Torsional instability of moderately thick composite cylindrical shells by various shell theories

被引：4

|

作者：

Tabiei, A

Simitses, G

机构：

[1] University of Cincinnati, Cincinnati

来源：

AIAA JOURNAL | 1997年 / 35卷 / 07期

关键词：

D O I：

10.2514/2.230

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

[No abstract available]

引用

收藏

页码：1243 / 1246

页数：4

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