NAVIER-STOKES SOLUTION OF TRANSONIC CASCADE FLOWS USING NONPERIODIC C-TYPE GRIDS

被引:62
作者
ARNONE, A [1 ]
LIOU, MS [1 ]
POVINELLI, LA [1 ]
机构
[1] NASA,LEWIS RES CTR,DIV INTERNAL FLUID MECH,CLEVELAND,OH 44135
关键词
D O I
10.2514/3.23493
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A new kind of C-type grid is proposed for turbomachinery flow calculations. This grid is nonperiodic on the wake and results in minimum skewness for cascades with high turning and large camber. The Reynolds-averaged Navier-Stokes equations are discretized on this type of grid using a finite volume approach. The Baldwin-Lomax eddy-viscosity model is used for turbulence closure. Jameson's explicit Runge-Kutta scheme is adopted for the integration in time, and computational efficiency is achieved through accelerating strategies such as multigriding and residual smoothing. A detailed numerical study has been carried out for a turbine rotor and for a vane. A grid dependence analysis is presented and the effect of the artificial dissipation is also investigated. Comparison of calculations with experiments clearly demonstrate the advantage of the proposed grid.
引用
收藏
页码:410 / 417
页数:8
相关论文
共 20 条
[1]  
ARNONE A, 1989, ASME89GT22 PAP
[2]  
ARNONE A, 1990, P CFD S AEROPROPULSI
[3]  
ARNONE A, 1988, ICASE8832 REP
[4]  
BALDWIN BS, 1978, AIAA780257 PAP
[5]   INVISCID AND VISCOUS FLOWS IN CASCADES WITH AN EXPLICIT MULTIPLE-GRID ALGORITHM [J].
CHIMA, RV .
AIAA JOURNAL, 1985, 23 (10) :1556-1563
[6]  
DAVIS RL, 1986, AIAA860033 PAP
[7]  
HAH C, 1990, AIAA900343 PAP
[8]   A 3-DIMENSIONAL EULER SOLVER FOR TURBOMACHINERY BLADE ROWS [J].
HOLMES, DG ;
TONG, SS .
JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 1985, 107 (02) :258-264
[9]  
JAMESON A, 1983, MAE1651 PRINC U MAE
[10]  
JAMESON A, 1981, AIAA811259 PAP