Transonic-Aerodynamic-Influence-Coefficient Approach for Aeroelastic and MDO Applications
Author:
Affiliation:
1. ZONA Technology,Inc., Scottsdale, Arizona 85251
2. Arizona State University, Tempe, Arizona 85287
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.2565
Reference28 articles.
1. A harmonic gradient method for unsteady supersonic flow calculations
2. Unsteady supersonic computations of arbitrary wing-body configurations including external stores
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