B I B LI 00 RAP lIT

BIBLIOGRAPHY

I. BOOKS

ARKIN H. andCOLTON R. R. (1940) Graphs,how to makeand use them (5thEd.) NewYork & London

BARRETT C. S. (1943) Structureof MetalsNew York.BLOM G. (1958) StatisticalEstimatesand TransformedBeta-variablesStockholm.BOWDEN F. P. and TABOR D. (1954) The Friction and Lubrication of SolidsRev. ed.,

New York.BROWNLEE K. A. (1949) IndustrialExperimentationLondon.CASEY R. S. and PERRY J. W. (1958) Punchedcards, their applicationsto Scienceand

InefustryNew York.CAZAUD R. (1948) Lafatiguedes Me’tauxParis.

(1953)FatigueofMetals(translated by PennerA.J.) New York & London.COCHRAN W. G. (1953) SamplingTechniquesNew York.COCHRAS.I W. G. and Cox G. M. (1950) ExperimentalDesignsNew York.CRAM~aH. (1945) MathematicalMethodsof StatisticsUppsala.DAVIES 0. L. (1954) The Designand Analysis of Industrial ExperimentsEdinburgh&

London.DAVIS H. E., TROXELL G. E. and WISKOCIL C. T. (1955) The Testingand Inspection

of EngineeringMaterials (2nd. Ed.) NewYork.DIXON W. J. and MASSEY F. J. (1951) Introduction to StatisticalAnalysis (2nd Ed.)

New York.FINNEY D.J. (1955) ExperimentalDesign and its StatisticalBasis Chicago.

(1952) Probit Analysis (2nd Ed.) London.FISHER R. A. (1951) The Design of ExperimentsEdinburgh & London.

(1954) Statistical Methodsfor ResearchWorkers (12thEd.) Edinburgh & London.Fox L. (1956) The Use andConstructionof MathematicalTables London.FbPPL 0., BECKER E. andHEYDENKAMPr G.V. (1929)DieDauerprufungo’er Werkstoffe

Berlin.G0UGH H. J. (1924) The Fatigueof MetalsLondon.

(1926) TheFatigueof MetalsLondon.GuA.s’ 0. (1929) DieDauerfestigkeito’er Werkstoffeundo’er KonstruktionselementeBerlin.

GROVERH. J.,GORDON S. A. andJACKSON L. R. (1954)FatigueofMetalsand StructuresWashington.

GUMBEL E.J. (1958) Statisticsof ExtremesNewYork.HALD A. (1953)Statistical Theorywith EngineeringApplicationsNew York.HEMPEL M. andFINK K. (1952) Grundlagenund AnwendungdesDehnungsmess-strejfens

Düsseldorf.HEROLD W. (1934) Die Wechselftstigkeitmetallischer Werkstoffe, ihre Bestimmungund

AnwendungWien.JURGENSMEYER W. (1937) Die WilizIagerBerlin.KAPP R. 0. (1948) The Presentationof TechnicalInformation London.KEMPTSIORNE 0. (1952) The Design and AnalysisofExperimentsNewYork.LEHR E. (1931) SchwingungstechnikBerlin.LESSELLS J. M. (1954) Strengthand Resistanceof MetalsNew York.LEvY P. (1953) RandomFunctionsBerkeley, Calif.LIPsoN C., NOLL G. C. and CLOCK L. S. (1950) Stressand Strengthof Manufactured

Parts New York.

LOCATI L. (1950)Lafatica dci nlateriali metallici Milano.

MASen J. Y. (1954) Bibliography on the Fatigue of Iviaterials, Componentsand StructuresMelbourne.

MOOD A. M. (1950) Introduction to the Theoryof StatisticsNewYork.MOORE H. F. (1927) Manualof Enduranceof Metals underRepeatedStress. A summary

of views and test data, with instructionsfor use. Gonzpiledfor designing, inspectingandtestingengineersNew York.

MOORE H. F. and KOMMERS J. B. (1927) TheFatigueofMetalsNew York.MOORE H. F. andMOoRE M. B. (1953) Textbookofthe MaterialsofEngineering(8thEd.)

New York.NEUBER H. (1946) Theory of Notch Stresses: Principlesfor exactstress calculation Ann

Arbor, Mich.NIELSEN K. L. (1956) Methodsin NumericalAnalysisNewYork.OWENJ. B. B. (1943) Reviewofthe Testingof StructuresNewYork.PERTZ H. (1928) Die Bestimmungo’er Baustoffdampfungnachdem Verdrehungs-Ausschwing-

verfahrenBraunschweig.PETERSON R. E. (1953) StressConcentrationDesignFactors NewYork.PFLIER P. M. (1940) ElektrischeMessungmechanischerGrössenBerlin.ROBERTS H. C. (1946) MechanicalMeasurementsby Electrical MethodsPittsburgh.SMITH G. V. (1944) Propertiesof Metalsat Elevated TemperaturesNew York.SMITH W. A., KENT F. L. andSTRATTON 0. B. (1952) World List ofScient(tic Periodicals

1900—1950London.SNEDECOR G. W. (1950)StatisticalMethods(4th Ed.) Ames, Iowa.TEED P. L. (1950) The Propertiesof MetallicMaterials at Low TemperaturesNew York.TIMOSHENKO S. (1956) Strengthof Materials (3rd. Ed.) New York.TOLANSKY 5. (1948) Multiple BeamInterferometryofSurfacesandFilms New York.VILLARS D. 5. (1951) Statistical Design and Analysis of Experimentsfor Development

ResearchDubuque,Iowa.VAN DER WAERDEN B. L. (1957) MathematischeStatistikBerlin.WOLD H. (1952) DemandAnalysis Stockholm.WORTHING A. G. and GEFPNERJ. (1948) Treatmentof ExperimentalData New York.v. ZEERLEDER A. (1930) 50 Jahre EMPA Zurich Zurich.

II. TABLES

Army Ordnance Corps, (1952) TablesoftheCumulativeBinomialProbabilitiesWashington.FISHER R. A. and~YATESF. (1943) Statistical Tables (2ndEd.) Edinburgh& London.Harvard University, Staff of the ComputationLaboratory, (1955): Tables of the

CumulativeBinomial l’robabilitv Distribution Cambridge,U.S.A.HALD A. (1952) Statistical Tables andFormulasNew York.KENDALL M. G. and BAnOINGTON SMITH B. (1940) TablesofRandomSamplingNumbers

Tracts for computers, no. 24.LIEBLE5N J. and SALZER H. E. (1957) Table of the First Momentof RankedExtremes

J. Res.N.B.S.59, 203—206.LdscII-SCH0uLIK (1951) Die Fakult/it (Ganmnsafunktionen)und verwandle Funktionen

Leipzig.MILLER J. C. P. (1954) TableofBinomial Coefficients.Royal Soc.Math. Tables,vol. 3,

New York.MILLER L. H. (1956) Tableof Percentage Points of Kolmogorov Statistics. J. Amer.

Stat. Ass., 51, 111—121.NAIR K. R. (1940) Table of ConfidenceInterval for the Median in Samples from

any Continuous Population. Sankhya,4, 551—558.

250 251

BIBLIOGRAPHY BIBLIOGRAPHY

National Bureauof Standards,(1941): Tablesof Probability functionsVols. I, II.MathematicalTables8, Washington.

National Bureau of Standards, (l953a): Probability Tables for the Analysis ofExtreme-Valuedata. Washington.

National Bureauof StaDdards,(1953b): Tablesof Normal Probability Functions(3rd Ed.) Washington.

PEARSON K. (1922) Tablesof the Incomplete T-function CambridgeUniversity Press.PEARsON K. (1932) Tables of IncompleteBeta Function CambridgeUniversity Press.Rand Corporation (1935) A Million RandomDigits with 100,000 Normal Deviates

Glencoe, Ill.SMITH R. W. JR. and EDWARDS H. E. (1953) Table of the IncompleteBetafunctisn

(f,p,g) Pittsburgh.TEICMROEW D. (1956) “Tables of ExpectedValues of Order StatisticsandProducts

of Order Statistics for Samplesof Size Twenty and less from the NormalDistribution”. Ann. Math.Stat.27, 410—426.

TsPs’En L. H. C. (1927) “Random Sampling Numbers”. Tractsfor computersno. 15.

WsLCoxoN F. (1947) “Probability Tablesfor Individual Comparisons by RankingMethods.”Biometrisa3, 119—122

HI. PAPERS

A

AITCHI5ON L. andJoMNsoNL. W. (1925) Theeffect of grainuponthefatiguestrengthof steelsJ. Iron St Inst. 3, 351—378. 61.2; 61.8

AITKEN A. C. (1935) On least squaresand linear combination of observationsProc. Roy. Soc.Edinb. 55, 42—48. 90.41

ALLEN N. P. andFORRESTP. G. (1956) The influenceof temperatureon thefatigueof metalsLondon Conf., Session4. Paper1. 32.2;64.5; 65.1

ALMEN J. 0. (1943) Peenedsurfacesimprove enduranceof machine Parts MetalProgr. (Feb.) 209. 61.5

(1950) Fatigueweaknessof surfaceSProd. Engng.21, 118—140. 61.8(1951a) Fatiguefailuresare tensilefailuresProd. Engng.22, 102—123. 61.8(1951b) Fatiguedurability of prestressedscrewthreadsProd. Engng.22. 61.5(195Ic) Fatigue—Lossandgainby electroplatingProd. Engng.22. 63.5(195ld) TorsionalfatiguefailuresPartI andII. Prod. Engng.22, 167—182. 62.4

AMATULLY A. andHENRY 0. H. (1938) Fatigue testsof welds atelevatedtempera-tures Weld. .1., Easton,Pa 17, l4s—20s. 32.2

ANDREWI H. J. and HOLT M. (1945) Fatigue tests on 1/8-inchaluminumalloy rivetsNACATN 971. 54.2

ATKINsON R.J. (1950) Permissible design values and variability test factors Aero. Res.

Counc.Lond. Rep.Mem. no. 2877; AMR 9, Rev. 443. 64.5AT5UM5 A. (1958) Stressconcentrationsin a strip under tensionand containingan

infinite row of semicircularnotchesQuart. J. Meeh.(Nov.), 478—490; mt. aero.abstr.4 (1), 15. 63.3

AUOMTIE F. (1931) Phil. Mag. Series7, 1, 517. 34.1AUONTIE F. and CoxH. L. (1935) A new typeof fatigue testing machine, A.R.C.,

R. & M., No. 1880. 34.1B

BAILEY A.J.andCOURTNEY-PRATTJ. S. (1955)Proc. Roy.Soc. A227,500-515 45.3BAILEY R. (1946) Aluminum alloy 75S-T. Effect of machinalsurfacefinisheson

fatigue life, ConvairCVAC ReportNo. 4809. 63.4

BA5LET R. W. (1956) Usefulnessand role of repeatedstrain testing as an aid toengineeringdesignandpractice,LondonConf., Session2, Paper14. 28.1

BA5E5row L. (1909) The elasticlimits of iron andsteelundercyclical variationsofstress Phil. Trans.210A,35—55. 95.0

(1910) The elasticlimits of iron and steelunder cyclic variationsof stressPhil.Trans. 210A. 95.0

(1911)Formof theS-NcurveProc.Instn. Mech.Engrs.,Land.Pt.s.3-4, 919-924. 82.1BALL L. M. (1945) Strain gage techniqueProc. Soc. Exp. StressAnal. 3 (1), 1-22

34.3; 42.21BALLET M. and SALMON-LEOACNEUR C. (1954) Sur l’utilisation de l’aralrIite en

figeagedescontraintes,Cong.Photoelast.& Photoplast.,Brussels. 44.1BANKS L. B. (1950) Machinefor testing rails in bendingfatigue Engineering,Lond.

169 (4400), 585—587; AMR 4, Rev. 1172. 31.23; 33.4BARON F. andLARsON E. W. JR. (1952) Theeffect of grip on thefatiguestrengthof

rivetedandboltedjoints Bull. Amer.Rly. Engng.Ass.54 (503), 175—190; AMR6,Rev. 1562. 64.2

BARTLETT M. 5. (1945)J. Roy. Statist.Soc. (Supplement)8, 113-117 90.1(1947) The useof transformationsBiometrics3, 39—52. 90.1(1949) Fitting a straight line when both variablesaresubject to errorBiometrics5, 207—212. 90.4

BA5QUIN 0. H. (1910) The exponentiallaw of endurancetestsProc. Amer.Soc. Test.Mater. 10, 625—630. 85.1

BA5TENAIEE F. (1957) DistributionsItatistiquesdesduréedcvie a Ia fatigue etformedela courbedeWtshler C.R.,245, 136—139. 83.2; 85.1

BAT5ON R. G. C. andBEADLETJ. (1931) Fatiguestrengthof carbon-andalloy-steelplatesasusedfor laminatedsprings. Proc. .1. Meeh. Engrs.120, 301—316. 33.2

BECEER A. (1949) Elektrisches Mehrfach-Schaltzalslwerkzur Steuerung vonBelastungsprogrambci Betriebsfestigkeits-VersuchenFeinw. Tech. 53 (7),189—193. 31.13; 32.4

(1950a) Last-Steuerautomatenfur Bauteil-Prufmaschinenmit selbstthtigemVersuchsablaufZ. 1/er. Dtsch.Ing. 92, 266—271. 31.3; 32.4

(1 950b) SchaltzahlwerkeArch. Tech.Messen170, T29—T30. 34.5BEDFORD G. M. (1956) Reviewof thecurrentmachinesystemsfor handlinginforma-

tion AGARD Rep.46; Index aero2/14/5. Bibl.BEacsslNoR. andNscssoLLsW. (1948) A theoreticaldiscussionof pittingfailures in

gearsProc. Iustn. Meeh. Engrs.,Lond. 158, 317. 62.7BELYAEv N. M. (1951) Laboratory exercisesiss strengthof nsaterials(Russian),

Moscow-Leningrad,Gosud.fed. 1’ekls.; AMR 7, Rev. 798. 20; 30BENAED A. and Bos-LEvENuAcss E. 1). (1953) The plotting of observationson

probability paperStatistisa7, 163. 83.0; 90.3BENDA E. K. and GAlLANT R. A. (1954) An automaticload control for fatigue test

cquipnsentProc. Soc.Esp. StressAnal. 12 (1), 209—214; AMR 8, Rev.3082.31.23; 32.4; 34.4

BENNETT J. A. (1944) Early detection of cracks resulting from fatigue stressingNACA RB 4115 (WR W-78). 46.0

(1945) Effect of fatigue-stressingshortof failure on sometypical aircraft metalsNACA TN 992. 24.2

(1946) A study of the damagingeffect of fatigue stressingon X4130steel Proc.Amer. Soc. Test. Mater. 46, 693—714. 24.6; 63.3

(1956) The distinction betweenimitation and propagationof a fatigue crackLondon Conf., Senion6. Paper8. 27.0

252 253

BIBLIOGRAPHY BIBLIOGRAPHY

BENNETTJ. A. and BAKERJ. L. (1950) Effectsofprior static anddynamicstressesonthe fatiguestrengthof aluminium alloys J. Res. Nat. Bur. Stand.45, 449—457;AMR 4, Rev. 2506. 24.1; 51.2; 61.7; 85.1; 92.1

BERG5. (1941)ZumTecknikdesSchwingversuchesZ. Ver.Dtsch.Ing.85, 605—608 20BERNERandKA5TRON (1938) Influence of thedirectionof fiber on the resistanceto

thefatigueof anAl-Cu-Mg alloy Luftwissen. 61.8BERNHARD R. K. (1937) Proc. Amer. Soc. Test. Mater. 37, 634. 31.23BEasosmIN M. L. (1949) Maschine zur Prufung auf Wechselfestigkeitbei hohen

Temperaturen15(4), 497—500. Saw. Labor., 15. 32.2BLA5ER R. U., TUCKER J. T., JR. andK00I5TEA L. F. (1952) Biaxial fatigue testson

flat-platespecimensWeld.Res.Suppl. 17 (3) l6ls—168s; AMR 5, Rev. 3416.62.6

BLEAKNET W. M. (1938) Fatigue testingof beamsby the resonancemethodNACATN 660. 31.24; 33.4; 33.5

BLIssC.J.(1935a)Estimatingthedosage-mortalitycurveJ.Econ.Ent. 28, 23.11; 95.0(l935b) The calculation of the dosage-mortalitycurve Ann. Appl. Biol. 22,

134—167. 23.11; 95.0(1935c) The comparisonof dosage-mortalitydata Ann. Appl. Biol. 22, 307—333.

23.11; 95.0(1937) The calculationof the time mortality curveAnn. AppI. Bisl. 24, 8 15—852.

23.11; 95.0BLOM G. (1956) Onlinear estimateswith nearlyminimum varianceArk. Mat. 3 (31),

365—369. 90.43; 93.0; 94.1BonuszEwsez0. and SpArix W. (1928) Die SchnellbestimmungderDauerwechscl-

festigkeit Arch. Eisenhuttenw.2 (4), 249—255; Stahl u. Eisen,Düsseldorf48 (43),1505—1506. 26.3; 31.44

BOLLENRATB F. (1938) Zeit-und Dauerfestigkeitder WerkstoffeJb. Dtsch.Lufifahrtf.147—157. 24.1; 61.7

BOLLENRATH F. and CoarcELrnsH. (1938) Zeit- und Dauerfestigkeitungeschweister

und StumpfgeschweisterCr-Mo Stahlrohrebei verschiedenenZugmittelspan-nussgen.Jb. Dtsch. Lufifahrtf Pt. 1, 549—553. 62.1

(1940) DerEinflussvon BetriebspausenaufZeit undDauerfestigkeitmetallischerWerkstoffeZ. Ver. Dtsch.Ing. 84, 295—299. 66.3

(1942/43) Die Ermittlung der Schadenslinievon Stahl Arch. Eisenhuttenw.16,49—56. 24.2

BOLLENEATM F., CORNELIUS H. and SIEDENBURGW. (1938) Influence of the cross-sectionalshapeon thefatiguestrengthof soft ingot steel (in German),Lufifohrt-farsch. 15, 214—217. 63.2

BooNE W. D. andWI5HAET H. B. (1935) High-speedfatigue testsof severalferrous

and non-ferrousmetals at low temperatureProc. Amer. Soc. Test. M’nter. 35,Pt. 2, 147—155. 65.1

BORE C. L. (1956) The presentationof fatigue data for fatigue life calculationsJ.R. Aero.Soc.60, (545), 331—346; Index aero. 130/12/6. 82.1

BORE5I A. P. and DOLAN T. J. (1953) An appraisalof the Prot methodof fatiguetestingUniv. Ill., Tech.Rep.34. 23.22; 96.2

BOWDEN F. P. (1956) Methods of studying the surfacestructure of solids J. ColloidSci. 11, 555—564. 45.0

BowsassC. E. (1955) Studiesof the biaxial fatigue propertiesof pressurevesselsteelsWeld.J., Land. 55 (1), 51s—59s. 62.6

BowM~C. E. and DOLAN T. J. (1953) Biaxial fatigue propertiesof pressurevesselsteelsWeld.J., Loud. 32 (11), 529s—537s;AMR 7, Rev. 2856. 62.6

BOYEE H. E. (1948)Effectsof grinding on physicalpropertiesof hardenedsteelpartsTrans. Amer. Soc. Metals40, 491. 61.4; 63.4

BRAD5HAW W. H. (1945) Standardfatigue testerfor useby the rayonmanufacturersBull. Amer. Soc. Test. Mat. (136), 13—16. 33.1

BRAND L. (1957) Erfahrungenmit RisstiefenmessernStahl u. Eiseu,Düsseldorf77,Pt. 1(9), 576—581; Index nero. 154/14/1. 46.2

BRODRICR R. F., KURIRALLA A. A. and BABCOCK L. E. (1956) A new resonantfatigue testing machinefor reversedbending (In preparation). 32.4

BROWN R. L. EssenceofdesignofexperimentsAMR 8, No. 10,Featurearticle. 71.0BROWN R. W. (1947) Stressanalysisutilization in dynamic testingProc. Soc. Esp.

StressAnal. 4 (2), 42—51. 33.5BROWNLEE K. A., HODGES J. L. and RO5ENBLATT M. (1953) The up-and-down

methodwith small samplesJ. Amer. statist. Ass.48, 262—277. 23.12; 95.0BEUDERE. (1943) MaschinezurErzeugungsynchroner,kombinierterBiege-Verdreh-

DauerbeanspruchungenZ. Ver. Dtsch.lug. 87, 82—92. 31.51BRUEGGEMAN \V. C., KEUPEN P. and Rno~F. C. (1944) Axial fatigue testsof 10

airplane wing-beamspecimensby the resonancemethod NACA TN 959.31.24; 33.5

p BKUEGGEMAN W. C. and MAYER M. JR. (1944) Guidesfor preventingbuckling inaxial fatigue testsof thin sheet-metalspecimensNACA TN 931. 34.2

(1948)Axial fatigue testsatzeromeanstressof 24S-Tand755-Taluminum-alloystripswith a centralcircular holeNACA TN 1611; AMR 1, Rev. 1481. 34.2

BRUEGGEHAN W. C., MAYER M. andSMITH W. H. (1944) Axial fatigue testsat zeromeassstressof 245-1’ aluminum alloy sheetwith and without a circular holeNACA TN 955. 63.3

(1945) Axial fatigue tests at two stressamplitudes of 0~032-inch24S-T sheetspecimenswith circularholesNACA TN 983. 24.2

BEUTON R. A., COHEN H. L. and Hiun P. R. (1956) The developmentof a randomload controller for fatigue testingfull-scalestructuresARL, Melbourn,SM Rep.(In preparation). 32.4

BUCHANAN J. G. and THUR5TONR. C. A. (1956) The measurementof crack depthsby the direct-currentconductionmethod Non-Destr. Test. 14, (5) 36—39; Indexacm. 121/12/12. 27; 46.2

BUcEINGNAM E. (1944) Surfacefatigue of plastic materials Trans. Amer.Soc. Meeh.Eugrs. 66 (4), 297—310. 32.5

BUcKWALTER T. V. and HOEUER 0. J. (1937) Investigation of fatigue strengthofaxles, press-fits,surfacerolling and effect of size Trans. Anser. Soc. Metals 25,229—2 II 61.5; 61.6

Buno C. B. and LARETeK L. (1945) Statisticalcomparisonof rayon tire cord fatiguetestingrnaclsinesBull. Amer.Soc. Test. Mat. (136), 19—25. 33.1

BULLEN F. P., HEAD A. K. and WoonW. A. (1953) Structural changesduring thefatigueof metalsProc. Roy. Soc. 216, 332. 61.7

BUNnY R. W. and MAEIN J. (1954) Fatigue strengthof l4S-T4 aluminum alloysubjectedto biaxial stressesProc. Amer.Soc. Test. Mater. 54, 755—768 31.6; 626

BUNnAEDT K. (1938)Dynamicstrengthpropertiesof light alloys at low temperatures(In German) Z. MetallIc. 30 (7), 235—237. 65.1

BU5EMANN A. (1925) Die Dampfungsfhhigkeit von Eisen Dr.-Ing.-Diss., T. H.Braunsehweig. 31.41

BUNYAN T. W. and ATT5A H. H. (1953) Investigationof the effect of fillet radii onthe torsional fatiguestrengthof marine shafting. Instn. Engineers& Ship-builders in Scotland,425—492. 63.3

254 255

BIBLIOGRAPHY

BUTLER R. H., BEAR H. R. and CARTER T. L. (1957) Effect of fiber orientationonball failuresunderrolling-contactconditionsNACA TN 3933. 32.5; 61.8

BUHLER H. (1952) Determinationof residualstressesin finishedpieces(in German)Arch. Eiseahtittenw.23 (7/8), 293—297; AMR 6, Rev. 1264. 63.5

BOMME W. (1958) Non-destructivetestingof aluminium work-piecesby ultrasonics(In German). Aluminium,Düsseldorf, 34 (4), 200—205; Index aero. 115/14/7.

46.5

C

CAMP B. H. (1951) Approximation to the point binomial Assu. Math. Statist. 22,130—131. 90.3

CARL R. A. and WEGENG T. J. (1954) Investigationsconcerning the fatigue ofaircraft structuresASTM, Ann. Meeting,No. 68. 25.1

CARTER T. L. (1958) Effect of fibre orientationin racesand balls under rolling-contactfatigue conditionsNACA TN 4216; Index aero. 163/14/5. 61.8

CARTER B. C., SMANNON J. F. and FOR5NAwJ. R. (1945) Measurementof dis-placementand strain by capacitymethodsProc. Inst. Meeh.Eugrs., Loud. 152,215—221. 43.22

TEN CATE (1949) Extensionof program for fatigue test on wing SIl N. V. FokkerRapp.No. P-ll-527b. 25.1

CAEAUD R. (1934) Metal fatigueand methodsfor its measurementJ. Aero. Sri. 1,137—143. 20.0

CAEAUD R. (1949)La résistancea lafatiguedesaciersTech. Mod. 41, 377—384. 60.0(1950) La forme despiècesdemachineset la tenuea lafatigueProt. Industr. Méc.33, 35—40, 67—74. 63.2

(1952) Contributiona l’étude de l’effet de dimensiondans lesessaisdefatiguedes metaux. Résultats statistiques VI° Convegnn Nazionale AIM, Genova.

63.2(1953)Contributiona l’étudestatistiquedeladispersiondanslesessaisdeflexionrotativeRes.Métall. 50, 291—298. 92.0

(1956) Fatiguefailure and serviceexperiencewith particular reference to theshapeof the part London Conf., Session7. Paper3. 28.1

CHADWIcK R. (1954) Designstressesin light alloy rolling stock Engineering,Land.178, 43. 62.3

CHERNOPF H. andL5RBEEMAN G.J. (1954) Use of normalprobability paperJ. Amer.Statist. Ass. 49, 778. 83.0; 90.3

(1956) The use of generalizedprobability paperfor continuous distributionsAnn. Math.Statist. 27, 806—818. 83.0

CNOQURT A. (1954) Effectof prestressingon fatiguestrengthof spot-weldedstainlesssteelsWeldJ.A. (10), 509s—523s. 24.2

CssoDoaowssuW. T. (1956) Fatiguestrengthin shearof analloy steelLondonConf.,Session2. Paper6. 31.4; 31.6; 34.2; 34.3; 62.4

Cssstss’rOLE. (1937) Fatigue tests (in French)Artset Met. 91, 173—183. 20.0Cz.

4&pp V. W. (1956) Operational problemsrequiring docunsentationresearch.AGARD Rep.48; Index acm. 1/14/5. Bibl.

CLAYDON D. CL W. (1958) Instrumentationin ultrasonicflaw detectionJ. Inst. Met.86, (6), 241—251; Index aero. 155/14/4. 46.5

CLAYTON-CAVE J., TAYLOR R.J. and INE50N E. (1955) Reproducibilityof Wöhler-type fatigue testJ. Iran St. Inst. 180, Pt. 2, 161—169;AMR 9, Rev.457. 64.5

CLEDwYN-DAvIES D. N. (1954) The effect of grinding on the fatigue strengthofsteelsInstn. mech.Engrs.3—11; AMR8, Rev. 1030 63.4

BIBLIOGRAPHY

COATE5R. C. andPOFEJ.A. (1956) Fatiguetestingof compression-typecoil springsLondon Conf., Session7. Paper6. 33.2; 34.4; 36.0; 62.4; 63.5

CoFFIN L. F. (1 954a) A study of the effects of cyclic thermal stresseson a ductilemetal Trans.Amer.Soc. Mech.Eugrs.76, 931—950. 32.2

(1 954b) The problemof thermal stressfatigue in austenitic steelsat elevatedtemperaturesASTM STP 165, 31—50. 32.2

COFFIN L. F. and READ J. H. (1956) A study of the strain cycling and fatiguebehaviourofacold-workedmetalLondonConf.,Sessions.Paper1. 31.17; 61.7

COFFIN L. F. andWESLEY R. P. (1954) Apparatusfor the studyof effects of cyclicthermalstressesonductilemetalsTrans. Amer.Soc.Mech.Eugrs.76, 923. 31.17

(1953) An apparatusfor the studyof the effects of cyclic thermalstressesonductilemetalsASME PaperNo. 53-A-77. 31.17; 32.2

COLEMAN I.J. (1958)An evaluationofthecriticisms by Toppingof Marins’s strengthhypothesisJ. Aero. Sri. 25 (6), 408. Index aero. 104/14/7. 62.8

CooMas S. G. H., SBEERATT F. and Pos~aJ. A. (1956) An analysisof theeffectsofshot-peeningupon the fatigue strengthof hardenedand temperedspring steelLondon Conf., Session3. Paper1. 63.5

CoRNELIUsH. (1941)VerhalteneinigerKurbelwellen-GusswerkstoffebeiDauerbean-spruchungdurchBiegung und VerdrehungJb. Dtsch.Luftfahrtf. Pt.2, 325—332.

62.5(1941) Einfluss von Bctriebspausenauf die Zeitfestigkeitvon Stahlenmit FerritLuflfahrtforseh.B18 Lfg 8, 285—288. 66.3

(1944) Einfluss von Einspannungenauf das DauerfestigkeitsverhalteneinerF kaltausgehartetenAluminium-Kupfer-Magnesium-KnetlegierungZ. Metallk.

36 (5), 101—105. 32.3; 64.2C0ENELIU5H. andKRAmER H. (1941)Festigkeitseigenschaftenvon Chmom-Mangan-

Molyhden-VergutungsstablenStahL u. Eisen,Düsseldorf61, 871—877. 61.8CORnNP. (1953) Essaidepiècesmoyennesa la flaxion rotativeRem. Met. Mem.,50,

761—767. 31.32CoEsoN M. G. (1949) The N S relationship in endurancetesting Iran Age 163,

F 103—105. 85.1CORTEN H. T. (1955) Univ. 18., DTAM, TR 88. 32.3CORTEN H. T., DIMOFF T. and DOLAN T. J. (1954) An appraisal of the Prot method

of fatigue testing, Proc. Amer. Soc. Test. Mater. 54, 875—894; AMR 9, Rev. 749.23.22; 96.2

COETEN H. ‘F., DIM0PF T., DosAN T. J. and SuesM. (1953) An appraisalof theProtmethodoffatigue testing,PartII, Univ. 18., DTAM TR 35. 23.22; 96.2

COETEN H. ‘F. andDOLAN T. J (1956) Cumulativefatigue damageLondonConf.,Session3. Paper2. 24.2; 64.1

COETEN H. 1’. and SINcLAIR G. M. (1955) A wire fatiguemachinefor investigationof the influence of complexstresshistoriesUniv. Ill., Dept. DTAM Rep.81.

31.31; 32.4; 33.1; 64.1CORTEN H. T., SINCLAIR G. M. and DnLAN T. J. (1954) An experimentalstudy of

theinfluenceof fluctuatingstressamplitudeon fatiguelife of 75S-T6AluminumASTM PreprintNo. 70. 24.2

CO55LRTT V. E. (1952) Electron microscopy of solid surfacesNature, Loud. 110,861—863 45.5

COTTELL G. A. (1954) Fatigue failures,with specialreferenceto fracturecharacter-istics, British Engine, Boiler & Electrical Insurance Co., Ltd. Manchester,Tech. Rep.NesuSeries,2, 22 1—256. 28.1

256 257

BIBLIOGRAPHY aInLsoGEAPnv

COTTELL, G. A. (1956) Lessonsto be learnt from failures in service, London Conf.,Session7. Paper1. 28.1

COURTNEY-PRATTJ. 5. (1951) Direct optical measurement of the length of organicmoleculesNature, Loud. 165, 346—348 45.3

Cox H. L. (1956) Stressconcentrationin relationto fatigueLondonConf., Session2.Paper16. 63.3

CoxH. L. andCOLEMAN E. P. (1950)A noteon repeatedloadingtestsoncomponentsandcompletestructuresJ. R.Aero. Soc.54, 1—10; AMR 4, Rev. 227. 34.1

Cox H. L. and OWEN N. B. (1955) 10-tonfatigue testingmachine; load providedby massand springsystemoscillating resonantlyEngineering,Loud. 179, (4656),500—504. 31.13

CoxJ. W., KREPP5J. G. andBANEAED M. H. (1955)A studyof thefatigue life andstructuralbehaviourof seaplanehull bottom plating Glenn L. Martin Co.Engng.Rep. (6659). 25.1; 53.0

CRATE H., OCMILTRRE D. W. andGRAVES W. T. (1946) Effect of ratio of rivetpitchto rivet diameteron the fatiguestrengthof riveted joints of 24S-T aluminum-alloy sheetNACA TN 1125. 54.12

CEO5SLAND B. (1954) The effect of fluid pressureon the shearpropertiesof metalsProc. Instu. Merh. Essgrs.,Loud. 168, 935—946 31.6; 34.2

(1956) Effect of largehydrostaticpressureson the torsional fatigue strengthofanalloy steel,LondonConf., Session2. Paper8. 31.6; 62.4; 65.3

CUMMINGS H. N., STULEN F. B. andSeNULTE W. C. (l955a) Relation of inclusions tothefatigue properties of SAE 4340 steel,WADC TR 55—456.

55.1; 61.3; 61.8; 66.1(l955b) Investigation of materials fatigue problems applicable to propellerdesign WADC TR 54-531and Suppl. 1. 61.3; 61.8

CtsR’rsssJ. H. (1943) On transformationsusedin the analysisof varianceAnn. Math.Statist. 14, 107—122. 90.1

CUTHBEET5ONJ. W. (1935) The loaddeflectionfatigue test,a critical investigationof its application CarnegieSchoolMem., 24, 1—50. 20.0

D

DARvas K., GEROLD E. and SCHULTZ E. H. (1940) Becinflussungder LebensdauerwechselbeanspruchterTeilc durch RuhepauscnStahl ss. Eiseu, Düsseldorf60,100—103. 66.3

DANIELS N. H. G. andDORN J. E. (1957) The effect of temperature,frequencyandgrain sizeon thefatigue ofhigh purity aluminumASTM STP 196. 61.2; 64.3

DAVIES R. B. andMANN J. Y. (1956) The changesin hardnessduringfatigue testson copperat 6,000 cycles/minuteARL, Melbourne, Rep.,(MET 16); Indexaero.116/12/12. 61.7

DAVIES H. E. and MCKEOWN J. (1947) The significanceof mechanical testingMetallurgia, Mouchr. 37, 19—22; AMR I, Rev.289. 65.1

DECK W. (1956) Crack detectionin aircraft structuresJ. R. Aero. Soc. 60 (551),739—747; Index aero. 120/12/12. 27.0; 76.1

DEGENBARDT H. (1942) Ergebnissevon Betriebsfestigkeits-Versuchenmit Flugzeug-bauteilenLilienthal-Ges.Ber. 152, 23—28. 25.1

DEENEEL. J. (1955) FatiguecrackdetectionmethodsPt. 2. Reviewof experimentaldata on the initiation and propagation of fatigue cracks in test specimens

WADC TR 55—86, Part 2. 27.0; 46.0DEENEEL. J. (1956) Bibliographyof thematerialdampingfield (with abstractsand

punchedcard endings) WADC TR 56—180 Bibl.

DEEMAN C. (1954) Standarderrors of estimateof parametersof fatigue failuresurvivorship functions Columbia Univ., N.Y., Tech. Rep. T-2A. Office ofOrdnanceResearchContract. 92.0

(1955) Someremarkson the endurancelimit problem Columbia Univ., N.Y.Tech.Rep.T-4A, Office of OrdnanceResearchContract. 95.0

DEOcH C. H., SPEOULED. P. andDAwsoN W. J. (1946) Detectionof cracksin steelby meansof supersonicwavesJ. Iran St. Inst., 153, 319—353. 46.5

DEUTLER H. (1956) Die dynamisehcUniversal-Prufmasehineder mechanisehenAbteilung der Bundesbahn-VersuchsanstaltMunchen Eisenbahn-tcchnisclseRundschau,1—4. 31.13; 32.4

DscK J. and WILliAMs L. 5. (1952) Elevated-temperature fatigue-testing machinefor ceramicmaterialsEugiueeriug,Loud. 173, (4497)422—423; AMR 6, Rev. 153.

32.2DIcKINsON T. A. (1956) Chemical milling of steelsand titanium Sheetmetal md.

33, (354) 735—736; Index acm. 197/12/12. 55.1DIEP5CHLAG E., MATTING A. and OLOENBURG G. (1935/36) ElastizitatsverhAltnisse

in SchweissverbindungenundderenZugsehwingungsfestigkeitArch. Eiseuhuttenw.9, 341—345. 31.15

DIETER G. E., HORNEG. T. and MEHL R. F. (1954) Statisticalstudyof overstressingin steel,NACA TN 3211;AMR 7, Rev. 3571. 24.2; 66.1

DIETER G. E. and MEaL R. F. (1953) Investigationof the statisticalnatureof thefatigue of metalsNACATN 3019; AMR 7, Rev. 1808. 61.3

Dsarx A. G. H. and GR5N5FELOEKH. (1944) Behaviour of syntheticphenolic resinadhesivesin plywood underalternatingstressesTrans.Amer.Soc.Mech.Engrs. 66,3 19—328, 442—446.

Dsx E. H., JE. (1956) Aluminum alloys for elevatedtemperatureserviceAerouaut.Eugug.Rem. 15 (1), 40-48, 57; Index acro272/12/2. 65.1

DIxoN W. J. and Moon A. M. (1948) A method for obtaining and analyzingsensitivity dataJ. Asner. Statist. Ass. 43, 109—126. 23.1; 23.2; 83.0; 95.0

DOLAN T. J. (1950) Pastwork on fatigue of metalsin the high temperaturefieldUniv. Ill., DTAM TR 17. 65.1

(1951) Electrically excited resonant-typefatigue testing equipmentBull. Amer.Soc. Test. Mat. (75), 60—67; AMR 5, Rev. 120. 31.24; 34.4; 63.2

(1952) Problemsofmetallic fatigueathigh temperatureMetal Progr. 61, 97. 65.1(1954) Basicconceptsof fatiguedasnagein metalsASM, Cleveland,Ohio. 60.0

DOLAN T. J. andBROWN H. F. (1952) Effectof prior repeatedstressingon thefatiguelife sf 75S-T aluminum,Univ. Ill., DTAM TR 29. 24.2

I)OLAN T. J. and HANLLY B. C. (1948) The effect of size and notch sensitivity onfatigue characteristicsof two metallic materials,Part II-SAE 4340 steel, AirMateriel Command,USAF, TR 5626. 63.1

I)OLAN ‘I. J., McCcow J. Fl. and CEA5n W. J. (1950) The influenceof shapeofcrosssectionon thefiexural fatiguestrengthofsteelTrans.Amer.Soc. Mech.Eugrs.72 (5), 469—477; AMR 4, Rev. 1593. 63.2

DOLAN T.J. andYEN C. S. (1948) Someaspectsoftheeffectofmetallurgicalstructureon fatiguestrengthandnotch-sensitivityof steelProc. Amer. Soc. Test. Mater. 48,664—695. 61.2

DOREY S. F. (l948a) Large-scaletorsional fatigue testingof marine shaftingProc.Inst. Mech. Eugrs., Loud. 159 (46), 399—415;AMR 3, Rev. 1103. 31.43; 31.44

(1 948b) Torsional fatigue testingof marine shaftingEugiueeriug,Loud. (March).63.1

25858 259

BIBLIOGRAPHV

DOEEY S. F. andSMEDLEY G. P. (1956)The influenceof fillet radiuson the fatiguestrengths of large steel shafts London Conf., Session3. Paper3. 63.1; 63.3

DDEGEELON E. (1929) Eine neue Prufmaschinezur Untersuchungder Werkstoffebei wechselnden nftmals wiederholten BiegebeanspruchuugenMetallwirtsrhafl8, 986—990. 32.2; 31.32

D0UGI.As W. D. and TAYLOR W. J. (1938) Effect of initial plasticstrainon fatiguestrengthof threelight alloys M.T. ReportNo. 5649. 24.1; 61.7

Dow N. F. and PETERS R. W. (1955) Preliminary investigation of the failure ofpressurizedstiffened cylinder, NACA RM L55D15L. 33.5; 53.0

Dow?rrON F. (1954) Least-squaresestimatesusingorderedobservationsAnn. Math.Statist. 25, 303—316. 90.42

DROzD A., GEROLD E. and SCHULTZ E. H. (1950) Der Einfluss von weehselndenund von schlagartigen Uberbelastungen auf die Lebcnsdauervon Stahl beiBiegewechselbeanspmuchungArch. Eisenhütteuw.21, 181—189. 24.2; 61.7

DRYDEN H. L., RHODE R. V. and KUHN P. (1952) The fatigueproblemin airplanestructuresMIT Conf., 18—51. 31.13; 32.4

DUGUE D. (1937) Application des proprietésde la limitC au sens du calcul desprobabilitéu a l’étude de diverses questionsd’estimation J. Er. Polyt., Paris305—373. 90.4

DURRLLI A. J. andOKuao S. (1954) Crack density studies in “stress-coat” Proc. Soc.Exp. StressAnal. 11 (2), 153—160;AMR 8 Rev. 2667. 46.1

F

EASTMAN F. S. (1935) Flexurepivots to replaceknife edges andball bearingsUniv.Ill. Engng.Exp.Stat.; Bull. 86. 34.2

ECKELJ. F. (1951)Proc. Amer.Soc. Test. Mater. 51, 745—760. 64.3EDEN E. M., RosE W. N. and CUNNINGHAM F. L. (1911) The enduranceof metals

Proc. Instu. Mech. Eugrs.,Laud Pts. 3—4, 839—880. 57.0; 65.5; 85.1EUWAKD5 D. H. (1958) A piezo-electricpressurebox gaugeJ. Sri. Instrum. 35 (9),

346—349; Index aero. 106/14/11. 43.3Et5ENHART C. (1947)Inversesinetransformationof proportionsBook,397-416. 90.1EN5LOW W. H. and PIPER G. (1952) Repeatedload test of main landing gear

GlennL. Martin Co. Engng.Rep.4912. 25.1EPREMIMO E. and MRHL R. F. (1952) Investigationof statisticalnatureof fatigue

properties,NACA TN 2719;AMR 6, Rev.488. 24.2; 51.22; 51.3; 56.2; 85.1EPsTEINB. andSOBEL M. (1953) Life testingJ. Amer.Statist.Ass.48,486—502. 90.0EssscKsoNE. C. 0. andMACKIN G. E. (1945) Propertiesanddevelopmentof papreg,

a high-strengthlaminatedpaperplastic Trans. Amer. Soc.Merh. Eugrs. 67 (4),267—277. 28.3

EEKER A. and SVENSON 0. (1951) Kraftmessungbei wechselnderBeanspmuchungATM, V 131—1. 43.1

ERLINGEK E. (1935) Investigationconcerningthepossibleuseof staticallycalibratedmeasuringsprings for dynamic forcemeasurement(in German). T. H. Gras.Dr. Diss. 34.3; 36.0

(1936) Die Genauigkeit von dynamisehenMatemialprttfmasehinenMessterhuik12 (6), 109—111. 35.0; 36.0; 64.4

(1936/37) Eine Prüfmaschinezur Erzeugung wechselndcrZug-Druck-KrafteArch. Eiseuhütteuw.10 (7), 317—320. 31.13; 34.4

EELINGER E. (1938) A bendingfatigue machine (in German) Arch. Eiseuhütteuw.11 (9), 455—456. 31.21

asa Lb GRAPHV

ERLINGER E. (1938/39) Prufanlagensum Ermittlung der Wechselfcstigkeitvon Ma-schinenteilenArch. Eiseuhütteuw.12, 613—621. 31.13(1941) Eine Sehwingungsprufmaschinefür 200 kg Zugoder Druck-kraftMetall-uirtsrhafl. 20, 414—416, 748—749. 31.11; 31.32

(1943) Umlaufbiegcmaschinefür DrahtprobenMetallwirtsrhafl. 22, (12), 178.31.13

E5AU A. and KORTUM H. (1930) Mitt. Forschg.-Anst. GHH-Konzemn, 3, 279.31.44

EVANS U. R. (1947) The electrochemistryof corrosion-fatigueMelbourne Symp.,84—94. 65.4

F

FAIEMAN R. G. (1955) Life tests on Martin Model 404 M.L.G. oleo drag StrutMenascoMfg. Co. ReportR728. 25.1

FALLHAuER R., BUcHssoLTx H. and SCHULZ E. H. (1933) The influence of testdiasncteron the bendingfatigue strengthof steel (in German)Mitt. Forsrhlnst.mer. Stoltlw. A.-G. 3, 153—172. 63.1

FAUST C. L. (1948) Surfacepreparation of electropolishing,Pittsburgh Int. Conf.,Corrosion PublishiugCo. 55.1; 63.4

FEARNOW D. 0. (1951) Investigationof the fatigue strengthof full-scale airplanewing structuresNACA RM. L51. D13a. 33.5; 54.6

FELGAR R. P. (1958) Effect of shot-peeniagon fatigue strength, ASME Prep.(S8-SA-46);Indexacro. 192/14/8. 61.5

FENNEE A. J., WRIGHT K. I-I. R. and MANN J. Y. (1956) Fretting corrosionanditsinflucssceon fatiguefailure,LondonConf., Session4. Paper8. 26.5; 32.3; 65.5

FERGUSON R. L. (1954) A furtlscr investigation of the effect of surfacefinish onfatigue propertiesat elevatedtemperaturesNACA TN 3142; AMR 7, Rev.2845. 63.4

FlEw P. M. (1943) Basic physical properties of laminates Mod. Plast. 20, (12),91—102, 126—130. 28.3

FINOLEv W. N. (1941) Mechanicaltestsof celluloseacetatePror. Amer. Soc. Test.Mater. 41, 1231—1245. 28.3

(1943a) Mechanical tests of maccrated phenolic molding material NACAWartime Rep.W99. 28.3

(I 943b) Mechanical tests of cellulose acetate III Trans. Amer. Soc. Merh. Eugrs.65 (5), 479 487. 28.3

(1945) Fatigue tests of :s lansissatedMitsclscrlich paper plastic Proc. Amer. Soc.Test. Mater. 45, 8789(19. 28.3; 31.51

(1947) New apparstns fur axial-load fatigue testing BulL Amer. Soc. Test. Mat.(147), 54—56. 35.1

(1949) Test procedureassdtechniqueMouuolou Fatigue Testing,ASTM STP-91,Section V. 70.0

(1952) Fatigue of 76S-T61 Aluminum Alloy under combinedbending andtorsionPror. Asuer.Sor. Test. Mater. 52, 818-832. 62.5

(I 953a) Combined-stressfatigue strength of 76S-T6I aluminum alloy withsuperimposedmean stressesand correction for yielding NACA TN 2924;AMR 7, Rev. 130. 62.5

(1953h) Effect of rangeof stresson fatigueof 76S-T61 aluminumalloy undercombined stresseswhich produceyielding J. Appl. Mcrh. 20 (3), 365—374;AMR 7, Rev. 1108. 62.5

260 261

BIB Lb GRAP isv

FINDLET W. N.(1953c) Plastics:their mechanicalbehaviourandtestingAMR 6 (2),Featurearticle. 28.3

(1954) Experimentsin fatigue underrangesof stressin torsion and axial loadfrom tension to extremecompressionProc. Auser. Soc. Test. Mater. 54, 836—852.

62.1; 62.4(1956)FatigueofmetalsundercombinationsofstressesASME, PaperNo. 56—A74.

62.5FINDLEY W. N., CENTURY B. A. and HENDRICKsON C. P. (1952) Fatiguetestsunder

axial loadsof aluminumjoints bondedwith a resinousadhesiveBulL Amer. Soc.Test. Mat. (179), 67—71; AMR 5, Rev.1686. 21.1

FINDLEY W. N., COLEMAN J. J. and HANLEY B. C. (1956) Theory for combinedbending and torsion fatigue with data for SAE 4340 steel, London Conf.,Session2. Paper9. 62.8

F5NDLET W. N. and HINTS 0. F.JR. (1943) Therelationbetweenresultsof repeatedblow impacttestsandof fatigue testsProc. Amer. Soc. Test. Mater. 43, 1226—32.6

FINDLET W. N.,JONES P. G., MITCHELL W.J. andSUTHERLAND R. L. (1952) Fatiguemachinesfor low temperaturesand for miniaturespecimensBull. Auser. Soc.Test. Mat. (184), 53—55. 32.2

FISmLEY W. N. and MATHUR P. N. (1955a)Anisotropyof fatiguestrengthof steeland two aluminum alloys in bendingand torsionProc. Amer. Soc. Test. Mater.55, 924—941. 61.8; 62.4; 62.8

(1955h) Modified theories of fatigue failure under combinedstressProc. Soc.ExJs. StressAual. 14 (1), 35—45. 62.8

FINDLRY W. N. and MITCHELL W. J. (1953) Two machinesfor combinedbendingand torsion fatigue Proc. Soc. Exp. StressAnal. 11 (1), 203—212; AMR 8, Rev.2380. 31.51

FINDLEY W. N., MITCHELL W. J. and MARTIN D. F. (1955) Combinedbendingand torsion fatigue tests of 25S-T aluminum alloy Amer. Soc. Mech. Eugrs.,585—593; AMR 9, Rev. 1467. 62.5; 66.1

F5NDLEV W. N., MITCHELL W. J. and STROHuRCR D. D. (1955) Effect of rangeofstressin combinedbendingandtorsion fatigue testsof 25S-T6aluminum alloyASME Prep.(55—68); Index aero.274/12/2. 62.5

F5NOLEY W. N. and WOKLEY W. J. (1948) Mechanicalpropertiesof five laminatedplasticsNACA TN 1560;AMR 2, Rev.65. 28.3

FINE M. (1958) A standardisedmethodof representingfatigue test resultsJ. R.Aero.Soc. 62 (570), 456—; Indexaero. 112/14/7. 82.1

F5NR K. (1950) Der DehnungsmesstreifenZ. Ver. Dtseh. lug. 92, 89—94, 176—176.42.0

(1952) ZweckmassigeAuswahl von DehnungsmessvcrfalsrcnZ. Ver. I)tseh. lug.94, 1037—1038;VDI-Sonderh. 1953, 75—76. 42.0

FINK K. andHEMPEL M. (1949)UbermagnetischeMessungenandauerbcanspruchtenStahlstabenMitt. MPI Eisenforschg.487; Arch. Eiseuhüttenw. 20 (1/2), 75—78.

27.0FINK K. andHEMPEL M. (1951) Untersuchungenvon Dauerschwing-Prüfmaschinen

mit DchnungsmesstreifenArch. Eiseuhütteuw.22 (7/8), 265—273. 36.0; 64.4F5NNEY J. M. (1957) The effect of pickling andanodisingon the fatigueproperties

of 2L40and DTD 683 aluminum alloys Aero. res. Lab. Rep., SM255; Indexaero305/14/4. 63.4

F5NNEY J. M. andJOMNITONE W. W. (1955) Random load fatigue testson simplespecimens,ARL, Melbourne,Rep.F 28/40/1. 32.4

Bt B Lb 0GRAPH V

FISCHER FR. P. (1933) Vorsehlagsum Festlegungder zulassigenBeanspruchungenim MasehincnbauTech. Mitt. Krupp 1, (Sept) 67—83. 82.2

FISCHER G. (1938) Uberdie Kerbwirkungbei DauerweehselbeanspruchungunddenEinfluss der Kaltvcrformung auf die DaucrhaltbarkeitJb. Dtsch. LuftfahrtfBd I, 517—523. 24.1; 61.7

FI5IsER R. A. (1912) On an absolutecriterion for fitting frequencycurvesMesseug.Math. 41, 155—160. 90.4; 93.0

(1921) On themathematicalfoundationsof theoreticalstatisticsPhiL Traus.222,309—368. 90.4

(1925) Theory of statisticalestimationProc. Comb. Phil. Soc. 22, 700—725. 90.4(1935) The logic of inductiveinferenceJ. Roy. Statist.Soc.98, 39—54 90.4; 93.0

FIsHER W. A. P. (1949) A comparisonof theenduranceof variousaircraftstructuresunder fluctuating loadBrit. RAE, Rep.No. Structure45. 33.5

(l958a) Experimentalcorrelation betweenthe enduranceof a wing sparjointand the ratio between0.1% proofandultimate tensilestrengthof thematerialAero.res. Comm.curr.Pap. (CP 371/ARC 18 T26); Indexaero.2 10/14/5. 26.0

(1958b) Programmefatigue testson notchedbars to a gust loadspectrumRAE.Tech.Note No: Structures236. 25.1

FssssaRW. A. P., CROSSR. H. andNoRRIsG. M. (1952) Pretcnsioningfor preventingfatiguefailuresin boltsAirer.Eugug.24 (280),160—163;AMR 5, Rev.3441. 24.1

FLUCK P. G. (1951) The influenceofsurfaceroughnesson thefatigue life andscatterof testresultsoftwo steelsProc. Amer.Soc. Test.Mater. 51,584—592. 63.2; 63.4

DR FORa5T A. V. (1932) Magnetic test locatesflaws in valve springsIron Age 130,Pt. 2, 107—128. 46.4

DR FORESTA. V. and HOPKINS L. W. (1932) Testingrope wire andwire ropeProc.Amer. Soc. Test.MoteL 32, Pt. 2, 398—412. 33.1

FORRESTG. (I 955a) The fatiguepropertiesof aluminiumalloys, Nottingham,Symp.on Fatigue, 1955. 62.2

(1955b) The effect on fatigue of notches,surface finishes,etc., Inst. of Metal-lurgists Refresher Course. 62.2; 63.3

FORREsT C., GUNN K. W. and W000WARD A. R. (1953) The fatiguepropertiesofZ-section test pieces completely machined from an aluminium extrusionconformingto DTD 364B J. R.Aero. Soc. 57, 103—107. 63.2

FORREST P. G. and TAP5RLL H. J. (1954) Proc. Iustss. Meeh.Eugrs., Loud. 168, 763.65.1

FnRsYTss P. J. E. (1952) Somefurtherobservationson the fatigueprocessin purealunsissum’s,Roy. Aircr. Establ.,Rep. No. Met. 70. 61.7

(1956) Ilse basicmechanismspffatigue and its depcrsdanceon the initial stateofa material, LondonConf., Session6. Paper5. 61.7

FosrRRFl. W. (1943) Dynasssic testsof lansinated plastics, Lockheed Aircr. Corp.Rep.No. 4400. 28.3

(1947) A methodof detectingincipient fatigue failure Proc. Soc. Exp. StressAnal.4 (2), 25—31; AMR I, Rev. 655. 46.2

FOSTER H. W. and SELIGRE V. (1944) Fatigue testing methodsand equipmentMccli. Eugug., N.Y. (Nov.) 719—725. 33.5

FOSTER P. F. (1932) The Haigh alternatingstresstestingmachineMoehiuery,Loud.40, 621—624. 31.14

FRANCER. D. (1931) Endurancetestingofsteel:Comparisonof resultsobtainedwithrotating beamversusaxially loadedspecimensProc. Amer. Soc. Test. Mater. 31,Pt. 2, 176—193. 62.3

262 OCQ

H IB Lb 0RAP H v

FRANK W. E. andGsasoNR.J. (1954)A newpressure-tensinginstrumentJ.FranklinInst. 258 (1), 21—30; AMR 8, Rev.488. 43.22

Fa.ANKE F. (1929) Uber Dauerbrückean Maschinenteilenund geeignetcPrüfver-fahren zur Bcstimsnussgder Dauerfestigkeit ATZ, 643—645. 20.0

FRANSSON A. (1956) Effect of simultaneous cyclic variation of stress and temperatureon a high temperature material, Stockholm Conf., 43—52. 25.1

FRASER D. A. S. and GUTTMAN I. (1956) Tolerance regions Ann. Moth. Statist. 27,162—179. 90.7,

FRENCH H. J. (1933) Fatigue and the hardeningof steels Trous. Amer. Soc. SteelTreat. 21, 899—946. 24.2

FEEUDENTMAL A. M. (195Ia) Planrsing and interpretationof fatigue tests, ASTMSTPNo. 121, 3—22. 70.0

(l951b) Fatiguetestingandtestinterpretation,Univ. Ill., Tech.Rep.26. 95.0(1953) A randomfatigue testing procedureand machineProc. Amer. Soc. Test.Mater. 53,896-910. 25.1; 31.32; 32.4

(1956) Cumulative damageunder randomloading, London Conf., Session3.Paper4. 25.1; 31.32; 32.4

FRRUDENTMAL A. M. and GUMBEL E. J. (1953) On the statistical interpretation offatigue tests Proc. Roy. Soc. (A), 216 (1126), 309—332; AMR 7, Rev. 1117.

710; 92.0(l954a) Minimum life in fatigue J. Amer. Statist.Ass. 49, 575—597. 92.0(l954b) FailureandpermanentsurvivalJ.AppI. Phys.25 (11), 1435. 92.0(1956a) Physicalandstatisticalaspectsof fatigueAdmour. Appl. Meeh.4. 94.0(l956b) Distribution functions for the prediction of fatigue life and fatiguestrength,London Conf., Session3. Paper5. 83.0; 92.0

FKEUDENTMAL A. M. and HELLER R. A. (1956) Accumulationof fatigue damagein aircraft structural materials, Columbia Conf., N.Y. 25.1

FREUDENTMAL A. M., HELLER R. A. andO’LEARY P. J. (1955) Cumulativedamageof aircraft structural materials, Part I: 2024 and7075 aluminumalloy, WADCTN 55—273Pt. 1. 25.1

FRIEDMAN M. (1947) Planningan experimentfor estimatingthemeanandstaDdarddeviationof a normal distributionfrom observationson the cumulativedistri-bution: Cf. Eisenhart(1947),ChapterII. 23.12; 90.4; 95.0

FRITsi P. H. (1948) Fatigue testson crankshaftsteelsJ. Irott St. Inst., 159, 385-409;AMR 2, Rev.742. 31.51; 61.1; 62.5

(1954) Fatigue tests on rolled alloy steelsmade in electric and open-IseartisfurnacesSpec.Rep. Iron St. lust., Loud. No. 50, 130 pp. 61.3

(1956) Fatigue of wrought high tensilealloy steels,Lossdon Cssnf., Sessiors5.Paper7. 61.1

FROST N. F. andDUGUALE D. S. (1958) The propagationof fatiguecracksOs slsectspecimens .1. Meeh.Phys. Solids 6 (2), 92—110; Index aero. 151/14/4. 27.0

FROSTN.E. andPHILLIPs C. F. (1956a)The fatiguestrengthofspecimenscontainingcracks, Instn. Mech.Engrs.Prep.,19—31; Index acro.87/12/7. 63.3

(l956b) Studiesin the formatiorsandpropagationof cracksin fatiguespecisnensLondon Conf., Session6. Paper2. 27.0

FULLER T. S. (1931a) Influenceof corrosionon fatigueof notchedspecimensMm.& Metoll., N.Y.12, 446. 65.4

(1931b) Endurancepropertiesof Some well known steelsin steamTraus.Amer.Soc.Steel Treat 19, 97—111. 65.2

DI0 Lb CRAPSI V

FULLER F. B. and OuERG T. f (1947) Fatigue characteristicsof rotating-beamversus rectangularcantilever specimensof iteel and aluminum alloys Proc.Amer.Soc. Test.Mater. 47, 665—676. 62.3

F6PPL 0. (1909) Fatiguetestswith notchedbars (in German),Mitt. Meeh. -techn.Lab. Mbnchen,No. 31; Stahlu. Fiseu,Düsseldorf(March), 409—410. 31.41

0

GAEETNERH. (1918)UcherLebcnsdauervonKugellagernDiuglersJ. 99,35—38. 85.1GASEK M. (1955) Untersuchungentiber den Einfluss der Oberflachenbesehaffenheit

auf die DaucrschwingfestigkcitmetalliseherBauteile beim Raumstemperatur,T. H. Stuttgart,DiM. 63.4

GALLANT R. A. andBENDA F. K. (1954) An automaticload control for tuning-forkfatigue test equipmentGeu. Mot. Eugug.J., 1, (9), 6—9 31.23

GARDINER G. C.J. (1949) Someaspectsofpropellerfatigue testingAirer. Eugug.21,149—152; AMR 3, Rev. 1361. 33.3

GAEMAN C. P. (1950) Vibration fatigue in Boulder transmissionlines Elect. West104, 62—64 28

GARWOOD M. F., ZUESSURO H. H. and ERICKSON M. A. (1951) Correlation oflaboratorytestsaadserviceperformance,ASM. Publ., 1—77. 61.4

GASSNER F. (1939a) Festigkeitsversuchemit wicderholter BeanspruehungimFlugzcughauLuJiwisseu6, 61—64. 25.1

(l939b) tJber bisherige Ergebnissc aus Festigkeitsversuchenim Sinnc derBetricbSstatistik,Liliessthal-Ges.,Berieht 106 : 1, 9—14; Transl. NACA TM1266; AMR 4, Rev. 2187. 25.1

(1941) Auswirkung betriebsahnlieherBelastungsfolgenauf die Feotigkeit vonFlugzeugbautcilen.lb. Dtsch. Luftfohrtf. 1, 472—483; Deutseh.Vcrsuchsantt.Luftfahrt. (DVL), Bcr. Cf 407/5; Dr. diss.TH. Darmstadt,Dr. Diss. 25.1

(1954) Zur Frage der Ermtidungsfcstigkcitim Flugzeugbau.Jb. Wiss. Ges.Flugterh. Luftf 286—294. 25.1

GATEWOOn B. F. and HONAKEE J. P. (1919) On S-N curvesfor fatigue analysisJ. Aero.Sri., 23 (3), 276 Index aero.93/12/4. 82.1

GATTO F. (1955) Statisticalinterpretationof fatigue tests, (in Italian), Allumiuio 24(6), 543—554; Index aero.94/12/9. 91.0

(1956) New statisticalmethodsapplied to the analysisof fatiguedata StockholmCoof., 66—77. 91.0

Cs;5NEN M.J. W. (1956) A machinefor bendtestsPhilips Tech.Rem. 17 (9), 246—248;Index aero. 107/12/4. 31.2

C’ NSAMSE M., PEAESALt. F. B., PEILINI W. S. and LosvJ. R. (1942) The tensileprssjserticsof pearlitc, bainite and spheroidite Ts-ous. Amer. Soc. Metals 30,983. 61.2

GENTNER F. (I 936) The evaluationof fatigue tests (in German) Arch. Eiseuhutteuw.9 (9), 441—450. 91.0

GEEuER W. (1874) Relationbetweenthe Superiorand inferior streslesof a cycleoflimiting stress(in German),Z. Bayer. Arch. Ing. Ver. 6, 101. 62.1;82.2; 85.2

GEROLD F. andKARIUS A. (1950)Abkürzungsverfahrenzur ErmittlungderWechsel-festigkeitArch. Eiseuhutteuto.21, 191—195. 26.0

GILBERT G. N. J. and PALMER K. B. (1955) The influenceof understresoingon thefatigue propertiesofflake graphiteandnodulargraphitecastirons B.C.J.R.A.E69. 24.2

GILCHEI5T J. (1900) WohIer’s laws on material underrepeatedstressEugiueer,Loud.90, 203—204. 82.1

264~g ç

BIHLIOGRAPNV 55 lB 1.10U RAP MT

GILL F.T. and000DACRER. (1934)Someaspectsof thefatiguepropertiesofpatentedsteelwire J. Irou St Inst. 130, 293—323. 31.32; 33.1; 61.4

GILLETT H. W. (1929) Haveheat-treatedaluminiumalloys a true endurancelimit?Metals & Alloys 1, 2 1—22. 95.0

GILLETT H. W., GROVER H.J. andJAeKsoNL. R. (1946)Americantrendsin endur-ancetestingRem. Mltall. 43, 268—270 20.0

GILLETT H. W. and MACK F. L. (1924) Noteson someendurancetestsof metalsProc. Amer.Soc. Test Mater. 24, Pt. 2, 476—546. 50.0; 65.5; 95.0

GsaScssbGR. (1953) StatistiseheAuowertungvon Dauerschwingverouchen(inFrench)Rem. Métall. 50 (4), 248—252; Stahl a. Eiseu,Düsseldorf73 (15), 1000. 91.0

GI5EN F. andGL6CKER R. (1938) RontgenographischeBestimmungender zeidichenAnderung des Figenspannungszustandesbei BicgeweehselbeanspruchungZ.Metallk. 30 (9), 297—298. 42.21

GODFREY D. (1950) Investigationof fretting corrosionby microscopicobservationNACA TN 2039. 65.5

GOHN G. R. (1952) High speed machinefor fatiguestudiesBell Lab. Rec.30(12),459—463. 31.21

GOHN 0. R. and MORTON F. R. (1949) A new high-speedmetal fatigue testingmachine for unsymmetricalbendingstudiesProc. Amer. Soc. Test. Mater. 49,702—716; AMR4, Rev.689. 31.21

GoLDa A. and GRUBBS F. F. (1956) Analysis of sensitivity experimentswISeD thelevels of stimulus cannot be controlled J. Amer. Statist. Ass. 51, 257—265.

23.11; 95.1GOENuAUD M. (1955)Applicationof statisticalanalysisto theclassificationofsurface

finishesandto theirstudy: Pt. 1. (inFrench),Lab. Cent.Arm. Etude,(11—100),Note 16; Transl. No. T 4774; Index aero. 14/5. 45.0; 63.4

GoonoastA. H. (1956) Corrosionfatigue crackingresulting from wetting of heatedmetalsurfacesLondonConf., Session4. Paper9. 65.4

GOUGM H. J. (1933) Crystallinestructurein relationto fatigueof metals—especiallyby fatigueProc. Amer.Soc. Test. Mater. 33, Pt. 2, 3—114. 61.7

(1949) Engineering steelsunder combinedcyclic and static stressesEugiueer,Loud. 188, 497—500, 510—514,540—543, 570—573. 31.53; 62.5

(1950) Fngineeringsteelsundercombinedcyclic andstaticstresses.1. AppI. Mech.17 (2), 113—125; AMR 4, Rev. 3564. 31.53; 62.5

(1951) Some experimentson resistanceof metals to fatigue under combinedstressesAero.Res. Counc.Rep. (London). 62.5

GOUGM H. J. and CLENSHAW W. J. (1935) The testing of engineeringmaterialsTrans.Inst. Mar. Eugrs.57 (10). 20.0

(1951) Someexperimentson the resistanceof metalsto fatigueunder combinedstresses Ministry of Supply Aeronautical Research Council Reports andMemoranda,Pt. 2, 126. 62.1; 62.5

GOUGM H. J. and Cox H. L. (1932) A new form of combinedstressfatigue testingmachineA.R.C., Rep.F.F. 325. 31.53

GOUGM H.J.andPOLLAKO H. V. (1935,1937)Thestrengthof metalsundercombinedalternatingstressesProc. Instu. Meeh. Eugrs., Loud. 131, 3—103; .1. lustu. Auto.Eugrs. 5, No. 6. 31.53

(1936) The effect of specimenform on the resistanceof metals to combinedalternatingstressesProc. Instu. Alec/s. Eugrs., Loud. 132, 549—573. 63.2

GOUCH H. J., POLLARB H. V. and CLENSHAW W. J. (1951) Someexperimentsonthe resistanceof metalsto fatigstc under combinedstressesAero. Res. Coune.Lond. Rep.Mcm. 2522; AMR 6, Rev. 133. 62.5

GOUCN FE. J. and S0PWITHD. G. (1 932a) Atmosphericactionas a factor in fatigueof metalsJ. lust. Met. 49 (2), 93—122. 65.2

(1932b) Relativetemperaturesof brasswhensubjectedto reverseddirect stressesin vacuo and in air Rep. Memor. Aero. Res. Comm.,Loud. (1482). 65.2

GOUGH H. J. and SOPWIT51 D. G. (1933) Some comparativecorrosion-fatiguetestsemployingtwo typesofstressingactionJ. Iron St. lust. 127 (1), 301—335. 32.3

GOULD A. J. (1936)The influenceof temperatureon the severity of corrosion-fatigueEugiueeriug,Loud. 141, (3669), 495—496. 32.3

(1949) Corrosion-Fatigueof steelunderasymmetricstressin seawater J. Iron St.Inst 161, 11—16. 32.3

(1956) CorrosionfatigueLondonConf., Session4. Paper2. 28.2; 32.3; 65.4GOULD A. J. and FVAN5 H. R. (1939) A scientific studyof corrosion-fatigue. Pre-

liminary reportson experimentsat CambridgeUniv. Iron & Steel Inst., Rep.Alloy SteelsRes. Comm.,325—342. 32.3

GRANT J. W. (1950) Notchedandunnotchedfatigue testson flakeandnodulareastiron. 61.3

GRANT N.J. (1952) FatigueatelevatedtemperatureMIT Conf., 292—301. 65.1GEEKNALL C. H. and GossNG. R. (1937) Fatigue propertiesof non-ferroussheet

metalsProc. Amer. Soc. Test.Mater. 37, Pt. 2, 160—191. 31.21GRIFFIN C. B. (1948) Fatigue testingproductionpartsIrou Age(Jan),59—62. 33.0GRIFF5TN G. F. (1948) Experimentalinvestigationof the effects of plasticflow in a

tensionpanelwith a circularhole, NACA TN 1705. 63.3GROVER H. J. (1943) The usc of electric strain gagesto measurerepeatedstress

Proc. Soc. Exp.StressAunt. 1 (1), 110—115. 34.3; 42.21(1956) Allowancefor stressconcentrationin designto preventfatigue, LondonConf., Session2. Paper 1. 63.3

GROVER H.J., BISHoP S. M. andJACKSON L. R. (l9

51a) Fatiguestrengthof aircraftmaterials. Axial-load fatigue testson unnotchedsheet specimensof 24S-T3and 755-T6aluminum alloys andof SAF 4130 steel,NACA TN 2324; AMR4, Rev. 2508. 24.2; 34.2; 62.1; 63.4; 64.3

(1951b) Fatigue strengthsof aircraft materials. Axial-load fatigue tests onnotclsedsiscetSpecimensof 24S-T3 and 75ST6 aluminum alloys and of SAF4130 steelwith stress-concentrationfactor of 5.0, NACA TN 2390; AMR 4,Rev.4471. 24.2; 34.2; 62.1; 63.4; 64.3

GROVER H. J.. HYLER W. S., KUHN P., LANOERS C. B. andHOWELL F. M. (1953)Axial-loasi fatiguepropertiesof24S-Tatsd

7SS-Faluminumalloyasdeterminedin

severallahssratories,NACA TN 2928; AMR 6, Rev. 3745 andAMR 9, Rev.1839. 34.2; 34.4; 36.0; 43.21; 57.11; 57.0

GRUuus F. F. (1948) On estimatingprecisionof measuringinstrumentsandproductvariability J. Amser.Statist. Ass. 43, 243—264. 74.0

GUARD R. W. (1956) MetalsatelevatedtemperaturesProd. Eug,sg.27 (10), 160—164;Index acro. 113/12/12. 65.1

GUMuEL F. J. (1945) Simplified plotting of statistical observations Trous. Amer.Geophys.Un. 26, Pt. 1, 69. 90.3

(l954a) Statistical theory of extremevalues and somepractical applications,Nat. BureauStand.Applied MatlsematiesSeries33. 83.0; 90.3

(1954b) Statisticaltheoryof droughtsProc. Amer.Soc.rim. Engrs. SeparateNo.439;AMR 8, Rev. 881. 90.0

266 907

BI BLI 00 RAPStY 5SIBLIOGHY

GUMBEL E.J. (1955) Statisticalestimationof the endurancelimit ColumbiaUniv.,Office of OrdnanceRes. Contr., Rep.T-3A. 95.0

(1956a) StatistiseheTheorie der Ermudungserscheinungenbei Metallen Mitt.Math.Statist.8 (2), 97—130. 90.0

(l956b) Statisticalestimationof theendurancelimit ColumbiaUniv., Office ofOrdnanceRes. Contr. Rep.T-6A. 95.0

(1 956c) Statistical interpretation of fatigue life and fatigue strengths Trans.N.Y. Acad. Sci. 18 (4), 334—346. 94.0

GUMBEL E.J. andCARL5ON P. G. (1954) Extremevaluesin aeronauticsJ. Aero. Sci.21 (6), 389—398; AMR 8, Rev.328. 94.0

GONN K. (l955a) The fatigue propertiesof two aluminium alloys testedundervariablestressconditionsS andT Memo. No. 5/56. 24.2

(1955b) Effect of yieldingon thefatiguepropertiesof testpiecescontainingstressconcentrationsAeronaut.Quart. 6 (4), 277—294; Index aero.246/12/1. 63.3

GU5r.AyssoNG. (1947) Somebasic characteristicsof wire straio gaugesand bridgecircuits for thesegaugesFFA Rep.22. 42.2

GU5TAs’ssoHG. V. A. andOLssoreC. 0. (1956) An electronicapparatusfor accuratemeasurementofperiodicstrainsFFARep.63; Indexaero.108/12/4. 34.3;42.21

GOTFREUND K. (1950) VerdrehdauerprUfmasehinefür grosseProbenlad. Anz. 72,315—316. 31.41

(1951) Umlaufbiegemaschinefür 12000 Lastwcchselpro Minute lad. Anz. 73,44—45. 31.32

H

HABNaMANN and PRAGERW. (1933) Zur Frage der ErmudungsfestigkeitbeimehrachsigenSpannungszustandenMetallwirkschaJI342—343. 62.8

HA5OH B. P. (1912) A new machine for alternating load tests Engineering, Land.94, 721—723. 31.14; 51.11

(1915) Reporton alternatingstresstestsof a sampleof mild steel receivedfromthe B. A. StressCommitteeRep. Brit. Ass. 163—170. 62.1

(1917) Experimentson the fatigue of brassesJ. Inst. Met. 18, Pt. 2, 55—86;Engineering, Load. 104 (Sept),315—319. 31.14; 32.3; 62.1; 82.2; 85.2

(1922) Elasticandfatigue limits in metalsBgham Metall. Soc., 8, 412—422. 95.0HALL L. D. and PARKER E. R. (1948) Effect of residualtension stresson thefatigue

strength of mild steel, Weld. Res. Suppl. 13, 421—425; AMR 1, Rev. 1360.24.1; 61.7

HALL W. J. and S5NNAMON G. K. (1952) A mechanismfor controlling large-scalefatigue testing machinesProc. Soc. Exp. Stress Anal. 10 (1), 203—208; AMR 6,Rev. 1263. 31.1; 32.4

HALM5HAw R. (1958) Recentadvancesin radiographictechniquesJ. Inst. Met. 86(5), 207—211; Indexaero. 153/14/4. 40

HANR5N5 G. A. andBECKER M. L. (1931) The effect of surfaceconditionsproducedby heat treatmenton the fatigue resistanceof spring steel J. Iron St. Inst. 124(2), 387. 61.4

HARscsNsG. A., BECKER M. L. andMILLs H. R. (1935) Furtherexperimentson theeffect of surfaceconditionon the fatigue resistanceof steel.1. Iron St. Inst. (1),129. 61.4

HANLEY B. C. and DOLAN T. J. (1951) The effects of rangeof stressand stateofstress on thefatiguestrengthof SAE 4340 steelUniv. Ill., Rep.No. 22, ProjectNR-03l-005. 62.5

HAN5LIP R. E. (1952) Residual stressesin surfacehardenedoil field pump rodsProc. Soc. Exp. Stress Anal. 10 (1). 63.5

HAN5T0eR R. F. and MURRAY A. (1946) I)ampingcapacityandthefatigue of metals

.1. Inst. Met. 72, 97—132. 31.44; 32.1HAFEME55TER R. N. (1954) The ultrasonic testingof forging ingots Bull. Amer. Soc.

Test. Mat. (197), 52—55; AMR 7, Rev. 4068. 46.5HARA 5. (1956) An investigationon the corrosionfatigue of marinepropellershafts

London Conf., Session4. Paper3. 32.3; 65.4HARBRATH H. F. and ILLG W. (1954) Fatiguetestsat stressesproducingfailure in

2 to 10,000 cycles; 245-T3 and755-T6 aluminum-alloy sheetspecimenswitha theoreticalstress-concentrationfactorof 4.0 subjectedto completelyreversedaxial load NACA TN 3132; AMR 7, Rev. 3577. 22.1; 32.1; 63.4

HARORATFI H. F., LANBER5 C. B. and UTLEY E. C. JR. (1953) Axial load fatiguetests on notched and unnotchedsheetspecimensof 61S-T6 aluminum alloy,annealed347 stainlesssteeland heat-treated403 stainlesssteel, NACA TN3017; AMR 7, Rev. 793. 22.1; 55.1; 57.2; 63.3

HARORATH H. F. andLavnoLn H. A. (1958) Further investigationof fatigue-crackpropagationin aluminum-alloy box beams NACA TN 4246; Index aero.252/14/8. 27

HARDRATS5 H. H., LavaoLn H. A., LANOER5 C. B. and HAuscsssLn L. W. (1956)Fatigue-crackpropagationin aluminum-alloy box beamsNACA TN 3856.

27; 53HARORATH H. F. andOHMAN L. (1951) A studyof elasticandplasticstressconcen-

trationfactorsdue to notchesand fillets in fiat platesNACA TN 2566; AMR5, Rev.2299. 52.2; 56.3; 63.3

HARDRATH H. F. andUTLEY E. C.JR. (1932) An experimentalinvestigationof thebehaviorof 245-T4aluminum alloy subjectedto repeatedstressesof constantand varying amplitudes,NACA TN 2798; AMR 6, Rev. 2789. 25.2;

31.32; 32.4; 51.31; 55.1

HARINOx J. A. (1948—1949)Onhighly compressiblehelicalspringsandrubberrods,and their applicationfor vibration-freemountingsI, II, III, IV Philips Res.Rep.3, 401—449; 4, 49—80, 206—220, 261—290. 34.6

(1949) The cross-springpivot as a constructionalelementAppI. Sci. Res.,HagueA 1, 313—332. 34.2

HARPUR N. F. (1958) Fail-safestructuraldesignJ. R. Aero. Soc. (May), 363—376;Int. tiers. Abstr. 3 (7), 109. 33.5

}JAER55 51., FIOEWITZ D. G. and Moon A. NI. (1948) On the determinationofsamplesizc~in designing experiments .1. Amer. Statist.Ass. 43, 391—402. 71

ITAETMAN A. (1953) Preliminary investigation to verify the cumulanve damageIsypothesis Sn/N = 1 on rivetedjoints (in Dutch), NLL. Rep.M 1923. 24.2

(1954) A comparative investigation on the influenceof sheetthickness,typeofrivet, and numberof rivet rowson thefatiguestrengthat fluctuatingtensionofriveted single lap joints of 24S-T alclad sheet and 17S rivets, NLL Rep. M.1943. 54.12

HARTMAN A. andDUYN C. (1952)A comparativeinvestigationon thefatiguestrengthat fluctuating tensionof several types of riveted lap joints, bolted andgluedlapjoints of 24S-T aiclad, NLL Rep. Ml857. 54.11; 54.12; 54.22

HARTMAN A. andJt\coasF. A. (1957) Researchon thestatic andfatiguestrengthsof bondedand rivetedsingle lapjoints in clad 2024 and7075 aluminium alloyat room and elevated temperatures,NLL Rep. M.2041; Index aero.264/14/8. 65.1

ORG

BIBLIOGRAPHY BtB LI 0 CRAP H V

HAKTMAN A. and KLAASEN W. (1956) The fatigue strengthat fluctuating tensionof single lap joints of clad 24S-T and 75S-T aluminium alloy with 2 rows of175 rivets,NLL Rep.M.2Oll; Index aero. 115/12/12; lut. Aero. Abstr., 2 (1),128—128. 54.12

HAKTMAN A. and RONDREL J. H. (1954) Static tests and fatigue tests on redux-bondedbuilt-up and solid light-alloy spar booms. NLL Rep. M. 1936. 54.5

HAKTMANN E. C. (1956) Fifect of unintentionalstressraiserson the fatiguestrengthof structural components,London Conf., Session2. Paper13. 63.4

HARTMANN F. C., HOLT M. andFATON J. D. (1951) Staticandfatiguestrengthsofhigh-strengthaluminum-alloyboltedjoints,NACA TN 2276and3269. 54.11

HAKTMANN F. C., LT5T J. 0. and ANDKEWS H. J. (1944) Fatigue tests of rivetedjoints,NACA ARR 4115 (WR W-55). 54.12

HAKTMANN F. C. and STSCKLET 0. W. (1942) The direct stressfatigue strengthof1 7S-T aluminum alloy throughout the rangefrom 1/2 to 500,000,000cyclesofstress,NACA TN 865. 22.1

HEAD A. K. (1950) Statisticalpropertiesof fatigue dataon 24S-Taluminum alloyBull. Amer. Soc. Test Mat. (169), 51—53; AMR 4, Rev. 3250. 63.4

HEAD A. K. andHOOKE F. H. (1956) Randomnoisefatigue testingARL, MelbourneRep.52; London Conf., Session3. Paper9. 25.2; 32.4

HEADJ. W. andOULTON 0. M. (1957) Fitting curvesto experimentaldata by leastsquaresAfter. Eugug. 29, 268—270; Index acm. 2/13/10. 90.41

HEINDLHOS°KRK. andSJöTALL H. (1923) Fndurancetestdata andtheir interpreta-tion Tram. Amer. Soc. Meeh. Eugrs. 45, 141—145; Mech. Eugug., N.Y. 45,579—580. 91.0

HOLMS H. F. (1950) Size effect on endurancelimit stressfor SAF 4140steel,Masterof ScienceThesis,PurdueUniv. 63.1

HEMKLKIJK J. (1949) Constructionof a confidenceregionfor a line Proc. Acad. Sci.Amst. 52, 374—384. 90.7

HEMPEL M. (1937) Dauerfestigkeits-Sehaubildervon gckerbtenund kaltverformtenStahlen und von SchraubenZ. Ver. Dtseh. lug. 81, 870 Stahl a. Eiseu,Düsseldorf57, 274—275. 61.5

(1937/38)Weehselfestigkeitsschaubildervon Rund- und Flaeh-staben,T-Tragernund DrahtcnausStahlArch. Eiseuhutteuw.11, 231—240. 63.2

(1938) Die Beziehungenzwischen dem Rontgen-Grobgefugebildund dcrZugschwellfestigkeitvon geschweistenProbenauS St. 37 Stahla. Eiseu,Düsseldorf58, 756—760. 61.2

(1938) Finflussder Beanspruchungsartaufdie Wechselfestigkeitvon Stalslltãbcnmit Querbohrungenund Kcrben Arch. Eiseuhütteum. 12, 433—444.

62.4; 63.2; 64.2(1939a)Zur FragedesDauerbruches:Magnetpulverbildund DauerbrnchanrissMitt. K.- Wilh.-Iust. Eiseuforsch.21 (9), 147—162. 46.4

(1 939b) Finfluss der Probenform, Prufmasehincund Versuchsdurchfuhrungauf die Wechselfestigkeit Mitt. K.- Wilh.-Imt. Eiseuforseh. 21 (1), 21—26.

35.2; 63.2; 64.2(1939/40) Magnetpulverbildund Dauerhaltbarkeitvon SchraubenfedernArch.Eiseuhütteuw. 13 (II), 479—487. 46.4

(1943) Wechselbeanspruehungvon Stahlin der Kalte und WarmeTeehn.Mitt.HDT, Fssen,36 (1/2), 5—7. 65.1

(1951) Beitrag zur Frageder Weehsellestigkeitbei unterschiedlicherProben-grUsse Arch. Eiseuhütteuw.22 (11/12), 425—436. 63.1

HEMPaL M. (1952)DauerfestigkeitprufungenundWerkstoffverhaltenbei der Schwin-gungsbcanspruchungZ. Ver. Dtseh. lug. 94 (25), 809—815; (26), 882—887; AMR6, Rev. 1616 & 3413. 23.21; 60; 96.0

(l954a) Dauerfestigkeitund Kerbwirkuog Droht 5 (6), 208—211. 63.3(1954b) Dauerfestigkeitund OberflaeheDraht 5 (7), 255—259. 63.4(1 954c) Dauerschwingversucheund deren Auswertung mit Hilfe statistischerVerfahrenDroht 5 (10), 375—378. ¶14.0

(1 956a) Uber Vcrformungserseheinungenin ,Stählenbei der Weehselbeanspru-chung,StockholmCool., 78—91. 61.7

(l956b) Performanceof steelunder repeatedloading Columbia Cool., N.Y.,83—103. 61.7

(l957a) Dauerschwingversuchebei 500 his 650°Can ferritischen und au.steni-tisehenStahlenArch. Eiseuhütteuw. 28 (5/6), 311—316. 65.1

(1957b) Stand der Erkentnisseuber den Finfluss der Probengrosseauf dieDauerfestigkeitDroht 8 (9), 385—394. 63.1

HRMPEL M. and ARDELT F. (1938/39) Verhalten von Stahl gegen Zug-DruekWeehselbeanspruchunghei 500°Arch. Eiseuhütteuw.12, 553—564. 65.1

(1939) VerhaltendesStahlesin der Warmeunter Zugdruek-Wechselbeanspru-ehungMitt. K- Wilh.-Iust. Eiuseuforsch21, 115—132. 65.1

HEMPEL M. and FINK K. (1953) Naehprufungder Lastanzeigevon Dauersehwing-PrufmasehinenArch.Eiseuhütteuw.24 (1/2), 83—91. 36; 64.4

HEMPEL M., K0CHENDOEmEK A. and H5LLNHACEN F. (l957a) Finfluss der KriStall-orienticrung auf die Wechselfestigkeit von E-Fisen-Fiuknstallen Mitt. MPI.Fisenforschg., Abh. 715; Arch. Eiseuhütteuw.28 (7), 417—422. 61.2

(1957b) Fioflussder Kristalloricntierungaol die Ausbildungvon Gleitspurenander Oberflaehe biegeweehselbeanspruchtcrce-Fisen-FinkristallprobenMittMPI Fisenforschg,Abh. 717; Arch. Eiseuhütteuw.28 (8), 433—444. 61.8

HEMPEL M. andKRUC H. (l942a) Zugdruek-Dauerversuehean Stahl bei hoherenTemperaturenund ihre Aruwertung nach vemsehiedenenVerfahren Mitt.K.- Wilh.-Iust. Eiseuforsch. 24, 71—95. 65.1

(1 942b) Dauerfestigkeitund Dehnvcrhaltenvon Stahlenin der WArmc Z. Ver.Dtsch. log. 86, 599—605. 65.1

(194

2c) Finfluss der Strcckgrenzeaol die Biegewechselfestigkeitvon StahlMitt. IC.-Wilh.-Iust. Eiseuforseh.24, 97—103. 26

(l942/43a) Streckgrenzenverhaltnisund Bicgewcehsclfestigkeitvon Stahl Arch.Eiseulsii/te,sw.16 (1), 27—30. 26

(1942/436) Weclsselfestigkeits-Schaubildervon Stählen bei hoherenTempera-lssressArch. Eiss’n/sutteuw.16 (7), 261—268. 65.1; 82.2

HEuPEL M. and LUCEJ. (1941) Vcmhalten von Stahlbei tiefen TemperaturenunterZugdrssck-WeclssclbeanspmnchungMitt. Kl-Wilh.-Iust. Eiseuforseh.23 (5), 53—79;Arch. Eiseuhiittensv.15, 423—430. 65.1

HEM5’EL M. andM0LLER H. (1949)Die Auswirkungvon Schweissfehlemnin Probenaus Stahl St 37 aufderenZugschwellfestigkeit,Mitt. MPI Fiscnforschg,Abh.504; Arch. Eiseuhutteuw.20, 375—383. 61.3

HEMS°EL M. and SADNKK H. R. (1948) fIber den Finfluss dem Formanderungs-geschwindigkeitaoldiemeclsanischenKcnnwerte, insbesonderebeiweebselndemBelastuogGlas. Auu. 72 (10), 145—149. 64.3

HEMPEL M. andTILLMANNS H. F. (1936)VerhaltendesStahlesbeihOhercnTempera-turen unter wechselnderZugbcanspruchungMitt. K-Wilh.-Iust. Eiseuforsch. 18(12), 163—182. 65.1

270 271

BIBLIOGRAPHY BIB LI OCR A PSI V

HEMPEL M. and TILLMANI H. F. (1936/37) Zugschwcllversuchemit Stahl beiTemperaturenhis 600°Arch. Eiseuhütteuw.10, 395—403. 65.1

HENRIK5EN F. K. (1948) Residualstressesin machinedsurfacesTraus.Dauish Aced.Tech. Sd. 7; AMR 3, Rev. 1967. 63.5

(1951) Residualstressesin machinedsurfacesTram. Amer. Soc. Mcdi. Eugrs. 73,69—76. 63.5

HENRY D. L. (1951) Predictionof endurancelimits usinglinearly increasingloads(UnpublishedRep.) 23.22

HENTScMEL G. andSCMWEIZERHOP S. Le “Vibrator” nouvelexcitateurdevibrations(1954) Rech. Aéro. (37), 51—55 31.44

HRRTEL H. (1931) Dynamisehe Bruchversuche mit Flugzeugbauteilen DVL-Bericht248; Jb. Dtsch. Vers Aust. Lufif 165. 54.4

Hess R. W., Fa.ALIcm R. W. and HUBBARD H. H. (1957) Studies of structuralfailure due to acousticloading,NACA TN 4050; Index aero.226/13/10. 25.2

HessW. F.,WYANT R. A., WIN5ORF.J. andCooRH. C. (1944) An investigationofthefatiguestrengthof spotwelds in the aluminumalloy aiclad 24S-T, NACAOCR ProgressRep.no. 15. 54.21

HEYER K. (1943) Mehrstufenversuchean Konstruktions-Flementcn,Lilierithal-Gesellsehaft,Bericht152, 29—54. 24.2; 54.3; 54.4

HRWSON T. A. (1954) Further notes on automatic control as applied to fatiguetesting equipmentProc. Soc. Exp. Stress Aual. 12 (1), 215—226; Index acro.110/12/4; AMR 8, Rev. 3083. 33.4; 34.4; 35.0

v. HEYDENKAMPF (1929) NeuereDauerbiegemasehinenmit schwingendemProbestab(Bicgungsschwinguagsmasehinen)TH Bmaunschweig,Dr. Ing-Diss; Metall-wirtschaft. 9, 321—326. 31.24

Havwoon R. B. (1953) The fatigue testing of Structuresby the resonancemethodSehweiz.Arch. 19 (8), 249—260; AMR 7, Rev. 1809. 33.4

(1955) The effect of high loadson fatigue, RAF. Internal Memo.No. Structures289. 24.1; 61.7

(1956a)Theeffect of highloadson fatigue,StockholmConf., 92—102. 24.1; 61.7(l956b) The influence of pre-loadingon the fatigue life of aircraft componentsandstructures,Acm. res. Coun. curr. Pap. (CP232/ARCI7898); Index aero.208/12/7. 24.1; 61.7

HOHENEM5ER K. and PRACER W. (1933) Metallwirtsehafi.24, (June). 31.53HOLLOWAY A. A. (1956) The layout of technical reports, ACARD Specification

No. 1. Bib].HOLT M. (1950) Resultsof shearfatigue tests of joints with 3/16-inch-diameter

24S-T3l rivetsin 0.064-inch-thickalcladsheetNACA TN 2012. 54.12HOLTScHMIDT 0. (1935) Alternating and damping testing machine of the MAN

(in German)Mitt. ForsehAust.Gatehoffu.,Nüruberg3, 279—284. 31.44HONECCRR F. (1926) The fatigue of metalswhen stressedbeyond the yield point

Browu Boseri Rev.13, 169—174. 24.1HOPRINSON B. (1911/12) A high-speedfatigue testerand the enduranceof metals

under alternating stressat high frequency Proc. Roy. Soc. A86, 131—149;Eugiucer, Loud. I S. 113—1 14, 123. 31.14

HORCER0. J. (1935)Fffect of surfacerolling on thefatiguestrengthof steelJ. Appl.Mech. 2 (4), Al28-A136. 32.3; 61.5

(1938) Photoelasticanalysispracticallyappliedto designproblemsJ. AppI. Phys.9,457-465. 44.1

(1953) ASTM STPno. 144, 40. 32.3; 65.5

HORGER 0. J. (194) Stressingaxles and other railroad equipmentby cold rolling,SurfaceStressingof Metals,ASM. 85—142. 61.5

(1954) Fatigue characteristicsof largesections,ASM, Cleveland,Ohio.61.6; 63.1

(1956) Fatigue of largeshafts by fretting corrosion,London Cool., Session4,Paper4. 32.3; 65.5; 66.2

HORGER 0. J. and MAULBETScM J. L. (1936) Increasing the fatiguestrengthofpress-fittedaxle assembliesby surfacerolling J. Appl. Mech. 3 (3), A9l—A98.

32.3; 61.5HORCER0. J. andNEIFERT H. R. (1939) Fatiguestrengthof machinedforging 6 to

7 in. diameterProc. Amer. Soc. Test. Mater. 39, 723—740. 63.1(1941) Effect of surface conditions on fatigue properties ASM Symposium:Surfacetreatmentofmetals,Cleveland,279—298. 63.4; 65.5

(1952) Fatigue propertieSof largespecimenswith related Size and statisticaleffectsASTM STPno. 137, 70—91. 61.6; 63.1; 63.3

HossssssoJ. (1956) Somestudieson the pitting of marinereductiongears,LondonConf., Session9. Paper7. 62.7

HOTRLLING H. (1941) Theexperimentaldeterminationof themaximumof afunctionAuu. Math. Statist. 12, 20—45. 70

HOTTENRGTT F. (1953) Influence of prestressingand elastic characteristicson thefatigue life of bolt, nut assemblies(in French)Rech.Aéro.no. 36, 47—56; AMR7, Rev. 2855. 24.2

HorsoNA. W. (1949) Recentdevelopmentsin methodsofstrengthtestingprcssuriSedfuselagesRAF Re. No. Structures55. 33.5; 54.7

HOWARD D. M. (1953) Developmentofa fatiguedamageindicatorPartI Preliminaryinvestigation WADC TR. 53—393. 27

HOWARD D. M. and SM5TH F. C. (1952) Fatigueand static testsof flush-rivetedjoints NACA TN 2709. 54.12

HOWELL F. M. andHOWARTH F. 5. (1937) A fatiguemachinefor testing metalsatelevatedtemperaturesProc. Amer. Soc. Test. Mater. 37, Pt. 2, 206—215.

31.32; 32.2HOWELL F. M. et al. (1948) Effectsof surfacefinish of certaindefectsand of repair

of defects by weldingon fatiguestrengthof 355-T6sandeastingsand effectsofprior fatiguestressingon tensilepropertiesNACA TN 1464. 24.2

HOWLAND R. C.J. (1930) On stressesin the neighbourhoodof a circular holein astrip undertensionPhil. Traus. Ser. A. 229 (Jan),49—86. 52.2; 63.3

HUANC T. C. (1954) Bibliography on residualstressSAF SP-125. 63.5Hunasn V. (1936)Dreh-undBicgcschwingungsmaschinemit Stromrichtcr-Steuerung

Z. Ver. Dtsrli. log. 80, 261—262. 31.44HunsoNR. A. and CInCRJ. F. (1937) Aecelcratinnof fatigue testsAero Dig. 31 (3),

78. 26HULIiERT 0. C. (1956) Plasticsstructures.1. R. Aero. Soc. 60 (542), 114—120; Index

nero. 286/12/3. 28.3HULT J. (l957a) Fatigue crack propagation in torsion J. Mccli. Phys. Solids 6,

47—52. 27(l957b) Flastic-plastictorsion of sharplynotchedbars .1. Mech. Phys. Solids 6,

79—82. 27(1958a) Fatigue crack propagation,a problem of plasticity KTH, Stockholm,Doct. Diss. 27

(l958b) Fxperimcntal studies on fatigue crack propagationin torsion,KTH:sHandl. No. 119. 27

272 97q

BIBLIOGRAPHY BIBLIOGRAPHY

HUNTER M. S. andFEICRE W. G. (1954) Metallographicaspectsof fatiguebehaviourof aluminum Proc. Amer. Soc. Test. Mater. 54, 7 17—736. 61.7; 66.1

HUTCHI50N M. M. and BEI5IEL F. E. (1955) A refined treatmentheat method forsteelfatiguespecimensAero. res. Lab. Note (MET. 3); Index aero. 161/12/5.

55.2; 61.4HYLER W. S., Pops’ H. G., GIDEON D. N., GORDONS. A. andGR0YERH. G. (1958)

Fatiguebehaviorof aircraft structuralbeams,Appendix.—Typicalcalculationsof momentsof inertia, buckling stresses,bending momentsand dcflcctions,NACA TN 4137; Index aero.234/14/4; mt. aer. abstr. 3 (3), 44. 53; 54.5

HANsEL H. (1937/38) Die Fehlererkennbarkeitbei der magnetischenzerstUrungs-freien Prufung Arch. Eisenhuttenw. 11, 497—502. 46.4

I

ILLG W. (1956) Fatiguetestson notchedandunnotchedsheetspecimensof 2024-T3and 7075-T6aluminumalloys andof SAE 4130 steelwith specialconsiderationof the life range from 2 to 10,000 cycles, NACA TN 3866; Aero Engng.Rev., 2(2), 142; Index aero. 106/13/4. 22.1

ILLO W. andMCEYILY A. J. (1957) Staticstrengthof cross-grain7075-T6aluminiumalloy extrudedbar containingfatigue cracks,NACA TN 3994; Ismdcx aero.117/13/7. - 63.3

INE5ONB., CLAYTON-CAYEJ. andTAYLOR R.J. (1956)Variation in fatiguepropertiesover individual castsof steelJ. Iroa St. Inst. 184, 178—185. 61.9

IPIEN J. andJEENE N. K. (1944) Graphicalevaluationof thedistribution of smallexperimentalseriesActa Path. Microbiol. Scand.21, 343—361. 90.3

IRWIN P. L. (1925) Fatigueof metals by directstressProc. Amer.Soc. Test. Mater. 25,Pt. 2, 53—65. 51.11

VAN ITER5ON F. K. (1950) The theoreticalfatiguecurve (in Dutch) Ingeaienr’sGras.62 (24), MK55—59; AMR 4, Rev. 1578. 85.1

IVANOVA V. S. andODIN0 J. A. (1957) Isv. Akad. JsTaskSSSR,Otd. Tech. Nank(1),95—102; Ref Tekn.Tidskr. 87, 968. 60

J

JACKSONB. B. (1956) Aeronauticaldocumentationpracticesin EuropeandAnscricaSpec.Libr. 47 (2). Bibl.

JACKsONL. R. andPoessAPsxYT. B. (1947) The effectof compositionon the fatiguestrengthof decarburizedsteelTrans.Amer.Soc.Metals39, 45—60. 61.1; 61.4

JACKSONL. R., WILsoN W. M., MOORE H. F. andGROVER H.J. (1946) TIse lhtiguecharacteristicsof bolted lap joints of 24S-T alclad slseetmaterials,NA( A TN1030. 54.11

JACOBSON P. H. (1947) The relative powerof threestatisticsJ. Amer. S/atisi. Ass.42, 575—584. 92.0

JACQUE55ONR. andLAURENT P. (1950) A newhigh-frequencyfatiguetestingmachine(in French)Rev.Gén. Mécan.34, 31—33; Engrs’ Dig. 11, 183. 31.21; 31.41

JASPERN. H. (1952) The TMB strain cycle gage and counter. An instrumentforthe statisticaldeterminationof the strain history of structuresProc. Soc. Exp.StressAnal. 10 (1), 87—96; AMR 6, Rev. 2474. 43.1; 48.1

JASPERT. M. (1923) The values of the energy relation in the testing of ferrousmetalsat varying rangesof stressand at intermediateand high temperaturesPhil. Mag. (Oct.), 609—627. 85.2

(1925) Typical static and fatigue testson steelat elevatedtemperaturesProc.Amer.Soc. Test. Mater. 25, Pt. 2, 27—52. 65.1

JASPERT. M. (1930) Overstressingin fatigueProc. Amer. Soc. Test. Mater. 30, Pt. I,293—294. 24.2

JATzKEwITICH Ss.J. (1949) Maschine zur Prufung einerfeststehendenProbeaufBiegcwechselfcstigkeitbei erhohtenTemperaturenSaw. Labor. 15, (1), 86—88.

31.32; 32.2JENEIN C. F. (1920) Fatigue limit in metalsIron Coal Tr. Rev.101, 265. 95.0

(1923a)Fatiguefailureof metalsProc. Roy.Soc. (103A), 121—138. 23.21; 96.0(l923b) Fatiguein metalsJ. R. Aero. Soc. 27, 89—104. 23.21; 96.0(1925) High frequencyfatigue tests Proc. Roy. Soc. A109, 119—143; A.R.C.,R & M. No. 982. 31.24; 32.1; 64.3

JENKIN C. F. and LEHMAN G. D. (1929) High frequencyfatigue, Proc. Roy. Soc.Arts. 125, 83—89; Stahl. u. Risen,Düsseldorf50, 702. 31.26; 32.1

JENKINs G. and STEPHENSB. (1956) Fatigue testson fuselageskin riveting. BristolAircraft Ltd. E.D.L.Rep.No. 9/262. 24.1; 54.12

JOANNIS M. (1957) Controlof instrumentfor checkingthe degree of finish of planesurfacesMicrotecaic 11(5), 211—215; Index aero. 110/14/3. 45.4

JOHNSON H. C. (1955) Development of a unitized statistical accelerometer and re-corder assemblyWADC TR 55—14. 43.1; 48.1

JoHNsoNJ. B. and OBERO T. T. (1933) Mechanicalpropertiesat minus 40 degreesof metals usedin aircraft constructionMetals & Alloys 4, 25—30. 65.1

(1934) Effects of notches on nitrided steelMetals & Alloys 5, 129—130. 63.3JOHNsoN L. G. (1951) Median ranks of sample values in their population with an

applicationto certainfatiguestudies Inanstr. Math. Soc. 2. 90.3(1953) An axiomatic derivationof a generalS—N equationIndnstr. Math.Soc.4.

91.0JoHNssoN S. (1949) Utmattningsforsok under stigande belastning Tekn. Tidskr.,

Stockh.79, 900. 23.22; 96.2J0HN5-roNE W. W. (1946) Methodsof investigatingthefatiguepropertiesof materials

Melbourne Symp., 135—164. 20; 30; 31.21J0HN5T0NE W. W. and Moonx’ B. S. (1953) Fatigueequipmentfor simulatingthe

flight stressesof aircraft, ARL, Melbourne,Rep.S.M. 296. 33.5JOI•INSTONE W. W., PATCHING C. A. andPAYNE W. 0. (1950)An experimentaldeter-

mination of the fatiguestrengthof CA-12 Boomerang wings, ARL. Melbourne,Rep.SM-16. 54.6

JONES D. T. (1956) Variations in the strengthof aluminium alloy sheetARC CP229. 93.0

JONES R. V. (1951) Parallel and rectilinear spring movements.J. Sci. Instrwn. 28,38—41. 34.1

JoNEsW. E.andWIL.EEs G. B. (1950) lime Cffect of varioustreatmentson thefatiguestrengtls of notched 5-816 and Tiniken 16-25-6alloys at elevatedtemperaturesProc. Amer.Soc. Test. Mater. 50, 744-762. 65.1

JUNO J. (1955) On linear estimatesdefined by a continuous Weight function Ark.Mat. 3 (15), 199—209. 90.43

JUNGER A. (1930) Erfahrungenubcr die Prufungder DauerfestigkeitverschiedenerWerkstoffe auf der MAN-Biege-SchwingungsmaschineMitt. ForschAnst.Gntehoffn.,Nurnberg 1, 8—18. 61.8

KK~&o~J.H. K. (1956) The Weibull distribution in life-testingof electrontubes.1.

Amer.Statist. Ass. 51, 514. 92.0KAPP (1912) The Witton-Kramerfatigue-testsEngineering,Lond. 94, Pt. 2, 805—806.

31.4

274 19 275

BIBL500RAPHY nsaLIooRApHy

KARRY R. W. and DosssT. J. (1953) Influence of grain size on fatigue notchsensitivity, ASTM, Preprint72. 61.2

KEIL A. and MEYER C.-L. (1954)A nondestructivetechniquefor detectingcracksin

tungstenby meansof eddycurrents(in German) Z. Metallk. 45 (4), 194—196;AMR 8, Rev.668. 46.3

KEL5EY R. A. (1956) Measuring non-uniformresidualstressesby the hole drillingmethod Proc. Soc. Exp. Stress Aual. 14 (1). 63.5

KEMPERMAN J. H. B. (1956) Generalizedtolerancelimits Auu. Math.Statist. 27 (1),180—186. 90.7

KENNEDY A. J. (1952) A constantstressdevice adjustablefor specimenlengthJ. Sri. Imtrum. 29, 40—44. 34.4

(1953) Thedesignof constantstresscantilever.1. Sci. lmtrsim. 30, 371—374. 34.4(1956) Fffect of fatiguestresseson creepandrecovery,LondonConf., Session4.Paper10. 32.7; 41.2

KENNEDY A. J. and SLADE R. F. (1956) An automaticelectromechanicalstressingunit for creepand fatigue testingJ. Sri. Iustrssm. 33, 409—410. 32.7; 34.3

KENNEDY N. G. (1956) Fatigue of curved surfacesin contact under repeatedloadcycles,LondonConf., Session3. Paper7. 32.5; 62.7

KnwoN J. N. (1935) The rotating-wire arc fatigue machine for testing small-diameter wire Proc. AmerSoc. Test. Mater. 35, 156—166. 31.31; 33.1(1940) A pulsatingtension-fatiguemachinefor small diameterwire Proc. Amer.Soc. Test.Mater. 40, 762—770. 33.1

(1945) An automotivetire fatigue machine Bull. Amer. Soc. Test. Mat. (136),9—12. 33.1

KEPRET J. L. and PAYNE A. 0. (1956) Interim report on fatiguecharacteristicsof atypical metal wing. NACA TM 1397. 33.5; 36.0; 54.6

KERRY F. A., NscHoLs J. and V5NeENT K. (1952) Cumulative damagefatigueinvestigations. (Loaded holes), Saunders-Roe Rep. No. 3R/S/762.

24.1; 24.2K5NNEY J. S. (1938) An investigationof theeffects of elevatedtemperatureson the

fatigue propertiesof two alloy steelsProc. Amer. Soc. Test. Mater. 38 (2),197—201. 65.1

KNOWLTON H. B. andSNYDERF. H. (1940) Selectionof steelandheattreatmentforspur gearsTraits. Amer. Soc. Metals(Sept.). 32.5

KOENTG5aERCERF. (1955a) Fatiguestrengthof flame-cutSpecimensin bright mildsteelBrit. Weld. J. 55 (1), 37—41. 63.5

(l956b) Fatiguestrengthofflame-cutspecimensin blackmild steelBrit. Weld.J.55 (7), 313—321. 61.2; 63.5

KOMMER5 J. B. (1912) Repeatedstresstesting Int. Ass. Test. Mat. Congr., PapersV4a andV4b. 22.2

(1919) BroaderuseofJohnson’sformula for repeatedstressEugug.NewsRec.83,942—944. 85.2

(1930) Theeffect ofunder-stressingof castiron andopenhearthiron Proc. Amer.Soc. Test. Mater. 30, 368—383. 24.2

(1932) Understressingand notchsensitivenessin fatigue Eugug.NewsRec. 109,353—355. 24.2

(1934) Metal strengthincreasedby graduatedstressingSteel94, 26.23.21; 96.0

(1935) Understressingandoverstrcssingin iron andsteel Eugug.NewsRec.114,550—551. 24.2

KoMssaasJ. B. (1937) Overstressingand undcrstressingin fatigue Eugiueeriug,Loud.143 (3724), 620—622; (3726), 676—678. 24.2

(l938a)Designstressdiagramfor alternatingplussteadyloadsProd. Eugug9 (10),395—397. 82.2

(1938b) Fffectof overstressingand understressingin fatigueProc. Amer.Soc. Test.Mater. 38, 249—268. 24.2

(1943) The effect of ovcrstressisigand understressingin fatigue Proc. Amer. Soc.Test. Mater. 43, 749—764. 24.2

(1945) The effectof ovcrstressin fatigueon theendurancelife of steelProc. Amer.Soc. Test. Mater. 45, 532—541. 24.2

KoNlSnsJ. and SsssNozUIcA.M. (1956) Scatterin fatigue life of structural steelandits influence on safety of structure Kyoto Uuis. Faculty of Eugug. 18 (2), 73—83.

92.0KOETUM H. (1930) Uber die Materialdampfrmgbei Dauerbcanspruchtmgdurch

TorsionsschwissgungenZ. Tech. Mccli. Thermodyu.1 (8), 297—307. 31.44KOSHAL andTURNER (1930) Studiesin thesamplingof cotton for the determination

of fibre-propertiesJ. Text,lust. 21, 325—370. 83.0KRA5NER H. (1942) Theeffect of the degreeof reductionby forging on thebending

fatigue strengthof ‘ow alloy steelsparallel and right angle to the forgingdirection Arch. Eiseuhtatteuw.15, 543—546. 61.8

KRAUSE N. A. (1957) Strain gaugecalibrationsand flight loads testing techniquesAGARD Rep.113; Index acro.55/14/7. 42.21

KaooN R. P. (1940)Turbine bladefatiguetestingMccli. Eugug.,N.Y.53 1—535. 31.26KROU5E G. N. (1934)A high-speedfatigue testing machineandsometestsof speed

effecton endurancelimit Proc. Amer.Soc. Test.Mat. 34,Pt. 2, 156—164.31.32; 32.1; 64.3

KUHN P. andHAEDEATH H. F. (1952)An engineeringmethodfor estimatingnotch-sizeeffect in fatigue tests on steel,NACA TN 2805. 52.0; 63.3

KORBER F. (193

9a)Qbcrden DaucrbruchmetalliseherWerkstoffeSchriften Dtsch.Akad. Luftfahrtforsch.(15), 19—23. 23.21; 96.0

(l939b) DasVerhaltenmetallischerWerkstoffeim Bcreichkleiner VerformungenStahlu. Eiseu,Dtisseldorf59, 624—625. 23.21; 96.0

KöEBER F. and HEMFEL M. (1933) DaucrvcrsucheauleinerhochfrequcntcnZug-Druck MasehineMitt. K.- Wilh.-Iust. Eiseuforsch.15, 119—135. 31.14; 32.1

(1936) Abhangigkeit der Wechsclfcstigkeitdes Stables von der Lastwechsel-frequenzMitt K.-Wilh.-Iust.Eiseuforseh.18 (1), 15—19. 64.3

(1939) Zssgdruck-, Biege- und Verdrehwechselbeanspruchungan Stahlstabenmit Qncrbohrrngenund KerbenMitt. K.-Wilh.-Iust. Eiscuforsch.21(1), 1—19.

23.21; 62.4; 63.3L

LAnOMI5E M. J. DE (1946) Difficulties in carryingout andinterpretingrotatingbeamfatigue tests (in French) Res.Métall. 43, 271—285.

LAMB5EJ. B. (1952) Thecountingstrain gaugeEugiueeriug,Loud. 174(4515), 168—170;AMR 6, Rev. 1523. 42.1

LANE P. H. R. (1956) Fatigue testson seamlessmild-steelpipebends,LondonConf.,Session9. Paper3. 31.11

LANGDON H. H. and FRsaoB. (1948) Fatigueof gussetcdjoints, NACA TN 1514.54.11; 54.12; 54.21

LANCEvIN A. eta!. (1950) Abkurzungsverfahrenzur Bcstimmungder Wechselfcstig-keit durch Mesoungder Permeabilitkt (in French)C. R. Acad. Sci., Paris 230(12), 1138—1 140. 26

276 277

BIBL500RAPHY B snL5 0 0RAP NY

LARRScE L. (1945) Tension vibrator comparestire cord values Text. World 95,107—109. 33.1

LATSN A. (1950) Metallurgical examinationof lead and lead-alloy pressure-cablesheathsEugiueeriug,Loud. 170, 121—122. 31.6

LAUDENDALE R. H., DOwDELL R. L. and CASSELMAN K. (1939) Fndurance ofannealed gold and quenched dental alloy Metals & Alloys 10, (Jan)24—25

31.21LAUNHARDT (1873) Formula for rangeof stress(in German),Z. Arch.Iugeu.Hauuoser,

19, 139. 85.2LAURENT P. (1947) Sur l’influence dc la forme etdesdimensionsde l’éprouvettcsur

le résultatde l’essaidefatigueC. R.Acad. Sci., Paris 224, 719. 62.2LAzAN B. J. (1942) Mod. Plast. 20, 83. Baldwin LocomotiveWorks, Bull. No. 202

and266. 31.23; 33.4(1950) A studywith new equipmentof theeffectsof fatiguestresson the dampingcapacity and elasticity of mild steel Trans. Amer. Soc. Metals 42, 499—558;AMR 3, Rev. 2336. 26

LAzAN B. J., BROWN J., GANN5ETT A., KsEMsEstP. and KLUMPP J. (1952) Dynamictestingof materials andstructurewith a new resonancevibration excitcs~andcontroller Proc. Amer. Soc. Test. Mater. 52, 858—876; AMR 9, Rev. 1115. 33.4

LEA F. C. (1926) Theeffect of superimposinga torsional stresson repeatedbendingstresses,Brit. Ass., Rep.Sect.G. 62.2

LEA F. C. and BUDORON H. P. (1926) Combinedtorsional and repeatedbendingstressesEugiueeriug, Loud. 122, 242—245. 31.54; 62.2

LEA F. C. and HRYwOOD F. (1927) The failure of somesteelwires under repeatedtorsionalstressesProc. lustu. Mech.Eugrs., Loud. (2), 403—463. 33.2

LEBEY H. (1954) A new machinefor endurancetestswith stresscyclesof variableamplitudesCeu.Mat. Eugug.J. 1, 16—20. 32.4

LEESEE D. 0. andDAANE R. A. (1954) Residualstressesin a strip in termsof strainchangesduringclectropolishingProc. Soc. Exp. StressAual. 12 (1). 63.5

LEHE F. (1925) Die Abkurzungsverfahrcnzur Frmittlung der Schwingungsfcstigkeitvon MaterialicnDr. -Ing. Diss. TH., Stuttgart. 26; 31.14; 31.32

(1926/27) Die Daucrfcstigkeit,ihre Bedeutungfür die Praxisundihre kurzfristigcFrmittlung mittcls neuartigerPrufmaschincnGlasersAuu. Gew. 99, 1 09—l 14,117—122, 177—180; 100, 33—39. 95.0

(1930) Congr. Int. Méc. Ghn. Liege i, 218. 31.13; 31.41; 34.1; 34.3DRP664764. 31.16

(1932) Mindcrung der Wechselfcstigkeitvon Fahrzeugfederblattendurch dieWalzhautForseh.3, 54—55. 33.2

(1938) Dynamische Dehnungsmcssungcnan cincr Lokomotive-PleuclstangeZ. Ver. Dtsch.lug. 82, Pt. 1, (19), 541—545. 42.1

LEHE F. and MASLANDER R. (1938) Influenceof round notchesand drilled holesonthe repeated bending strengthof bars with reduced sections (in German)Arch. Eiseuhtitteuw.11, 563—568. 63.1; 63.3

LaNE F. and PRACEEW. (1933) Dauerprufmaschincfür uberlagertcZug-Druck-und Schub-WechselbeanspruchungFarseh. Jug. Wes. Gel. 4 (5), 209—214.

31.13; 31.53LEHR F. and RUEP R. (1943)Bcitragczur Fragedcr Daucrhaltbarkeitder Kurbel-

wellcn von Gross-Dicselmotoren,MTZ 5 (11/12), 349—357. 31.43; 63.1LaME F. and ScHULz R. (1942) Dynamischc Dchnungsmessungenan ciner Last-

wagenhintcrachscAuto.-Teeh.Z. 45, 461—470. 42.1

na LasRssH. (1956) The fatigue testing of components—Ameansof revealingthedangerpoint in piecesorstructures,London ConL, Session2. Paper5. 28.1

LE55ELL5 J. M. andBRODEE5CsCR. F. (1956) Shot-pccningasprotectionof surface-damagedpropeller-bladematerials,London Conf., Session8. Paper1. 31.24;

32.4; 63.5LETNRR H. R. (1953) Applicationof optical interferenceto the studyof residual

surfacestressesProc. Soc. Exp. StressAual. 10 (2). 63.5LETNRR H. R. andSNYDER H.J. (1953) Grindingandlappingstressesin manganese

oil-hardeningtool steel Tram.Amer. Soc.Mech. Eugrs.75 (July). 63.5LEvEN M. M. (1948) A new material for three-dimensionalphoto-elasticityProc.

Soc. Exp.StressAual. 6 (1), 19—28. 44.1(1949) Stressesin kcyways by photoclastic methods and comparison withnumericalsolutionProc. Soc.Exp. StressAual. 7, 106—110. 44.1

(1950) Further propertiesof photoelastic fosteritc at elevated temperaturesProc. Soc.Exp. StressAual. 8, 141—153. 44.1

Lan’ J. C. and S5NCLA5R G. M. (1955) An investigationof strain aginginfatigue,ASTM PreprintNo. 70. 61.7

L5EBLE5N J. (1953)On theexactevaluationof thevariancesandcovariancesof orderstatistics in samplesfrom the extreme-valuedistribution Auu. Math. Statist. 24(2), 282—287. 90.42

(1954) A new method of analyzing extreme-valuedata, NACA TN 3053;AMR7, Rev. 3795. 90.42; 92; 94.1

(1955) On momentsof order statisticsfrom the Wcibuil distributionAnsi. Math.Statist.26 (2), 330—333. 90.42

LSEuLE5N J. andZELEN M. (1956) Statisticalinvestigationof thefatiguelife of deep-grooveball bearingsJ. Res.Nat. Bar. Staues’. 57 (5), 273—316. 90.42; 94.1

LSNCE J. R. (1958) Somedevelopmentsand applicationsof brittle lacquersAircr.Eugug.30, 94—100; Index aero. 129/14/5. 44.1

L5TTLEwOOD J. H. and MASKEEY C. (1953) Null method of measuringperiodicstrains Eugiueeriug,Loud. 175 (4546), 351—352. 42.21

Lsu S.J. (1949)The effectsof precompressionon thelow cyclefatigue behaviorofthe aluminumalloy 24S-T in directstress,CaseInst.ofTechnology,MetalsRes.Lab, TR 17. 22.1; 24.1

(1951)Fffectsof prccompressinnon the behaviorof thealuminum alloy 245-T4duringcyclic directstressingJ. Metals, N.Y. 3 (6), 452—456; AMR 5, Rev. 148.

24.1; 61.7Lsu S.J., LvNessJ. J.,RSPLsNC F.J. and SACHS G. (1948) Low cyclefatigueof the

aluminum alloy 24S-T in direct stress Trans. Amer. Just. Miu. (Metall.) Eugrs.175, 469—496; AMR 3, Rev. 78. 22.2; 51.11

Liovu F. H. (1952) Least-squaresestimationof location and scaleparametersusingorderstatistics Biometrika39, 88—95. 90.42

Loeivrs L. (1952) Programmedfatigue tests, variableamplitude rotating bendingtests(in Italian) Metallarg. ltal. 44 (4), 135—144; AMR 5, Rev.2363. 25.2; 32.4

(1956) Alternatebendingfatigue testswith superposedfrequencies(in French),StockholmConL, 160—168. 25.2

L0MA5 T. W., WARD J. 0., RAsT J. R. andCOLBEcK F. W. (1956) The influenceoffi equeneyof vibration on the endurancelimit of ferrousalloys at speedsup to150.000 cyclesper minuteusing a pneumaticresonancesystemLondon Conf.,Session4. Paper7. 31.26; 32.1; 64.3

LOTR5N M. (1956) Note on the sensitivity of leastsquaressolutionsJ. Math. Phys.35 (3), 309-311. 90.41

278279

n5BLsO GRAP HY BIBL500EAPS5Y

Lova R.J. (1952) The influenceof surfaceconditionon thefatiguestrengthof steel,Symp. Proper. metall. Surf., Inst. of Metals, (London), 161—196; AMR 6,Rev. 1268. 63.4

Lova W. J. (1952) Structuralchangesin ingot iron causedby plasticandrepeatedstressing,Univ. Ill. TAM, ProjectNR-031-005. 61.7

Low A. C. (1956) Short endurancefatigue, London Conf., Session2. Paper 15.22.2; 31.21; 64.1

LUB5N G. and W5NAN5 R. R. (1944) Preliminarystudieson a drop ball impactmachineBull. Amer.Soc. Test Mat. (128), 13—18. 32.6

LtssswsscP. (1931)Frmudung,Congr. mt. Ass. Test.Mat., Zurich, 1, 190—206. 62.4LUDwSK P. and SCMEU R. (1923) Das Verhaltcn der Metalle bei wiedcrholtcr

BeanspruchungZ. Ver. Dtsch.Jug. 67, 122—126. 85.1LUTMANDRR S. andWALLOERN G. (1944) Statiskaochdynamiskaprov pA knppel-

bultar av hOgvardigtmaterial,FFA Rep.4. 54.3LUTMANDRE S. and WALLOERN G. (1946) Bestamningav livslangdcn vid utmatt-

ningsprov mcdvariabla lastgranscr,FFA Rep.18. 82.1LfiTscss K. (1956) On theuseof notchedtestpiecesin materialtesting (in German),

Weirmewirtseh.11 (9), 252—257; Index aero. 112/12/12. 52.0

M

MACGRECORC. W. andGEossssANN. (1952)Fffectsof cyclic loadingon mechanicalbehaviorof 24S-T4 and 75S-T6aluminum alloys, MACA TN 2812; AMR 6,Rev. 1266. 24.2; 51.31; 52.1

MAcKs F. F. (1953) The fatiguespin rig—A new apparatusfor rapidly evaluatingmaterialsandlubricantsfor rolling contactLubric. Eugug.9 (5), 254—258. 32.5

MAIER A. F. (1934) Wechselbeanspruchungvon Rohrenunter InnendruckStahl u.Eiseu,Dtisseldorf54(50), 1289—1291. 31.6

MA5LANDRE R. (1936) Uber die Dauerfestigkeitvon Gusseisen,TempergussundStahlgussTech.Mitt. Krupp 3, 59—66. 61.8

(1939) FrgebnissevonDauerversuchenan StahlenTech.Mitt Krupp. A. 2, 8—15;Lilienthal-Ges.Ber. No. 116, 18. 31.23; 31.41

MA5LANDEE R.andBAUERSPRLDW. (1934)FinflussderProbengrossemud Probeuformauf die Dreh-Schwiegungsfestigkeitvon Stahl Tech. Mitt. Krapp 2, 143—152.

31.41MAJORs H., M5LL5 B. D. and MCGRRCOE C. W. (1949) Fatigueunder combined

pulsatingstressesJ. Appl. Meeh.16 (3), 269—276; AMR 3, Rev. 2662.31.6; 62.6

MALLORY G. W. (1946) Fatigue test for tire cord U.S. Pat 2412524. 33.1MAI.sjoss’sR M. J. (1949) Fffect of puLsating loadson the creep characteristicsof

aluminum alloy l4S-T Proc. Amer. Soc. Test. Mater. 49, 788—803; Al\’IR 4,Rev.693. 32.7

MANN J. Y. (1950) The effect of surface finish on thefatigue resistanceof 24S-Taluminum alloy, ARL (Melbourne), Rep. S.M. 147.

55.1; 56.2; 57.0; 63.4; 81.0(1953) The effect of stressconcentrationson the fatigue resistanceof 24S-Taluminium alloy ARL (Melbourne), Rep. SM 217. 52.1; 63.3

(1954) The effectof rateof cycling on thefatiguepropertiesof24S-T aluminiumalloy, ARL (Melbourne),Rep. 188. 51.31; 55.2; 56.1; 64.3

MANN J. Y. and MCMURRSCK R. P. (1950) New ideasin mechanicaltesting (2)A noteon high-speedfatigue testingAust.Eugr. 49. 64.3

MARCO S. M. andSTARKEY W. L. (1954) A conceptof fatiguedamageTrans. Amer.Soc. Meeh.Eugrs. 76, 627—632; AMR 7, Rev. 3217. 61.3

MAsonsJ. (1947) Biaxial tension—tensionfatiguestrengthsof metalsJ. Appl. Mccli.16, 383—388; AMR 3, Rev. 1947. 31.6

(1948) Somenew testingmachinesfor combinedstressexperiments,Fracturingof Metals,ASM, 189—200. 31.6

(l9

49a)Biaxial temion—tensionfatiguestrengthsof metalsAmer.Sac.Mech.Eugrs.49-APM-7. 62.6

(1949b) Biaxial tension-tensionfatiguestrengthof metalsJ. Appl. Mech. 16 (4),383—388. 31.6

(1956) Interpretationof fatiguestrengthsfor combinedstresses,London Conf.,Session2. Paper12. 62.8

MAR5N J. and HuossasW. P. (1952) Fatiguestrengthsof l4S-T4 aluminum alloysubjected to biaxial tensile stresses,NACA TN 2704; AMR 5, Rev. 3112.

31.6; 62.6MAESNJ. andSSusLsoNW. (1949) Biaxial fatiguestrengthof 24S-Talusninumalloy,

NACA TN 1889; AMR 3, Rev.1289. 31.6; 62.6MARK J. W. and GoLusassrssW. (1955) Barium titanatestraingaugesProc. Soc. Exp.

StressAual. 13 (1), 139—150; Index acro. 124/12/6. 43.3MARKOwETz M. P., SBSJANJ.A. andMscssajawN.J. (1949) Maschinezur Prufung

der lliegewechselfestigkcitbci hohen TemperaturenSaw.Labor. 15 (1), 82—85.32.2

MAET5N D. F. (1957) Fvaluatiors of methods for measurementof residualstress,SAF TR-l47. 63.5

MASON W. (1917) Alternating stressexperimentsEugiueeriug, Loud. Pt. 1, 187—190,211—214. 31.41; 35.2

MAsoN W. P. and TsoUsosToNR. N. (1957) Use of piezoresistivematerialsin themeasurementof displacement,force and torque J. Acoust.Soc. Amer. 29 (20),1096—1101; Index aero.132/14/2. 41.21; 43.21

MATTMAL5 K. (1933) Fine Planbiegc-DauerprufmaschinederDVL und die damiterhaltcncn VersuchsergebnisseMetallwirtschafi 12, 485—488; Z. Ver. Dtsch.Jug.77, 27—28. 31.21

(1935) Fine S-t-Zug-Druck-Daucrprufmaschineder DVL Lqftfahrtfarsch. 12 (2),87—88. 31.11

MATTSON R. L. (1956)Fatigue, residualstressesand surfacecold working, LondonConf., Session7. Paper5. 63.5

MATTSONR. and COLEMAN IV. 5. (1954)Fffeet ofshutpeeningvariablesandresidualstresseson the fatigue life of leaf spring specimensTraus. Soc. Automat. Eugrs.,N.L62. 61.5

MCADAM D.J. (1920) A high speedalternatingtorsion testing-machineProc. Amer.Soc. TestMater. 20, Pt. 2, 366—371. 31.41

(1921) Fudurance of steel under repeated stressesChem. Metall. Eugug. 25,1081—1087. 31.32; 51.31; 91.0

(1923)Fndurancepropertiesof steel; their relationto otherphysicalproperties.and to chemicalcomposition Proc. Amer. Soc. Test. Mater. 23, Pt. 2, 56—105.

26; 91.0(l9

24

a) Accelerated fatigue tests and some endurancepropertiesof metalsProc. Amer.Soc. Test.Mater. 24, Pt. 2, 459—475. 26; 35.2

(I 924b) The endurancerange of steel Proc. Amer. Soc. Test. Mater. 24, Pt II,574—600. 85.2

280 281

BIBLIOGRAPHY

MCADAM D.J. (1926) Stress—strain—cyclerelationshipandcorrosion-fatigueofmetalsProc. Amer.Soc. Test. Mater. 26, Pt. 2, 225—254. 32.3; 65.4; 91.0

(1927a) Corrosion fRtigue of metalsasaffected by chemicalcomposition,heattreatmentandcold working Trans.Amer. Soc.Steel Treat. 11 (5), 355—390. 32.3

(1927b) Fatigueand corrosion-fatigueof metalsCongr. mt. Ass. Test. Mat. 7,Congr.,Amsterdam1, 305—358. 32.3; 65.4

(1927c) Corrosion fatigueof non-ferrousmetalsProc. Anser. Soc. Test. Mater. 27(2), 102—127. 32.3; 65.4

MCCLaNnON E. W., KLASJER L. W. and DsssroA. R. (1952) DeterminationofexpectedF-89C load-life history andrecommendedspectrumfor repeatedloadtestsof F-89Cwing, Northrop.Aircraft Inc. Rep.SRR-33. 54.3; 54.6

MeCLsreroescF. A. (1955a) The statistical theory of size and shape effects infatigue, ASME PaperNo. 55. 63.1 63.3

(l955b) A criterion for minimum scatterin fatigue testing,ASME PaperNo.55-APM-26. 63.2

(1956a) Variability in fatigue testing, sourcesand effect on notch sensitivity,StockholmConf., 171—177. 63.2

(1956b) The growth of fatigue cracks under plastic torsion, London Conf.,Session6. Paper6. 27

MCEvsLY A.J.JR.,ILLcs W.andHARnRATH H. F.(1956) Staticstrengthofaluminum-alloy specimenscontaining fatigue cracks, NACA TN 3816; Index aero.117/12/12. 52; 63.3

McGTJ5GAN M. J. (1953) Interim report on a fatigue inYestigation of full-scaletransportaircraft wing structure,NACA TN 2920. 33.5

MeGusoAN M. J.,Bav~s.ssD. F. andWHALEY R. E. (1954) Fatigue investigationoffull-scaletransport-airplanewings, NACA TN 3190. 33.5

McKxowso J. and BLACK L. H. (1948) A rotating-load, elevated temperaturefatigue-testingmachine Metallurgica, Manchr.38, 247—254; AMR 2, Rev. 747.

31.32; 32.2MCMAsTER R. C. and WarestS. A. (l951a) Nondestructivetesting of engineering

materialsandpartsMater. & Meth. 33, 8 1—96. 40(1951b)A basicguidefor management’schoiceof non-destructivetestingin theeconomicsof production,ASTM STP No. 112. 40

MCPHERsON A. E. (1952) A dual-amplitudeaxial-loadfatigue machine Proc. Soc.Exp. StressAnal. 10 (2), 143—152; AMR 6, Rev.2786. 31.11; 32.4

MRER H. P. YAH, and PLANTEMA F. J. (1949) Fatigueof structuresandstructuralmembers(in Dutch), NLL Rap.357; AMR 3, Rev. 1270. 33.4

MRLDAHL A. (1939) The Brown-Boveri testingapparatusfor gearwheel materialEngineering,Lond. (July), 63—65. 32.5

MENTER J. W. (1952)Directexaminationofsolidsurfacesusingacommercialelectronmicroscopein reflectionJ. Inst. Met. 81, 163—168. 45.5(1953) Direct observation of solid surfacesat higl resolution by reflectionelectronmicroscopeJ. PhotographicSd. (London), 1, 12—20. 45.5

MEREDSTH R. and PHELAN A. J. (1948) Hollow bladesfor axial flow compressorsMetal Progr. 841—847. 31.26

MEYER J. H. (1954) Test developmentof ~tructures designed under-strengthAeronaut.Engng.Rev.13, 54—64; AMR 8, Rev. 3348. 33.4

MILE5 J. W. (1954) On structural fatigue under randomloadingJ. Aero. Sd. 21,753—762. 25.2

MILLARn D. J. (1955) The cracking of layers of hrittle material by differentialstrains Brit. J. Appl. Phys. 6 (4), 124-127; AMR 8, Rev.3067. 46.5

B5 B L5O C RAP HY

M5NnL5N R. D. (1947) Stressdistributionaroundaholeneartheedgeofaplateundertension Proc. Soc. .Exp.StressAnal. 5 (2). 52.2; 63.3

M5NER M. A. (1945) Experimental verification of cumulative fatigue damageAutomat. Aviat. Indsstr.93, 20—24. 24.2

MOHR F. (1923) NeuzeitlichePrüfmasehinenund PrilfeinrichtungenZ. Ver. Dtsch.lug. 67, Pt. 1, 336—340. 31.11

MOLYNEUX W. G.and BROADBENTE. G. (1946)Groundresonancetestingofaircraft,Rep.Memo, aero.Res. Comic. London,No. 2155, 1—26; AMR 2, Rev. 248.

33.5Moonv E. S. and DaNRHv D. R. (1954) Recent strain gauge developmentsat

A.R.L., ARL, Melbourne, SM 211; AMR 8, Rev.2657. 43.21Mooaa A. J. W. (1948) A refinedmetallographictechniquefor the examinationof

surfacecontoursandsurfacestructureof metalsMetallurgica, Manchr. 38 (224),71—74. 45.2; 56.2

MooRE D. 5. (1956) A wide application control equipmentfor fatigue testing,Eng. El. Co. Ltd., Aircr. Div. ElectronicsDepartmentRep.No. 071/4.

33.4; 34.1; 34.4MOORE H. F. (1925)StudyingthefatigueofmetalsAmer.Mach.,N.Y.62,563—565. 20

(1936) How and when does a fatigue crack start? Metals & Alloys 7, (11),297—299. 27

(1941) Effect of typeof testingmachineon fatigue testresultsProc. Amer.Soc. Test.Mater. 51, 133—153. 64.2

(1945) A study of size effect and notch sensitivity in fatigue testsof steelProc.Amcr. Soc. Test. Mater. 45, 507—531. 63.1

MOORE H. F. and ALLEMAN N. J. (1931) Progressreport on fatigue testsof lowcarbon steel at elevated temperaturesProc. Amer. Soc. Test. Mater. 31,114—121. 31.32

MOORE H. F., Dot.AN T. J. and HANLEY B. C. (1948) The effect of sizeand notchsensitivity on fatigue characteristicsof two metallic materials, Air Force Tech.Rep.No. 5726. 61.6

MooRE H. F. and JAss’aR T. M. (1923) An investigationof the fatigueof metals.Seriesof 1922, Univ. Ill. Engng., Exp. Sta.Bull. No. 136, 1—97.

62.3; 82.2; 91.0(lti24a) Investigationof thefatigueof metals: Seriesof 1923, Univ. Ill., Engng.,Exp. Sta. Bull. 20 (37), 19—21, 21 (142),86 pp. Stahl a. Eisen, Düsseldorf45,237—238. 23.21; 31.11; 96.0

(1 924b) Evide,,ee for the endurancelimit, Engineering, Loud. 118, 580—582;658—660. 95.0

(1925) An investigation of the fatigue of metals, Univ. Ill., Engng. Exp. Sta.Bull. 152. - 65.1

MOORE H. F. andJOROANR. L. (1939) Stressconcentrationin steelshaftwith semi-circularnotches,Proc. Fifth lot. Cong. Appl. Mech., 188—192. 52.1

MOORE H. F. andKOMMERI J. B. (1921) An investigationof the fatigueof metals,Univ. Ill., Engng.Exp. Sta. Bull. 124. 31.41; 32.6; 50; 95.0

MOORE H. F.. K0MMEE5 J. B. and JAsPER T. M. (1922) Fatigueor progressivefailure of metals underrepeatedstress Proc. Amer. Soc. Test. Mater. 22, Pt. 2,266—311. 85.2

MOORE H. F. and KROUIE G. N. (1934) Repeated-stress(fatigue) testingmachinesused in the Materials Testing Laboratoryof the University of Illinois, Univ.Ill., Engng.Exp. Sta. Cire. No. 23, 7—36. 31.11; 31.32

282283

BIBLIOGRAPHY BIBLIOGRAPHY

Mooaz H. F. andMORKOVsN D. (1943) Secondprogressreport on the effect of sizeof specimenon fatiguestrengthof threetypesofsteelProc. Amer.Soc. Test. Mater.43, 109—124. 63.1

Mooste H. F. andPunSAN W. J. (1919) Fffect of cold working and of rest on theresistanceof steelto fatigue underreversedstressBull. Amer.Just. Miu. (Metall.)Eugrs. (146), 391—404. 66.3

Mooax H. F. andSEELY F. B. (1915) The failure of materialsunderrepeatedstressProc. Amer. Soc. Test. Mater. 15, Pt. 2, 438—462. 82.1; 85.2

(1916) Constantsand diagramsfor repeatedstresscalculationsProc. Amer. Soc.Test.Mater. 16, Pt. 2, 470-475. 82.1; 85.2

Mooaa H. F. and WI5HART H. B. (1933) An ‘overnight’ test for determiningendurancelimit Proc. Amer.Soc. Test. Mater. 33, Pt. 2, 334—347. 23.11; 95 -

Mooaa R. L. and HILL H. N. (1945) Comparativefatigue testsof rivetedjoints ofalclad 24S-T, alclad 245-T81, alelad 24S-RT, alclad 24S-T86, and alciad75S-Tsheet,NACA RB 5 F 11 (WR W-76). 54.12

MoRssawAG. K. and GRsFnL. (1945) The biaxial fatiguestrengthof low carbonsteelsWeld.J. Res.Suppt.24, 167—174. 31.6

MostscovssoD. and MooaE,H. F. (1944) Third progressreporton the effect of sizeof specimenon fatiguestrengthof threetypesof steelProc. Amer.Soc.Test. Mater.44, 137—158. 61.6

MosuossD. 0. (1947) Compositionand physical propertiesof steel in relation tofatigueMelbourneSymp.,336—361. 61.1; 61.8

MossassoNJ. L. M. (1939) The yield of mild steelwith particularreferenceto theeffect of sizeof specimenProc. Justu.Mech. Eager., Loud. 142, 193—223. 34.2

MosoassowJ.L. M., CaossI.AssnB. andPARRYJ.S. C. (1956) Fatigueundertriaxialstress: Developmentof a testingmachine andpreliminary resultsProc. Justu.Mech. Eugrs., Loud. 170 (21); Index aero102/12/7. 31.6; 34.2; 62.6; 65.3

MOSTELLERF. (1948) On poolingdataJ. Amer. Statist. Ass. 43, 231—242. 72Mua~swR. B. (1948) Non-parametrictolerance limits Auu. Math. Statist. 19,

581—589. 60.7MULLER W. (1937) A new methodof investigatingthe fatiguestrengthof riveted

andweldedjoints Schweiz.Arch. 3 (10), 276—279. 21.1; 31.24MULLER-STOCK H. (1938) Der Finfluss dauerndund unterbrochenwirkender,

schwingcnderUberbeanspruchungauf die Fntwicklung des DauerbruchsMitt. Kohle- u. Eiseuforschg.2 (2), 83—107. 24.2

MULLER-STOCK H., GEROLD F. andSCHULZ F. H. (1938)DerFinflusseinerWechsel-vorbeanspruchungauf Biegezeit- und Biegewechselfcstigkeitvon Stahl St. 37Arch. Eiseuhtitteuw.12, 141—148. 24.2

MULLER H. and HEMPEL M. (1938) Wechselbeauspruchungund Kristallzustand.II. Zur Fragc des Kristallverformungbeim DauerbruchMitt. K.- Wilh.-Just.Eiseuforsch.20, 229—238. 61.2

(1955) AnderungendesKristallzustandesdurch WechaelbeassspruchungForsch.Jug.-Wes. 21 (3), 96—97. 61.7

N

NA5R K. R. and BANEKJEE K. S. (1943) A note on fitting of straight lines in bothvariablesare subjectto error Saukhya~6, 331. 90.41

NALE5ZICIE%vICZ J. (1948) On the computationof endurancelimit stresses,Proc.Seventhmt. Congr. Appl. Mech. 4, 190—193; AMR 4, Rev. 682. 95.0

NELsONH. R. (1940)Proc.Coni. on Friction andSurfaceFinish,MIT, 217. 45.2

NaLssoN L. F. (1957) Ytbearbetningensinverkan ph utmattningshhllfastheten,(With a sumsnaryin Fnglish), KTH, Stockholm, Inst. for hhllfasthetslara,Stockholm. 63.4

NEWMAN R. P. and C0ATE5 G. (1956) Fatiguetestson thin-gaugebox-sectionbeams,London CooL, Session9. Paper2. 31.23; 33.4

NEWMARK N. M., MosBoRGR.J., Munsa W. H. andFLL5NG R. F. (1951) Fatiguetestsin axial compressionProc. Amer. Soc. Test. Mater. 51, 792—810. 62.1

NEYHAN J. (1934) On the two different aspectsof the representativemethod: themethod of stratified sampling and the method of purposiveselection J. Roy.statist.Sac.91, 558—606. 72

NssusNAaAT. andKAWAMOTO M. (1940)Fatiguetestsofsteelundercombinedbend-ing andtorsionSoc. Mech.Eug.(Japau)6 (24). 62.5

NI5HINARA T. andKAwAHOTO M. (1943) Metallwirtschafl22, 337. 31.51N555O5HANAT. and YAMADA T. (1950) The fatigue strengthof metallic materials

under alternating stressesof varying amplitude Japan ScienceReview 1 (3),1—6. 32.4

NoRRIs D. J. (1948) The measurementof finely finished metallic surfaces,CSIRDivision of Aeronautics,S & M Note 166. 45.2; 56.2

NoRsusG. M. (1953) Fifeet of mean stresson the fatigue strengthof D.T.D. 364round bars with and without transversal holes, ARC Curr. Pap. CP 120;Index Acm. 51/9/9. 85.2

0

OAscsJ. K. and howELL P. B. (1956) Somework on tensionpadsfor structuraltests,Aero. res. Coun. curr. Pap. (CP238/ARC 18904); Index aero.99/12/7.

34.2OBEROT. T. andJoHNsoNJ. B. (1936) Fffect of grain flow on mechanicalproperties

of forged èrankshaft,A.A.F. TechnicalRep.No. M2916. 61.8(1937) Fatiguepropertiesof metalsused in aircraft constructionat 3450 and10600cyclesProc. Amer. Soc. Test. Mater. 37, Pt. 2, 195—205. 31.32; 64.3

OmanT. T. andROONEY R. J. (1949a)Fatiguecharacteristicsof aluroinumalloy75S-T6platein reversedbendingasaffectedby typeof machineandspecimenProc. Amer. Soc. Test. Mater. 49, 804—814; AMR 4, Rev. 1199. 63.2

(1949b) Reversed bending fatigue characteristics of steel and high strengthaluminum alloys as affected by type of machine and specimen; Part I—Fxtruded aluminum alloys and rolled 4130 steelplate; Part Il—Aluminumalloy 755-T6 plate,A.A.F. Teclsn.Rep.No. 5775. 63.2

OBERC ~f 1. and TRAP? W. (1951) High-stressfatigueof alloy steelsProd, Eugag.22 (1) 159—161; AMR 4, Rev. 1591. 62.2

O’Cor’srsoR H. C. and M0RRHON J. L. M. (1956) The effect of meanstresson thepush-pull fatiguepropertiesof analloy steel,LondonConf., Session2, Paper3.

34.1; 2,6; 36; 62.1OuINO J. A. (1955) Metallovcdenijei obrabotka metallow Do/cl. A/cad. Nazi/c SSSR

105 (6). 91.0ODsNuJ. A. and IvANovA V. S. (1956) Fatigueof metalsunder contactfriction,

London Covsf., Session4. Paper 11. 32.3; 65.5OscuisoH. (1953) Determinationof the surface stressby meansof electroplating

J. AppI. Phys.24 (9), 1130—1133; AMR 7, Rev. 735. 44.1ONO A. (1929) Fatigue of steel under combinedbendingand torsion Mem. Colt.

Eugug.Kyusho2 (2), 117—142. 31.54

284 285

BIBLIOGRAPHY

OscssATzH. (1934) A fatigue testing machinefor determiningthe enduranceofspecimensand constructional parts (in German) Metallwirtschaft 13 (25),443—448. 33.4

O5cHATZ H. (1936) Prufmaschincnzur Frmittlung der DauerfestigkeitZ. Ver.Dtsch.Jug. 80, 1433—1439. 31.13; 31.41; 31.54

(1940) Ventilfedcr-Prufmaschine Z. Ver. Disc/i. Jug. 84 (33), 598—598. 33.2(1943) Metallwirtsc/saft22, 558—559. 31.12

OnszscY K. (1936) Dr.-Ing. Diss. TH. Wien. 31.21(1938) Dauerbiegeversuche an gewirskeltcn Flachstaben Z. Ver. Dtsch. Jug. 82,501—502. 31.21

OUvERKERK L. vAN (1958) Therelativeadvantageandlimitations of nondestructivetestingmethodsNou-Destr. Test. 16 (2), 113—127; Index aero.116/14/8. 20

P

PALHGREN A. (1924) Die Lebcnsdauervon KugellagernZ. Ver. Dtsch. Jug. 68 (14),339—341. 85.1

PAstrnm T. F., MELCH0RJ. L. andGoonW. B. (1950) Fnergy losses and fractureof somemetalsresultingfrom a small numberof cyclesof strain Proc. Soc. Exp.StressAnal. 7, 27—29; AMR 4, Rev. 236. 22.2

PARRY J. S. C. (1956) Further resultsof fatigueundertriaxial stress,LondonConf.,Session2. Paper7. 31.6; 62.6; 65.3

PATCHING C. A. (1951) Interim noteon repeatedload testing of MustangP-5lDwings, ARL, Melbourne, S & M Note 189. 33.5

PAUL J. A. and BRssTowJ. R. (1952) Torsionalfatiguemachinewith torquecontrolEngineering,Loud. 173 (4484),25—28. 31.41; 31.43

PAyNE A. 0. (1956a) Random and programmedload sequencefatigue tests on24STaluminumalloy wings,ARL, Melbourne,Rep.SM. 244; Acro. Fngng.Rev.2 (2), 147. 54.6

(1956b) An investigation into the fatigue characteristicsof a typical 24S-Taluminiumalloy wing, LondonConf., Session8. Paper3. 33.5; 54.6

PEARCEJ. F.(1952)A modifiedBudenbergbalanceJ. Sci.Justrum.29 (1), 18—19. 34.3PERCWAL A. L. and WEeK R. (1947) Fatigue tests by the resonancevibration

methodon four weldedH-beamsRep.Brit. Weld.Res.Ass. FE 8/33.31.23; 33.4; 34.4

PERLEw5TZ K. (1911) NeueelektrischeMaterialprufmaschineZ. Ver. Dtsch. Jug. 55,Pt. 2, 1445—1446. 31.14

PETERSON R. F. (1930) Fatigue testsof small specimenswitls par icular referencetosize effect Amer. Soc. Steel Treat. 18, 1041—1056. 31.32; 61.6; 63.1

(1937) Nomenclatureon rangein stressin fatigueProc. Atuer. Soc. Test.Mater. 37,Pt. 1, 162—163. 82.2

(1938) Methods of correlating data from fatigue tests of stressconcentrationspecimens,StephenTimoshenkoSixtiethAnniversary, 179—183. 63.3

(1945) Relation between life testing and conventional tests of material Bull.Amer. Soc. Test.Mat. (133), 9—16. 20; 63.3

(l949a) Approximate statistical method for fatigue data Bit/i. Amer. Soc. Test.Mat. (156, 158), 50—52, 62; AMR4, Rev. 1880. 91.0

(1949b) Application of fatigue data to machine design, ASSE PubI. Propertiesof Metals in Materials Fngineering. 63.1

(l952a) Brittle fracture and fatigue in machinery, MIT Symp.,74—102. 62.1;85.2(l952b) Review of the fatigue ofmaterialsfield, AMR 5, (1). leaturearticle. 20

B5 B L 100 RAP Fl Y

PETERSONR. F. and WABL A. M. (1935) Fatigueof shaftsat fitted memberswith arelatedphotoelasticanalysisJ. Appl. Mech.2 (1), Al—All. 26.5; 32.3; 65.5

(1936)Two- andthree-dimensionalcasesof stressconcentrationsandcomparisonwith fatigue testsJ. AppI. Mech.3 (1), A15—A22. 52.1; 52.2

PtssLuq’H. A. v. (1942)Forsch.Jag.-Wes. 13, 169—171. 35.2PHILLIPs C. F. and FENNEEA. J. (1951) Somefatigue testson aluminium-alloyand

mild-steel sheet, with and without drilled holes, Inst. Mech. Fngincers,Meeting. 63.1; 63.3

PHILLIPs C. F. andHn’wooo R. B. (1951) The size effect in fatigue of plain andnotchedsteelspecimensloadedunder reverseddirect stressProc. Jnstss. Mech.Engrs.,Land. 176, 113. 63.1

PH5LL5P5C. F. and THUR5T0NR. C. A. (1951) A noteon a rotatingbending-fatiguemachinefor testsat200°C,ARC, TR 2674 (8592), N 13047. 32.2

PsaRs’owr W. G. (1947) Fatiguetests of major aircraft structural componentsProc.Soc. Ezp. StressAnal. 4 (2), 1—15. 25.1; 54.6

PIRRL J. and vo~ LAIZNER H. (1938) Wechselfestigkeits-Prufmaschine mit AntriebdurchbandgefuhrteDiffcrentialrollen Arch. EisenhOttenw.12 (6), 305—308. 31.11

PsscssEs.W. (1953) Bcrucksichtigung des Finflusses der schwingendenMassenArch. Eiseuhutteow.24 (1/2), 89—91. 35.2

PLANTEMA F. J. (1956) Some investigationson cumulative damage,StockholmConf., 2 18—228. - 24.2

POHL R. (1932) MechaoischcProblemebci grossenTurbogcneratorenElectrotech.Z.53, Pt. 2, 1099—1101. 82.2

POHEYJ. andANCELLE A. (1935/36) Introduction a l’dtudc de Ia fatigue-corrosionMm. Comm.Etud. Corras. 17—42. 61.9; 65.4

POHP A. (1938) Verhaltendes Stahies bci erhohten Temperaturen. Uebersichtuber das SchriptumdesJahres1937 Stahl is. Eiseu,Düsseldorf58, 432—435. 65.1

POHP A. andDUCKw5rx C. A. (1931) Fndurance tests of steel wires under fluctuatingtensile stresses(in Ccrman) Mitt. K.- Wilh.-Just.Eiseuforsch.13 (5), 79—91. 33.1

POMP A. andFNDER5 W. (1931) Rapidmethodsof determiningenduranceof metals(in German)Z. bayer. (Dampf/c.)Revis. Ver., 35, 26—29; Stahl is. Eisen,Düsseldorf51, 157—162. 26

POMP A. and HEMPEL M. (1933) Untersucbungenan Stahlstabenbei wecbselnderZugbeanspruchungMitt. K.-Wilh.-Jnst. Eiseufarsch.15, 247—254. 31.15

(I 936a) Dauerfestigkeitsschaubildervon Stahlen bci verschiedenenZugmittel-spannungcu unter Berticksicistigung der Prtifstabform Mitt. K.- Wilh.-Jnstr.Eisessforsch.18 (1), 1—14. 62.1; 63.2; 82.2

(1936b) Daocrfcstigkcitsschaubildervon gckcrbtcnund kaltverformten Stählensowic von l”—und 1k”—Schraubenbei verschiedenenZugmittel—Spannungen

Mitt. K.-Wilh.-Jmt.Eiseufarsch.18, 205—215. 31.15; 62.1(1938) Daucrprufungvon Stahldrahtenunter wechsclnderZugbeanspruchung.II. Fiofluss der Zichbedingungenaufdie Zug-schwelffestigkeitvon StahldrahtMitt. K.- Wilh.-Just.Eisenfarsch.20 (1), 1—14. 33.1

(1940a) Ubcr die Daucrhaltbarkeitvon Schraubenfedernmit und ohm Obcr-flächcoverletzungcnMitt. K.-Wilh.-lnst. Eiseufarsch.22, 35—56. 63.4

(1940b) UebcrdasVtrhaltenvon GusseiseGund TempergussunterwecbselnderBeanspruchungMitt. K.-Wilh.-Jnst.Eiseaforsch.22 (11), 169—201. 62.1; 82.2

(l942a) Dauerversuche an Stahlen bei tiefen Temperaturen, Dtsch. Luftfahrt-forschg, Ber. 1704/1, 1—64. 65.1

(l942b) Daucrfestigkeit des Stahles bei erhohtenTemperaturen, Mitt. Dtsch.Akad. Luftfahrtforschg, (5), 235—260. 65.1

286 287

BIBLIOGRAPHY BIBLIOGRAPHY

POHP A. andHEHPEL M. (1949) Bruchhaufigkeit undObcrflachengutcvon Schrau-benfcdern, Mitt. MPI Fisenforschg,Abh. 505; Arch. Eiseuhütteuw.20 (11/12),385—393; AMR 3, Rev. 1870. 63.4

(1950a) WechselfestigkeitundKerbwirkungszahlcnvon unlegiertenund IegiertcnBaustahlenbei +20°und —78°Arch. Eisenhüttcnw.21 (1/2), 53—66. 63.3; 65.1

(l950b) Dauerfcstigkeitvon Schraubenfedernbei erhohterTemperatur,Mitt.MPI Fiscnforschg, Abh. 517; Arch. Eisen/sütteaw.21, 263—272. 65.1

POPEJ. A. and BARs0N C. W. (1956) Strength reduction factors for small quenchingcracksandfor decarburizedsteel,London Conf., Session 6. Papers 10. 63.3

POPE J. A., FOSTER B. K. andBLOOHER N. T. (1957) Limited life design: A surveyof the problemEngiueering, Load. 184 (4772—4773—),236—241, 275—278; Indexaero.122/13/10,123/13/10. 90 7

POWELL A. (1955) The problem of structural failure due to jet noise, ARC 17514.25.2

POwELL R. W. (1946) A failure-sequenceindicator for static testspecimensTrans.Amer. Soc.Mech.Ears. 68 (7). 46.2

PROT F. M. (1937) Unnouveau type tie machine d’essai desmbtauxa lafatigueparflexion rotative Rev.Métall. 34, 440—442. 31.32; 31.42; 32.4

(1947) L’essai de fatigue sous chargeprogressiveC. R. Acad. Sci., Paris 225,669—671; AMR 1, Rev. 111. 23.22; 96.2

(l948a) Une nouvelle technique d’essai des materiaux—L’essai de fatigue sonscharge progressive Ann.PoutsChauss.118,441-464; AMR 2, Rev.318.

23.22; 96.2(l948b) L’essai de fatigue sous chargeprogressive.—Unenouvelle technique

- d’essaide matcriauxRev.Méta/l. 45 (12), 481—489; 48 (11), 822—824; AMR3, Rev. 902. 23.22; 96.2

PUcBNER 0. (1946) The production of synchronous superimposedalternatingbending and torsional loads (in German) Schweiz.Arch. 12, 289—293. 31.51

(1948) Zur Dauerhaltbarkeitvon Formelementender Welle bci uberlagerterwecbselnderBiege-undVerdrehbeanspruchungSchweiz.Arch. 14, 217—229. 62.5

(1951) Fatiguestrengthof transversallyboredshaftsundercombinedstaticalandalternatebendingand torsionstress(in German)Sehweiz.Arch. 17 (2), 46—63;AMR 4, Rev. 3180. 62.5

0

QUINLAN F. B. (1946) Pneumatic fatigue machines, ASTM Techn. PubI. (72),41—45; Proc. Amer. Soc. TestMater. 46, 846—851. 31.26; 31.46

(1947) Pneumaticfatigue testing Autazuat.Aria!. Judustr.96 (2), 30—31. 31.26

R

RAs’s°M. 5. (1956) On approximatingthe point binomialJ. Amer.Statist. Ass. 51,293—303. 90.3

RA5THBY K. D. (1951)Fatiguetestson typical two sparlight alloy structures(Meteor4 tailplanes)underreversedloading,RAF Rep.No. Structures108. 33.5; 54.6

RAITBBY K. R. and LONG50N J. (1956) Somefatiguecharacteristicsof a two sparlight alloy structure—(Mctcor4 tailplane),ARC CP258; Jut. Acm.Abstr., 1(11), 144. 62.2

RA0 C. V. J. and STREENATHL. S. (1953) Designof low frequencyfatigue testingmachinesJ.JudianJust.Sei.,35 (2), 87—92; AMR 7, Rev. 795. 32.1

RANsOM J. T. (1954) The effect of inclusionson the fatiguestrengthof SAF 4340steels Trans. Amer. Soc. Metals46, 1254—1269. 61.3; 61.8

(1955)A guide to statisticalmethodsfor usein fatigue testing,StockholmConf.,229—234. 90.0

RANSOMJ. T. and MEHL R. F. (1949) The statisticalnatureof the endurancelimitJ. Metals, N. V. 185, 364-365. 95

(1952) TIse anisotropyof thefatigue propertiesof SAF 4340 steelforgingsProc.Amer.Soc. Test. Mater. 52, 779—790. 61.8

(1953)The statisticalnatureof thefatiguepropertiesof SAF 4340 steelforgings,ASTM STP.No. 137. 61.8

RATHER K. (1931) Universalprtifmaschinefür DauerwcchselbelastungZ. Ver. Dtsch.Jug. 75, Pt. 2, 1289. 31.15

RAv5LLY F. (1938) Contributionsa l’dtudede Ia rupture des fils mbtalliquessousnisa des torsions alterneesPubI. Sri. Miuist. Air No. 120. 82.1

REAsONR. F., HOPEIN5 M. R. andGARsconR.J. (1944)Reporton measurementofsurfacefinish by stylus method,Taylur-Hobson, Leiccstcr,Fngland. 45.1

REGnIossA. and FERA A. (1953) Characteristicsof metalsat high temperatures(in Italian) Ternsotecuica7 (7), 279—289; AMR 7, Rev. 1126. 32.2

REYNoLDs 0. and SMITH J. H. (1902) On a throw testingmachinefor reversalsofmeanstressPhil. Trans. SeriesA, 199,265—297. 31.13

RICHART F. F. JR. and NEwHAEK N. M. (1948) Cumulativedamagein fatigue,Univ. Ill. FngngFxp. Stat., Off. Naval Res. Contr. 24.2

R5OLAND D. M. (1954) The M.A.F.F. recording accelerometer,ARC curr. Paper177; AMR8, Rev.3504. 43.1; 48.1

R5PPEROER F. A. (1954) A piezoclectricstrain gaugeProc. Soc.Exp. StressAnal. 12(1), 117—124; Index aero.86/12/4. 43.3

ROBBIN5 H. (1944) On distribution-freetolerancelimits in randomsamplingAnn.Math. Statist 15,214-216. 71; 90.7

RoaasEsH. and M0NR0 S. (1951) A stochasticapproximationmethodAnn. Math.Statist. 22 (3) 400—407. 23.12; 95.2

ROBERTSA. M. and GREGORYA. A. (1951) Vibration test equipment for turbinebladesEngineer, Load. 191 (4965), 370—372. 31.24

RoBERTs H. C.andMCDoNALD V. J. (1954)Controlandprogrammingofa200,000-poundfatiguemachineProc. Sac.Exp.StressAnal. 11 (2), 1—10. 31.11

ROBERTS M. H. (1952) Precisemeasurementof fatigue load Metallurgia, Mane/jr. 46,107—1 14. 34.3

ROBERTS M. H. and NORTHCL5FFE J. (1947) Measurementof Young’smodulusathigh temperaturesJ. Jrou St. Just. 157, 345—348. 31.26

R0E5LI A., LOEwER A. C. and FNEY W.J. (1954) Machine to apply repeatedloadsto large flexural membersBull. Amer. Sac. Test. Mat. (196), 50—53; AMR 7,Rev. 3889. 33.4

R0MUALOI J. P., CFIANG C. L. and WestC. F. (1954) A fatigue testingmachineforrangeof stressBnll. Amer. Soc. Test.Mat. (200),39-43. 31.32

RONDELL J. H. and DUYN G. C. (1950) A ‘solid-guidefixture’ for determiningtheproperties of thin sheetmaterial in compression,NLL Rep. S368; AMR 4,Rev. 2493. 34.2

Roos0. J. (1912) Somestatic and dynamic endurancetests Proc. Jut. Ass. TestMater. Paper V 26. 32.6

RoosP. K. LEMHON D. C. and RAN50N J. T. (1949) Influenceof typeof machine,range of speed,and specimenshapeon fatigue test data Bull. Amer. Soc. Test.Mat. (158), 63—65; AMR 4, Rev. 1590. 63.2; 64.3

288 289

BIBLIOGRAPHY

Rog M. (1950) Ermüdungsversuche mit Hohlstabcn am reinen Schweissgut,‘Acros-Stabilend-B’ und ‘Acros-Ductilend-55’ bei mehraehsigenSpannungs-zustandenSchweiz.Arch. 16, 193—199; AMR 4, Rev. 1594. 62.6

Ro M. andEICNSNGER A. (1950) Die BruchgefahrfesterKorper bei wiederholtcnBeanspruchung-Frmtidung,FMPA Bull., (173), 102 pp. 31.6; 63.2

RoSEN C. G. A. and KING R. (1946) Someaspectsof fatigue in dieselenginepartsProc. Sac.Exp. StressAnal. 3, 152—160. 31.43

R05EssH0LTE J. L. and Ss~ssTs-sD. T. (1952) Dilastrain method for determiningendurancelimit of materialsMetal Pmagm.61 (2) 85—88. 26

ROSENTHAL D., SsrcasG. and ZxzscAs G. (1949) Fffcct of residual compressiononfatigueWeld. Res.Suppl. 14, 98—103;AMR 3, Rev. 278. 24.1

Rossscr-rsU. (1953) Fatiguestrengthof wire ropes. Fndurancetestundercombinedbendingandtension (in Italian) Jngegueme27 (7), 769—771; AMR 7, Rev. 746.

33.1RossvNoG. F.von (1942)Thebendingfatiguestrengthin transverseand longitudinal

directions (in German) Arch. Eisenhütteuw.15, 407—412. 61.8ROUCHET M. (1934) Study of endurance limit phenomena (in French) UsineFranc.

43, 37. 62.4Row~nF. F. (1913) Flastiehysteresisin steelProc. Ray.Sac.89, 528—543 31.41Ruisns S. (1958) Responseof complexstructuresfrom reed-gaugedata, ASMF

Prep.(58-APM-15); Index aero. 107/14/11. 41.1RUGE A. C. (1956) Force and weightstandardsgain new importancein industry

Bull. Amer. Soc. Test Mat (218), 31—33. 43.21RU5HPORTH S. K. andSELwOOD A. (1958) A vibrationpick-up which doesnot load

the system being examined .J. Sri. Jnstrum. 35 (9), 340—346; Index acm.105/14/11. 41.23

RussELL H. W. (1943) Fatigue strength and related characteristics of spot-weldedjoints in 24S-Taicladsheet,NACA ARR 3L01 (WR W-61). 54.21

RussELL H. W. andGILI.En H. W., JACKSON L. R. and FOLEY G. M. (1943) Theeffect of surfacefinish on thefatigueperformanceof certainpropellermaterials,NACA TN 917. 63.4

RUSSELL H. W. and JAcscsoNL. R. (1943) Progressreport on fatigueof spot-weldedaluminum,NACA APR (WRW-38). 54.21

RUssELL H. W., JACKSON L. R., GROvER H. J. andBEAvEE W. W. (1943) Fatiguecharacteristics of spot-welded 24S-T aluminum alloy, NACA ARR 3Fl6(WR W-64). 54.21

(1944a) Fatigue strength and related characteristics of aircraft joints. I-Com-parison of spot-weld and rivet patterns in 24S-T alclad sheet. Comparisonof245-Talcladand75S-Talclad,NACA ARR 4FOl (WRW-56). 54.12; 54.21

(1944b) Fatiguestrengthand relatedcharacteristicsof joints in 24S-T alcladsheet,NACA ARR 4F30 (WRW-63). 34.2; 54.21

(1948) Fatigue strength and related characteristics of aircraft joints. II. Fatiguecharacteristics of sheet and riveted joints of 0.040-in. 24S-T, 75S-T, andR303-T275aluminumalloys, NACA TN 1485,AMR I, Rev. 624. 54.12; 54.3

RussELL H. W.andWELCKEEW. A. (1931a)Fnduranceandotherpropertiesat lowtemperatures of somealloys for aircraft use, NACA TN 381. 65.1

(1931b) Apparatusfor low temperatureendurancetestingProc. Amer. Soc. Test.Mater. 31, Pt. 1, 122—128. 32.2

(1936) Damageand ovnrstrcssin the fatigue of ferrousmaterialsProc. Amer.Soc.Test. Mater. 36, Pt. 2, 118—128. 24.2

•1~~

BIBLIOGRAPHY

RU55ENBER0EE M. (1945) A dynamic tension-compression testing machine for thedetermination of fatigue strength anddampingSchweiz.Arc/i. 33—42. 31.14

(1952) Anwendungsmoglichkei~~~von Dauerprfifmaschincnmit Rcsonanzan..tricb Z. Ver. Dtsch. Jng. 94, 314—318; AMR 6, Rev. 128. 31.14

R055ENaEEGERM. and FOLBE5 G. (1955)High-speeduniversalfatiguetestingmachineverification of statically calibrated mechanical-opticaldynamometerProc. Soc.Exp. StressAnaL 12 (2), 9—20; AMR 9, Rev. 2212. 31.14

RUTTHAN W. (1933) TH, Darmstadt,Diss. 31.24

S

SAesssG. (1939) Internal stressesin piston rods of a large Diesel engineocean linerTrans.Amer.Sac. Metals27 (3). 63.5

(1947) Residual stresses,their measurementand their effect on structural parts,Proc. Melbourne Symp., 237—247. 63.5

SAcsisG., Muvns B. B. and KLIER F. D. (1957) Fifect of a number of variables onthefatigue propertiesof high strength steels,ASTM, STP 196. 60.0

SANREY H. R. (1905) Vibratory testing machineMcch.Eugng,N.Y. 13 (Nov.). 31.0SARHAN A. F. (1954) Fstimation of the mean and standard deviation by order

statisticsAnn. Math.Statist. 25, 317. 90.5SARHAN A. F. and GREENBERG B. G. (1956) Fstimationof location and scalepara-

meters by order statistics from singly and doubly censored samples. Part I.The normal distribution up to sampleof size 10 Ann. Math. Statist. 27 (2),452—459. 90.42

SAUEEJ. A. (1948)A studyof fatigue phenomenaundercombinedstressJnt. Cougr.Appl. Mech.4, 150—164; AMR 3, Rev.2349. 62.5

SAUL K. H. (1942) TH. Darmstadt,Kr. Ing.-Diss. 31.32SAvOR S. R. (1937) The useofthe median in tests of significance Proc. JndianAcad.

Sci. (SectionA) 5, 564—576. 71; 90.6SA%vERT W. (1943) Verhaltender Baustahlebei wechselndcrmehrachsigerBean-

spruchungZ. Ver. Dtsch. Jug. 87, 609—615. 62.5SCSSACHTEELE K. (1929) Beitrag zur Auswertungvon DauerversuchenStahlbou 2

(20), 238—240. 91.0SCHICK W. (1934) Untersuchungenan SchweissverbindungenTech. Mitt. Kropp 2

(2), 43—62. 31.15; 32.6ScMIJvE J. (1954) The possibilities of internal friction measurementsfor material

testing, in particular for fatigue testing(in Dutch), NLL Rep.M 1949; AMR8, Rev.412. 26

ScrssJvEJ. and JAcoes F. A. (1955) Fatigue testson notchedand unnotehedclad24S-i~slsectspecimensto verily the cumulative damagehypothesis,NLL Rep.M. 1982. 24.2

(1956) Researchon cumulative damagein fatigue of riveted aluminum alloyjoints, NLL Rep.54 1999. 24.1; 24.2(1957) Thefatiguestrengthof aluminium alloy lugs,NLL Rep.M 2024. 54.4

SCHLIEEELMANN R. J. and CooLs J. (1952) Fatigue propertiesof Redux-bondedlapjoints of 24S-Talelad, FokkerRep.R-26. 54.22

SCHH5DT M. V. (1937/38)Influenceof theforging reductionandheattreatmentonthe bending fatigue strength of various alloy structural steels (in German)Arc/s.Eiseo/sütteuw.11, 393—400. 61.8

SCHOn G. J. (1953) The statistical significanceof a few fatigue resultsNat. acro.Fstabl. Canad.LR58; AMR 7, Rev. 3573. 90.6

290so on t

BIBLIOGRAPHY BIBLIOGRAPHY

SOHREYERW. C. and Yosr K. B. (1956) Vibration-testing techniquesfor largespecimens,SAE Prep. (827); Index aero.225/12/12. 33.4

ScssuznaE. H. (1952) A critical look at fatigue equationsProd. Engng. (June),150—151. 91.0

(1954) A simplified statisticalprocedurefor obtainingdesign-levelfatiguecurvesProc. Amer. Soc. Test.Mater. 54, 853—864; AMR 9, Rev. 1823. 21.2

SCHULZ E. H.andBUCHBOLTZ H. (1931)Developmentof fatiguetestingin Germany,Zurich Goisgr. 1,278—303. 30; 31.14; 32.1

SCHWAIGERER S. (1952) ExperimentelleErmittlung von Spannungenin BauteilenZ. Ver. Dtscls. Ing. 94 (32), 1025—1036; VDI-Sonderheft1953, 63—74. 42.21

SCHWESZERHOF S. (1953) Magneticanalysesof theresidualstressesfollowing plasticdeformation and fatigue (in French), ONERA NT no. 17; AMR 8, Rev.1011. 26

ScsswmrrcsaGW. andSTROBEL E. (1930) VerfestigungdurchWechselbeanspruehungZ. MetallIc. 22, 378—381,402—402. 27.2

SCOTTJ. G. (1956) The developmentof a wire testing machine,AARL SM Note216. 33.1

SCOTTJ.G. (1957a)Furtherdrift testson resistancestraingauges,ARL, MelbourneS.M64; Index aero. 125/14/11. 42.21

(1959b) Long-timedrift in resistancestrain gauges,ARL, Melbourne, S.M65;Index aero. 124/14/11. 42.21

(1957c)A collectionof straingaugebridgeformulae,ARL, Melbourne S.M66;Index aero.126/14/11. 42.21

SEAGERG. C. and TAn W. H. (1938) Apparatusfor high-speedrepeatedimpacttesting of metal under separatelyappliedstressEngineering,Land. 146 (3802),611. 32.6

SELIGERV. (1943) Effect of rivet pitch upon the fatigue strengthof single rowriveted jointsof 0.025to 0.025 inch 24S-Talclad, NACA TN 900. 54.12

(1945) A suggestednew parameterfor fatiguestrengthanalysisBull. Amer. Soc.Test.Mat (132), 29—32 82.2

SERENSENS. W. (1956) On the enduranceof cast iron and steel under repeatedloading of varying amplitude, London Conf., Session3. Paper 11.

24.2; 25.2; 31.32; 31.43; 32.4; 62.0SHANLEY F. R. (1956) A proposedmechanismof fatigue failure, StockholmConf.,

251—259. 85.1SsassisNM. Y. (l95la) The effect of cyclic overloadingandunder-loadingon the

fatigueof metals(in Russian)J. Tech. Phys.,Moscow21, 1184—1193; AMR 5,Rev.1727. 24.2

(195lb) Effect of cyclical overstressingand under-stressingon the fatigue ofmetals (in Russian) J. Tech. Phys., Moscow 21, 1184—1193; AMR 5, Rev.1727. 24.2

SHELTON S. M. (1931/33/35) Fatigue testingof wire Proc. Amer. Soc. Test. Mater. 31,Pt. 2,204—220; 33, Pt.2,348-360;J.Res. Nat. Bur. Stand. 14, 17—32. 31.32; 33.1

SHULER W. T. (1951) Fatigueproblemsin transportaircraft Aeronaut. Engng. Rev.20—26.

S5EBEL E. (1938) The static and dynamic testing of materials Vortr. Dtsch. Ga.MetallIc. 11—15. 20

SSEBEL E. and G~unM. (1956) Untersuehungenuber den Einfluss der Ober-fiachenbesehaffenheitauf die Dauersehwingfestigkeit metalliseher Bauteile

Z. Ver. Dtsch. Ing. 98 (30), 1715—1723; Index aero. 106/12/12. 63.4

S5EBELE. andKEIL E. (1955)Prufimg von hochwarmfestenWerkstoffenfur Castor-binen und Strahltriebe Stahl u. Eisen, Düsseldorf 75, Pt. 2 (23), 1594—1596;Index aero.234/12/1. 28.1

SIEBEL E. andLETENSETTERW. (1936) Einfluss der SehnittgeschwindigkeitaufdieDauerfestigkeitvon PrufstabenZ. Vet.Dtsch. Ing. 80, 697—698. 63.4

S5EBEL E. and PFENDER M. (1947) Weiterentwicklungder FestigkeitsreehnungbeiWechselbeanspruchungStahl u. Eisen, Düsseldorf66/67 (19/20), 318-321;AMR 2, Rev. 741. 52.2; 62.2; 63.1

SsGwAaT H. (1956) Influenceof residualstresseson thefatigue limit, LondonConf.,Session3. Paper6. 63.5

S5GWART H. and PETERsON C. (1953) Entwicklungsmarkmaleder modernenMaterialprufung Werlcst. u. Betr. 86, 235—242. 20

S5MP50N M. and COLEMAN W. 5. (1957) Procedureand fixtures for residualstressdeterminationusingthedissectionor layerremovaltechniques,GeneralMotors

ResearchStaff Memorandum(Unpublished). 63.5SINCLA5R C. M. (1952) An investigationof the coaxingeffect in fatigueof metals

Proc. Amer.Soc. Test. Mater. 52, 743—751. 23.21; 96.0SsNcLAm C. M., CORTEN H. T. andDOLAN T. J. (1955) Effect of surfacefinish on

the fatigue strengthof titanium alloys RC 130B and Ti 140A, ASME, Paper55-A-197; AMR 9; Rev. 1458; Index aero.268/12/2. 63.4

S5NcLA5R C. M. and CRAIG W. J. (1952) Influence of grain sizeon workhardeningandfatiguecharacteristicsof Alpha brassTrans.Amer. Soc. Metals44,929—948.

61.2SsNcLksa C. M. and Dorsrc T. J. (1950) Someeffects of austenitiegrain size and

metallurgical structure on the mechanicalpropertiesof steel Proc. Amer. Soc.Test. Mater. 50, 587—616; AMR 5, Rev. 2051 61.

(1953)Effect of stressamplitude on statisticalvariability in fatiguelife of 75S-T6aluminumalloy Trans.Amer. Soc. Mech. Engrs. 75 (5), 867—870; AMR 7, Rev.498. 92.0

SINEs C. (1955) Failure of materials under combinedrepeatedstresseswith super-imposedstaticstresses,NACA TN 3495; AMR 9; Rev. 1461. 62.5

SjösTssöH5. (1950) On thestressesat the edgeof an eccentricallylocatedcircularhole in a strip undertension,FFARep.36. 52.2; 63.3

SMITH C. R. (1955) Spectrumand constantlevel loading fatigue tests, ConvairRep.7887. 25.1

SMITH C. R.andZANnMAN F. (1957) Photostressplasticfor measuringstressdistribu-tion aroundrivets,Convair Rep. 44.1

SMITH F. C., PRUEeGEHANW. C. andHARWELL R. H. (1950) Comparisonoffatiguestrengthsof bareandalelad 245-T3 Aluminum-alloy sheetspecimenstestedat12 and 1000 cyclesper minute, NACA TN 2231. 64.3

SMITH F. 0., HOWARn D. M., SMITH J. and HARwELL R. (1951) Fatigue testingmachinefor applying a sequenceof loadsof two amplitudes,NACA TN 2327;AMR4, Rev. 3241. 31.11; 32.4

SMITH J. H. (1905) A new testing machinefor reversalsof stressEngineering,Land.79, Pt. 1, 307—308. 31.13

(1909) FatiguetestingmachineEngineering,Land. 88, Pt. 2, 105—107. 31.13(1910) Some experimentson the fatigue of metalsJ. Iron St. lest. 82, Pt. 2,246—318; Engineering,Land. 90, 494—495. 31.13; 62.1; 82.2; 85.2

SMITH J. 0. (1942) The effect of rangeof stresson the fatigue strengthof metalsUniv. Ill., Expt. Sta. Bull. 334. 62.1; 85.2

292 293

B5BLIOGRAPHY

SM5TH J., HowANn D. M. and SanTHF. C. (1955) Cumulative fatigue damageofaxially loadedaiclad 75S-T6andaiclad24S-T3 aluminum-alloysheet,NACATN 3293; AMR 7, Rev. 144. 51.12

SNOWBALL G. (1949) Electrical methods of inducing and detecting vibrationEngineering,Land. 168,406—408; AMR 3, Rev.2587. 33.3

SOETE W. and VANCROMBRUOGE R. (1949) Resistanceto fatigue of wires usedinprestressedconcrete(irs French)Ann. Tray. Pubi. Belg.102 (5), 513—533; AMR4, Rev.230. 34.2

SONDERSCKER J. (1892) Description of some repeatedstressexperimentsTechnol.Quart. (April). 57.0

SOUTHER H. (1907) White-Southerendurancetest specimenProc. Amer. Soc. Test.Mater. 7, 616. 51

SPEARP., RoBINsoN J. R. andWOLFE K. I. B. (1953) The influenceof machiningand grinding methods on the mechanical and physical condition of metalsurfaces,The Instituteof Metals: Symposium: Propertiesof metallicsurfaces,London. 63.4

SPRETNAKJ.W., FONTANA M. G. andBaooxsH. E. (1951)Notchedandunnotchedtensilepropertiesof ten engineering alloys at 25 and — 196°CTrans. Agser.Soc.Metats43, 547. 65.1

SPATH W. (1938) Dauerprufmaschinefür VerdrehbeanspruchungZ. Ver. Dtsch. Ing.Pt. 2, 1465—1466. 31.14

(1950) Die Auswertungvon Dauerversuchenin dcr WcrkstoflfrufungMetal/ 4,374—377. 91

SzsTscmKowM. F. and WsscHNaWBTzscsS. D. (1948) PruiTung von Stahl aufDauerschwingungsfcstigkcitbei hohen Temperaturen Saw. Labor. 14 (1),86—91. 28.1

STANGE K. (1952) Uber das Ausgleichenvon gemessenenflachenhaft verteilten

raunthchenPunktreihen Z. Vermessungsw.77, (10,11,12). 90.41STANTON T. E. (1905) Alternating stresstesting machineof the National Physical

LaboratoryEngineering,Land.79, Pt. 1, 20 1—203. 31.13(1906) RepeatedimpacttestingmachineEngineering,Lond. (July), 33—34. 32.6

STANTON T. E. andBMsssTowL. (1906) The resistanceof iron andsteel to reversalsof direct stressProc. Instn. Mec/s. Engrs.,Land. 166. 50

STANTON T. E. and BAT5ON R. G. (1916) On the fatigueresistanceof mild steelundervariousconditionsof stressdistributions,Brit. Ass. Rep.288—291. 31.53

STARKEY W. L. andIVL&ssco S. M. (1954) A newfatigue-testingmachinecapableofinducing complex stress-time relationship in its specimen, ASME Ann. Meet.N.Y., Pap. 54-A-80; AMR8, Rev. 3759. 31.11; 32.4

(1956) Effects of complexstress-timecycleson the fatigue propertiesof metals,ASME. Prep.(56-A-I); Index acro.87/12/9. 25.2

STEPHENs B. G. (l956a) A statistical method of evaluating fatigue test ressslts,Bristol Aircr. Ltd. Engng.Devel. Lab. FatigueNote No. 1. 90

(l956b) Predictionof fatigue life for zero probability of failure, Bristol Aircr.Ltd. Engng.Devel. Lab. FatigueNoteNo. 3. 90

STEWART W. C. and WILLSAH5 W. L. (1948) Effectsof inclusionson the endurancepropertiesof steelsJ.Amer.Soc. Nay.Engrs. 60, 475—504. 61.3

STIcKLEY G. W. (1942) Improvement of fatigue life of an aluminum alloy byoverstressing,NACA TN 857. 24.2

STRANDHAGEN A. G. and SOMMER W. C. (1956) An electrostaticmethodof excitingthenaturalmodesofvibrationin bladesJ.Amer.Soc.Nay.Engrs.68 (2), 33 1—339;Index aero. 121/12/8. 33.3

BIBLIOGRAPHy

STE0H A. N. (1958) Dislocationsandcracksin anisotropicelasticity Phil. Mag. 8thScr., 625—646; mt. Aero.Abstr.3 (9), 137—137. 27

STROMEvER C. E. (1914) Thedeterminationoffatigue limits underalternatingstressconditionsProc. Roy.Soc.A90, 411—425. 31.41; 85.1

STULEN F. B. (1951) On the statisticalnatureof fatigue, ASTM Symposium onStatisticalNatureof Fatigue,STPNo. 121, 23—44. 23.21; 61.3; 61.8; 96.1

STULEN F. B. and CuMMINGs H. N. (1954) A failure criterion for muhiaxial fatiguestressesProc. Amer.Sac. Test. Mater. 54, 822—835; AMR 8, Rev.3745. 62.8

STULEN F. B., CUMMINGs H. N. and SCHULTE W. C. (1956) Relationof inclusionstothefatigue propertiesof high-strengthsteels,London Conf., Session5. Paper4. 61.3

SrvstsH. (1951) Fatigue strengthof ball-bearingracesandheattreated52100 steelspecimensProc. Amer.Soc. Test. Mater. 51, 682—700, 719—720. 61.3

STusss F. (1953) Dauerfestigkeitvon Aluminium-LegierungenMém.Ass. mt.Pont,Char/s. 13, 357—366. 85.1; 85.2

(1954) On the theoryof fatiguestrengthMdm.Ass. mt. PantsChar/s. 14,253—268;Indexaero.90J12/l 85.1; 85.2

(1955) Die Theorieder Dauerfestigkcitund die Vcrsuche von August Wohler,Mitt. TKVSB—No. 13. 83.1; 85.1; 85.2

SUGIHAaA S. (1956) Sometests for minimum life of fatigue failure survivorshipfunctions,ColumbiaUniv., Office OrdnanceRes. Cosstr.,Tech.Rep.T-SA. 92

SvEN50N 0. (1952) Unmittelbarc Bestimmungder Grasseand Häufigkeit vonBetriehsbeanspruchungenTrans.Instr. & MeasurementsConf Stockholm. 42.1

SvaNssoNN. L. (1953)A new electricresistancestraingagefor largestrainProc.Soc.Es/s. StressAnal. 11 (1), 197—202; AMR 8, Rev.2301. 41.21; 42.21

T

TATNALL R. R. (1937) The developmentof a fatigue testingmethodfor springsandspring wire Wire & Wire Prod. 12 (6), 297—301. 33.1; 33.2

TAPL5N L. B. andFINDLEY W. N. (1952) A servomechanismcontrolled universaltestingmachine,Univ. Ill., Unpubl. Rep. 32.4

TAP5ELL H.J. andCLEN5HAw W.J. (1927) Propertiesof materialsat high tempera-turesDSIR Engug Res. Spec.Re. No. 1. 65.1

TAaAsow L. P. andGROVER H. J. (1950) Effects of grinding and otherfinishingprocesseson the fatigue strength of hardenedsteel Proc. Amer. Sac. Test.Mater.50, 668—687; AMR 5, Rev. 129. 63.4

TAvLoa R. .1. (1956) Experimentaldesign and methodsof analysisusedin studyingeffects of metallurgical variation on fatigue, Stockholm Conf., 269—277.

64.5; 66.2TEED P. L. (I

952a) Fatigue of aircraft materialswith special referenceto micro-

structure JR. Aero. Soc. 56, 427—437; AMT 5, Rev. 3101. 61.2(1952b) The influence of mctallographic structure on fatigue, MIT Conf.,

252—291. 61.2TELFA5R D., ADAMs C. H. and MOHRMAN H. W. (1947) Creep,long-time tensile

and flexural fatigue properties of melamine, phenolic plastics Mod. Plast. 24,151, 152, 236—248; AMR 1, Rev. 112. 28.3

TEMPLIN R. L. (1930) Detectionof incipient fatigue failures Proc. Amer. Soc. Test.Mater. 30, Pt. 2, 289. 46.0

(1933) Fatigue machines for testing structural units Proc. Amer.Soc. Test. Mater.33, Pt. 2, 364—380. 31.11

294295

BIBLIOGRAPHYBIBLIOGRAPHY

TEMPLIN R. L. (1939) Fatiguemachinesfor testingstructuralunitsProc. Amer. SocTest. Mater. 39, 711—722 31.11; 33.4

(1954) Fatigueof aluminumProc. Amer. Soc. Test. Mater. 54, 641—699; AMR 9,Rev.468. 60

TEMPLIN R. L., HOWELL F. M. andHARTMANN E. L. (1950)Effect ofgrain directionon the fatiguepropertiesof aluminum alloys Prod. Engng.21 (July), 126—130.

61.2; 61.8TENOT A. (1947) Nouvellemachined’essaidynamiquedestextilesetdu caoutchouc

Genie Ciy. 124 (Sept),349—351. 33.13TNEI5 E. and BARTELD K. (1954) Investigationof test specimenshaving known

defects for determining the operating conditions in ultrasonic testing (inGerman) Arch. Eisenhutteuw.25 (3/4); Index aero. 100/12/5. 46.5

TssEwLssJ. (1958) The basis for optimum-test-methodsselectionNon-Destr. Test.16 (2), 84—94; Index aero. 117/12/8. 20

TMIEL5CH H. (1952) Thermalfatigueand thermal shock,Weld. Res. Counc.Bull.SeriesNo. 10; AMR 5, Rev. 2260. 32.2

THOM H. C. S. (1954) Frequencyof maximum wind speedsProc. Amer. Soc. Ciy.Engrs. 80 (539), 1—11, SeparateNo. 539. 90.8

TMOMAS W. N. (1923) Effect of scratchesandof variousworkshop finishesupon thefatiguestrengthof steelEngineering, Land. 116, 449—454, 483—485. 63.4

THOMPsoN N. (1956) Experimentsrelating to the basic mechanismof fatigueLondon Conf., Session6. Paper3. 61.7

Ts-soMEsoNN., W4

&nswoRTM N. andLOUAT N. (1956) The origin of fatigue fracturein copperPhil. Mag. Series8, 1, 113—126. 31.14; 32.1

THoMPsoN R. L. (1954) Correlation of gamma radiography and Magna-fluxindicationsin the inspectionof largecast-steelconnectingrods Bull. Amer. Soc.Test.Mat. (197),58—59; AMR 7, Rev.3887. 46.4; 46.8

THoMpsoN W. R. (1936) On confidencerangesfor themedianandotherexpectationdistributions for populationsof unknown distributionform Ann. Math. Statist.7, 122—128. 71

THROOP J. F. (1949) An investigationof thefatigue performanceof polystyrene,Master’sThesis,RensselaerPolyt. Inst., Troy, N.Y. 28.3

Tssus~sA. (1931) Zur Steigerungdcr Daucrfestigkeitgekerbter KorsstruktionenZ. Ver. Dtsch.mug. 75, Pt. 2, 1328—1330. 24.1

(1942) Dtsch.Kraftfahrtforseh. (73), 10. 31.32THUM A. andBERGMAN G. (1937a)DauerprufungvonFormelemcntenundBauteilen

in natürlicherGrosseZ. Ver. Dtseh. mug.81, Pt. 2 (35), 1013—1018.31.13; 31.32; 31.53; 33.4

(1937b) Dauerfprufungvon Formelementenund Bauteilenin naturlicherGrosscZ. Ver. Dtseh.mng. 81, 1013—1018. 31.43

Turns A. and ERKER A. (1942) Zeit- und Dauerfestigkeitand dcrcn Bceinflussungdurch eineeinmaligehoheUberlastungZ. Ver. Dtsch. mug. 86, 171—174. 24.1

THUM A., GRETM A. and JACoBI H. R. (1937) Flexural fatigue experimentsonmolded synthetic resin plastics (in German) VDI, Kuast- uud Press-Stoffe2,16—24. 28.3

TsstmsA. andJACOBI H. R. (1938) The enduranceof pressedmaterialsof artificialresins (in German) Maschinezwchadeu15, 85—91, 101—105. 28.3

(1939a) Festigkeitseigcnschaftenvon hochfcstcnKunsthartz-PresstoffenZ. Ver.Dtsch. mug.83, 1044—1048. 28.3

(1939b) Mechanische Festigkeit von Phenol-Formaldchyd-KunststoffcnForschungsh.Ver. Dtsch. mug.No. 396. 31.13

THUM A. and KIRM5ER W. (1943) Uberlagerte Wechselbeanspruchungen, ihreErzeugungmid ihr Einflussaufdie DauerhaltbarkeitandSpannungsausbildussgquergcbuhrtcr Wellen Farschuugsh.Ver. Dtsch.mug. No. 419, 1—33. 31.53

THUM A. and LORENZ H. (1941) VorspannungandDauerhaltbarkeitanSchrauben-verbiodungcn mit einer und mehrercn Schrauben Dtsch. Kraftfahrtforsc/l. (56).12. 31.13

THuM A. and SvEN50N 0. (1944) Kontaktdchnungsmesscrzum Messen vonBctriebsbeanspruchungen Z. Ver. Dtsch.mug. 88, 153—154. 42.1

THUR5T0N R. C. A. (1948) Dynamic calibration method uses modified provingring Bull. Amer.Soc. Test. Mat (154), 50—52. 35.2; 43.1

TIEDEMANN J. B., PAEnUE T. E. and VmNEssJ. (1955) Bending of rotating beamsProc. Soc. Er/s. StressAnal. 12 (2), 189—200; Index acro.203/12/2. 31.32

TsMosssENscoS. and D5ETz W. (1925) Stressconcentrationsproducedby holesandfillets Trans. Amer. Soc. Mech. Eugrs.47, 199—237. 63.3

T0MLIN50N G. A., THORPE PL. and GOUGH H.J. (1939) An investigation of thefretting corrosionof closelyfitting surfacesProc. J. Meek.,E., 141, 223—249.

65.5T00LIN R. R. and MOCHEL N. L. (1947) High temperaturefatigue strengthof

severalgas-turbinealloys Proc. Amer. Soc. Test. Mater. 47, 677—692. 65.1TORREY M. N. and GOMN G. R. (1956) A studyof statistical treatments of fatigue

dataProc. Amer. Soc. Test. Mater. 59th Ann. Meeting. 64.1; 91.0TowrqsENn J. R. and GREENELL C. H. (1929) Fatiguestudiesof non-ferroussheet

metals Proc. Amer. Sac. Test. Mater. 29, 353—370; Bell Lab. Rec.13 (1), 12—16.31.21

TuCEERJ. T. (1955) Studieson the biaxialfatiguepropertiesof pressurevesselsteelsWeld. J., Easton,Pa. (4), l79s—l82s. 62.6

U

UMPHREY W. (1958) Unit checksscratchdepthmrou Age 181 (24) 92—93; Indexaero. 110/14/8. 45.1

UsmEstwoon A. F. and GRIPPEN C. B. (1946) Amachine for fatigue testing full sizepartsProc. Soc.Ex/s.StressAual. 4 (2), 32—38. 31.15

UPTON C. B. and LEwss G. W. (1912) The fatigue failure of metalsAmer. Mach.,N.Y. 37, 633—635, 678—683. 31.21

Uxmsc G. V. (1956) Mechanicalaspectof size effect on fatigue of metals, LondonCossf., Session2. Paper17. 3.63

V

VALKENEuEO H. E. VAN (1948) The theory of ultrasonicmaterials testing Meek.Eugug.,N.Y. 71,817. 46.5

VALLAT P. (1956) Conceptionand designof a structurein a transportaircraft withpressurizedcabin to obtain good fatigue life (in French),Proc. 2ndEuro/s. aera.Cougr. 3 (73), 1—73; Index aero.249/14/4. 25.1

VALLUEI S. R. (1956) Someobservationson the relationshipbetweenfatigue andinternal friction NACA TN 3755; Index acro. 307/12/12. 26

(1957) Effect of frequencyand temperatureon fatigue of metals,NACA TN3972; mat Aero.Abstr. 2 (3), 108—108. 64.3

VENABLE C. S. (1945) Comparativefatigue test data Bull. Amer. Soc. Test. Mat.(136), 17—19.

296297

BIBLIOGRAPHY BIBLIOGRAPHY

VIDAL G. (1953a)Methodsof determininghotfatigue limit in commonor controlledatmospheres(in French)Rey.MétatI. 50, 21. 28.1

(l953b) Sur les méthodesrapidesde determinationde la limite de fatigue desmCtauxetalliagcsReek.A/so. (34), 49—54; AMR 7, Rev.794. 26

(1955) Installationd’essaide fatiguea chauden traction ondulee dans les gazdecombustiondepCtrolc Reek.Ae’ro. (July/Aug.), 25—29; Int. aero.abstr.1 (1),126—126. 32.2; 32.3

VIDAL G., GsssAssnF. and LMmssE P. (1956) Devicefor the fractureof metalsbyhigh-frequencysinusoidal alternating stress(in French) C.R. Aead. Sei., Paris242 (8), 986—988; Index aero.97/12/5. 31.44; 32.1

VINCENT K. (1952) Cumulative damagefatigue investigation (Loaded holes)Saunders-RoeRep. SR/S/762. 54.4

Vrrovac F. H. andLAEAN B. J. (1953) Reviewof previouswork on short-timetestfor predictingfatiguepropertiesof materialsWADC 53—122. 26

(1955) Effectofprior creepon thereversedstressfatiguepropertiesof temperatureresistantalloys, WADC TN 55—460. 23.22; 24.1; 96.2

VosoT E. (1928)EineneucMethodczur Bestimmungdcr innerenArbeitsaufnahme-

fhhigkeit von Werkstoffen bei dynamischerBeanspruchungZ. Tech. Phys. 9,321—337. 31.14

VOIGT E. and CHsusnNsEN K. H. (1932) Uber die Dampfungsffihigkeit andSchwingungsfcstigkeitdes StahiesMitt. K.-With.-mmt.Eiseaforsck.14, 151—166.

31.14; 32.1VOLK C. (1938) TheamplifiedWohierdiagram,thenewstressdiagram(in German)

Metallwirtsekafl 17, 1167—1169. 82.1VOTTA F. A. (1948) New wire fatigue testing method mrou Age (Aug) 78—81; Steel

(Dcc), 90. 31.31; 33.1VOUTE C. H. (1948) Investigationofmagnitudeandfrequencyof loadsfor a fatigue

teston wing, N. V. Fokker, Rapp.No. P-1l-527a. 25.1

w

WsnaA. R. and GROTENHIM5 P. (1954) Improvementsin electromagneticvibrators,British PatentApplication. 31.24; 32.1

(1956) Very high-speedfatigue testing,LondonConf., Session4. Paper5.26; 31.24; 32.1; 34.4; 64.3

WAIss,sMJ J. L. and PH5LLIP5 A. (1954) Simplified measurementof residualstressesProc. Soc. Ex/s.StressAnal. 11 (2), 29-44; AMR 8, Rev.2719. 44.1

WALD A. (1940) The fitting of straight lines if both variablesarc subjectto errorAnn. Math. Statist.11, 284—300. 90.41

WALPORD J. G. and WI5TRE5CH J. G. (1950) AbhangigkeitdesHin- mnd Hcrbiegc-versuchsan Drahtcn nach englischenNormvorschriften von der Prufmaschine(in English) Wire mud. 17 (200), 663—665,667—668,671. 64.2

WALKER H. (1947) A laboratory testing machine for helical gear tooth actionEngineer,Loud. (June), 486—488. 32.5

WALKER H. L. and CREIG W. J. (1948) Effect of grain size on tensilestrengthelongation,andendurancelimit of deepdrawingbrassMetals Tech. 15 (2478);AMR 2, Rev.753. 61.2

WALKER P. B. (1958) Fatigueof a nut and boltJ.R. Aero.Soc.62 (570), 395—407;Index aero. 173/14/77. 54.3

WALKER P. B. (1959) Pressure-cabinfatigue. A survey of the problemand thetestmethodsdeveloped,RAE Rep.Airer. Eugug.28, 11—19. 25.1

WALLI5 W. A. (1951) Toleranceintervals for linear regression,SecondBerkeleySymposiumon Math. Stat, andProb.,43—51. 90.7

WAMPLER C. P. andALLEMAN N.J. (1939) Fatiguetestsofwire Bull. Amer.Soc. Test.Mat. (101), 18. 31.32; 33.1

WARBORTON-BROWN D. (1942) Phenol-formaldehydeplastics under conditions ofbendingfatiguePlastics, Loud. 6, 210—218. 28.3

WARn E.J. (1952)Fatiguetesting underprogressiveloading—Anew techniquefortesting materials,WADC TN 52—148. 23.22

WARD E.J., SCHwARTZR. T. and SCHWARTZ D. C. (1952) An investigationof theProt acceleratedfatiguetest,WADC TR 52-234. 23.22; 96.2

WARNOCK F. V. andPOPEJ. A. (1947) The changein mechanicalpropertiesof mildsteelunderrepeatedimpactProc. mastu.Meek.Eugrs.,Loud. 157, 33—44; AMR 1,Rev. 303. 24.2

WATEIN50N J. F. (1956) The influence of somesurface factors on the torsionalfatiguestrengthof spring steels,London Conf., SSsion5. Paper5. 63.5

WAY S. (1935)Pitting dueto rolling contactJ. A/s/sI. Meek.A-49—A-58. 32.5WEanER D. and LEvY J. C. (1958) Cumulativedamagein fatiguewith referenceto

the scatterof results,Ministry of Supply, S & T Memo. No. 15/58. 24WanE R. (1950) The applicationof theresonancevibration method to thefatigue

testing of spotweldedlight alloy structuresWeld. Res.4, 33r. 21.1WEIaOLL I. (1952) The effect of decarburizationand other factorson the fatigue

strengthof rollthreadcdaircraft bolts, SAAB Tech. NoteNo. 4. 61.4WE5uULL W. (1 939a) A statistical theory of strengthof materialsProc. roy. Aead.

Eugag. Sei. No. 15. 63.1; 63.2; 90(1939b) The phenomenonof rupture in solids Proc. Roy. Acad. Eugug. Sci.,No. 153. 63.1; 63.2; 90

(1946) Influence of the volume on the fatigue strength (in Swedish), IVA (2).62—64. 63.1

(1948) Electrical resistanceof wiresat largestrainsNature, Laud. 162, 966—967.41.21; 42.21

(1949) A statistical representationof fatigue failures in solids K. Teku. Hogslc.Haudl. No. 27; AMR 3, Rev. 1098. 84; 85.1; 90.3

(1950) Statisticalviewpoints on thefatiguestrength(in Swedish)Teku. Tidskr.80, 1059—1064; AMR 4, Rev. 2045. 90

(1951) A statisticaldistributionfunction of wide applicability J. A/s/sl. Meek. 18(3), 293—297; AMR 6, Rev. 2. 83

(1952a) Statisticalplanning of fatigue tests (in Swedish) Teku. Tidskr. 82 (7),157—161; AMR 6, Rev. 4. 71

(1952b) Statisticaldesignof fatigue experimentsJ. A/s/sl. Meek. 19 (1), 109—113;AMR 5, Rev. 3103. 11

(I 952c) ‘Ilse statisticalaspectof fatigue failures IvIIT Conf., 182—196. 85.1(l952d) A surveyof statisticaleffectsin thefield of materialfailure AMR 5 (11),Featurearticle. 90(1953) Scatterin fatigue tests, Proc. SecondICAF Conf., Stockholm,App. 2.

92(l954a) Thepropagationof fatiguecracksin light-alloy plates,SAAB TN 25. 27(1954b) A new method for the statistical treatmentof fatiguedata,SAAB TN30; AMR 8, Rev. 2375. 90; 92; 94

(1954c) The staticstrengthand the fatiguestrengthof riveted,spotweldedandRedux-bondedjoints in 24S-T aluminumalloy sheet,SAAB TN 31.

54.12; 54.21; 54.22

298 299

BIB LI 0 GRAPH Y BIaL5OGRAPHY

WE5BULL W. (1955a) Scatterin fatigue life of 24S-T alclad specimenswith drilledhales,SAAB TN 32; AMR 8, Rev.3748. 21.2; 92

(l955b) New methods for computing parametersof complete or truncateddistributions,FFA Rep.58, AMR 9, Rev.459. 90.4; 92; 93

(1955c)Staticstrengthandfatiguepropertiesofthreadedbolts,FFARep.59. 54.3(1955d) Thepropagationoffatiguecracksin light-alloy plates,Proc.Third ICAFConE,Cranfield,App. 3. 27

(1955e) Scatterin fatigue life of 245-T alcladplates,Proc.Third ICAF Conf.,Cranfield,App. 4. 92

(1956a)Basicaspectsof fatigue,Stockhohn,Coll., 289—298. 27; 63.3(1956b) Effect of crack length and stressamplitude on the growth of fatiguecracks, FFA Rep.65. 27

(1956c) Static strengthand fatigue propertiesof unnotched circular 75S-Tspecimenssubjectedto repeatedtensileloading, FFA Rep.68; Aeronaut.Eugug.Rey.2 (2), 142—142. 21.2; 91; 92; 93; 94

(l956d) Scatter of fatigue life andfatigue strength in aircraft structural materialsandparts,ColumbiaConf., 1926—145. 92

(1956c) Scatter of fatigue life and fatigue strength of aircraft materials, Proc.Fourth ICAF Conf., Zurich, Doe. 94. 92

(1957a) Statisticalhandling of fatigue data and planning of small test series,FFA Rep.69; Int. aero.Abstr., 2 (6), 145—145. 71; 94

(1957b) History of servicesimulated load spectrumfatigue testing, Final Rep.ARDC Contr. 25.0

(1 957c) Scatteroffatigue life andfatiguestrengthin aircraft structuralmaterialsand parts,FFA Rep.73. 92

(I 958a) Researchon statisticalevaluation of datafrom small test series,Ann.Rep.ARDC Contr. (will appearasa WADC Tech Rep.) 21.1; 71; 90.4

(1958b) Remarqucssur Ic dosnmagecumulatif de fatigue Rev. Métall. 55 (8),778—784. 24.0

(1959a) Zur Abhangigkeit der Festigkcit von dcr Probcngrosselag. Arch.,Granunel-Festschrift.28, 360—362. 63.1(1959b) Statistical evaluation of data from fatigue and creep-rupturetests.PartI FundamentalconceptsandgeneralmethodsWADC TR 59—400. 90.4

WEssawsM. H. andKAPLAN M. H. (1950) Thefatiguestrengthof steelthroughtherange from 1/2 to 30,000 cyclesof stressProc. Amer. Soc. Test. Mater. 50, 649—665. 22.1; 91

WEYRAuC5-sJ.(1880)On thecalculationsof dimensionsasdependingon theultimate

working strengthof materials Mm. Proc. mast.Civ. Eugrs. 63, 275—296. 85.2WELCH W. P. and WILsoN W. A. (1941) A new high temperaturefatsguemachine

Proc. Amer.Soc. Test. Mater. 41, 733—746. 31.24WELLINGER K. (1955) Ermittlung der Schwingungsfcstikgeitvon Schwcissverbin-

dungen,SchweisSckueid(9), 392—396. 21.1WELL5NGERK. andHOFMANN A. (1948)Testingof metallicmaterialsatlow tempera-

tures (in German) Z. Metallk. 39 (8), 233—239; AMR 3, Rev. 1271. 65.1

WELTER G. (1948) Zwci neueVcrfahrenzur Prufung dreiachsigerProben,Weld.Res. Counc. (11), 529—536. 31.6

WER5CME55TERP. (1921) Ermittlungder plausibelstenGeradeneinerfehlerzeigendenPunktreihe,Z. augew.Math.Meek.1, 491—494. 90.41

(1930/32)Bestisnmungder Gleichung derplausibelstenGeradenciner fchlerzci-gendcnPunktreihe Z. Vermessuugskuude1930, 78—88; 1932,727—738. 90.41

WERREN F. (1948) Fatigue of sandwichconstructionsfor aircraft (cellular celluloseacetatecore material with aluminum or fiberglaslaminatefacings, testedinshear),For. Prod.Lab. Rep.,No. 1559-F; AMR 2, Rev. 1518. 54.5

(1949) Fatigue of sandwichconstructionsfor aircraft, For. Prod. Lab. Rep.No. 1559; AMR 3, Rev.2286. 54.5

WascoTTB. B. (1938) Fatigueand corrosion fatigue of steelsMeek. Eugug., N.Y.813—822. 65.4

WEYEE F. (1956) Fatiguepropertiesof steelat highertemperatures,LondonConf.,

Session4. Paper6. 61.8; 651WEYEE F. and HEMPEL M. (1956)Dauerschwingfestigkeitvon Stkhlenbei erhohten

Temperaturua,Forsch.Wirts. Verk. Nord.-Westf.No. 311 & 312. 65.1WEvEEF., HEuPEL M. andScHEADERA. (1955)MctallographischeUntcrsuchungen

uberVerformungserscheinungenanderOberflachebiege-wechsclbeanspruchter-ProbcnausSt. 37, Mitt. MPI Eiseaforschg,Abh. 650; Arck. Eiseukutteuw. 25(12), 739—754. 61.7

WEVER F., HEMPEL Iv!. and M6LLER H. (1937/38) Die Anderungendes Kristall-zustaadeswechsclbcanspruchterMetalle im Rontgcnbild Arch. Eiseukiitteuw.11, 315—318. 61.7

(1938) Die Verhaderungendes Kristallzustandcston Stahl bei Wechselbean-spruchuagbiszum DauerbruchStakl a. Eiseu,Düsseldorf59, 29—33. 61.7

WaVER F. and HANsEL H. (1938) Beitragezur magnetischenWcrkstofl~nufungMitt. K.-Wilk.-must.Eiseuforsck.20, 91—101. 46.4

WSIALEY R. E. (1957) Fatigue investigationof full-scaletransport-airplanewings;variable-amplitudetests with a gust-loadsspectrum, NACA TN 4132; Int.acm. Abstr., 3 (1), 9—9. 25.1

WHALEv R. E.,McGusoAN M.J. andBRYAN D.F. (1956)Fatigue-crack-propagationand residual-static-strengthresultson full-scale transport-airplanewings, NACATN 3847; Aerouaut.Eugug.Ret.2 (2), 145—145. 65.6

WsLsuNs E. W. C. (1956) Cumulative damagein fatigue, StockholmCouf., 321—332.24.2

WILKINsoN E. B. Ja.(1939) Effect of surfacefinish on fatigue strengthon helicalspring steel, MIT. B.S. Thesis. 31.24

WILEs S. S. (1941) Determinationof samplesizesfor setting tolerancelimits Ann.Mat/s. Statist. 12, 9 1—96. 71; 90.7

(1942) Statisticalpredictionwith special reference to the problem of tolerancelimits Auu. Math.Statist. 13, 400—409. 71; 90.3

(1948)OrderstatisticsBull. Amer. Matk. Soc.54, 6—50. 63.4WILcsAMs W. L. (1949)Tlsc effectsof mctallizingprocedureson thefatigueproperties

of steelProc. Amer.Soc. Test. Mater. 49, 683—701; AMR 4, Rev. 704. 43.3WILLMAETH W. W. (1958) Small barium titanatc transducerfor aerodynamicor

acousticpressuremeasurementsRev.Sd. mmtrssvs.29 (3), 218—222; Index aero.68/14/6. 35.1; 35.2

WILsoN B. andJOHNSON C. (1937) Calibrationof testing machinesunder dynamicloading J. Res.Not. Bssr. Stand.19, 41—57. 35.1

WILSON B. L., TATE D. R. and BoEscowsscsG. (1946) Provingrings for calibratingtestingmachines,NBS, CsrcularC454.

WILsoN W. M. and THOMAS F. P. (1938) Lever-type constant-strain fatigue machine,Univ. Ill., EagngExp.Stat. Bull., No. 302. 31.11; 36

WINGs’saLa C. H. (1911) The effect of the upper limit of stresson the safe rangeProc. must. Meek. Eugrs., Loud. Pts. 3—4, 904—919. 85.2

300 301

BIBL5OGRAPHY BIBLtOGRAPHY

WsNsoNJ. (1948) The testingof rotors for fatigue life J. Aero. Sri. 15, 392—402;AMR I, Rev. 1215. 28

WszEzcazL. (1937) Themeasuringaccuracyof theMartensmirror testingapparatusin fatigue tests (in German)Arch. EiseukUtteuw.11(4), 189—193. 42.3

WOEKNLE R. (1930) Daucrprufmaschinefur DrAhte und Seile,DRP. 501983. 33.1WOLF H. (1941) Beitrag xur Bestimmung der Gleichung dcr plausibclsten Geraden

einerfehlcrzeigendenPunktreihe,ZIV. 411-43. 90.41WOOD W. A. andHa~A. K. (1951) Somenew observationson the mechanismof

fatigue in metalsJ.mast. Met 79, 89—102. 64.3WoonwxssnA. R., GUmsK. W. and FoRREsT G. (1956) The effect of meanstress

on thefatigueof aluminium alloys, London Conf., Session2. Paper 10.62.1; 62.3

WORLEY W.J. (1948) Simplified dynamicstrainequipmentmastasmeutsMagazine21(April), 330—332. 31.11; 34.3; 42.21

WREY C. F. (1937) Automatic electrical fatigue testing machinesEugiueer, Laud.164, (4260),215—254. 31

WALLGaEN G. (1949) Fatigue testswith stresscycles of varying amplitude,FFARep.No. 28; AMR 3, Rev. 907. 25.1; 51.12; 54.12

(1953) Direct fatigue testswith tensileand compressivemeanstresseson 24S-Taluminium plain specimensand specimensnotched by a drilled hole, FFARep.No. 48. 62.1; 82.2

(1943/54) Programutmattningmed bultforband, (Program fatigue testing ofboltedjoints), FFA Rep.HU-429: I & 429:2. 54.11

(1954) Fatiguetestsof wing joints (in Swedish),FFA Rep.HU-473. 54.3WöHLER A. (1858—1870) Teststo determinethe forcesacting on railwaycarriage

axlesandthecapacityofresistanceoftheaxles(inGerman)Z. Baaw.8,641—652,10, 583—615, 13, 233—258, 16, 67—84, 20, 73—106; EugL Abstr.Eugog,11, 1871,199—200; 221; 244—261; 299—300; 327; 349—350; 397; 439—440. 82.1

(1870) Uberdie Festigkeits-Versuehemit Eisenund Stahl Z. Baaw. 20. 82.1

YYEN C. 5. (1950) An hypothesisfor explanationof the effects of size of specimen

andof stressraiserson the value of the endurancelimit of metals,Univ. Ill.,Engug.Exp. Stat.TR 16. 61.6

YEN C. S. andDOLAN T.J. (1952) Acritical reviewof thecriteriafor notch-sensitivityin fatigueof metals,Univ. Ill., Engng.Exp. Stat. No. 398. 52.1; 63.3

YoKoBoRs T. (1954) The statistical aspectof fatigue fracture of metals,Rep. Inst.Sci. Technol.,Tokyo,8 (1), 5—12; AMR 8, Rev. 102. 92

(1955) Theory of fatigue fracture.1. Phys. Soc.Ja/san10, (5), 368—374; AMR 9,Rev. 1822. 85.1

YORK J.E. (1958) Hydro fatigue testof theC13OA Hercules,Inst. aero.Sci. Prep.781; Index aero. 127/14/5. 25.33

YOUNG W. E. (1944) An investigationof the cross-springpivot J. A/s/sI. Meek. 11,All3—A120. 34.2

Yu As-T5NG and JossNsToNB. G. (1949) A method for vibration fatigue testsofstrandedconductorProc. Soc. Ex/s. StressAnal. 4, 1—6; AMR 3, Rev.267. 32

ZAHBROW J. L. and FONTANA M. G. (1949) Mechanicalproperties,includingfatigue of aircraft alloys at very low temperaturesTrans. Amer. Soc. Metals41,480—518. 65.1

ZEERLEDERA. vos~(1935) On the developmentof fatiguetestsof alusninumanditslight alloysLigkt MetalsRet.2, 256; Allumiuio 4, 95—105. 21.1

Z5MMERL5 F. P. (1941) Symposiumon the surfacetreatmentof metals,Cleveland,Ohio. 33.2

ZUNELER B. (1956) Vormichtungen fur BetricbsfestigkcitsversucheKoustruktiou8 (1),15—18. 32.4

Anonymous

(1 933a) Modern fatigue testing machiacs(in German), Tee/sn.BIatter, Bergwerkzeit.23, 82—84, 98—99. 30

(l933b) TentativespecificationII of the DVM-Testing MethodA 113, EndurancebeadingtestZ. Metallk. 25, 27—28. 21.1

(1937) Nomenclaturefor various rangesof stressin fatigueProc. Amer. Soc. Test.Mater. 37, 159—163. 10

(l938a) Revolving cantileverbeam testing machineJ. Sci. mastwm.15 (1), 28—29.31.32

(l938b) Rayflex fatigue testing machineAatomot. mudastr. N.Y. 78 (Feb), 211—212.31.24

(1938c) Dynamicfatigue testingmachinesMachiuery,Loud. 52 (1344),469—471. 30(1941) The effect of type of testingmachine on fatigue test resultsProc. Amer.Sac.

Test. Mater. 41, 133. 64.2(1944) Statistical analysisfor a new procedurein sensitivity experiments,AMP

Rep.no. 101 .IR, StatisticalResearchGroup, Princeton,no. 40. 95(1946) Provingrings for calibrating testingmachines,National Bureauof Standards

C454. 41.1; 43.1(1948a)Fatigue testing machinefor wire Ret.Sri. mmtmm.19, 930—931. 33.1(1 948b) Symbols and nomenclaturefor fatigue testing Bull. Amer. Soc. Test. Mat.

(153), 36—37. 10(1950) Presentationof technicalinformation Nature, Loud. 166, 500—501. 80(1951) NcucDauerschwing-Prtifmaschincn(in English) Engineer,Laud. 192, 671.

30Metallurgical researchat the NationalPhysicallaboratorymrou Coal Tr. Ret.162, 1251—1253; Foaudry Tr. i. 9,607. 31.11Viclprobenmaschissefur Daucrschwingvcrsuche(in English) Fosudry Tr. J.90, 607—608. 31.21Report on Comet accident investigation: Part 3. Fatigue tests on thepressurecabin and wings, RAE, AccidentNoteNo. 263; CAP 127.

25.1; 54.7Strain and vibration testing Metal mud., Laud. 88 (20), 417—418; Indexacro. 104/12/7. 43.3Structureslaboratory, Acro. Res. TN 181; Index acro. 107/14/3. 33

IV. COLLECTIVE PUBLICATIONSZ

Zn’s’s’E C. A. and WORDEN C. 0. (1951) Fractographic registrations of fatigueTrans.Amer.Soc. Metals43, 958. 40

1- Handbooks

EisenhartC. (Editor) (1947): SelectedTechniquesof StatisticalAnalysis,McGraw-HillBook Comp., New York.

(1951b)

(l95lc)

(1954)

(1956)

(1958)

302 303

BIBLIOGRAPHY BIBLIOGRAPHY

Hetenyi, (Editor) (1950) Handbook of Experimental Analysis,JohnWiley & Sons,NewYork.

Lyman, T. (Editor) (1948) ASMMetalsHandbook, Cleveland,Ohio.Siebel,E. & Ludwig N. (Editors) (1958) Prüf- andMesseiurichtuugeu,Zweite Aufiage

(Bd. I vom Handbuchder Werkstqffpri~fung)Springer-Verlag,Berlin.Alcoa (1940) StructuralAluminumHandbook.ASME (1954) ASMEHandbook: MetalsEngineeriugDesign, NewYork.AWS (1938): WeldingHandbook.Batelle Memorial Institute (1941): Preventionof the Failure of Metals under Re/seated

Stresses,JohnWiley & Sons,New York.

2. Proceedingsof Conferences1940 ASM: Sym/sosiumon Surface Treatmentof Metals, Cleveland,Ohio. Publ.:

Proc. 1941.1946 ASTM: Symposiumon Testingof Bearings. Publ.: STP 70.1946 ASTM: Symposiumon Testingof PartsandAssemblies.Pubi.: STP 72.1946 Melbourne: Symposiumon Fatigue. PubI.: Proc. 1947.1948 VII IUTAM Goof.,Paris.1948 mute~tioualConferenceon Surface Reactions.Publ.: Corrosion—PublishingCo.1951 ASTM: Symposiumon StatisticalNature ofFatigue. PubI.: STP 121.1952 ASTM: Symposiumon Fatigue with Emphasison Statistical Approach. PubI.:

STP137.1950 MIT: Couf on Fractureand Fatigue. PubI.,Proc. 1952.1952 Institute of Metals: Symposiumon Propertiesof Metallic Surfaces,London.1953 ASTM: Symposiumon FrettingCorrosion. Publ.: STP 144.1954 ASTM: Symposiumon Effectof Cyclic HeatingandStressingof Metalsat Elevated

Temperatures.Publ.: STP 165.1955 Nottingham: Symposium on Fatigue.1955 Stockholm: Colloquiumon Fatigue. Publ. Proc. 1956.1956 ColumbiaUniv.: Conf. on Fatigue in Aircraft Structures. Pubi.: Proc. 1956.1956 London: Conf. on Fatigueof Metals.1952—1958ICAF: Conferences: 1st Conf. Amsterdam1952,2nd Conf. Stockholm

1953, 3rd Conf. Cranfield 1955, 4th Conf. Zurich 1956, 5th Conf. Bruxelles1958.

3. SpecIal Technical PublicationsARC (1957): List of current paperspublished for the Aeronautical Research

Council Nos. 301—350.ARC (1958): Publishedreports and memorandaof the Aeronautical Research

Council, ARC R & M 2850; Indexaero.1/14/6.Alcoa (1950): Alcoa aluminumandits alloys.ADA (1955): The propertiesof aluminum and its alloys. ADA Inf. Bull. (2);

Index aero.269/12/5.ASM—SLA joint Committee(1950): ASM—SLA MetallurgicalLiteratureclassifica-

tion.ASM (1954): Fatigue. ASM, Cleveland,Ohio.ASM (1957): Fatiguedurability of carburizedsteel. ASM, Cleveland,Ohio.ASTM CommitteeE-9 on Fatigue (1949): Manual on Fatigue Testiug. STP91.

(1958): A tentativeguidefor fatiguetestingand thestatisticalanalysisoffatiguedata. STP91-A.

Univ. Ill., Engng.Exp.Stat.(1951): “Preparingtechnicalmaterialfor publication;a manualfor authorsof College and Station publications,” Circular SeriesNo. 62, Urbana.

Royal Society (1950): “General noteson the preparationof scientific papers.”CambridgeUniversityPress,London.

U.S. Navy Department,Bureauof Aeronautics(1938): “Theory and practice ofmagnaflux testing.” Aeronautical Mat. Lab., Naval Aircraft Factory, SerialNo. 381.

)

304305