Implicit time integration schemes for the unsteady compressible Navier-Stokes equations: Laminar flow

被引:127
作者
Bijl, H [1 ]
Carpenter, MH
Vatsa, VN
Kennedy, CA
机构
[1] Delft Univ Technol, Dept Aerosp Engn, Delft, Netherlands
[2] NASA, Langley Res Ctr, Computat Method & Simulat Branch, Hampton, VA 23681 USA
[3] Sandia Natl Labs, Combust Res Facil, Livermore, CA 94551 USA
基金
美国能源部;
关键词
D O I
10.1006/jcph.2002.7059
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
The accuracy and efficiency of several lower and higher order time integration schemes are investigated for engineering solution of the discretized unsteady compressible Navier-Stokes equations. Fully implicit methods tested are either the backward differentiation formulas (BDF) or stage-order two. explicit, singly diagonally implicit Runge-Kutta (ESDIRK) methods. For this comparison an unsteady two-dimensional laminar flow problem is chosen: flow around a circular cylinder at Re = 1200. At temporal error tolerances consistent with engineering simulation. E approximate to 10(-1)-10(-2). first-order implicit Fuler (BDFI) is uncompetitive. While BDF3 is quite efficient, its lack of A-stability may be problematic in the presence of convection. At these same error tolerances, the fourth-order ESDIRK scheme is 2.5 times more efficient than BDF2. It is concluded that reliable integration is most efficiently provided by fourth-order Runge-Kutta methods for this problem where order reduction is not observed. Efficiency gains are more dramatic at smaller tolerances. (C) 2002 Elsevier Science (USA).
引用
收藏
页码:313 / 329
页数:17
相关论文
共 20 条
[1]  
Badcock KJ, 2000, INT J NUMER METH FL, V32, P585, DOI 10.1002/(SICI)1097-0363(20000315)32:5<585::AID-FLD976>3.0.CO
[2]  
2-1
[3]  
BIJL H, 2001, 20012612 AIAA
[4]  
Bosch G, 1998, INT J NUMER METH FL, V28, P601, DOI 10.1002/(SICI)1097-0363(19980930)28:4<601::AID-FLD732>3.0.CO
[5]  
2-F
[6]   THE EARLY STAGE OF DEVELOPMENT OF THE WAKE BEHIND AN IMPULSIVELY STARTED CYLINDER FOR 40 LESS-THAN RE LESS-THAN 104 [J].
BOUARD, R ;
COUTANCEAU, M .
JOURNAL OF FLUID MECHANICS, 1980, 101 (DEC) :583-&
[7]   Computation of vortex shedding and radiated sound for a circular cylinder: Subcritical to transcritical Reynolds numbers [J].
Cox, JS ;
Brentner, KS ;
Rumsey, CL .
THEORETICAL AND COMPUTATIONAL FLUID DYNAMICS, 1998, 12 (04) :233-253
[8]  
Hairer E., 2008, Solving Ordinary Differential Equations I Nonstiff problems
[9]   Low-storage, explicit Runge-Kutta schemes for the compressible Navier-Stokes equations [J].
Kennedy, CA ;
Carpenter, MH ;
Lewis, RM .
APPLIED NUMERICAL MATHEMATICS, 2000, 35 (03) :177-219
[10]  
KENNEDY CA, UNPUB ADDITIVE RUNGE