Large-Amplitude Finite Element Flutter Analysis of Composite Panels in Hypersonic Flow
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia 23681
2. Old Dominion University, Norfolk, Virginia 23529
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.49051
Reference33 articles.
1. Theoretical considerations of panel flutter at high supersonic Mach numbers.
2. Panel flutter - A review of the aeroelastic stability of plates and shells
3. FLUTTER ANALYSIS OF FLAT RECTANGULAR PANELS BASED ON THREE-DIMENSIONAL SUPERSONIC POTENTIAL FLOW
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