Variable-Kinematics Approach for Linearized Buckling Analysis of Laminated Plates and Shells
Author:
Affiliation:
1. Université Paris Ouest, 92410 Ville d’Avray, France
2. Politecnico di Torino, 10129 Torino, Italy
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J050203
Reference55 articles.
1. Buckling
2. Computerized buckling analysis of shells
3. First-order second-moment analysis of the buckling of shells with random imperfections
4. Rigorous buckling of laminated cylindrical shells
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