Unsteady Airfoil with Dynamic Leading- and Trailing-Edge Flaps
Author:
Affiliation:
1. McGill University, Montreal, Quebec H3A 2K6, Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.42431
Reference14 articles.
1. Experimental Active Control of a Typical Section Using a Trailing-Edge Flap
2. Experimental measurements of dynamic control surface effectiveness
3. Active-Passive Hybrid Optimization of Rotor Blades with Trailing Edge Flaps
4. Aerodynamic Loads on Airfoil with Trailing-Edge Flap Pitching with Different Frequencies
5. Dynamic Stall Flow Control via a Trailing-Edge Flap
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