Application of Circulation Control to Advanced Subsonic Transport Aircraft, Part I - Airfoil Development
- 1 September 1994
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 31 (5) , 1160-1168
- https://doi.org/10.2514/3.56907
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
- Dynamic stall of circulation control airfoilsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1990
- Navier-Stokes Computations for Circulation Controlled AirfoilsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- A Navier-Stokes investigation of a circulation control airfoilPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- Numerical solution of unsteady viscous flow past rotor sectionsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- Analysis of circulation-controlled airfoils in transonic flowJournal of Aircraft, 1983
- Flight testing the circulation control wingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- Analysis Method for Viscous Flow over Circulation-Controlled AirfoilsJournal of Aircraft, 1979
- Two Dimensional Subsonic Wind Tunnel Tests on a 20 Percent Thick, 5 Percent Cambered Circulation Control AirfoilPublished by Defense Technical Information Center (DTIC) ,1970