POSTBUCKLING BEHAVIOR OF PRESSURE- OR CORE-STABILIZED CYLINDERS UNDER AXIAL COMPRESSION
Author:
Affiliation:
1. Lockheed Missiles & Space Company, Palo Alto, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.2063
Reference11 articles.
1. Postbuckling Behavior of Axially Compressed Circular Cylindrical Shells
2. The Stability Under Axial Compression and Lateral Pressure of Circular-Cylindrical Shells With a Soft Elastic Core
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3. Elastic buckling of cylindrical shells with elastic cores—II. Experiments;International Journal of Solids and Structures;1995-04
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