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Effect of Lamination Scheme on Buckling Load for Laminated Composite Decks Plates
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New numerical results are generated for in-plane compressive biaxial buckling which serve to quantify the effects of lamination scheme on buckling loading. The results indicate that the symmetric laminate is stiffer than the anti-symmetric one. This phenomenon is caused by coupling between bending and stretching which lowers the buckling loads of symmetric laminate.
Keywords
Biaxial Buckling, Classical Laminated Plate Theory, Composite Laminated Decks Plates, Finite Element, Fortran Program, Lamination Scheme.
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