Abstract
A simple theory for bending of composite anisotropic plates that are laminated symmetrically about their mid-plane is presented. This theory incorporates transverse shear deformation and transverse normal stress as well as the higher-order effects and fulfills the static conditions on the external boundary planes. Further on, by using Lévy-type solutions considered in conjunction with the state space concept, the state of stress and displacement of rectangular plates for a variety of edge conditions is determined and the results are compared to their first-order shear deformation and classical counterparts, obtained by using the same state-space technique. © 1988.
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CITATION STYLE
Librescu, L., & Khdeir, A. A. (1988). Analysis of symm{approaches the limit}tric cross-ply laminated elastic plates using a higher-order theory: Part I-Stress and displacement. Composite Structures, 9(3), 189–213. https://doi.org/10.1016/0263-8223(88)90014-1
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