Development of a three-dimensional viscous aeroelastic solver for nonlinear panel flutter
Author:
Affiliation:
1. USAF, Research Lab., Wright-Patterson AFB, OH
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2000-2337
Reference27 articles.
1. Nonlinear oscillations of a fluttering plate
2. Nonlinear oscillations of a fluttering plate. II.
3. Panel flutter - A review of the aeroelastic stability of plates and shells
4. Nonlinear Flutter of Composite Panels Under Yawed Supersonic Flow Using Finite Elements
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