A k-epsilon near-wall formulation for separated flows
- 18 June 1990
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Turbulence structure in a shock wave/turbulent boundary-layer interactionAIAA Journal, 1989
- Prediction of separated flows with a new backflow turbulence modelAIAA Journal, 1988
- Separated flow treatment with a new turbulence modelAIAA Journal, 1986
- Unsteadiness of the Separation Shock Wave Structure in a Supersonic Compression Ramp FlowfieldAIAA Journal, 1983
- Detailed Study of Attached and Separated Compression Corner Flowfields in High Reynolds Number Supersonic FlowAIAA Journal, 1979