Browse > Article

Convergence Characteristics of Preconditioned Euler Equations  

이상현 (울산대학교 수송시스템공학부)
Publication Information
Journal of the Korean Society of Propulsion Engineers / v.8, no.1, 2004 , pp. 27-37 More about this Journal
Abstract
The convergence characteristics of preconditioned Euler equations were studied. A perturbation analysis was conducted to understand the behavior of the preconditioned Euler equations. Various speed flows in a two-dimensional channel with a 10% circular arc in the middle of the channel were calculated. Roe's FDS scheme was used for spatial discretization and the LU-SGS scheme was used for time integration. It is shown that the convergence characteristics of pressure and velocity were maintained regardless of the Mach numbers but that the convergence characteristics of temperature were strongly related to the Mach number and became worse as the Mach number decreased. The perturbation analysis well explained the trend of the convergence characteristics and showed that the convergence characteristics are strongly related with the behavior o( the Preconditioning matrix.
Keywords
Preconditioning; Convergence Characteristics; Euler Equations; Peturbation Analysis; Roe's FDS; LV-SGS;
Citations & Related Records
연도 인용수 순위
  • Reference
1 Shuen, J. S., Chen, K. H., and Choi, Y., 'A Coupled Implicit Method for ChemicalNon-Equilibrium Flows at All Speeds,'Journal of Computational Physics 106, 1993, pp.306-318
2 Dailey, L. D., and Pletcher, R. H., 'Evaluation of Multigrid Acceleration for Preconditioned Time-Accurate NavierStokes Algorithms,' AIAA 1995, pp.95-1668
3 Sesterhenn, J., Muller, B., and H. Thomann,'On Cancellation Problem In Calculating Low Mach number Flows,' Journal of Computational Physics. Vol.151, 1999, pp.597-615   DOI   ScienceOn
4 Yoon, S., and Jameson, A., 'Lower-Upper Method for the Euler and Navier-Stokes Equation,' AIAA Journal, Vol. 26, No.9, 1988, pp.1025-1026   DOI   ScienceOn
5 Chen, K. H., and Shuen, J. S., 'Three Dimensional Coupled Implicit Methods for Spray Combustion Flows at All Speeds,' AIAA 1994, pp.94-3047
6 이상현, '저속 압축성 유동장 해석을 위한 예조건화 방법론 연구 II - 온도장 계산 성능 개선,' 공우주학회지, 29권, 8호, 2001, pp.26-36
7 이상현, '저속 압축성 유동장 해석을 위한 예조건화 방법론 연구 I,'항공우주학회지, 29권, 7호, 2001, pp.87-95
8 Lee, D., 'Design Criteria for Local Euler Preconditioning,' Journal of Computational Physics. Vol. 144, 1998, pp.423-459   DOI   ScienceOn
9 Hsieh, J. S-Y., and Yang V., 'A Preconditioning Flux-Difference Scheme for Chemically Reacting Flows at All Mach Numbers,' International Journal of CFD, Vol. 8. 1997, pp.31-49
10 Roe, P. L., 'Approximate Riemann Solvers, Parameter Vectors, and Difference Schemes,' Journal of Computational Physics, Vol. 43, No. 3, 1981, pp.352-372
11 Edwards, J. R., and Roy, C. J., 'Preconditioned Multigrid Methods for Two Dimensional Combustion Calculations at All Speeds,' AIAA Journal, Vol. 36, No.2, February, 1998, pp.185-192   DOI   ScienceOn
12 Edwards, J. R., and Liou M. S., 'Low Diffusion Flux Splitting Methods for Flows at All Speeds,' AIAA Journal, Vol. 36. No.9, 1998, pp.1610-1617   DOI   ScienceOn
13 Buelow, P..E, and Schwer, D. A., Feng, J, Merkle, C. L., and Choi, D., 'Three Dimensional Coupled Implicit Methods for Spray Combustion Flows at All Speeds,' AIAA 1994, pp.94-3047