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Effect of Local Grid Refinement on Performance of Scale-Resolving Models for Simulation of Complex External Flows

机译:局部网格细化对模拟复杂外部流动的尺度解析模型性能的影响

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Numerical simulations are crucial for fast and accurate estimations of the flow characteristics in many engineering applications such as atmospheric boundary layers around buildings, external aerodynamics around vehicles, and pollutant dispersion. In the simulation of flow over urban-like obstacles, it is crucial to accurately resolve the flow characteristics with reasonable computational cost. Therefore, Large Eddy Simulations on non-uniform grids are usually employed. However, an undesirable accumulation of energy at grid-refinement interfaces was observed in previous studies using non-uniform grids. This phenomenon induced oscillations in the spanwise velocity component, mainly on fine-to-coarse grid interfaces. In this study, the two challenging test cases of flow over urban-like cubes and flow over a 3-D circular cylinder were simulated using three different scale-resolving turbulence models. Simulations were performed on uniform coarse and fine grids on one hand, and a non-uniform grid on the other, to assess the effect of mesh density and mesh interfaces on the models’ performance. Overall, the proposed One-Equation Scale-Adaptive Simulation (One-Equation SAS) showed the least deviation from the experimental results in both tested cases and on all grid sizes and types when compared to the Shear Stress Transport-Improved Delayed Detached Eddy Simulation (IDDES) and the Algebraic Wall-Modeled Large Eddy Simulation (WMLES).
机译:在许多工程应用中,例如建筑物周围的大气边界层,车辆周围的外部空气动力学以及污染物扩散等方面,数值模拟对于快速,准确地估算流动特性至关重要。在模拟类似城市障碍物的流动过程中,以合理的计算成本准确解析流动特征至关重要。因此,通常采用非均匀网格上的大涡模拟。然而,在先前使用非均匀网格的研究中,观察到在网格细化界面上不希望有的能量积累。这种现象引起了翼展方向速度分量的振荡,主要是在细到粗网格界面上。在这项研究中,使用三种不同的尺度解析湍流模型模拟了两个具有挑战性的城市样立方体上的流动和3D圆柱上的流动的测试案例。一方面在均匀的粗网格和精细网格上进行仿真,另一方面在不均匀的网格上进行仿真,以评估网格密度和网格界面对模型性能的影响。总的来说,与剪切应力传输改进的延迟分离涡流仿真相比,拟议的一方程式自适应仿真(One-Equation SAS)在测试案例以及所有网格尺寸和类型上均显示出与实验结果的偏差最小( IDDES)和代数墙建模的大涡模拟(WMLES)。

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