Spatial and temporal features of a separated flow field at a convex wall induced by normal shock wave turbulent boundary layer interaction
- 18 June 1990
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Reynolds number effect on separation structures at normal shock wave/turbulent boundary-layer interactionAIAA Journal, 1989
- An experimental investigation of the Mach number effect upon a normal shock wave ? Tubulent boundary layer interaction on a curved wallActa Mechanica, 1989
- Mach number dependence of flow separation induced by normal shock-wave/turbulent boundary-layer interaction at a curved wallPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- Three-dimensional vortex structures and vorticity topologyFluid Dynamics Research, 1988