Vibration and Buckling of Cross-Ply Laminated Circular Cylindrical Panels
- 1 August 1975
- journal article
- research article
- Published by Cambridge University Press (CUP) in Aeronautical Quarterly
- Vol. 26 (3) , 211-218
- https://doi.org/10.1017/s0001925900007356
Abstract
Summary: The paper deals with the free transverse vibration and stability analysis of circular cylindrical composite panels. The panels are assumed to be composed of an arbitrary sequence of 0° and 90° layers. The non-dimensional vibration and buckling parameters are computed for simply-supported panels consisting of antisymmetric crossply graphite-epoxy laminates. The influence of the coupling between bending and extension, shear deformation, the panel curvature, and the aspect ratio are then discussed.Keywords
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