Analysis of circulation control airfoils using an implicit Navier-Stokes solver
Author:
Affiliation:
1. Lockheed-Georgia Co., Advanced Flight Sciences Dept., Marietta, GA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1985-171
Reference31 articles.
1. A Calculation Method for Circulation Control by Tangential Blowing Around a Bluff Trailing Edge
2. Two Dimensional Subsonic Wind Tunnel Tests on a 20 Percent Thick, 5 Percent Cambered Circulation Control Airfoil
3. Englar, Robert J. "Two-Dimensional Transonic Wind Tunnel Tests of Three 15-percent Thick-Circulation Control Airfoils", NSRDC Report BED-182, December 1970.
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