Mixed mode fatigue growth of curved cracks emanating from fastener holes in aircraft lap joints

被引：0
|
作者：
J. H. Park
S. N. Atluri
机构：
[1] Center for Aerospace Research & Education 7704,
[2] Boelter Hall,undefined
[3] School of Engineering & Applied Science,undefined
[4] UCLA Los Angeles,undefined
[5] CA,undefined
[6] 90095-1600 USA,undefined
[7] Dept. of Safety Engng,undefined
[8] Chungbuk National University,undefined
[9] Cheongju,undefined
[10] Chungbuk 361–763,undefined
[11] Rep. of Korea,undefined
来源：
Computational Mechanics | 1998年 / 21卷
关键词：
Fatigue Crack Growth; Plane Stress; Initial Crack; Crack Growth Behavior; Isotropic Plate;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
The finite element alternating method is extended further for analyzing multiple arbitrarily curved cracks in an isotropic plate under plane stress loading. The required analytical solution for an arbitrarily curved crack in an infinite isotropic plate is obtained by solving the integral equations formulated by Cheung and Chen (1987a, b).
引用
收藏
页码：477 / 482
页数：5
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