NASASP-7037(92)
A CUMULATIVE INDEX
TO THE 1977 ISSUES OF
AERONAUTICAL
ENGINEERING
A SPECIAL BIBLIOGRAPHY
JANUARY 1978
<■
NATIONAL AERONAUTICS AND SPACE ADMINISTRATION
SUPPLEMENTS COVERED IN THIS INDEX
Page
|
Document |
Range |
Dale |
Coverage |
|
NASA SP-7037(80) |
1-41 |
February 1977 |
January 1977 |
|
NASA SP-7037(81) |
43-87 |
March 1977 |
February 1977 |
|
NASA SP-7037(82) |
89-133 |
April 1977 |
March 1977 |
|
NASA SP-7037(83) |
135-187 |
May 1977 |
April 1977 |
|
NASA SP-7037(84) |
189-240 |
June 1977 |
May 1977 |
|
NASA SP-7037(85) |
241-293 |
July 1977 |
June 1977 |
|
NASA SP-7037(86) |
295-339 |
August 1977 |
July 1977 |
|
NASA SP-7037(87) |
341-390 |
September 1977 |
August 1977 |
|
NASA SP-7037(88) |
391-440 |
October 1977 |
September 1977 |
|
NASA SP-7037(89) |
441-497 |
November 1977 |
October 1977 |
|
NASA SP-7037(90) |
499-547 |
December 1977 |
November 1977 |
|
NASA SP-7037(91) |
549-598 |
January 1978 |
December 1977 |
This bibliography was prepared by the NASA Scientific and Technical Information Facility operated for the National Aeronautics and Space Administration by informatics Information Systems Company.
SPECIAL NOTICE
The abstract sections of the monthly supplements oi Aeronautical Engineering can be bound separately Individual abstracts can be located readily by means of the page num- bers given at each entry, eg, p331 N77-23063 To assist the user in binding Supple- ments SP-7037 (80) through SP-7037 (91), a title page is included in the back of this Cumulative Index
NASASP-7037 (92)
A CUMULATIVE INDEX TO
AERONAUTICAL ENGINEERING
A Special Bibliography
This Cumulative Index supersedes the indexes contained in supplements SP-7037 (80) through SP-7037 (91).
Scientific and Technical Infoinialion Offite JANUARY 1978
NATIONAL AERONAUTICS AND SPACE ADMINISTRATION
1 Washington, D C
This Index is available from the National Technical Information Service (NTIS), Springfield, Virginia 22161 for $9 00 domestic, $ 1 8 00 foreign
INTRODUCTION
WHAT THIS CUMULATIVE INDEX IS
This publication is a cumulative index to the abstracts contained in NASA SP-7037(80) through NASA SP-7037(91) oi Aeronautical Engineering A Special Bibliography NASA SP-7037 and Its supplements have been compiled through the cooperative efforts of the American Institute of Aeronautics and Astronautics (AIAA) and the National Aeronautics and Space Administration (NASA) Entries prepared by the two contributing organizations are identified as follows
1 NASA entries by their STAR accession numbers (N77- 10000 series)
2 AIAA entries by their !AA accession numbers (A77- 10000 series)
HOW THIS CUMULATIVE INDEX IS ORGANIZED
This Cumulative Index includes a subject index, a personal author index, a corporate source index, a contract number index, and a report/accession number index
HOW TO USE THE SUBJECT INDEX
Two types of cross-references appear in the subject index
1 Use (U) references indicate that the subject term is not "postable," le, not a valid term, and the following term or terms are used instead For example
AIRCRAFT PROTUBERANCES U PROTUBERANCES
FLIGHT PERFORMANCE
U FLIGHT CHARACTERISTICS
2 Narrower Term (NT) references refer the user to more specific headings in the same subject area, under which additional material on the subject may be found For example
FLOW RESISTANCE
NT AERODYNAMIC DRAG NT FRICTION DRAG NT SUPERSONIC DRAG
In addition, a searcher may use the title or title and title extension in the index to narrow further his quest for particular items This is because subject terms readily include more than one class of document For example
AIRLINE OPERATIONS
All-weather operations, including pilot role, instrument landing systems and guidance aids Airport congestion as constraint on air travel, considering runway capacity and adjusted demand
illustrates a case where two references on different topics are listed under the same subject term
III
HOW TO USE THE PERSONAL AUTHOR INDEX
All personal authors used in the abstract-section citations in the individual Supplements appear in the index Differences in transliteration schemes may require multiple searching of the index for variants of an author's name For example
EMELIANOV. M D and
YEMELYANOV. M D
HOW TO USE THE CORPORATE SOURCE INDEX
The corporate source index entries are abridged versions of the corporate sources used in the abstract-section citations in the individual Supplements The corporate source supplementary (organizational component) does not appear in the index For example
BOEING CO, SEATTLE, WASH MILITARY AIRCRAFT SYSTEMS DIV
(Source citation entry)
BOEING CO, SEATTLE, WASH (Source index entry)
HOW TO USE THE CONTRACT NUMBER INDEX
All contract numbers that are identified in the abstract-section citations in the individual Supplements appear in this index Changes by agencies in the style in which contract numbers are presented may require multiple searching for variants For example
AF 33(615)-71-C-1758 F33615-71-C-1758
HOW TO USE THE REPCRT/ACCESSION NUMBER INDEX
All report numbers that have been assigned by the corporate source, monitoring agency or cataloging activity appear in this index Variations in initial cataloging may result in different report number series For example
TP-924
ONERA-TP-924
IDENTIFICATION OF DESIRED SUPPLEMENT
The abstract and descriptive cataloging for any accession number selected from the indexes may be found in the appropriate Supplement The page-number range of each Supplement appears on the inside front cover of this index Once the range of page numbers containing the selected accession number is located in the second column, the desired Supplement number will be found in the first column For example
Page 331 will be found in Supplement 86
AVAILABILITY OF DOCUMENTS
Information concerning the availability of documents announced in the Aeronautical Engineering supplements is found in the Introduction to the most currently issued monthly supplement
IV
TABLE OF CONTENTS
SUBJECT INDEX A-1
PERSONAL AUTHOR INDEX B-1
CORPORATE SOURCE INDEX C-1
CONTRACT NUMBER INDEX D-1
REPORT/ACCESSION NUMBER INDEX E-1
V
SUBIECT INDEX
AERONAUTICAL ENGINEERING / A Special Bibliography 1977 Cumulative Index
Typical Subject Index Listing
H SUBJECT HEADING I
TITLE
EXTENSION
pi ?-8C adaptive flight ccotcol eztensicos ■axiaaa likelihood estiaation
— for
3
CHASl-CB~28en
P0596 H77-33203
REPORT
NUMBER
PAGE
NUMBER
NASA
ACCESSION
NUMBER
The title is used to provide a description of the subject matter When the title IS insufficiently descriptive of the document content a title extension is added separated from the title by three hyphens The STAR or iAA accession number is included in each entry to assist the user in locating the abstract in the abstract section of an individual issue of Aeronautical Engineering If applicable a report number is also included as an aid in identifying the document The page and accession numbers are located beneath and to the right of the title Under any one subject heading the accession numbers are arranged m sequence with the IAA accession numbers appearing first
A
A-4 AlfiCBAFT
Baseline data from an A*-4 cockpit in sioalated carrier deck fire
CAD-A034217] F0332 N77-23077
Void filler foaa accelerated load testing on an A-4 aircraft
[AD-A034118] p0338 N77-23273
Statistical analyses applied to the OS Navy aircrew automated escape systems
[AD-A035C67] p0381 H77-25129
Statistical analysis of OS Navy major aircraft accident rates, pilot and aircraft time^dependent variables
[AD-A040096] p0525 H77-30099
A-6 AIBCBAFT
AN/APO-IAS mnltimode radar for the A-bl all weather attack aircraft
p0397 A77-37420
Response of A-6 landing gear door to air shock loading
[AD-A035459] p0384 N77-25157
A>7 AIBCBAFT
Fiber optics application to A-7 aircraft
internal data-signal trabsnission system
p0117 A77-19242
Advanced composites manafactoring as inflaenced by design — fcr A-7D aircraft outer wing panel
p0159 A77-22145
Criteria for developing a mnlti-sensor
reconnaissance pod system for carriage on
tactical aircraft onboard A-7 aircraft
p0190 A77-23519
Qualification and in-service evaluation of the A-7D composite outer wing
[AIAA PABER 77-462] p0211 A77-25815
Manufacture of ribs for the a7d composite outer wing
p0359 A77-36700
Fiber optics cost models for the A-7 aircraft
p0359 A77-36972
Design of a digital flight control system using area multiplexing
pC396 A77-37405
A-7 titanium nose gear development
p0513 A77-46801
Accelerated environmental conditioning of the A-7D composite outer wing
p0514 A77-46838
Full temperature range protective system for fastener areas of carrier-based naval aircraft [AD-A024S23] p0026 H77-10210
JANUARY 1978
Inertially derived flying qualities and performance parameters
[AD-A026963] p0080 B77-130b4
Bole of head-up display in instrument flight
[AD-A030075] p0231 H77-18153
Results of A-7 aloft bottoms up model and weight sensitivity analysis
[AD-A033767] p0338 H77-23350
Master monitor display applications study for the A-7E
CAD-A039882] p0528 H77-30118
A-10 AIBCBAFT
Height and balance considerations in the design of the A-10A close air support aircraft [SAHE PAPBB 1104] pOOlO A77-12183
The Fairchild-Republic A-10 fighter
p0200 A77-25099
YA-10 stall/post-stall/spin avoidance flight test program
p0310 A77-33178
Advanced avionics for the A-10: A decision
analysis model
tAD-A027678] p0123 N77-14023
Bole of head-np display in instrument flight
[AD-A030075] p0231 H77-18153
A-37 AIBCBAFT
A-37B fatigue sensor evaluation program: Full
scale test and field aircraft instrumentation CAD-A042114] p0590 H77-33156
A-300 AIBCBAFT
Comparison of fatigue design load spectra with flight test measurement and service experience in A-300 aircraft development
p0048 A77-13772
Gasdynamic investigations of explosive
decompression of one of the cargo bolds of the Airbus A 300
CDGIR PAPBB 76-209] p009i A77-16561
A Wing for the Airbus
p0163 A77-22662
Comparison of applied propulsion jet simulation techniques, using models of the Airbus A 300
[BBB-0FE-1276-0B] p0267 A77-28789
Comparative impact tests on metal honeycomb
sandwich structures of A-300 B airbus
CFOK-B-1843] p0082 N77-13163
ABLATIVE BATBBIALS
Strength of glass-fibre-reinforced plastics at
one-sided beating aircraft ablative thermal
protection coatings
CIAP PAPBB 76-200] pOOOS A77-10939
Evaluation of carbon-carbon composite nosetlp materials
[AD-A033540] p0324 N77-22188
ABLATIVE BOSE COBBS
Thin shell calorimetric techniques for transition detection at ablation temperatures
p0242 A77-26804
Evaluation of carbon-carbon composite nosetlp materials
CAD-A033540] pOJ24 N77-22188
ABOBT APFABATUS
Study of a fail-safe abort system for an actively cooled hypersonic aircraft: Computer program
doc omenta t ion
tBASA-CB-1 44927] p0333 H77-23090
ABSOBPTIOB COSPFICIEBT 0 ABSORPTIVITY ABSOBPTIVB IBDBl 0 ABSOfiPTIVITY ABSOBPTXVITT
Calculation of radiant cooling of air behind intense shock wayes using mean optical characteristics
p0469 A77-43993
&C GEHEB&TOBS
SOBJECT IVDEZ
ZC GEBEBZTOBS
A high-pover rare earth cobalt permanent magnet generator in a variable speed constant fregoency -aircraft starter generator system
p0399 A77-37475
Aircraft electrical pover generation - The needs and practicalities
p0408 A77-38464
Subsystem design analysis light weight alternator (model test program). Addendum 2 [AD-A041257] p0592 H77-33171
ACCELEBATEO LIES TESTS
crack growth in Ti-SAl-lMo-IV with real-time and
accelerated flight-by-flight loading for
supersonic aircraft
p0044 A77-13291
Accelerated mission testing of gas turbine engines [AIAA PAPER 77-992] p0413 A77-38625
Equivalent testing of gas turbine engines
Russian book
p0467 A77-43619
Accelerated environmental conditioning of the A-7D composite outer wing
p0514 A77-46838
void filler foam accelerated load testing on
an A-4 aircraft
[AD-A034118] p0338 N77-23273
Accelerated mission test: A vital reliability tool
p0595 H77-33196
ACCELSRATIOB
Hinimum-time acceleration of aircraft turbofan engines
[HASA-TH-X-73624 ] p0335 K77-23112
ACCEIEBATIOB (PBTSICS)
FT AFGOLAB ACCELERATION FT DECE'lERATIOH FT HIGH ACCELERATION FT SPIN REDOCTIOF
Optimal control of thrust and angle of attack of an aircraft performing a climb-acceleration maneuver
p0135 A77-19329
The calculation of the rns value of an aircraft's normal acceleration due to Gaussian random atmospheric turbulence
[VTH-213] p0079 F77-13046
ACCBLSBOBBTEBS
FT STRAIF GAGE ACCELEROnETERS A damper for accelerometers
p0308 A77-32711
A Schuler tuned vertical indicating system — gyroless gravity vector indicator
[AIAA 77-1066] p0457 A77-42815
Statistical review of counting accelerometer data for Favy and Harine fleet aircraft [AD-A025182] pOOSO N77-13058
Development and tests of a simulator for a
pendulum accelerometer
[LRBA-E-410-FT-32/STE] p0082 F77- 13079
The reduction of base strain sensitivity of a triaxial accelerometer by the use of a mounting
pad measuring vibration signals up to 2 kHz
in aircraft instrument panels
[RAE-TM-IT-157] p0084 F77-13398
Statistical review of counting accelerometer data for Favy and Narine fleet aircraft from 1 January 1962 - 30 June 1976
[AD-A031833] p0282 F77-20096
The development of primary eguations for the use of on-board accelerometers in determining aircraft performance
[AD-A039174] p0527 F77-30112
Statistical review of counting accelerometer data for Favy and Narine fleet aircraft [AD-A041266] p0539 F77-31140
ACCIOEFT IHTESTIGATIOH FT AIRCRAFT ACCIDBFT IFVBSTIGATIOF
The flight recorder and accident investigation
p0237 F77-19035
An accident analysis of fighter aircraft in relation to modificatione introduced and new developments
p0237 F77-19036
ACCIDENT PBBVEFTIOH
Sundstrand maintains lead in GPiS battle - Hark II
system on offer Ground Proximity Warning
Systems
p0250 A77-27027
Basic safety concepts of ait transportation
compared with other travel modes
p0450 A77-41938
General aviation accidents Involving aerobatics,
1972 - 1974
[ PB-257747/6] p0177 F77-17020
The reduction of P-111 low-level enroute bird hazards
[AD-A032879] p0332 F77-2J076
ACCIDBHIS
FT AIRCRAFT ACCIDEFTS FT BIBD-AIBCHAFT COLLISIOFS ACCONDLATZOBS
Oxygen accumulation in hypobaric chambers
[AD-A025860] p0072 B77-1207J
ACCOHOLATOBS FT SOLAB COLLECTORS ACBTTLBRB
Polyphenylquinozallnes with terminal acetylene
gronps for military aircraft construction
materials
pOJ59 A77-36679
ACIDS
FT CARBOXYLIC ACIDS ACOOSTIC ATTBBOATIOF
Survey of inlet noise reduction concepts for gas turbine engines
p0150 A77-20634
Methods of reducing low fregnency cabin noise and sonically induced stresses, based on the intrinsic structural toning concept [AIAA 77-444] p0209 A77-2bb02
Boundary layer considerations for optimization of acoustic liners for aircraft engine ducts [SAB PAPER 760896] p0258 A77-28214
Acoustic shock from an aircraft flying along an arbitrary trajectory in a layered atmosphere with a three-component wind
p0296 A77-30B63
Shielding aspects of heated twin jet noise
[AIAA PAPER 77-1288] p0565 A77-51048
Inlet noise suppressor design method based upon the distribution of acoustic power with mode cutoff ratio
p0026 M77-10311
A research program to reduce interior noise in general aviation airplanes test methods and results
[BASA-CB-155154] p0598 H77-33959
ACOOSTIC COflBUSTIOB 0 COHBDSTIOF STABILITY ACOOSTIC DOCTS
Skin friction on a flat perforated acoustic liner
p0046 A77-13729
A theoretical study of the acoustic Impedance of orifices in the presence of a steady grazing flow
pOlOO A77-17066
Boundary layer considerations for optimization of acoustic liners for aircraft engine ducts [SAE PAPER 760896] p02S8 A77-28214
A finite element algorithm for sound propagation in azisymmetric ducts containing compressible mean flow
[AIAA PAPER 77-1301] p0565 A77-51067
Optimal one-section and two-section circular sound-absorbing duct liners for plane-wave and monopole sources without flow
[HASA-TF-D-8348] p0133 H77-15790
ACOOSTIC BBISSlOB
AS monitoring of rapid crack growth In a
production-size wing fatigue test article
Acoustic Emission
pons A77-186b0
Acoustic emission - Bonltoring fatigue cracks in aircraft structure
p0242 A77-268U2
In-flight crack detection system for the c-135 lower center wing skin
p0242 A77-26B03
Non-destructive testing of electron-beam welds to detect lack of fusion by acoustic emission
p0301 A77-31592
Acoustic emission system for monitoring components and structures in a severe fatigue noise environment
p0310 A77-3299b
Nodal synthesis for combined structural-acoustic systems
p0311 A77-JJ190
A-2
SUBJECT IBDBX
ACTO&TOBS
&coastic eiission investigation - helicopter rotor sjsteo
[AD-A033571] p0319 H77-22110
AcoQstic enission stractnre-borne noise neasareoents on aircraft daring flight CAD-&033188] p0319 H77-22111
ACOUSTIC BXCITATIOH
Material daaping developnents for aircraft
lightweight etractnres subjected to acoustic loads [AIAA 77-396] p0206 A77-25748
Plow regimes aoderlying aeroacoastic excitation of airplane wings
p0211 A77-26039
ACOUSTIC FATIGUE
Specialists' fleeting on Acoustic Fatigue fieview
aircraft construction materials
[ AGAED-CP-222] p0328 H77-22568
Review of acoustic fatigue activities in Germany
p0329 H77-22569
Experimental solutions cf acoustic fatigue problems — in aircraft construction materials
p0329 877-22572
Review of acoustic fatigue activities in the United Kingdcm
p0329 877-22573
ACOUSTIC GBBBBATOBS U SOUND GENERATORS
ACOUSTIC ISPECABCB
A theoretical study of the acoustic impedance of orifices in the presence of a steady graxing flow
pOlOO A77-17066
DC-10 integrally woven pclyimide/f iberglass acoustic panel program
p0255 A77-27498
ACOUSTIC IBSTABILITT
Effect of flow characteristics in a supersonic annular jet on the development of acoustic perturbations in the jet
p0203 177-25536
ACOUSTIC BBASUBBflBBTS NT NOISE HEASUBEflENT
Signal-treatment methods during aircraft-engine inspection based on vibroacoustic noises
p0008 A77-11603
Sound shielding on an engine model and comparison with theory
[DGLB PAPER 76-163] p0094 A77-16573
In-fligbt far-field measurement of helicopter impulsive noise
p0248 177-26886
Vibroacoustical method for determining the technical state of aircraft turbine engines
pOQ15 A77-39269
A revaluation of helicopter main rotor noise
p0463 A77-43346
Additional experiments with a four-bladed cyclic pitch stirring model rotor, part 2 of second yearly report
[NASA-CR-137966] p0017 877-10006
Acoustical evaluation of the NASA Langley V/STOL wind tunnel
[NASA-CR-145087] p0038 877-11068
Theoretical and experimental investigation of
noise shielding for jet engines acoustic and
aerodynamic interference measurements (BHFT-FB-8-76-09 ] p0183 877-17072
Aconstic tests of angmentor wing model
[NASA-TH-X-3519] p0315 877-22046
Effects of combined acoustic and flight loads of crack growth
CAD-A033573] p0338 877-23550
Noise of fan designed to reduce stator lift fluctuations
[HASA-TH-X-3538] p0371 877-24141
Attenuation of upstream-generated low frequency noise by gas turbines
[8ASA-CR-135219] p0477 877-28122
Investigation of the effects of a moving acoustic medium on jet noise oeasnrements
[BASA-CR-152038] p0497 877-29921
ACOUSTIC BOZZLBS
Aeroacoustic studies of coanoular nozzles suitable for supersonic cruise aircraft applications
p0219 877-18020
Coannular nozzle noise characteristics and \ application to advanced supersonic transport engines
p0220 877-18021
ACOUSTIC PfiOPAGATIOB
Calculation of carves of constant equivalent levels of enduring sound for implementation of the aircraft noise protection law - fletbods and preliminary results
p0090 A77-16417
Structural acoustic considerations for aircraft
p0150 A77-20633
The transmission of aconstic plane-waves at a jet exbaost
[AIAA PAPER 77-22] p0160 A77-22207
The effect of forward flight on the diffraction radiation of a high speed jet
p0195 A77-24301
Aconstic shock from an aircraft flying along an arbitrary trajectory in a layered atmosphere with a three-component wind
p0296 A77-30563
Aerodynamic and aconstic tests of duct-barning turbofan exhaust nozzles
[8ASA-CR-2628 ] p0l75 877-16986
Analytical studies of some acoustic problems of jet engines
[PB-264918/4] p0478 877-28133
ACOUSTIC PBOPBBIIBS ST ACOUSTIC IRPEDA8CB NT ACOUSTIC IBSTABILITT BT ACOUSTIC SCATTERING ST SOUND INTBHSITT
Radiation characteristics of acoustic sources in
circQlar notion helicopter noise
p0053 A77-14964
Acoustic properties of pneumatic vortex sprayers
p0441 A77-40703
Upper surface blowing aerodynamic and acoustic characteristics
[AIAA PAPER 77-608] p0449 A77-41857
Acoustical evaluation of the NASA Langley V/STOL wind tunnel
[NASA-CB-145087] p0038 N77-11068
Acoustic and aerodynamic performance of a
1 .5-pressure-ratio, 1.83-neter (6 it) diameter fan stage for tnrbofan engines (QF-2) [BASA-Tfl-X-3521 ] p0289 877-21051
ACOUSTIC BADIATIOB U SOUND SAVES ACOUSTIC SCATTBBIB6
Beasurement of wake vortex strength by means of acoustic back scattering
poooe A77-11712
Acoustic scattering of point sources by a moving prolate spheroid — - jet fuselage
[AIAA PAPER 77-1326] p0567 A77-51080
ACOUSTIC SIBDLATIOB
Simulation of flight-type engine fan noise in the SASA-Xevis 9 x 15 anechoic wind tunnel
p0504 A77-44456
Bethods of noise simulation and their application to flight simulators
[FB-22] p0494 877-29179
ACOUSTIC S0DBD1B6
floDitorlng of aircraft wake vortices at Heathrow Airport
p0400 A77-37711
ACOUSTIC STABILITI 0 FBSQUE8CT STABILITY ACOUSTIC VI6BATI0BS U SOUND 8AVES ACOUSTICS HT ABBOACOUSTICS NT PSTCB0AC0U5TICS ACQUISITION NT DATA ACQUISITION NT TARGET ACQUISITION ACTI80BBTBBS 87 IBFBABBD DETECTORS 8T INFRARED SCANNERS 87 8ICBONAVE BADIOBETBBS ACTOATOBS
Prediction and measurement stiffness and damping of — - of P-15 aircraft [AIAA 77-420]
Application of distributed
control surfaces in slender wings
p0254 A77-27159
Design and fabrication of an 8000 PSI
control-by-wire actuator for flight testing in a T-2 C airplane
of the dynamic hydraulic servo-actuators
p0208 A77-25790 boosters - — for
A-3
ADAPTIVE C09TEOL
SUBJECT IHOBX
[AD-A024487] p0037 N77-11065
Dual output variable pitch turbofan actuation sjsteia [NASA-CASE-LEW-12419-1] p0123 F77-14025
High speed hydraulic starter motor for aircraft auxiliary pover unit
[AD-A027413] p0172 H77-16065
Objectives for the design of improved actuation
systems for flight ccntrol systems
p0376 N77-25073
ADAPTIVE COEi'BOI.
The stochastic control of the F-8C aircraft using the multiple model adaptive control /MRAC/ method
pOOIl A77-12428
Application of Liapunov model - Tracking parameter identification for the CB-47 helicopter
pOOII A77-12460
Estimation of the parameters of the dynamic model of an aircraft with the purpose of designing adaptive numerical control
p020l A77- 25281
RASA'S advanced control lav program for the F-8 Digital Ply-By-Wire aircraft
p0267 A77- 28802
Haximum likelihood identifier refinements for P-8C adaptive ccntrol
p0267 A77-28803
An adaptive flight controller for the P-8 without explicit parameter identification
p0267 A77-28804
Digital controllers for VTCL aircraft
p0268 A77- 28845
Digital ccntrol of high performance aircraft using adaptive estimation techniques
p0295 A77-30480
Application of pole allocation to the design of stabilization systems, illustrated by the longitudinal motion of an aircraft
p0360 A77-36980
Flight data processing with the P-8 adaptive algorithm
[AIAA 77-1042] p0455 A77-42758
A two-level adaptive controller for application to flight ccntrol systems
[AIAA 7*»-1092] p0456 A77-42797
Application of OHF adaptive array to navigation/tracking systems
p057l A77-51185
F-8C adaptive flight control lavs
CNASA-CB-2880] p0596 H77-33202
F-8C adaptive flight ccntrol extensions — for maximum likelihood estimation
[NASA-CB-2881 ] p0596 N77-33203
ADAPTIVE CONTBOL STSTEBS 0 ADAPTIVE CCHTBCL ADAPTIVE PILTEBS
Improved navigation using adaptive Kalman filtering
p0150 A77-20657
Adaptive tracking of abruptly maneuvering targets
p0267 A77-28836
Adaptive fading memory filtering in a decentralized airborne tracking system [AIAA 77-1C88] ' p0456 A77-42793
ADDITIVES NT ANTIOXIDANTS NT OIL ADDITIVES NT PHOPELLAST ADDITIVES
The electrical conductivity during pumping and filtration of 6T fuel containing an antistatic additive
p0300 A77-31441
New potentials for conventional aircraft when powered by hydrogen-enriched gasoline
p0312 A77-33392
ADDBBSSIB6
ADSEL - A selective address secondary surveillance radar
p0402
ADBEBOBETEBS 0 ADHESION TESTS AOBESIOH TESTS
Durability of bonded aluminum structure
p0046
ADHESIVE B0HDIH6
Durability of bonded aluminum structure
p0046
Effect of surface exposure time on bonding commercially pure titanium alloy
p0046
A77-37722
A77- 13733
A77- 13733 of
A77- 13735
Aerospace adhesive bonding
p0198 A77-24924
Aerospace veld bonding-rivet bonding
p0198 A77-24925
Nays of improving joints in aircraft construction
p0253 A77-27149
PABST surface treatment and adhesive selection
Primary Adhesively Bonded Structure Technology for aircraft structures
' p0255 A7/-2/519
Research on adhesive bonding and surface characteristics of metals at Fokker-VFN [FOK-B-1816] p0039 N77-11405
Adhesive bonded aerospace structures standardized repair handbook
[AD-A035601] p0425 B77-26072
Exploratory development on durability of adhesive bonded joints
[AD-A039864] p0530 B77-30249
Surface finishing of metal airfoils by
adhesive bonding
[NASA-CASE-HSC-12631-2] p0538 N77-311J1
ADHESIVES
High performance composites and adhesives for 7/STOL aircraft
[AD-A035928] p0388 N77-25265
ADBIHISTBATIOH 0 MANAGEBENT
ADVAHCED AIBBOBNB COBBAHD POST 0 B-4A AIBCRAPT
ADVANCED TSCBNOL06T LZGfi'2 THIN AIRCBAFT D ATLIT PROJECT AEfilAL EXPLOSIONS
Research on smart target for aerial combat. Part 1: General description
[AD-A029171] p0180 N77-17050
Research on smart target for aerial combat. Part 2: Technical description
[AD-A029172] p0180 N77-17051
ABBIAL IBA6BBT D AERIAL PHOTOGRAPHY ABBIAL PHOTOGBAPBT
A new, versatile stereo-camera system for large-scale helicopter photography of forest resources in central Europe
p0189 A77-23271
The KA-102A Lorop camera airborne Long Range
Oblique Photography
p0191 A77-23536
KS-128 night photo system flight test results
p0192 A77-23540
The helicopter Ka-26 in the Special Purpose Plights Sector of interflug. II
p0555 A77-49657
ABBIAL BECONNAISSANCS
Aerial reconnaissance systems; Proceedings of the Seminar, Heston, Va., Rarch 24, 25, 1976
p0190 A77-23517
Reconnaissance design considerations for the F-5 multiple mission tactical fighter
p0190 A77-23518
Criteria for developing a multi-sensor
reconnaissance pod system for carriage on tactical aircraft — — onboard A-7 aircraft
p0190 A77-23519
Tactical reconnaissance pod system development for the P-14
p0190 A77-23520
fiPV sensor system interface
p0190 A77-23521
Integration of a tactical reconnaissance system with Navy attack aircraft
p0190 A77-23522
HOW real Is real time — - reconnaissance image data management
p0191 A77-23526
A CCD viewfinder as an adjunct to aerial reconnaissance systems
p0191 A77-23527
A simple technique for making long range imaging and surveillance systems trade-offs - — TV camera compensation nomographs for aerial reconnaissance
p0191 A77-23528
Otllization of IB imagery in tactical reconnaissance
p0191 A77-23529
Blcrovave radiometric imagor design for pods and aircraft
pOISI A77-23532
SUBJECT IBDEZ
ABBODTB&BIC CBABACTEBISTICS
The AB/OXD-1 electEODic caoera BP-4C airborne
reconnaissance pod sjstes
p0192 A77- 23537
Long wavelength radar - Its pnrpose and applications
p0192 A77-23538
The Ra-26 helicopter in the special flights domain of Inteiflng. I
p0«15 A77-39453
Beal-tioe aerial reconnaissance nslng the retarn-beaa vidicon
pOftai A77-40665
Aircraft laboratories and experience in using them for the development of methods and means of remote sensing of eacth resources
p0515 A77-47199
Space experiment simulation using an aircraft laboratory
p0515 A77-47200
An evaluation of futora BFV autcnatic navigation systems
p0518 A77-47349
Advanced avicnics for the Advanced fiemotely Piloted Vehicle /ABPV/
p0518 A77-47350
A miniature rotary-wing BPV
p0518 A77-47351
Analysis of phase IIB of PE 43.8 Scout
helicopter as an observation platform [AD-A028816] p0180 H77-17049
An analysis of personnel parachutes for use by Marine Corps Porce Beconnaissance Units [AD-A041151] p0587 H77-33124
&BBIAL BUDDSBS
The development of a carbon fiber-reinforced plastic rudder for the Alpha Jet
[DGLB PAPEB 76-193] p0094 A77-16572
Trapped rubber processing for advanced composites [SHE PAPEB EH76-172] p0563 A77-51Q09
Wind tunnel tests of the dynamic characteristics of the fluidic rudder
[HASA-CR-145142] p0232 H77-18163
Thrust augmented spin recovery device
[HASA-CASE-lAB-11970-1] p0323 H77-22147
ABBOACOOStICS
Semiempirical theory of the generation of discrete tones by a supersonic underexpaoded jet impinging on an obstacle
p0306 A77-32283
A parametric model study of the noise generated by the aerodynamic interaction of the tail rotor with the wake of the sain rotor
p0342 A77-33777
Aero-acoustic performance comparison of core
engine noise suppressors on HASA quiet engine *C* [AIAA PAPEB 77-922] p0412 A77-38597
Upper surface blowing aerodynamic and acoustic characteristics
[AIAA PAPEB 77-608] p0449 A77-41857
Core noise source diagnostics on a turbofan engine using correlation and coherence technigues
p0504 A77-44457
Coherent structures In the mixing zone of a subsonic hot free jet
[ONEBA, TP so. 1977-88] p0562 A77-50989
Theoretical jet exhaust noise model for the duct burning turbofan
[AIAA PAPEB 77-1264] p0564 A77-51028
Are wheel-well related aeroacoustic sources of any V significance in airftane noise
[AIAA PAPEB 77-1270] p0564 A77-51033
Boise component method for airframe noise
[AIAA PAPEB 77-1271] p0564 A77-51034
Hew scaling laws for hot and cold jet mixing noise based on a geometric aconstics model [AIAA PAPEB 77-1287] p0565 A77-51047
Unsteady surface pressure characteristics on aircraft components and farfield radiated airframe noise
[AIAA PAPEB 77-1295] p0565 A77-51052
Forward flight effects on EBP noise Externally
Blown Flaps
[AIAA PAPEB 77-1314} pOS66 A77-S1069
Bunerical prediction of aeroacoustic jet-flap floss [AIAA PAPEB 77-1316] p0566 A77-51071
Interim noise correlati.cn for some OTR
configurations using external jet-flow deflectors — engine Over The Wing
[AIAA PAPEB 77-1317] p0566 A77-51072
Summary of forward velocity effects on fan noise (AIAA PAPEB 77-1319] p0566 A77-51074
Investigation of subsonic fan noise sources by fluctuating pressure measurements on rotating blades
(AIAA PAPEB 77-1321] p0566 A77-51075
Acoustic scattering of point sources by a moving prolate spheroid — - jet fuselage
(AIAA PAPER 77-1326] p0567 A77-51080
Effect of flight on jet noise from supersonic under expanded flows
(AIAA PAPEB 77-1328] p0567 A77-51082
Effects of forward notion on jet and core noise
(AIAA PAPEB 77-1330] p0567 A77-51084
Acoustic performance of inlet multiple-pure-tone suppressors installed on basa Quiet Engine *c* (AIAA PAPEB 77-1333] p0567 A77-51087
Effects of simulated flight on fan noise suppression (AIAA PAPEB 77-1334] p0567 A77-51088
Helicopter rotor aerodynamic and aeroacoustic environments
(AIAA PAPEB 77-1338] p0568 A77-51091
Some results of the testing of a full-scale Ogee tip helicopter rotor; acoustics, loads, and performance
(AIAA PAPEB 77-1340] p0568 A77-51093
Interaction of rotor tip flow irregularities with stator vanes as a noise source
(AIAA PAPEB 77-1342] p0568 A77-51095
Effect of forward notion on turbomachinery noise
(AIAA PAPEB 77-1346] p0568 A77-51099
Simultaneoos characterization of jet noise sources
and acoustic field by a new application of conditional sampling
(AIAA PAPER 77-1349] p0569 A77-51102
Experimental results of large-scale structures in jet flows and their relation to jet noise prodnction
(AIAA PAPEB 77-1350] p0569 A77-5110J
Aeroacoustic performance of a scoop inlet
(AIAA PAPER 77-1354] p0569 A77-51107
The influence of the inlet duct contour on forward
radiated fan noise
(AIAA PAPEB 77-1355] p0569 A77-51108
Acoustic loads on upper-surface-blovn powered-lift systems
(AIAA PAPER 77-1363] p0569 A77-51115
Cabin noise behavior of a USB STOL transport upper surface blowing TC-14 aircraft (AIAA PAPEB 77-1365] p0569 A77-51117
An analytical model for entropy noise of subsonic nozzle flow
(AIAA PAPEB 77-1366] p0569 A77-bni8
ABBOSIBAHIC AXIS U AEBODIHAHIC BALABCE ASBODTBABIC BALABCE
Weight and balance considerations in the design of the A-10A close air support aircraft (SAWE PAPEB 1104} p0010 A77-12183
Scram jet exhaust simulation technique for hypersonic aircraft nozzle design and aerodynamic tests
(AIAA PAPEB 77-82] p0138 A77-19815
External force balance - The measurement of inflight loads on F-14 external stores — aircraft reliability design
p0243 A77-26829
Aerodynamic centre of wing-fuselage combinations (BSDO-76015] p0127 B77-14992
ABBODTBABIC BBAEES BT LEAD1B6 EDGE SLATS BT TBAIL1B6-EDGE FLAPS HT WIB6 FLAPS
F-15 composite speedbrake in production
p03S9 A77-36682
ABBODIBABIC BUSS U FLUTTER
ABBODTBABIC CBBTBB U ABBODTBABIC BALABCE ABBODTBABIC CBABACTEBISTICS BT ASBODTBABIC BALABCE BT ASBODTBABIC DBAG BT ABBODTBABIC STABILITT BT I8TEBFEBEBCE DBAG BT IBTEBFEBEBCB LIFT HT JET LIFT BT LIFT HT BOTOB LIFT
HT STATIC ABBODTBABIC CBABACTEBISTICS
A-5
&BBODTBARIC CBfiBACTBBISTICS COBTD
SUBJECT IHDEX
KT SOPBBSONIC DRAG
Practical regnirements in industry in
computerized aerodynamic calculations for aircraft
p00l3 A77-12552
Investigation of the effect of interference of a delta virg and a half-body
p0052 A77-'i4882
Israel Annual Conference on Aviation and
Astronautics, 18th, Tel Aviv and Haifa, Israel,
Bay 19, 20, 1976, Proceedings
p0053 A77-15026
ABA proposes nev propeller aerofoils
p0056 A77-15623
Determination of the aerodynamic damping of bending-tvisting oscillations of turbcnachine blades in air streams
p0059 A77-15978
Analysis of the nocstationary aerodynamic characteristics of cascades of arbitrarily shaped profiles
p0059 A77-15981
Determination of aerodynamic damping during torsional vibrations of turbine blades
p0060 A77- 15984
Influence of aerodynamic factors on the excitation of torsional flutter in the blades of compressor cascades
p0060 A77-15990
Effect of certain aerodynamic factors on
inducement of vibraticns in turfaomachine blades
p0061 A77-15995
Flight dynamics and contrcllability of large jet airplanes Russian book
p0089 A77-16175
The effect of twist on the aerodynamic investigation of axial compressor blades
p0098 A77-16786
General survey of the studies and testing
techniques that led to the definition of H500 performance
p0100 A77- 17050
Ejectors for supersonic transport aircraft - Analytical method
p0106 A77-17262
Ride control for high speed ground transportation including passenger-seat dynamics and active aerodynairic suspensions
p0115 A77-18724
Effect of a conical break in delta wings on aerodynacic characteristics
p0136 A77- 19733
Aeromechanics of mission completion for structurally damaged aircraft
[AIAA PAPEB 77-112] p0139 A77-19836
Effects of inviscid parallel shear flows on steady and unsteady aerodynamics and flutter [AIAA PAPER 77-158] p0140 A77-19864
On the analysis of the aerodynamic and flutter characteristics of transonic compressor blades
p0145 A77-20139
Handling quality criterion for heading control
aileron-rudder sequencing for coordinated turns
p0147 A77-20443
Aerodynamic design future aircraft design
factors
p0153 A77-20716
Improvement of the structure-dynamical properties of aircraft with CCV systems
[DGIB PA-’^EB 76-237] p0156 A77-21876
Possibilities and solution methods of CCV technology
[DGLB PAPEB 76-236] p0156 A77-21879
The technical concept of the IL-62R. II - Fuel system
p0159 A77-22120
On aerodynamic coupling between lateral and
longitudinal degrees of freedom - — for military flight conditions
[AIAA PAPER 77-4] p0160 A77-22206
Practical aerodynamics of the Yak-18T airplane
Russian book
p0162 A77-22450
A wing for the Airbus
, p0163 A77- 22662
Theory of an axisymmetric parachute. I
p0193 A77-23854
Supersonic gas flow past permeable plates
p0193 A77- 23860
Development of a turbulent boundary layer after interaction with a shock wave at H s: 2-6
p0202 A77-25J26
StructureSf Structural Dynamics and Baterlals '' Conference, 18th, Harch 21-23, 1977, and Dynamics Specialist Conference, San Diego,
Calif., Harch 24, 25, 1977, Technical Papers. Volume B - Dynamics, structural dynamics
p0207 A77-25778
Viscous and elastic perturbations of
two-dimensional hypersonic aerodynamics [AIAA 77-449] p0210 A77-25807
Flow regimes underlying aeroacoustic excitation of airplane wings
p0211 A77-26039
Refinement of the Bean Streamline Hethod of blade section design
[ASHE PAPEB 76-BA/FB-ll] p0213 A77-26437
The commercial supersonic aircraft
p0250 A77-26999
Theory and practice of designing passenger aircraft --- Russian book
p0251 A77-27126
Aerodynamics of passenger aircraft
p0251 A77-27127
Hetbods in the aerodynamical design of lifting surfaces
p0251 A77-27128
flethods of linear theory in problems involving optimization of the aerodynamical characteristics of subsonic profiles
p0251 A77-27130
Changes in aerodynamical characteristics due to structural deformations
p0252 A77-27134
High-lift devices on a wing and means of improving their effectiveness
p0253 A77-27148
Summary of NASA aerodynamic and beat transfer studies in turbine vanes and blades [SAE PAPER 760917] p0259 A77-28225
The calculation of aerodynamic characteristics of wing-body combinations at subsonic flight speeds
p0260 A77-28367
The variable geometry in supersonic compressors
[ASHE PAPEB 77-GTr35] p0263 A77-285b0
Further developments in the aerodynamic analysis of unsteady supersonic cascades. II - Aerodynamic response predictions
[ASHE PAPEB 77-GT-45] p0264 A77-28558
High-tenperature potential of uncooled radial turbines
[ASHE PAPEB 77-GT-46] p026« A77-285i)9
synthesis techniques for insensitive aircraft control systems
p0268 A77-28843
The aerodynamic design and testing of turbine blades having high turning angles
p0270 A77-29322
Flight mechanics. Collection of papers dedicated to the sixtieth anniversary of the academician Vladimir Vasll*evich Struminskli - — Bussian book
p0296 A77-30555
Nonlinear aerodynamic characteristics of slender wings of arbitrary planform
p0296 A77-J0556
Some specific features of the aerodynamic characteristics of cones situated in viscous hypersonic flow
p0297 A77-30576
Aerodynamic characteristics plane diffusor
cascades in which the flow over the blade backs is controlled by injecting air from slots into the boundary layer
p0305 A77-32092
Analytical calculation of carves of the 'airfoil profile' type
p0305 A77-32100
Effect of endvall cooling on secondary flows in turbine stator vanes
p0306 A77-J2239
Analysis of the geometry of an axisymmetric
hypersonic wake and of the gas velocities in the wake on the basis of aeroballistic test data
p0307 A77-32J83
Flow past an airfoil of arbitrary shape by a potential stream of fluid near a solid interface. 1, II
pOJOe A77-J2703
Calculation of the nonlinear aerodynamic
characteristics of a wing of complex planform
A-6
SOBJECT IHDEX
AEBOOTBiBIC CBABACTBBISYICS COBTD
vith allovance for vortex sheet at the nose
p0309 A77-32811
Theoretical prediction of over-ving-blowing aerodynaoics
[AIAA 77-575] p0348 A77-34935
Developoent of the circnlation control ving to provide STOI potential for high perforaance aircraft
CAIAA 77-578] p0348 A77-34937
V/STOL aerodynamic testing technigaes at British Aircraft Corporation
[AIAA 77-584] p0349 A77-34941
The AT-86 wing - Aerodynamic concept and design
[AIAA 77-607] p0351 A77-34959
A contribntion to calcnlate the performance of multistage axial-flcv compressors
p0360 A77-36977
Effect of angle of attack and Hach namber on
slender ving aerodynamics application to
space shuttle
[AIAA PAPER 77-667] p0361 A77-37021
A tvo-dimensional cascade solution using minimized surface singularity density distributions - with application to film ceded turbine blades [AIAA PAPER 77-715] p0362 A77-37055
In-flight measurements of the GA/W/-2 aerodynamic characteristics
[SAE PAPER 770461] p0393 A77-37079
An investigation of the aerodynamics and cooling of a horizontally-opposed engine installation [SAE PAPER 770467] p0393 A77-37085
The controlwing aircraft applied to flying boat
[SAE PAPER 770474] p0394 A77-37092
Ose of simplified flow separation criteria for
slotted flap preliminary design
[SAE PAPER 770481] p0394 A77-37097
The fenestron helicopter £an-in-tail concept
status and evolution
p0405 A77-37792
Fundamentals of aerodynamic design: Propellers /2nd enlarged edition/ Serbo-Croatian book
p0405 A77-37949
Aircraft anti-icing devices
p0415 A77-39275
Aerodynamics of helicopter flight near the ground
[AHS 77-33-04] p0418 A77-40052
Upper surface bloving aerodynamic and acoustic characteristics
[AIAA PAPER 77-608] p0449 A77-41857
Hethods and problems in practical aerodynamics /4th revised and enlarged edition/ — - Russian book
p0454 A77-42219
Determination of longitudinal aerodynamic
derivatives from steady-state measurement of an aircraft
[AIAA 77-1123] p0458 A77-43156
Nazimum likelihood estimation of aerodynamic derivatives for an oblique ving aircraft from flight data
[AIAA 77-1135] p0459 A77-43166
Aerodynamic characteristics of supersonic fighter airplane configurations based on Soviet design concepts
[AIAA 77-1162] p0460 A77-43188