Post-buckling analysis of stiffened laminated panel

被引:0
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作者
Sheinman, Izhak [1 ]
Frostig, Yeoshua [1 ]
机构
[1] Technion-Israel Inst of Technology, Israel
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Mathematical Techniques--Eigenvalues and Eigenfunctions - Stresses--Analysis;
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摘要
An analytical-numerical procedure is applied to investigate the post-buckling behavior of a composite laminated stiffened panel. The panel is modeled by plate elements for which the nonlinear equations are derived (via a variational principle) in terms of the lateral displacement and Airy stress function and treated by resolving the variables into eigenfunctions in conjunction with a finite-difference scheme.
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页码:635 / 640
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