Application of Lattice Boltzmann Method to Simulation of Compressible Turbulent Flow

被引:13
作者
Zhuo, Congshan [2 ]
Zhong, Chengwen [2 ,3 ]
Li, Kai [2 ]
Xiong, Shengwei [2 ]
Chen, Xiaopeng [4 ]
Cao, Jun [1 ]
机构
[1] Ryerson Univ, Dept Mech & Ind Engn, Toronto, ON M5B 2K3, Canada
[2] Northwestern Polytech Univ, Natl Key Lab Sci & Technol Aerodynam Design & Res, Xian 710072, Shaanxi, Peoples R China
[3] Northwestern Polytech Univ, Ctr High Performance Comp, Xian 710072, Shaanxi, Peoples R China
[4] Northwestern Polytech Univ, Sch Mech Civil Engn & Architecture, Xian 710072, Shaanxi, Peoples R China
基金
加拿大自然科学与工程研究理事会;
关键词
Lattice Boltzmann method; compressible turbulent flow; airfoil; body-fitted grid; MODEL; EQUATIONS; ALGORITHM; SCHEMES;
D O I
10.4208/cicp.300110.070510a
中图分类号
O4 [物理学];
学科分类号
0702 ;
摘要
The main goal of this paper is to develop the coupled double-distribution-function (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 the Non-Oscillatory and Non-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 the method presented in this study to simulations of both subsonic and transonic turbulent flows.
引用
收藏
页码:1208 / 1223
页数:16
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