Sahin, OS2020-03-262020-03-2620050266-3538https://dx.doi.org/10.1016/j.compscitech.2005.03.007https://hdl.handle.net/20.500.12395/19941In this paper, thermal buckling analysis of symmetric and antisymmetric laminated hybrid composite plates with a hole subjected to a uniform temperature rise for different boundary conditions is presented. The first-order shear deformation theory in conjunction with variational energy method is employed in mathematical formulation. The eight-node Lagrangian finite element technique is used for obtaining the thermal buckling temperatures of glass-epoxy/boron-epoxy hybrid laminates. The effects of hole size, layup sequences and boundary conditions on thermal buckling temperatures are investigated. The results are shown in graphical form for various boundary conditions. (c) 2005 Elsevier Ltd. All rights reserved.en10.1016/j.compscitech.2005.03.007info:eu-repo/semantics/openAccesshybrid composite platesthermal bucklingfinite element methodArticle6511.12.202017801790Q1WOS:000231046700018Q1