Effects of boundary conditions on postbuckling of compressed, symmetrically laminated thick plates
Author:
Affiliation:
1. Politecnico di Torino, 10129 Torino, Italy
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.12587
Reference16 articles.
1. Postbuckling behavior of selected flat stiffened graphite-epoxy panels loaded in compression
2. An experimental study on laminated panels in compression
3. Geometrically Nonlinear Behavior of Composite Plates: A Review
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