Buckling of a Finite-Length Cylindrical Shell Under a Circumferential Band of Pressure
Author:
Affiliation:
1. Lockheed Missiles and Space Division,
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Link
http://arc.aiaa.org/doi/pdf/10.2514/8.9077
Reference12 articles.
1. Ae 451;Glauert H.,1930
2. The Shape and Tension of a Light Flexible Cable in a Uniform Current
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