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首页> 外文期刊>Journal of Wind Engineering and Industrial Aerodynamics: The Journal of the International Association for Wind Engineering >Large-eddy simulation of flow over a surface-mounted prism using a high-order finite-difference scheme
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Large-eddy simulation of flow over a surface-mounted prism using a high-order finite-difference scheme

机译:使用高阶有限差分方案对表面安装棱镜上的流动进行大涡模拟

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Large eddy simulation (LES) of the flow field over a surface-mounted prism under two different conditions, namely smooth and turbulent inflows, are carried out. A higher-order scheme, in which artificial dissipation is controllable, is used. The simulations are validated through comparison with experimental measurements. The results present new physical aspects and details regarding the development of the primary separation flow on the upwind face of the prism, the development of the horseshoe vortex flow, the primary and secondary separations of the reversed flow on the roof, and finally the locations of the highest suction pressures (in the mean) on the roof and the sides of the prism with respect to the secondary separation lines. The effects of the incident turbulence are determined by pointing out differences in the flow topologies between the two incident flow cases. Based on the validation with the experimental results, the compact upwind difference fifth-order scheme, used here, is recommended for performing LESS of complex flows.
机译:在两个不同的条件下,即表面光滑和湍流流入,对表面安装的棱镜上的流场进行了大涡模拟(LES)。使用可以控制人工耗散的高阶方案。通过与实验测量值的比较来验证仿真。结果提供了新的物理方面和细节,涉及在棱镜的迎风面上的主要分离流的发展,马蹄涡流的发展,屋顶上反向流的主要和次要分离以及最终的位置。相对于辅助分隔线,在顶部和棱镜侧面上的最高吸气压力(平均值)。通过指出两种入射流情况之间的流拓扑差异来确定入射湍流的影响。基于实验结果的验证,建议在此处使用紧凑的迎风差分五阶方案来执行复杂流的LESS。

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