Separation control over an airfoil at high angles of attack by soundemanating from the surface
- 8 June 1987
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Active control of laminar-turbulent transitionJournal of Fluid Mechanics, 1982
- A discrete vortex method for the non-steady separated flow over an airfoilJournal of Fluid Mechanics, 1981
- Behavior of Vortex Wakes from Oscillating AirfoilsJournal of Aircraft, 1978