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ASTM Selected Technical Papers
Fatigue Crack Growth Under Spectrum Loads
By
RP Wei,
RP Wei
1
Lehigh University
, Bethlehem, Pa.
; ASTM Committee E-24, symposium cochairman
.
Search for other works by this author on:
RI Stephens
RI Stephens
2
The University of Iowa
, Iowa City, Iowa
; ASTM Committee E-9, symposium cochairman
.
Search for other works by this author on:
ISBN-10:
0-8031-0344-1
ISBN:
978-0-8031-0344-3
No. of Pages:
351
Publisher:
ASTM International
Publication date:
1976
Description
The Symposium on Fatigue Crack Growth Under Spectrum Loads was held on 23-24 June 1975 at the Seventy-eighth Annual Meeting of the American Society for Testing and Materials in Montreal, Quebec, Canada. Committee E24 on Fracture Testing of Metals and Committee E09 on Fatigue sponsored the symposium. R. P. Wei, Lehigh University, and R. I. Stephens, The University of Iowa, served as the symposium cochairmen. Serving as members of the Symposium Organizing/Program Committee and as session chairmen were J. M. Barsom, U. S. Steel Corp.; W. G. Clark, Jr., Westinghouse R & D Center; N. E. Dowling, Westinghouse R & D Center; C. M. Hudson, NASA Langley Research Center; E. K. Walker, Lockheed California Co.; and Howard Wood, AFFDL/FBR, Wright-Patterson AFB.
Wei, R, & Stephens, R.
Fatigue Crack Growth Under Spectrum Loads. ISBN-10: 0-8031-0344-1
ISBN: 978-0-8031-0344-3
No. of Pages: 351
ISBN (electronic): 978-0-8031-4672-3
Publisher: ASTM International
Published: 1976
Download citation file:
Table of Contents
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IntroductionByRP Wei,RP Wei1Lehigh University,Bethlehem, Pa.; ASTM Committee E-24,symposium cochairman.Search for other works by this author on:RI StephensRI Stephens2The University of Iowa,Iowa City, Iowa; ASTM Committee E-9,symposium cochairman.Search for other works by this author on:
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Observations on the Prediction of Fatigue Crack Growth Propagation Under Variable-Amplitude LoadingByJ SchijveJ Schijve1Professor, Department of Aeronautical Engineering,Delft University of Technology,Delft,.The NetherlandsSearch for other works by this author on:
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Fatigue Crack Growth with Negative Stress Ratio Following Single Overloads in 2024-T3 and 7075-T6 Aluminum AlloysByRI Stephens,RI Stephens1Professor and research assistants, respectively, Materials Engineering Division,The University of Iowa,Iowa City, Iowa 52242.Search for other works by this author on:DK Chen,DK Chen1Professor and research assistants, respectively, Materials Engineering Division,The University of Iowa,Iowa City, Iowa 52242.Search for other works by this author on:BW HomBW Hom1Professor and research assistants, respectively, Materials Engineering Division,The University of Iowa,Iowa City, Iowa 52242.Search for other works by this author on:
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Effect of Single Overload/Underload Cycles on Fatigue Crack PropagationByWX Alzos,WX Alzos1Mechanical engineer, Engineering Service Division,E. I. DuPont de Nemours and Company,Wilmington, Del. 19898.Search for other works by this author on:AC Skat, Jr,AC Skat, Jr2Graduate research assistant and professor, respectively,School of Mechanical Engineering, Purdue University,West Lafayette, Ind. 47907.Search for other works by this author on:BM HillberryBM Hillberry2Graduate research assistant and professor, respectively,School of Mechanical Engineering, Purdue University,West Lafayette, Ind. 47907.Search for other works by this author on:
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Effects of Rest Time on Fatigue Crack Retardation and Observations of Crack ClosureByWN Sharpe, Jr,WN Sharpe, Jr1Professor,College of Engineering, Michigan State University,East Lansing, Mich. 48842.Search for other works by this author on:DM Corbly,DM Corbly2Research metallurgist and materials research engineer, respectively, Metals Behavior Branch, Metals & Ceramics Division,Air Force Materials Laboratory,Wright-Patterson AFB, Ohio 45433.Search for other works by this author on:AF Grandt, JrAF Grandt, Jr2Research metallurgist and materials research engineer, respectively, Metals Behavior Branch, Metals & Ceramics Division,Air Force Materials Laboratory,Wright-Patterson AFB, Ohio 45433.Search for other works by this author on:
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Mechanisms of Overload Retardation During Fatigue Crack PropagationByPJ Bernard,PJ Bernard1Research metallurgist,Electricity Supply Board,Dublin.Search for other works by this author on:TC Lindley,TC Lindley2Research officers,Central Electricity Research Laboratories,Leatherhead,.United KingdomSearch for other works by this author on:CE RichardsCE Richards2Research officers,Central Electricity Research Laboratories,Leatherhead,.United KingdomSearch for other works by this author on:
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Spike Overload and Humidity Effects on Fatigue Crack Delay in Al 7075-T651ByO Buck,O Buck1Group leader and senior staff associate, respectively,Science Center, Rockwell International,Thousand Oaks, Calif. 91360.Search for other works by this author on:JD Frandsen,JD Frandsen1Group leader and senior staff associate, respectively,Science Center, Rockwell International,Thousand Oaks, Calif. 91360.Search for other works by this author on:HL MarcusHL Marcus2professor, Mechanical Engineering Department,University of Texas,Austin, Tex. 78712.Search for other works by this author on:
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Influences of Chemical and Thermal Environments on Delay in a Ti-6Al-4V Alloy
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Effect of Various Programmed Overloads on the Threshold for High-Frequency Fatigue Crack GrowthBySW Hopkins,SW Hopkins1Pratt Whitney Aircraft, Materials Engineering and Research Laboratory,E. Hartford, Conn. 06108; Mr. Rau is now withFailure Analysis Associates,Palo Alto, Calif. 94304.Search for other works by this author on:CA Rau,CA Rau1Pratt Whitney Aircraft, Materials Engineering and Research Laboratory,E. Hartford, Conn. 06108; Mr. Rau is now withFailure Analysis Associates,Palo Alto, Calif. 94304.Search for other works by this author on:GR Leverant,GR Leverant1Pratt Whitney Aircraft, Materials Engineering and Research Laboratory,E. Hartford, Conn. 06108; Mr. Rau is now withFailure Analysis Associates,Palo Alto, Calif. 94304.Search for other works by this author on:A YuenA Yuen1Pratt Whitney Aircraft, Materials Engineering and Research Laboratory,E. Hartford, Conn. 06108; Mr. Rau is now withFailure Analysis Associates,Palo Alto, Calif. 94304.Search for other works by this author on:
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A Model for Fatigue Crack Growth Delay Under Two-Level Block LoadsByOA Adetifa,OA Adetifa1Research student and professor, respectively, Department of Civil Engineering,University of Waterloo,Waterloo, Ontario N2L 3G1,.CanadaSearch for other works by this author on:CVB Gowda,CVB Gowda2Senior engineer, Advanced Reactors Division,Westinghouse Corp.,Madison, Pa. 15663.Search for other works by this author on:TH TopperTH Topper1Research student and professor, respectively, Department of Civil Engineering,University of Waterloo,Waterloo, Ontario N2L 3G1,.CanadaSearch for other works by this author on:
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Mathematical Modeling of Crack Growth Interaction EffectsByPD Bell,PD Bell1Senior structural mechanics engineer and member, Systems Engineering Staff, respectively,Grumman Aerospace Corporation,Bethpage, N. Y. 11714.Search for other works by this author on:A WolfmanA Wolfman1Senior structural mechanics engineer and member, Systems Engineering Staff, respectively,Grumman Aerospace Corporation,Bethpage, N. Y. 11714.Search for other works by this author on:
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Experimental Results and a Hypothesis for Fatigue Crack Propagation Under Variable-Amplitude LoadingByGH Jacoby,GH Jacoby1Director,Carl Schenck AG,Darmstadt,.West GermanySearch for other works by this author on:H Nowack,H Nowack2Department head and research fellow, respectively,Deutsche Forschungs- und Versuchsanstalt für Luft- und Raumfahrt (DFVLR), Institut für Werkstoff-Forschung,Porz,.West GermanySearch for other works by this author on:HTM van LipzigHTM van Lipzig2Department head and research fellow, respectively,Deutsche Forschungs- und Versuchsanstalt für Luft- und Raumfahrt (DFVLR), Institut für Werkstoff-Forschung,Porz,.West GermanySearch for other works by this author on:
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Effect of Spectrum Type on Fatigue Crack Growth LifeByJA Reiman,JA Reiman1Aerospace engineers, Fatigue and Fracture Branch, Structures Division,ASD/ENF,Wright-Patterson AFB, Ohio, 45433.Search for other works by this author on:MA Landy,MA Landy1Aerospace engineers, Fatigue and Fracture Branch, Structures Division,ASD/ENF,Wright-Patterson AFB, Ohio, 45433.Search for other works by this author on:MP KaplanMP Kaplan1Aerospace engineers, Fatigue and Fracture Branch, Structures Division,ASD/ENF,Wright-Patterson AFB, Ohio, 45433.Search for other works by this author on:
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Stress Spectrums for Short-Span Steel BridgesByKH Klippstein,KH Klippstein1Senior research engineer and section supervisor, respectively, Application Research Division,Research Laboratory, United States Steel Corporation,Monroeville, Pa. 15146.Search for other works by this author on:CG SchillingCG Schilling1Senior research engineer and section supervisor, respectively, Application Research Division,Research Laboratory, United States Steel Corporation,Monroeville, Pa. 15146.Search for other works by this author on:
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Fatigue Crack Growth Under Variable-Amplitude Loading in Various Bridge SteelsByJM BarsomJM Barsom1Section supervisor, Mechanical Behavior,Research Laboratory, United States Steel Corporation,Monroeville, Pa. 15146.Search for other works by this author on:
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Equivalent Constant-Amplitude Concept for Crack Growth Under Spectrum LoadingByW ElberW Elber1Research engineer,NASA Langley Research Center,Hampton, Va. 23665.Search for other works by this author on:
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Crack Growth in Ti-8Al-1Mo-1V with Real-Time and Accelerated Flight-by-Flight LoadingByLA ImigLA Imig1Research engineer,NASA Langley Research Center,Hampton, Va. 23665.Search for other works by this author on:
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Prediction of Fatigue Crack Growth under Irregular LoadingByDV Nelson,DV Nelson1Research assistant, Mechanical Engineering Dept.,Stanford University,Stanford, Calif. 94305; now withGeneral Electric Co.,Sunnyvale, Calif. 94086.Search for other works by this author on:HO FuchsHO Fuchs2Professor, Mechanical Engineering Dept.,Stanford University,Stanford, Calif. 94305.Search for other works by this author on:
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Structural Reliability Prediction Method Considering Crack Growth and Residual StrengthBySR Varanasi,SR Varanasi1Specialist engineers, Stress and Fatigue Research Group,Boeing Commercial Airplane Company,Seattle, Wash. 98124.Search for other works by this author on:IC WhittakerIC Whittaker1Specialist engineers, Stress and Fatigue Research Group,Boeing Commercial Airplane Company,Seattle, Wash. 98124.Search for other works by this author on:
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Spectrum Crack Growth Prediction Method Based on Crack Surface Displacement and Contact AnalysesByHD Dill,HD Dill1Project strength engineer and strength engineer, respectively,McDonnell Aircraft Company,St. Louis, Mo. 63166.Search for other works by this author on:CR SaffCR Saff1Project strength engineer and strength engineer, respectively,McDonnell Aircraft Company,St. Louis, Mo. 63166.Search for other works by this author on:
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Spectrum Fatigue Crack Growth in LugsByLF Impellizzeri,LF Impellizzeri1Section chief-Strength and lead engineer-Strength, respectively,McDonnell Aircraft Company, McDonnell Douglas Corporation,St. Louis, Mo. 63166.Search for other works by this author on:DL RichDL Rich1Section chief-Strength and lead engineer-Strength, respectively,McDonnell Aircraft Company, McDonnell Douglas Corporation,St. Louis, Mo. 63166.Search for other works by this author on:
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All rights reserved. This material may not be reproduced or copied, in whole or in part, in any printed, mechanical, electronic, film, or other distribution and storage media, without the written consent of the publisher.
© 1976
ASTM International
