Computational Modeling of Variable-Droop Leading Edge in Forward Flight
Author:
Affiliation:
1. Georgia Institute of Technology, Atlanta, Georgia 30332-0150
2. Washington University, St. Louis, Missouri 63130
3. Advanced Rotorcraft Technology, Inc., Mountain View, California 94035
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.39174
Reference33 articles.
1. Effect of Compressibility on Suppression of Dynamic Stall Using a Slotted Airfoil
2. Dynamic stall control for advanced rotorcraft application
3. Compressible Dynamic Stall Performance of a Variable Droop Leading Edge Airfoil with a Gurney Flap
4. Computational Investigation of the Effects of Gurney Flap on the Aerodynamic Performance of VR-12 Airfoil
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