“…where the second-order smoothness indicators β k , k = 0, 1, 2, derived by Hu [32] are adopted to measure the smoothness of f on the sub-stencils S k and are defined as…”
Section: Wcns Methodsmentioning
confidence: 99%
“…Remark 2. To update the solutions from t n to t n+1 by the p th -order IMEX-ARSp WCNS, we first solve the elliptic equation (32) to obtain ρ (k) and then calculate explicitly q (k) using (35). Here, (32) is a nonlinear equation for ρ (k) , which is solved by inexact Newton-generalized minimum residual (Newton-GMRES) algorithms.…”
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 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 and a fifth-order WCNS is used for the spatial discretization. The designed semi-implicit WCNS 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 method.
“…where the second-order smoothness indicators β k , k = 0, 1, 2, derived by Hu [32] are adopted to measure the smoothness of f on the sub-stencils S k and are defined as…”
Section: Wcns Methodsmentioning
confidence: 99%
“…Remark 2. To update the solutions from t n to t n+1 by the p th -order IMEX-ARSp WCNS, we first solve the elliptic equation (32) to obtain ρ (k) and then calculate explicitly q (k) using (35). Here, (32) is a nonlinear equation for ρ (k) , which is solved by inexact Newton-generalized minimum residual (Newton-GMRES) algorithms.…”
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 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 and a fifth-order WCNS is used for the spatial discretization. The designed semi-implicit WCNS 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 method.
“…where the second-order smoothness indicators β k , k = 0, 1, 2, derived by Hu [35] are adopted to measure the smoothness of f on the sub-stencils S k .…”
Section: Wcns Methodsmentioning
confidence: 99%
“…For the GSA IMEX-ARSp scheme, ρ n+1 = ρ (s) and q n+1 = q (s) . (35) and the gradient terms in (34) and (35) are solved by the fifth-order WCNS in the component-bycomponent and dimension-by-dimension forms. Here, in the interpolation process of the cell-edge pressures, the Lax-Friedrichs flux with zero numerical viscosity is considered, i.e., p = 1 2 p + 1 2 p, otherwise the numerical diffusion will become large when ε → 0 [10].…”
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.
“…The spatial discretization of both convective terms in (33)-(35) and the gradient terms in(34) and(35)are solved by the fifth-order WCNS in the component-by-component and dimension-by-dimension forms. Here, in the interpolation process of the cell-edge pressures, the Lax-Friedrichs flux with zero numerical…”
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 discretizationof 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 incompressibleregimes are given to demonstrate the advantages of the designed IMEX WCNS.
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