Stability of Rectangular Plates in Subsonic Flow with Various Boundary Conditions
Author:
Affiliation:
1. Department of Mechanical Engineering and Material Science, Duke University, Durham, North Carolina 27708
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C032738
Reference34 articles.
1. Aeroelastic Model of Multisegmented Folding Wings: Theory and Experiment
2. Nonlinear aeroelastic analysis of aircraft with high-aspect-ratio wings
3. Static and dynamic instability of panels and cylindrical shells in subsonic potential flow
4. Flutter of an elastic plate in a channel flow: Confinement and finite-size effects
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