Post-buckling analysis of imperfect laminated plates under combined axial and thermal loads
A post-buckling analysis of composite laminated plates subjected to combined axial compression and uniform temperature loading is presented. The initial geometrical imperfection of the plates is taken into account. The analysis uses perturbation technique to determine buckling loads and post-buckling equilibrium paths. Numerical examples are presented that relate to antisymmetrically angle-ply and symmetrically cross-ply laminated plates.
antisymmetrically angle-ply and symmetrically cross-ply laminated plates
scientific article; zbMATH DE number 859429