Tip-Vortex Dynamics of a Pitching Rotor Blade-Tip Model
Author:
Affiliation:
1. DLR, German Aerospace Center, 37073 Goettingen, Germany
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J054656
Reference28 articles.
1. TheodorsenT. “General Theory of Aerodynamic Instability and the Mechanism of Flutter,” NACA Rept. 496, 1935.
2. Dynamic Stall Experiments on Oscillating Airfoils
3. McCroskeyW. J. “The Phenomenon of Dynamic Stall,” NASA TM 81264, March 1981.
4. Near Field of the Tip Vortex Behind an Oscillating Rectangular Wing
5. Measurements in the Tip Vortex Roll-Up Region of an Oscillating Wing
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