A Navier-Stokes investigation of a circulation control airfoil
- 14 January 1985
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Boundary conditions for subsonic compressible Navier-Stokes calculationsComputers & Fluids, 1981
- Thin-layer approximation and algebraic model for separated turbulentflowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- Two-Dimensional Subsonic Wind Tunnel Evaluation of a 20-Percent-Thick Circulation Control AirfoilPublished by Defense Technical Information Center (DTIC) ,1975
- Two Dimensional Subsonic Wind Tunnel Tests on a 20 Percent Thick, 5 Percent Cambered Circulation Control AirfoilPublished by Defense Technical Information Center (DTIC) ,1970