High-order-accurate numerical method for complex flows

被引:114
作者
Gross, A. [1 ]
Fasel, H. F. [1 ]
机构
[1] Univ Arizona, Dept Aerosp & Mech Engn, Tucson, AZ 85721 USA
关键词
D O I
10.2514/1.22742
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A numerical method employing high-order-accurate (higher than third) upwind discretizations for solving the compressible Navier-Stokes equations on structured grids is discussed. The inviscid fluxes are computed by a procedure based on a weighted essentially nonoscillatory interpolation of the characteristic variables and the Roe scheme. Application of the numerical method to a number of test cases of increasing complexity, that are prototypical for several of the key aspects of practical flows, demonstrates the accuracy and robustness of the method even when computing on distorted curvilinear grids. Significant reductions in computer time are possible when a second-order-accurate implicit Adams-Moulton scheme is employed for time integration. The combination of implicit time integration and high-order-accurate spatial discretization is shown to lead to significant savings in compute time as the grid resolution requirement is lowered and the time step can be increased.
引用
收藏
页码:204 / 214
页数:11
相关论文
共 29 条
[1]   Monotonicity preserving weighted essentially non-oscillatory schemes with increasingly high order of accuracy [J].
Balsara, DS ;
Shu, CW .
JOURNAL OF COMPUTATIONAL PHYSICS, 2000, 160 (02) :405-452
[2]  
Ferziger JH, 1981, NUMERICAL METHODS EN
[3]  
GOTTLIEB D, 1976, MATH COMPUT, V30, P703, DOI 10.1090/S0025-5718-1976-0443362-6
[4]   Characteristic ghost-cell boundary condition [J].
Gross, A. ;
Fasel, H. F. .
AIAA JOURNAL, 2007, 45 (01) :302-306
[5]   Numerical investigation of low-pressure turbine blade separation control [J].
Gross, A ;
Fasel, HF .
AIAA JOURNAL, 2005, 43 (12) :2514-2525
[6]  
GROSS A, 2002, AIAA20022735 AIAA
[7]  
GUSTAFSSON B, 1975, MATH COMPUT, V29, P396, DOI 10.1090/S0025-5718-1975-0386296-7
[8]  
HANEL D, 1989, AIAA89274
[9]  
HARRIS PJ, 1997, THESIS U ARIZONA TUC
[10]  
Huang J., 2003, AIAA20031027