Navier-Stokes computational study of axisymmetric transonic turbulent flows with a two-equation model of turbulence
Abstract
A thin-layer Navier-Stokes code has been used to compute the turbulent flow over two axisymmetric bodies at transonic speeds and the results are compared to experiment. A critical element of calculating such flows is the turbulence model. Numerical computations have been made with an algebraic eddy viscosity model and the k-epsilon two-equation model. The k-epsilon equations are developed in a general spatial coordinate system and incorporated into the thin-layer, compressible, time dependent Navier-Stokes code. The same implicit algorithm that simultaneously solves the Reynolds-averaged mean flow equations is extended to solve the turbulence field equations using block tridiagonal matrix inversions. Calculations with the k-epsilon model are extended up to the wall and exact values of k and epsilon at the wall are used as boundary conditions.
- Publication:
-
NASA STI/Recon Technical Report N
- Pub Date:
- February 1985
- Bibcode:
- 1985STIN...8528265S
- Keywords:
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- Axisymmetric Flow;
- Mathematical Models;
- Navier-Stokes Equation;
- Transonic Flow;
- Turbulence Models;
- Turbulent Boundary Layer;
- Turbulent Flow;
- Equations Of Motion;
- Finite Difference Theory;
- K-Epsilon Turbulence Model;
- Kinetic Energy;
- Shear Stress;
- Shock Waves;
- Thermal Conductivity;
- Fluid Mechanics and Heat Transfer