Bifurcation Buckling as an Approximation of the Collapse Load for General Shells
Author:
Affiliation:
1. Lockheed Palo Alto Research Laboratory, Palo Alto, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference6 articles.
1. Collapse analysis for elliptic cones
2. Analysis of buckling and vibration of ring-stiffened, segmented shells of revolution
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