Lift enhancement of an airfoil using a Gurney flap and vortex generators
Author:
Affiliation:
1. Sterling Software, Inc.; NASA, Ames Research Center, Moffett Field, CA
2. California Polytechnic State Univ., San Luis Obispo
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1993-647
Reference13 articles.
1. Design of Subsonic Airfoils for High Lift
2. Rocsch, Philippe, and Vuillet, Alain, "New Designs for Improved Aerodynamic Stability on Recent Aerospatiale Helicopters," m,Vol.6,1982,pp.145-164.
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