACE ELECTROCHEMICAL RESEARCH AND TECHNOLOGY 

WRT) 

Sep. 1987 364 p Conference held in Cleveland, Ohio, 14-16 

Apr. 1987 

(NASA-CP-2484; E-3506; NAS 1.552484) 

Al61MF A01 CSCL 1OC 

ELECTRIC BATTERIES, ELECTROCATALYSTS, ELECTROCHEMISTRY, MATHEMATICAL MODELS, REGENERATIVE FUEL 

CELLS 

Avail: NTlS HC 

Includes aeronomy; upper and lower atmosphere studies; 

ionospheric and magnetospheric physics; and geomagnetism. 

N87-11358*# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

AIRBORNE LIDAR MEASUREMENTS OF EL CHICHON 

STRATOSPHERIC AEROSOLS, MAY 1983 

M. P. MCCORMICK and M. T. OSBORN (SASC Technologies, 

Inc., Hampton, Va.) Oct. 1986 91 p 

(NASA-RP-1172; L-16176; NAS 1.61 :1172) Avail: NTlS HC 

AO5/MF A01 

An experimental survey flight to determine the spatial distribution 

and aerosol characteristics of the El Chichon-produced 

stratospheric aerosol was conducted in May 1983. The mission 

included several different sensors flown abroad the NASA Convair 

990 at latitudes between 72 deg. and 56 deg. S. This report 

presents the lidar data from that flight mission. Representative 

profiles of lidar backscatter ratio, plots of integrated backscattering 

function versus latitude, and contours of backscatter mixing ratio 

versus altitude and latitude are given. In addition, tables containing 

numerical values of the backscatter ratio and backscattering 

function versus altitude are supplied for each profile. By May 1983, 

material produced by the El Chichon eruptions of late March-early 

April 1982 had spread throughout the latitudes covered by this 

mission. However, the most massive portion of the material resided 

north of 33 deg. N and was concentrared below 21 km. In this 

latitude region (33 deg. N to 72 deg. N), peak backscatter ratios 

at a wavelength of 0.6943 microns varied between 3.5 and 4.5, 

and the peak integratred backscattering function was about 18 X 

10 to the -4 powerlsr. corresponding to a peak optical depth 

calculated to be approximately 0.08. This report presents the results 

of this mission in a ready-to-use format for atmospheric and climatic 

studies. Author 

N87-13022'# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

DESCRIPTION OF DATA ON THE NIMBUS 7 LlMS MAP 

ARCHIVE TAPE: OZONE AND NITRIC ACID 

E. E. REMSBERG, R. J. KURZEJA, K. V. HAGGARD, J. M. 

RUSSELL, 111, and L. L. GORDLEY Dec. 1986 73 p 

(NASA-TP-2625; L-16136; NAS 1.60:2625) Avail: NTlS HC 

A04lMF A01 CSCL 04A 

SATELLITE, NITRIC ACID, OZONE, STRATOSPHERE 

N87-15528'# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

FUTURE DIRECTIONS FOR H SUB X 0 SUB Y DETECTION 

DAVID R. CROSLEY, ed. (SRI International Corp., Menlo Park, 

Calif.) and JAMES M. HOELL, ed. Dec. 1986 67 p Workshop 

held in Menlo Park, Calif., 12-15 Aug. 1985 

(NASA-CP-2448; L-16216; NAS 1.552448) Avail: NTlS HC 

A041MF A01 CSCL 04A 

HYDROXYL RADICALS, TROPOSPHERE, WATER 

N87-17417'# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

SAGE AEROSOL MEASUREMENTS. VOLUME 3 JANUARY 1, 

1981 TO NOVEMBER 18, 1981 

M. PATRICK MCCORMICK Feb. 1987 274 p 

(NASA-RP-1173; L-16177; NAS 1.61:1173) Avail: NTlS HC 

A12lMF A01 CSCL 04A 

The Stratospheric Aerosol and Gas Experiment (SAGE) satellite 

system, launched February 18, 1979, obtained profiles of aerosol 

extinction at 1.00 micron and 0.45 micron ozone concentration, 

and nitrogen dioxide concentration. Data taken during sunset events 

are presented in the form of zonal and seasonal averages of 

INFRARED DETECTORS, KALMAN FILTERS, NIMBUS 7 

ATMOSPHERIC COMPOSITION, HYDROGEN PEROXIDE, 

19 
46 GEOPHYSICS 

aerosol extinction of 1 .OO micron and 0.45 micron, ratios of aerosol 

extinction to molecular extinction at 1.00 micron and ratios of 

aerosol extinction at 0.45 micron to aerosol extinction at 1.00 

micron. Averages for 1981 are shown in tables, and in profile and 

contour plots (as a function of altitude and latitude). In addition, 

temperature data provided by NOAA for the time and location of 

each SAGE measurement are averaged and shown in a similar 

format. The stratospheric aerosol distribution for 1981 shows 

effects of volcanically injected material from eruptions of Ulawun, 

Alaid, and Pagan. Peak values of aerosol extinction at 0.45 micron 

and 1.00 micron were 2 to 4 times higher than typical peak values 

observed during near background conditions. Stratospheric aerosol 

optical depth values at 1.00 microns increased by a factor of 

about 2 from near background levels in regions of volcanic activity. 

During the year, these values ranged from between 0.001 and 

0.006. The largest were near the location of a recent eruption. 

The distribution of the ratio of aerosol to molecular extinction at 

1.00 microns also showed that maximum values are found in the 

vicinity of an eruption. These maximums varied in altitude, but 

remained below a height of about 25 km. No attempt has been 

made to give detailed explanations or interpretations of these data. 

The intent is to provide, in a ready-to-use visual format, 

representative zonal and seasonal averages of aerosol extinction 

data for the third calendar year of the SAGE data set to facilitate 

atmospheric and climatic studies. Author 

N87-18248*# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

SPACE OPPORTUNITIES FOR TROPOSPHERIC CHEMISTRY 

RESEARCH 

JOEL S. LEVINE, ed. Feb. 1987 92 p Workshop held in 

New York, N.Y., 9-13 Sep. 1985 

(NASA-CP-2450; L-16250; NAS 1.55:2450) Avail: NTlS HC 

A05/MF A01 CSCL 04A 

AEROSOLS, AIR POLLUTION, ATMOSPHERIC CHEMISTRY, 

ATMOSPHERIC COMPOSITION, CONFERENCES, GASES, 

REMOTE SENSING, TROPOSPHERE 

N87-20663'# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

AIRBORNE LIDAR MEASUREMENTS OF EL CHICHON 

M. PATRICK MCCORMICK and M. T. OSBORN (ST Systems Corp., 

Hampton, Va.) Apr. 1987 49 p 

(NASA-RP-1175; L-16234; NAS 1.61:1175) Avail: NTlS HC 

A03/MF A01 CSCL 04A 

A lidar-equipped NASA Electra aircraft was flown in January 

1984 between the latitude of 38 and 90 deg N. One of the primary 

purposes of this mission was to determine the spatial distribution 

and aerosol characteristics of El Chichon produced stratospheric 

material. Lidar data from that portion of the flight mission between 

lidar backscatter ratio, a plot of the integral backscattering function 

altitude and latitude are given. In addition, tables containing 

numerical values of the backscatter ratio and backscattering 

function versus altitude are applied for each profile. These data 

clearly show that material produced by the El Chichon eruptions 

of late March-early April 1982 had spread throughout the latitudes 

covered by this mission, and that the most massive portion of the 

material resided north of 55 deg N and was concentrated below 

17 km in a layer that peaked at 13 to 15 km. In this latitude 

region, peak backscatter ratios at a wavelength of 0.6943 microns 

were approximately 3 and the peak integrated backscattering 

function was about 15 X 10 to the -4/sr corresponding to a peak 

optical depth of approximately 0.07. This report presents the 

results of this mission in a ready-to-use format for atmospheric 

and climatic studies. Author 

I STRATOSPHERIC AEROSOLS, JANUARY 1984 

I 38 deg N and 77 deg N is presented. Representative profiles of 

versus latitude, and contours of backscatter mixing ratio versus I 

N87-20665"# National Aeronautics and Space Administration. 

Marshall Space Flight Center, Huntsville, Ala. 

UPPER AND MIDDLE ATMOSPHERIC DENSITY MODELING 

REQUIREMENTS FOR SPACECRAFT DESIGN AND 

OPERATIONS 

M. H. DAVIS, ed. (Universities Space Research Association, 

Boulder, Colo.), R. E. SMITH, ed., and D. L. JOHNSON, ed. Feb. 

1987 290 p Workshop held in Huntsville, Ala., 19-21 1985 

(NASA-CP-2460; M-548; NAS 1.55:2460) 

A13/MF A01 CSCL 04A 

(NAS8-36400) 

Avail: NTlS HC 

AEROSPACE ENVIRONMENTS, ATMOSPHERIC DENSITY, 

ATMOSPHERIC MODELS. SPACECRAFT DESIGN. THERMOSPHERE 

47 

METEOROLOGY AND CLIMATOLOGY 

Includes weather forecasting and modification. 

N87-12086'# National Aeronautics and Space Administration. 

Wallops Flight Center, Wallops Island, Va. 

PRELIMINARY ESTIMATES OF RADIOSONDE THERMISTOR 

ERRORS 

F. J. SCHMIDLIN, J. K. LUERS (Dayton Univ., Ohio.), and P. D. 

HUFFMAN Washington, D.C. Sep. 1986 19 p 

(NASA-TP-2637; NAS 1.60:2637) Avail: NTlS HC AO2IMF A01 

CSCL 04B 

ERROR ANALYSIS, RADIOSONDES, THERMISTORS 

N87-13043'# 

Marshall Space Flight Center, Huntsville, Ala. 

REVIEW 

W. W. VAUGHAN, comp. and F. PORTER, comp. 

143 p 

Columbia, Md., 8-12 Jul. 1985 

(NASA-CP-2402; M-503; NAS 1.55:2402) Avail: NTlS HC 

A07/MF A01 CSCL 048 

ATMOSPHERIC ELECTRICITY, ATMOSPHERIC SOUNDING, 

DATA PROCESSING, DOPPLER RADAR, GEOPHYSICS, 

MESOSCALE PHENOMENA, OPTICAL RADAR, SATELLITE 

IMAGERY, THUNDERSTORMS, WIND (METEOROLOGY) 

N87-20701'# National Aeronautics and Space Administration. 

Goddard Space Flight Center, Greenbelt, Md. 

ON REQUIREMENTS FOR A SATELLITE MISSION TO MEASURE 

TROPICAL RAINFALL 

OTTO W. THIELE, ed. Apr. 1987 67 p 

(NASA-RP-1183; NAS 1.61:1183) Avail: NTlS HC A04/MF A01 

CSCL 048 

Tropical rainfall data are crucial in determining the role of tropical 

latent heating in driving the circulation of the global atmosphere. 

Also, the data are particularly important for testing the realism of 

climate models, and their ability to simulate and predict climate 

accurately on the seasonal time scale. Other scientific issues such 

as the effects of El Nino on climate could be addressed with a 

reliable, extended time series of tropical rainfall observations. A 

passive microwave sensor is planned to provide information on 

the integrated column precipitation content, its areal distribution, 

and its intensity. An active microwave sensor (radar) will define 

the layer depth of the precipitation and provide information about 

the intensity of rain reaching the surface, the key to determining 

the latent heat input to the atmosphere. A visible/infrared sensor 

will provide very high resolution information on cloud coverage, 

type, and top temperatures and also serve as the link between 

these data and the long and virtually continuous coverage by the 

geosynchronous meteorological satellites. The unique combination 

of sensor wavelengths, coverages, and resolving capabilities 

National Aeronautics and Space Administration. 

NASA/MSFC FY-85 ATMOSPHERIC PROCESSES RESEARCH 

Oct. 1985 

Review held in Huntsville, Ala. 7-9 May 1985 and in 

20 
52 AEROSPACE MEDICINE 

together with the low-altitude, non-Sun synchronous orbit provide 

a sampling capability that should yield monthly precipitation 

amounts to a reasonable accuracy over a 500- by 500-km grid. 

Author 

N87-22341'# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

ATMOSPHERIC TURBULENCE RELATIVE TO AVIATION, 

MISSILE, AND SPACE PROGRAMS 

DENNIS W. CAMP, ed. and WALTER FROST, ed. (FWG 

Associates, Inc., Tullahoma, Tenn.) Apr. 1987 257 p Workshop 

held in Hampton, Va., 2-4 Apr. 1986 

(NASA-CP-2468; L-16296; NAS 1.55:2468) Avail: NTlS HC 

Al2/MF A01 CSCL 048 

AIRCRAFT SAFEV, ATMOSPHERIC MODELS, ATMOSPHERIC 

TURBULENCE, CONFERENCES, MISSILES, SPACE PROGRAMS, 

WEATHER FORECASTING 

N87-26489*# 

Langley Research Center, Hampton, Va. 

RADIATION DERIVED FROM NIMBUS 6 EARTH RADIATION 

BUDGET DATA SET, JULY 1975 TO JUNE 1978 

T. DALE BESS and G. LOUIS SMITH Aug. 1987 80 p 

(NASA-RP-1185; L-16325; NAS 1.61:1185) Avail: NTlS HC 

A05/MF A01 CSCL 048 

An atlas of monthly mean outgoing longwave radiation global 

contour maps and associated spherical harmonic coefficients is 

presented. The atlas contains 36 months of continuous data from 

July 1975 to June 1978. The data were derived from the first 

Earth radiation budget experiment, which was flown on the 

Nimbus-6 Sun-synchronous satellite in 1975. Only the 

wide-field-of-view longwave measurements are cataloged in this 

atlas. The contour maps along with the associated sets of spherical 

harmonic coefficients form a valuable data set for studying different 

aspects of our changing climate over monthly, annual, and 

interannual scales in the time domain, and over regional, zonal, 

and global scales in the spatial domain. Author 

National Aeronautics and Space Administration. 

ATLAS OF WIDE-FIELD-OF-VIEW OUTGOING LONGWAVE 

N87-26491*# 

Langley Research Center, Hampton, Va. 

THE DYNAMICS EXPLORER 1 SATELLITE 

WALTER E. BRESSETTE, GERALD M. KEATING, and DAVID F. 

YOUNG (ST Systems Corp.. Hampton, Va.) Aug. 1987 44 p 

(NASA-TP-2723; L-16150; NAS 1.60:2723) Avail: NTlS HC 

A03/MF A01 CSCL 048 

ALGORITHMS, CALIBRATING, DYNAMICS EXPLORER 1 

SATELLITE, OZONE, REGRESSION ANALYSIS, ULTRAVIOLET 

SPECTROMETERS 

National Aeronautics and Space Administration. 

CALIBRATION OF THE SPIN-SCAN OZONE IMAGER ABOARD 

N87-29996*# National Aeronautics and Space Administration. 

Goddard Space Flight Center, Greenbelt, Md. 

FIVE YEAR GLOBAL DATASET: NMC OPERATIONAL 

ANALYSES (1978 TO 1982) 

DAVID STRAUS and JOSEPH ARDIZZONE Sep. 1987 50 p 

Prepared in cooperation with Sigma Data Services Corp.. Rockville, 

Md. 

(NASA-RP-1194; REPT-87B0273; NAS 1.61 :1194) Avail: NTlS 

HC AWMF A01 CSCL 048 

This document describes procedures used in assembling a five 

year dataset (1978 to 1982) using NMC Operational Analysis data. 

These procedures entailed replacing missing and unacceptable 

data in order to arrive at a complete dataset that is continuous in 

time. In addition, a subjective assessment on the integrity of all 

data (both preliminary and final) is presented. Documentation on 

tapes comprising the Five Year Global Dataset is also included. 

Author 

40 

OCEANOGRAPHY 

Includes biological, dynamic, and physical oceanography; and 

marine resources. 

N87-24870' 

Goddard Space Flight Center, Greenbelt, Md. 

OBSERVATIONS 

CLAIRE L. PARKINSON, JOSEFINO C. COMISO, H. JAY ZWALLY, 

DONALD J. CAVALIERI, PER GLOERSEN, and WILLIAM J. 

CAMPBELL (Puget Sound Univ., Tacoma, Wash.) Jan. 1987 

301 p Original contains color illustrations 

(NASA-SP-489; NAS 1.21 :489; LC-86-23876) Avail: NTlS HC 

A14 CSCLO8L 

The Arctic region plays a key role in the climate of the earth. 

The sea ice cover affects the radiative balance of the earth and 

radically changes the fluxes of heat between the atmosphere and 

the ocean. The observations of the Arctic made by the Electrically 

Scanning Microwave Radiometer (ESMR) on board the Nimbus 5 

research satellite are summarized for the period 1973 through 

1976. B.G. 

National Aeronautics and Space Administration. 

ARCTIC SEA ICE, 1973-1976: SATELLITE PASSIVE-MICROWAVE 

51 

LIFE SCIENCES (GENERAL) 

N87-20727" # National Aeronautics and Space Administration. 

Marshall Space Flight Center, Huntsville, Ala. 

LIQUID DROP STABILITY FOR PROTEIN CRYSTAL GROWTH 

IN MICROGRAVITY 

ROBERT B. OWEN, BETH H. BROOM, ROBERT S. SNYDER, 

and RON DANIEL Apr. 1987 17 p 

(NASA-TP-2724; NAS 1.60:2724) Avail: NTlS HC A02/MF A01 

CSCL 06B 

APPLICATIONS, PROTEIN SYNTHESIS, STABILITY 

CRYSTAL GROWTH, DROPS (LIQUIDS), MICROGRAVITY 

AEROSPACE MEDICINE 

Includes physiological factors; biological effects of radiation; and 

effects of weightlessness on man and animals. 

N87-18976' National Aeronautics and Space Administration, 

Washington, D.C. 

AEROSPACE MEDICINE AND BIOLOGY A CUMULATIVE INDEX 

TO THE 1986 ISSUES (SUPPLEMENT 293) 

Jan. 1987 251 p 

(NASA-SP-701 l(293); NAS 1.21:701 l(293)) Avail: NTlS HC A1 2 

CSCL 06E 

This publication is a cumulative index to the abstracts contained 

in the Supplements 281 through 292 of Aerospace Medicine and 

Biology: A Continuing Bibliography. It includes seven indexes - subject, personal author, corporate source, foreign technology, 

contract number, report number, and accession number. Author 

21 
52 AEROSPACE MEDICINE 

N87-30041' National Aeronautics and Space Administration, 

Washington, D.C. 

AEROSPACE MEDICINE AND BIOLOGY: A CONTINUING 

BIBLIOGRAPHY WITH INDEXES (SUPPLEMENT 302) 

Oct. 1987 55 p 

(NASA-SP-701 l(302); NAS 1.21:701 l(302)) Avail: HC A04 

CSCL 06E 

This bibliography lists 131 reports, articles, and other documents 

introduced into the NASA scientific and technical information 

system in September, 1987. Author 

61 

COMPUTER PROGRAMMING AND SOFTWARE 

Includes computer programs, routines, and algorithms, and specific 

applications, e.g., CAD/CAM. 

N87-10720'# National Aeronautics and Space Administration. 

Goddard Space Flight Center, Greenbelt, Md. 

PROCEEDINGS OF THE 5TH ANNUAL USERS CONFERENCE 

M. SZCZUR, ed. and E. HARRIS, ed. 1985 400 p Conference 

held at Greenbelt, Md., 4-6 Jun. 1985 

(NASA-CP-2399; NAS 1.55:2399) 

CSCL 09B 

ACCESS CONTROL, COMPUTER NETWORKS, FORMAT, 

IMAGE PROCESSING, ORBITAL SPACE STATIONS, SOFTWARE 

ENGINEERING, SOFTWARE TOOLS 

Avail: NTlS HC A1 7/MF A01 

N87-19931'# National Aeronautics and Space Administration, 

Washington, D.C. 

COMPUTER SCIENCES AND DATA SYSTEMS, VOLUME 1 

Mar. 1987 356 p Proceedings of a Symposium held in 

Williamsburg, Va., 18-20 Nov. 1986 

(NASA-CP-2459-VOL-1; NAS 1.55:2459-VOL-l) Avail: NTlS HC 

A16/MF A01 CSCL 09B 

SING, CONFERENCES, DATA MANAGEMENT, DISTRIBUTED 

PROCESSING, EXPERT SYSTEMS, SOFTWARE ENGINEERING 

ARCHITECTURE (COMPUTERS), CONCURRENT PROCESN87-19932*# 

Washington, D.C. 

COMPUTER SCIENCES AND DATA SYSTEMS, VOLUME 2 

Mar. 1987 339 p Proceedings of a Symposium held in 

Williamsburg, Va., 18-20 Nov. 1986 

(NASA-CP-2459-VOL-2; NAS 1.55:2459-VOL-2) Avail: NTlS HC 

A1 5/MF A01 CSCL 09B 

SING, FIBER OPTICS, OPTICAL DATA PROCESSING, PARALLEL 

PROCESSING (COMPUTERS), VHSIC (CIRCUITS) 

National Aeronautics and Space Administration, 

CONFERENCES, DATA STORAGE, DISTRIBUTED PROCESN87-23156'# 

Goddard Space Flight Center, Greenbelt, Md. 

SIXTH ANNUAL USERS CONFERENCE 

MARTHA SZCZUR, ed. and ELFRIEDA HARRIS, ed. (Science 

Applications Research, Lanham, Md.) Oct. 1986 228 p 

Conference held in Pasadena, Calif., 8-10 Oct. 1986; sponsored 

by JPL and NASA. Goddard Space Flight Center 

(NASA-CP-2463; REPT-87B0176; NAS 1.55:2463) 

HC A1 1 /MF A01 CSCL 096 

APPLICATIONS PROGRAMS (COMPUTERS), COMPUTER 

SYSTEMS PROGRAMS, CONFERENCES. IMAGE PROCESSING, 

OPERATING SYSTEMS (COMPUTERS) 

National Aeronautics and Space Administration. 

Avail: NTlS 

INFORMATION SYSTEMS, MAN-COMPUTER INTERFACE, 

N87-26531'# National Aeronautics and Space Administration. 

Goddard Space Flight Center, Greenbelt, Md. 

FRONTIERS OF MASSIVELY PARALLEL SCIENTIFIC 

COMPUTATION 

JAMES R. FISCHER, ed. Jul. 1987 293 p Symposium held 

in Greenbelt, Md., 24-25 Sep. 1986; sponsored by NASA Goddard 

Space Flight Center and Goodyear Aerospace Corp. 

(NASA-CP-2478; REPT-87B9876; NAS 1.552478) Avail: NTlS 

HC A13/MF A01 CSCL 09B 

ALGORITHMS, COMPUTER GRAPHICS, COMPUTER 

SYSTEMS PERFORMANCE, COMPUTERIZED SIMULATION, 

PARALLEL COMPUTERS, PARALLEL PROCESSING 

(COMPUTERS) 

COMPUTER SYSTEMS 

Includes computer networks and special application computer 

systems. 

N87-23202'# 

Lewis Research Center, Cleveland, Ohio. 

National Aeronautics and Space Administration. 

APPLICATIONS AND REQUIREMENTS FOR REAL-TIME 

SIMULATORS IN GROUND-TEST FACILITIES 

DALE J. ARPASI and RICHARD A. BLECH 

(NASA-TP-2672; E-3189; NAS 1.60:2672) Avail: NTlS HC 

AOWMF A01 CSCL 09B 

TEST FACILITIES 

Dec. 1986 26 p 

GROUND TESTS, REAL TIME OPERATION, SIMULATORS, 

NUMERICAL ANALYSIS 

Includes iteration, difference equations, and numerical 

approximation. 

N87-14054*# 

Langley Research Center, Hampton, Va. 

NONLINEAR EQUATIONS AND COMPARISON WITH 

PARAMETRIC DIFFERENTIATION 

R. L. BARGER and R. W. WALTERS (Virginia Polytechnic Inst. 

and State Univ., Blacksburg.) 1986 16 p 

(NASA-TP-2654; L-16199; NAS 1.60:2654) Avail: NTlS HC 

AO2IMF A01 CSCL 12A 

COMPUTER PROGRAMMING, CRITICAL PATH METHOD, 

DIFFERENTIAL EQUATIONS, NONLINEAR EQUATIONS, 

PARAMETER IDENTIFICATION 

National Aeronautics and Space Administration. 

SOME PATH-FOLLOWING TECHNIQUES FOR SOLUTION OF 

N87-14918'# National Aeronautics and Space Administration. 

Lewis Research Center, Cleveland, Ohio. 

SOLUTION OF ELLIPTIC PARTIAL DIFFERENTIAL EQUATIONS 

BY FAST POISSON SOLVERS USING A LOCAL RELAXATION 

S. C. CHANG May 1986 17 p 

(NASA-TP-2530; E-2528-1; NAS 1.60:2530) 

AO2/MF A01 CSCL 12A 

PARTIAL DIFFERENTIAL EQUATIONS, PROBLEM SOLVING 

FACTOR. 2 TWO-STEP METHOD 

Avail: NTlS HC 

ELLIPTIC DIFFERENTIAL EQUATIONS, ELLIPTIC FUNCTIONS, 

22 
71 ACOUSTICS 

N87-22441'# National Aeronautics. and Space Administration. 

Langley Research Center, Hampton, Va. 

QUANTITATIVE ANALYSIS OF THE RECONSTRUCTION 

PERFORMANCE OF INTERPOLANTS 

DONALD L. LANSING and STEPHEN K. PARK (College of William 

and Mary, Williamsburg, Va.) May 1987 35 p 

(NASA-TP-2688; L-16164; NAS 1.60:2688) Avail: NTlS HC 

AO3/MF A01 CSCL 12A 

TION 

INTERPOLATION, QUANTITATIVE ANALYSIS, RECONSTRUCN87-22447'# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

AN ALGORITHM FOR SURFACE SMOOTHING WITH RATIONAL 

SPLINES 

JAMES R. SCHIESS Jun. 1987 17 p 

(NASA-TP-2708; L-16272; NAS 1.60:2708) Avail: NTlS HC 

A02/MF A01 CSCL 12A 

SPLINE FUNCTIONS, SURFACE ROUGHNESS 

ALGORITHMS, RATIONAL FUNCTIONS, SMOOTHING, 

N87-28367'# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

EXPERIMENTS IN ENCODING MULTILEVEL IMAGES AS 

QUADTREES 

DONALD L. LANSING Sep. 1987 60 p 

(NASA-TP-2722; L-16292; NAS 1.60:2722) Avail: NTlS HC 

A04/MF A01 CSCL 12A 

SCALE, IMAGE PROCESSING 

CODING, DATA COMPRESSION, DATA STORAGE, GRAY 

65 

STATISTICS AND PROBABILITY 

Includes data sampling and smoothing; Monte Carlo method; and 

stochastic processes. 

N87-23244'# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

DEVELOPMENT OF CONFIDENCE LIMITS BY PIVOTAL 

FUNCTIONS FOR ESTIMATING SOFTWARE RELIABILITY 

KELLY J. DOTSON Jun. 1987 12 p 

(NASA-TP-2709; L-16264; NAS 1.60:2709) Avail: NTlS HC 

A02/MF A01 CSCL 12A 

RELIABILITY ANALYSIS, SOFTWARE ENGINEERING 

CONFIDENCE LIMITS, FAILURE ANALYSIS, PREDICTIONS, 

N87-27474'# National Aeronautics and Space Administration. 

Marshall Space Flight Center, Huntsville, Ala. 

PROBABILISTIC RISK ANALYSIS OF FLYING THE SPACE 

SHUlTLE WITH AND WITHOUT FUEL TURBINE DISCHARGE 

TEMPERATURE REDLINE PROTECTION 

LEONARD HOWELL Aug. 1987 22 p 

(NASA-TP-2759; NAS 1.60:2759) Avail: NTlS HC AO2/MF A01 

CSCL 12A 

ENGINE FAILURE, MATHEMATICAL MODELS, SPACE 

SHUTTLE MAIN ENGINE, SPACECRAFT RELIABILITY, 

STOCHASTIC PROCESSES. TEMPERATURE SENSORS 

71 

ACOUSTICS 

Includes sound generation, transmission, and attenuation. 

N87-14120'# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

EFFECTS OF BACKGROUND NOISE ON TOTAL NOISE 

ANNOYANCE 

K. F. WILLSHIRE Jan. 1987 59 p 

(NASA-TP-2630; L-16153; NAS 1.60:2630) Avail: NTlS HC 

A04/MF A01 CSCL 46A 

BACKGROUND NOISE, EFFECTIVE PERCEIVED NOISE 

LEVELS, NOISE INTENSITY, NOISE POLLUTION, NOISE 

TOLERANCE 

N87-17479'# National Aeronautics and Space Administration. 

Langley Research Center, Hampton. Va. 

POWER CEPSTRUM TECHNIQUE WITH APPLICATION TO 

MODEL HELICOPTER ACOUSTIC DATA 

R. M. MARTIN and C. L. BURLEY Washington Jun. 1986 

(NASA-TP-2586; L-16070; NAS 1.60:2586) Avail: NTlS HC 

A04/MF A01 CSCL 20A 

HELICOPTERS, MODELS, SIGNAL REFLECTION 

68 P 

ACOUSTIC MEASUREMENT, CEPSTRAL ANALYSIS, 

N87-18399'# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

CORRELATION OF HELICOPTER IMPULSIVE NOISE FROM 

ANDREW B. CONNOR and R. M. MARTIN Mar. 1987 23 p 

(NASA-TP-2650; L-16145; NAS 1.60:2650) Avail: NTlS HC 

A02/MF A01 CSCL 20A 

BLADES (TURBOMACHINERY), VORTICES, WIND TUNNEL 

TESTS 

BLADE-VORTEX INTERACTION WITH ROTOR MEAN INFLOW 

BLADE SLAP NOISE, BLADE-VORTEX INTERACTION, ROTOR 

N87-20798*# 

Langley Research Center, Hampton, Va. 

National Aeronautics and Space Administration. 

EXPERIMENTAL VALIDATION OF A TWO-DIMENSIONAL 

SHEAR-FLOW MODEL FOR DETERMINING ACOUSTIC 

IMPEDANCE 

TONY L. PARROTT, WILLIE R. WATSON, and MICHAEL G. JONES 

(PRC Kentron, Inc., Hampton, Va.) May 1987 50 p 

(NASA-TP-2679; L-16203; NAS 1.60:2679) Avail: NTlS HC 

A03/MF A01 CSCL 20A 

DIMENSIONAL FLOW 

ACOUSTIC IMPEDANCE, MODELS, SHEAR FLOW, TWO 

N87-24161'# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

ANNOYANCE RESPONSE TO SIMULATED ADVANCED 

TURBOPROP AIRCRAFT INTERIOR NOISE CONTAINING 

TONAL BEATS 

JACK D. LEATHERWOOD Jul. 1987 28 p 

(NASA-TP-2689; L-16184; NAS 1.60:2689) Avail: NTlS HC 

A03/MF A01 CSCL 20A 

TOLERANCES, PSYCHOLOGICAL EFFECTS, RESPONSES 

AIRCRAFT COMPARTMENTS, AIRCRAFT NOISE, HUMAN 

23 
73 NUCLEAR AND HIGH-ENERGY PHYSICS 

73 N87-14998*# 

Lewis Research Center, Cleveland, Ohio. 

National Aeronautics and Space Administration. 

NUCLEAR AND HIGH-ENERGY PHYSICS 

Includes elementary and nuclear particles; and reactor theory. 

N87-17487'# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

DOUBLY DIFFERENTIAL CROSS SECTIONS FOR GALACTIC 

HEAVY-ION FRAGMENTATION 

FRANCIS A. CUClNOlTA (Old Dominion Univ., Norfolk, Va.), JOHN 

W. NORBURY, GOVIND S. KHANDELWAL, and LAWRENCE W. 

TOWNSEND Feb. 1987 23 p 

(NASA-TP-2659; L-16187; NAS 1.60:2659) Avail: NTlS HC 

AO2/MF A01 CSCL 20H 

PARTICLE COLLISIONS, SCATTERING CROSS SECTIONS 

COLLISION PARAMETERS, GALAXIES, HEAVY IONS, 

N87-24977'# 

Langley Research Center, Hampton, Va. 

NUCLEI AND ANTINUCLEI 

WARREN W. BUCK, JOHN W. WILSON, LAWRENCE W. 

TOWNSEND, and JOHN W. NORBURY (Idaho Univ., Moscow.) 

Jul. 1987 47 p 

(NASA-TP-2741; L-16275; NAS 1.60:2741) Avail: NTlS HC 

A03/MF A01 CSCL 20H 

HEAVY IONS, NUCLEI (NUCLEAR PHYSICS) 

National Aeronautics and Space Administration. 

POSSIBLE COMPLEMENTARY COSMIC-RAY SYSTEMS 

ANTIMATTER, ANTIPARTICLES, GALACTIC COSMIC RAYS, 

74 

OPTICS 

ASYMPTOTIC ANALYSIS OF CORONA DISCHARGE FROM THIN 

ELECTRODES 

P. A. DURBIN Sep. 1986 7 p 

(NASA-TP-2645; E-31 51; NAS 1.60:2645) 

A02/MF A01 CSCL 201 

DISCHARGES, ELECTRODES 

Avail: NTlS HC 

ASYMPTOTIC METHODS, ELECTRIC CORONA, ELECTRIC 

ai 

ADMINISTRATION AND MANAGEMENT 

Includes management planning and research. 

N87-20833. National Aeronautics and Space Administration, 

Washington, D.C. 

MANAGEMENT A BIBLIOGRAPHY FOR NASA MANAGERS 

(SUPPLEMENT 21) 

Apr. 1987 70 p 

(NASA-SP-7500(21); NAS 1.21:7500(21)) Avail: NTlS HC A04 

CSCL 05A 

This bibliography lists 664 reports, articles and other documents 

introduced into the NASA scientific and technical information 

system in 1986. Items are selected and grouped according to 

their usefulness to the manager as manager. Citations are grouped 

into ten subject categories: human factors and personnel issues; 

management theory and techniques; industrial management and 

manufacturing; robotics and expert systems; computers and 

information management; research and development; economics, 

costs, and markets; logistics and operations management; reliability 

and quality control; and legality, legislation, and policy. Author 

Includes light phenomena; and optical devices. 

DOCUMENTATION AND INFORMATION SCIENCE 

N87-13264*# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

THEORY FOR COMPUTING THE FIELD SCAlTERED FROM A 

SMOOTH INFLECTED SURFACE 

R. L. BARGER and A. K. DOMINEK 1986 23 p 

(NASA-TP-2632; L-16157; NAS 1.60:2632) Avail: NTlS HC 

A01 /MF A01 CSCL 20F 

BODIES OF REVOLUTION, ELECTROMAGNETIC RADIATION, 

MICROWAVES, REFLECTANCE, SURFACE PROPERTIES, WAVE 

SCATTERING 

75 

PLASMA PHYSICS 

Includes magnetohydrodynamics and plasma fusion. 

N87-10764'# 

Langley Research Center, Hampton, Va. 

LASER-POWERED MHD GENERATORS FOR SPACE 

APPLICATION 

N. W. JALUFKA Oct. 1986 15 p 

(NASA-TP-2621; NAS 1.60:2621) Avail: NTlS HC A02/MF A01 

CSCL 201 

INTERACTIONS, MAGNETOHYDRODYNAMIC GENERATORS 

National Aeronautics and Space Administration. 

ENERGY CONVERSION EFFICIENCY, LASER PLASMA 

Includes information management; information storage and retrieval 

technology; technical writing; graphic arts; and micrography. 

N87-25023* National Aeronautics and Space Administration, 

Washington, D.C. 

NASA PATENT ABSTRACTS BIBLIOGRAPHY: A CONTINUING 

BIBLIOGRAPHY. SECTION 1: ABSTRACTS (SUPPLEMENT 31) 

Jul. 1987 45 p 

(NASA-SP-7039(31); NAS 1.21 :7039(31)) Avail: NTlS HC A03; 

NTlS standing order as PB86-911100, $1 1.50 domestic, $23.00 

foreign CSCL 058 

Abstracts are provided for 85 patents and patent applications 

entered into the NASA scientific and technical information system 

during the period January 1987 through June 1987. Each entry 

consists of a citation, an abstract, and in most cases, a key 

illustration selected from the patent or patent application. Author 

N87-26689' National Aeronautics and Space Administration, 

Washington, D.C. 

NASA PATENT ABSTRACTS BIBLIOGRAPHY A CONTINUING 

BIBLIOGRAPHY. SECTION 2 INDEXES (SUPPLEMENT 31) 

Jul. 1987 493 p 

(NASA-SP-7039(31)-SECT-2; NAS 1.21 :7039(31)-SECT-2) Avail: 

NTlS HC A21 CSCL 058 

A subject index is provided for over 4600 patents and patent 

applications for the period May 1969 through June 1987. Additional 

indexes list personal authors, corporate authors, contract numbers, 

NASA case numbers, U.S. patent class numbers, and NASA 

accession numbers. Author 

24 
89 ASTRONOMY 

N87-27557' 

Washington, D.C. 

NASA THESAURUS SUPPLEMENT (SUPPLEMENT 3) 

National Aeronautics and Space Administration, 

Jul. 1987 325 p 

(NASA-SP-7053tSUPP-3); NAS 1.21 :7053(SUPP-3)) Avail: NTlS 

HC A14 CSCLO5B . 

The four part cumulative NASA Thesaurus Supplement to the 

1985 edition of the NASA Thesaurus includes Part 1, Hierarchical 

Listing, Part 2, Access Vocabulary, Part 3, NASA Thesaurus 

Definitions, and Part 4, Changes. The semiannual supplement gives 

complete hierarchies for new terms. Author 

N87-30218'# National Aeronautics and Space Administration, 

Washington, D.C. 

NASA SCIENTIFIC AND TECHNICAL PUBLICATIONS A 

CATALOG OF SPECIAL PUBLICATIONS, REFERENCE 

PUBLICATIONS, CONFERENCE PUBLICATIONS, AND TECHNICAL PAPERS. 1977-1986 

&p. 1987 390 p 

(NASA-SP-7063: .- NAS 1.21:70631 Avail: NTlS HC free as -- - - 

PR-655B; NASA Scientific and Technical Information Facility, P.O. 

Box 8757, BWI Airport, Md. 21240 HC free 

This catalog lists 231 1 citations of all NASA Special Publications, 

NASA Reference Publications, NASA Conference Publications, and 

NASA Technical Papers that were entered into the NASA scientific 

and technical database during the decade 1977 through 1986. 

The entries are grouped by subject category. Indexes of subject 

terms, personal authors, and NASA report numbers are provided. 

Author 

CSCL 05B 

URBAN TECHNOLOGY AND TRANSPORTATION 

Includes applications of space technology to urban problems; 

technology transfer; technology assessment; and surface and mass 

transportation. 

N87-70425' National Aeronautics and Space Administration, 

Washington, D.C. 

SIGNIFICANT NASA INVENTIONS. AVAILABLE FOR 

LICENSING IN FOREIGN COUNTRIES 

1977 103 p 

(NASA-SP-7038(04); NAS 1.21 :7038(04)) Avail: SOD HC $5.00 

as 003-000-00986-1; NTlS MF A01 

88 

SPACE SCIENCES (GENERAL) 

N87-23313'# National Aeronautics and Space Administration. 

Marshall Space Flight Center, Huntsville, Ala. 

DOUBLE LAYERS IN ASTROPHYSICS 

ALTON C. WILLIAMS, ed. and TAUNA W. MOOREHEAD. ed. May 

1987 321 p Workshop held in Huntsville, Ala., 17-19 Mar. 

1986 sponsored by NASA, Washington and USRA 

(NASA-CP-2469; M-560; NAS 1.55:2469) Avail: NTlS HC 

AlUMF A01 CSCL 038 

CONFERENCES, ELECTRIC FIELDS, ENERGY TRANSFER, 

MATHEMATICAL MODELS, PLASMA LAYERS, PLASMA 

PHYSICS, SPACE PLASMAS 

N87-24247'# National Aeronautics and Space Administration. 

Goddard Space Flight Center, Greenbelt, Md. 

ESSAYS IN SPACE SCIENCE 

REUVEN RAMATY, ed., THOMAS L. CLINE, ed., and JONATHAN 

F. ORMES, ed. Jun. 1987 424 p Symposium held in Greenbelt, 

Md., 23 Apr. 1985 

(NASA-CP-2464; REPT-87B0055; NAS 1 552464) Avail: NTlS 

HC A18/MF A01 CSCL 038 

ASTROPHYSICS, CONFERENCES, COSMIC RAYS, GAMMA 

RAY ASTRONOMY, INFRARED ASTRONOMY, X RAY 

ASTRONOMY 

N87-28471'# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

CALCULATION AND ACCURACY OF ERBE SCANNER 

MEASUREMENT LOCATIONS 

LAWRENCE H. HOFFMAN, WILLIAM L. WEAVER, and JAMES F. 

KIBLER Sep. 1987 34 p 

(NASA-TP-2670; L-16218; NAS 1.60:2670) Avail: NTlS HC 

A03/MF A01 CSCL 038 

COMPUTATION, EARTH ATMOSPHERE, EARTH RADIATION 

BUDGET EXPERIMENT, POSITION (LOCATION), REMOTE 

SENSING, SCANNING 

89 

ASTRONOMY 

Includes radio, gamma-ray, and infrared astronomy; and 

astrometry. 

N87-14219*# 

Goddard Space Flight Center, Greenbelt, Md. 

TEN YEAR PLANETARY EPHEMERIS 1986-1995 

F. ESPENAK Nov. 1986 249 p 

(NASA-RP-1176; NAS 1.61:1176; REPT-86B0471) Avail: NTlS 

HC A1 1 /MF A01 CSCL 03A 

Accurate geocentric positions are tabulated at five day intervals 

for the Sun, Mercury, Venus, Mars, Jupiter, Saturn, Uranus and 

Neptune during the ten year period 1986 through 1995. The 

apparent angular diameters, radial velocities, declinations and mean 

times of meridian transit of the seven planets and the Sun are 

graphically depicted for each year in the interval. Appendices are 

included which discuss the theory of planetary orbits and a 

FORTRAN program for calculating planetary ephemerides. 

Author 

National Aeronautics and Space Administration. 

N87-22573'# National Aeronautics and Space Administration. 

Goddard Space Flight Center. Greenbelt, Md. 

INFRARED SOURCE CROSS-INDEX, FIRST EDITION 

MARION SCHMITZ (Computer Sciences Corp., Beltsville, Md.), 

JAYLEE M. MEAD, and DANIEL Y. GEZARI Apr. 1987 323 p 

(NASA-RP-1182; REPT-87B0058; NAS 1.61 :1182) Avail: NTlS 

HC A14/MF A01 CSCL 03A 

The Infrared Source Cross-Index is a listing of correlated 

infrared source names (and positions) for astronomical objects 

observed at 1-1000 microns. The source names have been 

obtained from the database of the first edition of the Catalog of 

Infrared Observations (CIO NASA RP 11 le), covering observations 

published through 1982. Additional identifications were located by 

correlating these names with identifications contained in other 

machine-readable astronomical catalogs in the NASA National 

Space Science Data Center (NSSDC). There are some 80,000 

different source names in the Cross-Index, corresponding to over 

27,000 unique infrared sources. Author 

25 
89 ASTRONOMY 

N87-24266'# National Aeronautics and Space Administration, 

Washington, D.C. 

STAR FORMATION IN GALAXIES 

May 1987 755 p Conference held in Pasadena, Calif., 16-19 

Jun. 1986 

(NASA-CP-2466; NAS 1.55:2466) Avail: NTlS HC A99/MF E03 

CSCL 03A 

CONFERENCES, GALACTIC STRUCTURE, GALAXIES, 

INFRARED ASTRONOMY, MOLECULAR CLOUDS, RADIO 

ASTRONOMY, STAR FORMATION, STELLAR LUMINOSITY 

N87-25906'# 

Goddard Space Flight Center, Greenbelt, Md. 

FRED ESPENAK Jul. 1987 272 p 

Avail: NTlS HC A12/MF A01 

A complete catalog is presented, listing the general 

characteristics of every solar eclipse from 1901 through 2100. To 

complement this catalog, a detailed set of cylindrical projection 

the 200 year interval. Focusing in on the next 50 years, accurate 

geodetic path coordinates and local circumstances for the 71 

central eclipses from 1987 through 2035 are tabulated. Finally, 

the geodetic paths of the umbral and penumbral shadows of all 

109 solar eclipses in this period are plotted on orthographic 

projection maps of the Earth. Appendices are included which 

discuss eclipse geometry, eclipse frequency and occurrence, 

modern eclipse prediction and time determination. Finally, code 

for a simple Fortran program is given to predict the occurrence 

and characteristics of solar eclipses. Author 

National Aeronautics and Space Administration. 

FIFTY YEAR CANON OF SOLAR ECLIPSES 1986 - 2035 

(NASA-RP-1178-REV; REPT-87B0252; NAS 1.61 :1178-REV) 

CSCL 03A 

, world maps shows the umbral paths of every solar eclipse over 

~ 

90 

ASTROPHYSICS 

Includes cosmology; celestial mechanics; space plasmas; and 

interstellar and interplanetary gases and dust. 

N87-30235*# National Aeronautics and Space Administration. 

Goddard Space Flight Center, Greenbelt, Md. 

ATLAS OF COMET HALLEY 1910 I1 

BERTRAM DONN, JUERGEN RAHE, and JOHN C. BRANDT 

1986 597 p 

(NASA-SP-488; NAS 1.21:488; LC-86-16341) 

$48.00 as 033-000-00991-7; NTlS MF A01 

With the impending return of Halley's Comet in 1986, a major 

effort began to collect the material obtained at its last appearance 

in 1910. This material displays the evolving coma and tail 

phenomena, and is Useful for comparison with the present 

quantitative studies of spectroscopic and structural phenomena. 

Images in the atlas are arranged in chronological order by day. 

Days that have multiple images with varying scale are arranged in 

two sequences. Photographs showing tail phenomena are first, 

followed by photographs obtained with longer focus instruments 

showing the head or near-nuclear region. Drawings of Comet Halley, 

made from visual observations in 1835 and 1910, also are 

included. B.G. 

~ 

Avail: SOD HC 

CSCL 038 

I 

91 

LUNAR AND PLANETARY EXPLORATION 

Includes planetology; and manned and unmanned flights. 

N87-17598*# 

Goddard Inst. for Space Studies, New York, N.Y. 

THE JOVIAN ATMOSPHERES 

MICHAEL ALLISON, ed. and LARRY D. TRAVIS, ed. 

129 p 

Submitted for publication 

(NASA-CP-2441; NAS 1.55:2441) Copyright Avail: NTlS HC 

A07/MF A01 CSCL 848 

ATMOSPHERIC CHEMISTRY, CLOUDS (METEOROLOGY), 

GAS DYNAMICS, GAS GIANT PLANETS, HYDROGEN, JUPITER 

SPHERE, SPACE EXPLORATION, SYNOPTIC METEOROLOGY, 

THERMODYNAMICS, URANUS ATMOSPHERE 

N87-19322'# 

Washington, D.C. 

STATUS AND FUTURE OF LUNAR GEOSCIENCE 

1986 63 p 

(NASA-SP-484; NAS 1.21 :484) Avail: SOD HC $4.25 as 

The Moon is of special interest among the many and diverse 

bodies of the solar system because it serves as a scientific baseline 

for understanding the terrestrial planets, its origin is closely tied 

to the early history of the Earth, and its proximity permits a variety 

of space applications such as mining and establishment of bases 

and colonies. Data acquisition and analysis have enabled advances 

to be made and the remaining questions in many fields of lunar 

geoscience to be identified. The status and unresolved problems 

of lunar science are discussed. Immediate needs, new unmanned 

missions, and a return to the Moon (a lunar base) are examined. 

B.G. 

National Aeronautics and Space Administration. 

Oct. 1986 

Conference held in New York, N.Y., 6-8 May 1985 

ATMOSPHERE, NEPTUNE ATMOSPHERE, SATURN ATMONational Aeronautics and Space Administration, 

033-000-00997-6; NTlS MF A01 CSCL 038 

SOLAR PHYSICS 

Includes solar activity, solar flares, solar radiation and sunspots. 

N87-19328'# National Aeronautics and Space Administration. 

Goddard Space Flight Center, Greenbelt, Md. 

ENERGETIC PHENOMENA ON THE SUN: THE SOLAR 

MAXIMUM MISSION FLARE WORKSHOP. PROCEEDINGS 

MUKUL KUNDU, ed. (Maryland Univ., College Park) and BRUCE 

WOODGATE, ed. Dec. 1986 423 p Workshop held in Greenbelt, 

Md., 24-28 Jan. 1983, 9-14 Jun. 1983, and 13-17 Feb. 1984 

(NASA-CP-2439; NAS 1.55:2439) Avail: NTlS HC A18/MF A01 

CSCL 038 

CONFERENCES, MAGNETOHYDRODYNAMIC STABILITY, 

SOLAR CORONA, SOLAR FLARES, SOLAR MAGNETIC FIELD, 

SOLAR MAXIMUM MISSION, SOLAR PHYSICS, SOLAR 

PROMINENCES, SUN, SUNSPOTS 

N87-20871'# National Aeronautics and Space Administration. 

Goddard Space Flight Center, Greenbelt, Md. 

CORONAL AND PROMINENCE PLASMAS 

ARTHUR 1. POLAND, ed. Dec. 1986 435 p Workshop held 

in Greenbelt, Md., 9-11 Apr. 1985 and 8-10 Apr. 1986 

(NASA-CP-2442; REPT-86B0536; NAS 1 552442) 

HC A19/MF A01 CSCL 03B 

CONFERENCES, MAGNETIC FIELD CONFIGURATIONS, 

MAGNETOHYDRODYNAMIC STABILITY, MAGNETOSTATICS, 

PLASMAS (PHYSICS), RADIO ASTRONOMY, SOLAR 

Avail: NTlS 

26 
99 GENERAL 

ATMOSPHERE, SOLAR CORONA, SOLAR MAGNETIC FIELD, 

SOLAR PHYSICS, SOLAR PROMINENCES, SUN 

N87-20947'# National Aeronautics and Space Administration. 

Marshall Space Flight Center, Huntsville, Ala. 

STATISTICAL ASPECTS OF SOLAR FLARES 

ROBERT M. WILSON Apr. 1987 41 p 

(NASA-TP-2714; NAS 1.60:2714) Avail: NTlS HC AO3/MF A01 

CSCL 038 

SOLAR FLARES, SOLAR PROMINENCES, STATISTICAL 

ANALYSIS 

N87-21785'# National Aeronautics and Space Administration. 

Goddard Space Flight Center, Greenbelt, Md. 

RAPID FLUCTUATIONS IN SOLAR FLARES 

BRIAN R. DENNIS, ed., LARRY E. ORWIG, ed., and ALAN L. 

KIPLINGER. ed. (Systems Applied Sciences Corp.-Technologies, 

Landover, Md.) 1986 491 p Workshop held in Lanham, Md., 

30 Sep. - 4 Oct. 1985 

(NASA-CP-2449; NAS 1.552449) Avail: NTlS HC A21/MF A01 

CSCL 038 

PHYSICS, RADIO WAVES, SOLAR FLARES, X RAYS 

CONFERENCES, MICROWAVES, OSCILLATIONS, PLASMA 

SPACE RADIATION 

Includes cosmic radiation; and inner and outer earth's radiation 

belts. 

N87-25984'# National Aeronautics and Space Administration. 

Goddard Space Flight Center, Greenbelt, Md. 

COSMIC RAY HEAVY ION LET MAPPING FOR ALUMINUM, 

SILICON, AND TISSUE TARGETS 

E. G. STASSINOPOULOS, J. M. EARTH, and T. M. JORDAN 

(EMP Consultants, Northridge, Calif.) Apr. 1987 264 p 

(NASA-RP-1180; REPT-87B0034; NAS 1.61:1180) Avail: NTlS 

HC Al2lMF A01 CSCL 038 

Linear energy transfer (LET) values in aluminum, silicon, and 

tissue targets have been calculated for 31 galactic cosmic ray ion 

species in eight different units. The values are described for single 

event upset (SEU) effect assessments or radiobiological 

evaluations. The data are presented in graphical and tabular 

form. Author 

GENERAL 

N87-24390'# National Aeronautics and Space Administration. 

Langley Research Center, Hampton, Va. 

ENGINEER IN CHARGE A HISTORY OF THE LANGLEY 

JAMES R. HANSEN (Maine Univ., Orono.) Washington, D.C. 

1986 643 p NASA History Series 

(NASA-SP-4305; NAS 1.21 :4305) Avail: SOD HC $30.00 as 

A history is presented by using the most technologically 

significant research programs associated with the Langley 

Aeronautical Laboratory from 1917 to 1958 and those programs 

that, after preliminary research, seemed best to illustrate how the 

laboratory was organized, how it works, and how it cooperated 

B.G. 

AERONAUTICAL LABORATORY, 1917-1958 

(NASW-3502) 

033-000-00999-2; NTlS MF A01 CSCL 058 

with industry and the military. 

27 
SUBJECT INDEX 

NASA Scientific and Technical Publications 1987 

qpical Subject Index Listing 

T SUBJECT HEADING 

The subject heading is a key to the subject content 

of the document. The title is used to provide a 

description of the subject matter. When the title is 

insufficiently descriptive of document content, a 

title extension is added, separated from the title 

by three hyphens. The accession number and the 

page number are included in each entry to assist 

the user in locating the abstract in the abstract 

section. If applicable, a report number is also included as an aid in identifying the document. 

Under any one subject heading, the accession 

numbers are arranged in sequence. 

A 

ABSORPTION CROSS SECTIONS 

Atlas of absorption lines from 0 to 17900 cm (sup)-1 

[NASA-RP-1188] p 19 N87-28955 

Atlas of absorption lines from 0 to 17900 cm (sup)-1 

[ NASA-RP-11881 p 19 N87-28955 

ABSORPTION SPECTRA 

ACCESS CONTROL 

Proceedings of the 5th Annual Used Conference 

[NASA-CP-2399] p22 N87-10720 

Performance of textured carbon on copper electrode 

multistage depressed collectors with medium-power 

traveling wave tubes 

ACCUMULATORS 

[ NASA-TP-28651 p14 N87-17990 

Calculation of secondary electron trajectories in 

multistage depressed Co(lect0rs for microwave amplifiers 

[NASA-TP-Z664] p 14 N87-17991 

Descen. fabrication and performance of small. graphiie 

electrode, multistage depressed collectors with 200-W. 

CW, 8- to 18-GHz traveling-wave tubes 

[ NASA-TP-26931 p 14 N87-20474 

Analytical and experimental performance of a dual-mode 

traveling wave tube and multistage depressed collects 

[ NASA-TP-27521 p14 N87-25532 

The ACEE program and basic composites research at 

Langley Research Center (1975 to 1988): Summary and 

bibliraphy 

[NASA-RP-1177] p 11 N87-29612 

Expimental validation of a two-dimensional shear-flow 

model for determining -tic impedance 

[NASA-TP-2679] p23 N87-20798 

Power cepstrum technique with application to model 

[ NASA-TP-25861 p 23 N87-17479 

ACEE -RAM 

ACWSTlC IMPEDANCE 

ACOUSTK: MEASUREMENT 

helier awustic data 

ACOUSTICS 

Heliter Madevortex interaction locations: 

Scale-model acwstics and free-wake analysis results 

[NASA-TP-2658] p3 N87-18537 

The 20th Aerospace Mechanics Symposium 

p17 N87-16321 

The 2191 Aerospace Mechanisms Symposium 

[ NASA-CP-24701 pl8 N87-29858 

Piloted simulation study of the effects of an automated 

trim system on fliht characteristics of a liiht twin-engina 

airplane with one engine inoperative 

[ NASA-TP-26331 p 2 N87-10843 

AERODYNAMIC CHARACTERISTICS 

Effects of empennage surfaw location on aerodynamic 

characteristics of a twin-engine aftmbody model with 

nonaxisymmetric nozzles 

[ NASA-TP-23921 p6 N87-17693 

Low-speed aerodynamic characteristics of a twin-engine 

general aviation configuration with aft-fuselage-mounted 

[ NASA-TP-27631 p5 N87-29462 

AERODYNAMIC COEFFICIENTS 

Flightdetermined aerodynamic derivatives of the AB1 

obliquewing research airplane 

[NASA-TP-ZZZZ] p8 N87-10871 

Combined aerodynamic and structural dynamic problem 

emulating routines (CASPER): Theory and 

implementation 

[ NASA-TP-24181 p3 N87-17669 

Forward-swept wing mfguration designed for high 

maneuverability by use of a transonic wmputational 

method 

[ NASA-TP-26281 p 2 N87-11702 

Effects of winglet on transonic flutter characteristics of 

a cantilevered twin-engine-transport wing model 

[ NASA-TP-26271 p 17 N87-13789 

Flihl investigation of the eflect of tail configuration on 

stall, spin, and recovery characteristics of s low-wing 

general aviation research airplane 

[ NASA-TP-2644) p6 N87-16815 

Flight characteristics of the AD-1 obliquewing reaearch 

aircraft 

[ NASA-TP-22231 p8 N87-18570 

On minimizing the number of calculations in 

[ NASA-TP-27061 p3 N87-23586 

Effect of Reynolds number variation on aerodynamics 

of a hydrogen-fueled transport concept at Mach 6 

[ NASA-TP-2728) p4 N87-2M)31 

Subsonic Ionghdinal and lateraldirectional 

characteristics of a fomard-swept-wing fighter 

configuration at angles of attack up to 47 deg 

[NASA-TP-2727] p4 N87-26874 

Effects of tail span and empennage arrangement on 

drag of a typical singleengine fighter aft end 

[ NASA-TP-23521 p 1 N87-10838 

Effects of empennage surfsce location on aerodynamic 

characteristics of a twic-mgine aftebody model with 

nonaxisymmetric nonles 

[ NASA-TP-23921 p 6 N87-17693 

Drag measurements of blunt stores tangentially mounted 

on a flat plate at supersonic speeds 

[NASA-TP-2742] p5 N87-27626 

Steady and unsteady aerodynamic forces from the 

SOUSSA surface-panel method for a fighter wing with tip 

missile and comparison with experiment andPANAlR 

[NASA-TP-2728] p4 N87-28032 

Finite-element reentry heat-transfer analysis of space shuttle Mer 

[ NASA-TP-26571 p 16 N87-29795 

Interference effects of thrust reversing on horizontal tail 

effectiveness of twin-engine fighter aircraft at Mach 

numbers hom 0.15 to 0.90 

[NASA-TP-2350] p8 N87-10870 

ACTUATORS 

[ NASA-CP-2423-REV] 

AERODYNAMIC BALANCE 

Po- propella 

AERODYNAMIC CONFIGURATIONS 

designay-analysis codes 

AERODYNAMK: DRAG 

AERODYNAMIC FORCES 

AERODYNAMIC HEATING 

AERODYNAMIC INTERFERENCE 

AERODYNAMIC STABILITY 

Transonic flow analysis for rotors. Part 2: 

Three-dimensional, unsteady, full-potential calculation 

[NASA-TP-2375-PT-2 1 p2 N87-10841 

Flight investigation of the effect of tail configuration on 

stall, spin. and recovery characteristics of a low-wing 

general aviation research airplane 

[NASA-TP-26441 p6 N87-16815 

Flight investigation of the effects of an outboard 

wing-leading-edge modification on stalllspin 

chsracteristics of a low-wing. singleengine, T-tail light 

airplane 

[ NASA-TP-26911 p 6 N87-23614 

AERODYNAMIC STALLING 

AERODYNAMICS 

An experimental investigation of an advanced turtmprop 

installation on a swept wing at subsonic and transonic 

speeds 

[ NASA-TP-27291 p4 N87-26883 

Aeronautical engineering: A continuing bibliography with 

indexes (supplement 217) 

p 1 N87-27613 

In-flight total forces, moments and static aeroelastic 

characteristics of an obliquewing research airplane 

[ NASA-TP-2224) p8 N87-10103 

Engineer in charge: A history of the Langley Aeronautical 

[NASA-SP-7037(217)1 

AEROELASTIC RESEARCH WINGS 

AERONAUTICAL ENGINEERING 

Laboratory, 1917-1958 

[NASA-SP-4305] p27 ~87-24300 

Aeronautical engineering: A continuing bibliography with 

indexes (supplement 217) 

[ NASA-SP-7037(217)] p 1 N87-27613 

Airbome lidar measurements of El Chichon stratospheric 

aerosols, May 1983 

[NASA-RP-l172] p19 N87-11358 

SAGE aerosol measurements. Volume 3: January 1. 

1981 to November 18. 1981 

[NASA-RP-l173] p 19 N87-17417 

Space opportunities for Tropospheric Chemistty 

Research 

[NASA-CP-2450] p 20 N87-18248 

Airborne lidar measurements of El Chichon stratospheric 

aerosols. January 1984 

[NASA-RP-1175] p20 N87-20683 

Effects of aerosols and surface shadowing on 

bidirectional reflectance measurements of deserts 

[NASA-TP-2756] p 19 N87-28162 

Upper and Middle Atmospheric Density Modeling 

Requirements for Spacecraft Design and Operations 

[NASA-CP-2460] p20 N87-20685 

Microgravily Fluid Management Symposium 

[ NASA-CP-24651 p 13 N87-21141 

Spacelab 3 Mission Science Review 

[ NASA-CP-24291 p 15 N87-22103 

Material characterization of superplastically formed 

titanium (TibAI-2Sn-4Zr-2Mo) sheet 

[NASA-TP-2674] p 12 N87-20407 

Aerospace medicine and biology: A cumulative index 

to the 1986 issues (supplement 293) 

[NASA-SP-7011(293)] p 21 N87-18976 

Aerospace medicine and biology: A continuing 

bibliraphy with indexes (supplement 302) 

[NASA-SP-701 l(302)l p22 N87-30041 

NASA scientific and technical publications: A catalog 

of Speaal Publications. Reference Publications, 

Conference Publications. and Technical Papers, 

1977-1 988 [ NASA-SP-70631 p25 N87-30218 

AerothemaI testa of spherical dome protuberam on a flat plate at a Mach number of 6.5 

[ NASA-TP-28311 p14 N87-13864 

Structural Integrity and Curabili of Reusable Space 

Propulsion Systems 

[ NASA-CP-24711 p 11 N87-22768 

AEROSOLS 

AEROSPACE ENVIRONMENTS 

AEROSPACE INDUSTRY 

AEROSPACE MEDICINE 

AEROSPACE SCIENCES 

AEROTHERMODYNAMICS 

A- 1 
AFTERBODIES 

AFTERBODIES 

Effects of empennage Mace location on aerodynamic 

characteristics of a twin-engine afterbody model with 

nonaxisymmetric nozzles 

[NASA-TP-2392] p 6 N87-17693 

Effects of aftelbody boattail design and empennage 

arrangement on aeropropulsive characteristics of a 

twin-engine fighter model at bansonic speeds 

[NASA-TP-27041 p 3 N87-21673 

Simpli curve tits for the thermodynamic properties 

of equilibrium air 

[NASA-RP-1181] p 15 N87-26309 

AIR DATA SYSTEMS 

Qualitative evaluation of a flush air data system at 

transonic speeds and high angles of attack 

[ NASA-TP-27161 p6 N87-29497 

AIR NAVIGATION 

Joint University warn for Air Transportation 

Research. 1983 

[ NASA-CP-24511 p t N87-16520 

AIR POUuTKm 

SAGE aerosol measurements. Volume 3: January 1, 

1981 to November 16,1981 

[NASA-RP-1173] p 19 N87-17417 

Space opportunities for Tropospheric Chemistry 

Research 

[ NASACP-24501 p20 N87-18248 

Airborne lii measurements of El Chiihon stratospheric 

aor09018, January 1984 

[NASA-RP-1175] p20 N87-20663 

Atlas of absorption lines fmm 0 to 17900 cm (sup)-t 

[NASA-RP-1 1681 p 19 N87-28955 

Arctic Sea ice, 1973-1 976 Satellie passivemicrowave 

observations 

[NASA-SP-489] p21 N87-24870 

Groundbased time-guidance algorithm for control of 

auplanes in a timemetered aw traffic control environment: 

A piloted simulation study 

[NASA-TP-2618] p 7 N87-10884 

Joint University Program for Air Transportation 

Research. 1985 

[NASACP-2453] p 1 N87-27596 

Jet transport fliht operations using cockpit display of 

traffic information during instrument meteorological 

conditions: Simulation evaluation 

[NASA-TP-2567] p5 N87-29469 

Joint University Program for Air Transportation 

Research, 1983 

[NASACP-24511 p 1 N87-18520 

Joint University Program for Air Transportation 

Research. 1984 

[ NASA-CP-2452 ] p 1 N87-22804 

Joint University Program for Air Transportation 

Research. 1985 

[ NASA-CP-24531 p 1 N87-27596 

AIRBORNE EOWPMENT 

Airborne li measurements of El Chichon stratospheric 

aerwrols. May lW3 

[NASA-RP-1172) pl9 N87-11358 

Ailtwxne li measurements of El Chichon stratospheric 

ds, January 1984 

[ NASA-RP-11751 p20 N87-20663 

Any respnm to simulated advanced turboprop 

AIR 

AIR SEA ICE INTERACTIONS 

AIR TRAFFIC CONTROL 

AIR TRANSPORTATION 

AIRCRAFT COYPARTYEISTS 

aircraft intenor nome containing tonal beats 

[NASA-TP-2689] p23 N87-24161 

AIRCM COllFtQURATIOWS 

Effects of tail spen and empennage alwgmml on drag of a typkal single-engine fighter aft end 

[NASA-TP-23521 p 1 NB7-10838 

Joint University Program for Air Trmtion 

Research, 1984 

[NASA-CP-2452] p 1 N87-22604 

Applicaljon of parameter estimation to aircraft stability 

andconbol:Theartplt-emxspproach 

[NASA-RP-11681 p6 N87-29499 

In-flight total forces. moments and static aeroelastic 

AIRCRAFT CowTROL 

AIRCRAFTDESIQN 

~ticsof an obliquewinoresearch eftplane 

optimization. pert 1 

[NASA-TP-2224] P8 N87-10103 

Recent EXpmmmS in MuIIWCWinary Analysis and 

[NASACP-2327-PT-l] P5 N87-11717 

Recent ' in MuWplinary Analysis and 

[ NASACP-2327-PT-21 p6 N87-11750 

Engineer in charge: A history of the -ley Aeronautical 

Laboratay. 1917-1958 

[NASASP4305] P27 N87-24390 

QlWaljonT 

SUBJECT INDEX 

ANALOa DATA 

Analog signal conditioning for fliht-test 

instrumentation 

[NASA-RP-i159] p7 N87-29533 

Mach 6 experimental and theoretical stability and 

performance of a cruciform miwle at angles of attack 

up to 65 degrees 

[NASA-TP-27331 P4 N87-23592 

ANQLE OF AlTACK 

Subsonic longitudinal and lateraldirectional 

characteristics of a forward-swept-wing fighter 

configuration at angles of attack up to 47 deg 

Qualitative evaluation of a flush air data system ai 

transonic speeds and high angles of attack 

[NASA-TP-27161 p 6 N67-29497 

Arctic Sea ice, 1973-1976: Satellite passivemicrowave 

Observations 

[ NASA-SP-4891 p 21 N87-24670 

NASA/DOD ControllStructures Interaction Technology. 

Technology for Large Space Systems. A bibliography 

with indexes (supplement 17) 

[ NASA-SP-7046(17)] p9 N87-29576 

Possible complementary cosmic-ray systems: Nuclei 

and antinuclei 

[ NASA-TP-27411 p 24 N87-24977 

ANTIPARTICLES 

Possible complementary cosmic-ray systems: Nuclei 

and antinuclei 

[NASA-TP-2741] p 24 N67-24977 

Predicted effect of dynamic load on pining fatigue life 

for lowcontact-ratio spur 

[NASA-TP-2610] p 16 N87-18095 

Sixth Annual Users' Conference _._ Transportable 

Applications Executive (TAE) 

[ NASA-CP-24631 p 22 N87-23156 

A simulation evaluation of a pilot interface with an 

automatic terminal approach system 

[ NASA-TP-26891 p 7 N87-19393 

On minimmng the number of calculations in 

design-by-analysis codes 

[NASA-TP-2706] p3 N87-23586 

[ NASA-TP-27271 p4 N87-26874 

ANNUAL VARIATIONS 

ANENMAS 

1986 

[NASA-CP-2447-PT-l] p10 N87-16014 

ANTIMATIER 

APPLICATIONS PROaRAMS (COMPUTERS) 

APPROACH CONTROL 

APPROXIMATION 

ARCHITECTURE (COMPUTERS] 

Computer Sciences and Data Systems. volume 1 

[ NASA-CP-2459-VOL-11 p22 N87-19931 

Arctic Sea ice, 1973-1976: Satellite passivemicrowave 

[NASA-SP-489] p21 N87-24870 

Expenmental thrust performance of a hgh-area-ratio 

rocket nozzle 

[NASA-TP-2720] p 10 N87-20381 

ARCTIC REQIONS 

observations 

AREA 

ASTRONOMICAL CATALOOS 

lnlrared source cross-index, first edition 

FW year canon of solar eclipses: 1986 - 2035 

[NASA-RP-11821 p 25 N87-22573 

[NASA-RP-1178-RN] p26 N87-25906 

*oTRoNoyY 

Atlas of Comet Halley 1910 II 

[ NASASP-4BB I p26 N87-30235 

ASTROPHYSICS 

Easays in Space Science 

[NASA-CP-24641 p 25 N87-24247 

ASYMPTOTIC METHODS 

Asymptotic analysis of corona discharge from Win 

electrodes 

[NASA-TP-2645] p24 N67-14998 

ATMOSPHERIC CHEMISTRY 

The Jovian AtmospheceS 

[ NASACP-2441 I p 26 N87-17598 

Space opportunities for Tropospheric Chemistry 

Research 

[NASA-CP-24501 p 20 N87-16248 

ATMOSPHERIC COyPOSlTlON 

Future directions for H sub x 0 sub y detection 

[ NASA-CP-2448 I p 19 N87-15526 

SAGE aerosol measurements. Volume 3: January 1, 

1981 to November 18.1981 

[NASA-RP-11731 p 19 N87-17417 

Space opportunities for Tropospheric Chemistry 

R-ch 

[ NASA-CP-24501 p20 N87-18248 

System study of the carbon dioxide observational 

[NASA-TP-26961 p 9 N87-18588 

platform system (CO-OPS): Projact overview 

AIRCRAFT ENQINES 

Turbine Engine Hot Section Technology. 1984 

[NASA-CP-23391 p 17 N87-11180 

Joint University Program for Air Transportation 

Research. 1983 

[NASACP-2451 I pl N87-18520 

Joint University Program for Air Transportation 

Research, 1984 

AIRCRAFT GUIDANCE 

[ NASA-CP-24521 p 1 N87-22804 

AIRCRAFT HAZIRDS 

Doppler Radar Detection of Wind Shear 

[NASA-CP-24351 p5 N87-10054 

AIRCRAFT LANDING 

Langley Aimafl Landing Dynamics Facili 

[NASA-RP-1189] p9 N87-29544 

Annoyance response to simulated advanced turboprop 

aircraft interia noise containing tonal beats 

[ NASA-TP-26891 p 23 N87-24161 

Wind ShearlTurbulence Inputs to Flight Simulation and 

SystemsCertifiuttion 

[ NASACP-24741 p 1 N87-25267 

A- Turbulence Relative to Aviation. Missile, 

and Space Programs 

[NASACP-2488] p21 N87-22341 

Fliht investigation of the effect of tail configuration MI 

stall, spin, and recovery characteristics of a low-wing 

general aviation research airplane 

[ NASA-TP-26441 p6 N87-16815 

Application of parameter estimation to aircraft stabili 

and control: The outpul-enor approach 

[NASA-RP-11681 p6 N87-29499 

The ACEE program and basic composites research at 

Langley Research Center (1975 to 1986): Summary and 

bibliiraphy 

[NASA-RP-1177] p 11 N87-29612 

Measurements of Row rate and wajecto~~ of aircraft 

tire-generated water spray 

[ NASA-TP-27181 p6 N87-24458 

AIRCRAFT NOISE 

AIRCRAFT PERFORMANCE 

AIRCRAFT SA!TTY 

AIRCRAFT SPIN 

AIRCRAFT STABILITY 

AIRCRAFT STRUCTURES 

AIRCRAFT TIRES 

AIRFOILS 

Turbine Engine Hot Section Technology. 1984 

[NASA-CP-2339] p17 N87-11180 

Lewis inverae deaign code (LINDES): Usersmanual 

Calculation of viws effects on transonic flow for 

oscilating Moils and comparisons with experiment 

[NASA-TP-2731] p5 N87-27622 

Surface bidirectional reflectance properties of two 

southwestern Mona deserts for wavelengths between 

0.4 and 2.2 micrometers 

[ NASA-TP-26431 p 18 N87-22281 

An akpithm for awface smoothing with rational 

Calibration of the spin-scan ozone imager aboard the 

Frontiers of Massively Parallel Scientific Camputation 

Development and evaluation of an airplane electronic 

disphy format aliined with the inertial velodtyvector 

[NASA-TP--1 p 7 N87-13438 

Detailed Row surveys of turning vanes designed for a 

0.1-sULIe model of NASA Lewis Research Center's 

proposed akitude wind tunnel 

[ NASA-TP-26761 p3 N87-20238 

ALBEDO 

ALGORITHMS 

splines 

dynamics Explorer 1 satellite 

[NASA-TP-2708] p23 N87-22447 

[NASA-TP-2723] p21 N87-26491 

[NASA-CP-2478] p22 N87-26531 

AUQNMENT 

ALTITUDE (WMULATIOU 

[NASA-TP-26801 p9 N87-20295 

ALUMINUM 

Shot peening for TMAI4V alloy compressor blades 

COMlic ray heavy ion LET mapping for aluminum. silicon. 

[NASA-TP-2711] p 18 N87-20566 

and tiawe targets 

ALUMINUM ALLOYS 

Ester oxidation on an aluminum surface using 

chemiluminescence 

[NASA-TP-261 1 ] p12 N87-18666 

The cormsion mechanisms for primer coated 221 BT87 

aluminum 

[NASA-TP-2715] p 12 N87-21076 

Effects of thermal cycling on graphiifiber-reinforced 

6081 aluminum 

[NASA-TP-2612] p 11 N87-10184 

[NASA-RP-l180] p27 N87-25984 

ALUMINUM QRAPHITE CouPomES 

A-2 
SUBJECT INDEX 

ATMOSPHERIC DENSITY 

Upper and Middle Atmospheric Density Modeling 

Requirements for spaceaan Design and Operations [NASA-CP-2460] p20 N87-20865 

NASAIMSFC FY85 Amrodpheric Processes Research 

Review 

[NASA-CP-2402] p 20 N87-13043 

Upper and Middle Atmospheric Density Modeling 

~equirements for spacecran Design and Opera- 

[NASA-CP-2460] p20 N87-20865 

Atmospheric ' Turtulence Relative to Aviation. Mile, 

and Space Programs 

[ NASA-CP-24681 p 21 N87-22341 

NASAIMSFC FY-85 AtmOsphenc Recesses R-ch 

Review 

[ NASACP-24021 p 20 N87-13043 

Atmospheric . Turbrlence Relative to Aviation, Mile. 

[ NASACP-24681 p 21 N87-22341 

Electron stimulated desorption of atomic oxygen from 

silver 

[NASA-TP-2868] p12 N87-18629 

A simulation evaluation of a pilot interiace with an automatic terminal approach system 

[ NASA-TP-26691 p 7 N87-19393 

Piloted simulation study of the effects of an automated 

trim system on fliht characteristics of a liht twinagine 

airplane with one engine inoperative 

[ NASA-TP-26331 p2 N87-10843 

A simulation evaluation of a pilot interface with an 

automatic terminal approach system 

[ NASA-TP-26691 p7 N87-19393 

Joint University prosram for Air Transportation 

Research. 1983 

[NASA-CP-2451] p 1 N87-18520 

Joint University Program for Air TransportatiMl 

Research, t984 

[ NASA-CP-2452) p 1 N87-22604 

Wind ShearlTurtuulence Inputs to Fhght Simulation and 

Systems certification 

[NASA-CP-2474] p 1 N87-25267 

AXISYMMETRIC BODIES 

Static intemal performance of singleexpsnsion-ramp 

[ NASA-TP-23641 p 2 N87-10839 

Effects of empennage surface location on aerodynamic 

characteristics of a twin%ngine afterbody model with 

ronadsymmebic nonles 

[ NASA-TP-23921 p6 N87-17693 

Revised NASA axially symmebic ring model for 

coupled-cavity travelingwave tubes 

[NASA-TP-2675] p 14 N87-22923 

Effect of a trade belween boattail angle and wedge size 

on the performance of a ronadsymmebic wedge nozzle 

[NASA-TP-2717] p4 N87-23593 

Effects of aftwbcdy boattail dwgn and empennage 

arrangement on aeropropulsive characteristics of a 

twin-engine !ighter model at trammic speeds 

[NASA-TP-2704] p 3 N87-21873 

ATYOSPHERIC ELECTRICITY 

ATMOSPHERIC MODELS 

ATYOSPHERIC SOUNDINQ 

ATYOSPHERIC TURBULENCE 

andSpeceRograms 

ATOMIC BEAMS 

AUTOMATIC CONTROL 

AUTOMATIC FLIQHT CONTROL 

AUTOMATIC PILOTS 

AVIONICS 

noales m nlNEt-- capaway up to 60 dag 

AXISYMMETRIC FLOW 

CINEMATOGRAPHY 

B 

BACKGROUND NOISE 

Effects of backgrwnd noise on total noise annoyance [NASA-TP-2830] p23 N87-14120 

Aerospace medicine and biology: A cumulative index 

to the 1986 igsues (supplement 293) 

[ NASA-SP-7011(293)] p21 N87-18976 

Management: A bibliography for NASA managers 

(supplement 21) [NASA-SP-7500(21)] p24 N87-20833 

NASA patent abstracts bibliography: A continuing 

bibliography. Section 1: Abstmts (supplement 31) 

[ NASA-SP-7039(31)] p24 N87-25023 

Space station systerna: A bibliiaphy with indexes 

(supplement 4) 

[ NASASP-7056(04)] p 10 N87-28073 

NASA patent abstracts bibliography: A continuing 

bibliography. Section 2: indexes (supplement 31) 

[NASA-SP-7039(31 )SECT-O] p24 N87-28689 

Earth reswrces: A continuing bibliiaphy with indexes 

(issue 54) 

[ NASA-SP-7041(54)] p 18 N87-27315 

BIBUOQRAPHIES 

Aeronautical engineering: A continuing bibliography with 

indexes (supplement 217) 

[ NASASP-7037(217)1 p 1 N87-27613 

Technology for Large space Systems. A bibliography 

with indexes (supplement 17) 

[NASASP-7046(17)1 p9 N87-29576 

Aerospace medicine and biology: A continuing 

bibliography with indexes (supplement 302) 

[ NASASP-7011(302)] p22 N87-30041 

Surface bidirectional reflectance properties of two southwestem A~izona deserts for wavelengths between 

0.4 and 2.2 micrometers 

[ NASA-TP-26431 p 18 N87-22281 

Effects of aerosols and surface shadowing on 

bidirectional reflectance wrements of deserts 

[ NASA-TP-27561 p 19 N87-28162 

Aerospace medicine and biology: A cumulative index 

[ NASA-SP-701 l(293)l p 21 N87-18976 

Aerospace medii and biology: A continuing 

bibliaphy with indexes (supplement 302) 

[ NASA-SP-701t(302)] p22 N87-30041 

Bi-errcf-rate testing of highpower 30-GHZ traveling 

wave tubes for ground-terminal applications 

[ NASA-TP-26351 p 13 N87-17971 

Unique bit-error-rate measurement system for satellite 

communication syatems 

[ NASA-TP-26991 p 13 N87-20448 

Codation of helioopter impulsive noise from 

bladevortex interaction with rotor mean inflow 

[NASA-TP-2650] p 23 N87-18399 

Lowcost FM oscillatw for capacitance type of blade 

tip clearance measurement system 

[ NASA-TP-27461 p7 N87-24481 

helation of heriier impulsive noise from 

bladevortex interacth with rotor mean inflow 

[ NASA-TP-26501 p 23 N87-18399 

Helii blade-vortex interactiOn locations: 

Scaknodel acou8th and free-wake analysisresuns 

[ NASA-TP-26581 p3 N87-18537 

Preliminary sbuctural design of composite main rotor 

[NASA-TP-2730] p 11 N87-25435 

Drag meawemmts of blunt stores tangentially mounted 

on a flat plate at svpersonic speeds 

[NAsA-TP-2742] p5 N87-27826 

Effects of afterbody boattail design and empennage 

mangement on aeropropulsive characteristics of a 

twin-engina fighter rodel at transonic speeds 

[NASA-TP-2704] p3 N87-21873 

Effect of a trade between boattail angle and %'mi@ size 

on the performance of a nonaxisymmebic wedge nozzle 

[ NASA-TP-27t 71 p4 N87-23593 

Theory for computing the field scattered from a smooth 

infiected surface 

[ NASA-TP-26321 p24 N87-13264 

A wwnd+&r accurate kinetic-theocy-based method 

p 15 N87-18783 

Effect of LID (Registered) processing on the 

microstructureandmechenicalpropertiesofT~Vand 

TiI-ZSn-4Zr-ZMo titanium foilgauge materials 

[ NASA-TP-26771 p12 N87-18644 

In-fliht surface oil-Row Photographs with comparisons 

to pressure distribution and boundary-layer data 

[ NASA-TP-23951 p3 N87-20966 

NU- simulation of channel flow transition, 

resolution requirements and structure of the hairpin 

vortex p3 N87-19351 [ NASA-TP-2667 I 

Numeical sinwrlab!l Of channel flow transition. 

resolution requirements and structure of the hairpin 

vortex 

[NASA-TP-2667] p3 N87-19351 

Aerothennal evaluation of a spherically blunted body 

with a trapezoidal CYOS eectiOn in the Lanelev %foot 

huh-temperature tunnel 

[ NASA-TP-2841 I p 15 N87-18782 

BIDIRECTIONAL REFLECTANCE 

BIOLOQICAL EFFECTS 

to the 1986 issues (supphlent 293) 

BIT ERROR RATE 

BLADE SLAP NOISE 

BLAD€ TIPS 

BLADE-VORTEX INTERACTION 

BLADES 

MadesforminimUnweigM 

BLUNT BODIES 

BOATTAILS 

BODIES OF REVOLUTION 

BOLTZMA" TRANSPORT EQUATION 

for inviscid compressible flows 

[ NASA-TP-26131 

BONDING 

BOUNDARY LAYER FLOW 

BOUNDARY LAYER ST*BIU?Y 

BOUNDARY LAYER TRANSITION 

BOUNDARY LAYERS 

BOUNDARYVALUEPROBLEMS 

Numerical simulation of channel flow transition, 

resolution requirements and structure of the hairpin 

vortex 

[ NASA-TP-26671 p3 N87-19351 

BRAKINQ 

Wind-tunnel investigation et supersonic speeds of a 

remote-controlled canard missile with a free-rollina-tail 

brake torque system 

[ NASA-TP-2401 I p 3 N87-17668 

C 

CALIBRATING 

Calibration of the spin-scan ozone imager aboard the 

dynamics Explorer 1 satellite 

[ NASA-TP-27231 p 21 N87-26491 

Description and calibration of the Langley Hypersonic 

CF4 tunnel: A facility for simulating low gamma flow as occurs fw a real gas 

[ NASA-TP-23841 p 16 N87-29778 

Pressure measurements on a thick cambered and 

twisted 58 deg delta wing at hih subsonic speeds 

[ NASA-TP-2713 I p5 N87-27643 

Supersonic, nonlinear, attached-flow wing design fw 

high lift with experimental validation 

[ NASA-TP-2336) pl N87-10042 

Wind-tunnel investigation of the fliht Characteristics of 

a canard general-aviation airplane configuration 

[NASA-TP-2623] p 1 N87-10039 

Wind-tunnel investigation at supersonic speeds of a 

remote-controlled canard missile with a free-rolling-tail 

brake toque system 

[NASA-TP-2401 I p 3 N87-17668 

Traveling-wave-tube efficiency improvement by a 

lowcost technique for deposition of carbon on multistage 

CAMBER 

CAMBERED WlNQS 

CANARD CONFIQURATIONS 

CARBON 

depressed collector 

[NASA-TP-2719] p 14 N87-21239 

CARBON DIOXIDE 

System study of the carbon dioxide obaeraW 

platform system (CO-OPS): Project oveNiew 

[ NASA-TP-26961 p9 N87-18588 

CARBON DIOXIDE USERS 

Closed-Cycle. Frequency-Stable CO2 Laser 

Technology 

[ NASA-CP-24561 p 16 N87-20522 

CARBON FIBERS 

Effects of thermal cycling on graph-fiber-reinforced 

6061 aluminum 

[ NASA-TP-26121 pll N87-10184 

Description and calibration of the Langley Hypersonic 

CF4 tunnel: A facility for simulating low gamma flow as occurs for a real gas 

[ NASA-TP-23841 p 16 N87-29778 

NASA scientific and technical publications: A catalog 

of Special Publiitione, Reference Publiications. 

Conference Publications. and Technical Papers. 

1977-1986 

[NASA-SP-7083] p 25 N87-30218 

Space shuttle main engine hih pressure fuel pump aft 

platform seal cavity Row analyw 

[ NASA-TP-26851 p 14 N87-17MX) 

Experimental cavity pressure distributions at supersonic 

G-TP-26831 p3 N87-22626 

Revised NASA axially symmetric ring model fOr 

cwpleduwitV traveling-wave tubea 

[ NASA-TP-26751 p 14 N87-22923 

[NASA-RP-l17&REVl p26 N87-259% 

Pow cepsbum technique with app4ication to model 

CARBON TETRAFLUORIDE 

CATALOOS (WBLKATIDNS) 

cAvrnEs 

CELESTIAL MECHANICS 

Finy year UUWM of sdar dipsea: 1986 - 2035 

CEPSTRAL ANALYSIS 

heliter acoustic data 

[ NASA-TP-25861 p 23 N87-17479 

CHANNEL FLOW 

Numerical simulation of channel flow transition. 

resolution requirements and structure of the hairpin 

vortex 

[ NASA-TP-28671 p3 N87-19351 

CHEMILUMINESCENCE 

chemiluminescence 

[ NASA-TP-2611 I 

CINEMATDQRAPHY 

Ester oxidation on an aluminum surface using 

p12 N87-18666 

Evaluation of diffuseillumination holographic 

cinematography in a flutter cascade 

[ NASA-TP-25931 p 16 N87-13731 

A-3 
CIRCULAR CYLINDERS SUBJECT INDEX 

Joint University Program for Air Transportation 

Research. 1983 

[NASA-CP-2451 I p 1 N87-18520 

Energetic Phenomena on the Sun: The Solar Maximum 

Mission Flare Workshop. Proceedings 

[NASA-CP-2439] p 26 N87-19328 

Computer Saences and Data Systems. volume 1 

INASA-CP-2459-VOL-11 p 22 N87-19931 

Computer Sciences and Data Systems, volume 2 

[NASA-CP-2459-VOL-2] p 22 N87-19932 

The 1986 Get Away Special Experimenter’s 

Symposium 

[NASA-CP-24381 p9 N87-20302 

Coronal and Prominence Plasmas 

[NASA-CP-2442] p 26 N87-20871 

Mirogravity Fluid Management Symposium 

[NASA-CP-2465] p 13 N87-21141 

Rapid Fluctuations in Solar Flares 

[NASA-CP-2449] p 27 N87-21785 

Atmospheric Turbulence Relath to Aviation, Missile, 

and Space Programs 

[ NASA-CP-24681 p 21 N87-22341 

Structural Dynamics and Control Interaction of Flexible 

Structures 

[NASA-CP-2467-PT-2] p 10 N87-22729 

Structural Integrity and Durability of Reusable Space 

Propulsion Systems 

[NASA-CP-2471] p 11 N87-22766 

Si Annual Users’ Conference _-. Transportable 

Applications Executive (TAE) 

[NASA-CP-2463] p 22 N87-23156 

Double Layers in Astrophysics 

[NASA-CP-2469] p 25 N87-23313 

Essays in Space Science 

[NASA-CP-2464] p 25 N87-24247 

Star Formation in Galaxies 

[NASA-CP-2466] p26 N87-24266 

Supercomputing in Aerospace 

[NASA-CP-2454] p4 N87-25998 

Space Photovoltaic Research and Technology 1986. 

High Efficiency, Space Environment. and Array 

Technology 

[NASA-CP-2475] p 19 N87-28413 

Fifteenth NASTRAN Users’ Colloquium 

[NASA-CP-2481] p t8 N87-27231 

Joint University Program for Air Transportation 

Research, 1985 

[NASA-CP-2453] p 1 N87-27596 

NASA 8CienWic and technical publications: A catalog 

of Special Publications. Reference Publications, 

Conference Publications, and Technical Papers. 

1977-1986 

[NASA-SP-7063] p 25 N87-30218 

Development of confidence limits by pivotal functions 

p23 N87-23244 

Study of leeside flows over conically cambered delta 

wings at supersonic speeds, part 1 

[NASA-TP-2860-PT-l] p4 N87-23597 

Study of lee-side flows over conically cambered Delta 

wings at supersonic speeds. part 2 

CONFIDENCE LIMITS 

for estimating software reliability 

[ NASA-TP-27091 

CONICAL CAMBER 

[ NASA-TP-2660-PT-21 P4 N87-25301 

CONTOURS 

Atlas of wide-fieldof-view OotgOing longwave radiation 

derived from Nimbus 6 Earth radiation budget data set. 

July 1975 to June 1978 

[NASA-RP-l185] p21 N87-26489 

NASAIDOD ControllStructures Interaction Technology, 

CONTROL STABILITY 

1986 

[NASA-CP-2447-PT-2] p 10 N87-24495 

CONTROL SYSTEMS DESIGN 

Piloted simulator study of allowable time delays in 

large-airplane response 

[ NASA-TP-26521 p8 N87-16849 

Structural Dynamics and Control lnte~action of Flexible 

Structures 

[ NASA-CP-2467-PT-11 P 10 N87-22702 

Modeling digital control systems with MA-prefiltered 

measurements 

[ NASA-TP-27321 P 13 N87-22870 

NASAlDOD ControllStructurea Interaction Technology, 

1% 

[ NASA-CP-2447-PT-21 p 10 N87-24495 

A new approach to state estimation in deterministic 

duital control systems 

[ NASA-TP-27451 p 13 N87-24585 

CONTROL THEORY 

Joint University Program for Air Transportation 

Research, 1984 

[NASACP-24521 p 1 N87-22804 

CIRCULAR CYLINDERS 

Application of turbolence modeling to predict surface 

heat transfer in stagnation flow region of circular cylinder 

[ NASA-TP-27581 p 15 N87-27161 

Large-scale static investigation of 

circulationcontrol-wing concepts applied to upper 

surfaceblowing aircratt 

[NASA-TP-2684] p6 N87-15959 

Five year global dataset: NMC operational analyses 

(1978 to 1982) 

[NASA-RP-1194] p21 N87-29996 

CLOSED CYCLES 

Closed-Cycle, Frequency-Stable CO2 Laser 

Technology 

[NASA-CP-2456] p 16 N87-20522 

CIRCULATION CONTROL AIRFOILS 

CLIMATE 

CLOUDS (METEOROLOGY) 

The Jovian Atmospheres 

[ NASA-CP-24411 p 26 N87-17598 

Development testing of large volume water sprays for 

warn fog dispersal 

[NASA-TP-2607] p10 N87-12585 

Investigation of the effects of cobalt ions on epoxy 

[ NASA-TP-2B391 p12 N87-12680 

Jet transport fliht operations using cockpit display of 

traffic information during instrument meteorological 

conditions: Simulation evaluation 

[NASA-TP-25671 p 5 N87-29469 

Pulse Code Modulation (PCM) enoodec handbodc for 

Aydin Vector MMPdOO series system 

[NASA-RP-l171] p 13 N87-11916 

Lewis invecse design code (LINDES): Usersmanual 

[ NASA-TP-26761 p 3 N87-20238 

Experiments in encoding multilevel images as 

[ NASA-TP-27221 p 23 N87-28367 

Doubly differential cross sections for galactic heavy-ion 

COALEXING 

COBALT 

propecties 

COCKPIT SIMULATORS 

CODING 

quadbees 

COLLISION PARAMETERS 

fragmentation 

[NASA-TP-2659] p24 N87-17487 

COMBUSllBLE FLOW 

Automated Reduction of Data from Images and 

Holograms 

[NASA-CP-24771 p 5 N87-29432 

COMBUSTION 

NASA-Chinese Aeronautical Establishment (CAE) 

Symposium 

[NASA-CP-2433] p7 N87-20267 

Conventionally cast and forged copper alloy for 

hgh-heat-flux thrust chambers 

[NASA-TP-2694] p12 N87-16902 

COMBUSTION CHAMBERS 

COMET HEADS 

Atlas of Comet Halley 1910 II 

[NASA-SP-488] p26 N87-30235 

COMET NUCLEI 

Atlas of Comet Halley 1910 II 

[NASA-SP-488] p26 N87-30235 

COMET TAILS 

Atlas of Comet Halley 1910 I1 

[NASA-SP-488] p26 N87-30235 

Unique bl-enor-rate measurement system for satellie 

communication systems 

[ NASA-TP-26991 p13 N87-20448 

Calculation of viscous effects on transonic flow for 

oscillating airfoils and comparisons with experiment 

[NASA-TP-2731] p5 N87-27622 

Electronics reliability and measurement technology 

[NASACP-2472] P 17 N87-27204 

Preliminary structural deaign of wmposite main rotor 

blades tor minimm weight 

[NASA-TP-2730] P 11 N87-25435 

COMpoSm STRUCTURES 

The ACEE program and basic composites research at 

Langley Research Center (1975 to lW): Summary and 

[NASA-RP-lt77] P 11 N87-29612 

COMMUNlCATKm NETWORKS 

COMPARISON 

COMPONENT RELIABILITY 

COMpoSm MATERIALS 

~ographv 

COMPRESSOR BLADES 

Shot peening for T-EAI-4V alky mmpeasor blades 

[ NASA-TP-27111 pl8 N87-20566 

Designof 9.27l-pr~e-ra~Ss~c~ecompr~ 

and overall performance for first 3 ataw 

[ NASA-TP-25971 p7 N87-17899 

COYPRESSORS 

A-4 

COMPUTATION 

Calculation and accuracy of ERBE scanner 

measurement locations 

[NASA-TP-2670] p25 N87-28471 

COMPUTATIONAL ASTROPHYSICS 

Supercomputing in Aerospace 

[ NASA-CP-24541 p4 N87-25998 

COMPUTATIONAL CHEMISTRY 

Supercomputing in Aerospace 

COMPUTATIONAL FLUID DYNAMICS 

[NASA-CP-2454] p4 N87-25998 

Combined aerodynamic and structural dynamic problem 

emulating routines (CASPER): Theory and 

implementation 

[ NASA-TP-24181 p 3 N87-17669 

Numerical simulation of channel flow transition, 

resolution requirements and structure of the hairpin 

vortex 

[ NASA-TP-26671 p3 N87-19351 

[NASA-CP-2454] p4 N87-25998 

Supercomputing in Aerospace 

Simplified curve fits for the thermodynamic propertii 

of equilibrium air 

[NASA-RP-1181] p 15 N87-26309 

COMPUTATIONAL GRIDS 

Supercomputing in Aerospace 

[ NASA-CP-24541 p4 N87-25998 

Recent Experiences in Multidisciplinary Analysis and 

Optimization, part 1 

[NASA-CP-2327-PT-l I p5 N87-11717 

Recent Expenences in Multidisciplinary Analysis and 

Optimization. part 2 

[NASACP-Z3277-PT-2] p 6 N87-11750 

Fifteenth NASTRAN Users’ Colloquium 

[NASACP-2481] p 18 N87-27231 

Frontiers of Massively Parallel Scientific Computation 

[NASA-CP-2478] p22 N87-26531 

Proceedings of the 5th Annual Users’ Conference 

COMPUTER AIDED DESIGN 

COMPUTER GRAPHICS 

COMPUTER NETWORKS 

[ NASA-CP-23991 P22 N87-10720 

COMPUTER PROGRAMMING 

Some path-following techniques for solution of nonlinear 

equations and comparison with parameVic differentiation 

[ NASA-TP-26541 p 22 N87-14054 

Frontiers of Massively Parallel Scientific Computation 

Sixth Annual Users’ Conference --- Tranqmtable 

Applications Executive (TAE) 

[ NASA-CP-24631 p 22 N87-23156 

COMPUTER SYSTEMS PERFORMANCE 

[NASA-CP-24781 P 22 N87-26531 

COMPUTER SYSTEMS PROQRAMS 

COMPUTER TECHNIQUES 

Fifteenth NASTRAN Users’ Colloquium 

[NASA-CP-2481] p 18 N87-27231 

Combined aerodynamic and structural dynamic problem 

emulating routines (CASPER): Theory and 

implementation 

[ NASA-TP-24181 p3 N87-17669 

Tether Dynamics Simulation 

[NASA-CP-2458] p 16 N87-18821 

Supercomputing in Aerospace 

[NASA-CP-2454] p4 N87-25998 

Frontiers of Massively Parallel Scientific Computation 

[ NASACP-24781 p22 N87-26531 

A teGhnigoe for evaluating the application of the pin-level 

stuckat fault rodel to VLSl circuits 

[ NASA-TP-27381 p 17 N87-28025 

COMPUTERIZED SIMULATION 

COMPUTERS 

CONCURRENT PROCESSING 

Computer Sdences and Data Systems. volume 1 

Doppler Radar Detection of Wind Shear 

Thirteenth International Laser Radar Conference 

[NASA-CP-2459-VOL-l] p 22 N87-1993 t 

CONFERENCES 

[ NASA-CP-24351 p5 N87-10054 

[NASA-CP-2431] p 16 N87-10263 

The 1985 Goddard Space Fliht Center Battery 

[ NASA-CP-24341 p 14 N87-11072 

Turbine Engine Hot Section Technology. 1984 

NASA-CP-23391 p 17 N87-11180 

Recent Experiences in Multidisciplinary Analysis and 

Optimization, part 1 

[NASA-CP-Z327-PT-1] p5 N87-11717 

NASAlDOD ControllStructures Interaction Technology, 

1986 

[NASA-CP-2447-PT-1] p 10 N87-16014 

The 20th Aerospace Mechanii Symposium 

NASA-CP-Z423-REV] p 17 N87-16321 

opportunities for Tropospheric Chemistry 

Research 

[NASA-CP-2450] p20 N87-18248 

WMshop 
SUBJECT INDEX DYNAMIC STRUCTURAL ANALYSIS 

CONTROLUBlLlTY 

Piloted-simulation study of effects of vortex flaps on 

low-speed handling qualities of a Delta-wing airplane 

[NASA-TP-27471 p8 N87-26922 

Static internal performance of a two-dimensional 

cowergentdivergent nozzle with thrust vectoring [NASA-TP-2721] p4 N87-24432 

Traveling-wave-tube efficiency improvement by a 

lowast technique for deposition of carbon on multistage 

depressed collector 

[ NASA-TP-27191 p 14 N87-21239 

Conventionally cast and forged copper alloy for 

[ NASA-TP-26941 p12 N87-16902 

Effect of port mmer geometry on the internal 

performance of a rotating-vane-type thrust reverser [ NASA-TP-26241 p2 N87-12541 

Experimental evaluation of two tuming vane designs for 

fan drive corner of 0.1-scale model of NASA Lewis 

Research Center's proposed altitude wind tunnel 

[NASA-TP-Z646] p8 N87-18576 

The conosion mechanisms for primer coated 2219T87 

aluminum 

[ NASA-TP-27151 p 12 N87-21076 

[NASA-CP-2464] p 25 N87-24247 

Revised NASA axially symmetric ring model for 

cuupled-cavity traveling-wave tubes 

[ NASA-TP-28751 p 14 N87-22923 

Some path-following techniques for solution of nonlinear 

equations and comparison with parametric dfterentiation 

[ NASA-TP-26541 p22 N87-14054 

Mach 6 experimental and theoretical stability and 

performance of a uuciform missile at angles of attack 

up to 65 degrees 

[ NASA-TP-27331 p4 N87-23592 

Evolution. calibration, and operational charactecistics of 

the two-dimensional test section of the Langley 0.bmeter 

transonic cryogenic tunnel 

[ NASA-TP-27491 p9 N87-28570 

Liquid drop stabili for protein crystal grh in 

minogravity 

[ NASA-TP-27241 p 21 N87-20727 

Hydrogen trapping and the interaction of hydrogen with 

metals 

[NASA-TP-2744] p 12 N87-25463 

Performance of textured carbon on ccpper electrode 

multistage depressed collectors with mediumpuuer 

traveling wave tubes 

[NASA-TP-Z665] p 14 N87-17990 

CONVERGENT-DIVERGENT NOPLES 

COPPER 

COPPER ALLOYS 

high-heat-flux thrust chambers 

CORNER FLOW 

CORROSION RESISTANCE 

COSMIC RAYS 

Essays in Space Science 

COUPLED MODES 

CRITICAL PATH METHOD 

CRUCIFORM WINGS 

CRYOGENIC WIND TUNNELS 

CRYSTAL GROWTH 

CRYSTAL LAmCES 

CURRENT DENSITY 

CURVE FITTING 

SimplMd curve fils for the thwmdymw ' prw 

of equilibrium air 

[NASA-RP-1 t 81 ] p 15 N87-26309 

CYCLOHEXANE 

Velocity profiles in laminar dftusion flames 

[ NASA-TP-25961 p 15 N87-18035 

Straight cylindrical seal for high-performance 

turbomachines 

[NASA-TP-1850] p 15 N87-23936 

CYLINDRICAL BODIES 

D 

DATA Acauismw 

Analog signal conditioning for flight-test 

insburnentalion 

[NASA-RP-1159] p7 N87-29533 

Five year global dataset NMC operational analyses 

(1978 to 1982) 

[NASA-RP-l194] p 21 N87-29996 

Experiments in encoding multilevel images as quadtrees 

[ NASA-TP-27221 pZ3 N87-28367 

DATA COMPRESSION 

DATA MANAGEMENT 

Computer Sciences and Data Systems, vdume 1 

Pulse Code Modulalion (PCM) data StOWe and 

[NASAGP-2459-VOL-l I p22 N87-19931 

DATA PROCESSlNQ 

using a microcomputer 

[NASA-TP-2629] p 13 N87-12718 

NASAlMSFC FY-85 Atmospheric Processes Research 

Review 

[ NASA-CP-24021 p 20 N87-13043 

Earth resources: A continuing bibliography with indexes 

(issue 54) 

p 18 N87-27315 

Pulse Code Modulation (PCM) data storage and analysis 

using a miaocomputer 

[NASA-TP-2629] p 13 N87-12718 

A synchronous data analyzer for the Minimum Delay 

Data Format (MDDF) and Launch Trajectory Acquisition 

System (LTAS) 

[ NASA-TP-27431 p13 N87-24590 

DATA STORAGE 

Pulse code Modulation (PCM) data storage and analysis 

using a microcomputer 

[ NASA-TP-26291 p 13 N87-12718 

Computer Sciences and Data Systems, volume 2 

[ NASA-CP-2459-VOL-21 p 22 N87-19932 

Experiments in encoding multilevel images as 

quadtrees 

[ NASA-TP-27221 p 23 N87-28367 

DELTA WINGS 

Investigation of leading-ejge flap performance on delta 

and douMedelta wings at supersonic speeds 

[NASA-TP-26561 p3 N87-20233 

Study of lee-side flows over conically cambered delta 

wings at supersonic speeds, part 1 

[ NASA-TP-2660-PT-11 p4 N87-23597 

Study of leeside flows over conically cambered Delta 

wings at supersonic speeds. part2 

[NASA-TP-2660-PT-2] p4 N87-25301 

Piloted-simulation study of effects of vortex flaps on 

low-speed handling qualis of a Delta-wingairplane 

[ NASA-TP-27471 p8 N87-26922 

Pressure measurements on a thick cambered and 

twisted 58 deg delta wing at high subsonic speeds 

[NASA-TP-2713] p5 N87-27643 

[NASA-SP-7041(54)1 

DATA REDUCTION 

DEPLOYMENT 

The 21 st Aerospace Mechanisms Symposium 

[ NASA-CP-24701 p 18 N87-29858 

Traveling-wave-tube efficiency improvement by a 

lowcwlt technique for deposition of carbon on multistage 

depreseed collector 

[NASA-TP-27191 p 14 N87-21239 

Surface bidirectional reflectance properties of two 

southwegtem Amona dewis for wavelems between 

0.4 and 2.2 miuometws 

[ NASA-TP-26431 p 18 N87-22281 

Em ofaercds and surface shadowing on 

bidirectional reflectance measurements of deserts 

[ NASA-TP-27561 p 19 N87-28182 

Recent Experiences in Multiiisciplitmy Analysis and 

Optimization. part 1 

[NASA-CP-2327-PT-l] p5 N87-11717 

Applili of lineae&-theory attached-flow methods 

to design and analysis of flap systems at low speeds for 

thin swept wings with sharp leading edges 

[ NASA-TP-26531 p2 N87-15174 

Design of 9.271 -pressureratio 5-stage core compressor 

and werall performance lor first 3 stages 

[ NASA-TP-25971 p7 N87-17899 

Le& inverse design code (LINDES): Usenmanual 

[ NASA-TP-26761 p3 N87-20238 

Design, fabrication and performance of small, graphite 

electrode, multistage depressed collectors with 200-W. 

CW, S to 18-GHz traveling-wave tubes 

[ NASA-TP-26931 p 14 N87-20474 

Structural Ovnamrr, and Control Interaction of Flexible 

Structures 

[ NASA-CP-2467-PT-21 p 10 N87-22729 

00 minimizing Me number of calculations in 

[ NASA-TP-27061 p3 N87-23588 

Electron stimulated desorption of atomic oxygen from 

silver 

[NASA-TP-26681 p 12 N87-18829 

Some path-following techniques for solution of nonlinear 

eguations and cornperison with parametric ditferentiation 

[ NASA-TP-2654 1 p22 N87-14054 

Effect of LID (Registeradl processing on the 

microsbucture and mechanical properties of Ti-6AI-W and 

K6AI-2Sn-4Zr-2Mo titanium foilgauge materials 

[ NASA-TP-26771 p12 N87-18644 

DEPOSmON 

DESERTS 

DESIGN ANALYSIS 

~navgnalyslScOdes 

DESORPTION 

DIFFERENTIAL EQUATIONS 

DIFFUSION 

DIFFUSION FUNES 

velocity profiles in laminar diffusion flames 

[ NASA-TP-25961 p 15 N87-18035 

DIGITAL COMMAND SYSTEMS 

Exact state reconstruction in deterministic digital control 

systems 

[ NASA-TP-27571 p 13 N87-27067 

DIGITAL FILTERS 

Modeling digital control systems with MA-prefiltered 

measurements 

[NASA-TP-27321 p 13 N87-22870 

DIGITAL SYSTEMS 

Modeling digital control systems with MA-prefiltered 

measurements 

[ NASA-TP-27321 p 13 N87-22870 

A new approach to state estimation in deterministic 

digital control systems 

[NASA-TP-27451 p 13 N87-24585 

DIGITAL TECHNlaUES 

Automated Reduction of Data from Images and 

Holograms 

[NASA-CP-2477] p5 N87-29432 

Development and evaluation of an airplane electronic 

display format aligned with the inertial velocityvector 

[NASA-TP-26481 p7 N87-13438 

Surface bidirectional reflectance properties of two 

southwestern Arizona de- for wavelengths between 

0.4 and 2.2 micrometers 

[NASA-TP-2643] p 18 N87-22281 

Development and evaluation of an airplane electronic 

display format aligned with the inertial velocity vector 

[ NASA-TP-26481 p 7 N87-13438 

Jet transpwt flight operations using cockpit display Of 

traffic information during instrument meteorological 

condiins: Simulation evaluation 

[NASA-TP-2567] p5 N87-29489 

p 22 N87-19931 

p22 N87-19932 

NASA scientific and technical publications: A catalog 

of Special Publications. Reference Publications. 

Conference Publications, and Technical Papers. 

1977-1986 

[ NASA-SP-70631 p 25 N87-30218 

Frequency domain laser velocimeter signal processor: 

A new signal processing scheme 

[NASA-TP-2735] p 16 N87-27994 

DIRECTIONAL CONTROL 

DIRECTIVITY 

DISPLAY DEVICES 

DISTRIBUTED PROCESSING 

Computer Sciences and Data Systems, volume 1 

Computer Sciences and Data Systems, volume 2 

[NASA-CP-2459-VOL-l] 

[ NASA-CP-2459-VOL-21 

DOCUMENTATION 

DOMAINS 

DOPPLER RADAR 

Doppler Radar Detection of Wind Shear 

[ NASA-CP-2435) p 5 N87-10054 

NASAlMSFC FY-85 Atmospheric Procaa3es Research 

Review 

[NASA-CP-2402] p20 N87-13043 

Effects of afterbody boanail design and empennage 

arrangement on aeropropulsive characteristics of a 

twin-engim, fighter model at transonic speeds 

[ NASA-TP-27041 p 3 N87-21873 

Summary of studies to reduce wingmounted Wan 

installation drag on an M = 0.8 transport 

[ NASA-TP-26781 p6 N87-20990 

Liquid drop stability for protein crystal growth in 

microgravity 

[ NASA-TP-27241 p21 N87-20727 

DURABILITY 

Spectroscopic comparison of effects of electron 

radiation on mechanical prop-s of two polyimides 

[NASA-TP-2863] pll N87-18811 

Structural Integrity and Durability of Reusable Space 

Propulsion Systems 

[ NASA-CP-24711 p 11 N87-22766 

Effects of aerosols and surface shadowing on 

bidirectional reflectance measurements of deserts 

[NASA-TP-27561 p 19 N87-28162 

Predicted effect of dynamic load on pitting fatigue lae 

for lowcontact-ratio spw gears 

[NASA-TP-2610] p 16 N87-18085 

Langley Aircraft Landing Dynamics Facility 

[NASA-RP-11891 p9 N87-29544 

Threestep cylindrical seal for high-performance 

turbomachines 

DRAG 

DRAG REDUCTION 

DROPS (uauiw) 

DUST 

DYNAMIC LOADS 

DYNAMIC STABILITY 

[ NASA-TP-18491 p 15 N87-24639 

DYNAMIC STRUCTURAL ANALYSIS 

Combined aerodynamic and structural dynamic poblem 

emulating routines (CASPER): Theory and 

implementation 

[NASA-TP-2418] p 3 N87-17889 

A-5 
DYNAMIC TESTS SUBJECT INDEX 

ENGINE TESTS 

Comparison of thewetical and experimental thrust 

performance of a 10301 area ratio rocket nozzle at a 

chamber pressure d 2413 kNlm2 (350 psia) 

[NASA-TP-2725] p 11 N87-25423 

On the Maxwellian distribution, symmetric form, and 

entrw conservation for the Euler equations 

[NASA-TP-25831 p 14 N87-11963 

ENTROPY 

EPHEMERIDES 

FMy year anon of solar eclipses: 1986 - 2035 

p26 N87-25906 

Investigation of the effects of cobalt ions on epoxy 

properties 

[ NASA-TP-26391 p12 N87-12680 

Simplified curve fits for the thermodynamic properties 

[NASA-RP-l178-REV] 

EPOXY RESINS 

EQUILIBRIUM FLOW 

of equilibrium air 

ERROR ANALYSIS 

[NASA-RP-1 181 ] p 15 N87-26309 

Preliminary estimates of radiosonde thermistor errors 

[NASA-TP-26371 p 20 N87-12086 

Lowcost FM oscillator for capacitance type of blade 

lip clearance measurement system 

[ NASA-TP-27461 p 7 N87-24461 

A technique for evaluating the application of the pin-level 

stuck-at fault model to VLSl circuits 

[NASA-TP-27381 p 17 N87-28025 

Ester oxidation on an aluminum surface using 

chemiluminescence 

[ NASA-TP-26111 p12 N87-18666 

ESTERS 

ETHYL ALCOHOL 

Velocity profiles in laminar dithrsion flames 

[NASA-TP-2596] p15 N87-18035 

On the Maxwellian distribution, symmetric form, and 

entropy conservation for the Euler equations 

[ NASA-TP-25831 pt4 N87-lt963 

Efficient solutions to the Euler equations for supersonic 

flow with embedded subsonic regions 

[NASA-TP-25231 p2 N87-15183 

A secondorder accurate kinetic-theory-baaed method 

for invisdd compressible flows 

[ NASA-TP-2613 I p 15 N87-18783 

Experimental evaluation of blockage ratio and plenum 

evacuation system flow effects on pressure distribution 

for bodies of revolution in 0.1 scale model test section 

of NASA Lewis Research Center's proposed altitude wind 

tunnel 

[ NASA-TP-27021 p9 N87-22694 

-mental evaluation of Mockage ratio and plenum 

evacuabon system flow effects on pressure distribution 

for bodiis of revolution in 0.1 scale model test section 

of NASA Lewis Research Center's proposed altitude wind 

tunnel 

[ NASA-TP-27021 p9 N87-22894 

A technique for evaluating the application of the pin-level 

stuck-at fault model to VLSl circuits 

[NASA-TP-27381 p 17 N87-28025 

Evolution. calibration, and operational characteristics of 

the twodimensional test section of the Langley 0.3-meter 

transonic cryogenic tunnel 

[NASA-TP-27491 p9 N87-28570 

Experimental evaluabon of heat transfer on a 103O:l 

EULER EOUATIONS OF MOTION 

EVACUATlNQ (VACUUM) 

EVALUATION 

EVOLUTION (DEVELOPMENT) 

EXHAUST NOZZLES 

area ratio rocket node 

[ NASA-TP-27261 p 11 N07-25424 

EXOBIOLOGY 

Aerospace medicine and biology: A cumulative index 

to the 1986 issues (supplement 293) 

[ NASA-SP-7011(293)] p 21 N87-18976 

Aerospace medicine and biology: A continuing 

bibtiiraphy with indexes (supplement 302) 

[NASA-SP-7011(302)] p22 N87-30041 

Investigation of leading-edge flap performance on delta 

and doubledelta wings at supersonic speeds 

[NASA-TP-2656] p3 N87-m233 

Mach 6 experimental and theoretical stability and 

pertwmance of a cruciform missile at angles of attack 

up to 65 degrees 

[ NASA-TP-27331 p4 N87-23592 

EXPERT SYSTEMS 

EXPERIMENT MSKiN 

EXPERIMENTATION 

computer sciences and Data Systems, volume 1 

[NASACP-2459-VOL-l I p 22 N87-19931 

Drag measurements of blunt stores tangentially mounted 

EXTERNAL STORES 

on a flat plate at supersonic speeds 

[ NASA-TP-27421 p5 N87-27826 

Sensitivity Analysis in Engineering 

[NASACP-2457] p 17 N87-18855 

Modeling of joints for the dynamic analysis of truss SbllchlreS 

[ NASA-TP-26611 p 18 N87-20567 

Space station structures and dynamics test program 

[ NASA-TP-27101 p 18 N87-20568 

Structural Dynamics and Control Interaction of Flexible 

Structures 

[NASACP-2467-PT-1 I p 10 N87-22702 

Structural Dynamics and Control Interaction of Flexible 

Structures 

[ NASA-CP-2467-PT-21 p 10 N87-22729 

Structural Integrity and Dursbili of Reusable Space 

[NASA-CP-2471] p 11 N87-22766 

Preliminary sbuctural descgn of composite main rotor 

blades for minimum weight 

[ NASA-TP-27301 p 11 N87-25435 

%ace station structures and dvnamics test Drwram 

PtopUlsiMI systems 

DYNAMIC TESTS 

[ NASA-TP-27101 . p 18 NE7-25568 

Calibration of the spin-scan ozone imaaer aboard the 

DYNAMICS EXPLORER 1 SATELUTE 

dynamics ~xp~orer 1 Satellite 

[ NASA-TP-27231 p21 N87-26491 

E 

EARTH ATMOSPHERE 

Calculation and accuracy of ERBE scanner 

measurement locations 

[ NASA-TP-26701 p25 N87-28471 

Atlas of wide-fieldof-View out@ng longwave radiation 

derived from Nimbus 6 Earth radiation budget data set, 

July 1975 to June 1978 

[NASA-RP-1185] p 21 N87-26489 

Calculation and accuracy of ERBE scanner 

measurement locations 

[NASA-TP-2670] p25 N87-28471 

Earth resources: A continuing bibliraphy with indexes 

(issue 54) 

[NASA-SP-7041(54)] p 18 N87-27315 

Effects of background noise on total noise annoyance 

[ NASA-TP-26301 p 23 N87-14120 

Sensitivity Analysls in Engineering 

[NASA-CP-2457] p 17 N87-18855 

Space Electrochemical Research and Technology 

(SEW 

[NASA-CP-24841 p 19 N87-29914 

Asymptotic analysis of corona discharge from thin 

electrodes 

[ NASA-TP-26451 p 24 N87-14998 

from thin 

e(eCtr0des 

[ NASA-TP-26451 p24 N87-14998 

EARTH RADIATION BUDGET 

EARTH RADIATION BUDGET EXPERIMENT 

EARTH RESOURCES 

EFFECTIVE PERCEIVED NOISE LEVELS 

EIQENVALUES 

ELECTRIC BATERIES 

ELECTRIC CORONA 

ELECTRIC DISCHARGES 

Asymptotic analysis of corona 

ELECTRIC FIELDS 

Double Layers in Astrophysics 

[ NASACP-24691 p 25 N87-23313 

Space Electrochemical Research and Technology 

(SEW 

[NASA-CP-2484] p 19 N87-29914 

Space Electrochemical Research and Technology 

(SERT) 

[NASACP-2484] p 19 N87-29914 

ELECTRODES 

ASVmPt0tiC analysis of corona discharge from thin 

electrodes 

[NASA-TP-26451 p24 N87-14998 

Performance of textured cabn on copper electrode multistage depressed collectors with medium-power 

traveling wave tubes 

[NASA-TP-2665] p14 N87-17990 

Design. fabrication and performance of small. graphlte 

declmde. multistage depressed collectors with 200-w. 

ELECTROCATALYSTS 

ELECTROCHEMISTRY 

CW. 8- to lSGHz traveling-wave tubes 

[ NASA-TP-26931 p 14 N87-20474 

Traveling-wave-tube efficiency improvement by a 

lowcost technique for deposition of carbon on multistage 

depressed collector 

[NASA-TP-2719] p 14 N87-21239 

ELECTRODYNAMICS 

Tether Eymnlar Simulation 

[NASA-CP-2458] p 16 N87-18821 

New methods and results for quantification of 

[NASA-TP-2737] p3 N87-21871 

Theory for computing the field scattered from a smooth 

inflected surface 

[NASA-TP-2632] p24 N87-13264 

ELECTRON BEAMS 

Analyhcal and experimental performance of a dual-mode 

traveling wave tube and multistage depressed collector 

[ NASA-TP-27521 p 14 N87-25532 

Performance of textured carbon on copper electrode 

multistage depressed collectors with medium-power 

traveling wave tubes 

lightning-aircraft electrodynamics 

ELECTROMAGNETIC RArnAnw 

ELECTRON EMISSION 

[NASA-TP-2665] p 14 N87-17990 

Calculation of secundary electron trajectories in 

multistage depressed collectors for microwave ampliers 

[NASA-TP-2664] p 14 N87-17991 

Electron stimulated desorption of atomic oxygen from 

silver 

[NASA-TP-2668] p 12 N87-18629 

ELECTRON RADIATION 

Spectroscopic comparison of effects of electron 

radiation on mechanical properties of two polyimides 

[ NASA-TP-26631 pll N87-18611 

ELECTRONIC EQUIPMENT 

Development and evaluation of an airplane electronic 

display fmt aliined with the inertial velocityvector 

[NASA-TP-2648] p7 N07-13438 

Solution of elliptic partial diierential equations by fast 

Poisson solvers using a local relaxation factor. 2 Two-step 

method 

[NASA-TP-2530] p 22 N87-14910 

ELLIPTIC DIFFERENTIAL EWATIONS 

ELLIPTIC FUNCTIONS 

Solution of elliptic partial diierential equations by fast 

Poisson solvers using a local relaxation factor. 2: Two-step 

method 

[NASA-TP-2530] p 22 N87-14918 

ELLIPTICAL CYLINDERS 

Propagation of sound waves in tubes of mncircular cross 

section 

[NASA-TP-2601] p 2 N87-14284 

Efficient solufions to the Euler equations for supersonic 

Row with embedded subsonic regions 

[NASA-TP-2523] p2 N87-15183 

Ground-based timeguidance algorithm for control of 

airplanes in a timemetered air traffic control environment 

A piloted simulation study 

[NASA-TP-2616] p7 N87-10864 

Laser-powered MHD generators for space application 

[NASA-TP-26211 p24 N87-10764 

Space Photovoltaic Research and Technology 1986. 

High Efficiency, Space Environment, and Array 

Techndogy 

[NASA-CP-2475] pl9 N87-26413 

The 1985 Goddard Space Fliht Center Battery 

EMBEDDING 

ENERGY CONSERVATION 

ENERGY CONVERSION EFFICIENCY 

ENERGYSTORAGE 

wotl=hw 

[NASACP-2434] p 14 N87-11072 

ENERGY TRANSFER 

Double Layers in Astrophysics 

[NASACP-24691 p 25 N87-23313 

An experimental investigation of an advanced turboptop 

installation on a swept wing at subsonic and transonic 

speeds 

[NASA-TP-2729] p4 N87-%883 

Advanced detection. isolation and accommodation of 

s6-nsor failures: Real-time evaluation 

[ NASA-TP-27401 p8 N87-25331 

Piloted simulation sludy oi the effects oi an automated 

trim system on flight Characteristics of a liht twin-engine 

airplane with one engine inoperative 

[NASA-TP-2633] p2 N87-10843 

Advanced detection. isolation and accommodation of 

senaor failures: Real-time evaluation 

[ NASA-TP-27401 p8 N87-25331 

Probabilistic risk analysts of Hying the space shuttle with 

and without fuel turbine discharge temperature redline 

protection 

[NASA-TP-27591 p23 N87-27474 

Measurements of flow rate and trajectcq of aircraft 

tiregenerated water spray 

[NASA-TP-2718] p6 N87-24458 

ENGINE AIRFRAME INTEGRATION 

ENGINE CONTROL 

ENGINE FAILURE 

ENGINE INLETS 

ENGINE TESTING LABORATORIES 

Aeronautical facili awewnmt 

[NASA-RP-t146] p 8 N87-10876 
SUBJECT INDEX FUEL CONSUMPTION 

F 

F-106 AIRCRAFT 

Wind-tunnel free-flight investigation of a 0.15-scale 

model of the F-1066 airplane with vortex flaps 

[NASA-TP-27001 p 3 N87-21855 

New methods and results for quantification of 

liihtninggiraaft electrodynamics 

[NASA-TP-2737] p3 N87-21871 

Design, fabrication and performance of small, graphne 

electrode. multistage depressed collectors with xK)-W, 

CW. 8- to 1SGHz traveltng-wave tubes 

[ NASA-TP-26931 p 14 N87-XM74 

Development of confidence limits by pivotal functions 

for estimating software reliability 

[ NASA-TP-27091 p23 N87-23244 

Predicted effect of dynamic load on pitting fatigue lie 

for lowcontact-ratio spur gears [NASA-TP-2610] p16 N87-18095 

Structural Integrity and Durability of Reusable Space 

Propulsion Systems 

[NASA-CP-2471] p 11 N87-22786 

FAULT TOLERANCE 

Advanced detection, isolation and accommodation of 

sensor failures: Real-tima evaluation 

[ NASA-TP-27401 p8 N87-25331 

Joint University Program for Air Transportation 

[ NASA-CP-24531 p 1 N87-27596 

A technique for evaluating the mlication of the pin-level 

stuck-at fault model to VLSl circuits 

[NASA-TP-2738] p 17 N87-28025 

Analysis of quasi-hybrid soli rocket booster concepts 

for advanced eerth-toorbit vehicles 

[ NASA-TP-27511 p 11 N87-25425 

FABRICATION 

FAILURE ANALYSIS 

FATIGUE (MATERIALS) 

Researd, 1985 

FEASIBILITY ANALYSIS 

FIBEROPTICS , 

computer - and Data Systems. volume 2 [NASACP-2459-VOL-2] p 22 N87-19932 

Atlas of wide-fmldof-view outgoing hmgwave radiation 

derived from Nimbus 6 Earth radiation budget data set. 

July 1975 to June 1978 

[NASA-RP-1185] p21 N87-26489 

Interference effects of thruat reversing on horizontal tail 

effectiveness of twin-engine fighter aircraft at Mach 

numbers from 0.15 to 0.90 

[ NASA-TP-23501 p8 N87-10870 

Subsonic maneuver capability of a supersonic mise 

fighter wing wncapt 

[ NASA-TP-26421 p2 N87-15184 

Effects of empennage surface location on aerodynamic 

characteristics of a twin-engine aftwbocly model with 

nonaxisymmetric nonles 

[ NASA-TP-23921 p6 N87-17693 

Effects of afterbody boattail design and empennage 

arrangement on aeropropulsive characteristics of a 

twin-engine fighter model at transonic speeds 

[ NASA-TP-27041 p 3 N87-21873 

Mufliaxis contml power from thrust vectoring for a 

supersonic fighter aircraft model at Mach 0.20 to 2.47 

[NASA-TP-2712] p4 N87-24433 

Steady and unsteady aerodynamic forces from the SOUSSA surface-panel method for a fighter wing with tip 

missile and comparison with experiment andPANAlR 

[ NASA-TP-27361 p4 N87-26032 

Submit lorgtudinal and lateraldirectional 

charactwistics of a forward-sweptwing fighter 

configuration at angles of attack up to 47 deg 

[ NASA-TP-27271 p4 N87-26874 

Jet model for slot film cooling with effect of free-stream 

and coolant turbulence 

[ NASA-TP-26551 p 15 N87-18034 

FINITE ELEMENT METHOD 

ExplOibng symmebies in the modeling and amlysis of 

tires 

[NASA-TP-26491 p6 -7-17890 

Fifteenth NASTRAN Users' Colloquium 

[NASACP-2481] p 18 N87-27231 

Finiteelement reentry heat-transfer anatynis of space shultle olbiter 

[ NASA-TP-26571 p 16 N87-29795 

Wind-tunnel investigation at supersonic speeds of a 

remote-controlled canard missile with a free-collingtail 

brake torque system 

[NASA-TP-2401] p 3 N87-17668 

FIELD OF VIEW 

FIGHTER AIRCRAFT 

FILM COOLINQ 

FINS 

FLAPS (CONTROL SURFACES) 

Applicability of line&&theory attached-flow mews 

to design and analysis 01 flap systems at low speeds for 

thin swept wings with sharp leading edges 

[ NASA-TP-26531 p2 N87-15174 

Drag measurements of Munt stores tangentially mounted 

on a Rat plate at supersonic speeds 

[ NASA-TP-27421 p 5 N87-27626 

Smtural Dynamics and Control Interaction of Flexible 

Structures 

[ NASACP-2467-PT-11 p 10 N87-22702 

StruchKal pFamics and Control Interaction of FledMe 

Structures 

[ NASACP-2467-PT-21 p 10 N87-22729 

NASAID3D ControllStructures Interaction Technology. 

t986 

[ NASACP-2447-PT-l ] p 10 N87-16014 

The 20th Aerospace Mechanics Symposium 

[NASACP-2423-REV] p17 N87-16321 

Wind-tunnel inveswtion of the fliht Characteristics of 

a canard general-aviation airplane configuration 

[ NASA-TP-2623 I p1 N87-10039 

Piloted simulator study of allowable time delays in 

large-airplane response 

[ NASA-TP-26521 p8 N87-16849 

Fliht characteristics of the AD1 obliquewing resenrch 

aircraft 

[ NASA-TP-22231 p8 N87-18570 

FLIGHT CONTROL 

Joint University Program for Air Transportation 

Research, t983 

[NASA-CP-2451] pl N87-18520 

Joint University Program for Air Transportation 

Research, 1985 

[ NASACP-24531 p 1 N87-27596 

FLAT PLATES 

FLEXIBLE BOOlES 

FLEXIBLE SPACECRAFT 

FLIGHT CHARACTERISTICS 

FLIGHT CREWS 

Cockpit Resource Management Training 

[ NASA-CP-24551 p5 N87-22634 

Ground-based time-guidance algorithm for control of 

airplanes in a time-metered air traffic control environment: 

A piloted simulation study 

[ NASA-TP-26161 p 7 N87-10864 

Wind ShearlTurbulence Inputs to Fliht Simulation and 

[ NASACP-24741 p 1 N87-25267 

Groundbased time-guidance algorithm for control of 

airplanes in a timemetered air traffic control environment: 

A piloted simulation study 

[NASA-TP-2616] p7 N87-10864 

cockpit Resource Management Training 

[ NASAGP-24551 p 5 N87-22834 

Wind ShearlTurbulence Inputs to Fliht Simulation and 

Systems CeMicabon 

[ NASACP-24741 p 1 N87-25287 

Piloted-simulation shidy of effects of vwtex Raps on low-speed handling qualitjes of a Delta-wingairplane 

[ NASA-TP-27471 p8 N87-26922 

FLIGHT MANAGEYENT SYSTEMS 

FLIGHT SAFETY 

systems certification 

FLIGHT SIMULATION 

FLIGHT SIMULATORS 

Aeronautical fadlii assessment 

[NASA-RP-l146] p8 N87-10878 

Piloted simulator study of allowable time delays in 

largeairplane response 

[ NASA-TP-26521 p8 N87-16849 

FLIGHT TESTS 

In-flight total forces, moments and static aeroelastic 

characteristics of an oblique-wing research airplane 

[NASA-TP-2224] p8 N87-10103 

Development and evaluation of an airplane electronic 

display format algned with the inertial V~lodtyvector 

[NASA-TP-2648] p 7 N87-13438 

New memods and results for quantificabon of 

lihtningaircraft electrcdynamics 

INASA-TP-27371 D3 N87-21871 

Flight investigation of the effects of an outboard 

wing-leading-edge rodification on stalllspin 

characteristics of a bw-wing, single-engine. T-tail liht 

airplane 

[ NASA-TP-2691 I p6 N87-23814 

Application of parameter estimation to aircraft stability 

and control: The output-enor approach 

[NASA-RP-11681 p6 N87-29499 

Analog signal conditioning for flight-test 

instrumentation 

[NASA-RP-l1591 p7 N87-29533 

FLIGHT TRAINIMQ 

Cockpit Resource Management Training 

[NASACP-24551 p5 N87-22834 

FLOW DISTRIBUTION 

Design of 9.271-pressoreratio 5-stage core compressor 

and overall performance for first 3 stages 

[NASA-TP-2597] p7 N87-17689 

Aerothmal evaluation of a spherically blunted body 

with a trapezoidal cross section in the Langley 8-foot 

high-temperature tunnel 

[ NASA-TP-26411 p 15 N87-18782 

Detailed flow surveys of turning vanes designed for a 

0.1 -scale model of NASA Lewis Research Center's 

proposed altitude wind tunnel 

[NASA-TP-2680] p9 N87-20295 

Study of leeside flows over conically cambered delta 

wings at supersonic speeds, part 1 

[ NASA-TP-266O-PT-l] p4 N87-23597 

Study of leeside flows over conically cambered Della 

wings at supersonic speeds. part 2 

[ NASA-TP-2660-PT-21 p4 N87-25301 

Qualitative evaluation of a flush air data system at 

transonic speeds and high angles of attack 

[NASA-TP-2716] p8 N87-29497 

Experimental evaluation of wall Mach number 

distributions of the octagonal test section proposed for 

NASA Lewis Research Center's altitude wind tunnel 

[NASA-TP-Z666] p8 N87-17717 

Jet model for slot film cooling with effect of free-stream 

and cudant turbulence 

[NASA-TP-2655] p 15 N87-18034 

Measurements of flow rate and trajectory of aircraft 

tire-generated water spray 

[ NASA-TP-27181 p6 N87-24458 

Evaluation of diffuse-illumination holographic 

cinematography in a flutter cascade 

[ NASA-TP-25931 p 18 N87-13731 

In-flight surface oil-flow photographs with comparisons 

to pressore distribution and boundary-layer data 

[ NASA-TP-23951 p3 N87-20968 

Study of leeside flows over conically cambered Delta 

wings at supersonic speeds, part 2 

p4 N87-25301 

NASAChinese Aeronautical Establishment (CAE) 

Symposium 

[NASA-CP-2433] p7 N87-20267 

FLUID FLOW 

Exmrimental cavitv cfessure distributions at suoersonic 

FLOW VELOCITY 

FLOW VISUALIZATION 

[ NASA-TP-2660-PT-21 

FLUID DYNAMICS 

_. 4s 

[ NASA-TP-26831 p3 N87-22626 

FLUID MANAGEMENT 

Microgravity Fluid Management Symposium 

[NASACP-2465] p 13 N87-21141 

Effects of winglet on transonic flutter characteristics of 

p 17 N87-13789 

Development testing of large volume water sprays for 

FLUl-rER 

a cantilevered twin-engin&ransporl wing model 

[NASA-TP-2627] 

FOQ DISPERSAL 

warm fog dispersal 

[ NASA-TP-26071 p10 N87-12585 

FORMAT 

Promedings of the 5th Annual Users' conference 

[NASA-CP-2399] p 22 N87-10720 

Structural Integrity and Durability of Reusable Space 

Propulsion Systems 

[NASA-CP-2471] p 11 N87-22786 

Wind-tunnel free-fliht investigation of a 0.15-scale 

FRACTURE MECHANICS 

FREE FLIGHT 

model of the F-106B airplane with vortex flaps 

INASA-TP-27001 D3 N87-21855 

FREE FLOW 

Heliiter Made-vortex interaction locations: 

Scale-model acwstics and free-r*ske analysisresults 

[ NASA-TP-28581 p3 N87-18537 

Frequency domain laser velocimeter signal processor: 

A new signal processing scheme 

[NASA-TP-2735] p 16 N87-27994 

Lowcost FM oscillator for capacitance type of blade 

p7 N87-24481 

Closed-Cycle. Frequency-Stable CO2 Laser 

FREQUENCIES 

FREQUENCY MODULATION 

tip clearance measurement system 

[ NASA-TP-27461 

FREQUENCY STABILITY 

Technology 

[ NASACP-24581 P 16 N87-20522 

FUEL COMSUMPTION 

Ground-based timeguidance algorithm for control of 

airplanes in a time-metered air traffic control environment: 

A piloted simulation study 

[NASA-TP-2616] p 7 N87-10864 

A-7 
SUBJECT INDEX 

Preliminary structural design of composite main rotor 

blades for minimum weight 

[NASA-TP-27301 p 11 N87-25435 

HEPTANES 

Velocity profiles in laminar diffusion flames 

[NASA-TP-2596] p 15 N87-18035 

Space shuttle main engine high pressure fuel pump aft 

platform seal cavity flow analysis 

[NASA-TP-26851 p14 N87-17000 

Summary of studies to reduce wing-mounted propfan 

inStallation drag on an M = 0.8 transport 

[NASA-TP-26781 p 6 N87-20990 

Conventionally cast and for@ copper alloy for 

[ NASA-TP-26941 p 12 N87-16902 

Forward-swept wing configuration designed for high 

maneuverability by use of a transonic computational 

[ NASA-TP-26281 p 2 N87-11702 

Evolution, calibration, and operational characteristics of 

the two-dimensional test section of the Langley 0.3-meter 

transonic cryogenic tunnel 

[ NASA-TP-27491 p 9 N87-28570 

Lewis inverse design code (LINDES): Users manual 

[ NASA-TP-26761 p3 N87-20238 

HOLOGRAPHIC INTERFEROMETRY 

Evaluation of diffuse-illumination holographic 

cinematography in a fluiter cascade 

[ NASA-TP-25931 p 16 N87-13731 

Automated Reduction of Data from Images and 

Holograms 

[NASACP-2477] p5 N87-29432 

HOLOGRAPHY 

Evaluation of diffuse-illumination holographic 

cinematography in a flutter cascade 

[ NASA-TP-25931 p 16 N87-13731 

Experimental evaluation of honeycomblscreen 

configurations and short contraction section for NASA 

Lewis Research Center's altitude wind tunnel 

[ NASA-TP-26921 p9 N87-23662 

Annoyance response to simulated advanced turboprop 

aircraft interior noise containing tonal beats 

[ NASA-TP-26891 p 23 N87-24161 

HYBRID PROPELLANT ROCKET ENGINES 

Analysis of quasi-hybrid soli rocket booster concepts 

p 11 N87-25425 

HIGH PRESSURE 

HIGH SPEED 

HIGH TEMPERATURE 

high-heat-flux thNSt chambers 

HIGHLY MANEUVERABLE AIRCRAFT 

method 

HISTORIES 

HODOGRAPHS 

HONEYCOMB STRUCTURES 

HUMAN TOLERANCES 

for advanced earth-toorbi vehicles 

[ NASA-TP-27511 

HYDRAULIC EQUIPMENT 

The 20th Aerospace Mechanics Symposium 

[NASACP-2423-REV] p 17 N87-16321 

Preliminary design of turbopumps and related 

machinery 

[NASA-RP-1170] p2 N87-17665 

HYDROQEN 

HYDRODYNAMICS 

The Jwian Atmospheres 

[ NASACP-24411 p26 N87-17598 

Hydrogen trapping and the interaction of hydrogen with 

metals 

[ NASA-TP-27441 p 12 N87-25463 

HYDROQEN FUELS 

Effect of Reynolds number variation on aerodynamics 

of a hydrogen-fueled transport concept at Mach 6 

[ NASA-TP-27281 p4 N87-26031 

HYDROQEN PEROXIDE 

Future directions for H sub x 0 sub y detection 

[NASA-CP-2448] p 19 N87-15528 

HYDROXYL RADICALS 

Future directions for H sub x 0 sub y detection 

[NASA-CP-2448] p 19 N87-15528 

Effect of Reynolds number variation on aerodynamics 

of a hydrogen-fueled transpwt concept at Mach 6 

[ NASA-TP-27281 p4 N87-26031 

HYPERSONIC FLOW 

Simphfied curve fits for the thermodynamic propwties 

of equilibrium air 

[ NASA-RP-11811 p15 N87-26309 

HYPERSONIC SPEED 

Mach 6 eqwimental and theoretical stability and 

perfcmance of a auciform missile at angles of attack 

up to 65 dqees 

[ NASA-TP-2733 I p4 N87-23592 

Aerothermal tests of spherical dome protuberances on 

HYPERSONIC AIRCRAFT 

HYPERSONIC VEHICLES 

a flat plate at a Mach number of 6.5 

[ NASA-TP-26311 p 14 N87-13664 

FUEL PUMPS 

Space shuttle main engine hgh pressure fuel pump aft 

platform seal cavity flow analysis 

[ NASA-TP-26851 p 14 N87-17000 

Threestep labyrinth seal for high-performance 

turbomachines 

[NASA-TP-1848] p 15 N87-23921 

Straight cylindrical seal for high-performance 

turbomachines 

[ NASA-TP-18501 p 15 N87-23936 

Threestep cylindrical seal for hgh-performance 

turbomachines 

[ NASA-TP-18491 p 15 N87-24639 

G 

GALACTIC COSMIC RAYS 

Possible complementary cosmic-ray systems: Nuclei 

[NASA-TP-2741] p 24 N87-24977 

and antinuclei 

cosmic ray heavy ion LET mappicg for aluminum. silicon. 

and tissue targets 

[NASA-RP-1180] p27 N87-25984 

[NASACP-24661 p26 N87-24266 

Doubly differential cross sections for galactic heavy-ion 

fragmentation 

[ NASA-TP-26591 p 24 N87-17487 

Star Formation in Galaxies 

[ NASACP-24661 p26 N87-24266 

GALACTIC STRUCTURE 

Star Formation in Galaxies 

GALAXIES 

GAMMA RAY ASTRONOMY 

Essays in Space Science 

GAS DETECTORS 

A simplified method for determining heat of combustion 

of natural gas 

[NASA-TP-26821 p16 N87-20514 

GAS DYNAMICS 

[NASA-CP-2464] p 25 N87-24247 

The Jovian Atmospheres 

[NASA-CP-2441 ] p 26 N87-17598 

Preliminary desgn of turbopumps and related 

machinery 

[NASA-RP-1170] p2 N87-17665 

GAS GIANT PLANETS 

The Jovian Atmospheres 

[NASACP-2441] p26 N87-17590 

Hydrogen trapping and the interaction of hydrogen with 

metals 

[NASA-TP-2744] p 12 N87-25463 

Space Opportunities for Tropospheric Chemistry 

Research 

[NASACP-2450] p20 N87-18248 

GEAR TEETH 

Gear tooth stress measurements on the UH-GOA 

heliter transmiwn 

[ NASA-TP-2698 ] p 17 N87-22235 

Predicted effect of dynamic load on pitting fatigue life 

for lowcontact-ratio spur gears 

[NASA-TP-2610] p 16 N87-18095 

GENERAL AVIATION AIRCRAFT 

Wind-tunnel investigation of the fhht characteristics of 

a CBnard general-aviation airplane configuration 

[NASA-TP-2623] p 1 N87-10039 

Flight inveatigation of the effect of tail configuration on stall, spin. and recovery characteristics of a low-wing 

general aviation research airplane 

[NASA-TP-2644] p6 N87-16815 

A simulation evaluation of a pilot interface with an 

automatic terminal approach system 

[NASA-TP-2689] p 7 N87-19393 

Low-speed aerodynamic characteristics of a twin-engine 

mal aviation configuration with aft-fuselage-mounted 

puw propelb 

GAS-METAL INTERACTIONS 

GASES 

QEARS 

[NASA-TP-2763] p5 N87-29462 

QEOCENTRIC COORDINATES 

Ten year planetary ephemeris: 19861995 

[NASA-RP-11761 p 25 N87-14219 

QEWORPHOLOGY 

regional landforms 

Geomorphology from space: A global overview of 

[NASASP-486] p 18 N87-18139 

GEOPHYSICS 

NASAlMSFC FY-85 Atmo@wnc . RocessesResearch 

Review 

[ NASACP-24021 p20 N87-13043 

BET AWAY SPECIALS (Srs) 

The 1986 Get Away Special Experimenter's 

Symposium 

[ NASACP-24381 p9 N87-20302 

GLOBAL POSITIONING SYSTEM 

Joint University Program for Air Transportation 

Research, 1985 

[NASACP-24531 p 1 N87-27596 

The 1986 Get Away Special Experimenter's 

Symposium 

[ NASA-CP-24381 p9 N87-20302 

Permeation of oxygen through high purity, large grain 

silver 

[ NASA-TP-27551 p 12 N87-27024 

Experiments in encoding multilevel images as 

OVERNMENT/INDUSTRY RELATIONS 

GRAIN BOUNDARIES 

GRAY SCALE 

auadtrees 

[NASA-TP-2722] p 23 N87-28367 

Proceedings of the 1985 NASA Ames Research Center's 

GROUND EFFECT (AERODYNAMICS) 

Ground-Effects Workshop 

[ NASA-CP-24621 p4 N87-24410 

Largescale static investigation of 

circulationcontrol-wing concepts applied to upper 

surface-blowing aircraft 

[ NASA-TP-26841 p6 N87-15959 

Applications and requirements for real-time simulators 

in ground-test facilities 

[ NASA-TP-26721 p 22 N87-23202 

GROUND TESTS 

QROUP DYNAMICS 

Cockpit Resource Management Training 

[ NASACP-24551 p5 N87-22634 

Detailed flow surveys of turning vanes designed for a 

0.1 -scale model of NASA Lewis Research Center's 

proposed altitude wind tunnel 

[NASA-TP-2680] p9 N87-20295 

GUIDE VANES 

H 

HALLEY'S COMET 

Atlas of Comet Halley 1910 II 

[NASA-SP-488] p26 N87-30235 

Conventionally cast and forged cwr alloy for 

high-heat-flux thrust chambers 

[ NASA-TP-26941 p 12 N87-16902 

Expefpental evaluation of heat transfer on a 10301 

area raw rocket nozzle 

[ NASA-TP-27261 p 11 N87-25424 

HEAT OF COMBUSTION 

A simDlified method for determining heat of combustion 

HEAT FLUX 

Of natural gas 

[ NASA-TP-26821 

HEAT TRANSFER 

p 16 N87-20514 

Aerothermal evaluation of a spherically blunted body 

with a trapezoidal cross section in the Langley 8-foot 

high-temperature tunnel 

[ NASA-TP-26411 p 15 N87-18782 

Experimental evaluation of heat transfer on a 10301 

ares ratio rocket nozzle 

[NASA-TP-27261 p 11 N87-25424 

Application of turbulence modeling to predict surface 

heat transfer in stagnation flow region of circular cylinder 

[ NASA-TP-27581 p 15 N87-27161 

Finite-element reentry heat-transfer analysls of space 

shutw, orbiter 

[ NASA-TP-26571 p 16 N87-29795 

Doubly differential moss sections for galactic heavy-ion 

fragmentation 

[ NASA-TP-26591 p24 N87-17487 

Possible complementary cosmic-ray systems: Nuclei 

and antinudei 

[NASA-TP-2741] p 24 N87-24977 

Transonic Row analysis for rotors. Pad 2: 

Threedimensional. unsteady. full-potential calculation 

[ NASA-TP-2375PT-21 p2 N87-10841 

Testing of UH-GOA helicopter transmission in NASA 

Lewis 2240-kW (3000-hp) facility 

[NASA-TP-2626] p 16 N87-10391 

Recent Experiences in MuMisciplinary Ana)ysls and 

mmization. part 2 

[ NASACP-2327-PT-21 p6 N87-11750 

Power cspsbum technique with application to model 

heliiter acMllltic data 

[NASA-TP-2586] p 23 N87-17479 

Heliter Madwortex interaction locations: 

Scabmodel acowtica and freewake analyskresutts 

[NASA-TP-26581 p 3 N87-18537 

Vibration characteristicsof OH-58~ helicopter main rotor 

transmission 

[ NASA-TP-27051 p 17 N87-20555 

HEAT TRANSTrR COEFFICIENTS 

HEAW IONS 

HELICOPTER PERFORMANCE 

HELICOPTERS 

A-8 
SUBJECT INDEX 

HYPERSONIC WIND TUNNELS 

Description and calibration of the Langley Hypersonic 

CF4 tunnel: A facility for simulating low gamma flow as 

occurs for a real gas 

[ NASA-TP-23841 p 16 N87-29778 

I 

ICE MAPPING 

Arctic Sea ice, 1973-1976 Satellite passive-microwave 

observations 

[NASASP49] p 21 N87-24870 

Automated Reduction of Data from Images and 

Holograms 

[NASA-CP-2477] p5 N87-29432 

IMAGE ANALYSIS 

IMAGE PROCESSlNG 

Proceedings of the 5th Annual Users’ Conference 

[NASA-CP-2399] p22 N87-10720 

Sixth Annual Users’ Conference --- Transpomble 

Applications Executive (TAE) 

[NASA-CP-2463] p22 N87-23156 

Experiments in encoding multilevel images as 

quadtrees 

[ NASA-TP-27221 p23 N87-28367 

In-flight surface oil-flow photographs with comparisons 

to pressure disbibution and boundary-layer data 

[NASA-TP-2395] p3 N87-20966 

INDEXES (DOCUMENTATION) 

Technology for Large Space Systems. A bibliography 

with indexes (supplement 17) 

[ NASA-SP-7046(17)] p9 N87-29576 

NASA scientific and technical publications: A catalog 

of mal Publications. Reference Publications. 

Conference Publications, and Technical Papers. 

1977-1 986 

[ NASA-SP-70631 p 25 N87-30218 

Development and evaluation of an airplane electronic 

display format alined with the inertial velocityvector 

[NASA-TP-26481 p 7 N87-13438 

Joint University Program for Air Transportation 

Research, 1985 

[NASA-CP-2453] p 1 N87-27596 

socth Annual Users’ Conference --- Transportable 

Applications Executive (TAE) 

[ NASA-CP-2463 ] p 22 N87-23156 

IN-FLIGHT MONITORING 

INERTIAL NAVIGATION 

INFORMATION SYSTEMS 

INFRARED ASTRONOMY 

Infrared source cross-index, first edition 

Essays, in Space Science 

Star Formation in Galaxies 

[NASA-RP-1182] p 25 N87-22573 

[ NASA-CP-24641 p 25 N87-24247 

[NASA-CP-2466] p 26 N87-24266 

Description of data on the Nimbus 7 LlMS map archive 

tape: Ozone and nitric acid 

[ NASA-TP-26251 p 19 N87-13022 

Atlas of absorption lines from 0 to 17900 cm (sup)-1 

[NASA-RP-1168] p 19 N87-28955 

Infrared source cross-index. first edii 

[NASA-RP-1182] p 25 N87-22573 

Proceedings of the 1985 NASA Ames Research Center’s 

Ground-Effects Workshop 

[NASA-CP-2462] P4 N87-24410 

Measurements of flow rate and trajectory of airman 

tiregenerated water spray 

[ NASA-TP-27181 P6 N87-24458 

Electronics reliability and measurement technology 

[NASACP-2472] p 17 N87-27204 

Evaluation of installed performance of a 

wing-tipmounted pusher turboprop on a semispan wing 

[NASA-TP-2739] p6 N87-26041 

Jet transport fliiht operations using cockpit diaplay of 

traffic information during instrument meteorological 

cooditions: Simulation evaluation 

[NASA-TP-2567] p5 N87-29469 

Pulse code Modulation (PCM) encoder handbook for 

Aydin Vector MMP-600 series system 

[NASA-RP-1171] p 13 N87-11916 

A technique for evaluating the application of the pin-level 

stuck-at fault model to VLSl arc& 

[ NASA-TP-27381 p 17 N87-28025 INTERACTIONAL AERODYNAMICS 

Supercompning in Aerospace 

INFRARED DETECTORS 

INFRARED RADIATION 

INFRARED SOURCES (ASlROWY) 

INGESTION (ENQINES) 

INSPECTION 

INSTALLINQ 

INSTRUMENT APPROACH 

INTEQRATED CIRCUITS 

[ NASA-CP-24541 p4 N87-25998 

INTERACTIVE CONTROL 

NASAlDOD ControllStructures Interaction Technolcgy. 

1906 

[ NASA-CP-2447-PT-21 p 10 N87-24495 

Effect of LID (Registered) processing on the 

microsbucture and mechanical properlies of Ti-6AI-4V and 

TibAI-2Sn-4Zr-2Mo titanium foilgayle materials 

INTERFACES 

[ NASA-TP-26771 p12 N87-18644 

INTERPOLATION 

of interpolants 

Quantitative analysis of the reconstruction performance 

[ NASA-TP-26661 p 23 N87-22441 

INVENTIONS 

Significant NASA inventions. Available for licensing in 

foreign countries 

[NASASP-7038(04)] p 25 N87-70425 

INVERSIONS 

Lewis inverse desgn code (LINDES): Users manual 

[ NASA-TP-26761 p 3 N87-20238 

INVESTIGATION 

Investigation of the effects of cobalt ions on epoxy 

properties 

[ NASA-TP-26391 p12 N87-12680 

Flight investigation of the effects of an outboard 

wing-leadim modiition on stalllspin 

characteristics of a low-wing, single-engine, T-tail light 

airplane 

[ NASA-TP-26911 p6 N87-23614 

Calculation of viscous effects on transonic flow for 

oscillating airfoils and comparisons with experiment 

[NASA-TP-2731] p 5 N87-27622 

Investigation of the effects of cobalt ions on epoxy 

properties 

[NASA-TP-2639] p12 N87-12680 

Cosmic ray heavy ion LET mapping for aluminum, silicon. 

and tissue targets 

[NASA-RP-l180] p27 N87-25984 

INVISCID FLOW 

IONS 

J 

JET AIRCRAFT 

Jet transport fliiht operations using cockpit display of 

traffic information during instrument meteorological 

conditions: Simulation evaluation 

[ NASA-TP-25671 p5 N87-29469 

Jet model for slot film cooling with effect of heestream 

and coolant turbulence 

[ NASA-TP-26551 p 15 N87-18034 

Multiscale turbulence effects in supersonic jets 

exhausting into still air 

[NASA-TP-2707] p 15 N87-24672 

JET ENGINES 

JET EXHAUST 

JOINTS (JUNCTIONS) 

The 2ovI Aerospace Mechanics Symposium 

[ NASA-CP-2423-REVl p17 N87-16321 

Modeling of joints for the dynamic analysis of truss 

structures 

[NASA-TP-2661] p 18 N87-20567 

Structural Dynamics and Control Interaction of Flexible 

Structures 

[NASA-CP-2467-PT-Z] p 10 N87-22729 

JUPITER ATMOSPHERE 

The Jovian Atmospheres 

[ NASA-CP-24411 p26 N87-17598 

K 

KALMAN FILTERS 

Description of data on the Nimbus 7 LlMS map archive 

tape: Ozone and nibic acid 

[NASA-TP-2625] p 19 N87-13022 

Spectroscopic comparison of effects of electron 

radiation on mechanical properties of two mmides 

[NASA-TP-2663] pll N87-18611 

A second-order accurate kinetic-theoly-based method 

for imiscid compressiMe flows 

[ NASA-TP-26131 p 15 N87-18783 

KAPTON (TRADEMARK) 

KINETIC THEORY 

L 

LABYRINTH SEALS 

Three-step labytinm seal for highperformance 

turbomachines 

[NASA-TP-1 8481 p 15 N87-23921 

Aerothermal tests of spherical dome protuberances on 

[NASA-TP-2631] p14 N87-13664 

LAMINAR BOUNDARY LAYER 

a flat plate at a Mach number of 6.5 

LIFE (DURABILITY) 

LAMINAR FLOW 

Velocity profiles in laminar diffusion flames 

p 15 N87-18035 

Geomorphology from space: A global overview of 

regional landforms 

[NASA-SP-486] p 18 N87-18139 

[ NASA-TP-25961 

LANDFORMS 

LANDING GEAR 

Langley Airman Landing Dynamics Facility 

[NASA-RP-1189] p9 N87-29544 

LARGESPACESTRUCTURES 

Solar array flight dynamic experiment 

[ NASA-TP-25981 p9 N87-12581 

NASAlDOD ControVStructures Interaction Technology, 

1986 

[ NASA-CP-2447-PT-l ] p10 N87-16014 

Solar array flight experimenVdynamic augmentation 

experiment 

[NASA-TP-2690] p 10 N87-20380 

Modeling of joints for the dynamic analysis of truss 

structures 

[NASA-TP-2661] p 18 N87-20567 

Space station structures and dynamics test program 

[NASA-TP-2710] p 18 N87-20568 

Structural Dynamics and Control Interaction of Flerdbk 

Structures 

[NASA-CP-2467-PT-l] p 10 N87-22702 

StrUCtural Dynamics and Control Interaction of Flexible 

Structures 

[NASA-CP-2467-PT-2] p 10 N87-22729 

Technology for Large Space Systems. A bibliiraphy 

with indexes (supplement 17) 

[ NASA-SP-7046(17)] p9 N87-29576 

[ NASA-CP-24701 p 18 N87-29858 

The 2191 Aerospace Mechanisms Symposium 

LASER APPLICATIONS 

Thirteenth International Laser Radar Conference 

Solar array fliht dynamic experiment 

[NASA-CP-2431] p 16 N87-10263 

[ NASA-TP-25981 p9 N87-12581 

LASER DOPPLER VELOCIMETERS 

Frequency domain laser velocimeter signal processor: 

A new signal processing scheme 

[ NASA-TP-27351 p 16 N87-27994 

Evaluation of diftuse-illumination holographic 

cinematography in a flutter cascade 

[NASA-TP-2593] p 16 N87-13731 

Laser-powered MHD oeneraton for soace amlitin 

LASER OUTPUTS 

LASER PLASMA INTERACTIONS 

[NASA-TP-2621] p’24 N07-10764 

LASERS 

Thirteenth International Laser Radar Conference 

[NASA-CP-24311 p16 N87-10263 

Subsonic longitudinal and lateraldirectionel 

characteristics of a forward-swept-wing fighter 

configuration at angles of attack up to 47 deg 

[ NASA-TP-27271 p4 N87-28874 

Subsonic longitudinal and lateraldirectional 

characteristics of a forward-swept-wing fighter 

configuration at angles of attack up to 47 deg 

[ NASA-TP-27271 p4 N87-28874 

A synchronous data analyzer for the Minimum Delay 

Data Format (MDDF) and Launch Trajectwy AcquisMon 

System (LTAS) 

[ NASA-TP-27431 p 13 N87-24590 

Investigation of leading-edga flap performance on delta 

p3 N87-20233 

Flight investigation of the effects of an outboard 

wing-leadingedge modition on stall/spin 

characteristics of a low-wing. single-engine. T-tail light 

airplane 

[NASA-TP-2691] p6 N87-23614 

LEAKAGE 

Threestep cylindrical seal for high-performance 

p 15 N87-24639 

Study of leeside flows over conically cambered delta 

LATERAL CONTROL 

LATERAL STABILITY 

LAUNCHING 

LEADING EDQE FLAPS 

and doubledelta wings at supersonic speeds 

[ NASA-TP-26561 

LEADING EDGES 

turbomachines 

[ NASA-TP-18491 

LEE WAVES 

wings at supersonic apwds. part 1 

[NASA-TP-Z66O-PT-l] p4 N87-23597 

LICENSING 

SiinMant NASA inventions. Available for licensing in 

foreign countries 

[ NASA-SP-7038(04)] p25 N87-70425 

LIFE (DURABILITY) 

Turbine Engine Hot Sectbn Techndogy. 1984 

[NASA-CP-2339] p17 N87-11180 

A-9 
LIFT AUGMENTATION SUBJECT INDEX 

Predicted effect of dynamic load on pitting fatigue life 

for lowcontact-ratio spur gears 

[ NASA-TP-26101 p 16 N87-18095 

Larg?-sca!e static investigation of 

circulatlon-control-wing concepts applied to upper 

surfacehiowing eircrstt 

[NASA-TP-2684] p6 N87-15959 

Piloted simulation study of the effects of an automated 

trim system on flight characteristics of a light twin-engine 

airplane with one engine inoperative 

[NASA-TP-2633] p2 N87-10843 

New methods and results for quantification of 

LIFT AUGMENTATION 

UGHT AIRCRAFT 

UG"lNQ 

lightning-aircrafl electrodynamics 

[ NASA-TP-27371 p3 N87-21871 

LINE SPECTRA 

Atlas of absorption lines from 0 to 17900 cm (sup)-1 

[NASA-RP-11 881 p 19 N87-28955 

CosmicrayheavyionLETmappingforaluminum. silicon, 

[NASA-RP-lleO] p 27 N87-25984 

Applicability of linearized-theoly attached-flow methods 

to design and analysis of flap systems at low speeds for 

thin swept wings with sharp leading edges 

[NASA-TP-26531 p 2 N87-15174 

Turbine Engine Hot Section Technology. 1984 

[NASACP-2339] p17 N87-11180 

Conventionally cast and forged wpper alloy for 

high-heat-flux thrust chambeo 

[NASA-TP-2694] p 12 N87-16902 

Preliminary design of tu-mps and related 

machinery 

[NASA-RP-1170] p2 N87-17665 

Effect of LID (Registered) processing on the 

miaostructUre and mechanical properties of Ti-6AI-4V and 

Ti-6A1-2Sn-4Zr-2Mo titanium foil-gayle matefials 

[NASA-TP-2677] p12 N87-18644 

LINEAR ENERGY TRANSFER (LET) 

and tissue targets 

LINEARITY 

UNINQS 

UOUlD PROPELLANT ROCKET ENGINES 

LIacllDs 

UTHIUY SULFUR BAlTERIES 

The 1985 Goddard Space FlQht Center Battery 

[NASA-CP-2434] p 14 N87-11072 

Five year global dataset: NMC operational analyses 

(1 978 to 1982) 

[NASA-RP-11941 p21 N87-29996 

Atlas of midwield-of-view outgoing longwave radiation 

derived from Nimbus 6 Earth radiatim tudget data set. 

July 1975 to June 1978 

[NASA-RP-l185] p21 N87-26489 

Applicability of linearized-theory attached-flow methods 

to design and analysls of flap systems at low speeds for 

thin swept wings with sharp leading edges 

[NASA-TP-2653] p2 N87-15174 

Piloted simulator study of allowable time delays in 

large-awpiane response 

[ NASA-TP-2652 1 p8 N87-18849 

Fliiht characteistics of the AD1 obliquewing research 

aiman 

[NASA-TP-ZZZl] p8 N87-18570 

Piloted-simulation study of effects of vortex fhps on 

low-speed handling qualities of a Delta-wingairplane 

[NASA-TP-27471 p8 N87-26922 

Low-speed aerodynamic characteristics of a twin-angina 

general aviation configuration with aft-fuselagemounted 

PuW propellers 

[NASA-TP-2763] p5 N87-29462 

workshop 

LONG TERM EFFECTS 

LONG WAVE RADIATION 

LOW SPEED 

LUNAR BASES 

Status and Mue of lunar pxcimx 

[NASASP-4&I] P26 N87-19322 

M 

MACH NUMBER 

Expenmentill evaluation of wall Mach number 

disbibulions of the octagonal tent section proposed for 

NASA Lewis Research center's altitude wind tunnd 

[NASA-TP-26681 P8 N87-17717 

Mach 6 experimental and theoretical stability and 

performance of a cruciform missile at angles of attack 

upto=desrees 

[ NASA-TP-27331 p4 N87-23592 

Multiaxis control power from tksl vectoring for a 

supersonic fighter aircrafl model at Mach 0.20 to2.47 

[ NASA-TP-27121 p4 N87-24433 

Effect of Reynolds number variation on aerodynamics 

of a hydrogen-fueled transport concept at Mach 6 

[NASA-TP-2728] p4 N87-26031 

Description and calibration of the Langley Hypersonic 

CF4 tunneb A facility for simulating low gamma flow as 

occurs for a real gas 

[NASA-TP-2384] p 16 N87-29778 

MAGNETIC FIELD CONFIGURATIONS 

Caonal and Prominence Plasmas 

[ NASA-CP-24421 p26 N87-20871 

Laser-powered MHD generatws for space application 

[ NASA-TP-26211 p24 N87-10764 

MAGNETOHYDRODYNAMIC STABILITY 

Energetic Phenomena on the Sun: The Solar Maximum 

Mission Flare Workshop. Proceedings 

[ NASACP-24391 p 26 N87-19328 

Coronal and Prominence Plasmas 

[NASACP-2442] p26 N87-20871 

MAGNETOHYDRODYNAMICGENERATORS 

MAQNETOSTATICS 

Coronal and Prominence plasmas 

[ NASACP-24421 p26 N87-20871 

A simulation evaluation of a pilot interface with an 

automatic terminal approach system 

[NASA-TP-2669] p7 N87-19393 

MANCOMPUTER INTERFACE 

Sixth Annual Users' Conference --- Transportable 

Applications Executive (TAE) 

[NASACP-2463] p 22 N87-23156 

Management: A bibliography for NASA managers 

(supplement 21) 

[ NASA-SP-7500(21)1 p 24 N87-20833 

Management: A bibliography for NASA managers 

(suwlement 21) 

[ NASA-SP-7500(21)] p24 N87-20833 

Management: A bibliography for NASA managers 

(supplement 21) 

[ NASASP-7500(21) ] p24 N87-20833 

Subsonic maneuver capability of a supersonic mise 

fiehter wing concept 

[NASA-TP-2642] p2 N87-15184 

MAN MACHINE SYSTEMS 

MANAGEMENT 

MANAGEMENT MElHOD!3 

MANAGEMENT PLANNING 

MANEUVERS 

MANIPULATORS 

The 2Mh Aerospace Mechanics Symposium 

The 21st Aerospace Mechanisms Symposium 

[ NASA-CP-2423-REVl p 17 N87-16321 

[ NASA-CP-24701 p 18 N87-29858 

Atlas of wide-field-of-view outgoing longwave radiation 

derived from Nimbus 6 Earth radiation budget data set. 

July 1975 to June 1978 

[NASA-RP-1185] p 21 N87-26489 

MATHEMATICAL YOMLS 

MAPPING 

Turbine Engine Hot Section Technology, 1984 

Exploiting symmew in the modeling and analyss of 

tires 

[ NASA-TP-26491 p6 N87-17690 

Double Layers in Astrophysics 

[NASA-CP-2469] p 25 N87-23313 

Probabilistic risk analysis of Rylng the space shuffle with 

and without fuel turbine discharge temperature redline 

protection 

[ NASA-TP-27591 p 23 N87-27474 

Space Electrochemical Research and Technology 

(SEW 

[NASACP-2484] p 19 N87-29914 

MAXWELLBOLRYANN DENSITY FUllcTKm 

On the Maxwellian distribution. symmetric form, and 

entropy OMIsBIVBtion for the Euler equations 

[ NASA-TP-25831 p14 N87-11963 

On requirements for a satellite mission to measure 

tropicar rainfall 

[NASA-RP-l183] p20 N87-20701 

Earth rB8wrces: A continuing bibliraphy with indexes 

(issue 54) 

[NASASP-7041 (a)] p 18 N87-27315 

Investigation of the effects of coben ions on epoxy 

[NASA-TP-2639] p12 N87-12880 

Effect of LID (Registered) processing on the 

microstructure and mechanical prws of Tk6AI-4V and 

TcBAI-ZSn-4Zr-ZMo titanium foilgauge materials 

[NASA-TP-2677] p12 N87-18644 

NASAlMSFC FY-85 Atmospheric . -Research 

Review 

[NASA-CP-2402] p 20 N87-13043 

[NASA-CP-2339] p17 N87-11180 

MEASURINQ INSTRUMENTS 

MECHANICAL PROPERTIES 

MESOSCALE PHENOYENA 

METAL MATRIX COMPOSITES 

Effects of thermal cycling on graphiefiber-reinforced 

pll N87-10184 

Ester oxidation on an aluminum surface uslng 

chemiluminescence 

[NASA-TP-2611] p12 N87-18666 

6061 aluminum 

[NASA-TP-261 21 

METAL SURFACES 

METEOROLOQICAL PARAMETERS 

Thirteenth International Laser Radar Conference 

[NASA-CP-2431] p16 N87-10263 

kctic Sea ice. 1973-1976 Satellite passivemicrowave 

observations 

[NASA-SP-489] p 21 N87-24870 

Five year global dataset: NMC operational analyses 

(1978 to 1982) 

[NASA-RP-1194] p21 N87-29996 

On requirements for a satellite mission to measure 

tropical rainfall 

[NASA-RP-11831 p20 N87-20701 

MICROBURSTS 

METEOROLOQICAL SATELLITES 

Doppler Radar Detection of Wind Shear 

[NASA-CP-2435] p5 N87-10054 

Pulse Code Modulation (PCM) data storage and analysis 

using a microcomputer 

[ NASA-TP-26291 p 13 N87-12718 

Electronics reliability and measurement technology 

[ NASACP-24721 p 17 N87-27204 

Liquid drop stability for protein crystal growth in 

microgravily 

[NASA-TP-2724] p21 N87-20727 

Effect of LID (Registered) processing on the 

microstructure and mechanical pr- of Ti-8AI-4V and 

Ti-6AI-2Sn-4Zr-2Mo titanium foil-gauge materials 

[ NASA-TP-26771 p 12 N87-18644 

Calculation of secondary electron trajectories in 

multistage depressed collectors for microwave amplifiers 

[ NASA-TP-28841 p 14 N87-17991 

Thay for computing the field scattered from a smth 

inflected surface 

[NASA-TP-2632] p24 N87-13264 

[NASACP-2449] p 27 N87-21785 

[NASA-RP-11881 p 19 N87-28955 

MICROCOMPUTERS 

MICROELECTRONICS 

MICROQRAVITY APPLICATIONS 

MICROSTRUCTURE 

MICROWAVE AMPLIFIERS 

MICROWAVES 

Rapid Fluctuations in Solar Flares 

Atlas of absorption lines from 0 to 17900 cm (sup)-1 

MIDDLE ATMOSPHERE 

Thirteenth International Laser Radar Conference 

[NASACP-2431] p 16 N87-10263 

Wind-tunnel investigation at supersonic speeds of a 

remote-controlled canard missile with a free-rolling-tail 

brake torque system 

[ NASA-TP-24011 p3 N87-17668 

Atmospheric . Turbulence Relative to Aviation. Missile. 

and Space Programs 

[ NASACP-24881 p21 N87-22341 

Mach 6 experimental and theoretical stability and 

pertormance of a crucitorm missile at angles of attack 

up to 65 degrees 

MISSION PLANNING 

MISSILE CONFIGURATIONS 

MISSILES 

[ NASA-TP-27331 P4 N87-23592 

Status and Mure of lunar gbscience 

[NASASP-lW] p 26 N87-19322 

MODAL RESPONSE 

Sensilkity Analysis in Engineering 

[ NASA-CP-2457) p 17 N87-18855 

Power cepstrum technigue with application to model 

helicopter acoustic data 

[ NASA-TP-25861 p 23 N87-17479 

Modeling of joints for the dynamic analysis of truss 

Sbuctures 

[ NASA-TP-2661 I p 18 N87-20587 

model Experimental fu determining validation acoustic of a two-dimensional impedance shear-flow 

[ NASA-TP-26791 p23 N87-20798 

Revised NASA aniclrly symmetric ring model for 

coupled-sbty mvehnpwave tubes 

[NASA-TP-26751 p 14 N87-22923 

Application of trubulencs modeling to predii surface 

heat transfer in stagnation flow region of circular cylinder 

[ NASA-TP-27581 p 15 N87-27161 

MODELS 

MOLECULAR CLOUDS star Formation in Galaxies 

[ NASA-CP-24661 p26 N87-24266 

A-10 
SUBJECT INDEX PERFORMANCE TESTS 

OSCILLATIONS 

Rapid Fluctuations in Solar Flares 

[NASAGP-24491 p 27 N87-21785 

Calculation of viscous effects on transonic flow for 

oscillating airfoils and comparisons with experiment 

[NASA-TP-2731 I p5 N87-27622 

Lowcost FM oscillator for capacitance type of blade 

tip clearance measurement system 

[ NASA-TP-27461 p 7 N87-24481 

Ester oxidation on an aluminum surface using 

chemiluminescence 

[NASA-TP-2611 I p12 N87-18686 

OXYGEN 

Electron stimulated desorption of atomic oxygen from 

silver 

[NASA-TP-2668] p 12 N87-18629 

Permeation of oxygen through huh purity. large grain 

silver 

[NASA-TP-2755] p 12 N87-27024 

A simplified method for determining heat of combustion 

of natural gas 

[NASA-TP-2682] p16 N87-20514 

Description of data on the Nimtus 7 LlMS map archive 

tape: Ozone and nitric acid 

[ NASA-TP-2825 I p 19 N87-13022 

Calibration of the spin-scan ozone imager aboard the 

dynamics Explorer 1 satellite 

[NASA-TP-2723] p 21 N87-26491 

OSCILLATORS 

OXIDATION 

OXYGEN SUPPLY EQUIPMENT 

OZONE 

MOLECULES 

Miavity aystallization of macromolecules: An 

interim report and pcoposal for continued research 

[NASA-TP-2671 I p 13 N87-20423 

MOON 

Status and future of lunar geoscience 

Fftv year canon of sdar eclipses: 1986 - 2035 

[ NASA-SP-484 I p 28 N87-19322 

[NASA-RP-1178-REV] p26 N87-25906 

Drag measurements of blunt stores tangentially mounted 

on a Hat plate at supersonic speeds 

[ NASA-TP-27421 p5 N87-27626 

MOUNTING 

N 

NASA PROGRAMS 

Management: A bibliography for NASA managers 

(supplement 21) 

[ NASA-SP-7500(21)1 p24 N87-20833 

NASA patent abstracts bibliography: A continuing 

bibliography. Section 1: Abstracts (supplement 31) 

[ NASA-SP-7039(31)1 p24 N87-25023 

NASA patent abstracts bibliography: A continuing 

bibliography. Section 2: Indexes (supplement 31) 

[ NASA-SP-7039(31)-SECT-21 p24 N87-26689 

NASA Thesaurvs supplement (supplement 3) 

[ NASASP-7053(SUPP-3)1 p 25 N87-27557 

Fifteenth NASTRAN Users’ Colloquium 

[ NASACP-24811 p 18 N87-27231 

NATURAL GAS 

A slmpli method for determining heat of combustion 

of natural gas 

[ NASA-TP-26821 p16 N87-20514 

Multiscale hwbulence effects in supersonic jets 

exhausting into still air 

[ NASA-TP-27071 p 15 N87-24672 

[ NASA-CP-24541 p4 N87-25998 

The Jovian Atmospheres 

[NASACP-2441 I p26 N87-17598 

NICKEL CADMIUM BATTERIES 

The 1985 Goddard Space Fliht Center Battery 

;?2?P-24341 p 14 N87-11072 

The 1985 Goddard Space Flight Center Battery 

E2P-24341 p 14 N87-11072 

AH618 of wide-fieldof-view outgoing bngwave radiation 

derived from Nimbus 6 Earth radiation budget data set. 

July 1975 to June 1978 

[NASA-RP-1185] p21 N87-26489 

Desaiption of data on the Nimbus 7 LlMS map archive 

tape: Ozone and nitric acid 

[ NASA-TP-28251 p 19 N87-13022 

Description of data on the Nimbus 7 LlMS map archive 

tape: Ozone and nitric acid 

[ NASA-TP-28251 pl9 N87-13022 

Effects of background noise on total noise annoyance 

[NASA-TP-2830] p23 N87-14120 

Effects of background noise on total noise annoyance 

NASTRAN 

NAVIER-STOKES EOUATION 

Supercomputing in Aerospece 

NEPTUNEATYOSPnERE 

NICKEL HYDROGEN BAlTERlES 

NIMBUS 6 SATELLITE 

NIMBUS 7 SATELUTE 

NITRIC ACID 

NOISE INTENSITY 

NOISE PouuTloN 

[ NASA-TP-28301 p23 N87-14120 

Effects of background noise on total noise annoyance 

[NASA-TP-2830] p23 N87-14120 

Lowcost FM oscillator for capadtance type of blade 

tip clearance measurement system 

[NASA-TP-2746] p7 N87-24481 

Electmnics reliability and measurementtechndogy 

[NASA-CP-2472] p 17 N87-27204 

Some pathfollowing lechniquesforsoluofnonlii 

equations and comparison with parametric differentiation 

[NASA-TP-26541 p 22 N87-14050 

Static internal performance of single-expansion-ramp 

[NASA-TP-2364] p2 N87-10839 

Expehmtal evaluation of heat transfer on a 1030:l 

area ratio rocket nozzle 

[NASA-TP-2726] p 11 N87-25424 

Effect of pat caner Beometry on the intemal 

performance of a rotating-vanetype thrust revmer 

[NASA-TP-2624] p2 N87-12541 

NOISE TOLERANCE 

NONDESTRUCTIVE TESTS 

NONUNEAR EWATK)IIS 

NO- FLOW 

nonleswim mnrst-vectocing capaality up to 60 deg 

NOzzL€ aEoMETRY 

Effects of empennage surface location on aerodynamic 

characteristics of a twin-engine afterbody model with 

nonaxisymmetric nozzles 

[NASA-TP-23921 p 6 N87-17693 

Expeimental thrust peffwmance of a high-area-ratio 

rocket nozzle 

[NASA-TP-2720] p 10 N87-20381 

Effect of a trade between battail angle and wedge size 

on the performance of a nonaxisymmetric wedge node 

[ NASA-TP-27171 p4 N87-23593 

Effects of afterbody boaltail design and empennage 

arrangement on aeropropulsive characteristics of a 

twin-engine lighter model at transonic speeds 

[ NASA-TP-27041 p3 N87-21873 

Possible complementary cosmic-ray systems: Ndei 

and antinuclei 

[NASA-TP-2741 I p 24 N87-24977 

NUMERICAL ANALYSS 

Jet model for slot film cooling with effect of free-stream 

andcoolanltubulence 

[ NASA-TP-26551 p 15 N87-18034 

A sewdodw accuate kinetic-theory-based method 

for inviscid compessibk, flows 

[NASA-TP-2613] p 15 N87-18783 

On minimizing the number of calculations in 

[ NASA-TP-27061 p3 N87-23586 

NOZZLES 

NUCLEI (NUCLEAR PHYSICS) 

desgn-bYana)ysis0 

OBLIQUE WINQS 

In-flight total forces, moments and static aeroelastic 

characteristics of an OMiUewing research airplane 

[NASA-TP-2224] p8 N87-10103 

Fliiht-determined aerodynamic derivatives of the AD1 

obliquewing research airplane 

[ NASA-TP-22221 p8 N87-10871 

Fliht characteristics of the AD1 obliquewing research 

aircraft 

[NASA-TP-2223] p 8 N87-18570 

Arctic Sea ice. 1973-1976 Satellite passivemicrowave 

obsewations 

[ NASA-SP-4891 p 21 N87-24870 

OCEANOGRAPHIC PARAMETERS 

OCTANES 

Velocity profiles in laminer diffusion flames 

[NASA-TP-2596] p 15 N87-18035 

In-fliiht surface oil-flow photographs with comparisons 

to pressure distribution and boundary-layer data 

[NASA-TP-2395] p3 N87-200966 

Sixth Annual Users’ Conference .-- Transportable 

Applications Executive (TAE) 

[NASACP-2463] p 22 N87-23156 

OPTICAL DATA PAocESslNG 

Computer sdences and Data Systems, volume 2 [NASACP-2459-VOL-21 p 22 N87-19932 

Thirteenth International Lesec Radar Conference 

[NASA-CP-2431] p 16 N87-10263 

Airborne li measurements of El Chichon stratospheric 

aerosols. May 1983 

[NASA-RP-l172] pl9 N87-11358 

NASAlMSFC FY-85 Atmospheric Processes Research 

Review 

[NASA-CP-2402] p 20 N87-13043 

Airborne li measurements of El Chiin stratospheric 

aBTo8ds. Jarmery 1984 

[NASA-RP-l175] p20 N87-20663 

Recent Experiences in Multidisciplinary Anaiysis and 

Optimization, part 1 [NASACP-2327-PT-l] p5 N87-11717 

Recent mnces in Multidisciplinary Analysts and 

[ NASA-CP-2327-PT-21 p6 N87-11750 

[NASACP-2457] p 17 N87-18855 

OILS 

OPERATING SYSTEMS (COMPUTERS) 

OPTICAL RADAR 

OPnMUATKm, 

optimization. part 2 

SensitMy Analysis in Engineering 

ORBITAL SPACE STATIM 

proceedings of the 5th Annual Users’ Conference 

[ NASACP-23991 p 22 N87-10720 

Sbuctural Dynamics and Control Interaction of Flexible 

Sbuctues 

[ NASACP-2467-PT-21 p 10 N87-22729 

NASAlDOD ControllSbuctures Interaction Techndogy, 

1988 

[NASA-CP-2447-PT-21 p 10 N87-24495 

~ualitative evaluation of a flush air data system at 

transonic ape& and hgh angles of attack 

[ NASA-TP-27161 p6 N87-29497 

ORIFICE FLOW 

P 

PANEL METHOD (FLUID DYNAMICS) 

Steady and unsteady aerodynamic forces from the 

SOUSSA surface-panel method for a fighter wing with tip 

missile and comparison wilh experiment andPANAlR 

[ NASA-TP-27361 p4 N87-28032 

Frontiers of Massively Parallel Scientific Computation 

[ NASA-CP-24781 p22 N87-28531 

PARALLEL COMPUTERS 

PARALLEL PROCESSING (COMPUTERS) 

Computer Sciences and Data Systems, volume 2 

[ NASA-CP-2459-VOL-21 p 22 N87-19932 

Frontiers of Massively Parallel Scientific Computation 

[ NASA-CP-24781 p22 N87-28531 

Some path-following techniques for solution of nonlinear 

equations and comparison with parametric differentiation 

[ NASA-TP-26541 p22 N87-14054 

Application of parameter estimation to aircraft stability 

and control: The oulput-error approach 

[NASA-RP-1168] p6 N87-29499 

PARTIAL DIFFERENTIAL EQUATIONS 

Solution of elliptic partial differential equations by fast 

Poisson solvers using a local relaxation factor. 2 Twatep 

method 

[ NASA-TP-25301 p 22 N87-14918 

Doubly differential cross sections for galactic heavy-ion 

fragmentation 

[ NASA-TP-28591 p24 N87-17487 

PARAMETER IDENTIFICATION 

PARTICLE COLLISIONS 

PARTICLE SIZE DISTRIBUTION 

Automated eduction of Data from Images and 

Holograms 

[NASACP-24771 p5 N87-29432 

Calculation of secondary electron trajectories in 

multistage depressed collectors for microwave amplifiers 

[ NASA-TP-2664 I p14 N87-17991 

NASA patent abstracts bibliography: A continuing 

bibliography. Section 1: Abstracts (supplement 31) 

[ NASA-SP-7039(31)1 p24 N87-25023 

NASA patent abstracts bibliography: A continuing 

bibliography, Section 2: Indexes (supplement 31) 

PARTICLE TRAJECTORIES 

PATENT POUCY 

[ NASA-SP-7039(31 )-SECT-Z] p24 N87-26609 

PATENTS 

Sinificant NASA inventions. Available for licensing in 

p25 N87-70425 

Development and evaluation of an airplane electronic 

display fwmat alined with the inertial velodtyvector 

[ NASA-TP-26481 p 7 N87-13438 

Design of 9.27l-pressureratio Sstage core compessor and overall performance for first 3 stages 

[ NASA-TP-25971 p7 N87-17699 

Bit-error-rate testing of high-power SGHz traveling 

wave tubes for ground-terminal applications 

[ NASA-TP-26351 p 13 N87-17971 

foreign wuntfies 

[ NASASP-7038(04)] 

PERFORMANCE TESTS 

A-1 1 
PERMEATING SUBJECT INDEX 

PROTEIN SYNTHESIS 

Liquid drop stability for protein crystal growth in 

p 21 N87-20727 

Aerothermal tests of spherical dome protuberances on 

p14 N87-13664 

Annoyance response to simulated advanced turboprop 

p 23 N87-24181 

Pulse Code Modulation (PCM) encoder handbook for 

Aydin Vector MMP-MM series system 

[NASA-RP-1171] p 13 N87-11918 

Pulse Car% Modulation (PCM) data storage and analysis 

using a microcomputer 

[ NASA-TP-26291 p 13 N87-12718 

Threestep cylindrical seal for high-performance 

turbomachines 

[NASA-TP-1849] p 15 N87-24639 

PURITY 

Permeation of oxygen through high purity, large grain 

silver 

[ NASA-TP-27551 p 12 N87-27024 

Low-speed aerodynamic characteristics of a twin-engine 

general aviation configuration with aft-fuselage-mounted 

pusher propellers 

[ NASA-TP-27631 p 5 N87-29462 

Design. fabrication and performance of small, graphite 

electrode, multistage depressed collectors with 200-W, 

CW. 8- to 18-GHz traveling-wave tubes 

[ NASA-TP-2693 ] p 14 N87-20474 

Effects of variables upon pyrotechnically induced shock 

p 17 N87-12921 

microgravity 

[ NASA-TP-27241 

PROTUBERANCES 

a flat plate at a Mach number of 8.5 

[ NASA-TP-2631 I 

PSYCHOLOGICAL EFFECTS 

aircraft interior noise containing tonal beats 

[NASA-TP-2689] 

PULSE CODE MOWLATION 

PUMP SEALS 

PYLON MOUNTING 

PYRoLmc GRAPHITE 

PYROTECHNICS 

response spectra 

[NASA-TP-26031 

Effect of a trade between boattail angle and wedge sue 

on the performance of a nonaxisyrnmetric wedge nozzle 

[NASA-TP-2717] p4 N87-23593 

Engineer in charge: A history of the Langley Aeronautical 

Laboratwy. 1917-1958 

[NASA-SP-4305] p27 N87-24390 

Permeation of oxygen through high purity. large grain 

silver 

[ NASA-TP-27551 p 12 N87-27024 

Engineer in charge: A history of the Langley Aeronautical 

PERMEATING 

PERSONNEL 

Labocatory. 1917-1958 

[NASA-SP-4305] p27 N87-24390 

PERSONNELMANAGEMENT 

Cockpit Resource Management Training 

[ NASA-CP-24551 p5 N87-22634 

Geomcnphdogy from space: A global overview of 

regional landforms 

[NASA-SP-486] p 18 N87-18139 

In-fliiht surface oil-flow photographs with comparisons 

PHOTOOEOLOGY 

PHOTOGRAPHY 

to pcessure distribution and boundary-layer data 

Atlas of Comet Halley 1910 II 

[NASASP-488] p 26 N87-30235 

PHOTOVOLTAIC CONVERSION 

Space Photovoltaic Research and Technology 1986. 

Hgh Efficiency, Space Environment and Array 

Technology 

[ NASA-CP-24751 p 19 N87-26413 

PILOT PERFORMANCE 

Wind ShearfTurbulence Inputs to Flight Simulation and 

Systems Cmification 

[ NASA-CP-24741 p 1 N87-25267 

PILOTS (PERSONNEL) 

Ground-based timeguidance a!gmthm for control of 

airplanes in a timemetered air traffic control environment: 

A piloted simulation study 

[ NASA-TP-26161 p7 N87-10864 

Piloted-simulation study of effects of vortex flaps on 

low-speed handling quali of a Delta-wingai~~Aane 

[NASA-TP-27471 p8 N87-26922 

Prooaaation of sound waves in tubes of noncircular cross 

[ NASA-TP-23951 p3 N87-2GSS6 

PIPES (TUBES) 

.I 

section 

[NASA-TP-PEOl I 

PITOT TUBES 

p2 N87-14284 

Qualitative evaluation of a flush air data system at 

transonic speeds and high angles of attack 

[ NASA-TP-2716 I p8 N87-29497 

Prediied effect of dynamic load on pitting fatigue lie 

PITTING 

for lowcontact-ratio spur gears 

[NASA-TP-PBl O] p 16 N87-18095 

PLANET EPHEMERIDES 

Ten year planetary ephemeris: 1986-1995 

[NASA-RP-11761 p 25 N87-14219 

PLANETARY ORBITS 

Ten year planetary ephemeris: 1986-1995 

[NASA-RP-1176] p 25 N87-14219 

PLASMA LAYERS 

Double Layers in Astrophysics 

[NASACP-2469] p 25 N87-23313 

[NASACP-2449] p 27 N87-21785 

[ NASACP-24691 p 25 N87-23313 

PLASMA PHYSICS 

Rapid Fluctuations in Solar Flares 

DwMe Layers in Astrophysics 

Cwonal and Prominence Plasmas 

PLASMAS (PHYSICS) 

[ NASACP-24421 p26 N87-20871 

Expenmental evaluation of blockage ratio and plenum 

evacuabon system flow effects on pressure distribution 

for bodies of revdubon in 0.1 scale model test section 

of NASA Lewis Research Center's proposed altitude wind 

tunnel 

[NASA-TP-2702] p9 N87-22694 

POLLUTION TRANSPORT 

Ai- li measurements of El Chiin stratospheric 

aerds. January 1984 

[ NASA-RP-11751 p20 N87-20663 

Microgravity crystallization of macromolecules: An 

interim report and proposal for continued research 

[ NASA-TP-2671 I P 13 N87-20423 

Effect of pcil comer geomebv on the internal 

performance of a rotating-vane-type thrust reverser 

[ NASA-TP-26241 p2 N87-12541 

Calculation and accuracy of ERBE scanner 

measurement locations 

[NASA-TP-2670] p25 N87-28471 

PLENUM CHAMBERS 

POLYMER CHEMISTRY 

PORTS (OPENINGS) 

POSITION (LOCATION) 

POSTFLIGHT ANALYSIS 

Spacelab 3 Mission Science Review 

[ NASA-CP-24291 p 15 N87-22103 

POWERED LIFT AIRCRAFT 

PrOceedingsofthe 1985 NASA Ames Research Center's 

Ground-Effects Workshop 

[ NASA-CP-24621 p4 N87-24410 

PREDICTION ANALYSIS TECHNIQUES 

Turbine Engine Hot Section Technology, 1984 

[ NASA-CP-23391 p 17 N87-11180 

Aerothermal tests of spherical dome protuberances on 

a flat plate at a Mach number of 6.5 

[NASA-TP-2631] p14 N87-13664 

Effects of winglet on transonic flutter characteristics of 

a cantilevered twin-enginetransport wing model 

[NASA-TP-26271 p 17 N87-13789 

Aerothermal evaluation of a spherically blunted body 

with a trapezoidal cross section in the Langley 8-foot 

high-temperature tunnel 

[ NASA-TP-26411 p 15 N87-18782 

Development of confidence limits by pivotal functions 

for estimating software reliability 

[ NASA-TP-27091 p23 N87-23244 

Comparison of theoretical and experimental thrust 

performance of a 10301 area ratio rocket nozzle at a 

chamber pressure of 2413 kN/m2 (350 psia) 

[ NASA-TP-27251 p 11 N87-25423 

In-flight surface oil-flow photographs with comparisons 

to pressure distribution and boundary-layer data 

[NASA-TP-2395] p3 N87-20966 

Experimental cavity pressure distributions at supersonic 

speeds 

[ NASA-TP-26831 p3 N87-22626 

On minimizing the number of calculations in 

design-by-analysis codes 

[ NASA-TP-27061 p 3 N87-23586 

Expenmental evaluation of honeycomblscreen 

configurations and short contraction section for NASA 

Lewis Research Center's altitude wind tunnel 

[ NASA-TP-26921 p9 N87-23662 

Aerothermal evaluation of a spherically blunted body 

with a trapezoidal cross s&b in the Langley 8-loot 

high-temperature tunnel 

[NASA-TP-26411 p 15 N87-18782 

Pressure measurements on a thick cambered and 

twisted 58 deg delta wing at high subsonic speeds 

[NASA-TP-2713] p5 N87-27643 

The corrosion mechanisms for primer coated 2219-T87 

aluminum 

[NASA-TP-2715] p 12 N87-21076 

Solution of elliptic partial differential equations by fast 

Poisson solvers using a local relaxation factor. 2: Two-step 

method 

[NASA-TP-2530] p 22 N87-14918 

Efficient solutions to the Euler equations for supersonic 

flow wim embedded subsonic regions 

[ NASA-TP-25231 p2 N87-15183 

Summary of studies to reduce wing-mounted pcopfan 

installation drag on an M = 0.8 transport 

[ NASA-TP-26781 p6 N87-20990 

Evaluation of installed performance of a 

wing-tipmounted pusher tuhqxop on a semispan wing 

[ NASA-TP-27391 p8 N87-26041 

Low-speed aerodynamic characteristics of a twin-engine 

general aviatjon configuration with aft-fuselagemounted 

[NASA-TP-27631 p5 N87-29462 

Low-speed aerodynamic characteristics of a twin-engine 

general aviation configuration with aft-fuselagemounted 

[ NASA-TP-27831 p5 N87-29462 

[NASA-RP-1146] p 8 N87-10876 

Effects of afterbody boattail design and empennage 

arrangement on aeropropulsive characteristics of a 

twin-engine fighter model at transonic speeds 

[ NASA-TP-27041 p3 N87-21873 

Effect of LID (Registered) processing on Me 

microstructure and mechanical properties of Ti-6AI-W and 

Ti-6AI-2Sn-4Zr-2Mo titanium foilgauge materials 

[ NASA-TP-26771 p12 N87-18644 

The mfrosion mechanisms for primer coated 2219-T87 

aluminum 

[NASA-Tp-2715] p 12 N87-21076 

PREDICTIONS 

PRESSURE DISTRIBUTION 

PRESSUREMEASUREMENT 

PRIMERS (COATINGS) 

PROBLEM SOLVING 

PROP-FAN TECHNOLOGY 

PROPELLERS 

pu* prcmPROPULSION SYSTEM CONFIGURATIONS 

e PrWk 

PROPULSION SYSTEM PERFORMANCE 

Aeronautical facili aSSeSSment 

PROPULSIVE EFFICIENCY 

PROTECTIVE COATINGS 

Q 

QUALITY CONTROL 

Electronics reliability and measurement technology 

[ NASA-CP-24721 p 17 N87-27204 

Quantitative analysis of the reconstruction performance 

of interpolants 

[NASA-TP-26881 p 23 N87-22441 

QUANTITATIVE ANALYSIS 

R 

RADAR EQUIPMENT 

Thirteenth International Laser Radar Conference 

[NASACP-2431] p 16 N87-10263 

RADARMEASUREMENT 

Doppler Radar Detection of Wind Shear 

[ NASA-CP-24351 p 5 N87-10054 

Spectroscopic comparison of effects of electron 

radiation on mechanical properlies of two polyimides 

RADIATION DAMAGE 

[NASA-TP-2663] p 11 N87-18611 

RADIO ASTRONOMY 

[ NASA-CP-24421 p26 N87-20871 

[NASA-CP-2466] p26 N87-24266 

Coronal and Prominence Plasmas 

Star Formation in Galaxies 

RADIO WAVES 

Rapid Fluctuations in Solar Flares 

[NASACP-2449] p 27 N87-21785 

Cosmic ray heavy ion LET mapping for aluminum, silicon, 

RADIOBIOLOGY 

and tissue targets 

[NASA-RP-11801 p 27 N87-25984 

RADIOSONDES 

Preliminary estimates of radiosonde thermistor errors 

[ NASA-TP-26371 p20 N87-12086 

On requirements for a satellite mission to measure 

[NASA-RP-1183] p20 N87-20701 

RAIN GAGES 

tropical rainfall 

RATIONAL FUNCTIONS 

An algorithm for surface smoothing with rational 

[ NASA-TP-27081 p 23 N87-22447 

Desaiption and calibration of the Langley Hypersonic 

CF4 tunnel: A facility for simulating low gamma flow as 

occurs for a real gas 

[ NASA-TP-23841 p 16 N87-29778 

splines 

REAL GASES 

A-12 
SUBJECT INDEX SHOCK LOADS 

REAL TIME OPERATION 

Applications and requirements for real-time simulators 

in grwnd-test faali 

[NASA-TP-2672] p22 N87-23202 

Supersonic, nonlinear, attached-flow wing destgn for 

hgh IR with experimental validation 

[ NASA-TP-23361 p 1 N87-10042 

Quantitative analysis of the reconstruction performance 

of interpdants 

[ NASA-TP-26881 p23 N87-22441 

Microgravity crystallization of macromolecules: An 

interim report and proposal for continued research 

[NASA-TP-2671] p 13 N87-20423 

Microgravity crystallization of macromolecules: An 

interim report and proposal for continued research 

[ NASA-TP-26711 p 13 N87-20423 

Spacelab 3 Mission Science Review 

[ NASA-CP-24291 p 15 N87-22103 

Advanced detection. isolation and aCcOmmodation of 

sensor failures: Real-time evaluation 

[ NASA-TP-27401 p8 N87-25331 

Finiteelement reentry heat-transfer analysis of space 

shuttleorbiter 

[NASA-TP-2657] p16 N87-29795 

REFLECTANCE 

Tkoty for computing the field scattered from a smooth 

inflected surface 

[NASA-TP-26321 p24 N87-13264 

Space Electrochemical Research and Technology 

(SERT) 

[ NASACP-24841 p19 N87-29914 

REQIONS 

Geomorphology from space: A global overview of 

regional landforms 

[NASA-SP-486] p 18 N87-18139 

Calibration of the spin-scan ozone imager aboard the 

dynamics Explorer 1 satellite 

[ NASA-TP-27231 p21 N87-26491 

Effects of thermal cycling on graph-fiber-reinforced 

6061 aluminum 

[NASA-TP-2612] pll N87-10184 

Development of confidence limits by pivotal functions 

for estimating software reliility 

[NASA-TP-2709] p23 N87-23244 

Electmni relili and measurementtechnology 

[ NASA-CP-24721 p 17 N87-27204 

Wind-tunnel invesligation at supersonic speeds of a 

remotecontrolled canard missile with a free-rolling-tail 

brake torque system 

[NASA-TP-2401] p 3 N87-17868 

SAGE aerosol measurements. Volume 3 January 1. 

1981 to November 18,1981 

[NASA-RP-1173] p 19 N87-17417 

Geomorphology from space: A global overview of 

regional landforms 

[NASA-SP-4861 p 18 N87-18139 

Research 

INASACP-24501 p20 N87-18248 

System study of the carbon dioxide observational 

platform system (CO-OPS): Project overview 

[NASA-TP-Z6698] p9 N87-18588 

Earth rescurcaa: A continuing bibli with indexes 

(issue 54) 

[NASASP-7041(54)] p 18 N87-27315 

Effects of .aerosols and surface shadowing on bidirectional refiectance measurements of deserts 

[ NASA-TP-27581 p 19 N87-28182 

Cakulation and accuracy of ERBE scanner 

measurement IoCaIium 

[ NASA-TP-28701 p25 N87-28471 

Atlas of absorption lines from 0 to 17900 un (sup)-l 

[NASA-RP-1188] pl9 N87-28955 

Advanced detection. isolation and accommodation of 

sensor failures: Real-time evaluation 

[ NASA-TP-27401 p8 N87-25331 

NASA scientific and technical publications: A catalog 

of Special Publiications. Reference Publications. 

Conference Publiicabons. and Technical Papera. 

1977-1 986 

[NASA-SP-7063] p 25 N87-30218 

REATTACHED FLOW 

RECONSTRUCTION 

RECRYSTALLIZATION 

REDUCED QRAVITY 

REDUNDANCY ENCODING 

REENTRY SHIEUHNQ 

REQENERATIVE FUEL CELLS 

REQRESSION ANALYSIS 

REINFORCINQ FIBERS 

RELIABILITY ANALYSIS 

RELIABILITY ENQINEERINQ 

REMOTE CONTROL 

REMOTE SENSINQ 

Space Opportunities for Tropospheric ' chemistry 

REMOTE SENSORS 

RESEARCH 

RESEARCH AIRCRAFT 

In-flight total forces. moments and static aeroelastic 

characteristics of an oblique-wing research airplane 

[ NASA-TP-22241 p8 N87-10103 

Flightdetermined aerodynamic derivatives of the AD-1 

oblique-wing research airplane 

[ NASA-TP-22221 p8 N87-10871 

Flight investigation of the effect of tail configuration on 

stall, spin, and recovery characteristics of a low-wing 

general aviation research airplane 

[ NASA-TP-26441 p6 N87-16815 

Fliiht characteristics of the AB1 oblquewing research 

aircraft 

[ NASA-TP-22231 p 8 N87-18570 

New methods and resuits fOi quantification of 

lghtning-aircraft eldmdymmb 

[ NASA-TP-27371 p3 N87-21871 

RESEARCH FACILITIES 

Engineer in charge: A history of the Langley Aeronautical 

Laboratory, 1917-1958 

The ACEE program and basic composites research at 

Langley Research Center (1975 to 1986): Summaty and 

[ NASA-RP-11771 p 11 N87-29612 

Closedcycle, Frequency-Stable co2 Laser 

Technology 

[NASA-CP-2456] p 16 N87-20522 

RESFONSES 

Annoyance response to simulated advanced turboprop 

aircraft interior noise containing tonal beats 

[ NASASP-43051 p27 N87-24390 

biblibgraphV 

RESEARCH MANAQEMENT 

[NASA-TP-2689] p 23 N87-24161 

REVISIONS 

Flight investigation of the effects of an outboard 

wing-leading-edge Mition on stalllspin 

characteristics of a low-wing, single-engine. T-tail liht 

airplane 

[NASA-TP-2691] p6 N87-23614 

Effect of Reynolds number variation on aerodynamics 

of a hydrogen-fueled transport concept at Mach 6 

[NASA-TP-2728] p4 N87-26031 

Revised NASA axially symmetric ring model for 

coupledewily traveling-wave tubs 

[ NASA-TP-28751 p 14 N87-22923 

REYNOLDS NUMBER 

RlNQS 

ROBOTICS 

The 2181 Aerospace Mechanisms Symposium 

[NASAGP-24701 p 18 N87-29858 

Preliminary design of turbopumps and related 

machinery 

[NASA-RP-1170] p2 N87-17665 

Experimental thrust perfmance of a high-area-ratio 

Comparison of theoretical and experimental thrust 

performance of a 103o:l area ratio rocket nozzle at a 

chamber pressure of 2413 kNlm2 (350 psia) 

[NASA-TP-2725] p 11 N87-25423 

Experimental evaluation of heat transfer on a 10301 

area ratio rocket nozzle 

[NASA-TP-2726] p 11 N87-25424 

ROCKET THRUST 

Expenmental hat performance of a high-area-ratio 

rocket nozzle 

[ NASA-TP-27201 p 10 N87-20381 

Comparison of theoretical and experimental thrust 

performance of a 103o:l area ratio rocket nozzle at a 

chamber pressure of 2413 kNlm2 (350 psia) 

[ NASA-TP-27251 p 11 N87-25423 

Wind-tunnel investigation at supersonic speeds of a 

remote-contrdled canard missile with a free-rdling-tail 

brake toque system 

[NASA-TP-2401] p3 N87-17668 

Effect of port tamer geometry on the internal 

pformance of a rotating-vane-type thrust reverser 

[ NASA-TP-28241 p2 N87-12541 

Vibration characterishof OH-58A helicopter main rotor 

v- 

[ NASA-TP-27051 p 17 N87-20555 

Rotordynamic Instabill hoblems in Hih-Performance 

[ NASACP-24431 p 17 N87-22199 

ROCKET EWalNE DESIQN 

ROCKET NOZLES 

rocket nozzle 

[NASA-TP-27201 p 10 N87-20381 

ROLLING MOMENTS 

ROTATING BODIES 

ROTOR AERODYNAMICS 

Tubomad-u 'W. 1986 

ROTOR BLADES (TURBOMACHINERY) 

Turbine Engine Hot SeCtDn Technology. 1984 

Design of 9.271 pressureratio 5-stage co1e compressor 

and overall p6dormance fa first 3 stages 

[ NASA-TP-25971 p 7 N87-17699 

[NASA-CP-2339] p17 N87-11180 

Correlation of heliter impulsive noise from 

blade-voltex interaction with rotor mean inflow 

[NASA-TP-28501 p 23 N87-18399 

Low-cost FM oscillator for capacitance type of blade 

tip clearance measurement system 

p 7 N07-24481 [NASA-TP-27461 

Transonic flow analysis for rotors. Part 2: 

Threedimensional, unsteady, full-potential calculation 

p2 N87-10841 

Helicopter blade-vortex interaction locations: 

Scalemodel acwstics and free-wake analysisresults 

[ NASA-TP-2658) p3 N87-18537 

Preliminary structural design of composite main rotor 

blades for minimum weight 

[NASA-TP-2730] p 11 N87-25435 

ROTORS 

[NASA-TP-2375-PT-21 

RUNWAYS 

Langley Aircraft 

[NASA-RP-11891 

Landing Dynamics Facili 

P9 N87-29544 

S 

SAQE SATELLITE 

SAGE aerosol measurements. Volume 3 January 1, 

1981 to November 18,1981 

[NASA-RP-l173] p 19 N87-17417 

A synchronous data analyzer for the Minimum Delay 

Data Fomt (MDDF) and Launch Tra@toly Acquisition 

System (LTAS) 

[ NASA-TP-27431 p 13 N87-24590 

Unique bit-enor-rate measurement system for satellite 

communication systems 

[NASA-TP-2699] p 13 N87-20448 

NASAlMSFC FY-85 Atmospheric Processes Research 

Review 

[ NASA-CP-24021 p20 N87-13043 

Arctic Sea ice, 1973-1 976 Satellite passive-microwave 

observations 

[ NASA-SP-489) p21 N87-24070 

Geomorphology from space: A global overview of 

[NASA-SP-488] p 18 N87-18139 

SAMPLINQ 

SATELLITE COMMUNICATION 

SATELLITE IMAQERY 

SATELLITEgORNE PHOTOORAPHY 

regional Worms 

SATURN ATYOSPHERE 

The Jovian Atmospheres 

[NASA-CP-2441] p 26 N87-17508 

Calculation and accuracy of ERBE scanner 

measurement locations 

[NASA-TP-2670] p25 N87-28471 

Doubly differential NOSS sections for galactic heavy-ion 

fragmentation 

[ NASA-TP-28591 p 24 N87-17487 

Experimental evaluation of honeycomblscreen 

configurations and short contradim section for NASA 

Lewis Research Center's altitude wind tunnel 

[ NASA-TP-28921 p9 N87-23882 

Space shutwe main engine huh pressure fuel pump aft 

platform seal cavity flow analysis 

[ NASA-TP-26851 p14 N87-17000 

Straight cylindrical seal for high-performance 

turbomachines 

[ NASA-TP-18501 p 15 N87-23936 

Evaluation of installed performance of a 

wing-tipmounted pusher tu-op on a semispan wing 

[NASA-TP-2739] 

SCANNINQ 

SCAllERlNQ CROSS SECTIONS 

SCREENS 

SEALS (STOPPERS) 

SEMISPAN MODELS 

p6 N87-28041 

SENSITIVITY 

SenSitMty Adysis in Engineering 

[ NASA-CP-24571 p 17 N87-18855 

Effects of aerosols and surface shadowing on bidirectional reflectance measurements of deserts 

[NASA-TP-27561 p 19 N87-28162 

Applicability of linearized-thewy attached-flow methods 

to descgn and analys~s of flap systems at low speeds for 

thin swept wings with sharp leading edges 

[NASA-TP-2653] p2 N87-15174 

Experimental validation of a twodimensional ahear-flow 

SHADOWS 

SHARP LEAMNQ EWES 

SHEAR FLOW 

model for determining acoustic impedance 

[NASA-TP-2679] p23 N87-20798 

SHOCK LOADS 

Effects of variables upon pyotechnically induced shock 

r-fm=sPecba 

[ NASA-TP-26031 p 17 N87-12921 

A-13 
SHOCK SPECTRA SUBJECT INDEX 

SHOCK SPECTRA 

response spectra 

Effects of variables upon pyrotechnically induced shock 

[NASA-TP-2603 I p 17 N87-12921 

SHOCK WAVE PROPAGATION 

A second-order accurate kinetic-theory-basad method 

for inviscid compressible flows 

[NASA-TP-26131 p 15 N87-18783 

Large-scale static investigation of 

circulationcontrol-wing concepts applied to upper 

surface-blowing aircraft 

[NASA-TP-2684] p6 N87-15959 

Shot peening for Ti-6AI-4V alloy compressor blades 

[NASA-TP-2711] p 18 N87-20566 

Frequency domain laser velocimeter signal processor: 

A new signal processing scheme 

[NASA-TP-27351 p 16 N87-27994 

Analog signal conditioning for flight-test 

instrumentation 

[NASA-RP-1159] p 7 N87-29533 

Power cepsbum technique with application lo model 

helicopter acoustic data 

[ NASA-TP-25861 p 23 N87-17479 

Cosmic ray heavy ion LET mapping for aluminum, silicon, 

and tissue targets 

[NASA-RP-1 1801 p27 N87-25984 

SILVER 

Electron stimulated desorptbn of atomic oxygen from 

silver 

[NASA-TP-2668] p 12 N87-18629 

Permeation of oxygen through high purity. large grain 

silver 

[NASA-TP-27551 p 12 N87-27024 

SHORT TAKEOFF AIRCRAFT 

SHOT PEENING 

SIQNAL PROCESSING 

SIGNAL REFLECTION 

SILICON 

SIMULATORS 

Applications and requirements for real-time simulatws 

in ground-test facilities 

[NASA-TP-2672] p 22 N87-23202 

SINGLE EVENT upsm 

Cosmic ray heavy ion LET mapping for aluminum, silicon, 

[NASA-RP-11801 p27 N87-25984 

Effects of tail span and empennage arrangement on 

drag of a typical single-engine fighter aft end 

[NASA-TP-2352] pl N87-10838 

An algmlhm for surface smoothing with rational 

splines 

[ NASA-TP-27081 p23 N87-22447 

and tissue targets 

SKIN FRICTION 

SMOOTHING 

SOFWARE ENGINEERING 

Proceedings of the 5th Annual Users' Conference 

Computer Sciences and Data Systems, volume 1 

Development of confidence limits by pivotal functions 

for estimating software reliability 

[NASA-TP-2709] p23 N87-23244 

[NASA-CP-2399] p22 N87-10720 

[ NASA-CP-2459-VOL-l] p 22 N87-19931 

SOFWARE TOOLS 

Proceedings of the 5th Annual Users' Conference 

Solar array flight dynamic experiment 

[ NASA-TP-25981 p9 N87-12581 

sdar array flight experimentldynamic augmentation 

experiment 

[NASA-TP-2690] p 10 N87-20380 

[NASACP-2399] p22 N87-10720 

SOLAR ARRAYS 

SOLAR ATMOSPHERE 

coronal and Prominence Plasmas 

[NASA-CP-2442] p26 N87-20871 

SOUR CELLS 

Space Photovoltaic Research and Technology 1986. 

High Efficiency. Space Environment. and Array 

:$SA324751 p 19 N87-26413 

Energetic phenomena on the Sun: The Solar Madmum 

Min Flare Workshop. Proceedings 

[NASACP-2439] p '26 N87-19328 

comnal and Prominence Plasmas 

[NASACP-24421 p26 N87-20871 

SOLAR DYNAMIC POWER SYSTEYS 

Solar array flight experimentldynamic augmentation 

experiment 

[NASA-TP-26901 p10 N87-20380 

SOLAR CORONA 

SOLAR ECLIPSES 

FW year canon of solar eclipses: 1966 - 2035 

[NASA-RP-1178-REV] P26 N87-25906 

Energetic Phenomena on the Sun: The Solar Maximum 

Mi Flare Workshop. Proceedings 

[ NASACP-24391 p26 N87-19328 

SOURFURES 

Statistical aspects of solar flares 

Rwd Fluctuations in Solar Flares 

[NASA-TP-2714] p 27 N87-20947 

[ NASA-CP-24491 p 27 N87-21785 

Energetic Phenomena on the Sun: Ttw Solar Maximum 

Mission Flare Workshop. Proceedings 

[NASA-CP-2439] p 26 N87-19328 

Coronal and Prominence Plasmas 

[ NASA-CP-24421 p 26 N87-20871 

Energetic Phenomena on the Sun: The Solar Maximum 

Mission Flare Workshop. Proceedings 

[ NASA-CP-24391 p 26 N87-19328 

Energetic Phenomena on the Sun: The Solar Maximum 

Mission Flare Workshop. Proceedings 

[NASA-CP-2439] p 26 N87-19326 

Cwonal and Prominence Plasmas 

[ NASA-CP-24421 P26 N87-20871 

Surface bidirectional reflectance properties of two 

Southwestern Arizona deserts for wavelengths between 

0.4 and 2.2 miaometers 

SOLAR MAGNETIC FIELD 

SOLAR MAXIMUM MISSION 

SOLAR PHYSICS 

SOLAR MION 

[ NASA-TP-26431 p 18 N87-22281 

SOLAR POWER SATELLITES 

Technology for Large Space Systems. A bibliraphy 

with indexes (supplement 17) 

[NASA-SP-7046(17)] p9 N87-29576 

Energetic Phenomena on the Sun: The Solar Maximum 

Mission Flare Workshop. Proceedings 

[ NASA-CP-24391 p 26 N87-19328 

Coronal and Prominence Plasmas 

[ NASACP-24421 p26 N87-20871 

Statistical aspects of solar flares 

[NASA-TP-2714] p27 N87-20947 

Propagation of sound waves in tubes of noncircular cross 

section 

[NASA-TP-2801] p2 N87-14284 

SOLAR PROMINENCES 

SOUND WAVES 

SPACE COMMERCIALIZATION 

Spacelab 3 Mission Science Review 

[ NASACP-24291 p 15 N87-22103 

Technology for Large Space Systems. A bibliiraphy 

with indexes (supplement 17) 

[NASA-SP-7046(17)] p9 N87-29576 

War array flight experimentldynamic augmentation 

experiment 

[ NASA-TP-26901 p 10 N87-20380 

Space station systems: A bibliography with indexes 

[ NASA-SP-7056(04)] p 10 N87-26073 

The 2191 Aerospace Mechanisms Symposium 

[ NASACP-24701 p 18 N87-29858 

The Jovian Atmospheres 

SPACE COMMUNICATION 

SPACEERECTABLESTRUCTURES 

(suppleme* 4) 

SPACE EXPLORATION 

[NASA-CP-2441] p '26 N87-17598 

SPACE PLASMAS 

Double Layers in Astrophysics 

[ NASACP-24691 p 25 N87-23313 

System study of the carbon dioxide observational 

platform system (COOPS): Prokt overview 

[ NASA-TP-26961 p9 N87-18588 

Space station systems: A bibliraphy with indexes 

(supplement 4) 

[ NASA-SP-7056(04)] p 10 N87-28073 

SPACE PROGRAMS 

Atmospheric Turbulence Relative to Aviation. Mile, 

and Spaa, Programs 

SPACE PLATFORMS 

[ NASA-CP-24681 p 21 N87-22341 

SPACE SHUTTLE BOOSTERS 

Analysis of quasi-hybnd soli rocket booster concepts 

for advanced earth-toorbit vehicles 

[NASA-TP-27511 p 11 N87-25425 

Conventionally cast and forged copper alloy for 

[ NASA-TP-26941 p 12 N87-16902 

Space shuttle main engine high pressure fuel pump aft 

Platform seal cavity flow anaiysls 

[NASA-TP-2685] p 14 N87-17000 

Structural lntegrily and Gurabili of Reusable Space 

Propulsion Systems 

[NASA-CP-2471] p 11 N87-22766 

Threestep labyrinth seal for high-performance 

turbomachines 

[NASA-TP-t848] p 15 N87-23921 

Straight cylindrical seal for high-performance 

turbomachines 

[NASA-TP-1850] p 15 N87-23936 

SPACE SrmTTLL WIN ENGINE 

high-heat-flux thrust Chambers 

Threestep cylindrical seal for high-performance 

turbomachines 

[NASA-TP-1 8491 p 15 N87-24639 

Probabilistic risk analysis of flying the space shuttle with 

and without fuel turbine discharge temperature redline 

protection 

[ NASA-TP-2759 J p 23 N87-27474 

Finkelement reentry heat-transfer analysis of space 

shuttle Orbiter 

[ NASA-TP-2657) p 16 N87-29795 

SPACE SHUTTLE ORBITERS 

SPACE SHUTTLE PAYLOADS 

Solar array flight dynamic experiment 

[ NASA-TP-25981 p9 N87-12581 

The 1986 Get Away Special Experimenter's 

Symposium 

[ NASA-CP-24381 p9 N67-20302 

Solar array flight axperimantldynamic augmentation 

experiment 

[ NASA-TP-26901 p 10 N87-20380 

Development testing of large volume water sprays for 

warm fog dispersal 

[ NA.SA-TP-2607] p10 N87-12585 

Spacelab 3 Mission Science Review 

[ NASA-CP-24291 p 15 N87-22103 

Space station structures and dynamics test program 

[ NASA-TP-27101 p 18 N87-20568 

NASA1 DOD ControllStructures Interaction Technology, 

1986 

[NASA-CP-2447-PT-l] p10 N87-16014 

The 20th Aerospace Mechanics Symposium 

[ NASA-CP-2423-REV] p 17 N87-16321 

Space station structures and dynamics test program 

[NASA-TP-27101 p18 N87-20568 

Space station systems: A bibliography with indexes 

(supplement 4) 

[ NASA-SP-7056(04)] p 10 N87-28073 

SPACE SHUTTLES 

SPACE STATION STRUCTURES 

SPACE STATIONS 

SPACEBORNE EXPERIMENTS 

Spacelab 3 Mission Science Review 

[NASA-CP-2429] p 15 N87-22103 

NASAlDOD ControllStfuctures Interaction Technology, 

1 g66 

[ NASA-CP-2447-PT-11 p10 N87-16014 

Structural Dynamics and Control Interaction of Flexible 

Structures 

[ NASA-CP-2467-PT-11 p 10 N87-22702 

NASAlDOD ControllStfuctures Interaction Technology. 

1 986 

[NASACP-2447-PT-21 p 10 N87-24495 

NASAlDOD ControllSbuctures Interaction Technology, 

Upper and Middle Atmospheric Density Modeling 

Requirements for Spacecraft Design and Operations 

[ NASACP-24601 p20 N87-20665 

SPACECRAFT CONTROL 

SPACECRAFT DESIGN 

1986 

[NASACP-2447-PT-l I p 10 N87-16014 

SPACECRAFT INSTRUMENTS 

The 20th Aerospace Mechanii Symposium 

p 17 N87-16321 

Earth resources: A continuing bibliography with indexes 

p 18 N87-27315 

Development testing of large volume water sprays for 

warm fog dispersal 

[NASA-TP-2607] p 10 N87-12585 

Space Photovoltaic Research and Technology 1988. 

High Efticiency, Space Environment, and Array 

Technology 

[NASA-CP-2475] p 19 N87-26413 

Structural Integrity and Gurabili of Reusable Space 

Propulsion Systems 

[NASA-CP-2471] p 11 N87-22766 

Probebilistic risk analysis of Rylng the space shuttle with 

and without fuel turbine discharge temperature redline 

[NASA-TP-2759] p 23 N87-27474 

Effects of thermal Cycling on graphiefiber-reinforced 

6081 aluminum 

[NASA-TP-26121 pll N87-10184 

[ NASACP-2423-REV] 

(isaue 54) 

[ NASA-SP-7041(54)] 

SPACECRAFT LAUNCHINQ 

SPACECRAFT POWER SUPPLIES 

SPACECRAFT PROPULSION 

SPACECRAFT REUABILITV 

protection 

SPACECRAFTSTRUCTURES 

SPACESpacelab 3 Mission Science Review 

[ NASA-CP-24291 p 15 N87-22103 

Numerical simulation of channel Row transition, 

resolution requirements and structure of the hairpin 

vortex 

[ NASA-TP-26871 p3 N87-19351 

SPECTRAL METHODS 

A-14 
SUBJECT INDEX 

SPIN 

Flight invesligalion of the effects of an outboard 

wing-leadin@ge modiition on stall/spin 

characteristics of a low-wing, singleengine. T-tail lght 

airplane 

SPLAMINQ 

[ NASA-TP-26911 p6 N87-23614 

Measurements of flow rate and trajectory of aircraft 

tiregenerated water spray [NASA-TP-2718] p6 N87-24458 

An algodthm for surface smoothing with rational 

splines 

[NASA-TP-2708] p23 N87-22447 

Development testing of large volume water sprays for 

warm fog dispersal 

[NASA-TP-2607] p10 N87-12585 

Measurements of flow rate and trajectory Of aircraft 

tiregenerated water spray 

[NASA-TP-2718] p6 N87-24458 

SPUNE "CTKms 

SPRAY NOZLES 

SPRAYIM 

SPWITERINQ 

The 20th Aerospace Mechanics Symposium 

[ NASA-CP-2423-REVI p 17 N87-16321 

Lquid drop stability for protein aystal gmwth in 

microgravity 

Rotordynamic Instability Problems in High-Performance 

Turbomachinery. l9W 

[ NASA-CP-24431 p 17 N87-22199 

Appliition of turbulence modeling lo predict surface 

heat transfer in stagnation flow region of circular cylinder 

[ NASA-TP-27581 p 15 N87-27161 

Qualitative evaluation of a flush air data syslem a1 

transonic speeds and high angles of atlack 

[NASA-TP-2716] p6 N87-29497 

[NASA-CP-2466] p26 N67-24266 

A new approach to state estimation in deterministic 

digital control SyslemS 

[NASA-TP-2745] p13 N87-24585 

Exacl state reconstruction in deterministic digital control 

Systems 

[NASA-TP-2757] p 13 N87-27067 

STABILITY 

[ NASA-TP-27241 p21 N67-20727 

STAQNATION FLOW 

STAQNATION PRESSURE 

STAR FORMATION 

Star Formation m Galaxies 

STATE ESllYATION 

STATE VECTORS 

Modeling digital control systems with MA-prefillered 

measurements 

[NASA-TP-2732] p 13 N87-22870 

Exact state reconstruction in deterministic digital control 

systems 

[NASA-TP-27571 p 13 N87-27067 

Largegcale static investigation of 

circulationcontrol-wing wncepts applied to upper 

surfaceblowing aircraft 

[NASA-TP-2884] p 6 N87-15959 

Three-step labyrinth seal for highperformance 

turbomachines 

[NASA-TP-1848] p 15 N87-23921 

Static internal performance of a two-dimensional 

STATIC TESTS 

comergentdtvergent no* with thnrst vectoring 

[NASA-TP-27211 p4 N87-24432 

STATISTICAL ANALYSIS 

Statbtical aspects of solar Wes 

Star Formation in Galaxies 

[NASA-TP-2714 J p27 N87-20947 

STEW LUMINOSITV 

[NASACP-2466] p26 N87-24266 

STIMULATED EMISSION 

Electron stimulated desorption of atomic oxygen from 

silver 

[NASA-TP-ZME] p 12 N87-18629 

and wimwt fuel turbine discharge temperature redline 

potection 

[NASA-TP-27591 p 23 N87-27474 

Airbwne li measurements of El Chichon stratospheric 

aero!&, May 1983 

[NASA-RP-1172] pl9 N87-11358 

oescription of data on the Nimbus 7 LlMS map archive 

tepe:oroneandnitricad 

[NASA-TP-2625] pl9 N87-13022 

SAGE aemsol measuremnts. Volume 3: January 1. 

1981 to November 18,1981 

Airbome lidar measurements of El Chichon stratospheric 

STOCHASTIC PROCESSES 

Robabilislicmkana~offfyinethespaoeshotllewith 

STRATOSPHERE 

[NASA-RP-1173] p 19 N87-17417 

aerosols. Jarmary 1884 

[NASA-RP-1175] ~20 N87-20863 

STRESS MEASUREMENT 

Gear tooth stress measurements on the UH-GOA 

helier transmission 

[NASA-TP-2698] p 17 N87-22235 

STRUCTURAL ANALYSIS 

[NASA-CP-2481] p 18 N67-27231 

In-flight total forces, mts and static aeroelastic 

characteristics of an obliquewing research airplane 

[NASA-TP-2224] p8 N67-10103 

Recent Experiences in Multidisciplinary Analysis and 

Optimization, part 1 

[ NASA-CP-2327-PT-l ] p5 N87-11717 

Study of leaside flows over conicalty cambered ddla 

wings at supersonic speeds, part 1 

[ NASA-TP-266O-PT-11 p4 N87-23597 

Status and Mure of lunar gexckw 

[NASA-SP-484] p26 N87-19322 

Structural lnlegrity and Burability of Reusable Space 

Propulsion Systems 

[NASA-CP-2471] p 11 N87-22766 

Fineenth NASTRAN Users' Colloquium 

STRUCTURAL MSIQN 

STRUCTURAL PROPERTIES (QEOLOQY) 

STRUCTURAL RELIABILITY 

STRUCTURAL VIBRATION 

Fineenth NASTRAN Users' Colloquium 

[NASA-CP-2481] p 18 N87-27231 

Subsonic longitudinal and lateraldirectional 

characteristics of s forward-swept-wing fighter 

configuration at angles of atlack up lo 47 deg 

[ NASA-TP-27271 p4 N87-26874 

Efficient solutions lo the Euler equations for supersonic 

flow with embedded subsonic regions 

[ NASA-TP-25231 p2 N67-15183 

Subsonic manewer capability of a supersonic CN~ 

fighter wing M)(IcBpt 

[ NASA-TP-26421 p2 N67-15184 

An experimental investigation of an advanced turboprop 

installation on a swepl wing a1 subsooic and transonic 

speeds 

[ NASA-TP-27291 p4 N87-28883 

Pressure measurements on a thick cambered and 

twisted 58 

[ NASA-TP-27131 p5 N87-27643 

Energetic Phenomena on the Sun: The Solar Maximum 

Mission Flare Workshop. proceedings 

[ NASA-CP-24391 p 26 N87-19328 

coronal and Rominence Plasmas 

[ NASA-CP-24421 p26 N87--71 Fm year canon of solar eclipses: 1986 - 2035 

[NASA-RP-1178-REV] p26 N87-25906 

Energetic Phenomena on the Sun: The Solar Maximum 

MiWn Flare Workshop. Proceedings 

[NASA-CP-2439] p 26 N87-19328 

Supercomputing in Aerospace 

[NASA-CP-2454] p4 N87-25998 

Supersonic, nonlinear, attached-flow wing design for 

hgh li with expedmenlal validation 

[NASA-TP-2336] p 1 N87-10042 

Material charactefizalion of superplastically formed 

iitanii (TiiI-2Sn-4Zr-ZMo) sheet 

[NASA-TP-2674] p12 N87-20407 

SUPERSONIC AIRCRAFT 

MuHiscak twtwlence effects in supersonic jets 

exhausting into still air 

[ NASA-TP-27071 p 15 N87-24672 

SUPERSONIC AIRFOILS 

Supersonic, nonlinear, atlached-flow wing design for 

high 1% with experimental valiition 

[NASA-TP-Z336] p 1 N87-10042 

Subsonic manewer capability of a supersonic mise 

fighter wing wncept [NASA-TP-2842] p2 N87-15184 

~uwi wtrol power from thrust Vectoring for a 

supenonic fighter aircraft model at Mach 0.20 to 2.47 

[ NASA-TP-27121 p4 N87-24433 

Supersonic. nonlinesr, atlachedfhm wing design for 

hi@ lii with experimental validation 

[ NASA-TP-23361 p t N87-10042 

Efficient solutions lo lhe Euler equations for supersonic 

Row with embedded subsonic regions 

[NASA-TP-2523] p 2 N87-15183 

Study of bside f!ws over conically cambered delta 

wings at supmonk speeds, part 1 

[ NASA-TP-2860-PT-11 p4 N87-23597 

SUBSONIC AIRCRAFT 

SUBSONIC FLOW 

SUBSONIC SPEED 

delta wing a1 hgh subsonic speeds 

SUN 

SUNSPOTS 

SUPERCOMPUTERS 

SUPERCRmCAL FLOW 

SUPERPIASTICITY 

SUPERSONIC CRUISE AIRCRAFT RESEARCH 

SUPERSONIC FLOW 

TAIL ASSEMBLIES 

Study of lee-side flows over conically cambered Delta 

[NASA-TP-Z%O-PT-Z] p4 N87-25301 

Wind-tunnel investigation a1 supersonic speeds of a 

remote-controlled canard missile with a free-rolling-tail 

brake torque syslem 

[NASA-TP-2401] p3 N87-17688 

lnvestigatbn of leadinggdge flap performance on delta 

and doubledelta wings at supemnic speeds 

[NASA-TP-2656] p3 N87-20233 

Exmimental cavitv wessure distributions at su~ersonic 

wingsatwpeoooic speeds, part2 

SUPERSONIC SPEED 

.. s&s 

[ NASA-TP-2683 I p3 N87-22626 

Draa measurements of blunt stores tanaentiillv -. mounted 

on a iat plate at supersonic speeds 

[NASA-TP-2742] p5 N87-27626 

SUPPLEMENTS 

NASA Thesaurus supplement (supplement 3) 

[NASA-SP-7053(SUPP-3)1 p 25 N87-27557 

Joint Unhrsiiy Program for Air Transportation 

Research, 1984 

[ NASA-CP-2452) p 1 N87-22804 

Theory for computing the field scattered from a smooth 

inflected surface 

[NASA-TP-2632] p24 N87-13264 

Applition of turbulence modeling lo predii surface 

heal transfer in stagnation flow region of circular cylinder 

[ NASA-TP-27581 p 15 N87-27161 

Effects of ads and surface shadowing on bidirectional reflectance measurements of deserts 

[ NASA-TP-27581 p 19 N87-28162 

An algorithm for surface smoothing with rational 

splines 

[ NASA-TP-2708 I p 23 N87-22447 

Forward-swept wing configuration designed for high 

maneuverability by use of a transonic computational 

method 

[ NASA-TP-26281 p 2 N87-11702 

Subsonic longludinal and lateraldirectional 

characteristics of a forward-swept-Wing fighter 

configuration a1 angles of attack up to 47 deg 

[ NASA-TP-2727 I p4 N87-26874 

Aqpllcability of linearized-theny attached-flow methods 

to design and analysis of flap systems at low speeds for 

thin swept wings with sharp leading edges 

[ NASA-TP-26531 p 2 N87-15174 

An experimental investigation of an advanced turboprop 

installation on a swepl wing at subsonic and transonic 

SURFACE NAVIQATION 

SURFACE PROPERTIES 

SURFACE ROUQHNESB 

SWEPT FORWARD WINQS 

SWEPT WINQS 

G!-TP-2729] 

SYMMETRY 

p4 N87-28883 

Exploiting symmehies in the modeling and analysis of 

tires 

[NASA-TP-2649] p 6 N87-17890 

A synchronws data analyzer for the Minimum Daky 

Data Format (MDDF) and Launch Trajeclwy Acquisition 

System (LTAS) 

[ NASA-TP-27431 p 13 N87-24590 

SYNCHRONISM 

SYNOPTIC METEOROLOQY 

The Jovian Atmospheres 

[NASA-CP-2441 I p 26 N87-17598 

Fie year global dataset: NMC operational analyses 

[NASA-RP-11941 p21 N87-28896 

Unique bil-error-rate measurement syslem for satellite 

communication syalems 

[NASA-TP-BBB] p 13 N87-20448 

Space station slructures and dynamics test program 

[NASA-TP-27101 p 18 N87-20588 

NASAlDOD Control6tructures Interaction Technology. 

1986 

[ NASA-CP-2447-PT-l ] p10 N87-18014 

Modeling digital control systems with MA-prenllered 

measurements 

[ NASA-TP-27321 p 13 N87-22870 

(1 978 10 1982) 

SYSTEMS ANALYSIS 

SYSTEMS ENQINEERINQ 

T 

TAIL ASSEMBLIES 

Effects of tail span and empennage mangemen1 on drag of a lypical aingle-engine fighter aft end 

[ NASA-TP-2352 I pl N87-10838 

Interference effects of thrust revenring on homontal tail 

effectiveness of twin-engine fighter aircraft at Mach 

numbers from 0.15 to 0.90 

[NASA-TP-2350] p8 N87-10870 

A-15 
TAIL SURFACES SUBJECT INDEX 

Fliht investigation of the effect of tail configuration on 

stall. spin, and recovery characteristics of a low-wing 

general aviation research airplane 

[NASA-TP-26441 p6 N87-16815 

Wind-tunnel investigation at supersonic speeds of a 

remote-controlled canard missile with a free-rolling-tail 

brake toque system 

[NASA-TP-2401] p3 N87-17668 

Effects of empennage surface location on aerodynamic 

characteristics of a twin-engine afterbody model with 

nomisymmetric nozzles 

[ NASA-TP-23921 p 6 N87-17693 

Effects of afterbody boattail design and empennage 

arrangement on aeropropulsive characteristics of a 

twin-engine fighter model at transonic speeds 

[ NASA-TP-27041 p3 N87-21873 

Effects of empennage surface location on aerodynamic 

characteristics of a twin-engine afterbody model with 

nonaxiaymmetric nozzles 

[NASA-TP-2392] p6 N87-17693 

Drag measurements of blunt stores tangentially mounted 

on a flat plate at supersonic speeds 

[ NASA-TP-27421 p5 N87-27626 

Aeronautical facilis assessment 

TAIL SURFACES 

TANGENTS 

TECHNOLOGY ASSESSMENT 

[NASA-RP-1146] p8 N87-10876 

TEMPERATURE PROFILES 

Velocity profiles in laminar difhrsion flames 

[NASA-TP-25961 p 15 N87-18035 

TEMPERATURE SENSORS 

Probabilistic risk analysis of flying the space shuttle with 

and without fuel tufbine discharge temperature redline 

protection 

[ NASA-TP-27591 p 23 N87-27474 

TENSILE CREEP 

Material characterization of superplastically formed 

titanium (li-6AI-2Sk4Zr-2Mo) sheet 

[ NASA-TP-26741 p 12 N87-20407 

Sp&msmw comparison of effects of electron 

radiation on mechanical properties of two polyimides 

[NASA-TP-2663] p 11 N87-18811 

Applications and requirements for real-time simulators 

in ground-test facilities 

[NASA-TP-2672] p 22 N87-23202 

Langley Aircraft Landing Dynamics Facility 

[NASA-RP-1189] p9 N87-29544 

Desaiption and calibration of the Langley Hypersonic 

CF4 tunnel: A faulty for simulating low gamma flow as 

occurs for a real gas 

[ NASA-TP-23841 p 16 N87-29778 

TETHERED SATELLITES 

TENSILE PROPERTIES 

TEST FACILITIES 

Tether Dynamics Simulation 

[NASA-CP-2458] p 16 N87-18821 

TETHERLINES 

Tether Dynamics Simulation 

[NASA-CP-2458] p 16 N87-18821 

Finite-element reentry heat-transfer analysls of space 

Shmk orbiter 

[NASA-TP-2657] p 16 N87-29795 

Effects of thermal cycling on graphbfiber-reinforced 

[NASA-TP-2612] p 11 N87-10184 

THERMAL ANALYSIS 

THERMAL CYCLING TESTS 

6081 aluminum 

THERMAL PROTECTION 

Aerothennal teats of sphericel dome protuberances on 

a flat plate at a Mach number of 6.5 

[NASA-TP-26311 p14 N87-13664 

Amthermal evaluation of a spWly blunted body 

with a trapezoidal cross section in the Langley &foot 

hightemperature tunnel 

[NASA-TP-2641] p 15 N87-18782 

Relimim eatimates of radwnde thennistor wors 

[NASA-TP-2637] P20 N87-12086 

THERMISTORS 

THERMODYNAMIC PAOpERnES 

Simplified curve fits for the thermodynamic propeh 

of equilibrium air 

[NASA-RP-1181] P 15 N87-26309 

THERMODYNAMICS 

TlWJOVianAtmospher~ 

[ NASA-CP-24411 P 26 N87-17598 

NASAChinese Aeronautical Establishment (CAE) 

Symposium 

[NASA-CP-24331 P7 N87-20267 

Upper and Middle Atmospheric Density Modeling 

Requirements for Spacecraft Dmgn and Operations 

[ NASA-CP-24601 P20 N87-2Q665 

THERMOSPHERE 

THESAURI 

NASA Theaaunm supplement (supplement 3) 

[ NASA-SP-7053(SUPP-3)] P 25 N87-27557 

THICKNESS 

Pressure measurements on a thick cambered and 

twisted 58 deg delta wing at hgh subsonic speeds 

[ NASA-TP-27131 p 5 N87-27643 

THIN FILMS 

Traveling-wave-tube efficiency improvement by a 

lowcosl technique for deposition of carbon on multistage 

depressed collector 

[ NASA-TP-27191 p 14 N87-21239 

Applicability of linearized-theory attached-flow methods 

to design and analysis of flap systems at low speeds for 

thin swept wings with sharp leading edges 

THIN WINGS 

[NASA-TP-2653] p2 N87-15174 

THREE DIMENSIONAL FLOW 

Evaluation of dftuse-illumination holographic 

cinematography in a flutter cascade 

[ NASA-TP-25931 p 16 N87-13731 

Large-scale static investigation of 

circulationcontrol-wing concepts applied to upper 

surface-blowing aircraft 

[NASA-TP-rn] p 6 N87-15959 

Interference effects of thrust reversing on horizontal tail 

effectiveness of twin-engine fighter aircraft at Mach 

numbers from 0.15 to 0.90 

THRUST CONTROL 

THRUSTREVERSAL 

[NASA-TP-2350] p8 N87-10870 

Effect of port corner geometry on the internal 

pertormance of a rotating-vane-type thrust reverser 

[ NASA-TP-26241 p2 N87-12541 

Static internal performance of singleexpansion-ramp 

Males with thrust-vectoring cepabili up to 60 deg 

[NASA-TP-23641 p2 N87-10839 

Static internal performance of a two-dimensional 

convergentdwergent nozzle with thrust vectoring 

[NASA-TP-2721] p4 N87-24432 

Multiaxis control power from thrust vectciing for a 

supersonic fighter aircraft model at Mach 0.20 to 2.47 

[NASA-TP-2712] p4 N87-24433 

NASAIMSFC FY-85 Atmospheric Processes Research 

Review 

[NASA-CP-2402] P20 N87-13043 

Aerothermal tests of spherical dome protuberances on 

THRUST VECTOR CONTROL 

THUNDERSTORMS 

TILES 

a flat plate at a Mach number of 6.5 

[NASA-TP-2631] pi4 ~a7-i~~ 

TIME LAG 

Piloted simulator study of allowable time delays in 

large-airplane response 

[NASA-TP-2652 J p8 N87-16849 

Ground-bawd timeguidance algorithm for control of 

airplanes in a time-metered air traffic control environment: 

A piloted simulation study 

TIMING DEVICES 

[NASA-TP-26161 p7 N87-10864 

np VANES 

Transonic flow analysis for rotors. Pm 2: 

Threedimensional. unsteady. fullpotential calculation 

[ NASA-TP-2375-PT-21 p2 N87-10841 

TIRES 

Exploibng symmetries in the modeling and analysis of 

tires 

[NASA-TP-26491 p 6 N87-17690 

cosmic ray heavy ion LET mapping for aluminum, silicon, 

[NASA-RP-11801 p27 N87-25984 

Effect of LID (Registered) processing on the 

microstructure and mechanical properties of liiAI-4V and 

TiI-2Sn-4Zr-2Mo titanium foilgauge materials 

[NASA-TP-2677] p12 N87-18644 

Material characterization of superplastically formed 

titanium (li-6AI-2Sn-4Zr-ZMo) sheet 

[NASA-TP-2674] p 12 N87-20407 

Shot peening for TiiAI4V alby compr- blades 

[NASA-TP-2711] p 18 N87-20566 

Wind-tunnel investigation at supersonic speeds of a 

remotecontrolled canard missile with a free-rolling-tail 

brake toque system 

[NASA-TP-2401] p3 N87-17668 

TISSUES (BIOLOGY) 

andtibsuetargets 

TITANIUM ALLOYS 

TORWE 

TRACKING (PosmoN) 

sdar array flight dynamic experiment 

[NASA-TP-2596] p9 N87-12581 

Effect of a trade between boattail angle and wedge size 

on the perfomuvl~e of a -metric wedge nozzle 

[NASA-TP-2717] p4 N87-23593 

TRADEOFFS 

TRAJECTORY ANALYSIS 

A synchronous data analyzer for the Minimum Delay 

Data Format (MDDF) and Launch Trajectwy Acquisition 

System (LTAS) 

TRANSDUCERS 

instrumentation 

[NASA-TP-27431 p 13 N87-24590 

Analog signal condiboning for flight-test 

[NASA-RP-1159] p7 N87-29533 

Bit-error-rate testing of high-power 30-GHz traveling 

wave tubes for ground-terminal applications 

[NASA-TP-26351 p 13 N87-17971 

Testing of UH-GOA helicopter transmission in NASA 

Lewis 2240-kW (3000-hp) facility 

[NASA-TP-2626] p 16 N87-10391 

Vibration characteristics of OH-SA helicopter main rotor 

transmission 

Gear tooth stress measurements on the UH-GOA 

TRANSMISSION EFFICIENCY 

TRANSMISSIONS (MACHINE ELEMENTS) 

[NASA-TP-2705] p 17 N87-20555 

helicopter transmission 

[NASA-TP-2698] 

TRANSONIC FLOW 

p 17 N87-22235 

Transonic flow analysis for rotors. Part 2 Threedimensional. unsteady, full-potential calculation 

[NASA-TP-2375-PT-2] p2 N87-10841 

Effects of winglet on transonic flutter characteristics of 

a cantilevered twin-engine-tranwrt wing model 

[NASA-TP-26271 p 17 N87-13789 

Calculation of viscous effects on transonic flow for 

Oscillating airfoils and comparisons with experiment 

[NASA-TP-27311 p5 N87-27622 

Effects of tail span and empennage arrangement on 

drag of a typical single-engine fighter aft end 

[NASA-TP-2352] p 1 N87-10838 

Forward-swept wing configuration designed for hgh 

maneuverability by use of a transonic computational 

method 

[NASA-TP-2628] p 2 N87-11702 

An experimental investigation of an advanced turboprop 

installation on a swept wing at subsonic and transonic 

speeds 

[ NASA-TP-27291 p4 N87-26883 

Qualitative evaluation of a flush air data system at 

transonic speeds and high angles of attack 

[NASA-TP-2716 J p6 N87-29497 

Evolution, calibration. and operational characteristics of 

the Mimensional test section of the Langley 0.3-meter 

transonic cryogenic tunnel 

[NASA-TP-2749 J p9 N87-28570 

TRANSPORT AIRCRAFT 

Piloted simulator study of allowable time delays in 

largeairplane response 

Summary of studies to reduce wing-mounted propfan 

installation drag on an M = 0.8 transport 

[NASA-TP-2678 J p6 N87-20990 

Effect of Reynolds number variation on aerodynamics 

of a hydrogen-fueled transport concept at Mach 8 

[NASA-TP-27281 p4 N87-26031 

Jet transpolt fliht operations using wckpil display of 

traffic information during instrument meteorological 

condiins: Simulation evaluation 

[ NASA-TP-25671 p5 N87-29469 

Hydrogen eapping and the interaction of hydrogen with 

p 12 N87-25463 

BI-enor-rate testing of hgh-power 30-GHz traveling 

wave tubes for ground-terminal applications 

[NASA-TP-2635] p 13 N87-17971 

Performance of textured carbon on coppec electrode 

multistage depressed collectors with medium-power 

traveling wave tubes 

Calculation of secondary electron trajectories in 

multistage depressed collectors for microwave ampli 

[NASA-TP-Z664] p 14 N87-17991 

Design. fabrication and performance of small, graphite 

electrode, multistage depressed collectors with 200-W. 

CW. 8- to 18-GHz traveling-wave tubes 

[ NASA-TP-26931 p 14 N87-20474 

Traveling-wave-tube efficiency improvement by a 

lowco8t technique for depoWn of carbon on multistage 

[NASA-TP-27191 p 14 N87-21239 

Revised NASA axially symmebic ring model for 

coupredcavity traveling-wave tubes 

[ NASA-TP-26751 p 14 N87-22923 

Analykal and experimental perfcmance of a dual-mode 

traveling wave tube and multistage depressed collector 

[ NASA-TP-27521 p 14 N87-25532 

TRANSONIC SPEED 

TRANSONIC WIND TUNNELS 

[ NASA-TP-26521 p8 N87-18849 

TRAPPINQ 

metal8 

[NASA-TP-2744 1 

TRAVELINQ WAVE TUBES 

[NASA-TP-26651 p14 N87-17990 

depressed collector 

A-16 
SU8JECTINDEX 

TRIBOLOGY 

The 20th Aemspace Mechanics Symposium 

[NASA-CP-2423-REVl p 17 N87-16321 

On requirements for a satellite mission to measure 

tropical rainfall 

[NASA-RP-1183] p20 N87-20701 

On requirements for a satellite mission to measure 

tropical rainfall 

[NASA-RP-1183] p20 N87-20701 

TROPOSPHERE 

Future directions for H sub x 0 sub y detection 

[ NASA-CP-24481 p 19 N87-15528 

Space Opportunities for Trmsphenc Chemistry 

Research 

[NASA-CP-2450] p20 N87-18248 

TRUSSES 

NASAIWD ControllStwclutures Interaction Technology. 

1986 

[NASA-CP-2447-PT-l I p10 N87-16014 

Modeling of joints for the dynamic analysis of truss 

structures 

[NASA-TP-2661] pl8 N87-20567 

Lewis in- design code (LINDES): Users manual 

[NASA-TP-2676] p3 N87-20238 

Turbine Engine Hot Section Technology. 1984 

[ NASA-CP-23391 p17 N87-11180 

Advanced detection. isolation and ammodation of 

sensor failures: Real-time evaluation 

[ NASA-TP-27401 p8 N87-25331 

Space shutne main engine tugh pressure fuel pump afl 

platform seal cavity flow analysis 

[ NASA-TP-ZW51 p14 N87-17000 

Straight cylindrical seal for high-performance 

turbomachines 

[ NASA-TP-18501 p 15 N87-23936 

Threestep cylindrical seal for high-performance 

turbomachines 

[ NASA-TP-18491 p 15 N87-24639 

Rotordynamic Instability Problems in High-Perlormance 

TROPICAL METEOROLOGY 

TROPICAL STORMS 

TURBINE BLADES 

TURBINE ENGINES 

TURBINE PUMPS 

TURBOCOMPRESSORS 

Turbomachinery, 1986 

[ NASA-CP-24431 p 17 N87-22199 

TURBOFAN ENGINES 

Large-scale static investigation of 

circulationcontrol-wing concepts applied to upper 

surfaceblowing aircraft 

Evaluation of installed performance of a 

wing-tipmounted pusher turbopcop on a semispan wing 

[ NASA-TP-27391 p6 N87-28041 

Rotordynamic Instability Problems in High-Performance 

Turbomachinery, 1986 

[ NASA-CP-24431 p 17 N87-22199 

Three-step labyrinth seal for high-performance 

turbomachinea 

[ NASA-TP-18481 p 15 N87-23921 

Straight cylindrical seal for high-performance 

turbomachinea 

[ NASA-TP-18501 p 15 N87-23938 

Evaluation of installed performance of a 

wing-tipmounted pusher turbopcop on a semispan wing 

[ NASA-TP-27391 p6 N87-28041 

An experimental investigation of an advanced twboprop 

installation on a swept wing at subsonic and transonic 

E-TP-27291 p4 N87-26603 

Low-speed aerodynamic characteristics of a twin-engine 

general aviation configuration with aft-fuselagemounted 

posher propellers 

[NASA-TP-Z684] p6 N87-15959 

TURBOMACHINERY 

TURBOPROP ENGINES 

[NASA-TP-2763] p5 N87-29462 

TURBULENCE 

MuHjscale tubulence effects in supersonic jets 

exhausting into still air 

[ NASA-TP-27071 p 15 N87-24672 

Awlcation of turbulence modeling to predict surface 

heat transfer in stagnation flow region of circular cylinder 

[NASA-TP-2758] p 15 N87-27161 

TURBULENCE EFFECTS 

Jet model for slot film cooling with effect of free-stream 

and Coolant tubulence 

[ NASA-TP-26551 p15 N87-18034 

Experimental evaluation of honeycomblscreen 

configurations and short contraction secthn for NASA 

Lewis Research Center's altitude wind tunnel 

[ NASA-TP-26921 p9 N87-23662 

Aerothermal testa of spherical dome protuberancas on a flat plate at a Mach number of 6.5 

[NASA-TP-Z631] p14 N87-13864 

TURBULENT BOUNDARY LAYER 

TURBULENT FLOW 

Expenmental evaluation of honeycomblscreen 

configurations and short contraction section for NASA 

Lewis Research Center's altitude wind tunnel 

[NASA-TP-26921 p9 N87-23662 

Pressure measurements on a thick cambered and 

twisted 58 deg delta wing at high subsonic speeds 

[ NASA-TP-27131 p5 N87-27643 

ExDerimental valiition of a two-dimensional shear-flow 

TWISTED WINGS 

TWO DIMENSIONAL FLOW 

model for determining acoustic impedance 

[ NASA-TP-26791 p23 N87-20798 

Static internal performance of a two-dimensional 

convergentdivergent nozzle with thrust vectoring 

[NASA-TP-27211 D4 N87-24432 

Evolution. calibration. and operational charactehstics of 

the two-dimensional test section of the Langley 0.3-meter 

transonic cryogenic tunnel 

[ NASA-TP-27491 p9 N87-28570 

U 

UMA HELICOPTER 

Gear tooth stress measurements on the UH-GOA 

helicopter transmission 

[ NASA-TP-26981 p 17 N87-22235 

Calibration of the spin-scan ozone imager aboard the dynamics Explorer 1 satellite 

[ NASA-TP-2723 I p21 N87-26491 

UNIVERSITIES 

The 1986 Get Away Special Expetimenter's 

Symposium 

[ NASA-CP-24381 p9 N87-20302 

ULTRAVIOLET SPECTRouE+ERS 

UNMANNED SPACECRAFT 

Status and Mure of lunar geoscience 

[NASA-SP-484] p 26 N87-19322 

Steady and unsteady aerodynamic forces from the 

SOUSSA surfacepanel method for a fighter wing with tip 

missile and comparison with experiment andPANAlR 

[NASA-TP-27361 p4 N87-26032 

Largesale stak investigation of 

circulation-control-wing concepts applied to upper 

surface-blowing aircraft 

LNASA-TP-26841 p6 N87-15959 

URANUS ATMOSPHERE 

UNSTEADY FLOW 

UPPER SURFACE BLOWING 

The Jovian A-es 

[NASA-CP-2441 I p26 N87-17598 

Pulse Code Modulation (EM) encoder handbook for 

Lewis inverse dmgn code (LINDES): Users manual 

[NASA-TP-26761 p3 N87-20238 

USER MANUALS (COMPUTER PROORAMS) 

Aydin Vector MMP-600 series system 

[NASA-RP-1171 I p 13 N87-11916 

V 

V/STOL AIRCRAFT 

Proceedings of the 1985 NASA Ames Research Center's 

Ground-Effects Workshop 

[NASA-CP-2462 I p 4 N87-24410 

Shot peening for TiiAI4V alloy compressorblades 

[ NASA-TP-2711 I p 18 N87-20586 

Effect of port comer geometry on the internal 

performance of a rotating-vanetype thrust reverser 

[ NASA-TP-2624 I p2 N87-12541 

Expenmental evsluatbn of two turning vane designs for 

fan drive corner of 0.1-scale model of NASA Lewis 

Research Center's proposed aithde wind tunnel 

[ NASA-TP-26481 p 8 N87-18576 

Effects of variables upon pyrotechnically induced shock 

[NASA-TP-2603] p 17 N87-12921 

Flight-determined aerodynamic derivatives of the AD1 

obliquewing reaearch airplane 

[ NASA-TP-22221 p8 N87-10871 

Development and evaluation of an airplane electronic 

display formst aligned with the inertial velodyvector 

[ NASA-TP-W] p 7 N87-13438 

VANADIUM 

VANES 

VARIABIUTY 

response 

VARIABLE SWEEP WINGS 

VELOCITY 

VELOCITY MEASUREMENT 

velocity pofiles in laminar diffusion flames 

[ NASA-TP-259Bl p 15 N87-18035 

Procwdings of the 1985 NASA Ames Research Center's 

Ground-Effects Workshop 

[NASA-CP-24621 p 4 N87-24410 

VERTICAL UNDlWa 

WEATHER FORECASTING 

VERY LARGE SCALE INTEGRATION 

A technique for evaluating the application of the pin-level 

stuck-at faun model to VLSl circuits 

[NASA-TP-2738] p 17 N87-28025 

VHSIC (CIRCUITS) 

Computer Sciences and Data Systems, volume 2 

[ NASA-CP-2459-VOL-2 I p 22 N87-19932 

NASA/ WD ControllStructures Interaction Technology, 

1988 

[ NASA-CP-2447-PT-1 I p10 N87-16014 

NASAlDOD ControllStructures Interaction Technology, 

1986 

[ NASA-CP-2447-PT-21 p 10 N87-24495 

Testing of UH-60A helicopter transmission in NASA 

Lewis 2240-kW (3000-hp) faulty 

[ NASA-TP-26261 p 16 N87-10391 

Vibration characteristics of OH-58A helicopter main rotor 

transmission 

[ NASA-TP-27051 p 17 N87-20555 

Jet transport flight operations using cockpit display of 

traffic information during instrument meteorological 

conditions: Simulation evaluation 

[ NASA-TP-25671 p5 N87-29469 

Calculation of vis~xls effects on transonic flow for 

oscillating airfoils and comparisons with experiment 

[NASA-TP-27311 p5 N87-27622 

VIBRATION DAMPING 

VIBRATION MEASUREMENT 

VIDEO COMMUNICATION 

VISCOUS FLOW 

VISUAL OBSERVATION 

Atlas of Comet Halley 1910 II 

[NASA-SP-4881 p 26 N87-30235 

VOLCANOES 

Airborne lidar measurements of El Chichon stratospheric 

aerosols. May 1983 

pl9 N87-11358 [NASA-RP-1172] 

Airborne laar measurements of El Chichon stratospheric 

aerosols. January 1984 

[NASA-RP-l175] p20 N87-20683 

ApP',Wl"y of linearized-theory attached-flow methods 

to deslgn and analysis of flap aystems at low speeds for 

thin swept wings with sharp leading edges 

p2 N87-15174 [NASA-TP-2653] 

Wind-tunnel free-flight investigation of a 0.15-scale 

model of the F-1066 airplane with vortex flaps 

[ NASA-TP-27001 p 3 N87-21855 

Piloted-simulation study of effects of vortex Raps on 

low-speed handling qualities of a Delta-wing airplane 

[NASA-TP-27471 p8 N87-26922 

Correlation of helicopter impulsive noise from 

bladevortex interaction with rotor mean inflow 

[ NASA-TP-26501 p23 N87-18399 

Helicopter bladevortex interaction locations: 

Scalemodel acoustics and free-wake analysisresults 

[ NASA-TP-26581 p 3 N87-18537 

Study of lee-side flows over conically cambered delta 

wings at supersonic speeds. parl 1 

[NASA-TP-2660-PT-l] p4 N87-23597 

VORTEX FLAPS 

VORTICES 

WAKES 

Heliter Madevortex interaction locations: 

Scale-model acoustics and free-wake analysis results 

[NASA-TP-2658] p3 N87-18537 

Jet model for slot film cooling with effect of free-stream 

WALL JETS 

and coolant turtxrlence 

[ NASA-TP-26551 P 15 N87-18034 

WALL TEMPERATURE 

Experimental evaluation of heat transfer on a 103O:l 

p 11 N87-25424 

Development testing of large volume water sprays for 

Future directions for H sub x 0 sub y detection 

area ratio rc&et nozzle 

[ NASA-TP-27261 

WATER 

warm fog dispersal 

p 10 N87-12585 [NASA-TP-2807] 

[NASA-CP-2448] p 19 N87-15528 

Propagation of sound waves in tubes of noncirwlar moas 

WAVE PROPAQATlON 

section 

[NASA-TP-2601] 

WAVE SCAlTERINQ 

inflected swface 

[ NASA-TP-26321 

Atrosphenc ' Twbulence Relalive to Aviation. Missile. 

and Space Programs 

[NASA-CP-24681 p 21 N87-22341 

p2 N87-14284 

Theory for computing the field scattered from a Smooth 

P24 N87-13264 

WEATHER FORECASTINQ 

A-17 
SUBJECT INDEX 

WEWES 

Effect of a trade between boattail angle and wedge sire 

[NASA-TP-2717] p4 N87-23593 

Preliminary structural design of composite main rotor 

blades for minimum weight 

[ NASA-TP-27301 p 11 N87-25435 

I on the performance of a nonaxisymmetric wedge nozzle 

WEIGHT REDUCTION 

WEIGHTLESSNESS 

Miivity Fluid Management Symposium 

[ NASAGP-24651 p 13 N87-21141 

NASAlMSFC FY85 Atmospheric Processes Research 

Review 

[ NASA-CP-24021 p 20 N87-13043 

I WIND (YETEOROLOaY) 

WIND SHEAR 

I Ooppler Radar Detection of Wind Shear 

[NASACP-2435] p5 N87-10054 

Wind ShearlTurblence Inputs to Fliiht Simulation and 

Systems Certification 

INASA-CP-24741 p 1 N87-25267 

Experimental evaluation of wail Mach number 

dishibutions of the octagonal test section proposed lor 

NASA Lewis Research Center's aHitude wind tunnel 

[ NASA-TP-26661 p8 N87-17717 

Expenmental evaluation of two tuming vane designs for 

fan drive corner of 0.1-scale model of NASA Lewis 

Research Center's proposed altitude wind tunnel 

[NASA-TP-2646] p8 N87-18576 

Detailed flow surveys of turning vanes desgned for a 

0.1-scale model of NASA Lewis Research Center's 

proposed allitude wind tunnel 

[ NASA-TP-26801 p9 N87-20295 

WIND TUNNEL CALIBRATION 

Expenmental evaluation of honeycomb/screen 

configurations and shod contraction section for NASA 

Lewis Research Center's altitude wind tunnel 

[ NASA-TP-26921 p9 N87-23662 

Experimental evaluation of two turning vane designs for 

fan drive mer of 0.1-scale model of NASA Lewis 

ResearchCenter'sprcposedaltitudewindtunnal 

[ NASA-TP-2646 1 p8 N87-18576 

Detailed Row surveys of turning vanes desgned for a 

0.1-scale model of NASA Lewis Research Center's 

proposed altitude wind tunnel 

[NASA-TP-2680] p9 N87-20295 

Wind-tunnel free-fliht investigation of a 0.1 5-scale 

model of the F-1068 airplane with vmex flaps 

[ NASA-TP-27001 p3 N87-21855 

Experimental evaluation of blockage ratio and plenum 

evacualnn system Row effects on presswe disbhtkm 

for bodies of revolution in 0.1 scale model test section 

of NASA Lewis Research Center's proposed altihrde wind 

tunnel 

[NASA-TP-27021 p9 N87-22694 , WIND TUNNEL TESTS 

I Wind-tunnel investigation of the fliht characteristics of 

a canard general-aviation airplane configuration 

[NASA-TP-2623] p 1 N87-10039 

In-flight total forces, moments and static aeroelastic 

characteristics of an obligue-wing research ahpiam 

[NASA-TP-2224] p8 N87-10103 

WIND TUNNEL APPARATUS 

WIND TUNNEL DRIVES 

WIND TUNNEL MODELS 

Interference effects of thrust reversing on Mzontal tail 

effectiveness of twin-engine fighter aircraft at Mach 

numbers from 0.15 to 0.90 

[ NASA-TP-23501 p8 N87-10870 

Effect of port comer geomeby on the internal 

perfamance of a rotating-vane-typa Uwst reverser 

[NASA-TP-2624] p2 N87-12541 

Effects of winglet on transonic flutter characteristics of 

a cantilevered twin-engine-transport wing model 

[ NASA-TP-26271 p 17 N87-13789 

Wind-tunnel investigation at supmonic speeds of a 

remotecontrolled canard missile wim a free-rolling-tail 

brake torque system 

[NASA-TP-WJl ] p3 N87-17669 

Conelation of Miter imputsive noise from 

blade-vwtex interaction with rotor mean inflow 

[NASA-TP-2650] P 23 N87-18399 

Summary of studies to reduce wingmounted propfan 

installation drag on an M = 0.8 tramport 

[NASA-TP-2678] p6 N87-20980 

Wind-tunnel free-flight investigation of a 0.15-scale 

model of the F-1068 airplane with vortex flaps 

[NASA-TP-2700] p 3 N87-21855 

Experimental evaluation of blockage ratio and plenum 

evacuation system Row effects on pessure distribRion 

for bodies of revolution in 0.1 scale rodel test section 

of NASA Lewis Research Center's altitude wind 

tunnel 

[NASA-TP-2702] p9 N87-22604 

WIND TUNNEL WALLS 

ExperifIWntal evaluation of wall Mach number 

distributions of the octagonal test section proposed for 

NASA Lewis Research Center's altitude wind tunnel 

[ NASA-TP-26661 p8 N87-17717 

WIND TUNNELS 

Aeronautical fadlis assessment 

[NASA-RP-1146] p8 N87-10876 

Engineer in charge: A history of the Langley Aeronautical 

Laboratory, 1917-1958 

[NASA-SP-4305] p27 N87-24390 

Study of lee-side Rw over conically cambered Delta 

wings at supersonic speeds, part 2 

[ NASA-TP-2660-PT-21 p4 N87-25301 

Evaluation of installed performance of a 

wing-tipmounted pusher turbqxop on a semispan wing 

Effects of winglet on transonic flutter charactecistics of 

WlNQ LOADING 

WIN np VORTICES 

[NASA-TP-2739] p6 N87-26041 

WINGLETS 

a cantilevered twin-engimtranspnl wing model 

[ NASA-TP-26271 p 17 N87-13789 

WINOS 

Effects of winglet on transonic flutter characteristics of 

Subsonic manewer capability of a supersonic cruise 

fighter wing concept 

Flight investigation of the effects of an outboard 

wing-leading-edge modification on stall/spin 

characteristics of a low-wing, single-engine. T-tail liht 

sirplane 

[NASA-TP-2691] p 6 N87-23614 

Steady and unsteady aerodynamic forces from the 

SOUSSA surface-panel method for a fighter wing with tip 

missile and comparison with experiment and PANAIR 

[NASA-TP-2736] p4 N87-26032 

Jet transport flight operations using cockpit display of 

traffic information during instrument meteorological 

conditions: Simulation evaluation 

[ NASA-TP-25671 p5 N87-29469 

a cantilevered twinengine-transport wing model 

[NASA-TP-2627] p 17 N87-13789 

[ NASA-TP-26421 p2 N87-15184 

WORKLOADS (PSYCnOPHYSlOLOaY) 

X 

X RAY AISTRONOYY 

Essays in Space Science 

Rapid Fluctuations in Solar Flares 

[ NASACP-24641 p 25 N87-24247 

X RAYS 

[NASACP-2449] p 27 N87-21785 

z 

ZENITH 

Surface bidirectional reflectance properties of two 

SMmFWestem Arizona deserts for wavelengths between 

0.4 and 2.2 micrometers 

[ NASA-TP-26431 p 18 N87-22281 
PERSONAL AUTHOR INDEX 

NASA Scientific and Technical Publications 1987 

Typical Personal Author 

Index Listing 

PERSONAL AUTHOR bBLECH. RICHARO A Appluboni ad requirements for real.(lme sunulalcfs 

p 22 N87-23202 r KI pmunblest fuYhbn8 [ NASA-TP-28721 

Listings in this index are arranged alphabetically 

by personal author. The title of the document provides the user with a brief description of the subject matter. The report number helps to indicate 

the type of document listed. The page and accession numbers are located beneath and to the right 

of the title. Under any one author's name the accession numbers are arranged in sequence. 

A 

ABWL-HAYID, KHALED S 

MuHiscale twbulenca effects in supersonic jets 

exhausting into sM1 air 

[NASA-TP-27071 p 15 N87-24672 

ADEL", HOWARD Y. 

senslbnty hatyais in Engineering 

[NASACP-2457 J p 17 N87-18855 

ALBER". CINDY W. 

Abrolhermal evaluation of a aphmidty blunted bo& 

with a trapezoidal o(u) section in the hngh 8-fooi 

hgh-lempenhre tunnel 

[NASA-TP-2641] p 15 N87-18782 

TheJovianAbnospherea 

[NASACP-2441] p 26 N87-17598 

Wng symmelrias in the modeling and analysis of 

tires 

[NASA-TP-Z649] - p6 N87-17890 

~UWOU.YML 

ANDERSEN. CARL Y. 

ANDERSON, B. J. 

Development hh2 of kge volume water sprays for warm log dirpenvrl 

APPUY ZACHARY 1. 

[NASA-TP-2807] p 10 N87-12585 

Low-speed sero6ynamc . chamt-ofaDenenl arirlbll confiovacon wrim anp5 N87-28482 

BANGERT, LINDA S. 

Effects of afterbody boaltail design and empennage 

arrangement on aeropropulsive characteristics of a 

twin-engine ftghler rodel at transonic speeds 

[ NASA-TP-2704 J p3 N87-21873 

BARE, E. ANN 

Effect of a trade between boattail angle and wedge size 

on the performance of a nonaxisyrnmetric wedge nozzle 

[NASA-TP-2717] p4 N87-23593 

Static internal pedormance 01 a two-dimensional 

convergenldivergent nozzle with thrust vectoring 

[NASA-TP-2721] p4 N87-24432 

Multiaxis conbol power lrom thrust vectoring for a 

supersonic hghter aircraft model at Mach 0.20 to 2.47 

[ NASA-TP-27121 p4 N87-24433 

Theory fa Wng the lield sanered from a smooth 

inRected dace 

[NASA-TP-Z632] p24 N87-13264 

Some path-following technigues for solution 01 nonlinear 

equations and comparison wim paramebic dinerentiation 

[ NASA-TP-2654) p22 N87-14054 

On minimizing the number of calculations in 

[ NASA-TP-27061 p3 N87-23586 

Lowcoat FM osdllator for capacitance tvpe of blade 

BARBER, R. L 

BARBER. RAYMOND L 

desgrrtyaMlyrisBARRANGER. JOHN P. 

tip clearance measurement system 

[ NASA-TP-2746 J p7 N87-24481 

BARTH. J. Y. 

Cosmic ray heavy ion LET mapping for aluminum, sili. 

cndti.clueL¶rwts 

['NASA-RP-I ria] p27 N87-25984 

BIRTLETT. QLYNN R. 

EvaluatDn of installed performance of a 

wing-tipmounted pusher mop on a semispan wing 

[NASA-TP-2739] p6 N87-26041 

ch&Cvde. Freauencv-StaMe CO2 Laser 

BAITEN. CARMEN E. 

Technology 

[NASACP-2456] p 16 N87-20522 

BEARD. K. V. 

l%vdommt tesbng of large volume water sprays fa 

rnfoedgpersal 

[ NASA-TP-28071 p 10 N87-12585 

BELVIN, W. KEITH 

Modeling of plnts fa the dynam analys~~ of buss 

structures 

[ NASA-TP-28611 p 18 N87-20567 

BERRIER, B. L 

Effects of Icul wan and empennage arrangement on 

drag of a lvpcar wgbmgne whler aft end 

[ NASA-TP-23521 p 1 N87-10838 

Stak mtemal perfonname of mngleexpanwn-ramp 

[NASA-TP-2364] p2 N87-10839 

Effect of port oomer oeomeby on the mtemal 

perfamancaofar&bng-vanetypethnalreverser 

[NASA-TP-2824] p2 N87-12541 

Atlas of mde-flelbot-new outoolng longwave ndum 

norrles m ~-vectorlng cap&My up to 60 deg 

BE= 1. DALE 

denved fKm Nnag 8 Em mdmm tudgel data set. 

July 1975 to June 1978 

[NASA-RP-1185] 

BHAMK.Q. 

p21 N87-28489 

Elf& of winglel on transonic flutter chamteristia, of 

[NASA-TP-2827] p17 N87-13789 

speeds of a canard Wle with a treerolling-tail 

[NASA-TP-2401] p 3 N87-17BBB 

Geomorphology from space: A global oveniew of 

acantilevered -banspat*model 

BLAIR,A.a,JR. 

Wind-tunnel invgboatDn a1 

BLAIR, ROBERT W, JR. 

reoicMlBLAHD,SIYULLR 

[NASA-9-=1 pl8 N87-18139 

CakulaUon of viuxxa Mecb on transonic flow for 

[NASA-TP-2731] p 5 N87-27822 

oEcillathl!J~Mdcompvironswrim~ 

BLECH, RICHARD A. 

Applications and requirements for real-time simulators 

in ground-test facilities 

[NASA-TP-2672] 

BOQUE, RODNEY K. 

p 22 N87-23202 

Analog signal condiiioning for flight-test 

instrumentation 

[NASA-RP-1159] p 7 N87-29533 

Experimental evaluation of two turning vane designs for 

fan drive corner of 0.1-scale model of NASA Lewis 

Research Center's proposed attitude wind tunnel 

[ NASA-TP-26461 p8 N87-18576 

Detailed flow surveys 01 turning vanes designed for a 

O.l-sale model of NASA Lewis Research Center's 

proposed aWe wind tunnel 

[ NASA-TP-28801 p9 N87-20295 

Effects of aerosols and surlace shadowing on 

p 19 N87-28162 

BOWLES ROLAND L 

Wind ShearlTulbulence Inputs to Flight Simulation and 

Systems Certification 

[ NASA-CP-24741 p 1 N87-25267 

Piloted-simulation study of effects of vortex Raps on low-speed handling quali of a Delta-wingairplane 

[NASA-TP-2747] p8 N87-26922 

BOLDMAN, DONALD R. 

BOWKER, DAVID E. 

bidirectional reflectance measurements of deserts 

[NASA-TP-27561 

BRANDON, JAY Y. 

BRANDT, JOHN C. 

Atlas of Cwnet Haby 1910 II 

[ NASA-SP-4881 p26 N87-30235 

Caliation of the spin-scan ozone imager aboard the 

BRESSETTr, WALTER E. 

dynamics Eyqlore~ 1 satellie 

[ NASA-TP-27231 p21 N87-26491 

Liquid drop stability for protein crystal growth in 

[ NASA-TP-2724 J p21 N87-20727 

Piloted simulation s- of the effects of an automated 

trim system on fliht characteriatics of a liht twin-engine 

airplanewithoneer@neinopersthre 

[ NASA-TP-2833 J p 2 N87-10843 

Piloted-simulation study 01 effects of vortex flaps on 

low-speed handling qualities of a Della-winglurphne 

[ NASA-TP-27471 p8 N87-28922 

Adwlcad delectiar. isolation and Mxxwnmodation of 

BROOY,BET". 

micr0glS~ 

BROWN, P. W. 

BROWN, PHILIP w. 

BRUTON. WILLIAM Y. 

sensor failues: Real-time evaluation 

[NASA-TP-2740] 

BUCK, WARREN W. 

p8 N87-25331 

Possible complementary cosmic-ray systems: Nuclei 

p 24 N87-24977 

Paer cepsbum technique wim application to rodel 

[NASA-TP-2586] p23 N87-17479 

E- of W apan and.empennage amqmml on 

[ NASA-TP-23521 p 1 N87-10838 

Effeciofabadebehveen boatt.ilan#eandwadgasizs 

on the perlamanca of a noMdsMnmelrk wedaa nozde 

and MEnudei 

[NASA-TP-2741] 

BURLEY, C. L 

Miter amustic data 

BURLEY. J. R, II 

WofaW- me^ aft end 

BURLEY, JAMES R, II 

[NASA-TP-2717] . p4 67-23593 

BURLEY, RICHARD R. 
BURNS, R. A. PERSONAL AUTHOR INDEX 

Experimental evaluation of honeycomblscrwn 

confiurations and short contraction section for NASA 

Lewis Research Center's altitude wind tunnel 

[ NASA-TP-26921 p9 N87-23662 

Development testing of large volume water sprays for 

warm fog dispersal 

[NASA-TP-2607] p10 N87-12585 

BURNS. R. A. 

C 

CAMP, DENNIS W. 

Atmospheric Turbulence Relative to Aviation, Missile. 

and Space Programs 

[NASA-CP-2468] p 21 N87-22341 

CAMPBELL, WILLIAM J. 

Arctic Sea ice, 1973-1976 Satallite passive-microwave 

observations 

[NASA-SPJ891 p 21 N87-24870 

CAPONE. F. J. 

Interference effects of thrust reversing on hocizontal tail 

effectiveness of twin-engine fighter aircraft at Mach 

numbers from 0.15 to 0.90 

[ NASA-TP-23501 p8 N87-10870 

Effect of port wrner geometry on the internal 

performance of a rotating-vanetype thrust reverser 

[ NASA-TP-26241 p2 N87-12541 

CAPONE, FRANCIS J. 

Effects of empennage surface location on aerodynamic 

characteristics of a twin-engine afterbody model with 

nonaxisymmetric nozzles 

[ NASA-TP-23921 p 6 N87-17693 

Multiaxis control power from thrust vectoring for a 

supmonk fighter aircrafl model at Mach 0.20 to 2.47 

[NASA-TP-2712] p4 N87-24433 

Shot peening for T1lbAl4V alloy compressor blades 

[NASA-TP-2711] p 18 N87-20566 

Applicability of linearized-theory attached-flow methods 

to design and analysis of flap systems at low speeds for 

thin swept wings with sharp leading edges 

CAREK. GERALD A. 

CARLSON. HARRY W. 

[NASA-TP-2653] p2 N87-15174 

CARLSON, JOHN R. 

An experimental investigation of an advanced turboprop 

installation on a swept wing at subsonic and transonic 

[NASA-TP-27291 p4 N87-26883 

Effects of empennage surface location on aerodynamic 

characteristics of a twikengine afterbody model with 

nonexisymmetric nozzles 

NASA-TP-23921 p 6 N87-17693 

Effect of a trade between boanail angle and wedge size 

on the performance of a nonaxisymmetric wedge nozzle 

[ NASA-TP-2717 1 p4 N87-23593 

Arctic Sea ice, 1973-1976: Satellite passive-microwave 

mations 

[NASA-SP-489] p21 N87-24870 

Transonic flow analysis for rotors. Part 2: 

Threedimensional. unsteady. fullpotential calculation 

[ NASA-TP-2375-PT-21 p2 N87-10841 

Solution of elliptic patijal ditfwential equations by fast 

Poisson solvers using a local relaxation factor. 2 Two-step 

method 

[ NASA-TP-25301 p 22 N87-14918 

A simplified method for determining heat of combustion 

speeds 

CARSOW, GEORGE T., JR. 

CAVALIERI, DONALD J. 

c"G, 1. c. 

CHANG, S C. 

CHEGINI, HOSHANG 

of natural gas 

[NASA-TP-2682] p 16 N87-20514 

CHU, JULIO 

Pressure measurements on a thick cambered and 

twisted 58 deg delta wing at hih subsonic speeds 

[NASA-TP-2713] p5 N87-27643 

Frequency domain laser velocimeter signal processor: 

A new signal processing scheme 

[ NASA-TP-27351 p 16 N87-27994 

CLEMYOWS, JAMES I, JR. 

CLINE, THOMAS L 

Essays in Space sdence 

[NASA-CP-2464] P 25 N87-24247 

Testing of UHM)A heliter transmission in NASA 

Lewis 2240-kW (3000-hp) facility 

[NASA-TP-2626] P 16 N87-10391 

Arctic Sea ice, 1973-1 976: Satellie passive-microwave 

observations 

[NASA-SP-489] P 21 N87-24870 

COE. H. H. 

COYISO, JOSEFINO C. 

CONNOR. ANDREW B. 

Correlation of helicopter impulsive noise lrom 

blade-vortex interaction with rotor mean inflow 

[ NASA-TP-26501 p 23 N87-18399 

Electron stimulated desorption of atomic oxygen from 

silver 

[ NASA-TP-26681 p 12 N87-18629 

Expanmental evaluation of wall Mach number 

distributions of the octagonal test section proposed for 

NASA Lewis Research Center's altitude wind tunnel 

[NASA-TP-26661 p8 N87-17717 

Investigation of leading-edge flap performance on delta 

and double-delta wings at supersonic speeds 

[ NASA-TP-26561 p3 N87-20233 

COY, JOHN J. 

Vibration characteristics of OH-58A helicopter main rotor 

transmission 

[ NASA-TP-27051 p 17 N87-20555 

[ NASA-CP-24481 p 19 N87-15528 

Doubiy ditferential cross sections for galactic heavy-ion 

fragmentation 

CORALLO, GREGORY R. 

CORBAN. ROBERT R. 

COVELL, PETER F. 

CROSLEY, DAVID R. 

Future directions for H sub x 0 sub y detection 

CUCINOlTA, FRANCIS A. 

[ NASA-TP-26591 p24 N87-17487 

CUNNINGHAM, HERBERT J. 

Steady and unsteady aerodynamic forces from the 

SOUSSA surface-panel method for a fighter wing with tip 

missile and comparison with experiment and PANAIR 

[ NASA-TP-27361 p4 N87-26032 

Performance of textured carbon on copper electrode 

multistage depressed collectors with medium-power 

traveling wave tubes 

[NASA-TP-2665] p 14 N87-17990 

Pulse Code Modulation (EM) encoder handbook for 

CURREN, ARTHUR N. 

CURRIER, S. F. 

Aydin Vector MMP-600 series system 

[NASA-RP-1171] p 13 N87-11916 

CURRY, R. E. 

In-flight total forces, moments and static aeroelastic 

characteristics of an oblique-wing research airplane 

[NASA-TP-2224] p8 N87-10103 

Flihtdetermined aerodynamic derivatives of the AD1 

oblique-wing research airplane 

[ NASA-TP-22221 p8 N87-10871 

Fliht characteristics of the AD-1 oblque-wing research 

aircraft 

[ NASA-TP-22231 p8 N87-18570 

CURRY, ROBERT E. 

D 

DANFORD, MERLIN D. 

The conosion mechanisms for primer coated 2219.T87 

[ NASA-TP-27151 p 12 N87-21076 

Hydrogen trapping and the interaction of hydrogen with 

metals 

[ NASA-TP-27441 p 12 N87-25463 

DANIEL, RON 

Liquid drop stability for protein -tal growM in 

microgravity 

[NASA-TP-27241 p21 N87-20727 

@likability of linearized-theory attached-flow methods 

to desgn and analyss of flap systems at low speeds for 

thin Swept wings with sharp leading edges 

[NASA-TP-2653] p2 N87-15174 

Measurements of flow rate and trajectay of aircraft 

tiregenerated water spray 

[NASA-TP-2718] p6 N87-24458 

Upper and Middle Atmospheric Density Modeling 

Requirements for Spacecraft Design and Operations 

[NASA-CP-2460] p20 N87-20665 

aluminum 

DARDEN, CHRISTINE Y. 

DAUGHERTY, ROBERT H. 

DAVIS, M. H. 

DAVIS. PAMELA A. 

Langley Aircraft Landing Dynamics Facility 

[NASA-RP-1189] p9 N87-29544 

Effects of aerosols and surface shadowing on bidirectional reflectance measurements of deserts 

[NASA-TP-27561 p 19 N87-28162 

Evaluation of diffuseillumination holographic 

cinematcgraphy in a flutter cascade 

DAVIS, RICHARD E. 

DECKER, A. J. 

[NASA-TP-25931 p 16 N87-13731 

MLMT, JOHN C. 

Advanced detection, isolation and accommodation of 

sen801 failures: Real-time evaluation 

[NASA-TP-2740] p8 N87-25331 

DELNORE, V. E. 

Doppler Radar Detection of Wind Shear 

[NASA-CP-2435] p5 N87-10054 

DENNIS, BRIAN R. 

Rapid Fluctuations in Solar Flares 

[ NASA-CP-24491 p 27 N87-21785 

On the Mamellian distribution, Symmetric form, and 

entropy conservation for the Euler equations 

[NASA-TP-2583] p14 N87-11963 

A second-order accurate kinetic-theory-based method 

DESHPANDE, 8. M. 

DESHPANDE, SURESH M. 

for inviscid compressible flows 

[NASA-TP-2613] p 15 N87-18783 

DICARLO, DANIEL J. 

Flight investigation of the effects of an outboard 

wing-leading-edge modification on stalllspin 

characteristics of a low-wing, single-engine, T-tail light 

airplane 

[ NASA-TP-28911 p 6 N87-23614 

Theocy for computing the field scattered from a smooth 

inflected surface 

[ NASA-TP-26321 p24 N87-13264 

DONN, BERTRAM 

DOYINEK, A. K. 

Atlas of Comet Halley 1910 II 

[NASA-SP-488] p26 N87-30235 

Development of confidence limits by pivotal functions 

for estimating software reliability 

[ NASA-TP-27091 p23 N87-23244 

The ACEE program and basic composites research at 

Langley Research Center (1975 to 1986): Summary and 

bibliography 

[NASA-RP-1177] p 11 N87-29612 

Effects of thermal cycling on graphie-fiber-reinforced 

DOTSON, KELLY J. 

DOW, MARVIN B. 

DRIES, 0. A. 

6061 aluminum 

[ NASA-TP-26121 pll N87-10184 

DUNHAM, DANA MORRIS 

Low-speed aerodynamic characteristics of a twin-engine 

general aviation configuration with aft-fuselage-mounted 

pusher propellers 

[NASA-TP-2763] p 5 N87-29462 

DURBIN, P. A. Asymptotic analysis of corona discharge from thin 

electrodes 

[ NASA-TP-26451 p24 N87-14998 

Efficient solutions to the Euler equations for supersonic 

flow WiM embedded subsonic regions 

[NASA-TP-2523] p2 N87-15183 

DWOYER. DOUGLAS L 

E 

EBIHARA, BEN T. 

hsgn. fabrication and performance of small, graphite 

electrode, multistage depressed collectors with 200-W. 

CW, 8- to 18-GHz traveling-wave tubes 

[ NASA-TP-26931 p 14 N87-20474 

Traveling-wave-tube efficiency improvement by a 

lowco8t technique for deposition of carbon on multistage 

depressed collector 

[ NASA-TP-27191 p 14 N87-21239 

EHERNBERGER, L J. 

Qualitative evaluation of a flush air data system at 

transonic speeds and huh angles of attack 

[ NASA-TP-27181 p8 N87-29497 

ENQLAR, R. J. 

Large-scale static investigation of 

circulationcontrol-wing conc8pts applied to uwr 

surface-blowing aircraft 

[ NASA-TP-26841 p6 N87-15959 

Large-scale static investigation of 

circulationcontrol-wing concepts applied to upper 

surface-blowing aircrafl 

[NASA-TP-2684] p 6 N87-15959 

EPPEL. J. C. 

ESPENAK. F. 

Ten year planetary ephemeris: 1986-1995 

[NASA-RP-11761 p 25 N87-14219 

ESPENAK, FRED 

Fii year canon of solar eclipses: 1986 - 2035 

[NASA-RP-1178-RNl P26 N87-25906 

F 

FICHTL. GEORGE H. 

[ NASA-CP-24291 

Spacelab 3 Mission Science Review 

p 15 N87-22103 

E2 
PERSONAL AUTHOR INDEX KIBLER, JAMES F. 

FINELLI, GEORGE B. A technique for evaluating the application of the pin-level 

stuck-at fault model to VLSl circuls 

[ NASA-TP-27361 p 17 N87-28025 

Frontiers of Massively Parallel Scientific Computation 

[ NASACP-24781 p22 N87-26531 

Calculation of secondary electron traiectories in 

multistage depressed wllectas for microwave ampMiers 

[NASA-TP-2664] p 14 N87-17991 

Analyhcal and experimental performance of a dual-mode 

traveling wave tube and mubtage depressed wllector 

[ NASA-TP-27521 p14 N87-25532 

FISHER, JAMES R. 

FORCE, DALE A. 

FOUSHEE, H. CUYTON 

Cockpit Resource Management Training 

[NASA-CP-24551 p 5 N87-22634 

FOX, CHARLES H., JR. 

Subsonic maneuver capability of a supecsonic mise 

fighter wing cmcept 

[NASA-TP-2642] p2 N87-15184 

Subsonic hgihrdinal and lateraldirectional 

characteristics of a forward-swept-wing fighter 

configuration at angles of attack up to 47 deg 

[ NASA-TP-27271 p4 N87-26874 

FROST, WALTER 

Atmospheric ' Turbulence Relative to Aviation, Missile, 

and Space Programs 

[ NASA-CP-24681 p21 N87-22341 

Wind Shear/Turbulance Inputs to Flight Simulation and 

Systems Certification 

[NASACP-2474] pl N87-25267 

Bit-emx-rate testing of hgh-power 30-GHz traveling 

wave tubes for ground-terminal applications 

[ NASA-TP-26351 p 13 N87-17971 

FWIKAWA, QENE 

G 

GELD€R, THOUAS F. 

Detailed Row surveys of turning vanes designed for a 

0.1 -scale model of NASA Lewis Research Center's 

proposed altitude wind tunnel 

[NASA-TP-ZWO] p9 N87-20295 

GENTRY, GARL L. JR. 

Low-speed aerodynamic characteristics of a twin-engine 

general aviation conliguration with aft-ba&gemmted 

Plh Pmpelm 

[ NASA-TP-27631 p5 N87-29482 

GEZIRI, DANIEL Y. 

Infrared source cross-index. first ed&n 

[NASA-RP-1182] p 25 N87-22573 

Aerothermal tests of spherical dome protuberances on 

a flat plate at a Mach number of 6.5 

[NASA-TP-2631] p14 N87-13664 

QLOERSEN, PER 

Arctic Sea ice, 1973-1976 Satellite passivemicrowave 

obseFvstions 

[NASASP-489] p21 N87-24870 

MkXOgravity aystallization of macromolecules: An 

interim repat and proposal for continued research 

[NASA-TP-2671] p13 N87-20423 

GLASS, c. E. 

QOLDBERQ. BENJAMIN E. 

OOFM. LESLIE 

Finiteelement reenby heat-transfer analysls of space shuttle Mer 

[NASA-TP-2657] p 16 N87-29795 

QORDLEY. L L 

Description of data on the Nimbus 7 LlMS map archive 

[NASA-TP-2625] pl9 N87-13022 

Piloted simulator study of allowable time delays in 

[NASA-TP-2652] p8 N87-16849 

A SvnchmnWs data analyzer for the Minimum Delay 

Data Format (Mow) and Launch Trajectcq Acqucaition 

System (LTAS) 

[NASA-TP-27431 p13 N87-24590 

tape:oroneandnitlicacid 

GRANTHAM. WILLIAM D. 

-responee 

GREEN, ANDREW J. 

H 

HAFrKA, RAPHAEL 1. 

sensitivity AM)ysis in Engineering 

[NASACP-2457] p17 N87-18855 

HAQQARD, K. V. 

of data on the Nimbus 7 LlMS map archive 

[NASA-TP-26251 p 19 N87-13022 

tape:ozareandnibicacid 

HANSEN, JAMES R. 

Engineer in charge: A histay of the Langley Aeronautical 

Laboratory, 1917-1958 

[NASASP-4305] p27 N87-24390 

Experimental evaluation of wall Mach number 

distributions of the octagod test section proposed for 

NASA Lewis Research Center's altitude wind tunnel 

[ NASA-TP-26661 p8 N87-17717 

EXperimerW evaluation of Mockage ratio and plenum 

evacuation syatem Row effects on pressure distribution 

for bodies of revolution in 0.1 scale model test section 

of NASA Lewis Research Center's proposed altitude wind 

tunnel 

[ NASA-TP-27021 p9 N87-22694 

Experimental evaluation of honeywmblscreen 

configurations and shoct contraction section for NASA 

Lewis Research Center's altitude wind tunnel 

[NASA-TP-2692] p9 N87-23662 

HARRINGTON. DOUGLAS E. 

HARRIS,€. ' 

Proceedings of the 5th Annual Users' Conference 

[ NASACP-23991 p 22 N87-10720 

HARRIS, ELFRIEDA 

Sixth Annual Users' Conference 

[NASA-CP-2483] p22 N87-23156 

Mach 8 experimental and theoretical stability and 

performance of a cruciform missile at angles of attack 

upto65degrws 

[ NASA-TP-27331 p4 N87-23592 

HARTMAN, EDWARD R. 

HENDRICKS, ROBERT C. 

Threestep labynnm seal for hgh-performance 

turbomachines 

[ NASA-TP-18481 p 15 N87-23921 

Straight cylindrical sen1 for hgh-perfcfmance 

turbomachines 

[ NASA-TP-18501 p 15 N87-23936 

Threestep cylindrical seal for hgh-performance 

turbomachines 

[ NASA-TP-18491 p 15 N87-24639 

Electronics reliability and measurement technology 

[ NASACP-24721 p 17 N87-27204 

HEYMAN, JOSEPH S 

HILL, CHARLES K. 

Spacelab 3 Mi- Science Review 

[ NASACP-24291 p 15 N87-22103 

A simulation evaluation of a pilot interface with an 

automatic terminal approach system 

[NASA-TP-2689] p 7 N87-19393 

Helicopter bladsvortex interaction locations: 

Scalemodel acoustics and free-wake analyslsrewlts 

[ NASA-TP-26581 p3 N87-18537 

HINTON, DAVID A. 

HOAD, DANNY R. 

WELL, JAMES M. 

Future directions for H sub x 0 sub y detection 

[NASA-CP-2448] p 19 N87-15528 

HOFFMAN. LAWRENCE H. 

Calculation and accuracy of ERBE scanner 

measurement locations 

[NASA-TP-2670] p25 N87-28471 

Electron stimulated desorption of atomic oxygen from 

silver 

[NASA-TP-m] p 12 N87-18629 

Penneation of oxygen through hgh purity. large grain 

silver 

[ NASA-TP-27551 p 12 N87-27024 

HOFLUND, GAR B. 

HOWELL, LEONARD 

Probabilistic risk andysk Of flying the space shuttle with 

and without fuel turbine discharge temperature redline 

[NASA-TP-2759] p23 N87-27474 

Calculation of viscars effects on transonic flow for 

[NASA-TP-2731] p5 N87-27622 

subsonic hgitudnal and lateral-directiod 

characteristics of a forward-swept-wing fighter 

configuration at angle% of attack up to 47 deg 

[NASA-TP-27271 p4 N87-28874 

protection 

HOWLElT, JAMES 1. 

oscillating airfoils and comparisons with experiment 

HUFFMAN. JARRm K. 

HUFFMAN. P. D. 

Preliminary estimates of radiosonde thermistor enws [NASA-TP-2637] p 20 N87-12088 

Aerothennal tests of sphmcal dome protuberances on a Rat plate at a Mach number of 6.5 

[NASA-TP-2631] p14 N87-13664 

HUNT. L R. 

I 

ILIFF, KENNETH W. 

Application of parameter estimation to aircraft stabili 

and control: The outpot-error approach 

[NASA-RP-1 1681 p6 N87-29499 

Ground-based time-guidance algorithm for control of 

airplanes in a timemetered air traffic control environment: 

A piloted simulation study 

[ NASA-TP-26161 p7 N87-10864 

Space station structures and dynamics test program 

[ NASA-TP-27101 p 18 N87-20588 

IMBERT, N. 

IVEY, EDWARD W. 

J 

JALUFKA, N. W. 

Laserpowered MHD generators for space application 

[NASA-TP-2621] p24 N87-10764 

In-flight surface oil-flow photographs with comparisons 

JENNETT, USA A. 

to pressure distribution and boundary-layer data 

[ NASA-TP-23951 P3 N87-20966 

JOHNSON, D. L 

Upper and Middle Atmospheric Density Modeling 

Requirements lor Spacenaft Design and Operations 

[ NASACP-24601 p20 N87-20665 

Qualitative evaluation of a flush air data system at 

transonic speeds and hgh angles of attack 

[NASA-TP-2716] p6 N87-29497 

Mach 6 experimental and theoretical stability and 

performance of a cruciform missile at angles of attack 

up to 65 degrees 

[ NASA-TP-27331 p4 N87-23592 

JONES, MICHAEL Q. 

Experimental validation of a two-dimensional shear-flow 

JOHNSON. J. BLAIR 

JOHNSTON. PATRICK J. 

rodel for determining acoustic impedance 

[NASA-TP-2679] P23 N87-20798 

JONES, WILLIAM H. 

Combined aerodynamic and strubrral dynamic probkm 

emulating routines (CASPER): Theory and 

implementation 

[NASA-TP-2418] p3 N87-17669 

Ester oxidation on an aluminum surface using 

chemiluminesceoce 

[ NASA-TP-26111 p12 N87-18886 

Cosmic ray heavy ion LET mapping for aluminum, silicon. 

and tissue targets 

[NASA-RP-1180] p27 N87-25984 

JONES, WILLIAM R, JR. 

JORDAN, 1. M. 

K 

KACYNSKI, KENNETH J. 

Experimental thrust performance of a hgh-area-ratio 

rocket nozzle 

[ NASA-TP-27201 p 10 N87-20381 

Comparison of theoretical and experimental thrust 

performance 01 a 10301 area ratio rocket noale at a 

chamber pressure of 2413 kNlm2 (350 psia) 

[ NASA-TP-27251 p 11 N67-25423 

Experimental evaluation of heat transfer on a 10301 

area ratio rocket nozzle 

[NASA-TP-27261 p 11 N87-25424 

Conventionally cast and forged copper alloy for 

[ NASA-TP-26941 p12 N87-18902 

Calibration of the spin-scan ozone imager aboard the dynamics Eqbrer 1 satellite 

[ NASA-TP-27231 p21 N87-26491 

Space shume main engine hgh pressure fuel pump aft 

platform seal cavity flow analysis 

[ NASA-TP-26851 p14 N87-17000 

Development testing of large volume water sprays for 

[ NASA-TP-26071 p10 N87-12585 

DwMy differential cross sections for galactic heavyion 

fragmentation 

KAUROFF. JOHN M. 

highheat-flW thNSt Challlben, 

KEATINCI, QERALD Y. 

KEETON, L W. 

KELLER. V. W. 

warm fog dispersal 

KHANDELWAL, QOVlND 8. 

[ NASA-TP-26591 p24 N87-17487 

KIBLER. JAMES F. 

Calculation and accuracy of ERBE scanner 

meaaurerrmnt locations 

[ NASA-TP-26701 p25 N87-28471 

8-3 
KIPLINGER, ALAN L 

KIPUNGER, ALAN L 

Rapid Fluctuations in Solar Flares 

The COnOSiOn mechanisms for primer coated 2219-T87 

aluminum 

[NASA-TP-27151 p 12 N87-21076 

KNOX. C. E. 

Ground-based time-guidance algorithm for control 01 

airplanes in a time-metered air traffic control environment 

A piloted simulation study 

[ NASA-TP-26161 p7 N87-10864 

KO, WILLIAM L 

Finiteelement reentry heat-transfer analysis of space 

shuttle Mer 

[ NASA-TP-26571 p 16 N87-29795 

Analytical and experimental performance of a dual-mode 

traveling wave tube and multistage depressed collector 

[ NASA-TP-27521 p 14 N87-25532 

Numerical simulation of channel flow transition, 

resolution requirements and struclure of the hairpin 

vortex 

[NASA-TP-2667] p3 N87-19351 

Energetic Phenomena on the Sun: Tha Solar Maximum 

Mission Flare Workshop. Proceedings 

[NASACP-24391 p 28 N87-19328 

Description of data on the Nimbus 7 LlMS map archive 

tape: Ozone and nihic acid 

[ NASA-TP-26251 p 19 N87-13022 

[ NASA-CP-24491 p 27 N87-21785 

KNOCKEMUS, WARD W. 

KOSMAHL, HENRY 0. 

KRIST, STEVEN E. 

KUNW, MUKUL 

KURZEJA, R. J. 

KUTLER, PAUL 

Supercomputing in Aerospace 

[ NASACP-24541 p4 N87-25998 

L 

LADSON. CHARLES L Evolution. calibration, and operational characteristics of 

the twodimensional test secfion 01 the Langley 0.3-meter 

transonic cryogenic tunnel 

[NASA-TP-27491 p9 N87-28570 

Development testing of large volume water sprays for 

warm fog dispersal 

[NASA-TP-2607] p 10 N87-12585 

Pressure measurements on a thick cambered and 

twisted 59 dag delta wing at hgh subsonic speeds 

[ NASA-TP-27131 p5 N87-27643 

Quantitative analysis of the reconstruction performance 

of interpolants 

[ NASA-TP-26681 p23 N87-22441 

Expenments in encoding multilevel images as 

[ NASA-TP-27221 p 23 N87-28367 

LALA, 0.0. 

LAMAR, JOHN E. 

LANSING, DONALD L 

quadtrees 

LARSON, TERRY J. 

Witive evaluation of a flush air data system at 

transonic speeds and high angles of attack 

[NASA-TP-2716] p6 N87-29497 

Annoyance response to simulated advanced turboprop 

LEATHERWOOD, JACK D. 

aircraft interior noise containing tonal beats 

[ NASA-TP-26891 p 23 N87-24161 

LEAVllT, L D. 

Static internal performance of singleexpansion-ramp 

[ NASA-TP-23641 p2 N87-10839 

Effects of afterbody boattail &sign and empennage 

arrangement on aeropropulsive characteristics of a 

twin-engine fighter model at transonic speeds 

nonles with thrust-vectoring capability up to 60 dag 

LEAVITT, LAURENCE D. 

[ NASA-TP-27041 p3 N87-21873 

LECROY. STUART R. 

Surface bidirectional reflectance properties of two 

sammestem Arizona deserts for wavelengths between 

0.4 and 2.2 micrometers 

[ NASA-TP-26431 p 18 N87-22281 

LEE, 0. 

Automated Reduction of Data from Images and 

Holograms 

[ NASACP-24771 p5 N87-29432 

LEE, LARRY D. 

New methods and results for quantification of 

[NASA-TP-27371 p3 N87-2t871 

Summary of studies to reduce wing-mwnted propfan 

installation drag on an M = 0.8 transport 

[ NASA-TP-26781 p6 N87-20990 

lightning-aircraft electrodynamics 

LEVIN, ALAN D. 

PERSONAL AUTHOR INDEX 

LEVINE. JOEL S. 

Space Opportunities for Tropospheric Chemistry 

Research 

[ NASA-CP-24501 p 20 N87-18248 

Predicted effect of dynamic load on pitting fatigue life 

for low-contact-rstic spur gears 

[ NASA-TP-26101 p 18 N87-18095 

Vibration characteristics of OH-58A helicopter main rotor 

transmisbn 

[ NASA-TP-27051 p 17 N87-20555 

Spectroscopic comparison of effects of electron 

radiation on mechanical properties of twopdyimides 

[ NASA-TP-2663 I p 11 N87-18611 

Spectroscopic comparison of effects of electron 

radiation on mechanical properties of twopoiyimides 

[NASA-TP-26631 p 11 N87-18611 

Space shuffle main engine high pressure fuel pump aft 

platform seal cavity flow analysis 

[ NASA-TP-26851 p14 N87-17000 

Preliminary estimates of radiosonde thermistor enors 

[ NASA-TP-26371 p 20 N87-12086 

LEWICKI. DAVID 0. 

LONG, EDWARD R., JR. 

LONG, SHEILA ANN T. 

LOWRY, S. A. 

LUERS, J. K. 

LYONS, VALERIE J. 

Velocity profiles in laminar diffusion flames 

[ NASA-TP-25961 p15 N87-18035 

M 

MAINE, RICHARD E. 

Application of parameter estimation lo aircraft stability 

and control: The wtput-enor approach 

[NASA-RP-11681 p6 N87-29499 

A simpli method for determining heat of combustion 

[NASA-TP-26821 p 16 N87-20514 

MALL, GERALD H. 

of natural gas 

YANN, M. J. 

Forward-swept wing configuration designed for high 

maneuverability by use of a transonic computational 

method 

[ NASA-TP-26281 p 2 N87-11702 

Subsonic longitudinal and lateraldirectional 

characteristics of a forward-swept-wing fighter 

configuration at angles of attack up to 47 deg 

[ NASA-TP-27271 p4 N87-26874 

Low-speed aerodynamic characteristics of a twin-engine 

general aviation configuration with aft-fuselagemounted 

pusher propellers 

[ NASA-TP-27631 p 5 N87-29462 

Effect of Reynolds number variation on aerodynamics 

of a hydrogen-fueled transpoct concept a1 Mach 6 

[NASA-TP-2728] p4 N87-26031 

YANN, MICHAEL J. 

MANUEL, GREGORY S. 

MARCUM, DON C., JR. 

MARGLE, JANICE M. 

Velocity profiles in laminar diffusion flames 

[NASA-TP-25961 p 15 N87-18035 

Power cepstrum technique with application to model 

heliter acoustic data 

[NASA-TP-25861 p 23 N87-17479 

Correlation of helicopter impulsive noise from 

bladevortex interaction with rotor mean inflow 

[ NASA-TP-26501 p 23 N87-18399 

Interference effects of thNSt reversing on horizontal tail 

effectiveness of twin-engine fighter aircraft at Mach 

numbers from 0.15 to 0.90 

[NASA-TP-2350] p8 N87-10870 

Supersonic. nonlinear. attached-flow wing design for 

high li with experimental validation 

[ NASA-TP-23361 p 1 N87-10042 

Pulse Code Modulation (PCM) data storage and analysis 

MARTIN, R. M. 

MASON, M. L 

MASON, W. H. 

MASSEY, D. E. 

using a microcomputer 

[ NASA-TP-26291 p 13 N87-12718 

MCCLELUN, V. A. Doppler Radar Detection of Wind Shear 

[NASACP-2435] p5 N87-10054 

Aibnw lidar measurements of El Chichon stratospheric 

aerosols. May 1983 

[NASA-RP-1172] pl9 N87-11358 

SAGE aerosol measurements. Volume 3 January 1. 

1981 to November 18,1981 

[NASA-RP-1173] p 19 N87-17417 

MCCORMICK, M. P. 

MCCORMICK, M. PATRICK 

Airborne lidar measurements of El Chichon stratospheric 

aerosols, January 1984 

[NASA-RP-1175] p20 N87-20663 

[NASA-RP-1182] p 25 N87-22573 

MEADOR, MICHAEL A. 

Ester oxidation on an aluminum surface using 

chemiluminescence 

[NASA-TP-2611] p 12 N87-18666 

Forward-swept wing configuration designed for hgh 

maneuverability by use of a transonic computational 

method 

MEAD, JAYLEE M. 

Infrared source cross-index, first edition 

MERCER, C. E. 

[ NASA-TP-26281 p2 N87-11702 

MERRILL, WALTER C. 

Advanced detection, isolation and accommodation of 

sensor failures: Real-time evaluation 

[ NASA-TP-27401 p 8 N87-25331 

Development testing of large volume water sprays for 

MEYER, Y. 8. 

warm fog dispersal 

[ NASA-TP-26071 p 10 N87-12585 

MEYER, ROBERT R., JR. 

In-flight surface oil-flow photographs with comparisons 

lo pressure distribution and boundary-layer data 

[ NASA-TP-23951 p3 N87-20966 

Piloted simulator study of allowable time delays in 

large-airplane response 

[ NASA-TP-26521 p8 N87-16849 

Frequency domain laser velocimeter signal processor: 

MEYER, ROBERT T. 

MEYERS, JAMES F. 

A new signal processing scheme 

[ NASA-TP-27351 p 16 N87-27994 

MIDDEN, RAYMOND E. 

Description and calibration of the Langley Hypersonic 

CF4 tunnel A facility for simulating low gamma flow as 

occurs for a real gas 

[ NASA-TP-23841 p 18 N87-29778 

MILLER, CHARLES G., 111 

Description and calibration of the Langley Hypersonic 

CF4 tunnel: A facility for simulating low gamma flow as 

occurs for a real gas 

[ NASA-TP-23841 p 16 N87-29778 

Supersonic, nonlinear. attached-flow wing design for 

high li with experimental validation 

[ NASA-TP-23361 pl N87-10042 

Investigation of leading-edge flap performance on delta 

and doubledelta wings at supersonic speeds 

[ NASA-TP-26561 p3 N87-20233 

Closed-Cycle, Frequency-Stable CO2 Laser 

Technology 

[ NASACP-24561 p 16 N87-20522 

Testing of UH-GOA helicopter transmission in NASA 

MILLER, D. S. 

MILLER, DAVID S. 

MILLER, IRVlN M. 

MITCHELL, A. M. 

Lewis 2240-kW (3000-hp) facility 

[ NASA-TP-26261 p 16 N87-10391 

Proceedings of the 1985 NASA Amas Research Center's 

Ground-Effects Workshop 

[ NASA-CP-24621 p 4 N87-24410 

On minimizing the number of calculations in 

design-by-analysis codes 

[ NASA-TP-27061 p3 N87-23586 

Space station structures and dynamics test program 

[NASA-TP-2710] p 18 N87-20568 

Experimental evaluation of two turning vane designs for 

fan drive mer of 0.1-scale model of NASA Lewis 

Research Center's proposed altitude wind tunnel 

[ NASA-TP-26461 p8 N87-18576 

for a 

0.t-scale model of NASA Lewis Research Center's 

proposed altitude wind tunnel 

MITCHELL, KERRY 

MOW ANUTOSH 

MOORE, CARLETON J. 

MOORE. ROYCE D. 

Detailed Raw surveys of turning vanes 

[NASA-TP-M] p9 N87-20295 

MOOREHEAD, TAUNA W. 

Double Layers in Astrophysics 

[NASACP-24691 p 25 N87-23313 

MORALES, WILFRED0 

Ester oxidation on an aluminum surface using 

chemiluminescence 

[NASA-TP-2611 I p 12 N87-18666 

Joint University Program for Air Transportation 

Research. 1983 

[NASA-CP-2451 I p 1 N87-18520 

Joint University Program for Air Transportation 

Research. 1984 

[ NASACP-24521 p 1 N87-22604 

MORRELL, FREDERICK R. 

E4 
PERSONAL AUTHOR INDEX 

Joint University Program for Air Transpcftation 

Research. 1985 

[NASA-CP-2453] p 1 N87-27596 

The 1985 Goddard Space Flight Center Battery 

p 14 N87-11072 

The lges Get Away Speaal Expenmentec's 

Symposium 

[ NASACP-24381 p9 N87-20302 

MORROW, Q. 

Workshop 

[ NASA-CP-24341 

YOSIER. mmEs L 

N 

NAQARWA, K. S. 

Effects of winglet on transonic flutter characteristics of 

a cantikwered twin-engiwtransport wing model 

[NASA-TP-2627] p 17 N87-13789 

Atlas of absaption lines from 0 to 17900 an (sup)-t 

Large-& static investigation of 

circulation-cmtrd-wing CMlCepts applied to upper 

surfaceblowing airaafl 

NAYKUNQ, J. S 

[ NASA-RP-t 1881 p 19 N87-28955 

NICHOLS, J. H, JR. 

[NASA-TP-2684] p6 N87-15959 

NIXON. MARK W. 

Preliminmy structural design of compoeite main rotor 

blades for minimum weight 

[NASA-TP-27301 p 11 N87-25435 

NOOR. AHYED K. 

Expbibng symmebies in the modeling and anelysls of 

tires 

[NASA-TP-Z649] p 6 N87-17690 

Doubly differential cross sections for galactic heavyjon 

fragmentation 

[ NASA-TP-26591 p 24 N87-17487 

Possible complementsry cosmic-ray systems: Nuclei 

and antinuclei 

[ NASA-TP-2741 I p 24 N87-24977 

NORBURY. JOHN W. 

0 

ORLADY, HARRY W. 

Cockpit Resource Management Training 

Essays in Space science 

Rapid Fluctuations in Solar Flares 

Aifbome li measurements of El Chichon stratospheric 

aerosols. May 1983 

Aibcfne lii measurements of El Chichon stratospheric 

ads. January 1984 

[NASA-RP-t175] p20 N87-20663 

Material characterization of superplasticsrly formed 

titanium (liiAI-2Sn-4Zr-2Mo) sheet 

[NASACP-24551 p5 N87-22834 

ORYES, JONATHAN F. 

[NASACP-24641 p 25 N87-24247 

ORWIQ, LARRY E. 

[ NASA-CP-24491 p 27 N87-21785 

OSBORN, Y. T. 

[NASA-RP-l1721 pl9 N87-11358 

OSSA, WILLIAM A. 

[ NASA-TP-28741 p 12 N87-20407 

OSWALD. F. B. 

Testing of UHBOA helier transmission in NASA 

Lewis 2240-kW (30oO-h~) facility 

[NASA-TP-2826] p 18 N87-10391 

Gear tooth stress measurements on the UH-GOA 

[NASA-TP-Z698] p 17 N87-22235 

Electron stimulated desorption of atomic oxygen from 

silver 

[NASA-TP-2868] p 12 N87-18829 

Permeation of oxygen through Mgh pxnv. large grain 

silver 

[ NASA-TP-27551 p 12 N87-27024 

Wi drop stability for protein crystal growth in 

[ NASA-TP-27241 p21 N87-20727 

OSWALD, FRED B. 

Ileliiermm 

OUTLAW, R. A. 

OWEN, ROBERT B. 

P 

PACK, HOMER C, JR. 

Solar may flight ewdynamic augmentation 

experiment 

[NASA-TP-2890] p 10 N87-20380 

A technique for evaluating the application of the pin-level 

stuck-at faun model to VLSl circuits 

[NASA-TP-2738] D 17 N87-28025 

PALUYBO. DANIEL L 

PARK, J. H. 

Atlas of absorption lines from 0 to 17900 cm (sup)-1 

[NASA-RP-1 1881 p 19 N87-28955 

QuanWative analysis of the reconstruction performance 

of interpolants 

[NASA-TP-2688] p23 N87-22441 

Arctic Sea ice. 1973-1976: Satellite passivemiawave 

observations 

[NASA-SP-489] p21 N87-24870 

Experimental Validation of a two-dimensional shear-flow 

model for determining acoustic impedance 

[ NASA-TP-26791 p23 N87-20798 

Evaluation of installed performance of a 

wing-tipmarnted pusher turboprop on a semispan wing 

[ NASA-TP-27391 p6 N87-26041 

Flight imregtigation of the effect of tail configuration on stall, spin, and recovery characteristics of a law-wing 

gem1 aviation rewarch airplane 

[NASA-TP-2644] p6 N87-16815 

Flight investigation of the effects of an outboard 

wingleadingedoe modition on stalllspin 

characteristics of a low-wing. si~ine. T-tail lit 

airplane 

[ NASA-TP-26911 p6 N87-23614 

PAVU, ALBERT J. 

Expehwntal thrust performance of a high-area-ratio 

rocket nozzle 

[ NASA-TP-27201 p10 N87-20381 

Comparison of theoretical and experimental thrust 

performance of a 1030:t area ratio rocket nozzle at a 

chamber presswe of 2413 kNlm2 (350 paia) 

[NASA-TP-2725] p 11 N87-25423 

Expedmmlal evaluath of heat transfer on a 1OW.1 

area ratio &et nozzle 

[ NASA-TP-27281 p 11 N87-25424 

Traveling-wave-tube efficiency improvement by a 

low-coal temnique for deposition of carbon on multistage 

depressed collector 

[ NASA-TP-27191 

PENARANDA, F. E. 

PARK, STEPHEN K. 

PARKINSON, CLAIRE L 

PARROTT. TONY L 

PAlTERSON. JAMES C., JR. 

PATTON, JAMES Y, JR. 

PEET. SHELLY 

p 14 N87-21239 

Aemnruticlll hcilib;es assessment 

[NASA-RP-t148] p8 N87-10876 

An expa&mW investigation of an advanced tutbprop 

btablbn on a mept wing at subsonic and transonic 

~-TP-2729] p4 N87-26883 

Effect of Reynolds number variation on aerodynamics 

of a hydrogen-tueled transport concept at Mach 6 

[NASA-TP-2728] p4 N87-28031 

New memods and results for quantification of 

lightning-aircraft -a, 

[NASA-TP-2737] p3 N87-21871 

Electron stimulated dewrption of atomic oxygen from 

silver 

[NASA-TP-28681 p 12 N87-18629 

Penneation of oxygen thrweh hgh PUW. krge grain 

silver 

[NASA-TP-2755] p 12 N87-27024 

Piloted simulator study of allowable time delays in 

large-airplane response 

PENDERQRAFT. ODlS C, JR. 

PENLAND, JIM A. 

PERALA, RODNEY A. 

PEREQOY, W. K. 

PERSON, LEE H, JR. 

[NASA-TP-26521 p8 N87-16849 

PICKElT, H. Y. 

Atlas of absorption liw from 0 to 17900 cm (sup)-1 

[NASA-RP-11881 p 19 N87-28955 

Supemtic. nonlinear. attached-flow wing design for 

[ NASA-TP-23361 pt N87-10042 

liightning-ahafl electrodynamics 

PITIYAN, J. L 

Mgh li with experimentlll Validation 

Pm FEUX L New mahods and resub for quantification Of 

[NASA-TP-2737 I p3 N87-21871 

POLAND, ARTHUR 1. 

[ NASA-CP-24421 

Coronal and Prominence Plasmas 

p26 N87-20871 

Modeling digital control systems with MApretiHered 

measurements 

[ NASA-TP-27321 p13 N87-22870 

A new epproach to slate estimation in deterministic 

digital mbd systems 

Exact state reconsmction in deterministic digllal control 

systems 

[ NASA-TP-27571 p13 N87-27067 

POLITE& MICHAEL E. 

[ NASA-TP-27451 p13 N87-24585 

ROTHYAN. L. S. 

PORTER, F. 

NASAIMSFC FY-85 Atmospheric Processes Research 

Review 

[NASA-CP-2402] p20 N87-13043 

Pulse code Modulation (PCM) enwdef handbook for 

Aydin Vector MMP-600 series system 

[NASA-RP-1171] p 13 N87-11916 

Surface bidirectional reflectance properties of huo 

southwestern Arizona deserts for wavelengths between 

0.4 and 2.2 miaOmeterS 

[ NASA-TP-26431 p 18 N87-22281 

POWELL, W. R. 

PURQOLD, G. CARLTON 

Q 

WlNN. ROBERT D. 

Finite-element reentry heat-transfer analysis of space 

shuttle Orbiter 

[ NASA-TP-28571 pt6 N67-29795 

auimo, P. FRANK 

Low-speed aerodynamic characteristics of a hvin-engine 

aeneral aviation configuration with aft-fuselacremounted 

pusher propellers - [NASA-TP-27631 p5 N87-29462 

R 

RAHE. JUERQEN 

Atlas of Comet Halley 1910 II 

[NASASP488] p26 N87-30235 

RAYATY, REUVEN 

[ NASACP-24641 

Essays in Space Sdence 

p 25 N87-24247 

Perfwmance of textured carbon on copper electrode 

multistage depressed collectors with medium-power 

traveling wave tubes 

Design. fakicstion and pmformance of small. grclphie 

electmde. mullistage depressed collectors with 200-W. 

CW. E to 1EGHz traveling-wave tubes 

[NASA-TP-26931 p14 N87-20474 

Traveling-wave-tube efficiency improvement by a 

lw~t techniaue for deWsition of carbon on multist.ee 

RAYINS, PETER 

[ NASA-TP-28851 pt4 N87-17880 

depressed colbitor 

INASA-TP-27191 D 14 N87-21239 

Analybcalande~mentalperformancsofadual-mode 

traveling wave tube and multistage depressed colleclor 

[NASA-TP-27521 p 14 N87-25532 

Analysis of quasi-hybrid solid rocket booster concepts 

lor advanced earlh-toorM vehlcles 

[NASA-TP-27511 p 11 N87-25425 

Evolution, calibration. and operational chamcteristice of 

me two-dimensional twt section Of me Langley 0.3-mer 

transonic cryopnic tunnel 

[ NASA-TP-27491 p9 N87-28570 

Description of data on the Nimbus 7 LlMS map archive 

[NASA-TP-Z625] p 19 N87-13022 

RAPP, DOUOLAS C. 

RAY, EDWARD J. 

REYSBERQ, E. E. 

tape: &One and nitric acid 

REPAS, QEORQE A. conventiwlly cast and forged copper alloy for 

high-heat-flux thrust chambers 

[ NASA-TP-28941 p12 N87-16802 

Effects of aflabody bosttail dwgn and empennage 

arrangement on aeropropulsive characteristics of a 

hviwng~ne fighter model at transonic speed8 

[NASA-TP-P7MI p3 N87-21873 

Static internal performance of a two-dimensional 

conwgmtdvagent nozzle with thrust vectwing 

[NASA-TP-27211 p4 N87-24432 

Propagation of swnd wavesintubesofnonckularcroaa 

sechon 

[NASA-TP-28011 pi? N87-14284 

RICHARDSON. D. J. 

Alias of abrorpbon linea from 0 to 17900 cm (wp)-l 

[NASA-RP-l188] p 19 N87-28955 

RIEBE. QREQORY D. 

Subsonc maneuver capability of a supersonic cnrise 

fighter mng concept 

[ NASA-TP-28421 p2 N87-t5184 

Atlas of absorphon lines from 0 to 17900 cm (sup)-l 

[NASA-RP-11881 p 19 N87-28855 

Atlas of absorphon linea from 0 to 17900 cm (wp)-l 

[NASA-RP-1188] p 19 N87-28955 

REUBUSH. DAVID E. 

RICHARDS, W. B. 

RINSLAND. C. P. 

ROTHYAN, L S 
ROYSTER, DICK M. PERSONAL AUTHOR INDEX 

Flight investigation of the effects of an outboard 

wing-laading-edge modification on stall/spin 

characteristics of a low-wing. single-engine, T-tail light 

airplane 

[ NASA-TP-26911 p 6 N87-23614 

STRAUS, DAVID 

Five year global dataset: NMC qxrational analyses 

[NASA-RP-1194] p21 N87-29996 

Measurements of flow rate and trajectory of aircraft 

tiregenerated water spray 

[NASA-TP-2718] p6 N87-24458 

[NASA-RP-1189] p9 N87-29544 

(1978 to 1982) 

STUBBS, SANDY Y. 

Langley Aircraft Landing Dynamics Facility 

SLCZUR, Y. 

Proceedings of the 51h Annual Users' Conference 

[ NASA-CP-23991 p 22 N87-10720 

SLCZUR, MARTHA 

Sixth Annual Users' Conference 

[NASA-CP-24631 p 22 N67-23156 

ROYSTER. DICK Y. 

Material characterization of superplastically lonned 

titanium (Ti-EAl-2Sn-4Zr-2Mo) sheet 

[ NASA-TP-26741 p 12 N87-20407 

New methods and resuns for quantification of 

lightningaircraft elechodynamics 

[ NASA-TP-27371 p3 N87-21871 

Effects of winglet on transonic flutter characteristics of 

a cantileveced lwin+ngine-transpod wing model 

[ NASA-TP-26271 p 17 N87-13789 

Description of data on the Nimbus 7 LlMS map archive 

tape: Ozone and nitric acid 

[ NASA-TP-26251 p 19 N67-13022 

Sbuctural Dynamics and Control Interaction of Flexible 

Structures 

[NASA-CP-2467-PT-l] p 10 N87-22702 

Structural Dynamics and Control Interaction of Flexible 

Structures 

[NASA-CP-2467-PT-Z] p 10 N67-22729 

RUDOLPH. TERENCE H. 

RUHLIN. C. L 

RUSSELL, J. Y., 111 

RYAN, ROBERT S 

S 

SANZ JOSE Y. 

L&S inverse design code (LINDES): users manual 

INASA-TP-26761 D3 N87-20238 SATRAN. D. R. 

Wind-tunnel investigation of the Riht characteristics of 

a canard general-aviation airplane configuration 

[NASA-TP-2623] p1 N87-10039 

An algorithm for surface smoothing with rational 

splines 

[ NASA-TP-27081 pa N87-22447 

Preliminary estimates of radiosonde thermistor errors 

[ NASA-TP-26371 p 20 N87-12086 

SCHIESS, JAMES R. 

SCHYIWN, F. J. 

SCHYITZ, MARION 

Infrared Swrce cross-index. first ediion 

[ NASA-RP-11821 p 25 N87-22573 

SCHOCK, R. W. 

Solar array fliht dynamic experiment 

[ NASA-TP-25981 p9 N87-12581 

Structural Dynamics and Control Interaction of Flexible 

Structures 

[ NASACP-2467-PT-11 p 10 N87-22702 

Sbuctural Dynamics and Control Interaction of Flexible 

Structures 

[ NASACP-2467-PT-21 p 10 N87-22729 

BR-enor-rate testing of hgh-power 3ffiHz traveling 

wave tubes for ground-terminal applications 

[NASA-TP-2635] p 13 N87-17971 

SHORT, NICHOLAS Y. 

Geomorphology from space: A global overview of 

regmal landforms 

[ NASASP-4861 p 18 N87-18139 

Lar~scale static investigation of 

cirwlationumtrd-wing concepts applii to upper 

aurface-blowing aircraft 

[ NASA-TP-26941 p6 N87-15959 

Expeimental evaluation of two turning vane designs for 

fan drive mer of 0.1-scale model of NASA Lewis 

Research Center's proposed allit& wind tunnel 

[ NASA-TP-26461 p8 N87-18576 

Detailed Raw surveys of turning vanes designad for a 

0.1-scale model of NASA Lewis Research Center's 

proposed ahde wind tunnel 

[NASA-TP-ZWO] p9 N87-20295 

Quelitative evaluation of a flush air data system at 

transonic speeds and huh angles of attack 

[ NASA-TP-27161 p6 N87-29497 

In-flight total forces, moments and stak aerodastic 

IICOFIELD, HAROLD N. 

SHALKHAUSER, KURT A. 

SHOVUN, Y. D. 

SHYNE, RICKEY J. 

SEVERS, PAUL Y, 111 

SIN, A. 0. 

charactefislics of an obliquewing research airplane 

[ NASA-TP-22241 P8 N87-10103 

Flightdetenninad aerodynamic derivatives of the AD1 

-wing research airp&ne 

[ NASA-TP-22221 p8 N87-10871 

Fliiht characteristics of the AD1 obliquewing research 

aircraft 

[ NASA-TP-22nI p 8 N87-18570 

Jet model for slot film cooling with effect of free-streem 

andccolanttukrlence 

[ NASA-TP-26551 p15 N87-18034 

SIN, ALEX Q. 

SIMON, FREDERICK F. 

SINQH, J. J. 

Investigation of the effects of cobalt ions on epoxy 

properties 

[NASA-TP-2639] p 12 N87-12680 

SINQH, JAG J. 

A simplified method for determining heat of combustion 

of natural gas 

[NASA-TP-2682] p 16 N87-20514 

Fliiht investigation of the effect of tail configuration on 

stall, spin, and recovery characteristics of a low-wing 

general aviation research airplane 

SLIWA, STEVEN Y. 

[ NASA-TP-26441 p6 N67-16815 

SMITH, Q. LOUIS 

Atlas of wide-field-of-view outgoing longwave radiation 

derived from Nimbus 6 Earth radiation budget data set. 

July 1975 to June 1978 

[NASA-RP-1185] p21 N87-26489 

Effects of variables upon pyotechnically induced shock 

response spectra 

[ NASA-TP-26031 p17 N87-12921 

Piloted simulator study of allowable he delays in 

largeairplane response 

[ NASA-TP-26521 p8 N87-16849 

Upper and Middle Atmospheric Density Modeling 

Requirements for Spacecraft Design and Operations 

[ NASA-CP-24601 p20 N87-20685 

Summary of studies to reduce wingmounted propfan 

installation drag on an M = 0.8 transport 

[NASA-TP-2678] p6 N87-20990 

Experimental thNSt performance of a high-area-ratio 

rocket nozzle 

[ NASA-TP-27201 p 10 N87-20381 

Comparison of theoretical and experimental thrust 

performance of a 10301 area ratio rocket nozzle at a 

chamber pressure of 2413 kN/mP (350 psia) 

[NASA-TP-2725] p 11 N87-25423 

Expenmental evaluation of heat transfer on a 10301 

area ratio rocket noale 

[ NASA-TP-27261 p 11 N87-25424 

Liquid drop stabili for protein ccystal growth in 

[ NASA-TP-27241 p21 N87-20727 

Recent Experiences in Multidisciplinary Analysls and 

Optimization. part 1 

[ NASA-CP-2327-PT-11 p5 N87-11717 

Recent Expenences in Multidisciplinary Analysis and 

Optimization. part 2 

[NASA-CP-2327-PT-Z] p 6 N87-11750 

Simpli curve fib for the thermodynamic properties 

of equilibrium air 

[NASA-RP-l181] p 15 N87-26309 

Expenmental cavity pressure distributions at supersonic 

p3 N87-22626 

Cosmic ray heavy ion LET mapping for aluminum, silicon. 

and tissue targets 

[NASA-RP-llEO] p27 N87-25984 

STEINKE, RONALD J. 

Deaign of 9.271-pressure-ratio 5-stage me compressor 

[NASA-TP-2597] p 7 N87-17699 

Development and evaluation of an airplane electronic 

display fonnat aliened with the inertial velodtyvactor 

[NASA-TP-2648] p 7 N87-13438 

System study of the carbon dioxide observational 

platform system (CO-OPS): Project overview 

[NASA-TP-2696] p9 N87-18588 

piloted simulation study of me effects of an automated 

trim system on fliht characteristics of a liiht lwin-engine 

airplane with one engine inoperative 

[NASA-TP-2633] p2 N87-10843 

Investigation of the effects of cobalt ions on epoxy 

properties 

[NASA-TP-2839] p 12 N87-12680 

Fliht investigation of the effect of tail configuration on stall, spin, and recovery characteristics of a low-wing 

general aviation research airplane 

[NASA-TP-26441 p6 N87-16815 

SMITH, J. L 

SMITH, PAUL Y. 

SMITH, R. E. 

SMITH, RONALD C. 

SMITH, TAMARA A. 

SNYDER, ROBERT S. 

nlicrogravity 

SOBIESKI, J. 

SRINIVASAN, S. 

STALUNGS, ROBERT L, JR. 

speeds 

[ NASA-TP-26831 

STASSlNopouLOS, E. 0. 

and overell performance for first 3 stages 

STEINUE'VZ, Q. 0. 

STEPHENS, J. BRlSCOE 

STEWART, E. C. 

STOAKLEY, D. Y. 

STOUGH. H. PAUL, 111 

T 

TANNEHILL, J. C. 

Simplied curve fits for the thermodynamic properties 

of equilibrium air 

[NASA-RP-1181] p 15 N87-26309 

TANNER, JOHN A. Exploiting symmetries in the modeling and analysis of 

tires 

[ NASA-TP-26491 p6 N87-17690 

[NASA-RP-l189] p9 N87-29544 

Langley Aircraft Landing Dynamics Facility 

THEON, JOHN S. 

Spacelab 3 Mission Science Review 

[NASA-CP-2429] p 15 N87-22103 

On requirements for a satellite mission to measure 

tropical rainfall 

[NASA-RP-l183] p20 N87-20701 

The 1986 Get Away Special Experimenter's 

Symposium 

[ NASA-CP-24381 p9 N87-20302 

System study of the carbon dioxide observational 

platform system (CO-OPS): Project overview 

[ NASA-TP-26961 p9 N87-18588 

Piloted simulator study of allowable time delays in 

large-airplane response 

[ NASA-TP-26521 p8 N87-16849 

TOMPKINS, S. S. 

Effects of thermal cycling on graphie-fiber-reinforced 

6061 aluminum 

[ NASA-TP-26121 pll N87-10184 

Space station structures and dynamics test program 

THIELE, OTTO w. 

THOMAS, LAWRENCE R. 

THOMPSON, WILBUR E. 

TINQAS, STEPHEN A. 

TOWNSEND, JOHN S. 

[NASA-TP-2710] p 18 N67-20568 

TOWNSEND, LAWRENCE W. 

Doubly difterential cross sections for galactic heavy-ion 

fragmentation 

[NASA-TP-2659] p 24 N67-17487 

Poasibk complementary wsmic-ray systems: Nuclei 

and antinuclei 

[NASA-TP-2741] p 24 N87-24977 

TRAVIS, LARRY D. 

The Jovian Atmospheres 

[NASACP-2441] p 26 N87-17598 

Automated Reduction of Data from Images and 

[ NASACP-24771 p5 N87-29432 

TRWNQER, JAMES D. 

nolograms 

V 

VAUQHAN. OTHA H. 

Spacelab 3 Mission Science Review 

[ NASA-CP-2429 I p 15 N87-22103 

NASA/MSFC FY-85 Atmospheric Pr-sSeS Research 

Review 

[ NASACP-2402 I p20 N87-13043 

Aoalog , signal conditioning for Riht-test 

insbumenlabon 

[NASA-RP-1159] p7 N87-29533 

VAUQHAN. W. W. 

VEATCH. DONALD W. 
PERSONAL AUTHOR INDEX ZWALLY, H. JAY 

W 

WALTERS, R. W. 

Some path-following techniques for solution of nonlinear 

equations and comparison with parametric differentiation 

[ NASA-TP-26541 p22 N87-14054 

Efficient solutions to the Euler equations for supersonic 

flow with embedded subsonic regions 

[ NASA-TP-25231 p2 N87-15183 

Application of turbulence rodeling to predii surface 

heat transfer in stagnation flow region of circular cylinder 

[NASA-TP-2758] p 15 N87-27161 

Study of lee-side flows over conically cambered delta 

wings at supersonic speeds, part 1 

[ NASA-TP-2660-PT-11 p4 N87-23597 

Study of lee-side flows over conically cambered Delta 

wings at supersonic speeds. pati 2 [ NASA-TP-2660-PT-21 p4 N87-25301 

Eqmimental validation of a twudimensicmal shear-flow 

model fw determining acoustic impedance 

[ NASA-TP-26791 p23 N87-20798 

Calculation and accuracy of ERBE scanner 

measurement locations 

[ NASA-TP-26701 p25 N87-28471 

Simpli curve fits for the thermodynamic propertiis 

of equilibrium air 

[NASA-RP-l181] p 15 N87-26309 

Jet transport fliht operations using cockpit display of 

traffic information during instrument meteorological 

condiis: Simulation evaluation 

[NASA-TP-2567] p5 N87-29469 

Surface bidirectional reflectance properties of two southwestern Arizona deserts for wavelengths between 

0.4 and 2.2 micrometers 

[ NASA-TP-2643 ] p 18 N87-22281 

WHMORE. STEPHEN A. Qualitative evaluation of a flush air data system at 

transonic speeds and huh angles of attack 

[NASA-TP-2716] p6 N87-29497 

Emerimental cavitv oressure distributions at sweraonic 

WALTERS. ROBERT W. 

WAMG, CHI R. 

WATSON, CAROLYN 8. 

WATSON, WILLIE R. 

WEAVER. WILLIAM L 

WEILYUENSTER. K. J. 

WELLS, DOUGLAS C. 

WHITLOCK, CHARLES H. 

WILMX, FLOYD J, JR. 

_. 

e-TP-26831 p3 N87-22626 

Drag measurements of Munt stores tanoentinllv mounted -. on a Rat plate at supersonic speeds 

[ NASA-TP-27421 p5 N87-27626 

ClosedGycle. Frequency-Stable C02 Laser 

Technology 

[NASACP-2456] p 16 N87-20522 

WILLETTS, DAVID V. 

WILLIAMS, ALTON C. 

Double Layers in Astrophysics 

[ NASACP-2469 ] p 25 N87-23313 

Jet transport fliht operations using cockpi display of 

traffic information during instrument meteorological 

conditions: Simulation evaluation 

[ NASA-TP-25871 p5 N87-29469 

Effects of background noise on total noise annoyance 

[ NASA-TP-26301 p 23 N87-14120 

WILMOTH, RICHARD Q. 

Multiscale turbulence effects in supersonic @ts 

exhausting into still air 

[NASA-TP-2707] p 15 N87-24672 

WILLIAMS, DAVID H. 

WILLSHIRE, K. F. 

WILSON. JEFFREY D. 

Revised NASA axially symmetric ring model for 

coup(edcavity traveling-wave tubes 

[ NASA-TP-26751 p 14 N87-22923 

WILSON, JOHN W. 

Possible complementary cosmic-ray systems: Nudei 

and antinuclei 

[ NASA-TP-27411 p 24 N87-24977 

WILSON. ROBERT Y. 

Statistical aspects of solar flares 

[ NASA-TP-27141 p27 N87-20947 

WINDMILLER, MARY JO 

Unique bit-error-rate measurement system for satellite 

communication systems 

[NASA-TP-2699] p 13 N87-20448 

WISLICENUS, QEOROE F. 

Preliminary dwgn of turbopumps and related 

[NASA-RP-1170] p 2 N87-17665 

ClosebCycle, Frequency-Stable CO2 Laser 

Technology 

[NASACP-2456] p16 N87-20522 

machinery 

WOOD, OEORQE Y, JR. 

WOOD, RICHARD D. 

Summary of studies to reduce wing-mounted propfan 

installation drag on an M = 0.8 transport 

[NASA-TP-2678] p6 N87-20990 

Investigation of leading-&@ flap performance on delta 

and doubledelta wings at supersonic speeds 

[ NASA-TP-26561 p 3 N87-20233 

Study of lee-side flows over conically cambered delta 

wings at supersonic speeds, part 1 

[ NASA-TP-2660-PT-11 p4 N87-23597 

Study of leeside Ram over conically cambered Delta 

wims at supersonic speeds, wrt 2 

WOOD, RICHARD Y. 

[N&A-TP-%O-PT-Z] ' p 4 N87-25301 

WOODOATE. BRUCE 

Energetic Phenomena on the Sun: The Solar Maximum 

Mission Flare Workshop. Proceedings 

[ NASA-CP-24391 p26 N87-19328 

NASAlDOD ControllStruchrres Interaction Technology, 

1988 

[NASA-CP-2447-PT-l] p10 N87-16014 

NASAlDOD ControllStructures Interaction Technology, 

1986 

[ NASA-CP-2447-PT-21 p 10 N87-24495 

Piloted-simulabn study of effects of vortex flaps on 

low-speed handling qualibs of a Delta-wing airplane 

[ NASA-TP-27471 p8 N87-26922 

WRIQHT, ROBERT L 

WUNSCHEL ALFRED J. 

Y 

YEE, HELEN 

Superccinprting in Aerospace 

[NASACP-2454] p4 N87-25998 

Application of turbulence modeling to predii surface 

heat transfer in stagnation Row region of circular cylinder 

[NASA-TP-2758] p 15 N87-27161 

piloted simulation study of the effects of an automated 

trim system on fliht characteristics of a light twin-engine 

airplane with one engine inoperative 

[NASA-TP-2633] p2 N87-10843 

Wind-tunnel free-flight investigation of a 0.15-scale 

model of the F-108B airplane with vortex flaps 

[NASA-TP-2700] p3 N87-21855 

Calibration of the spin-scan ozone imager aboard the 

dynamics Explorer 1 satellite 

[ NASA-TP-27231 p 21 N87-26491 

Solar array flit experimentldynamic augmentation 

expefiment 

[NASA-TP-2690] p 10 N87-20380 

~utomated Reduction of Data from Images and 

Holograms 

[NASACP-2477] p5 N87-29432 

YEH, FREDERICK C. 

YENNI. K. R. 

YIP, LONG P. 

YOUNQ, DAVID F. 

YOUNQ. L" E. 

YU, Y. H. 

z 

UNQ, THOMAS A. 

Numerical simulation of channel flow transition, 

resolution requirements and structure of the hairpin 

vortex 

[ NASA-TP-26671 p3 N87-19351 

Analysis of quasi-hybnd soli rocket booster concepts 

for advanced earth-toetA vehicles 

[NASA-TP-2751 I p 11 N87-25425 

ZWALLY, H. JAY 

Arctic Sea ice, 1973-1976 Satellite passive-microwave 

observations 

[NASA-SP-489] p21 N87-24870 

LURAWSKI, ROBERT L 

B-7 
REPORT NUMBER INDEX 

NASA Scientific and Technical Publications 1987 

Typical Report Number 

Index Listing 

NASA.RP-1171 ............................... p 13 N87-11818 

T-lListings in this index are arranged alphanumerically by report number.The page number indicates 

the page on which the citation is located . The 

accession number denotes the number by which 

the citation is identified . 

NASACP-2327-PT-1 ..................... p 5 

N ASACP-2327-PT-2 .......... N A SA C P -2339 .................... NASA-CP-2399 ............................... p 22 

NASACP-2402 ............................... p 20 

NASACP-2423-REV ............. NASACP-2429 ...................... NASA-CP-2431 ...................... NASACP-2433 ...................... NASA-CP-2434 ............................... p 14 

NASA-CP-2435 ............................... p 5 

NASACP-2438 ............................... p 9 

NASACP-2442 ............................... p 26 

NASACP-2443 ............................... p 17 

NASACP-2447-PT-1 ..................... p 10 

NASACP-2447-PT-2 ..................... p 10 

NASACP-2448 ............................... p 18 

NASACP-2449 ............................... p 27 

NASA-- 2450 ............................... p 20 

NASACP-2451 ............................... p 1 

P26 

NASACP-2441 P26 ............................... 

NASACP-2454 ............................... p 4 

NASACP-2455 ............................... p 5 

NASACP-2456 ............................... p 18 

NASA--245940 L-2 

NASACP-2482 ............................... p 4 

NASACP-2463 ............................... p 22 

NASA-- 2465 ............................... p 13 

P26 

P 10 

P 10 

NASACP-2468 P 21 NASA-- 2489 ............................... p 25 

NASACP-2470 ............................... D 18 

P 25 

.......... 

N87-11717 

N87-11750 

N87-11180 

N87-10720 

N87-13043 

N87-16321 

N87-22103 

N87-10263 

N87-20267 

N87-11072 

N87-10054 

N87-20302 

N87-19328 

N87-17598 

N87-20871 

N87-22199 

N87-16014 

N87-24495 

N87-15528 

N87-21785 

N87-18248 

N87-18520 

N87-22604 

N87-27596 

N87-25998 

N87-22834 

N87-20522 

N87-18855 

N87-18821 

N87-19931 

N87-19932 

N87-20885 

N87-24410 

N87-23156 

N87-24247 

N87-21141 

N87-24266 

N87-22702 

N87-22729 

N87-22341 

N87-23313 

N87-29858 

NASA-. 2471 ............................... p 11 N87-22766 

NASACP-2472 ............................... 0 17 N87-27204 

NASA-. 2474 ............................... p 1 

P 19 

NASACP-2477 ..................... P5 

NASA-- 2478 ............................... p 22 

NASA-RP-1148 ............................... p 8 

“IP-1170 ............................... p 2 

N87-25287 

N87-28413 

N87-29432 

N87-26531 

N87-27231 

N87-29814 

N87-10876 

N87-29533 

N87-29488 

N87-17665 

NASA-RP-1171 ............................... p 13 

NASA-RP-1172 

NASA-RP-1 175 ............................... p 20 

NASA-RP-1176 .......... P 25 

NASA-RP-1177 P 11 NASA-RP-117EREV ...................... p 26 

NASA-RP-1180 ............................... p 27 

NASA-RP-1 181 ............................... p 15 

NASA-RP-1 182 ............................... p 25 

.......... 

NASA-RP-1183 ............................... p 20 

NASA-RP-1185 ............................... p 21 

NASA-RP-1189 ............................... p 9 

NASA-RP-1194 ............................... p 21 

NASASP4305 ............................... p 27 

NASA-SPW ................................. p 26 

NASA-SP-486 ................................. p 18 

NASA-SP-488 ................................. p 26 

NASA-SP-489 ................................. p 21 

NASA-SP-7011(293) ...................... p 21 

NASA-RP-1188 ............................... p 19 

NASA-SP-7038(04) ........................ p 25 

NASA-SP-7039(31)-SECT-2 .......... p 24 

NASA-SP-7039(31) ........................ p 24 

NASA-SP-7046(17) ........................ p 9 

NASASP-7058(04) ........................ p 10 

NASA-SP-7041(54) ........................ p 18 

NASA-SP-7053(SUPP-3) ............... p 25 

P 25 

P 24 

NASA-TP-1848 ............................... p 15 

NASA-TP-1849 P 15 

NASA-TP-1850 P 15 

NASA-TP-2222 P8 

NASA-TP-2336 . ............ Pl 

NASA-TP-2350 . ............ Pa 

NASA-TP-2352 . ............ Pl 

NASA-TP-2223 ............................... p 8 

NASA-TP-2224 ............................... p 8 

NASA-TP-2364 ............................... p 2 

NASA-TP-2375-PT-2 ...................... p 2 

NASA-TP-2384 ............................... p 18 

NASA-TP-2392 ............................... p 8 

NASA-TP-2395 ............................... p 3 

NASA-TP-2401 ............................... p 3 

NASA-TP-2418 ............................... p 3 

NASA-TP-2523 ............................... p 2 

NASA-TP-2530 ... 

NASA-TP-2588 ............................... p 23 

NASA-TP-2593 ............................... p 18 

NASA-TP-2596 ............................... p 15 

NASA-TP-2587 ............................... p 7 

NASA-TP-2598 ............................... p 9 

NASA-TP-2807 ............................... p 10 

NASA-TP-2610 ............................... p 16 

NASA-TP-2611 

NASA-TP-2612 

NASA-TP-2841 ............................... p 15 

N87-11918 

N87-11358 

N87-17417 

N87-20683 

N87-14219 

N87-29812 

N87-25906 

N87-25984 

N87-26309 

N87-22573 

N87-20701 

N87-26489 

N87-28955 

N87-29544 

N87-29996 

N87-24390 

N87-19322 

N87-18139 

N87-30235 

N87-24870 

N87-18978 

N87-30041 

N87-27613 

N87-70425 

N87-26669 

N87-25023 

N87-27315 

N87-29578 

N87-27557 

N87-28073 

N87-30218 

N87-20833 

N87-23921 

N87-24839 

N87-23938 

N87-10871 

N87-18570 

N87-10103 

N87-10042 

N87-10870 

N87-10838 

N87-10839 

N87-10841 

N87-29778 

N87-17893 

N87-20966 

N87-17668 

N87-17689 

N87-15183 

N87-14918 

N87-29489 

N87-11883 

N87-17479 

N87-13731 

N87-16035 

N87-17899 

N87-12581 

N87-14284 

N87-12921 

N87-12585 

N87- 18095 

N87-18666 

N87-10184 

N87-18783 

N87-10864 

N87-10784 

N87-10038 

N87-12541 

N87-13022 

N87-10391 

N87-13789 

N87-11702 

N87-12718 

N8Z-1 41 20 N87-13864 

N87-13284 

N87-10043 

N87-17871 

N87-12080 

N87-12880 

N87-18782 

NASA-TP-2642 ............................... p 2 

NASA-TP-2843 ............................... p 18 

NASA-TP-2644 ............................... p 8 

NASA-TP-2849 ............................... p 8 

NASA-TP-2652 .......... P8 

NASA-TP-2653 ............................... p 2 

NASA-TP-2654 ............................... p 22 

NASA-TP-2655 .......... ...... p15 

NASA-TP-2858 .......... ...... p3 

NASA-TP-2657 .......... ...... p16 

NASA-T P -2659 .......... ...... p24 

NASA-TP-2860-PT-1 . ...... p4 

NASA-TP-2860-PT-2 . ...... p4 

NASA-T P -2650 .......... P 23 

NASA-TP-2658 ............................... p 3 

NASA-TP-2881 ............................... p 18 

NASA-TP-2663 ............................... p 11 

P 14 

P 14 

P8 

NASA-TP-2667 ............................... p 3 

NASA-TP-2668 ............................... p 12 

P7 

NASA-TP-2671 ............................... p 13 

NASA-TP-2672 ............................... p 22 

NASA-TP-2674 .................... NASA-T P -2675 .................... NASA-TP-2676 .................... 

NASA-TP-2678 ............................... p 8 

NASA-TP-2679 ............................... p 23 

NASA-TP-2880 ............................... p 9 

NASA-TP-2882 ............................... p 18 

NASA-TP-2883 ............................... p 3 

NASA-TP-2884 ............................... p 8 

NASA-TP-2885 ............................... p 14 

NASA-TP-2088 ............................... p 23 

NASA-TP-2889 ......... 

NASA-TP-2691 ...................... NASA-TP-2692 ............................... p 9 

NASA-TP-2693 ............................... p 14 

P 25 

NASA-TP-2677 ............................... P 12 

P 12 

P9 

P 17 NASA-TP-2899 ............................... p 13 

NASA-TP-2700 ............................... p 3 

NASA-TP-2702 

NASA-TP-2708 ............................... p 3 

NASA-TP-2707 ............................... p 15 

NASA-TP-2710 ............................... p 18 

NASA-TP-2711 ............................... p 18 

NASA-TP-2712 

NASA-TP-2708 ......... P 23 

NASA-TP-2708 Pa ......... 

NASA-TP-2715 ............................... p 12 

NASA-TP-2718 ............................... p 8 

NASA-TP-2717 P4 

NASA-TP-2718 P8 

P 14 NASA-TP-2720 ............................... p 10 

NASA-TP-2721 ............................... p 4 

NASA-TP-2722 Pa 

NASA-TP-2723 P 21 NASA-TP-2724 ............................... p 21 

NASA-TP-2725 ............................... p 11 

NASA-TP-2728 

NASA-TP-2728 ............................... p 4 

NASA-TP-2730 ............................... p 11 

NASA-TP-2731 ........ . P5 

NASA-TP-2732 ........ . p13 

NASA-TP-2733 ............................... p 4 

NASA-TP-2735 ............................... p 18 

N87-15184 

N87-22281 

N87-16815 

N87-14998 

N87-18578 

N87-13438 

N87-17890 

N87-18399 

N87-16849 

N87-15174 

N87-14054 

N87-18034 

N87-20233 

N87-29795 

N87-18537 

N87-17487 

N87-23597 

N87-25301 

N87-20587 

N87-18611 

N87-17991 

N87-17990 

N87-17717 

N87-19351 

N87-18629 

N87-19393 

N87-28471 

N87-20423 ~~~ 

N87-23202 

N87.20407 

N87-22923 

N87-20238 

N87-18844 

N87-20990 

N87-20798 

N87-20295 

N87-20514 

N87-22626 

N87-15959 

N87-17000 

N87-22441 

N87.24181 

N87-20380 

N87-23814 

N87-23882 

N87-20474 

N87-18902 

N87-18588 

N87-22235 

N87-2ouB 

N87-21855 

N87-22894 

N87-21873 

N87-20555 

N87-23588 

N87-24872 

N87-22447 

N87-23244 

N87-20588 

N87-20588 

N87-24433 

N87-27843 

N87-20947 

N87-21078 

N87-29497 

N87-23593 

N87-24458 

N87-21239 

N87-20381 

N87-24432 

N87-28387 

N87-26481 

N87-20727 

N87-25423 

N87-25424 

N87-28874 

N87-28031 

N87-28883 

N87-25435 

N87-27822 

N87-22870 

N87-23592 

N87-27894 

c-1 
NASA-TP-2736 

NASA-TP-2736 ............................... p 4 

NASA-TP-2737 P3 ................, NASA-TP-2738 ............................... p 17 

NASA-TP-2739 ............................... p 6 

NASA-TP-2740 _.__._. . __ ..... p8 

NASA-TP-2741 .__.__._._ ...._ p24 

NASA-TP-2742 ................................ p 5 

NASA-TP-2743 ................................ p 13 

NASA-TP-2744 ._____ NASA-TP-2745 .___._ NASA-TP-2746 _._.__ 

NASA-TP-2758 ............................... p 15 

NASA-TP-2759 ................................ p 23 

REPORT NUMBER INDEX 

N87-26032 

N87-21871 

N87-28025 

N87-26041 

N87-25331 

N87-24977 

N87-27626 

N87-24590 

N87-25463 

N87-24585 

N87-24481 

N87-26922 

N87-25425 

N87-25532 

N87-27024 

N87-28162 

N87-27067 

N87-27161 

N87-27474 

N87-29462 

NW-28570 

c-2 
I. ReportNo. 

NASA SP-7063(02) 

10. Work Unit No. 

3. Performing Organization Name and Address 

2. Government Accession No. 3. Recipient's Catalog No. 

Office of Management 

Scientific and Technical Information Division 

National Aeronautics and Space Administration 

Washington, DC 20546 

12. Sponsoring Agency Name and Address 

National Aeronautics and Space Administration 

Washington, DC 20546 

1. Title and Subtitle 

NASA Scientific and Technical Publications: A Catalog 

of Special Publications, Reference Publications, 

Conference Publications, and Technical Papers, 1987 

7. Author(s) 

11. Contract or Grant No. 

5. Report Date 

6. Performing Organization Code 

March, 1988 

8. Performing Organization Report No. 

13. Type of Report and Period Covered 

1 this page) 

14. Sponsoring Agency Code 

21. No. of Pages 22. Price' 

70 Free 

15. Supplementary Notes 

19. Security Classif. (of this report) 

Unclassified 

16. Abstract 

This catalog lists 239 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 accession year 1987. The entries are grouped by subject category. Indexes of subject terms, 

personal authors, and NASA report numbers are provided. 

20. Security Classif. 

Unclassified 

17. Key Words (Suggested by Authors(s)) 

Catalogs (Publications) 

18. Distribution Statement 

Unclassified - Unlimited 

Subject Category 82 

I 

Available from the National Technical Information Service, 

Springfield, Virginia 22161 as PR 828. NASA-Langley, 1988