A matrix stability analysis of the carbuncle phenomenon

被引:116
作者
Dumbser, M
Moschetta, JM
Gressier, M
机构
[1] Univ Stuttgart, Inst Aerodynam & Gasdynam, D-70550 Stuttgart, Germany
[2] SUPAERO, Dept Aerodynam, F-31400 Toulouse, France
[3] Off Natl Etud & Rech Aerosp, Dept Models Aerodynam Energet, F-31400 Toulouse, France
关键词
carbuncle phenomenon; shock instability; stability analysis; numerical shock structure; riemann solvers; upwind schemes;
D O I
10.1016/j.jcp.2003.12.013
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
The carbuncle phenomenon is a shock instability mechanism which ruins all efforts to compute grid-aligned shock waves using low-dissipative upwind schemes. The present study develops a stability analysis for two-dimensional steady shocks on structured meshes based on the matrix method. The numerical resolution of the corresponding eigenvalue problem confirms the typical odd-even form of the unstable mode and displays a Mach number threshold effect currently observed in computations. Furthermore, the present method indicates that the instability of steady shocks is not only governed by the upstream Mach number but also by the numerical shock structure. Finally, the source of the instability is localized in the upstream region, providing some clues to better understand and control the onset of the carbuncle. (C) 2004 Elsevier Inc. All rights reserved.
引用
收藏
页码:647 / 670
页数:24
相关论文
共 40 条
[1]  
[Anonymous], 1991, NUMERICAL COMPUTATIO
[2]  
[Anonymous], 1974, APPL OPTIMAL ESTIMAT
[3]  
Aso S, 2002, 20020646 AIAA
[4]   On the choice of wavespeeds for the HLLC Riemann solver [J].
Batten, P ;
Clarke, N ;
Lambert, C ;
Causon, DM .
SIAM JOURNAL ON SCIENTIFIC COMPUTING, 1997, 18 (06) :1553-1570
[5]  
Bogdonoff S., 1959, J AERONAUT SCI, V26, P584
[6]  
BRACKEN RM, 2001, 20010796 AIAA
[7]  
COQUEL F, 1995, TM106843 NASA
[8]   A low-diffusion flux-splitting scheme for Navier-Stokes calculations [J].
Edwards, JR .
COMPUTERS & FLUIDS, 1997, 26 (06) :635-659
[9]   ON GODUNOV-TYPE METHODS NEAR LOW-DENSITIES [J].
EINFELDT, B ;
MUNZ, CD ;
ROE, PL ;
SJOGREEN, B .
JOURNAL OF COMPUTATIONAL PHYSICS, 1991, 92 (02) :273-295
[10]   FLOW OF A JET FROM A BODY OPPOSING A SUPERSONIC FREE STREAM [J].
FINLEY, PJ .
JOURNAL OF FLUID MECHANICS, 1966, 26 :337-&