Control of shock-wave/boundary-layer interactions with passive blowing and bleeding
- 6 July 1997
- conference paper
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 18 references indexed in Scilit:
- Experimental investigation of blowing for controlling oblique shock/boundary layer interactionsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1997
- Shock-wave/boundary-layer interactions with bleed through rows of holesJournal of Propulsion and Power, 1996
- Flowfield measurements in a normal-hole-bled oblique shock-wave and turbulent boundary-layer interactionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1995
- Flow coefficient behavior for boundary layer bleed holes and slotsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1995
- Effect of bleed configuration on shock/laminar boundary-layer interactionsJournal of Propulsion and Power, 1995
- Three-dimensional shock-wave/boundary-layer interactions with bleedAIAA Journal, 1993
- Modeling supersonic inlet boundary-layer bleed roughnessJournal of Propulsion and Power, 1993
- Numerical study of shock-wave/boundary-layer interactions with bleedAIAA Journal, 1993
- Passive control of shock-boundary layer interactionProgress in Aerospace Sciences, 1988
- Shock wave/turbulent boundary layer interaction and its controlProgress in Aerospace Sciences, 1985