1、JAI Fatigue and Fracture Mechanics:36th VolumeSTP 1508NeuWallinThompsonJournal of ASTM InternationalSpecial Technical Publication STP 1508Fatigue and Fracture Mechanics36th VolumeRichard W.NeuKim R.W.WallinSteven R.ThompsonGuest Editorswww.astm.orgISBN:978-0-8031-3416-4Stock#:STP1508Cover image cour
2、tesy of AFRL/RXSAIn cooperation with ESIS Journal of ASTM InternationalSpecial Technical Publication STP1508Fatigue and Fracture Mechanics:36th VolumeGuest Editors:Richard W.NeuKim R.W.WallinSteven R.ThompsonASTM International100 Barr Harbor DrivePO Box C700West Conshohocken,PA 19428-2959Printed in
3、U.S.A.ASTM Stock#:STP1508 Library of Congress Cataloging-in-Publication DataISBN:978-0-8031-3416-4ISSN:1040-3094Copyright 2009ASTM International,West Conshohocken,PA.All rightsreserved.This material may not be reproduced or copied,in whole or in part,in anyprinted,mechanical,electronic,film,or other
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9、paper.Printed in Bridgeport,NJOctober,2009 ForewordTHIS SPECIAL ISSUE OF JAI,Special Technical Publication STP 1508,Fatigue andFracture Mechanics:36th Volume,contains papers presented at the Seventh Interna-tional ASTM/ESIS Symposium on Fatigue and Fracture?36th ASTM National Sympo-sium on Fatigue a
10、nd Fracture Mechanics?held November 14-16,2007 in Tampa,Florida.The symposium was jointly sponsored by ASTM International Committee E08 on Fatigueand Fracture and the European Structural Integrity Society?ESIS?.The symposium was co-chaired by Dr.Richard W.Neu of Georgia Institute of Technol-ogy,USA,
11、Dr.Kim R.W.Wallin of the Academy of Finland,Finland,and Mr.Steven R.Thompson of Air Force Research Laboratory,USA.ContentsOverview.ixSwedlow LectureAnalysis of Material Inhomogeneity in the European Round Robin Fracture ToughnessData SetJ.A.Joyce and X.Gao.3Elastic-Plastic Fracture MechanicsThe Sign
12、ificance of a Crack Growth Law for a C(T)Fracture Specimen UndergoingStable Crack ExtensionJ.R.Donoso,K.Vasquez,and J.D.Landes.33Assessing the Loading Rate for a Fracture Toughness Test in the Ductile-to-BrittleTransition RegionE.Lucon and M.Scibetta.54Experimental Estimation of J-R Curves from Load
13、-CMOD Record for SEBSpecimensX.-K.Zhu,B.N.Leis,and J.A.Joyce.66On the Quantification of the Constraint Effect Along a Three-Dimensional Crack FrontX.Wang.87Residual Stress Effects on FatigueInfluence of Residual Stresses on Fretting Fatigue Life Prediction in Ti-6Al-4VP.J.Golden,D.Buchanan,and S.Nab
14、oulsi.105Fatigue Response of Aluminum Aircraft Structure under Engineered Residual StressProcessingK.Langer,S.VanHoogen,and J.Hoover,II.122Influence of the Peening Intensity on the Fatigue Behavior of Shot Peened TitaniumComponentsH.Leitner,B.Oberwinkler,H.-P.Gaenser,and M.Stoschka.134Fretting Fatig
15、ue Behavior of Shot-Peened Ti-6Al-4V and IN100S.Mall,J.L.Ng,and E.Madhi.147Prediction of the Fatigue Limit of Prestrained Carbon Steel Under Tensile MeanStressM.Kang,K.Irisa,Y.Aono,and H.Noguchi.164Practical Challenges Testing Coupons with Residual Stresses from Cold ExpandedHolesL.Reid and J.Ransom
16、.183The Influence of Residual Stresses on the Fatigue Strength of Cold-Formed StructuralTubesS.Heinil,T.Bjrk,and G.Marquis.200The Influence of Residual Stress on the Design of Aircraft Primary StructureD.L.Ball.216Elastic-Plastic Finite-Element Analyses of Compression Precracking and Its Influenceon Subsequent Fatigue-Crack GrowthY.Yamada,J.C.Newman,III,and J.C.Newman,Jr.240 Compression Precracking to Generate Near Threshold Fatigue Crack Growth Rates inan Aluminum and Titanium AlloyJ.J.Ruschau