Buckling of stiffened two-layered shells of revolution with a circumferentially cracked unbonded layer.
Author:
Affiliation:
1. The Aerospace Corporation, San Bernardino, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.5424
Reference7 articles.
1. Buckling of circular cylindrical shells with multiple orthotropic layers and eccentric stiffeners.
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