In this paper a first-order shear deformation laminate theory that accounts for the Green Lagrange strain vector is described and its finite element model is developed. The element is used to study the effects of anisotropy, transverse shear moduli, aspect ratio and boundary conditions on the buckling behaviour under in-plane triangular loading. It is observed that for an angle ply (± θ) thick plate, maximum load occurs at ±15°, whereas for thin plate it occurs at ±30°. It is found that the effects of aspect ratio, boundary conditions and transverse shear are significant on buckling load.
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