TRANSVERSE-SHEAR EFFECTS ON BUCKLING AND POSTBUCKLING OF LAMINATED AND DELAMINATED PLATES

被引:18
作者
CHEN, HP
机构
[1] California State University, Department of Aerospace Engineering, Long Beach, CA
关键词
D O I
10.2514/3.11333
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The one-dimensional buckling and postbuckling solutions of unsymmetric laminates with clamped edges subjected to constant membrane strain loads are obtained based on the large deflection shear deformation theory. Closed-form expressions of the critical buckling load and postbuckling deflection have been derived. It is found that both effects of bending-extension coupling and transverse shear deformation will reduce the equivalent bending rigidity and buckling load and increase the postbuckling deformation. These solutions are used to study the behavior of a thin-film strip delamination in a base laminate. The analytic form of energy release rate is obtained by a variational energy principle that shows that the slope of the energy release rate with load parameter will be decreased due to effects of both bending-extension coupling and transverse shear deformation.
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页码:163 / 169
页数:7
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