Unsteady flow calculations with a multigrid Navier-Stokes method

被引:37
作者
Liu, F
Ji, SH
机构
[1] University of California, Irvine, Irvine
关键词
D O I
10.2514/3.13351
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A multigrid Navier-Stokes method with a two-equation k-omega turbulence model is developed for calculating unsteady flows, The method uses a staggered finite volume scheme to discretize the Navier-Stokes and the turbulence model equations in space. A fully implicit time-accurate scheme is reformulated so that an efficient explicit multistage method with local time stepping, residual smoothing, and multigrid can be used to accelerate convergence within each unsteady time step, The method combines the advantages of implicit and explicit schemes for unsteady Bow calculations, Solutions for the forced oscillation of an airfoil are obtained with the Euler and the Navier-Stokes equations. Results are compared with experimental data.
引用
收藏
页码:2047 / 2053
页数:7
相关论文
共 17 条
[1]  
Alonso J., 1994, AIAA 32 AER SCI M RE
[2]  
ALONSO J, 1995, 950048 AIAA
[3]   INTEGRATION OF NAVIER-STOKES EQUATIONS USING DUAL TIME-STEPPING AND A MULTIGRID METHOD [J].
ARNONE, A ;
LIOU, MS ;
POVINELLI, LA .
AIAA JOURNAL, 1995, 33 (06) :985-990
[4]  
ARNONE A, 1993, P AIAA 11 COMP FLUID
[5]   CALCULATION OF UNSTEADY TRANSONIC FLOW OVER AN AIRFOIL [J].
CHYU, WJ ;
DAVIS, SS ;
CHANG, KS .
AIAA JOURNAL, 1981, 19 (06) :684-690
[6]  
DAVIS SS, 1982, AGARDR702
[7]  
Jameson A., 1991, AIAA 10 COMPUTATIONA, DOI DOI 10.2514/6.1991-1596
[8]  
JAMESON A, 1983, 1651 MAE PRINC U DEP
[9]  
JAMESON A, 1984, 811259 AIAA
[10]   STAGGERED FINITE-VOLUME SCHEME FOR SOLVING CASCADE FLOW WITH A K-OMEGA TURBULENCE MODEL [J].
LIU, F ;
ZHENG, XQ .
AIAA JOURNAL, 1994, 32 (08) :1589-1597