Implicit unified gas-kinetic scheme for steady state solutions in all flow regimes

被引:103
|
作者
Zhu, Yajun [1 ]
Zhong, Chengwen [1 ]
Xu, Kun [2 ]
机构
[1] Northwestern Polytech Univ, Natl Key Lab Sci & Technol Aerodynam Design & Res, Xian 710072, Peoples R China
[2] Hong Kong Univ Sci & Technol, Dept Mech & Aerosp Engn, Dept Math, Hong Kong, Hong Kong, Peoples R China
基金
中国国家自然科学基金;
关键词
Implicit scheme; Unified gas kinetic scheme; LU-SGS; Steady state solution; Rarefied and continuum flows; NAVIER-STOKES EQUATIONS; BGK SCHEME; RAREFIED-GAS; CONTINUUM; PLANE; EULER; MODEL;
D O I
10.1016/j.jcp.2016.03.038
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
This paper presents an implicit unified gas-kinetic scheme (UGKS) for non-equilibrium steady state flow computation. The UGKS is a direct modeling method for flow simulation in all regimes with the updates of both macroscopic flow variables and microscopic gas distribution function. By solving the macroscopic equations implicitly, a predicted equilibrium state can be obtained first through iterations. With the newly predicted equilibrium state, the evolution equation of the gas distribution function and the corresponding collision term can be discretized in a fully implicit way for fast convergence through iterations as well. The lower-upper symmetric Gauss-Seidel (LU-SGS) factorization method is implemented to solve both macroscopic and microscopic equations, which improves the efficiency of the scheme. Since the UGKS is a direct modeling method and its physical solution depends on the mesh resolution and the local time step, a physical time step needs to be fixed before using an implicit iterative technique with a pseudotime marching step. Therefore, the physical time step in the current implicit scheme is determined by the same way as that in the explicit UGKS for capturing the physical solution in all flow regimes, but the convergence to a steady state speeds up through the adoption of a numerical time step with large CFL number. Many numerical test cases in different flow regimes from low speed to hypersonic ones, such as the Couette flow, cavity flow, and the flow passing over a cylinder, are computed to validate the current implicit method. The overall efficiency of the implicit UGKS can be improved by one or two orders of magnitude in comparison with the explicit one. (C) 2016 Elsevier Inc. All rights reserved.
引用
收藏
页码:16 / 38
页数:23
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