Buckling and vibration of laminated composite plates using various plate theories
Author:
Affiliation:
1. Virginia Polytechnic Institute and State University, Blacksburg, Virginia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.10338
Reference35 articles.
1. Finite-Element Modeling of Layered, Anisotropic Composite Plates and Shells: a Review of Recent Research
2. A Review of the Literature On Finite-Element Modeling of Laminated Composite Plates
3. A comparison of closed-form and finite-element solutions of thick laminated anisotropic rectangular plates
4. A Simple Higher-Order Theory for Laminated Composite Plates
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