From Piston Theory to a Unified Hypersonic-Supersonic Lifting Surface Method
Author:
Affiliation:
1. Arizona State University, Tempe, Arizona 85287
2. ZONA Technology, Mesa, Arizona 85202
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.2199
Reference26 articles.
1. On hypersonic similitude
2. Oscillating Airfoils at High Mach Number
3. Piston Theory-A New Aerodynamic Tool for the Aeroelastician
4. A harmonic gradient method for unsteady supersonic flow calculations
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