Implicit/multigrid algorithms for incompressible turbulent flows on unstructured grids

被引:96
作者
Anderson, WK [1 ]
Rausch, RD [1 ]
Bonhaus, DL [1 ]
机构
[1] LOCKHEED ENGN & SCI CO,HOUSTON,TX 77058
关键词
D O I
10.1006/jcph.1996.0219
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
An implicit code for computing inviscid and viscous incompressible flows on unstructured grids is described. The foundation of the code is a backward Euler time discretization for which the linear system is approximately solved at each time step with either a point implicit method or a preconditioned generalized minimal residual (GMRES) technique. For the GMRES calculations, several techniques are investigated for forming the matrix-vector product. Convergence acceleration is achieved through a multigrid scheme that uses nonnested coarse grids that are generated using a technique described in the present paper. Convergence characteristics are investigated and results are compared with an exact solution for the inviscid flow over a four-element airfoil. Viscous results, which are compared with experimental data, include the turbulent flow over a NACA 4412 airfoil, a three-element airfoil for which Mach number effects are investigated, and three-dimensional flow over a wing with a partial-span flap. (C) 1996 Academic Press, Inc.
引用
收藏
页码:391 / 408
页数:18
相关论文
共 56 条
[1]   BEHAVIOR OF LINEAR RECONSTRUCTION TECHNIQUES ON UNSTRUCTURED MESHES [J].
AFTOSMIS, M ;
GAITONDE, D ;
TAVARES, TS .
AIAA JOURNAL, 1995, 33 (11) :2038-2049
[2]   AN IMPLICIT UPWIND ALGORITHM FOR COMPUTING TURBULENT FLOWS ON UNSTRUCTURED GRIDS [J].
ANDERSON, WK ;
BONHAUS, DL .
COMPUTERS & FLUIDS, 1994, 23 (01) :1-21
[3]  
ANDERSON WK, 1993, AIAA930645
[4]  
ANDERSON WK, 1992, 4295 NASA
[5]  
[Anonymous], 1989, 27 AER SCI M
[6]  
[Anonymous], THESIS G WASHINGTON
[7]  
[Anonymous], 890122 AIAA
[8]  
Barth T.J., 1991, 910721 AIAA
[9]  
BARTH TJ, 1995, 950213 AIAA
[10]  
BARTH TJ, 1995, 950221 AIAA