Vibration of compressively loaded shear deformable flat panels exhibiting initial geometric imperfections
- 1 November 1992
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 30 (11), 2793-2795
- https://doi.org/10.2514/3.11305
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Layup optimization against buckling of shear panelsStructural and Multidisciplinary Optimization, 1991
- Stiffness Optimization of Orthotropic Laminated Composites Using Lamination ParametersAIAA Journal, 1991
- Postbuckling Analysis of Shear Deformable Composite Flat Panels Taking Into Account Geometrical ImperfectionsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1990
- Non-linear free vibration analysis of composite plates with initial imperfections and in-plane loadingInternational Journal of Solids and Structures, 1989