PROGRESSIVE FAILURE ANALYSIS OF COMPOSITE PLATES BY THE FINITE STRIP METHOD

被引:17
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
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.
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页码:49 / 61
页数:13
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