Elastic stability of thin-walled cylindrical and conical shells under combined internal pressure and axial compression
Author:
Affiliation:
1. University of Southern California, Los Angeles, Calif.
2. Aerojet-General Corporation, Azusa, Calif.
3. Aerospace Corporation, El Segundo, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.3064
Reference12 articles.
1. Lo, H., Crate, H., and Schwartz, E. B. "Buckling of thinwalled cylinders under axial compression and internal pressure," NACARept. 1027(1951).
2. Buckling of Thin-Walled Circular Cylinders Under Axial Compression and Internal Pressure
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