1、STP 1406 Fatigue and Fracture Mechanics:32nd Volume Ravinder Chona,editor ASTM Stock Number:STP1406 ASTM 100 Barr Harbor Drive PO Box C700 West Conshohocken,PA 19428-2959 Printed in the U.S.A.Copyright by ASTM Intl(all rights reserved);Tue Dec 15 13:10:18 EST 2015Downloaded/printed byUniversity of W
2、ashington(University of Washington)pursuant to License Agreement.No further reproductions authorized.ISBN:0-8031-2888-6 ISSN:1040-3094 Copyright?9 2002 AMERICAN SOCIETY FOR TESTING AND MATERIALS,West Conshohocken,PA.All rights reserved.This material may not be reproduced or copied,m whole or in part
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5、wers and at least on editor.The authors addressed all of the reviewers comments to the satisfaction of both the technical editor(s)and the ASTM Committee on Publications.The quahty of the papers in this publication reflects not only the obvious efforts of the authors and the technical edttor(s),but
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7、 September 2001 Copyright by ASTM Intl(all rights reserved);Tue Dec 15 13:10:18 EST 2015Downloaded/printed byUniversity of Washington(University of Washington)pursuant to License Agreement.No further reproductions authorized.Foreword This publication,Fatigue and Fracture Mechanics:32nd Volume,contai
8、ns papers presented at the symposium of the same name held at ASTM Headquarters,West Conshohocken,Pennsylvania,on 14-16 June 2000.The symposium was sponsored by ASTM Committee E-8 oD Fatigue and Fracture and was chaired by Dr.Ravinder Chona of Texas A&M University.Copyright by ASTM Intl(all rights r
9、eserved);Tue Dec 15 13:10:18 EST 2015Downloaded/printed byUniversity of Washington(University of Washington)pursuant to License Agreement.No further reproductions authorized.Contents TRANSITION ISSUES AND MASTER CURVES Microstructural Limits of Applicability of the Master Curve-M.T.KIRK,M.E.NATISHAN
10、,AND M.WAGENHOFER.3 Correlation Between Static Initiation Toughness Kjc and Crack Arrest Toughness Kin 2024-T351 Aluminum Alloy-K.WALLIN.17 NORMALIZATION PROCEDURES A Sensitivity Study on a Normalization Procedure-w.A.VAN DER SLUYS AND B.A.YOUNG.37 Separability Property and Load Normalization in AA
11、6061-T6 Aluminum Alloy-A.N.CASSANELLI,H.ORTIZ,J.E.WAINSTEIN,AND L.A.DEVEDIA.49 FATIGUE Physical Reasons for a Reduced AK as Correlation for Fatigue Crack Propagation-c.MARCI AND M.LANG.75 Influence of Specimen Geometry on the Random Load Fatigue Crack Growth-J.c.RADON AND K.NIKBIN.88 Fatigue Behavio
12、r of SA533-B1 Steds-j.-Y.HUANG,R.-Z.LI,K.-F.cnmN,R.-C.KUO,P.K.LIAW,B.YANG,AND J.-G.HUANG.105 Scanning Atomic-Force Microscopy on Initiation and Growth Behavior of Fatigue Slip-Bands in-Brass-Y.NAKAI,T.KUSUKAWA,AND N.HAYASHI.122 DYNAMIC LOADING-PART Compliance Ratio Method of Estimating Crack Length
13、in Dynamic Fracture Toughness Tests-J.A.JOYCE,P.ALBRECHT,H.C.TJIANG,AND W.J.WRIGHT.139 Dynamic Fracture Toughness Testing and Analysis of HY-100 Welds-s.M.GRAHAM,.158 WELDS AND CLADDING Creep Crack Growth in X20CrMoV 12 1 Steel Weld Joints-K.s.Kn,N.W.LEE,Y.K.CHUNG,AND J.J.PARK.179 Application of the
14、 Local Approach to Fracture in the Brittle-to-Ductile Transition Region of Mismatched Welds-F.MINAMI,T.KATOU,AND H.JING.195 An X-Specimen Test for Determination of Thin-Walled Tube Fracture Toughness-H.H.HSU,K.F.CHIEN,H.C.CHU,R.C.KUO,AND P.K.LIAW.214 APPLICATIONS An Energetic Approach for Large Duct
15、ile Crack Growth in Components-s.CHAPULIOT,S.MARIE,AND D.MOULIN.229 Copyright by ASTM Intl(all rights reserved);Tue Dec 15 13:10:18 EST 2015Downloaded/printed byUniversity of Washington(University of Washington)pursuant to License Agreement.No further reproductions authorized.vi CONTENTS Prediction
16、of Residual Stress Effects on Fracture Instability Using the Local Approach Y.YAMASHITA,K.SAKANO,M.ONOZUKA AND F.MINAMI.ANALYTICAL ASPECTS 247 Advantages of the Concise K and Compliance Formats in Fracture Mechanics Calculations-J.R.DONOSO AND J.D.LANDES.263 Three-Dimensional Analyses of Crack-Tip-Opening Angles and 5-Resistance Curves for 2024-T351 Aluminum Alloy-M.A.JAMES,J.C.NEWMAN,JR.,AND W.M.JOHNSTON,JR.279 COMPOSITES AND CERAMICS Modeling Multilayer Damage in Composite Laminates Under Stat