Evaluation of turbulence models for three primary types of shock-separated boundary layers
- 27 June 1977
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Numerical investigation of turbulence models for shock separated boundary-layer flowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1977
- Numerical Solutions of Supersonic and Hypersonic Laminar Compression Corner FlowsAIAA Journal, 1976
- Computation of Turbulent FlowsAnnual Review of Fluid Mechanics, 1976
- Turbulence stress measurements in a nonadiabatic hypersonic boundarylayerAIAA Journal, 1975
- Incipient separation of a supersonic turbulent boundary layer at moderate to high Reynolds numbersPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- The prediction of laminarization with a two-equation model of turbulenceInternational Journal of Heat and Mass Transfer, 1972