Hypersonic flutter of a curved shallow panel with aerodynamic heating
Author:
Affiliation:
1. California Univ., Los Angeles
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1993-1318
Reference28 articles.
1. Heeg, J., Gilbert. M.G. and Pototzky, A. "Active Control of Aerothermoelastic Effects for a Conceptual HypersonicAircraft,"NASATM102'113, August 1990.
2. Piston Theory-A New Aerodynamic Tool for the Aeroelastician
3. Oscillating Airfoils at High Mach Number
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