First-ply failure analysis of laminated composite cylindrical panels

被引：5
|
作者：
Rattanawangcharoen, N [1 ]
机构：
[1] Univ Manitoba, Dept Civil Engn, Winnipeg, MB R3T 5V6, Canada
来源：
JOURNAL OF REINFORCED PLASTICS AND COMPOSITES | 2005年 / 24卷 / 14期
关键词：
laminated composite cylindrical panels; first-ply failure; three-dimensional finite element model; mixed finite element; panel with openings;
D O I：
10.1177/0731684405051657
中图分类号：
TB33 [复合材料];
学科分类号：
摘要：
A first-ply failure (FPF) analysis of laminated composite cylindrical panels is presented in this paper. In the computation of stress and strain components, a 3D layerwise mixed stress-displacement finite element model is employed. The maximum stress, Tsai-Hill, Tsai-Wu, and Hoffman failure theories are used in the prediction of the FPF loads. This study illustrates that all four theories provide more or less the same FPF loads. The effects of the ply layup scheme, the fiber orientation angle, the panel thickness, the loading direction, and the location of the opening on the FPF loads of laminated cylindrical panels, are studied.
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页码：1521 / 1537
页数：17
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