论文标题
保守的笛卡尔切割细胞法,用于交错网格上不可压缩的Navier-Stokes方程
A Conservative Cartesian Cut Cell Method for the Solution of the Incompressible Navier-Stokes Equations on Staggered Meshes
论文作者
论文摘要
计算流体动力学应用中复杂几何形状的处理是一项具有挑战性的努力,浸入边界和切线技术可以通过减轻物体拟合网格所需的网格锻造过程来大大简化。然而,这些方法引入了新的挑战,因为准确且良好的离散操作员的配方变得不平凡。在这里,提出了一种保守的笛卡尔切割细胞法,以解决不可压缩的Navier的解决方案 - 交错的笛卡尔网格上的stokes方程。重点放在离散操作员的结构上,旨在模仿连续的操作员,同时保留最近的邻居模具。对于对流传输,只要满足无差异条件,就提出了发散并显示出偏斜的对称性,从而确保质量,动量和动能能量保存(后者在无粘性极限处)。对于粘性运输,为Dirichlet边界条件提出了保守和对称操作员。对称性确保在离散的动能预算中存在下沉术语(粘性耗散),这对稳定性是有益的。切换离散化具有众多所需的逐个总和(SBP)属性。此外,它是完全保守的,在数学上是稳定的,并支持任意的几何形状。然后,通过圆形圆柱体和机翼的流动来证明该方法的精度和鲁棒性。
The treatment of complex geometries in Computational Fluid Dynamics applications is a challenging endeavor, which immersed boundary and cut-cell techniques can significantly simplify by alleviating the meshing process required by body-fitted meshes. These methods however introduce new challenges, as the formulation of accurate and well-posed discrete operators becomes nontrivial. Here, a conservative cartesian cut cell method is proposed for the solution of the incompressible Navier--Stokes equation on staggered Cartesian grids. Emphasis is set on the structure of the discrete operators, designed to mimic the properties of the continuous ones while retaining a nearest-neighbor stencil. For convective transport, a divergence is proposed and shown to also be skew-symmetric as long as the divergence-free condition is satisfied, ensuring mass, momentum and kinetic energy conservation (the latter in the inviscid limit). For viscous transport, conservative and symmetric operators are proposed for Dirichlet boundary conditions. Symmetry ensures the existence of a sink term (viscous dissipation) in the discrete kinetic energy budget, which is beneficial for stability. The cut-cell discretization possesses the much desired summation-by-parts (SBP) properties. In addition, it is fully conservative, mathematically provably stable and supports arbitrary geometries. The accuracy and robustness of the method are then demonstrated with flows past a circular cylinder and an airfoil.