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一种高效的多重网格三维N-S方程计算方法及其应用
引用本文:乔渭阳,王占学,蔡元虎. 一种高效的多重网格三维N-S方程计算方法及其应用[J]. 中国航空学报, 2002, 15(4): 193-199
作者姓名:乔渭阳  王占学  蔡元虎
作者单位:Aero engine Department,Northwestern Polytechnical University,Xi′an 710072,China
基金项目:Aeronautic Science Foundation(0 1C5 3 0 11)
摘    要:介绍一种基于 Jameson中心差分和 Runge-Kutta时间推进的三维 N-S方程计算的有限体积方法 ,计算点选取体积单元中心 ,为了提高收敛效率和程序稳定性 ,采用了当地时间步长和多重网格方法 ,特别是针对粘性计算中计算网格形状比高的特点 ,隐式残差光顺采用当地变系数的方法 ,并专门设计了考虑计算网格形状比的人工粘性模型。应用本文方法对收扩喷管的三维流场和NACA0 0 1 2翼型二维流场进行了计算 ,结果表明程序具有良好的收敛能力和较高的稳定性。

关 键 词:CFD  有限体积方法  N-S方程

Efficient Cell-Centered Multigrid Scheme for the Three-Dimensional Navier-Stokes Equations
Qiao Wei-yang,WANG Zhan-xue,CAI Yuan-hu. Efficient Cell-Centered Multigrid Scheme for the Three-Dimensional Navier-Stokes Equations[J]. Chinese Journal of Aeronautics, 2002, 15(4): 193-199
Authors:Qiao Wei-yang  WANG Zhan-xue  CAI Yuan-hu
Affiliation:Aero-engine Department, Northwestern Polytechnical University, Xi′an 710072,China;Aero-engine Department, Northwestern Polytechnical University, Xi′an 710072,China;Aero-engine Department, Northwestern Polytechnical University, Xi′an 710072,China
Abstract:A cell centered scheme for three dimensional Navier Stokes equations, which is based on central difference approximations and Runge Kutta time stepping, is described. By using local time stepping, implicit residual smoothing, a multigrid method, and carefully controlled artificial dissipative terms, good convergence rates are obtained for two and three dimensional flows. The emphases are on the implicit smoothing and artificial dissipative terms with locally variable coefficients which depend on cell aspect ratios. The computational results for two dimensional subsonic airfoil flows and three dimensional transonic C D nozzle flows are essentially coincident with other experimental and calculated results.
Keywords:CFD  finite volume method  N S equations
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