Nonlinear dynamic instability of laminated composite plates using finite element method

被引：43

作者：

Balamurugan, V

Ganapathi, M

Varadan, TK

机构：

[1] INST ARMAMENT TECHNOL,PUNE 411025,MAHARASHTRA,INDIA

[2] INDIAN INST TECHNOL,DEPT AEROSP ENGN,MADRAS 600036,TAMIL NADU,INDIA

来源：

COMPUTERS & STRUCTURES | 1996年 / 60卷 / 01期

关键词：

D O I：

10.1016/0045-7949(95)00368-1

中图分类号：

TP39 [计算机的应用];

学科分类号：

081203 ; 0835 ;

摘要：

investigation is carried out on the dynamic instability of anisotropic laminated composite plates considering geometric nonlinearity. The mathematical model is formulated using C degrees shear flexible, field consistent, QUAD-9 plate elements. The nonlinear governing equations are solved using the direct iteration technique. The effect of a large amplitude on the dynamic instability is studied for a simply-supported laminated composite plate. Detailed numerical results are presented for various parameters, namely, ply-angle, number of layers and thickness of plates. Copyright (C) 1996 Elsevier Science Ltd

引用

页码：125 / 130

页数：6

共 14 条

[1] PARAMETRIC-INSTABILITY OF THICK, ORTHOTROPIC, CIRCULAR CYLINDRICAL-SHELLS [J].