Conservative hybrid compact-WENO schemes for shock-turbulence interaction

被引:400
作者
Pirozzoli, S [1 ]
机构
[1] Univ Roma La Sapienza, Dipartimento Meccan & Aeronaut, I-00184 Rome, Italy
关键词
compact schemes; shock-capturing schemes; shock-turbulence interaction;
D O I
10.1006/jcph.2002.7021
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
In the present paper an efficient hybrid compact-WENO scheme is proposed to obtain high resolution in shock- turbulence interaction problems. The algorithm is based on a fifth-order compact upwind algorithm in conservation form to solve for the smooth part of the flow field, which is coupled with a high-resolution weighted essentially nonoscillatory (WENO) scheme to capture the discontinuities. The derivation of the compact scheme is discussed in detail, and a stability study of the full discretization is included. The performance of the numerical algorithm has been assessed by performing preliminary simulations on benchmark problems, such as the interaction of a shock wave with entropy and vortical disturbances. The algorithm here developed is proven to have better resolution properties than standard WENO schemes and hybrid compact-ENO schemes as well, at a lower computational cost. In addition. the application to more realistic shock-turbulence interaction problems is discussed. (C) 2002 Elsevier Science (USA).
引用
收藏
页码:81 / 117
页数:37
相关论文
共 50 条
[1]   A high-resolution hybrid compact-ENO scheme for shock-turbulence interaction problems [J].
Adams, NA ;
Shariff, K .
JOURNAL OF COMPUTATIONAL PHYSICS, 1996, 127 (01) :27-51
[2]   Direct numerical simulation of turbulent compression ramp flow [J].
Adams, NA .
THEORETICAL AND COMPUTATIONAL FLUID DYNAMICS, 1998, 12 (02) :109-129
[3]   On postshock oscillations due to shock capturing schemes in unsteady flows [J].
Arora, M ;
Roe, PL .
JOURNAL OF COMPUTATIONAL PHYSICS, 1997, 130 (01) :25-40
[4]   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
[5]  
CARPENTER M, IN PRESS J SCI COMPU
[6]   INTERACTION OF A PLANE SHOCK AND OBLIQUE PLANE DISTURBANCES WITH SPECIAL REFERENCE TO ENTROPY WAVES [J].
CHANG, CT .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1957, 24 (09) :675-682
[7]   NON-LINEAR INTERACTIONS IN A VISCOUS HEAT-CONDUCTING COMPRESSIBLE GAS [J].
CHU, BT ;
KOVASZNAY, LSG .
JOURNAL OF FLUID MECHANICS, 1958, 3 (05) :494-514
[8]   NONLINEARLY STABLE COMPACT SCHEMES FOR SHOCK CALCULATIONS [J].
COCKBURN, B ;
SHU, CW .
SIAM JOURNAL ON NUMERICAL ANALYSIS, 1994, 31 (03) :607-627
[9]  
Collatz L., 1966, NUMERICAL TREATMENT
[10]   BOUNDARY-CONDITIONS FOR DIRECT COMPUTATION OF AERODYNAMIC SOUND GENERATION [J].
COLONIUS, T ;
LELE, SK ;
MOIN, P .
AIAA JOURNAL, 1993, 31 (09) :1574-1582