CLOSED-FORM SOLUTION FOR THE FREE-EDGE EFFECT IN CROSS-PLY LAMINATES

被引：44
|
作者：
BECKER, W
机构：
[1] Dornier GmbH, Deutsche Aerospace, Abteilung R5T111, W-7990 Friedrichshafen-1
来源：
COMPOSITE STRUCTURES | 1993年 / 26卷 / 1-2期
关键词：
D O I：
10.1016/0263-8223(93)90042-O
中图分类号：
O3 [力学];
学科分类号：
08 ; 0801 ;
摘要：
Within the framework of linear elasticity the free-edge effect of a symmetric cross-ply laminate is treated in a closed-form analytical way. To this end a higher-order plate theory approach is used. The essential characteristic of the present analysis is the introduction of a warp deformation mode for the near-edge displacements. For a laminate coupon under uniaxial tension the displacement field and the accompanying stresses are determined. In particular, this includes the straightforward calculation of the interlaminar stress components.
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页码：39 / 45
页数：7
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