On the simulation of crack-propagation in pressurized fuselages

被引：0
|
作者：
Rankin, CC [1 ]
Riks, E [1 ]
机构：
[1] Lockheed Martin, Palo Alto, CA USA
来源：
COLLECTION OF THE 41ST AIAA/ASME/ASCE/AHS/ASC STRUCTURES, STRUCTURAL DYNAMICS, AND MATERIALS CONFERENCE AND EXHIBIT, VOL 1 PTS 1-3 | 2000年
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D O I：
暂无
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
In this paper, we will discuss the finite element modeling of a crack propagating in a fuselage shell under increasing load. In particular, we will describe a computational procedure that enables the determination of the critical crack length, the point at which crack propagation becomes unstable.
引用
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页码：1405 / 1415
页数：3
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