Shock-boundary layer interaction control with low-profile vortex generators and passive cavity
- 6 January 1992
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Numerical analysis of shock-induced separation alleviation using vortex generatorsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1992
- Passive control of shock-boundary layer interactionProgress in Aerospace Sciences, 1988
- Interactions between shock waves and turbulent boundary layersProgress in Aerospace Sciences, 1970
- Mixing length and kinematic eddy viscosity in a compressible boundary layer.AIAA Journal, 1968