2020
DOI: 10.1016/j.jcp.2020.109367
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A HWENO reconstruction based high-order compact gas-kinetic scheme on unstructured mesh

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Cited by 37 publications
(20 citation statements)
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“…In recent years, a class of high-order compact gas-kinetic scheme (CGKS) [23,15] has been developed from the second-order gas-kinetic scheme (GKS) [34]. The time-dependent interface evolution solution in CGKS is based on an analytical integral solution of the Bhatnagar-Gross-Krook equation [5], which recovers a transition process from the kinetic scale flux vector splitting to the central difference Lax-Wendroff type discretization.…”
Section: Introductionmentioning
confidence: 99%
“…In recent years, a class of high-order compact gas-kinetic scheme (CGKS) [23,15] has been developed from the second-order gas-kinetic scheme (GKS) [34]. The time-dependent interface evolution solution in CGKS is based on an analytical integral solution of the Bhatnagar-Gross-Krook equation [5], which recovers a transition process from the kinetic scale flux vector splitting to the central difference Lax-Wendroff type discretization.…”
Section: Introductionmentioning
confidence: 99%
“…Due to their differences in the updating schemes, the compact GKS can use a larger time step and has better robustness than the corresponding DG methods. For example, a CFL number around 0.5 can be taken for the third-order compact GKS [9] while it is restricted to be less than 0.33 for the third-order P1P2-rDG scheme. The P1P2-rDG is claimed to be unstable on tetrahedral mesh with smooth reconstruction.…”
Section: Introductionmentioning
confidence: 99%
“…In this paper, a multiscale method will be developed for the system with the gas-kinetic scheme (GKS) for the gas phase and the UGKWP for the particle phase [61,60]. The GKS is a gas-kinetic theory-based Navier-Stokes solver which is basically the limiting scheme of UGKWP in the continuum flow regime [24,67,25]. For the continuum flow, the GKS has been used in the turbulence flow [5,6], acoustic wave [66], multi-component flow [59,44], and hypersonic flow studies [27].…”
Section: Introductionmentioning
confidence: 99%