Simultaneous Excitation of Multiple-Input/Multiple-Output CFD-Based Unsteady Aerodynamic Systems
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia 23681-0001
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.34328
Reference38 articles.
1. Über die Entstehung des dynamischen Auftriebes von Tragflügeln
2. Some Aspects of Non-Stationary Airfoil Theory and Its Practical Application
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