Buckling of rectangular symmetric angle-ply laminated plates determined by eigensensitivity analysis
Author:
Affiliation:
1. U.S. Naval Academy, Annapolis, Maryland 21402
2. Howard University, Washington, D.C. 20056
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.12876
Reference16 articles.
1. THERMAL BUCKLING OF THICK ANTISYMMETRIC ANGLE-PLY LAMINATES
2. Buckling of Anisotropic Composite Plates under Stress Gradient
3. Buckling Analysis of Anisotropic Plates Using Perturbation Technique
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