PROGRESSIVE FAILURE ANALYSIS OF COMPOSITE PLATES BY THE FINITE STRIP METHOD

被引：16
|
作者：
CHEUNG, MS [1 ]
AKHRAS, G [1 ]
LI, W [1 ]
机构：
[1] ROYAL MIL COLL CANADA,DEPT CIVIL ENGN,KINGSTON,ON K7K 5L0,CANADA
来源：
COMPUTER METHODS IN APPLIED MECHANICS AND ENGINEERING | 1995年 / 124卷 / 1-2期
关键词：
D O I：
10.1016/0045-7825(95)00788-3
中图分类号：
T [工业技术];
学科分类号：
08 ;
摘要：
In the present study, a finite strip method for the progressive failure analysis of anisotropic composite laminates is developed based on the higher-order shear deformation theory and Lee's strength criterion. This method produces results in a good agreement with existing analytical and numerical solutions. The effects of fibre orientation and the number of plies on the load-carrying capacity are also investigated in numerical examples.
引用
收藏
页码：49 / 61
页数：13
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