Further studies of harmonic gradient method for supersonic aeroelastic applications
Author:
Affiliation:
1. Arizona State University, Tempe, Arizona 85287
2. Zona Technology, Inc., Mesa, Arizona 85202
3. Lockheed Engineering & Sciences Company, Hampton, Virginia 23666
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.46070
Reference32 articles.
1. Supersonic aeroelastic applications of harmonic potential panel method to oscillating flexible bodies
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