Onal, Gurol2020-03-262020-03-2620060731-6844https://dx.doi.org/10.1177/0731684406066750https://hdl.handle.net/20.500.12395/20576Buckling analysis of symmetric and antisymmetric cross-ply laminated hybrid composite plates with an inclined crack subjected to a uniform compression is investigated in this article. The first-order shear deformation theory in conjunction with the variational energy method is employed in the mathematical formulation. The effects of crack size, crack inclination angle, and lay-up sequences on the buckling loads are investigated. The results are shown in graphical form for various conditions.en10.1177/0731684406066750info:eu-repo/semantics/closedAccesshybrid composite platesbucklingfinite element methodArticle251415351544Q1WOS:000240832900008Q3