Initial and post buckling of axially compressed orthotropic cylindrical shells
Author:
Affiliation:
1. University College, London, England
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference12 articles.
1. A branching solution for the local buckling of a circumferentially cracked cylindrical shell
2. 3Koiter, W. T. "Over de Stabiliteit van net Elastisch Evenwicht," Ph.D. Thesis,Delft University, Netherlands, 1945, D.C. 20546, N 67-20533 NACA Translation, Mar. 1967.
3. Localized Diamond-Shaped Buckling Patterns of Axially Compressed Cylindrical Shells
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