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A geometrically nonlinear theory of transversely isotropic laminated composite plates and its use in the post-buckling analysis
AbstractA higher-order, geometrically nonlinear theory of transversely isotropic symmetrically laminated composite plates is formulated and their post-buckling behavior is analysed. The numerical illustrations emphasize the role played by transverse shear deformation, transverse normal stress, higher-order effects and the character of in-plane boundary conditions. The results obtained within the present higher-order theory are compared with those of first-order transverse shear deformation and classical (Kirchhoff) theory, and conclusions on their range of applicability and the influence of various parameters are outlined.
A geometrically nonlinear theory of transversely isotropic laminated composite plates and its use in the post-buckling analysis
AbstractA higher-order, geometrically nonlinear theory of transversely isotropic symmetrically laminated composite plates is formulated and their post-buckling behavior is analysed. The numerical illustrations emphasize the role played by transverse shear deformation, transverse normal stress, higher-order effects and the character of in-plane boundary conditions. The results obtained within the present higher-order theory are compared with those of first-order transverse shear deformation and classical (Kirchhoff) theory, and conclusions on their range of applicability and the influence of various parameters are outlined.
A geometrically nonlinear theory of transversely isotropic laminated composite plates and its use in the post-buckling analysis
Librescu, L. (Autor:in) / Stein, M. (Autor:in)
Thin-Walled Structures ; 11 ; 177-201
01.01.1990
25 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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