Abstract
New numerical results are generated for in-plane compressive biaxial buckling which serves to quantify the effect of reversing lamination scheme on buckling loading. The buckling loads have been determined for two modulus ratios 40 and 5. It is observed that the buckling loads are completely the same for the given first three modes. Therefore, it can be concluded that the buckling load of laminated plates will remain the same even if the lamination order is reversed. The reason behind this is that the transformed elastic coefficients are equal for both lamination schemes.
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