EFFECT OF RESIDUAL-STRESSES ON CRACK-GROWTH FROM A HOLE

被引：4

作者：

LIU, AF

机构：

[1] Northrop Corp, Aircraft Div,, Hawthorne, CA, USA, Northrop Corp, Aircraft Div, Hawthorne, CA, USA

来源：

AIAA JOURNAL | 1984年 / 22卷 / 12期

关键词：

D O I：

10.2514/3.8852

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

This paper employs a 'variable stress intensity ratio' concept to elucidate the mechanics of a crack growing through a superimposed stress field (i. e. , combining the residual stresses around a hole and the subsequently applied cyclic stresses). The validity of this concept is supported by experimental results generated from specimens containing residual stresses.

引用

页码：1784 / 1785

页数：2