Advances in Aerodynamics | |
High order semi-implicit weighted compact nonlinear scheme for the all-Mach isentropic Euler system | |
Shuguang Zhou1  Xun Chen2  Xu Zhang2  Yanqun Jiang2  Tao Xiong3  | |
[1] Computational Aerodynamics Institute, China Aerodynamics Research and Development Center;Department of Mathematics, Southwest University of Science and Technology;School of Mathematical Sciences, Fujian Provincial Key Laboratory of Mathematical Modeling and High-Performance Scientific Computing, Xiamen University; | |
关键词: High order scheme; IMEX time discretization; WCNS; Asymptotic-preserving property; Low Mach number; Isentropic Euler equations; | |
DOI : 10.1186/s42774-020-00052-9 | |
来源: DOAJ |
【 摘 要 】
Abstract The computation of compressible flows at all Mach numbers is a very challenging problem. An efficient numerical method for solving this problem needs to have shock-capturing capability in the high Mach number regime, while it can deal with stiffness and accuracy in the low Mach number regime. This paper designs a high order semi-implicit weighted compact nonlinear scheme (WCNS) for the all-Mach isentropic Euler system of compressible gas dynamics. To avoid severe Courant-Friedrichs-Levy (CFL) restrictions for low Mach flows, the nonlinear fluxes in the Euler equations are split into stiff and non-stiff components. A third-order implicit-explicit (IMEX) method is used for the time discretization of the split components and a fifth-order WCNS is used for the spatial discretization of flux derivatives. The high order IMEX method is asymptotic preserving and asymptotically accurate in the zero Mach number limit. One- and two-dimensional numerical examples in both compressible and incompressible regimes are given to demonstrate the advantages of the designed IMEX WCNS.
【 授权许可】
Unknown