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Transient flow over generic rear view mirror using computational fluid dynamics

机译:使用计算流体动力学在通用后视镜上的瞬态流动

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The present paper is an attempt to investigate the transient flow over generic rear view mirror with different turbulent models, Reynolds numbers and model yawing angles using computational fluid dynamics (CFD) with identical grid, second order schemes and the incompressible assumption. Average pressure coefficient, standard deviation (SD) of velocity and pressure fluctuations, power spectral density (PSD) of flow parameters were taken into consideration. Mean pressure coefficient on the surface of the mirror in good agreement with the experimental data available from literature indicates that both detached eddy simulation (DES) and large eddy simulation (LES) have ability to predict the flow field of mirror. Further discussion can be found that flow separation is the key factor leading to large σ(Cp'') value of the rear face and the instability of shear layer leads to a large velocity fluctuation. The distribution of pressure and velocity fluctuations is symmetric when the mirror is 0°. The PSD of pressure fluctuations shows that most of its energy focuses on low frequency and those sensors which locate at the separation zone have larger fluctuation than it is at other zones. All findings help us to better understand the transient flow mechanism of rear view mirror, and it is beneficial to control the aerodynamic noise generated by mirror.
机译:本文尝试使用具有相同网格,二阶格式和不可压缩假设的计算流体力学(CFD)研究具有不同湍流模型,雷诺数和偏航角的通用后视镜上的瞬态流动。考虑了平均压力系数,速度和压力波动的标准偏差(SD),流动参数的功率谱密度(PSD)。反射镜表面的平均压力系数与文献提供的实验数据高度吻合,表明分离涡模拟(DES)和大涡模拟(LES)都具有预测反射镜流场的能力。进一步的讨论可以发现,流分离是导致背面大σ(Cp'')值的关键因素,而剪切层的不稳定性会导致较大的速度波动。当反射镜为0°时,压力和速度波动的分布是对称的。压力波动的PSD显示,其大部分能量集中在低频上,并且位于分离区域的那些传感器的波动比在其他区域的传感器大。所有的发现有助于我们更好地理解后视镜的瞬态流动机理,并且有利于控制由后视镜产生的空气动力噪声。

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