Interaction strength and model geometry effects on the structure of crossing-shock wave/turbulent boundary-layer interactions
- 11 January 1993
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 9 references indexed in Scilit:
- Hypersonic crossing shock-wave/turbulent-boundary-layer interactionsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1993
- Physical model of the swept shock wave/boundary-layer interaction flowfieldAIAA Journal, 1992
- Shock Wave Reflection PhenomenaPublished by Springer Nature ,1992
- 3-D Navier-Stokes analysis of crossing, glancing shocks/turbulent boundary layer interactionsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1991
- Mach number effects on conical surface features of swept shock-wave/boundary-layer interactionsAIAA Journal, 1990
- Glancing interactions between single and intersecting oblique shock waves and a turbulent boundary layerJournal of Fluid Mechanics, 1986
- Regular and Mach Reflection of Shock WavesAnnual Review of Fluid Mechanics, 1986
- Topology of Three-Dimensional Separated FlowsAnnual Review of Fluid Mechanics, 1982
- Detailed Study of Attached and Separated Compression Corner Flowfields in High Reynolds Number Supersonic FlowAIAA Journal, 1979