Avci, ASahin, OSUyaner, M2020-03-262020-03-2620050263-82231879-1085https://dx.doi.org/10.1016/j.compstruct.2004.03.017https://hdl.handle.net/20.500.12395/19942Thermal buckling analysis of symmetric and antisymmetric cross-ply laminated hybrid composite plates with a hole subjected to a uniform temperature rise for different boundary conditions are presented in this paper. The first-order shear deformation theory in conjunction with variational energy method is employed in the mathematical formulation. The eight-node Lagrangian finite element technique is used for finding the thermal buckling temperatures of hybrid laminates. The effects of hole size, lay-up sequences and boundary conditions on the thermal buckling temperatures are investigated. The results are shown in graphical form for various conditions. (c) 2004 Published by Elsevier Ltd.en10.1016/j.compstruct.2004.03.017info:eu-repo/semantics/openAccesshybrid composite platesthermal bucklingfinite element methodArticle682247254Q1WOS:000227692900012Q2