Optimum buckling design of composite sti
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Wei Wang; S. Guo; Nan Chang; Wei Yang
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Article
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2010
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Elsevier Science
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English
โ 652 KB
Optimal design of laminated composite stiffened panels of symmetric and balanced layup with different number of T-shape stiffeners is investigated and presented. The stiffened panels are simply supported and subjected to uniform biaxial compressive load. In the optimization for the maximum buckling