Separated flow predictions using a hybrid k-L/backflow model
- 1 June 1990
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 28 (6) , 1005-1009
- https://doi.org/10.2514/3.25157
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
- Prediction of separated flows with a new backflow turbulence modelAIAA Journal, 1988
- Separated flow treatment with a new turbulence modelAIAA Journal, 1986
- The versatility and reliability of Euler solvers based on high-accuracy TVD formulationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- A mathematically simple turbulence closure model for attached and separated turbulent boundary layersAIAA Journal, 1985
- Application of a new class of high accuracy TVD schemes to the Navier-Stokes equationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- 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
- Details of a Shock-Separated Turbulent Boundary Layer at a Compression CornerAIAA Journal, 1976