Control of the Spanwise Distribution of Circulation on NACA 0012 and Flat Plate Wings
Author:
Affiliation:
1. Illinois Institute of Technology
2. California Institute of Technology
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2007-1121
Reference4 articles.
1. Force production and flow structure of the leading edge vortex on flapping wings at high and low Reynolds numbers
2. Dixon, C.J. "Lift Augmentation by Lateral Blowing Over a Lifting Surface," AIAA Paper 69-193, AIAA/AHSVTOL Research,DesignandOperations Meeting,Atlanta, GA,Feb.1969.
3. Low Aspect Ratio Aerodynamics at Low Reynolds Numbers
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