Aeroelastic stability characteristics of cylindrical shells considering imperfections and edge constraint.
Author:
Affiliation:
1. Sandia Corporation, Albuquerque, N. Mex.
2. University of Texas, Austin, Texas
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.5244
Reference28 articles.
1. Some aspects of cylindrical shell panel flutter.
2. INFLUENCE OF IMPERFECTIONS AND EDGE RESTRAINT ON THE BUCKLING OF AXIALLY COMPRESSED CYLINDERS
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