_STP_410-1966.pdf

PLANE STRAIN CRACK TOUGHNESS TESTING OF HIGH STRENGTH METALLIC MATERIALS by William F.Brcwn,Jr.,and John E.Srawiey ASTM SPECIAL TECHNICAL PUBLICATON NO.410 List price$5.50;30 per cent discount to members published by the AMERICAN SOCIETY FOR TESTING AND MATERIALS 1916 Race Street,Philadelphia,Pa.19103 in cooperation with the NATIONAL AERONAUTICS AND SPACE ADMINISTRATION Copyright by ASTM Intl(all rights reserved);Mon Dec 21 10:55:49 EST 2015Downloaded/printed byUniversity of Washington(University of Washington)pursuant to License Agreement.No further reproductions authorized.B Y AMERICAN SOCIETY FOR TESTING AND MATERIALS 1966 Library of Congress Catalog Card Number;66-29517 NOTE The Society is not responsible,as a body,for the statements and opinions advanced in this publication.Printed in Baltimore,Md.December,1967 Copyright by ASTM Intl(all rights reserved);Mon Dec 21 10:55:49 EST 2015Downloaded/printed byUniversity of Washington(University of Washington)pursuant to License Agreement.No further reproductions authorized.Foreword The objective of this report is to present a state-of-the-art survey of the analytical and experimental basis for determination of the plane strain crack toughness of metallic materials.It is anticipated that the informa-tion presented will serve as a basis for formulating recommended practices for K.testing.This publication is a cooperative effort of ASTM and NASA.Most of the data contained here were obtained at the NASA-Lewis Research Center as part of a NASA-NRL Cooperative Program for Plane Strain Fracture Toughness Testing.By cooperating with ASTM in publication of this information,NASA is helping to fulfill its obligation to provide the widest practicable and appropriate dissemination of the results from its research activities.This publication was prepared for ASTM Committee E-24 on Frac-ture Testing of Metals as the first report of Subcommittee I on High Strength Metallic Materials.The authors are with NASA Lewis Research Center,Cleveland,Ohio.The members of the subcommittee are:G.E.Pellissier(chairman),U.S.Steel Corp.;C.D.Beachem,U.S.Naval Research Laboratory;W.F.Brown,Jr.,NASA Lewis Research Center;J.E.Campbell,Battelle Memorial Inst.;T.J.Dolan,University of Illi-nois;R.H.Heyer,Armco Steel Corp.;J.H.Hodge,U.S.Steel Corp.;G.R.Irwin,U.S.Naval Research Laboratory;J.G.Kaufman,Alcoa Research Laboratory;J.M.Krafft,U.S.Naval Research Laboratory;F.R.Larson,Watertown Arsenal;J.R.Low,Jr.,General Electric Co.Research Laboratory;P.C.Paris,Lehigh University;J.E.Srawley,NASA Lewis Research Center;C.F.Tiffany,Boeing Co.;and Volker Weiss,Syracuse University.Copyright by ASTM Intl(all rights reserved);Mon Dec 21 10:55:49 EST 2015Downloaded/printed byUniversity of Washington(University of Washington)pursuant to License Agreement.No further reproductions authorized.Related ASTM Publications Flow and Fracture of Metals and Alloys in Nuclear Environments,STP 380(1 965),$24.00 Fracture Toughness Testing and Its Applications,STP 381(1965),$19.50 Copyright by ASTM Intl(all rights reserved);Mon Dec 21 10:55:49 EST 2015Downloaded/printed byUniversity of Washington(University of Washington)pursuant to License Agreement.No further reproductions authorized.Contents Introduction 1 Fundamentals of Specimen Design and Testing 2 Popin K,c Measurements with Flat Plate Specimens 5 K Calibrations of Specimens 8 Adjustment of Two-Dimensional K Calibrations 8 Methods for K Calibration 9 Center-Cracked Plate Under Uniform Tension 11 Double-Edge-Cracked Plate 11 Single-Edge-Cracked Plate Specimens 11 Single-Edge-Cracked Plates in Tension 12 Single-Edge-Cracked Bend Specimens 13 Crackline Loaded Single-Edge-Cracked Specimen 14 Circumferentially Cracked Round Bar 15 Specimen Size Requirements 16 Crack Length Requirement 20 Thickness Requirement 23 Ligament Requirement 25 Summary of Suggested Size Requirements 25 Variability of Ki,Results 26 Practical Specimen Types 27 Recommended Specimen Dimensions and Corresponding Load Re-quirements 28 Considerations in Selecting Specimens for Particular Applications 29 Surface-Crack Specimen 30 Cracked Charpy Specimens 33 Instrumentation 34 Displacement Measurements 34 Electric Potential Measurements 37 Acoustic Emission 40 Comparison of Methods 40 Criteria for Analysis of Load-Displacement Records 41 Types of Load-Displacement Records 42 Criteria and Data Analysis 44 Specimen Preparation and Testing 46 Fatigue Crack Starter Notches 46 Fatigue Cracking 48 Face Grooving 51 Pin Friction Effects in Bendi ng 53 Appendixes IBasis for the Analysis of Load-Displacement Records 56 IISpecimen Types 60 IIINotation 62 References 63 Discussion 66(Discussers and page numbers:M.J.Manjoine,66;E.J.Ripling,70;W.K.Wilson,75;C.E.Feddersen,77;H.P.Chu,79;G.M.Orner and B.S.Lement,82;J.G.Kaufman.86;R.H.Heyer,86;P.N.Randall,88;S.R.Novak and S.T.Rolfe,126)Copyright by ASTM Intl(all rights reserved);Mon Dec 21 10:55:49 EST 2015Downloaded/printed byUniversity of Washington(University of Washington)purs