Postbuckling behavior of orthotropic cylinders under axial compression
Author:
Affiliation:
1. Lockheed Missiles and Space Company, Palo Alto, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.2667
Reference6 articles.
1. POSTBUCKLING BEHAVIOR OF AXIALLY COMPRESSED CIRCULAR CYLINDERS
2. Becker, H., Gerard, G. and Winter, R. "Experiments on axial compressive instability of monolithic circumferentially stiffened circular cylindrical shells," New York Univ. TR SM62-5(1962).
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