Algebraic turbulence models for the computation of two‐dimensional high‐speed flows using unstructured grids
- 1 September 1989
- journal article
- research article
- Published by Wiley in International Journal for Numerical Methods in Fluids
- Vol. 9 (9) , 1121-1143
- https://doi.org/10.1002/fld.1650090907
Abstract
The incorporation of algebraic turbulence models in a solver for the 2D compressible Navier–Stokes equations using triangular grids is described. A practical way to use the Cebeci–Smith model and to modify it in separated regions is proposed. The ability of the model to predict high‐speed perfect‐gas boundary layers is investigated from a numerical point of view.Keywords
This publication has 12 references indexed in Scilit:
- On nonlinear K-l and K-ε models of turbulenceJournal of Fluid Mechanics, 1987
- Hypersonic flow past 3-D configurationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Numerical simulation of 3-D hypersonic Euler flows around space vehicles using adapted finite elementsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Separated flow treatment with a new turbulence modelAIAA Journal, 1986
- Calculation of a class of two-dimensional turbulent boundary layer flows using the Baldwin-Lomax modelPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- The Baldwin-Lomax Turbulence Model for Two-Dimensional Shock-Wave/Boundary-Layer InteractionsAIAA Journal, 1984
- Upwind difference schemes for hyperbolic systems of conservation lawsMathematics of Computation, 1982
- Numerical Solution for Supersonic Turbulent Flow over a Compression RampAIAA Journal, 1975
- A modified wall wake velocity profile for turbulent compressible boundary layers.Journal of Aircraft, 1973
- Hypersonic Turbulent Skin-Friction and Boundary-Layer Profiles on Nonadiabatic Flat PlatesAIAA Journal, 1972