Stress intensity factor and compliance solutions for an eccentrically loaded single edge cracked geometry

被引:11
作者
John, R [1 ]
机构
[1] USAF,WRIGHT LAB,MAT DIRECTORATE,MLLN,WRIGHT PATTERSON AFB,OH 45433
关键词
compliance; eccentric load; fracture; fatigue crack growth; single edge crack; stress intensity factor; test geometry;
D O I
10.1016/S0013-7944(97)00070-2
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
Eccentrically pin-loaded single edge cracked geometries are an excellent alternative to compact tension type geometries for testing some advanced composite materials. This paper discusses the development of stress intensity factor and compliance solutions for an eccentrically pin-loaded single edge cracked geometry, ESE(T). (C) 1997 Elsevier Science Ltd.
引用
收藏
页码:87 / 96
页数:10
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