Computational Investigation of the Effects of Gurney Flap on the Aerodynamic Performance of VR-12 Airfoil
Author:
Affiliation:
1. Georgia Institute of Technology
2. U.S. Army Research and Development Engineering Command
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2005-4960
Reference20 articles.
1. A Computational Study of an Oscillating VR-12 Airfoil with a Gurney Flap
2. Lecture Notes for the Von Karman Institute for FluidDynamics Lecture Series, Belgium, January20-24,1986;Pulliam T. H.
3. Approximate Riemann solvers, parameter vectors, and difference schemes
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