Natural vibration and flutter of cylindrically curved panels.
Author:
Affiliation:
1. National Aerospace Laboratory, Chofu, Tokyo, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference3 articles.
1. Influence of the in-plane boundary conditions on the natural frequency of cylindrically curved panels with simply supported edges
2. Nonlinear flutter of curved plates. II
3. Panel flutter - A review of the aeroelastic stability of plates and shells
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