NASA SP 7037 (92)
`
`A CUMULATIVE INDEX
`
`TO THE 1977 ISSUES OF
`
`AERONAUTICAL
`ENGINEERING
`
`A SPECIAL BIBLIOGRAPHY
`
`JANUARY 1978
`
`c
`
`NATIONAL AERONAUTICS AND SPACE ADMINISTRATION
`
`GE-1008.001
`
`

`
`SUPPLEMENTS COVERED IN THIS INDEX
`
`Document
`
`NASA SP-
`NASA SP-
`NASA SP-
`NASASP-
`NASA SP-
`NASA SP-
`NASASP-
`NASA SP-
`NASA SP-
`NASA SP-
`NASA SP-
`NASA SP-
`
`7037(80)
`7037(81)
`7037(82)
`7037(83)
`7037(84)
`7037(85)
`7037(86)
`7037(87)
`7037(88)
`7037(89)
`7037(90)
`7037(91)
`
`Page
`Range
`
`1-41
`43-87
`89-133
`135-187
`189-240
`241-293
`295-339
`341-390
`391-440
`441-497
`499-547
`549-598
`
`Dale
`
`Coverage
`
`February 1977
`March 1977
`April 1977
`May 1977
`June 1977
`July 1977
`August 1977
`September 1977
`October 1977
`November 1977
`December 1977
`January 1978
`
`January 1977
`February 1977
`March 1977
`April 1977
`May 1977
`June 1977
`July 1977
`August 1977
`September 1977
`October 1977
`November 1977
`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.
`
`GE-1008.002
`
`

`
`SPECIAL NOTICE
`
`The abstract sections of the monthly supplements of 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
`
`GE-1008.003
`
`

`
`NASA SP-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).
`
`JANUARY 1978
`Scientific and Technical Infoimotion Offite
`NATIONAL AERONAUTICS AND SPACE ADMINISTRATION
`Washington, D C
`
`GE-1008.004
`
`

`
`This Index is available from the National Technical Information Service (NTIS),
`Springfield, Virginia 22161 for $9 00 domestic, $ 18 00 foreign
`
`tf
`
`GE-1008.005
`
`

`
`INTRODUCTION
`
`WHAT THIS CUMULATIVE INDEX IS
`
`through
`This publication is a cumulative index to the abstracts contained in NASA SP-7037(80)
`NASA SP-7037O1) of 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 IAA 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," i e, 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
`
`GE-1008.006
`
`

`
`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)
`(Source index entry)
`
`BOEING CO, SEATTLE, WASH
`
`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 REPORT/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
`
`GE-1008.007
`
`

`
`TABLE OF CONTENTS
`TABLE OF CONTENTS
`
`SUBJECT INDEX
`A-1
`SUBJECT INDEX ............................................................. .. A-1
`PERSONAL AUTHOR INDEX
`B-1
`PERSONAL AUTHOR INDEX .......................................... .. B-1
`CORPORATE SOURCE INDEX
`C-1
`CORPORATE SOURCE INDEX ...................................... .. C-1
`CONTRACT NUMBER INDEX
`D-1
`CONTRACT NUMBER INDEX ......................................... .. D—1
`REPORT/ACCESSION NUMBER INDEX
`E-1
`REPORT/ACCESSION NUMBER INDEX ...................... .. E-1
`
`V
`
`GE-1008.008
`
`GE-1008.008
`
`

`
`AERONAUTICAL ENGINEERING IA Special Bibliography
`
`SUBJECT INDEX
`
`JANUARY 1978
`
`1977 Cumulative Index
`
`Typical Subject Index Listing
`p-| SUBJECT HEADING |
`•
`
`ADAPTIVE C01TBOL
`
`r-l F-8C adaptive flight control extensions
`maximum likelihood estimation
`[HASA-CB-2881]
`..
`
`P0596 H77-33;
`
`EXTENSION
`T
`
`for^—'
`
`TITLE
`
`REPORT
`NUMBER
`
`PAGE
`NUMBER
`
`_H
`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 in sequence with the IAA accession numbers
`appearing first
`
`A-« AIRCRAFT
`Baseline data from an A-4 cockpit in simulated
`carrier fleck fire
`F"332 H77-23077
`[AD-A03U217]
`Void fillet foam accelerated load testing
`on
`an A-« aircraft
`p0338 H77-23273
`[AD-A031118]
`Statistical analyses applied to the OS Navy
`aircrew automated escape systems
`p0381 H77-25129
`[AD-A035C67]
`Statistical analysis of OS Navy major aircraft
`accident rates, pilot and aircraft
`tine-dependent variables
`[AD-AOU0096]
`1-6 AIRCRAFT
`AN/APQ-118 mnltimode radar for the A-61 all
`weather attack aircraft
`
`p0525 H77-30099
`
`p0384 H77-25157
`
`p0397 A77-37120
`Response of A-6 landing gear door to air shock
`loading
`[AD-A0351I59]
`A-7 AIBCEAFT
`Fiber optics application to A-7 aircraft
`internal data-signal transmission system
`p0117 A77-192U2
`Advanced composites manufacturing as influenced by
`design
`fcr A-7D aircraft outer wing panel
`p0159 A77-22145
`Criteria for developing a multi-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 »ing
`p0211 A77-25815
`[AIAA PAPER 77-<l62]
`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 A77-37H05
`
`A-7 titanium nose gear development
`
`p0513 A77-H6801
`Accelerated environmental conditioning of the A-7D
`composite outer ving
`
`p051U A77-U6838
`Fall temperature range protect I've system for
`fastener areas of carrier-based naval aircraft
`[AD-A02U523]
`p0026 H77-10210
`
`A-1
`
`Inertially derived flying qualities and
`performance parameters
`pOOSO B77-1JOb<!
`[AD-A026963]
`Bole of head-up display in instrument flight
`[AD-A030075]
`p0231 N77-18153
`Results of A-7 aloft bottoms np model and weight
`sensitivity analysis
`p0338 H77-2J350
`[AD-A033767]
`Master monitor display applications study for the
`A-7E
`[AD-A039882]
`1-10 AIRCRAFT
`Height and balance considerations in the design of
`the A-10A close air support aircraft
`[SA1E PAPER 1101]
`pOOlO A77-12183
`The Fairchild-Republic A-10 fighter
`
`p0528 K77-30118
`
`p0200 A77-25099
`Y.A-10 stall/post-stall/spin avoidance flight test
`program
`
`p0310 A77-3J178
`advanced avionics for the A-10: A decision
`analysis model
`p012J H77-11I02J
`[AD-A027678]
`Bole of head-up display in instrument flight
`[1D-1030075]
`p0231 H77-18153
`i-37 AIRCRAFT
`S-37B fatigue sensor evaluation program: Full
`scale test and field aircraft instrumentation
`[AD-AO«211<4]
`pOSSO 877-33156
`A-300 MBCBAF*
`Comparison of fatigue design load spectra with
`flight test measurement and service experience
`in A-300 aircraft development
`
`p009J A77-16561
`
`pOO«8 A77-13772
`Gasdynamic investigations of explosive
`decompression of one of the cargo holds of the
`Airbus A 300
`[DG1H PAPER 76-209]
`& wing for the Airbus
`
`p0163 A77-22662
`Comparison of applied propulsion jet simulation
`technignes, using models of the Airbus A 300
`[HBB-OFE-1276-OB]
`p0267 A77-28789
`Conparative impact tests on metal honeycomb
`sandwich structures
`of A-300 B airbus
`[FOK-H-1813]
`p0082 H77-1J163
`ABLATIVE HATERIALS
`Strength of glass-fibre-reiuforced plastics at
`one-sided heating
`aircraft ablative thermal
`protection coatings
`pOOOS A77-10939
`[IAF PAPER 76-200]
`Evaluation of carbon-carbon composite nosetip
`materials
`[AD-A033SHO]
`ABLATIVE 10SE COHES
`Xhin shell calorimetric techniques for transition
`detection at ablation temperatures
`
`p032<l 1177-22188
`
`p0242 A77-26804
`Evaluation of carbon-carbon composite nosetip
`materials
`[AD-A033540]
`ABOB! APPARATUS
`Study of a fail-safe abort system for an actively
`cooled hypersonic aircraft: Computer program
`documentation
`[FASA-CB-10U927]
`ABSOBPTIOB COEFFICIZBT
`0 BBSOBPTIVITY
`ABSORPTIVE IBDBX
`0 BBSOBPTIVITY
`ABSORPTIVITT
`Calculation of radiant cooling of air behind
`intense shock wayes using mean optical
`characteristics
`
`p032« H77-22188
`
`p0333 H77-2J090
`
`pO«69 A77-Q3993
`
`GE-1008.009
`
`

`
`AIBCBAFT EHGIHES COHTD
`
`SUBJECT IHDBI
`
`fluid
`
`injection
`
`p0259 A77-28237
`
`p02S6 477-27781
`Boundary layer considerations for optimization of
`acoustic liners for aircraft engine ducts
`[SAE PAPEB 760896]
`p0258 A77-28214
`Quietening a quiet engine - The RB211 demonstrator
`programme
`p0258 A77-28215
`[SAE PAPEB 760897]
`The inpact of emission standards on the design of
`aircraft gas turbine engine combustors
`[SAE PAPEB 760909]
`p0259 A77-28220
`TJ101/YF-17 flight test experience
`[SAE PAPER 760932]
`Poverplant for Tornado - The EB.199
`p0262 A77-28466
`Development of a hybrid catalytic conbnstor
`p0261| A77-28595
`[ASHE PAPEB 77-GT-84]
`Engine cycle selection and propulsion system
`integration for future high performance fighter
`aircraft
`p0265 A77-28611
`[ASHE PSPEB 77-GT-101]
`Status report of the tnrbofan engine development
`program in Japan
`p0265 A77-28612
`[ASBE PAPEB 77-GT-102]
`Quiet, Clean, Short-Hani Experimental Engines
`/QCSEE/ - A technology development program
`[ A S HE PAPEB 77-GT-109]
`p0265 A77-28618
`The shaft coupled lift/cruise fan propulsion
`system for Havy mnltimssion 7/STOL aircraft
`[ASBE PAEEB 77-GT-112]
`p0266 A77-28621
`Engine health monitoring in the Boyal Air Force
`p0266 A77-28751
`Design of a mnltivariable controller for an
`advanced t n r b o f an engine
`
`p0268 A77-28844
`Theoretical questions of aircraft GTE design
`parameter optimization
`
`p0272 A77-29512
`Future trends in aero-gas turbine design -
`Conventional engines
`
`p0272 A77-29653
`Future trends in aero-gas turbine design -
`Unconventional engines
`
`p0272 A77-2965H
`A variable pitch fan for an ultra quiet
`demonstrator engine
`
`Engines - Towards lover costs
`for aircraft engine selection
`
`p0272 A77-29655
`computer method
`
`p0273 A77-29663
`The supersonic commercial aircraft. II
`p0301 A77-31717
`Determination of acceptance-inspection parameters
`for gas-turbine engines
`
`p030i| A77-32083
`Influence of the intended nse of an aircraft on
`the optimal parameters of gas-turbine power plants
`p0304 A77-32086
`
`Future propulsion plants. I
`
`p0306 A77-32251
`Investigation of the fatigue strength of aircraft
`gas-turbine twin blades
`
`p0309 A77-32716
`Electric pulsations in turbulent electrogasdynamic
`flows
`
`p0309 A77-32816
`Hew directions in combustion research as related
`to jet propulsion systems
`
`p0341 A77-33702
`Phenomenology and design of jet engine combustors
`p0341 A77-33705
`Baman measurements of specie concentration and
`temperature in an aircraft turbine exhaust
`p0342 A77-33716
`Airplane/engine optimization for an operational
`lift/cruise V/ST01 airplane
`[AIAA 77-572]
`Future propulsion plants. II
`
`p0348 A77-34932
`
`p0353 A77-35032
`Face hardening as a means of improving the fatigue
`strength of aircraft gas-turbine compressor disks
`p0354 A77-35692
`A computer technique for the determination of
`brake horsepower output of normally-aspirated
`reciprocating aircraft engines
`p0393 A77-37083
`[SAE PAPIB 770465]
`Automotive engines - A viable alternative for
`aircraft
`[SAE PASIB 770466]
`
`p0393 A77-37084
`
`An investigation of the aerodynamics and cooling
`of a horizontally-opposed engine installation
`[SAE PAPEB 770467]
`p0393 A77-37085
`Engine structural Integrity Program /ENSIP/,
`fatigue life considerations
`
`p0399 A77-376J9
`Complex mission history effects on low cycle
`fatigue of disks
`
`p0399 A77-37640
`A discussion of reasons for condemning engine
`components before reaching their design fatigue
`life
`
`p0399 A77-37644
`Operation of a turbine stage under variable
`conditions
`flow parameters determination in
`aerodynamic design
`
`The H-mp aircraft engine
`
`p0408 A77-J81J6
`Bnssian book
`p0408 A77-J8JOO
`
`Fan inlet for a V/STOL airplane
`p0409 A77-38544
`[AIAA PAPES 77-802]
`Failure detection of aircraft engine output
`sensors via Bayesian hypothesis testing
`[AIAA PAPEB 77-838]
`pO»09 A77-38554
`Evaluation of propulsive lift enhancement and
`variable cycle engines for advanced tactical
`aircraft
`pO<!11 A77-38575
`[AIAA PAPEB 77-885]
`Engine life considerations in the preliminary
`design of a tactical weapon system
`for
`aircraft
`'
`[AIAA EAPEB 77-955]
`p0412 A77-J8612
`Engine life, usage and cycle selection
`[AIAA PAPEB 77-956]
`p0413 A77-38613
`Accelerated mission testing of gas turbine engines
`[AIAA PAPEB 77-992]
`p04 1 3 A77-386^5
`Vibroaconstical method for determining the
`technical state of aircraft turbine engines
`p0115 A77-J9269
`Constraints on the operational ranges of turbojet
`engines
`
`p0415 A77-J9272
`Propulsion cycle effects for a two-fan V/STOL
`aircraft
`pO<(16 A77-J9477
`[AIAA PAPEB 77-580]
`Separation and investigation of wear particles
`from aircraft engines
`
`Aero engine development costing
`
`p0416 A77-39492
`
`p0417 A77-40010
`Operational reliability of aircraft powerplants
`Bnssian book
`
`pOMSO A77-41961
`
`pO<450 A77-41969
`
`p0447 A77-41648
`Airframe/engine integration with variable cycle
`engines
`[AIAA PAPEB 77-798]
`Propulsion designed for V/STOL
`p0450 A77-4196J
`[AIAi PAPEB 77-804]
`Advanced supersonic transport propulsion
`requirements
`[AIAA PAPEB 77-831]
`Supersonic propulsion - 1970 to 1977
`p0451 A77-41970
`[AIAA PAPEB 77-832]
`An engineering approach to estimating propulsion
`contributions to system life cycle costs
`[AIAA EAPEB 77-879]
`p0452 A77-41981
`Testing of propulsion system diagnostic equipment
`aircraft engine monitoring and inspection
`systems
`p0452 A77-41983
`[AIAA PAPEB 77-895]
`Engine design decisions impact aircraft life cycle
`costs
`p0452 A77-41986
`[AIAA PAPEB 77-916]
`Advanced design procedure for aircraft engine
`selection
`p0452 A77-41989
`[AIAA PAPEB 77-953]
`Life considerations in the engine design process
`[AIAA PAPEB 77-954]
`p0452 A77-41990
`The airjet distortion generator system - A new
`tool for aircraft turbine engine testing
`[AIAA PAPEB 77-993]
`p04b3 A77-42000
`A review of methods enabling increased service
`lives of high-thermal-load turbojet propulsion
`plants
`
`p0461 A77-4J331
`Theory of automatic aircraft power plant control:
`Russian book
`
`p0467 A77-4J604
`
`A-38
`
`GE-1008.010
`
`

`
`DABCI, 7. J.
`
`PEBSORAL AdtBOB INDEX
`
`DABCT, 7. J.
`Inherent errors in asynchronous, redundant digital
`flight controls
`p019i| A77-24192
`Analysis of inherent errors in asynchronous
`redundant digital flight control systems
`[AD-A026954]
`p0124 H77-14035
`DABRELL, 0. i.
`National Airlines Fuel Management and Allocation
`Hod el
`
`p0466 A77-43399
`
`p0488 N77-29108
`
`DABHOZBS, J. S.
`Behavior of a subsonic flow past a thin ving in
`the vicinity of the leading edge
`[OHBRA-HT-1976-16]
`p0380 H77-25107
`Behavior of a subsonic flov past a thin ving in
`the vicinity of the leading edge
`[BSA-TT-401]
`DASB, B.
`Turbulence generated noise on either side of a
`, doable layer jet
`
`p01Q6 A77-20238
`
`DAT, B.
`Dnsteady aerodynamics of helicopter blades
`[ESA-TT-327]
`p0077 H77-13015
`DAD. K.
`Evaluation of vibration levels at the pilot seat
`caused by wing flow separation
`
`p0533 H77-31078
`
`DAOBIA, P. T.
`A nethod for predicting the stability
`characteristics of an elastic airplane. Tolnme
`2:
`FLEX SUB 1.02.00 user's nannal
`p0337 H77-23125
`[NASA-CB-114713J
`A nethod for predicting the stability
`characteristics of an elastic airplane. Volume
`3:
`FLEXSTAB 1.02.00 program description
`tKASA-CB-114714]
`p0337 B77-23126
`DAOSIB, L. B.
`A review and analysis of the niTBE beacon
`collision avoidance system
`[AD-A037225]
`DA7ABI, B.
`Effects of cross-coupling on the stability of
`aircraft
`
`p0366 N77-24090
`
`p0336 H77-23122
`DAVBJPOBT, 0. B.
`Northrop/Dnited States Air Force durability and
`damage-tolerance assessment of the F-5E/F aircraft
`p0327 B77-22558
`
`DATIDSOH, 3. B.
`Bationale for structural inspections
`
`DATIDSOB, B. 1.
`Analysis of phase IIB of FE 43.8
`tAD-A028816]
`DA7IBS, 0. 6. B.
`A variable pitch fan for an ultra quiet
`demonstrator engine
`
`p0228 H77-18100
`
`p0180 R77-17049
`
`p0272 A77-29655
`DA7I1S, 1. E.
`Applications of augmented multilateration
`tracking
`systems
`
`p0570 A77-51183
`"
`DA7IES, P. J.
`An assessment of the accuracy of subsonic
`linearized theory for the design of warped
`slender wings
`pO»76 M77-28110
`[ABC-CP-1324]
`D1TIBS, B. B.
`Design mechanical properties, fracture toughness,
`fatigue properties, exfoliation and
`stress-corrosion resistance of 7050 sheet,
`plate, hand forgings, die forgings and extrusions
`[AD-A024609]
`p0025 H77-10195
`DA7IBS, i. B. B.
`Velocity measurements on the aerodynamic vake of a
`hovercraft using laser Doppler anemometry
`[OTIAS-TR-203]
`p0065 R77-12010
`DATIS, D. 6. B.
`Developing an Agprop
`
`p0298 A77-31026
`DA7IS, 0. B.
`The effect of thrust vectoring on aircraft
`maneuvering
`[AD-A027367]
`p0082 H77-13074
`DATIS, D. I., JB.
`Analysis of the turbulent wake of a cascade airfoil
`,
`p0256 A77-27616
`
`p0592 H77-3J168
`
`DATIS, F. 6.
`Pollution reduction technology program for small
`jet aircraft engines, phase 1
`[HASA-CB-135214]
`DATIS, 6. R.
`Advanced structures technology applied to a
`supersonic cruise arrow-wing configuration
`p0220 N77-18027
`Evaluation of structural design concepts for an
`arrow-wing supersonic'cruise aircraft
`[HASA-CB-2667]
`p0389 H77-2S581
`DATIS, J. B.
`Accuracy of the Rirchoff formula in determining
`acoustic shielding with the use of a flat plate
`[HASA-TH-73261] "
`p0532 H77-30906
`DAVIS, B. B.
`A brief description of the Janeson-Caughey KYU
`transonic swept-wing computer program: FLO 22
`[HASA-TH-X-73996]
`p0167 H77-15977
`DATIS, S.
`Experimental studies of trailing-edge conditions
`on an oscillating airfoil at frequency
`parameters of up to one
`[AIAA PAPBB 77-450]
`DATIS, S. J,
`Research requirements for development of improved
`helicopter rotor efficiency
`p0428 H77-26121
`[BASA-CB-145117]
`Identifying and analyzing methods for reducing the
`energy consumption of helicopters
`[RASA-CB-144953A]
`DATIS, R. Bf
`Through-flow calculations based on matrix
`inversion: Loss prediction
`
`p0257 A77-28044
`
`p0435 H77-27104
`
`p0066 H77-12016
`
`DABB, B. B.
`Failure mode analysis in the light of experience
`p0237 H77-19040
`
`DAI, I. J.
`Prediction of compressor performance in rotating
`stall
`[ASBE PAPEB 77-GT-10]
`DE BOEB, 6. J.
`FAA's flight service stations in modernization
`process
`
`p0262 A77-28S29
`
`pOJ58 A77-36570
`
`DE CBOOS, K. A,
`Boughness element geometry required for wind .
`tunnel simulations of the atmospheric wind
`[ASBE PAPEB 76-RA/FE-18]
`p0213 A77-264J9
`DB 6OBXSE, 1.
`A combined cycle with a partial-oxidation reactor
`p0109 A77-175J4
`
`DB HOFF, B. L,
`Design of a mnltivariable controller for an
`advanced turbofan engine
`
`p0268 A77-28844
`Bodeling and instrumentation requirements for
`multivarianle control of an advanced tnrbofan
`engine
`[AIAA PAPEB 77-834]
`DB JOIGB, J. B,
`A fighter aircraft loading standard for fatigue
`evaluation /'FALSTAFF1/- I - Introduction to
`FALSTAFF
`
`p0409 A77-38551
`
`p0048 A77-13766
`
`DB JOBGB, B, J,
`Flight test evaluation of helicopter operational
`loads and dynamic response characteristics
`p0407 A77-38030
`
`DE KOOBEB, 3, B.
`Fokker-TFB
`
`p0147 A77-20377
`
`DB IEOF7ILLB, B.
`Airport systems planning: A critical look at the
`methods and experience
`
`p0270 A77-294J5
`Bationalization of the European air net
`p0551 A77-48474
`
`DB BOQOBFOB1, T. A.
`Strong coupling and weak coupling between boundary
`layer and external flow
`
`DEAL, P. L.
`A flight investigation of piloting techniques and
`crosswind limitations daring visual STOL-type
`landing operations
`[HASA-TH-D-8284]
`
`p0030 1177-11001
`
`p0269 A77-28940
`
`B-30
`
`GE-1008.011
`
`

`
`AERONAUTICAL ENGINEERING
`
`A Special Bibliography
`
`Abstracts
`January—December 1977
`
`TABLE OF CONTENTS
`
`SP-7037
`Supplement
`
`80
`81
`82
`83
`84
`85
`86
`87
`88
`89
`90
`91
`
`Page
`
`1
`43
`89
`135
`189
`241
`295
`341
`391
`441
`499
`549
`
`GE-1008.012
`
`

`
`1 Report No
`
`2 Government Accession No
`
`3 Recipient's Catalog No
`
`(92)
`
`NASA SP-7037
`4 Title and Subtitle
`Aeronautical Engineering
`A Cumulative Index to the 1977 Issues
`
`5 Report Date
`January 1978
`6 Performing Organization Code
`
`7 Author(s)
`
`8 Performing Organization Report No
`
`9 Performing Organization Name and Address
`National Aeronautics and Space Administration
`Washington, D. C. 205^6
`
`12 Sponsoring Agency Name and Address
`
`10 Work Unit No
`
`11 Contract or Grant No
`
`13 Type of Report and Period Covered
`
`14 Sponsoring Agency Code
`
`15 Supplementary Notes
`
`16 Abstract
`
`This publication is a cumulative index to the abstracts
`contained in NASA SP-7037 (80) through NASA SP-7037 (91)
`of 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). This
`cumulative index includes subject, personal author,
`corporate source, contract, and report number indexes.
`
`17 Key Words (Suggested by Author(sl)
`Aerodynamics
`Aeronautical Engineering
`Aeronautics
`B ibliographies
`
`18 Distribution Statement
`
`Unclassified - Unlimited
`
`19 Security Qassif (of this report)
`
`20 Security Classif (of this page)
`
`Unclass ifled
`
`Unclass ified
`
`21 No of Pages
`638
`
`22 Price*
`
`$9.00 HC
`
`For sale by the National Technical Information Service, Springfield. Virginia 22161
`
`•frUS GOVERNMENT PRINTING OFFICE 1978-735-078/2
`
`GE-1008.013
`
`

`
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`
`DOMESTIC
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`Each library is prepared to furnish the public such services as
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`documents for retention
`
`CALIFORNIA
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`University of Colorado, Boulder
`DISTRICT OF COLUMBIA
`Library of Congress
`GEORGIA
`Georgia Institute of Technology, Atlanta
`ILLINOIS
`The John Crerar Library, Chicago
`
`MASSACHUSETTS
`Massachusetts Institute of Technology. Cambridge
`MISSOURI
`Linda Hall Library. Kansas City
`NEW YORK
`Columbia University, New York
`OKLAHOMA
`University of Oklahoma, Bizzell Library
`PENNSYLVANIA
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`WASHINGTON
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`
`NASA publications (those indicated by an
`the following public and free libraries
`
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`
`CALIFORNIA
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`An extensive collection of NASA and NASA-sponsored documents and aerospace publications
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`and Astronautics. Technical Information Service. 750 Third Avenue. New York. New York 10017
`
`EUROPEAN
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`An extensive collection of NASA and NASA-sponsored publications is maintained by the British
`Library Lending Division. Boston Spa. Wetherby. Yorkshire. England By virtue of arrangements other
`than with NASA, the British Library Lending Division also has available many of the non-NASA
`publications cited in STAR European requesters may purchase facsimile copy of microfiche of NASA
`and NASA-sponsored documents, those identified by both the symbols "#" and "*".
`from ESA -
`Space Documentation Service. European Space Agency. 8-10 rue Mano-Nikis. 75738 Pans CEDEX
`15. France
`
`GE-1008.014
`
`

`
`NATIONAL AERONAUTICS AND SPACE ADMINISTRATION
`WASHINGTON DC 2O546
`
`OFFICIAL BUSINESS
`
`SPECIAL FOURTH CLASS MAIL
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`
`N A S A - 4 SI
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`
`If Hndrlivcr.iblp (Section 158,
`rust.il M.iiiu.il) Do Not Rotur
`
`NASA CONTINUING BIBLIOGRAPHY SERIES
`
`NUMBER
`
`NASA SP-7011
`
`NASA SP-7037
`
`NASA SP-7039
`
`NASA SP-7041
`
`NASA SP-7043
`
`NASA SP-7500
`
`TITLE
`
`AEROSPACE MEDICINE AND BIOLOGY
`Aviation medicine, space medicine, and
`space biology
`
`AERONAUTICAL ENGINEERING
`Engineering, design, and operation of
`aircraft and aircraft components
`
`NASA PATENT ABSTRACTS BIBLIOGRAPHY
`NASA patents and applications for patent
`
`EARTH RESOURCES
`Remote sensing of earth resources by
`aircraft and spacecraft
`
`ENERGY
`Energy sources, solar energy, energy
`conversion, transport, and storage
`MANAGEMENT
`Program, contract, and personnel
`management, and management techniques
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`
`G PO 9 4 4 - 3 70
`
`GE-1008.015