Effect of Aspect Ratio on Gurney-Flap Performance
Author:
Affiliation:
1. Aerospace and Mechanical Engineering Department, Embry Riddle Aeronautical University, Prescott, Arizona 86301
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C032140
Reference15 articles.
1. ZimmermanC. H. “Characteristics of Clark Y Airfoils of Small Aspect Ratios,” NACA TR-431, 1933.
2. Progress in Aeronautics and Astronautics;Torres G. E.,2001
3. Predictions of vortex-lift characteristics by a leading-edge suctionanalogy
4. Aerodynamic Characteristics of a Gurney/Jet Flap at Low Reynolds Numbers
5. Design of Subsonic Airfoils for High Lift
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