On delamination buckling of composite laminates under compressive loading

被引:17
|
作者
Gaudenzi, P [1 ]
机构
[1] Univ Rome La Sapienza, Dipartimento Aerospaziale, I-00184 Rome, Italy
关键词
D O I
10.1016/S0263-8223(98)80017-2
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
The effects of the presence of a delamination on the buckling load of composite laminates under compression are investigated. The linearized buckling analysis for two-and three-dimensional solid finite elements is proposed as an effective and practical tool for the prediction of the critical loads both for bi-dimensional and for tri-dimensional cases. The accuracy of the numerical procedure is assessed by comparing the results with existing analytical solutions obtained from the literature for simple bi-dimensional applications. A tri-dimensional analysis is then presented for the case of a square plate with a circular delamination. The effects of radius and depth of the delamination on the buckling load are also illustrated. (C) 1997 Elsevier Science Ltd.
引用
收藏
页码:21 / 30
页数:10
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