Lift-enhancing tabs on multielement airfoils
Author:
Affiliation:
1. NASA Ames Research Center, Moffett Field, California 94035-1000
2. Sterling Software, Moffett Field, California 94035-1000
3. Ford Motor Company, Dearborn, Michigan 48121-2053
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.46769
Reference21 articles.
1. Design of Subsonic Airfoils for High Lift
2. Application of Divergent Trailing-Edge Airfoil Technology to the Design of a Derivative Wing
3. Computational evaluation of an airfoil with a Gurney flap
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