Aerodynamic Modification of NACA 0012 Airfoil by Trailing-Edge Plasma Gurney Flap
Author:
Affiliation:
1. Beijing University of Aeronautics and Astronautics, 100191 Beijing, People’s Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.43379
Reference38 articles.
1. Design of Subsonic Airfoils for High Lift
2. Gurney Flap Scaling for Optimum Lift-to-Drag Ratio
3. Aerodynamics of Gurney Flaps on a Single-Element High-Lift Wing
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