Iris Publishers - Global Journal of Engineering Sciences (GJES)
Effect of Lamination Scheme on Buckling Load for Laminated Composite Decks Plates
Authorized by Osama Mohammed Elmardi Suleiman
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.
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