On the simulation of crack-propagation in pressurized fuselages
被引:0
|
作者:
Rankin, CC
论文数: 0引用数: 0
h-index: 0
机构:
Lockheed Martin, Palo Alto, CA USALockheed Martin, Palo Alto, CA USA
Rankin, CC
[1
]
Riks, E
论文数: 0引用数: 0
h-index: 0
机构:
Lockheed Martin, Palo Alto, CA USALockheed Martin, Palo Alto, CA USA
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
关键词:
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.