Unsteady unified hypersonic/supersonic method for aeroelastic applications including wave/shock interaction
Author:
Affiliation:
1. University of Maryland, College Park, Maryland 20742
2. Arizona State University, Tempe, Arizona 85287
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference13 articles.
1. Oscillating Airfoils at High Mach Number
2. On hypersonic similitude
3. Piston Theory-A New Aerodynamic Tool for the Aeroelastician
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