Buckling of orthogonally stiffened finite oval cylindrical shells under axial compression
Author:
Affiliation:
1. Grumman Aerospace Corp., Bethpage, N. Y.
2. American Bureau of Shipping, New York, N. Y.
3. Polytechnic Institute of New York, Brooklyn, N. Y.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference26 articles.
1. Influence of edge conditions on the stability of axially compressed cylindrical shells.
2. INFLUENCE OF IMPERFECTIONS AND EDGE RESTRAINT ON THE BUCKLING OF AXIALLY COMPRESSED CYLINDERS
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