Aerodynamic Characteristics of Airfoil with Perforated Gurney-Type Flaps
Author:
Affiliation:
1. McGill University, Montreal, Quebec H3A 2K6, Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.38474
Reference18 articles.
1. Design of Subsonic Airfoils for High Lift
2. Lift enhancement of an airfoil using a Gurney flap and vortex generators
3. Gurney Flap Experiments on Airfoils, Wings, and Reflection Plane Model
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