Application of Lattice Boltzmann Method to Simulation of Compressible Turbulent Flow

被引:10
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
相关论文
共 43 条
  • [1] LATTICE BOLTZMANN THERMOHYDRODYNAMICS
    ALEXANDER, FJ
    CHEN, S
    STERLING, JD
    [J]. PHYSICAL REVIEW E, 1993, 47 (04) : R2249 - R2252
  • [2] Anderson J.D., 2002, COMPUTATIONAL FLUID
  • [3] Lattice Boltzmann method for fluid flows
    Chen, S
    Doolen, GD
    [J]. ANNUAL REVIEW OF FLUID MECHANICS, 1998, 30 : 329 - 364
  • [4] THERMAL LATTICE BHATNAGAR-GROSS-KROOK MODEL WITHOUT NONLINEAR DEVIATIONS IN MACRODYNAMIC EQUATIONS
    CHEN, Y
    OHASHI, H
    AKIYAMA, M
    [J]. PHYSICAL REVIEW E, 1994, 50 (04): : 2776 - 2783
  • [5] Development and application of Spalart-Allmaras one equation turbulence model to three-dimensional supersonic complex configurations
    Deck, S
    Duveau, P
    d'Espiney, P
    Guillen, P
    [J]. AEROSPACE SCIENCE AND TECHNOLOGY, 2002, 6 (03) : 171 - 183
  • [6] Multiscale lattice Boltzmann schemes with turbulence modeling
    Filippova, O
    Succi, S
    Mazzocco, F
    Arrighetti, C
    Bella, G
    Hänel, D
    [J]. JOURNAL OF COMPUTATIONAL PHYSICS, 2001, 170 (02) : 812 - 829
  • [7] GACHERIEU C, AIAA982737
  • [8] Two-dimensional lattice Boltzmann model for compressible flows with high Mach number
    Gan, Yanbiao
    Xu, Aiguo
    Zhang, Guangcai
    Yu, Xijun
    Li, Yingjun
    [J]. PHYSICA A-STATISTICAL MECHANICS AND ITS APPLICATIONS, 2008, 387 (8-9) : 1721 - 1732
  • [9] Thermal lattice Boltzmann equation for low Mach number flows: Decoupling model
    Guo, Zhaoli
    Zheng, Chuguang
    Shi, Baochang
    Zhao, T. S.
    [J]. PHYSICAL REVIEW E, 2007, 75 (03):
  • [10] Non-equilibrium extrapolation method for velocity and pressure boundary conditions in the lattice Boltzmann method
    Guo, ZL
    Zheng, CG
    Shi, BC
    [J]. CHINESE PHYSICS, 2002, 11 (04): : 366 - 374