计算物理 ›› 1990, Vol. 7 ›› Issue (3): 275-282.

• 论文 • 上一篇    下一篇

一种数值模拟S形进气道内可压缩湍流的隐式迎风增量迭代法

姜宗林   

  1. 北京空气动力研究所 100074
  • 收稿日期:1989-08-01 出版日期:1990-09-25 发布日期:1990-09-25

AN IMPLICIT FINITE DIFFERENCE SCHEME FORSIMULATION OF COMPRESSIBLE TURBULENCEFLOWS IN A S-SHAPED CHANNEL

Jiang Zonglin   

  1. Beijing Institute of A erodynamics
  • Received:1989-08-01 Online:1990-09-25 Published:1990-09-25

摘要: 在这篇文章里,我们提出了一个二阶隐式迎风的增量迭代法,用以离散BFC(Body-Fitted Coordinates)坐标变换下的Navier-Stokes方程。使用这种算法结合Lomax两层代数湍流模型数值求解了S形进气道内的可压缩湍流。数值实验表明:计算过程具有较好的稳定性和收敛性。二维Poissuil流动和Couette流动的计算结果和精确解符合良好,两种壁面曲率不同的S形进气道内流场的计算结果也是令人满意的。

关键词: 湍流, Navier Stokes方程, 增量迭代法

Abstract: In this paper, an implicit and upwind incremental Block-Line-Gauss-Seidel Method is developed for solving compressible Navier Stokes equations in the Body-Fitted coordinate system. The computational solutions of the internal compressible turbulence flow have been obtained by the method with a two-layer eddy viscosity model employing a Baldwin-Lomax algebraic turbulece model. Numerical experiments show that the computational procedure is of good stability and convergence. Numerical results of the Poissuil flow and Couette flow are good agreement with its analytic solution and computational results of flows in S-Shaped channel with different wall curvature are satisfactorily.

Key words: turbulence flow, Navier-Stokes equations, increment line-seidel technique