Analysis of circulation control airfoils using an implicit Navier-Stokes solver
- 14 January 1985
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 14 references indexed in Scilit:
- Analysis of circulation-controlled airfoils in transonic flowJournal of Aircraft, 1983
- High-speed characteristics of circulation control airfoilsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- Numerical simulation of transonic flow about isolated afterbodiesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- Circulation controlled STOL wing optimizationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- Reynolds number and compressibility effects on dynamic stall of a NACA 0012 airfoilPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980
- Investigation into and application of the high velocity circulation control wall jet for high lift and drag generation on STOL aircraftPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1974
- Two-Dimensional Transonic Wind Tunnel Tests of Three 15-Percent Thick Circulation Control AirfoilsPublished by Defense Technical Information Center (DTIC) ,1970
- Two Dimensional Subsonic Wind Tunnel Tests on a 20 Percent Thick, 5 Percent Cambered Circulation Control AirfoilPublished by Defense Technical Information Center (DTIC) ,1970
- A Calculation Method for Circulation Control by Tangential Blowing Around a Bluff Trailing EdgeAeronautical Quarterly, 1968
- A general formulation of alternating direction methodsNumerische Mathematik, 1964