Effect of Lamination Scheme on Buckling Load for Laminated Composite Decks Plates


(osama mohammed elmardi suleiman khayal) #1

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.IJEART0502001.pdf (737.5% u)