Lift Enhancement by Static Extended Trailing Edge
Author:
Affiliation:
1. Western Michigan University, Kalamazoo, Michigan 49008
2. NASA Langley Research Center, Hampton, Virginia 23681
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.31995
Reference23 articles.
1. Design of Subsonic Airfoils for High Lift
2. Lift enhancement of an airfoil using a Gurney flap and vortex generators
3. Lift-enhancing tabs on multielement airfoils
4. Gurney Flap Experiments on Airfoils, Wings, and Reflection Plane Model
5. Numerical investigation of an airfoil with a Gurney flap
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