Unsteady Aerodynamic Modeling of Aircraft Control Surfaces by Indicial Response Methods
Author:
Affiliation:
1. High Performance Computing Research Center, U.S. Air Force Academy, Colorado 80840
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J052946
Reference43 articles.
1. Dynamic leading-edge flap scheduling
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4. Numerical Simulation of Maneuvering Aircraft by Aerodynamic, Flight Mechanics and Structural Mechanics Coupling
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