Prediction of separated transonic wing flows with nonequilibrium algebraic turbulence model
- 1 August 1990
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 28 (8) , 1426-1431
- https://doi.org/10.2514/3.25234
Abstract
No abstract availableKeywords
This publication has 11 references indexed in Scilit:
- Development of an efficient multigrid code for 3-D Navier-Stokes equationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- Navier-Stokes solutions for transonic flow over a wing mounted in a tunnelPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1988
- Validation of a multigrid method for the Reynolds averaged equationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1988
- Extension of the Johnson-King turbulence model to the 3-D flowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1988
- Artificial dissipation and central difference schemes for the Euler and Navier-Stokes equationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Accurate numerical solutions for transonic viscous flow over finite wingsJournal of Aircraft, 1987
- Numerical simulation of viscous transonic airfoil flowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- A mathematically simple turbulence closure model for attached and separated turbulent boundary layersAIAA Journal, 1985
- Predictions of transonic separated flow with an eddy-viscosity/Reynolds-shear-stress closure modelPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- Numerical solution of the Euler equations by finite volume methods using Runge Kutta time stepping schemesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981