基于高阶投影的上风法模拟过渡湍流

Philip L. Lederer, Xaver Mooslechner, Joachim Schöberl
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引用次数: 0

摘要

我们提出了一种针对不可压缩过渡流动的可扩展高阶隐式大涡度模拟(ILES)方法。该方法采用质量守恒混合应力(MCS)方法离散纳维-斯托克方程。MCS 方法的低耗散特性与引入的算子拆分求解技术相结合,产生了一种优化的高阶求解器,可高效并行计算欠分辨湍流。通过加入高阶上风通量,我们进一步增强了 ILES 模型的固有能力,并正在研究其在过渡气动流问题中的近似行为。在这项研究中,我们使用雷诺数高达 3 \cdot 10^5$ 的 Eppler 387 机翼上的流体作为模拟基准。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
High-order projection-based upwind method for simulation of transitional turbulent flows
We present a scalable, high-order implicit large-eddy simulation (ILES) approach for incompressible transitional flows. This method employs the mass-conserving mixed stress (MCS) method for discretizing the Navier-Stokes equations. The MCS method's low dissipation characteristics, combined with the introduced operator-splitting solution technique, result in a high-order solver optimized for efficient and parallel computation of under-resolved turbulent flows. We further enhance the inherent capabilities of the ILES model by incorporating high-order upwind fluxes and are examining its approximation behaviour in transitional aerodynamic flow problems. In this study, we use flows over the Eppler 387 airfoil at Reynolds numbers up to $3 \cdot 10^5$ as benchmarks for our simulations.
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