Unsteady shock-induced turbulent separation in Mach 5 cylinder interactions
- 11 January 1988
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 9 references indexed in Scilit:
- Some new aspects of the shock-wave/boundary-layer interaction in compression-ramp flowsJournal of Fluid Mechanics, 1987
- Supersonic Separated Flow past a Cylindrical Obstacle on a Flat PlateAIAA Journal, 1984
- Simulation of blunt-fin-induced shock wave and turbulent boundary-layer interactionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1984
- Scaling of interactions of cylinders with supersonic turbulent boundary layersAIAA Journal, 1981
- Details of a Shock-Separated Turbulent Boundary Layer at a Compression CornerAIAA Journal, 1976
- Surface pressure fluctuations in hypersonic turbulent boundary layersPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1973
- Wall-pressure fluctuations associated with subsonic turbulent boundary layer flowJournal of Fluid Mechanics, 1967
- Resolution of Pressure in TurbulenceThe Journal of the Acoustical Society of America, 1963
- Measurements of the fluctuating pressure at the wall beneath a thick turbulent boundary layerJournal of Fluid Mechanics, 1962