作者: Ahmet Avci , Ömer Sinan Sahin , Mesut Uyaner
DOI: 10.1016/J.COMPSTRUCT.2004.03.017
关键词: Buckling 、 Calculus of variations 、 Finite element method 、 Composite material 、 Composite number 、 Antisymmetric relation 、 Lagrange polynomial 、 Thermal buckling 、 Materials science 、 Boundary value problem 、 Geometry
摘要: Thermal buckling analysis of symmetric and antisymmetric cross-ply laminated hybrid composite plates with a hole subjected to uniform temperature rise for different boundary conditions are presented in this paper. The first-order shear deformation theory conjunction variational energy method is employed the mathematical formulation. eight-node Lagrangian finite element technique used finding thermal temperatures laminates. effects size, lay-up sequences on investigated. results shown graphical form various conditions.