Aeroelastic stability of aircraft with uncertain structural parameters

被引：0
|
作者：
Poirion, F [1 ]
机构：
[1] Off Natl Etud & Rech Aerosp, Chatillon, France
来源：
STRUCTURAL SAFETY AND RELIABILITY, VOLS. 1-3 | 1998年
关键词：
D O I：
暂无
中图分类号：
TU [建筑科学];
学科分类号：
0813 ;
摘要：
A stochastic finite element method is utilized in order to perfom a flutter analysis of an airplane with uncertain structural parameters.A second order perturbation technique yields too crude results to be applicable in an industrial context. In the other hand Monte carlo method has proved to be industrially effective in the sense that it can deal with high dimensional realistic problems.
引用
收藏
页码：947 / 950
页数：4
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