Buckling of laminated composite rectangular plates under transient thermal loading

被引：11

作者：

Shukla, KK ^{[1
]}

Nath, Y

机构：

[1] MNR Engn Coll, Dept Appl Mech, Allahabad 211004, Uttar Pradesh, India

[2] Indian Inst Technol, Dept Appl Mech, New Delhi 110016, India

来源：

JOURNAL OF APPLIED MECHANICS-TRANSACTIONS OF THE ASME | 2002年 / 69卷 / 05期

关键词：

D O I：

10.1115/1.1485755

中图分类号：

O3 [力学];

学科分类号：

08 ; 0801 ;

摘要：

This paper deals with the nonlinear dynamic buckling of laminated composite rectangular plates subjected to uniform time-dependent in-plane temperature-induced loading. The dynamic post-buckling deflection response is obtained and dynamic critical temperatures are estimated. The nonlinear governing equations of motion are solved analytically using fast Chebyshev series technique. The numerical results for CCCC, CCCS, CCSS, CSCS, CSSS and SSSS boundary conditions are presented.

引用

页码：684 / 692

页数：9

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