Aerodynamic Performance Analysis of a Gurney Flap for Rotorcraft Application
Author:
Affiliation:
1. Pusan National University, Busan 609-735, Republic of Korea
2. Doosan Heavy Industries and Construction, Daejeon 305-348, Republic of Korea
3. Seoul National University, Seoul 151-742, Republic of Korea
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.26868
Reference24 articles.
1. Design of Subsonic Airfoils for High Lift
2. Computational evaluation of an airfoil with a Gurney flap
3. Lift enhancement of an airfoil using a Gurney flap and vortex generators
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