论文标题
3D Navier-Stokes方程在所有马赫数字上的高压基基压力IMEX方案
High order pressure-based semi-implicit IMEX schemes for the 3D Navier-Stokes equations at all Mach numbers
论文作者
论文摘要
本文旨在开发一个基于高阶压力的求解器,以在所有马赫数下的3D可压缩Navier-Stokes系统的解决方案。我们提出了以细胞为中心的管理方程式的离散化,将通量分为快速和缓慢的尺度部分,分别被隐式和显式地处理。为动能以及能量方程中的焓通量提出了一种新型的半无限制离散化,因此避免了任何需要迭代求解器的需求。隐式离散化产生了在理想气体和状态(EOS)方程(EOS)方程的压力上产生的椭圆方程。在非线性EOS的情况下,使用嵌套的牛顿方法来解决压力的轻度非线性系统。及时的高阶是通过隐式解释(IMEX)阶段逐步授予的,而一种新颖的CWENO技术有效地以尺寸划分的方式实施,以实现在空间中实现高阶,以离散显式对流和粘性通量。然后得出数值通量的高阶近似值,并得出一个无正素的有限体积求解器。最终,没有耗散适当准确性顺序的中央方案最终用于隐式项的数值近似。因此,最大可允许的时间步骤上的CFL型稳定性条件仅基于流体速度,而不基于声速,因此新型方案可用于所有MACH数字。通过涉及低和高马赫数制度以及无粘性和粘性流的广泛基准问题来评估所提出方法的收敛性和鲁棒性。
This article aims at developing a high order pressure-based solver for the solution of the 3D compressible Navier-Stokes system at all Mach numbers. We propose a cell-centered discretization of the governing equations that splits the fluxes into a fast and a slow scale part, that are treated implicitly and explicitly, respectively. A novel semi-implicit discretization is proposed for the kinetic energy as well as the enthalpy fluxes in the energy equation, hence avoiding any need of iterative solvers. The implicit discretization yields an elliptic equation on the pressure that can be solved for both ideal gas and general equation of state (EOS). A nested Newton method is used to solve the mildly nonlinear system for the pressure in case of nonlinear EOS. High order in time is granted by implicit-explicit (IMEX) time stepping, whereas a novel CWENO technique efficiently implemented in a dimension-by-dimension manner is developed for achieving high order in space for the discretization of explicit convective and viscous fluxes. A quadrature-free finite volume solver is then derived for the high order approximation of numerical fluxes. Central schemes with no dissipation of suitable order of accuracy are finally employed for the numerical approximation of the implicit terms. Consequently, the CFL-type stability condition on the maximum admissible time step is based only on the fluid velocity and not on the sound speed, so that the novel schemes work uniformly for all Mach numbers. Convergence and robustness of the proposed method are assessed through a wide set of benchmark problems involving low and high Mach number regimes, as well as inviscid and viscous flows.