Parametric Evaluation of Thin, Transonic Circulation-Control Airfoils
Author:
Affiliation:
1. NASA Langley Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2007-272
Reference35 articles.
1. 3Englar, R. J.; Williams, R. M.: Test Techniques for High Lift, Two-Dimensional Airfoils with Boundary Layer and CirculationControl for Application to Rotary Aircraft. Naval ShipResearchand Development Center, Report 4645,July 1975.
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