在周期性二维粗糙度上的湍流边界层中进行局部吹风以控制近平流和涡旋结构

Ali M. Hamed, Ryan Gallary, Bailey McAtee
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引用次数: 0

摘要

为研究局部吹气(喷射)作为 k 型二维粗糙度上湍流边界层的控制策略,进行了体积三分量流动测量。流动测量是在雷诺数为 100,000 时使用粒子跟踪测速仪进行的。粗糙度约占边界层厚度的 13%,由间距与高度比为 11 的横向方棒周期性定位组成。考虑了两种情况:无喷气的基线情况和从第 11 根方棒下游面喷出五个跨向喷气的情况。结果表明,吹风可以有效地减小再循环区的大小和穿过横杆的湍流。具体来说,吹气情况下的跨向平均流场显示,与基线情况相比,再附着长度减少了 40%,最大雷诺切应力减少了约 25%。此外,基线情况下穿过棒材的可视化涡旋结构显示出连贯的跨向涡旋,与穿过孤立的二维棒材和后向台阶时观察到的涡旋相似。吹风扰乱了这些跨向涡旋,并产生了新的较弱的涡旋结构,其旋转方向与壁面方向一致。因此,吹风导致 k 型二维粗糙度上流动的跨向平均涡度特征降低。跨向涡旋的破坏和再循环区面积的减小可能是近尾流雷诺切应力和湍流动能减小的原因。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Localized Blowing for Near-Wake Flow and Vortical Structure Control in Turbulent Boundary Layers Over Periodic 2D Roughness
Volumetric three-component flow measurements were made to investigate localized blowing (injection) as a control strategy for turbulent boundary layers over k-type 2D roughness. The flow measurements were made using particle tracking velocimetry at a Reynolds number of 100,000. The roughness occupied ~ 13% of the boundary layer thickness and consisted of transverse square bars positioned periodically at a pitch to height ratio of 11. Two cases were considered: a baseline case without blowing and a case with blowing through five spanwise jets issuing from the downstream face of the 11th bar. The results highlight the effectiveness of blowing in reducing the size of the recirculation zone and turbulence past the bar. Specifically, the spanwise-averaged flow field for the blowing case shows a 40% reduction in the reattachment length and ~ 25% reduction in the maximum Reynolds shear stress relative to the baseline case. Moreover, visualizations of the vortical structures past the bars for the baseline case display coherent spanwise vortices similar to those observed past isolated 2D bars and backward-facing steps. Blowing disrupts these spanwise vortices and produces new weaker vortical structures with a wall-normal sense of rotation. As such, blowing results in a reduction in the spanwise-averaged spanwise vorticity characteristic of the flow over k-type 2D roughness. The disruption of the spanwise vortices and the reduction in the size of the recirculation zone are likely responsible for the reduction in the Reynolds shear stress and turbulent kinetic energy in the near wake.
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