1、STP 982 Mechanics of Fatigue Crack Closure J.C.Newman,Jr.and Wolf Elber,editors#ASTM 1916 Race Street Philadelphia,PA 19103 Copyright by ASTM Intl(all rights reserved);Wed Dec 23 18:36:58 EST 2015Downloaded/printed byUniversity of Washington(University of Washington)pursuant to License Agreement.No
2、further reproductions authorized.ASTM Publication Code Number(PCN):04-982000-30 ISBN:0-8031-0996-2 Library of Congress Catalog Card Number:88-6303 Copyright by AMERICAN SOCIETY FOR TESTING AND MATERIALS 1988 NOTE The Society is not responsible,as a body,for the statements and opinions advanced in th
3、is pubUcation.Peer Review Policy Each paper published in this volume was evaluated by three peer reviewers.The authors addressed all of the reviewers comments to the satisfaction of both the technical editor(s)and the ASTM Committee on Pubhcations.The quality of the papers in this publication reflec
4、ts not only the obvious efforts of the authors and the technical editor(s),but also the work of these peer reviewers.The ASTM Committee on Publications acknowledges with appreciation their dedication and contribution of time and effort on behalf of ASTM.Printed in Baltimore,MD June 1988 Copyright by
5、 ASTM Intl(all rights reserved);Wed Dec 23 18:36:58 EST 2015Downloaded/printed byUniversity of Washington(University of Washington)pursuant to License Agreement.No further reproductions authorized.Foreword The International Symposium on Fatigue Crack Closure was held in Charleston,SC,on 1-2 May 1986
6、.ASTM Committees E-24 on Fracture Testing and E-9 on Fatigue were co-sponsors.J.C.Newman,Jr.,NASA Langley Research Center,and Wolf Elber,U.S.Army Aerostructures Directorate,presided as symposium chairmen and are editors of this pub-lication.Copyright by ASTM Intl(all rights reserved);Wed Dec 23 18:3
7、6:58 EST 2015Downloaded/printed byUniversity of Washington(University of Washington)pursuant to License Agreement.No further reproductions authorized.Herbert F.Hardrath Dedication Herbert F.Hardrath contributed greatly to the success ofASTM Committee E-9 on Fatigue.He was a member of the committee f
8、rom 1958 until his death on 25 September 1985,and was the Chairman of Committee E-9 from 1966 to 1971.Herb grew up in Manitowoc,WI,and joined the Navy during World War 11.He received a Bachelor of Science and a Master of Science degree in Civil Engineering at Tulane University and the Case Institute
9、 in Cleveland,OH.In 1947,he joined the National Advisory Committee on Aeronautics(NACA)as a Structural Engineer to forge a fatigue research effort.In 1952,he became the Head of the embryonic Fatigue Section.Under his leadership,the Fatigue Section became a Branch at the National Aeronautics and Spac
10、e Administration(NASA)Langley Research Center.In 1970,he was elevated to Assistant Division Chief of the Materials Division.Also in 1970,he received a Special Achievement Award for his amassed contri-butions.Herb retired from NASA in 1980.Herb was very active in ASTM Committee E-9 on Fatigue.He rece
11、ived the ASTM Award of Merit in 1970 for his many contributions to fatigue research and for the development of fatigue standards.He was invited,in 1970,to present the AIAA Structures Design Lecture.In 1972,he presented the ASTM Gillett Memorial Lecture and,in 1974,he presented the AIAA Dry den Resea
12、rch Lecture.Because of his expertise in fatigue and fracture mechanics.Herb was chosen to be pari of a select group to visit technical centers in the U.S.S.R.in 1976.Herb was the United States delegate to the International Committee on Aeronautical Fatigue(ICAF)from 1965 to 1980.In 1971,he hosted an
13、 international meeting of ICAF in Miami,FL.He presented the Sixth Plantema Memorial Lecture to open the 1977 ICAF meeting in the Federal Republic of Germany.As an eminent fatigue expert,he was chosen to participate in many investigations of fatigue problems in military and commercial aircraft,such a
14、s the B-47,F-111,C-5,and the DC-10.Herb is remembered for more than his technical accomplishments;he was a model for personal integrity and dedication.Copyright by ASTM Intl(all rights reserved);Wed Dec 23 18:36:58 EST 2015Downloaded/printed byUniversity of Washington(University of Washington)pursua
15、nt to License Agreement.No further reproductions authorized.Contents Introduction 1 MECHANISMS Fatigue Crack Closure:Observations and Technical SignificanceJAAP SCHIJVE 5 On Crack Closure in Fatigue Crack GrowthARTHUR J.MCEVILY 35 Plasticity Induced Fatigue Crack ClosureDAVID L.DAVIDSON 44 Overview
16、of Crack Closure at Near-Threshold Fatigue Crack Growth Levels PETER K.LIAW 62 On the Role of Crack Closure Mechanisms in Influencing Fatigue Crack Growth FoUovtlng Tensile Overloads in a Titanium Alloy:Near Threshold Versus Higher AK Behaviorc.M.WARD-CLOSE AND R.O.RITCHIE 93 The Effect of Test Frequency and Geometric Asperities on Crack Closure MechanismsJATIN K.SHETH AND WILLIAM W.GERBERICH 112 The Dependence of Crack Closure on Fatigue Loading Variables STEPHEN J.HUDAK,JR.AND DAVID L.DAVIDSON
