The stability of composite material stiffened conical shells under axial compression

被引：9

作者：

Li, LC ^{[1
]}

机构：

[1] Univ Western Ontario, Dept Mech & Mat Engn, London, ON N6A 5B9, Canada

来源：

COMPOSITE STRUCTURES | 1997年 / 38卷 / 1-4期

关键词：

D O I：

10.1016/S0263-8223(97)00053-6

中图分类号：

O3 [力学];

学科分类号：

08 ; 0801 ;

摘要：

The stability of composite material stiffened conical shells under uniform axial compression and with classical clamped boundary conditions is investigated. The effects of stiffeners are uniformly distributed over the whole surface of the shell, and the shell is treated as an equivalent orthotropic shell. A method of solution is developed by using energy principles and Rayleigh-Rize approximations. It is shown that the approach proposed in this paper is practical, effective and satisfactory. (C) 1997 Elsevier Science Ltd.

引用

页码：169 / 177

页数：9

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