Modeling crack closure and damage in variable amplitude fatigue using smooth specimen fatigue test data

被引:5
作者
El-Zeghayar, M. [1 ]
Topper, T. H. [1 ]
Conle, F. A.
Bonnen, J. J. F. [2 ]
机构
[1] Univ Waterloo, Dept Civil Engn, Waterloo, ON N2L 3G1, Canada
[2] Ford Motor Co, Dearborn, MI 48121 USA
关键词
Fatigue crack closure; Crack opening stress; Effective strain-life curve; Steady state crack opening stress; Variable amplitude fatigue loading; PROPAGATION; STEEL;
D O I
10.1016/j.ijfatigue.2010.08.010
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
During overloads in variable amplitude fatigue, local stresses at small cracks growing from notches reach yield stress magnitude. Such high stress levels result in a large decrease in crack opening stress and an increase in the fatigue damage of subsequent smaller stress cycles. This paper presents a methodology for modeling changes in crack opening stress level and fatigue damage using data derived from periodic underload fatigue tests of smooth specimens. Predicted crack closure stress levels agree well with those obtained from crack growth observations made with a high magnification microscope. (C) 2010 Elsevier Ltd. All rights reserved.
引用
收藏
页码:223 / 231
页数:9
相关论文
共 17 条
[1]  
Dabayeh A., 1980, INT J FATIGUE, V17, P261
[2]  
DABAYEH A, 1998, THESIS U WATERLOO WA
[3]  
DUQUESNAY DL, 1991, THESIS U WATERLOO WA
[4]  
DUQUESNAY DL, 2001, SAE TECHNICAL PAPER
[5]  
Elber W., 1971, Damage tolerance in aircraft structures, P230, DOI DOI 10.1520/STP486-EB
[6]   FATIGUE CRACK-PROPAGATION OF SHORT CRACKS [J].
ELHADDAD, MH ;
SMITH, KN ;
TOPPER, TH .
JOURNAL OF ENGINEERING MATERIALS AND TECHNOLOGY-TRANSACTIONS OF THE ASME, 1979, 101 (01) :42-46
[7]   Prediction of crack-opening stress levels for 1045 as-received steel under service loading spectra [J].
Khalil, M ;
Topper, TH .
INTERNATIONAL JOURNAL OF FATIGUE, 2003, 25 (02) :149-157
[8]  
LAM T, 1997, INT J FATIGUE, V19, P137
[9]  
McEvily AJ, 1977, FAT 1977 C CAMBR UK, P1
[10]  
MILLER KJ, 1984, P IUTAM ESH MEM C 19, P477