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This bibliography is a selection of references to reports on general and specific aspects of Atmospheric Turbulence. Abstracts of reports written before ...
Typology: Lecture notes
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ATMOSPHERIC (^) TURBULENCE
for public release and sale; its
!~
September 1968 JAN 131"
Reproduced (^) by thq C L I A R ING (^140) US.. r'y Fuderal Scientitfc & Techr -cal Informekhon (^) Sp!ingietld Va 22'
U N C L A S S I F I E D -LI N L I M I T E D
AD-678 760
A DDC BIBLIOGRAPHY ON
ATMOSPHERIC TURBULENCE
Volume I of (^) II Volumes
DDC-TAS-68-
This document has (^) been approved for public release (^) and sale; its distribution is unlimited.
SEPTEMBER 1968
DEFENSE DOCUMENTATION CENTER for SCIENTIFIC and TECHNICAL INFORMATION Cameron Station, Alexandria, Virginia (^22314)
UNCLASSIFIED-UNLIMITED
Atmospheric Turbulence, AD-844^ 020,^ contains^ references^ to
Unclassified reports with^ specific^ distribution^ limitations.
BY ORDER OF THE DIRECTOR, DEFENSE SUPPLY AGENCY
OFFICIAL
,eFRT R. STEGM4. JR. Admiklistrator Defense Do. .. ntation Center
iv
Pages
PREFACE ................................................ iii
AD BIBLIOGRAPHIC REFERENCES
I. GENERAL TURBULENCE STUDIES ................. Gusts; Turbulence Exchange Cuefficients; Gravity Waves; Eddies
II. SPECTRAL ANALYSIS ........................... 33 Power Density^ Spectra;^ Energy^ Spectra; Wave Spectra; Cross-Spectral Analysis
III. TURBULENT DIFFUSION AND DISPERSION .......... 49 Diffusion Equations; Fickian Diffusion Process
IV. TURBULENCE INTERACTION WITH^ ELECTROMAG- 4ETIC AND ACOUSTIC WAVES .................... 61 Optical Turbulence; Acoustic Wave Disturbance; Radio and Radar Wive Propagation
V. PLANETARY BOUNDARY LAYER TURBULENCE: GENERAL STUDIES ............................. 87 Friction Layer Disturbances; Geostrophic Surface Winds; Turbulent Energy Budget; Free Air and Friction Layer Exchange; Laminar Instability
VI. PLANETARY BOUNDARY LAYER TURBULENCE: SURFACE LAYER ............................... 111 Surface Roughness; Vegetative Canopy Flow; T*,-bulent Transfer of Momentum; Thermal Str•ti fi cation.
VII. PLANETARY BOUNDARY LAYER TURBULENCE: LOW L EV EL............... ............. ........... 1 35 Low-Level Jet Streams; Low-Level Gusts
VIII. PLANETARY BOUNDARY LAYER TURBULENCE: O'IER
Stress; Surface Roughness
v
I
DOC REPORT BIBLIOGRAPHY SEARCH CONTROL NO@ /AOiS
AD-275 OS ARMY MISSILE COMMAND REDSTONE ARSENAL ALA ANALYSIS OF^ ATMOSPHERIC^ TURBULENCE^ FROM^ MISSILE FLIGHT WIND MEASUREMENTS fUl AUG 61 IV ESSENWANGEROSKAR Mel REPTs NO. RR TR 61 7
UNCLASSIFIED REPORT
DESCRIPTORS: oATMOSPHERE,^ TURBULENCE,^ eWIND, ANALYSIS, ERRORS. FLIGHT TESTING GUIDED MISSILES, INSTRUMENTATION. MEASUREMENT^ (U)
THE SPLIT OF AN INSTANTANEOUS WIND PROFILE INTO^ ITS MEAN (QUASI-STEADY) PROFILE^ AND^ ITS^ NONSTATIONARY COMPONENTS IS^ DISCUSSED.^ IT^ IS^ SHOWN^ THAT^ TWO MATHEMATICAL CONOITIONS CAN^ SE^ ESTABLISHED^ FOP^ THIS SEPARATION PROCEDURE. FIRST, THE SUM OF THE REMAINING FLUCTUATIONS MUST^ BE^ ZERO,^ IF^ THE VARIATIONS REPRrSENT^ TURBULENCE.^ SECONDLY,^ IT^ MAY RE POSTULATED THAT THE FIRST LAG^ CORRELATION^ BE POSITIVE, AND^ THE^ SECOND^ ONE^ NEGATIVE^ FOR^ A^23 POINT ANALYSIS. THE SEPARATION OF^ THE^ MEAN^ PROFILE^ FROM THE TURBULENT PART IS DEMONSTRATED ON HAND OF AN EXAMPLE FOR DATA OF THE JUPIYER MISSILE FLIGHT^30 BETWEEN '00^ AND^3000 M^ ALTITUDE^ FROM^12 M^ HEIG!4T INTERVAL RECORDINGS. (AUTHOR) (U)
UNCO.ASSIFIED /AO
WIND, WINO SHEAR AND TURBULENCE REPREtENTATIOW FOR ATMOSPHERIC BALLISTICS.^ fUl FEB A) 32P ESSENANGEROSKAR I REPT, NO RR T11) 7 PROJ: 182 79191D
UNCLASSIFIED REPORT
WIND SMEAR PARAMETERS AS A FUNCTION Or THE SCALE OF DISTANCE DELINEATE THE DEFICIENCY^ Of^ DERIVING^ SHEAR PARAMETERS FROM^ SMOOTH^ RADIOSONDE^ RECCRDS,^ THE FINAL TOPIC DEALS WITH THE ANALYSIS OF THE TURBULENCE PARAM ETERS, AND THE SEPARATION OF THE NINO PROFILE FROM MISSILE FLIGHT RECORDINGS INTO STATIONARY AND NONSTATIONARY PARTS. (AUTHOR) fU)
AO-qO0 896
TEX#S A AND M UNIV COLLEGE (^) STATION A STUDY OF SPATIAL VARIATIONS IN MICROMETEOROLOGI CAL PARAMETERS. fUý DESCRIPTIVE NCTE: FINAL REPT., APR 63 96P CLAYTONvWILLIAM Hsi MISTRYPURACHAND De. REPT. NOe 63 15F CONTRACT: AFI9 60' 5527 PROJ: NOS* 7655 v TASK: NOSe 74561 860o MONITOR: AFCRL 63 629
UNCLASSIFIED REPORT
PARAMETERS), (oHEAT, CONVECTION). toTURBULENCE, ANALYSIS)* EXPERIMENTAL DATA. WIND* ATMOSPHERIC TEMPERATURE, (^) TEMPERATURE, ELECTROMAGNETIC WAVES, METEOROLOGICAL INSTRUMENTS, METEOROLOGICAL CHARTS, EVAPORATION, STABILITY, VELOCITY, TABLES, (^) NUMEkICAL ANALYSIS. (^) (U) IDENTIFIERS: M9.)3 SPATIAL VARIATIONS. (^) (U)
A STUDY WAS MADE OF THE TURBULENT (^) EXCHANGE COEF FICIENTS BASED ON ENERGY BALANCE AND MEAN FLOW PARAMETERS MEASURED AT PROJECT GREEN GLOW IT REVEALS THAT THE RATIOS OF THE EXCHANGE COEFFI CIENTS ARE FUNCTIONALLY RELATED TO THERMAL STABIL jTYý THEREBY CONTRADICTING (^) THOSE POSTULATES WHICH HAVE ASSUMCD CONSTANCY OF THE RATIOS FOR ALL STABILITY SITUATIONS. 4AUTHOR) 4U)
UNCLASSIFIED (^) iA
oDC REPORT B!BLIOGRAPHY SEARCH CONTROL NO#^ /AO
AO-4;O (^012) CORNELL AERONAUTICAL LAB INC BUFFALO N Y FIXED-BASE SIMULATOR INVESTIGATION OF^ THE^ EFFECTS^ OF L ALPHA AFr TRUE SPEED ON PILOT OPINION OF LONGITUDINAL FLYING QUALITIES, U) NOV 61 1714P CHALKeCHARLES R, I CONTRACT: AF23 697 7442 PROJ: 8219 TASK: B MONITOR: ASP TDR63 399
UNCLASSIFIED REPORT
SUPPLEMENTARY NOTE:
DESCRIPTORS: 10AIRPLANES, ELEVATORS), (*ELEVATORS, PILOTS), 40PILOTS, REACTION (PSYCMOLOGYI), FLIGHT SIMULATORS, PERFORMANCE (ENGINEERING), FIGHTERS, BOMBERS, TURBULENCE, ACCELERATIO;4, LIFT, TESTS, FLIiHT SPEEDS, SIMULATION, FUNCTIONS, GUSTS, ANGLE OF ATTACK(U) IDENTIFIERS: !963, T-33 AIRCRAFT IU)
THE STUDY IS DIRECTED TOBARD INVESTIGATING THE EFFECTS ON PILOTS RATING OF^ LARGE^ VARIATIONS^ IL ALPHA) IN THE RELATIVE AMPLITUDE^ &NO^ PHASE^ OF^ THE BASIC AIRPLANE RESPONSES TO ELEVATOR CONTROL* TME EFFECTS OF^ L^ ALPHA^ AND^ TRUE^ SPEED^ ON^ LONGITUDINAL FLYING QUALITIES* OPTIMUM CONTROL GAIN, AND NORMAL ACCELERATION RESPONSE TO TURBULENCE WERE INVESTIGATfD IN A GROUND SIMULATOR, THE STEADY STATE VAYIO OF NORMAL ACCELERATION TO ANGLE OF ATTACY dAS FOUNo TO BE OF SIGNIFICANCE BOTH TO THE FLYING QUALITIES Of AN AIRPLANE AND TC THE OPTIMUM LON41TUDINAL CONTROL GAIN* NORMAL ACCELERATION RESPONSE TO ROU4N 4IR WAS )EHONSTRATEC TO BE^ PRIMARILY^ A^ FUNCTION^ OF^ L^ ALPHA AND THE SHORY^ PERIOD^ FRIQUENCY^ ANO^ DAMPING^ RATIO. (AUTHOR! (U)
UNCLASSIFIED
DOC REPORT BIBLIOGRAPHY^ SEAACM^ CONTROL^ NO*^ 1A
AF6 OHIO METEDROLOGY AND THE PILOT (LETCHIKU 0 METEOROLOGIIi,
DEC 6) 394P KRAVCMENKol, V9 I
MONITOR: FTD^ TTY6^620
UNCLASSIFIED REPORT
SUPPLEMENTARY NOTE: TRANS. FROM VOYENNOYE IZOATEL'STVO MINISTERSTYA O0ORONY,^ PP.^ I1)21,^ 1942*
DESCRIPTORS: (SMETEORCLOGY, !NSTRUCTION MANUALSIo PILOTS. AIR^ MASS^ ANALYSIS.^ ATMOSPHERIC^ TEMPERATURE, bAROMETRIC PRESSURE, DENSITY, HUMIDITY, WIND, CLOUDS. ATMOSPHERIC PRECIPITATION. FCG. ANTICYCLONES, CYCLONES. WEATHER FORECAS(ING, ATMOSPHERIC MOTION. THUNDERSTORMS, LIGHTNING, ICE.^ ICE^ FORMATION INDICATORS, AERIAL RECONNAISSANCE,^ AIRCRAFT, AIRPLANES (U) IDENTIFIERS: 2964, US3Ro^ AIRCRAFT^ ICING^ fUl
CONTENTS: BASIC^ METEOROLOGICAL^ ELEMENTSt AIR MASSES, ATMOSPHERIC FRONTS, CYCLONES AND ANTICYCLONESS AIRFLONS AND ATMOSPHERIC TURSULENCEI THUNDERSTORMS AND SQUALLSI AIRCRAFT ICING* .Ul
UNc'..&S;IV 1( /AO
I UNCLASSIFIED
DOC REPORT BIBLIOGRAPHY SEARCH CONTROL NO. IAO
AD-402 998 FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFP OHIO LATERAL VIBRATIONS OF^ AN^ AIRCRAFT,^ CAUSED^ BY^ EFFECT Of WIND GUSTS, DEC 6A 24P DUBOV,As S. I MONITOR: FTD ,1T MTi) 1is. ,6q 11969
UNCLASSIFIED REPORT
SUPPLEMENTARY NOTE: EDITED MACHINE TRANS,^ OF^ GLAVNAYA SEOFIZICHESKAYA OBSERVATORIYA, LENINGRA'ý, TRvDY IUSSRI 1999o NO. 96 I&O P. -16,
DESCRIPTORS: (AIRCRAFT,^ VIBRATION1,^ 4oUST^ LOADS, AIRCRAFT), GUSTSt AERODYNAMIC LOADING,^ BOUNDARY^ LAYER, DIFFERENTIAL EQUATIONS, FUNCTIONS, MOMENTS, CENTER OF GRAViTY, ACCELERATION, USSR (Ul
IN THE ARTICLE EQUATIONS ARE DEVELOPED ESTABLISHING THE CONNECTiON BETWEEN LATERAL VIBRATIONS OF^ AIRCRAFT^ AND^ HORIZONTAL^ GUSTS. EQUATIONS ARE WRITTEN IN A GENERAL FORM TARING INTO ACCOUNT POSSIBLE DIFFERENCFS OF COMPONENTS Of WIND^ ON CIFFERENT SECTIONS OF TME BOUNDARY LATER OF^ THE AIRCPAFT, THE SOLUTION IS INTROOUCED FOR^ THE PARTICULAR CASE, WHEN WIND CAN BE ASSIGNED ONE^ VALUE, BY AVERAGING ALc ALONG THE BOUNDARY LATER OF THE AIRCRAFT. AN^ ANALYSIS^ OF^ THE^ EFFECT^ OF^ G6'STS^ Of DIFFERENT INTENSITIES ON THE^ SIDE^ ACCELERATION^ OF^ TIIE AIRCRAFT'S IENTER OF GRAVITY^ I|^ CONDUCTED.^ THE POSSIBILITV IS^ EXPLAINED^ OF^ SOLVING^ THE^ INVERSE PROBLEM --^ FINDING^ CHARACTERISTICS^ OF^ NORIZnNTAL GUSTINESS OF^ THE^ WING^ BY^ SIDE^ ACCFLERATIONS^ OF AIRCRAFT. NUMERICAL CALCULATIONS sERE^ MADE^ FOR^ A 'NORTHROP 2f' AIRCRAFTo IAUTmOR) (U)
U
UNCLASSIFIED iAO)
MECHANICS AND MECHANICAL ENGINEERING, 1961, NO* q SELECTED ARTICLES, (U) JAN 64 1P SASYKINoVo (^) Vo I ROMANOVSKIIYU No. IAMSARTSUMYAN.S* A. I GAGOASARYANZM* (^) Es IHISHENKOVG* V. a MONITOR: FTO *TT "T62 191 ,64 71396
UNCLASSIFIED REPORT
SUPPLEMENTARY NOTE: EDITED MACHINE TRANS* OF AKADENIYA NAUK SS.1. IZVESTIYA, RCw-4NIKA (^) I MASHINOSTROE4|E, 1961, NO. q, P. 42-10,
DESCRIPTORS: 40MECHANICS, REPORTS,, 4WINGS,* FLUTTER), 40SUPERSONIC FLOW, FLAT PLATE MOOELS), 40PANELS ISTRUCTURAL,, OSCILLATION), AIRCRAFT, AILERONS, FRICTION, ATMOSPHERIC NOTION, (^) GUSTS, OSCILLATION, MODELS (SIMULATIONSo MATHEMATICAL ANALYSIS, STABILITY, RECTANGULAR BODIES, GASES. STRESSES, DIFFERENT!AL EQUATIONS, FUNCTIONS, ELASTICITY, LOADING M"ECHANICS,, CYLINORICA&L BODIES, USSR STRUCTRUAL SHELLS (U)
CCNTENTS: NONLINEAR FLUTTER OF WING OF AIRCRAFT DURING FLIGHT IN BURPY AIRS STA3ILITY OF ORTHOTROPIC PLATES AROUND WHICH FLOES A SUPERSONIC FLOW Or GASS ANO FORCED NONLINEAR OSCILLATIONS OF ELASTIC PANELS. (U)
ADO60i 16b ARMY TRANSPORTATION RESEARCH^ COMMAND^ FORT^ EUSTIS^ VA SUPPLEMENTARY STUDY^ OF^ DESIGN^ FACTORS^ IN^ AIR^ DELIVERY FOR CV-7 CARIBOU AIRCRAFT, AUG 4q^ 39P^ JONESR,^ O0^ mH, TASK: IDiq;124oI99O MONITOR: TRECOM 9 TR64 q
DESCRIPTORS: IeTRANSPORT PLANES, DESIGN), (CONTAINERS, MOTION), CARGO. CARGO PARACHUTES. AIR DROP OPERATIONS, SHORT TAKE-OFF^ PLANES,^ FLOORS. FRICTION, STABILITY, LOADING IMECHANICS), VECTOR ANALYSIS, SAFETY, GUSTS, HANDLING,^ PROGRAMMING LANGUAGES (U) IDENTIFIERS: V-2^ AIRCRAFT,^ V-7^ AIRCRAFT^ (U) A STUDY^ WAS^ MAOE^ OF^ THE^ EXTRACTION^ OF^ LOADS^ BY PARACHUTE FROM THE CV-7 CARIBOU AIRCRAFT TWO FORTRAN PROGRAMS ARE INCLUDED TO^ SHOW^ THE CALCULATION OF THE MAXIMUM SAFE ENVELOPE FOR THE LOADSi VARIOUS CONDITIONS^ WITH^ A^ WIDE^ RANGE^ OF ADJUSTABLE PARAMETERS^ ARE^ CONSIDERED.^ IN^ THE PROGRAMS, THE PARAMETERS MAY BE SET AS DATA TO SIMULATE ANY VALUES, SUCH AS THOSE FOR THE EXTRACTIVE FORCE OF THE EJECTION PARACHUTE,^ FOR^ THE^ COEFFICIENT OF SLIDING FRICTION^ BETWEEN^ THE^ FLOOR^ AND^ THE^ LOAD, AND FOR THE LENGTH OF THE PALLET ON WHICH THE LOAD IS MOUNTED. THE^ CONCLUSIONS^ REACHED^ ARE^ NEGATIVE^ IN CHARACTER, 911T THEY^ CAN^ BE^ OF^ VALUE^ AS^ A^ BASIS^ FOR FURTHER STUDIES. THE LOAD TIPS SO LITTLE AT^ THE SILL OF THE FLOOR WITH THE^ RAMP^ UP^ THAT^ THE^ MAAIMVM SAFE ENVELOPE DEPARTS^ ONLY^ SLIGHILY^ FROM^ THE RECTANGULAR FORM. IT IS BELIEVED THAT THE EFFECTS OF GUST DISTURBANCES AND OF POSSIBLE JAMMING IN THE RAIL RESTRAINT AND RELEASE SYSTEM SHOULD OE INVESTiGATED, SINCE, PROM TIME^ TO^ TIME,^ THfSE INFLUENCES WILL^ CAUSE^ THE^ LOAD^ TO^ TIP^ THROUGH^ ANGLES OF .NCLINATION OF^ A^ HIGHER^ ORODR^ OF^ MAGNITUDE^ THAN THOSE DUE TO DYNAMICAL CONSIDERATIONS. (AUTHOR) (U)
UNCLASSIFIED /AO3,§
AD-t14 016 FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON (^) AF6 OHIO EXPERIMENTAL PROGNOSES OF AIRCRAFT BUMPINESS BY A DEFINED RICHARDSON CRITERION, (U) MAR A5 IP ZAVARINASM V. ;EMEL'YANOVAM. SZ. I
KEPT* NO. FTD-TT-64- MONITOR: TT , 69-619O
UNCLASSIFIED REPORT
SUPPLEMENTARY NOTE: UNEDITED^ ROUGH^ DRAFT^ TRANS.^ OF RUSSIAN MONO. MATERIALY NAUCHNO! KONFERENTSII PO AVIATSIONNOI METEOROLOGII,^ N.P.^ P9,-S^19603
IDENTIFICATION, USSR (Up
TRANSLATION OF^ RUSSIAN^ RESEARCH:^ EXPERIMENTAL PROGNOSES OF AIRCRAFT BUMPINESS BY A DEFINED RICHmRDSON CRITERION.
