Method for calculating the unsteady flow of an elliptical circulation-control airfoil
Author:
Affiliation:
1. Beijing Institute of Aeronautics and Astronautics, Beijing, China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.45860
Reference16 articles.
1. ^ind, R. J. "A Proposed Method of Circulation Control/' Ph.D. Thesis,Univ. of Cambridge, UK, June 1967.
2. STOE Potential of the Circulation Control Wing for High-Performance Aircraft
3. Circulation control airfoils as applied to rotary-wing aircraft
4. Analysis Method for Viscous Flow over Circulation-Controlled Airfoils
5. Aerodynamic force calculations of an elliptical circulation control airfoil
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