Effect of Transverse Shear Deformation on Anisotropic Plate Buckling
- 1 July 1982
- journal article
- research article
- Published by SAGE Publications in Journal of Composite Materials
- Vol. 16 (4) , 301-312
- https://doi.org/10.1177/002199838201600404
Abstract
Critical in-plane normal and shear loads of rectangular anisotropic laminated plates are presented. These were calculated using the shell code FASOR, which includes the effect of transverse shear deformation. For simply-supported orthotropic laminates with midplane symmetry normal buckling loads are verified by a closed-form solution derived from transverse shear deformation plate theory. Results are compared to previously pub lished solutions from three-dimensional elasticity theory and classical plate theory.Keywords
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