Flutter analysis of stiffened laminated composite plates and shells in supersonic flow
Author:
Affiliation:
1. National Taiwan Institute of Technology, Taipei, 107 Taiwan, Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.11865
Reference23 articles.
1. Panel flutter - A review of the aeroelastic stability of plates and shells
2. Finite elements applied to panel flutter.
3. Some flutter solutions using finite elements
4. Flutter of clamped skew panels in supersonic flow
5. Finite element analysis of Supersonic panel flutter
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