Application of the finite element method to postbuckling analysis of laminated plates
Author:
Affiliation:
1. National Cheng Kung University, Tainan, Taiwan 70101, Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.12850
Reference15 articles.
1. Stein, M. "The Phenomenon of Change in Buckle Pattern in Elastic Structures," NASA TR R-39,1959.
2. 2Stein, M. "Loads and Deformations of Buckled Rectangular Plates," NASA TRR-40,1959.
3. Postbuckling Behavior of Rectangular Plates With Small Initial Curvature Loaded in Edge Compression
4. Post-Buckling of Rectangular Plates with Various Boundary Conditions
5. Postbuckling of orthotropic composite plates loaded in compression
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