Parameter-Varying Aerodynamics Models for Aggressive Pitching-Response Prediction
Author:
Affiliation:
1. University of Minnesota, Minneapolis, Minnesota 55455
2. Princeton University, Princeton, New Jersey 08544
Funder
Air Force Office of Scientific Research
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/am-pdf/10.2514/1.J055193
Reference35 articles.
1. Über die Entstehung des dynamischen Auftriebes von Tragflügeln
2. TheodorsenT. “General Theory of Aerodynamic Instability and the Mechanism of Flutter,” NACA TR 496, 1935.
3. GarrickI. E. “Propulsion of a Flapping and Oscillating Airfoil,” NACA TR 567, 1937.
4. Airfoil Theory for Non-Uniform Motion
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