Abstract
The main goal of this paper is to develop the coupled double- distributionfunction (DDF) lattice Boltzmann method (LBM) for simulation of subsonic and transonic turbulent flows. In the present study, we adopt the second-order implicit-explicit (IMEX) Runge-Kutta schemes for time discretization and theNon-Oscillatory andNon- Free-Parameters Dissipative (NND) finite difference scheme for space discretization. The Sutherland's law is used for expressing the viscosity of the fluid due to considerable temperature change. Also, the Spalart-Allmaras (SA) turbulence model is incorporated in order for the turbulent flow effect to be pronounced. Numerical experiments are performed on different turbulent compressible flows around a NACA0012 airfoil with body-fitted grid. Our numerical results are found to be in good agreement with experiment data and/or other numerical solutions, demonstrating the applicability of themethod presented in this study to simulations of both subsonic and transonic turbulent flows.
Original language | English |
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Pages (from-to) | 1208-1223 |
Number of pages | 16 |
Journal | Communications in Computational Physics |
Volume | 8 |
Issue number | 5 |
DOIs | |
State | Published - Nov 2010 |
Keywords
- Airfoil
- Body-fitted grid
- Compressible turbulent flow
- Lattice Boltzmann method