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Here's the list' reports prepared fr~~gx;~~~ shows the thought you were listed tests. I but I was mistaken. as an author, NASA 1M X- 73925

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A COMPILATION OF RESEARCH REPORTS OF

.PHYSICAL RESEARCH DIVISION

DYNAMIC LOADS DIVISION

LOADS DIVISION

ACOUSTICS AND NOISE REDUCTION DIVISION

1921 1975

--- by ·-

Gloria R. Champine

July 1976

This Informal documentation medium is used to provide accel erated or special release of technical information to selected · users. The contents may not meet NASA formal editing and publication standards, may be re­vised, or may be incorporated· in another publication.

NI\SI\ National Aeronautics and Space Administration

Langley Research Center : Han:pton, Virginia 23665

,

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NASA TECHNICAL

MEMORANDUM NASA TM X- 73925

I

>< A COMPILATION OF RESEARCH REPORTS OF

.PHYSICAL RESEARCH DIVISION

DYNAMIC LOADS DIVISION

LOADS DIVISION

ACOUSTICS AND NOISE REDUCTION DIVISION

1921 1975

---by--

Gloria R. Champine

July 1976

This informal documentation medium is used to provide accel erated or special release of technical information to selected · users. The contents may not meet NASA formal editing and publ icat ion standards, may be re­vised, or may be incorporated ' in another publ ica t ion .

NI\S/\ National Aeronautics and Space Administration

Langley Research Center . Ha~pton . Virginia 23665

I

. " 1944

No III er 191.:.4

November 1944

I~ovember 1944

1941

Dece:r.ber 194.4.

Decenber 1944

December 1941

January 1945

JanUary 1945

J~"'1uary 1945

Ja.Yltlar.r 1945

Harch 194:S

- .) -

Plight Tests of Dive-~ecovery Flaps on an XP-51 Airplane, by De E. Be 21er cr.d ~'!alter C. lpTilliams

Accelerations and Bottom Pressures Eeasured on a B-24J Airplane in a Ditcn-ing Test, by Hargaret F. steiner

Variation of Hydrodyn~~c lrn?act Loads with Flight­Path k11g1e for a PrisITl.atic :float at 30 Trim and with a 22 1/20 Angle of D;:;ad Eise - Ted No. NACA 2401, by Sicney A. Batterson

Ditching Tests 1-lith a l/J.O-Size Nodel of the Army A-20A Air~la.11E. in Langley Tank Ho. 2 and on an Outdoor Cataplli. t, by George A. Jarvis a11d Hargaret F. Steiner

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/ Herno. Rept.

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Henn. Re~t.

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Nemo: Rent. I . I

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Proi':j..le:-Drag :. Heasurements on the XP-51 Airplane at Hemd. Rept. \ :

High Each Nu.rn.bsrs, by George Gerard and De . E. \1 Beeler / l/1)c/l / /'1 1,/ Y c; i

Ch..arts :for the Deter!J1ination of I'ling Torsional Stiffness Required .lor Spec:ii"ied 2011i..11g Characteristics or Aileron Reversal Speed, by " Henry A.. Pearson a11d ';'Jillia!il S. Aiken, "Jr.

Characteristics of Vertical Drai'ts and Associated Vertical-Gust Velocities Hii:.h:L'1 ConvEctive­Type Clouds, by A. 1. Nos~ovitz

Analysis of High-Speed-Flight Pressure Distributions by 2...11 Inverse Hethod Applicable to Incompressible Flol"l, by Philip J. Davis

Characteristics of Vertical Drafts a'1d Associated .. Vertical-Gust Velocities :'Tithin Convective-Type

.. Clouds, by A. I . Noskovitz

Frequency o f OGcurrence of Critical Gust Loads on Overloaded Airplanes, by Tb.oTIl.as D. Reisert

Partial Correlation of HodEl and i<Ull-Scale Ditching Perf ormance o f the B-24D Airpla..'1e, by Hargarct F. steiner

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Variation of' Hydrodyna,"'!ic Irrr:;.:act Loads Hith Flight- Re·st. BU. · Path Angle for a Pris:r.Jatic .noat at 30

Tri..TTl ~'1d ~dth J....S"A ~ a 22 1/20 Angle o f Dead ?cise, by Sidney A. Battc:rson ! i

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Theoretical and ExperL~ental Dyn~uic Loads for a Prismatic .l:"loat of 22 1/2u ~ead Itise - Ted No. NACA 2401~ by Hilbur L. }{ayo

Frequency of Occurre~~e of Critical Gust Loads on Overloaded Airplanes, by Thornas D. Reisert

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Barch 194)

April 1945

April 1945

April 1945

't 1945

\ may 1945

Hay 1945

Hay 1945

JlLl1e 1945

June 1945

July 1945

I'

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Variation of Hycrudyna.:'T1.ic Inpact Loads .·lith· F'light­p<:-t~ Anz1e 1'05 2. Pris~tic ~l~~t at 120 Tri!'l and Wl tn a 22 1/2 An:;..!...E 01 Deac ",..lSE, by Sidney A. Batterson

R:;p~.

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Ditching Tests '.-rith 1/.!-6-Si.~e l'~odels of the Ar!'l:v B-17 Hemo. ,

P.ept. Airpla.':.e in La,.""lg l.ey Tan:-:: ~;o. 2 a.'1C on an Outdoor Catapult, by Robert P. Tarshis and TheLma Stewart

Ditchi21g Tests 1-:ith a l/16-Size D:vnamic Hodel of the Army B-24 Airpla.l1e in Langley Ta.'L.1.c No. 2 and on an Outdoor CatapUlt, by IJ..oyd J. l''isher and l1argaret F. Steiner

An Ini'rared Cloud Indicator I - Analysis of Iru::rared-Radiation Excr.2.nge Hith Tables aDd Charts fqr Calibration of tte Cloud Indicator, by Calvin N. Har.field and R.obert L. Keni'Tler

Variation of HydrodYTI2..T71ic Impact Loads Hith Flight-Path ~l1g1e for a Frisr.4tic ?loat at 60 and 99

-Tr:lin a.l1d a 22 1/20 A..l1gle oi' Dead Rise - Ted No. NACA 2401, by Sidney A. Batterson a'1d Thelma SteHart

Flight Tests of Dive-Recovery Flaps on al1 XP-51 Airplane, by De E. Beeler Cl..i"ld Halter C. 1vi1lia."Tls

Flight Tests of Dive-Recovery it'.laps on ari XF-5l Airp1a'1e, by De E. Bee..Ler. al1d 1..Jalter C. Hillia."Tls

Action of the 1<1-1-2 Landi..l1g Gear at the:folding F.J-11ge Point During La-l1ding Ted No. NA.CA 2101, by l1argaret F. Steiner

Theoretical and ExperL'Tlenta1 Dynamic Loads for a PriST:1atic i<'loat Having an-Angle of Dead Rise of 22 1/20 , by "f:.Ji1bur L. Hayci

A..n. A..n.e.lysis of Life ~e~tancy o:f Airpla..'1e l-Jins-s . in Normal Cruising !"li=-,ht, "by Abbott A. Putna.."Tl

Airspeed F-Luctnations as a Heasure of Atmospheric Turbulence, by H. B: Tolefson

HeasDTements of Atmospheric 'Turbulence 1-lith AAi B-25D Airpla'1e Ho. 3666, by H. B. Tolefson

A -j,... Technical Service COr.:;-;'..and, Pxrr:y Air !:brces~ Sp2..:.'1 Load 2Jistrib"l.;.tions iOor FYoject ro7.:-553, by Hen:'Y A. Pearson and Cloyce E. ~/Iatheny

Theoretical a'1c Ezperirr.sntal =tv.nar.ic Loads for a Pri0P.atic Float Hav;'1 ,o an A-'1-le 01.- Dead Rise of 22 l/2°, by ~·!i1tn.:r - L. lIayo

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July 1945

July 194)

July 1945

July 1945

July 1945

August 1945

August 1-945

August 1945

November 1945

November 1945

Harch 1.946

November 1945

October 1945

/'

1945

February 1946

- 7 - u Airspsed PluctUCltioC1S as a HEaS1.lI'S OI' AtmosphE.ric

Turbulence, by H. B. To~elson

.An Analysis of Li1'e :2;::cscta"'1C;-{ 0': Airpl2..!1e Hin,s in Normal Cruisj.n: F1i=-h:t~ by Abcott A. Putnar:1

Comparison Behleen Ca.i.cUJ.ated a'1G. HsasU!'E.d Loads on i.tJin.s and Hor:i_zontal Tai-L in Pull-Up Haneuvers, by Cloyce E. HathEI!Y'

Analysis of V-G Reco:,d TIc.r:.oved }iTom E-IJO Airplane NC-147l6 ltbl~01,riJlg AcciciEnt:at Port-oi'-Spain, Trinidad Jal1uary ti, 1.945; by Richard V. Pllode

Statistical Analysis oi' the Cr.aracteristics of Repeated Gusts in TurbuJ.ent Air, by A. I. Nds'r~ovitz al1d A. H. PEiser

Impact Destruction Test oi' SC-l Auxiliary li'~oat Ted No. NACA 24l.3. 2, by VincEnt G. Redmond

Anal.ysis 01' the Effect 01" ?...o~l ing ?-l1l1-Outs on the Hil1g and Aileron I.oads OI a Fighter Air­plane, by Henry A. Pearson al'1d tJi11ianLS. A:Lk:En, Jr. ,

Standard Nomenclature ior Airspeeds Ttiith Tables and Chftr-!:,s for use :Ll1 C?~culation of Airspeed, by Hil1iarn.. S. Ai}:en, Jr.

Statistical Analysis of th9 Characteristics of REpeated Gusts in 'J.'urbulent Air, by A. 1-Hoskovitz and A. H. Peiser

,Analy'sis of ITli'rareG-?.adiation Exch;:ongE "lith Tables a.l'1d Chart ior Calibration oj.' the C~oud Inc.icator, by Calv:LTl l'l. ~>Jariield and RobErt L. Ken.irr.er

ArlaJ..~'T5is OI' Ei".:L"€ct oi' TI.oD:L.-:g [Jo.tl..U..-CrJ.ts ari ~.5ng -and Aileron Loads o i.' a '.r<'i;hter Airplane, by Henry A. Pearson anQ ~'lilliarn S. ,Aiken, Jr.

A Hethod oi' Analysis oi 'iJ--G Hecords From TransDort Operations, by A. H. Peiser and H. l-Tilkerson

Some Flight Heas1ITeI'l€nts oi' Pre:::sure Distribution During Tail Buf'i'etiTlg-, by Jor.::n Boshar

1:!a:-:e Eeasllrements Bet..; !ld XP-3l Airplane :in ~'ast

C-Erard

a :'J--:rcg SEction 01" the ~iVES, by De E. BeEler

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Hemo. Rept.

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Variation 01.' Eyc.rooj-!12.,"":1.ic kpact I.oads -with ~'lig-nt- nest. BlJ1.

Path Ang-lc i"or a I'ri:::;:-:.2.tic :r'..Loat at 60 a!!C yO Tri..>n 1-5K"l and a 22 1/20 Ar,C..LC2 o.!. :::Jead ?,i SE, b:,~ .Bat"!:,el'so.!:. ar.d lStc~'ja~

" . . } 'eb~ary 1946 Vari~tion of Hycirod:ma"ric .J.r.:,=,ac"(, .L02.CS "rith f .lifht­

?a-:h An; l e for a ?ris::-..at :.c' l,'loat at 120 TrL':l 2...'1:1 Hit:, a 22 1/20 A.. ...... ~ ..!.. e 0:' Jeac ]iS2, by SidnEY A. Bat'Gerson

A..11 Anal;:,-sis oi' the .:<"atisue Lii'e 0:::-' an Airpla.l1C ":lir..g St~ucture Unde r Overload Conditions, by Abbott A. Futnan a.'1G Thor-.as J. 2e isErt

Anal:,'sis of 17 -G 2.ecor ds ,r'rOTIl "-,he S~JJ -4 Airpla..."1e, by H. W~l:erson cmo S. A. 3ennett

Landing Tests 01 a B-2 4D A -i s-lane to Deterrnine ' the Time Historie s 0':" the Impact .i<'orces and the Horizonta-Tail Loads, by Joh..TJ. R. Hesti'a11

.An Application 0 1 Statistical Data in the DeVelOD­Inent oi' Gust-Load Criteria, by Reginald B. Bland and T. D. Reisert

Accuracy of Airspe~d l1eas1.lI'ements and Flight Calibration Procedui-es, by Td-i !ber B. Huston

Variation of Hydro dYT'!2J7'.:ic Impact Loads lTith Flight­Path Angle f or a PriST."2.tic ,float at cP and -30

Trim and lvith a 22 1/20 Angle oi' Dead Rise - Ted }!o. NACA::~ 2401, by SidneX A. Batterson

Flight Heasurements by 'larious l.l-1ethods of the Drag Characteristics)ol the X?-5l Airplane, by Henry A. Pearson and Do~o-:hy ~. Beadle

l1eteorological Conditions Associated 1·rith Plight J1easure.ments of Atr..ospheric 'l'm'bulence, by B. B. HeJ...:L'and

Analysis o i ' V-G Records from the SHB-l Airp1ane, by ~'Jalter G. ~vall~er and Ha.;:.r T. }Ieadolfs

A The oretical Investigation of HJurodynamic ~pact Loads on Scalloped-Bottom Seapla...l1es and Comparisons with E:cperiment Ted 1';0. NACA 2413 • .L, by BEnjaJnin Hil:~ritzl~

Hydrodynamc Impact Loads and Pressure Distributions on a Scalloped-Bottom L-53 l"loat - Ted No. HACA 2413.1, by Danie.i Savits~:y

An .'inalysis of the TTlc.ications of the Universi'ty of Chicago Airoorne ~b~ence Indicator in o~sty Air, by H. B. To.Leison ~d K. G. Pratt

All Anal~rsis 01' Airs~eeds and. Each EUT.1oers Attair..ed by ioc~~hesd Cor..ste.!.latior:. Air?J..a."'!es ill Tra.r. s _ Atla..,tic O~Eratiur. !)-~1Tin~ the S:;rin~ of 194(;, by ?oy Steiner ano A. I,j. Eeissr

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1946

A ue;ust 1946

August 1946

September 1946

October 1946

-October 1946

1947 \

- 9 -

Solu'c~CJns .{or HydrodYYl2.J:'.iC Irr:?2.ct i'o r c e: and Res Donse 01' a 'I\iO-Ea3s S:"'S~ €r:1 2.r.d A~pJ.ic ation to 211 ilastic A~i·re.rne , b y Hi.lo'.:.r i.,. Ea::D

Evaluatiun of Gust and ~.:'ai't Ve ..!..ocitie s from YJ..ights oi' P - 61c Airplane s ~-Ji thi....'1 Thunderstorms , by Harold B. Toleison

Investigation of t !1e Characteristics of a High-. Aspect-? atio Hins ; n the Lang.le:T 8-Foot High­Speed Tu_nnel, b y Ric!>..2.I'd T. ~,rni tcorrtb

'k'later Loads on the XJ.L,-l Hull as Obtained in La....1! gley Impact Basin; by Eargaret 1<'. Steiner and Rob ert '-II. HiLLer

Ef.fect of Nach Number on the Naximmn Lift and BU .. {f e tir;.g Boundary Det eTI'li..'leci in io·J..ight . on a No:l1th A.~erica..71 p-5m Airplane, b y Jofu"l. P. Hayer

Eva..luation of Gust "md Draf t ITrights oi' P...;6lc Air':J~ar!es by H. B. Tole.i'son

Evaluation oi' Gust 2.J.'"1d Dr ait Flights of P-61c Air~lane s by H. B. To l eison

Velocities From

Velocities :from Hithin Thunr,:; Grstorns.

Evaluation of Gust ar!d Dra f t Velocities from Flights .. of P-6lc Airpl..ar!es ~'!ithin Thunderstorrr.s, by H.B. Tolefson

Eva..Luation of Gust ~d Jr att TJelocit-i·es from Flights oi'- ?-61c Ai....-plar..es ~'Jith:ir: T:hu.r..derstorrns, b~~ . H. B. Tolet'son"

PreliTrinary Analysis of ~r.J\CA !1easurements of 'Atmos­pheric TurbulenCE ~-Jit[-.J.....71 a Tn-lmderstorm - U.· s. Ueather Bureau Thunderstorm Project, by H. B • . Tolefson

'Air-PloH Behavior Over the I'ling of: an XP-51 Airplane as Indicated b y Ui...'l g;:;.Suriace Tufts at Subcritical and Supercriticai Speeds, by De E. Beeler

A Conp2rison of Tr.ree T:"1eorET.:ical Hethods cDI Cal­culat;ng Sp a.."1 load Distr~olltion en SHept ~.Jings, by Nicholas H. Va.'"1 Ibm and John .DeYoung

An A;nalysis oi' Airspeeds and Each IJ1.L':loers Attained by Loc~:heed Cor.steiJ..ation Airplanes in TJ:'aIlscon­ti....TJ.er!t2.1 O':Js r2 .. t i ons I;'\IT; "1E.; the 2.rly Summ~r of 191..;6, by Poy Ste; ner

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