An equivalent driving force model for crack growth prediction under different stress ratios

被引:35
作者
Kwofie, Samuel [2 ]
Rahbar, Nima [1 ]
机构
[1] Univ Massachusetts Dartmouth, Dept Civil & Environm Engn, N Dartmouth, MA 02747 USA
[2] Kwame Nkrumah Univ Sci & Technol, Dept Mat Engn, Kumasi, Ghana
关键词
Stress ratio; Cyclic driving force; Static driving force; Equivalent driving force; Crack growth rate; LOAD RATIO; FATIGUE; THRESHOLD; PROPAGATION; CLOSURE;
D O I
10.1016/j.ijfatigue.2011.03.006
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
An equivalent driving force (EDF) model is proposed for the correlation and prediction of crack growth under different stress ratio, R, values. The equivalent driving force defines a completely-reversed stress intensity range that is expected to yield the same crack growth rate as a given stress intensity range Delta K and stress ratio R. Thus, the suggested equivalent driving force (EDF) model seeks to unify the crack growth data into a single master curve for fatigue design. The EDF depends on a single factor known as the mean-stress-sensitivity factor, which can be readily determined from experimental data. Application of the EDF model to the published data of Titanium and Aluminum alloys indicates that there exists an R-value below and above which the mean-stress-sensitivity factor differs. It was found that for -1 <= R <= 0.3 the mean-stress-sensitivity factor was much higher than for 0.3 < R <= 1. This difference in mean-stress-sensitivity to crack growth behavior in the two R-regimes could be explained in terms of the dominant mechanism controlling damage/crack growth rate. (C) 2011 Elsevier Ltd. All rights reserved.
引用
收藏
页码:1199 / 1204
页数:6
相关论文
共 18 条
[1]   Effect of load ratio and maximum stress intensity on the fatigue threshold in Ti-6Al-4V [J].
Boyce, BL ;
Ritchie, RO .
ENGINEERING FRACTURE MECHANICS, 2001, 68 (02) :129-147
[2]   Correlation and prediction of fatigue crack growth for different R-ratios using Kmax and ΔK+ parameters [J].
Dinda, S ;
Kujawski, D .
ENGINEERING FRACTURE MECHANICS, 2004, 71 (12) :1779-1790
[3]  
Donald K, 1999, INT J FATIGUE, V21, pS47
[4]  
Elber W., 1971, Damage tolerance in aircraft structures, P230, DOI DOI 10.1520/STP486-EB
[5]   EFFECT OF STRESS CYCLE ASYMMETRY ON FATIGUE CRACK GROWTH [J].
KLESNIL, M ;
LUKAS, P .
MATERIALS SCIENCE AND ENGINEERING, 1972, 9 (04) :231-&
[8]   A FATIGUE CRACK-GROWTH MODEL WITH LOAD RATIO EFFECTS [J].
KUJAWSKI, D ;
ELLYIN, F .
ENGINEERING FRACTURE MECHANICS, 1987, 28 (04) :367-378
[9]   Fatigue life prediction under conditions where cyclic creep-fatigue interaction occurs [J].
Kwofie, S. ;
Chandler, H. D. .
INTERNATIONAL JOURNAL OF FATIGUE, 2007, 29 (12) :2117-2124
[10]   An exponential stress function for predicting fatigue strength and life due to mean stresses [J].
Kwofie, S .
INTERNATIONAL JOURNAL OF FATIGUE, 2001, 23 (09) :829-836