Solution Verification Studies of a Pressure-Based Compressible Flow Solver

J. Muralha, C. Silva, L. Eça, C. Klaij
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引用次数: 2

Abstract

. Although considering the fluid to be incompressible is a common and valid approximation in most hydrodynamic simulations, certain phenomena like sloshing or slamming involve compressibility effects. In order to capture such effects, the maritime CFD code ReFRESCO is being extended with a compressible flow solver for the air in two-phase flow simulations. The compressible Navier-Stokes equations, discretized with a cell-centered, collocated finite volume method, are solved with a pressure-based SIMPLE algorithm that is compatible with the incompressible flow solver and enforces pressure-velocity-density coupling with a pressure-correction equation and an equation of state. In this paper, the compressible solver is tested for subsonic, transonic and supersonic flow of an inviscid perfect gas in a channel with an arc circular bump. We confirm that the pressure-based solver can indeed achieve iterative convergence to levels close to machine accuracy for all three regimes, with moderate decrease of convergence rate at higher Mach numbers and on finer grids. Grid refinement studies are performed to determine its accuracy and show observed orders of grid convergence between one and two for different quantities and different convection schemes, with lowest order for the supersonic regime, as expected. Finally, we notice that monotonic grid convergence can be
基于压力的可压缩流动求解器的解验证研究
. 虽然在大多数流体力学模拟中,考虑流体不可压缩是一种常见而有效的近似,但某些现象,如晃动或撞击,涉及可压缩性效应。为了捕捉这种效果,海上CFD代码ReFRESCO正在扩展可压缩流求解器,用于空气两相流模拟。采用基于压力的SIMPLE算法求解可压缩Navier-Stokes方程,该算法与不可压缩流动求解器兼容,并通过压力修正方程和状态方程实现压力-速度-密度耦合。本文用可压缩解算器对无粘理想气体在带圆弧凸点的通道中的亚、跨、超声速流动进行了测试。我们证实,基于压力的求解器确实可以在所有三种情况下实现迭代收敛,达到接近机器精度的水平,在较高马赫数和更细的网格上收敛速度适度下降。网格细化研究确定了其准确性,并显示了不同数量和不同对流方案下观测到的1和2之间的网格收敛阶数,如预期的那样,超音速区域的网格收敛阶数最低。最后,我们注意到单调网格可以收敛
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