Effect of Gurney flaps on a NACA 0011 airfoil
Author:
Affiliation:
1. Wichita State Univ., KS
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1996-59
Reference7 articles.
1. Design of Subsonic Airfoils for High Lift
2. Lift enhancement of an airfoil using a Gurney flap and vortex generators
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