A Compact Third-order Gas-kinetic Scheme for Compressible Euler and Navier-Stokes Equations

TL;DR

This paper introduces a high-order, compact third-order gas-kinetic scheme for solving compressible Euler and Navier-Stokes equations, utilizing a high-order gas evolution model for accurate flux and flow variable computation.

Contribution

It develops a novel compact third-order scheme based on a high-order gas evolution model, avoiding Gaussian points and multi-stage Runge-Kutta methods, with enhanced shock capturing.

Findings

Achieves third-order accuracy in smooth regions

Effectively captures shocks and discontinuities

Reduces computational complexity by avoiding Gaussian points

Abstract

In this paper, a compact third-order gas-kinetic scheme is proposed for the compressible Euler and Navier-Stokes equations. The main reason for the feasibility to develop such a high-order scheme with compact stencil, which involves only neighboring cells, is due to the use of a high-order gas evolution model. Besides the evaluation of the time-dependent flux function across a cell interface, the high-order gas evolution model also provides an accurate time-dependent solution of the flow variables at a cell interface. Therefore, the current scheme not only updates the cell averaged conservative flow variables inside each control volume, but also tracks the flow variables at the cell interface at the next time level. As a result, with both cell averaged and cell interface values the high-order reconstruction in the current scheme can be done compactly. Different from using a weak formulation for high-order accuracy in the Discontinuous Galerkin (DG) method, the current scheme is based on the strong solution, where the flow evolution starting from a piecewise discontinuous high-order initial data is precisely followed. The cell interface time-dependent flow variables can be used for the initial data reconstruction at the beginning of next time step. Even with compact stencil, the current scheme has third-order accuracy in the smooth flow regions, and has favorable shock capturing property in the discontinuous regions. Many test cases are used to validate the current scheme. In comparison with many other high-order schemes, the current method avoids the use of Gaussian points for the flux evaluation along the cell interface and the multi-stage Runge-Kutta time stepping technique.