论文标题

轴向变化的砂纸粗糙度对泰勒 - 库特湍流的起泡阻力减少的影响

Effect of axially varying sandpaper roughness on bubbly drag reduction in Taylor-Couette turbulence

论文作者

Bullee, Pim A., Bakhuis, Dennis, Ezeta, Rodrigo, Huisman, Sander G., Sun, Chao, Lammertink, Rob G. H., Lohse, Detlef

论文摘要

我们实验研究了交替的粗糙和光滑壁对起泡拖动减少(DR)的影响。我们在$ 48.4 \,毫米$和$ 148.5 \,毫米$和粗糙度高度$ k = 695 \,μm$之间应用粗糙的砂纸带,$ s $ s $ s $ s $ s $ s $ s $ s $ s $ s $。在砂纸带之间,将IC在相似的宽度$ s $上揭开,从而导致交替的粗糙和光滑的带,这是轴向方向恒定的模式。我们在水中的水中测量了从(剪切)reynolds编号$ \ textIt {re} _s $从$ 0.5 \ times 10^6 $到$ 1.8 \ times 10^6 $的dr,源于(剪切)reynolds编号$ \ textit {re} _s $。将结果与具有完全光滑的IC和IC完全覆盖的砂纸相同的粗糙度$ K $的IC进行比较。所有变化的外缸保持光滑。还将结果与气泡的DR测量值进行了比较,在该测量中,光滑的外部圆柱体沿与光滑IC相反的方向旋转。这种反旋转引起的二级流结构与IC由IC组成时观察到的二级流量结构非常相似。对于粗糙度的测量,发现起泡的DR最初使用$ \ textit {re} _s $更强烈地增加,然后才能达到不再取决于$ \ textit {re} _s $的值。这归因于气泡的更均匀的轴向分布,这是由于流动的湍流强度的增加而与在相同$ \ textit {re} _s $上完全光滑的壁上流动相比。气泡被认为在流动的粗壁部分积聚。在本地,阻力最大,因此气泡的阻力减少效果最强。因此,与完全粗糙的壁相比,发现了交替的粗糙和光滑壁的最大气泡DR的最大值。

We experimentally investigate the influence of alternating rough and smooth walls on bubbly drag reduction (DR). We apply rough sandpaper bands of width $s$ between $48.4\,mm$ and $148.5\,mm$, and roughness height $k = 695\,μm$, around the smooth inner cylinder (IC) of the Twente Turbulent Taylor-Couette facility. Between sandpaper bands, the IC is left uncovered over similar width $s$, resulting in alternating rough and smooth bands, a constant pattern in axial direction. We measure the DR in water that originates from introducing air bubbles to the fluid at (shear) Reynolds numbers $\textit{Re}_s$ ranging from $0.5 \times 10^6$ to $1.8 \times 10^6$. Results are compared to bubbly DR measurements with a completely smooth IC and an IC that is completely covered with sandpaper of the same roughness $k$. The outer cylinder is left smooth for all variations. Results are also compared to bubbly DR measurements where a smooth outer cylinder is rotating in opposite direction to the smooth IC. This counter rotation induces secondary flow structures that are very similar to those observed when the IC is composed of alternating rough and smooth bands. For the measurements with roughness, the bubbly DR is found to initially increase more strongly with $\textit{Re}_s$, before levelling off to reach a value that no longer depends on $\textit{Re}_s$. This is attributed to a more even axial distribution of the air bubbles, resulting from the increased turbulence intensity of the flow compared to flow over a completely smooth wall at the same $\textit{Re}_s$. The air bubbles are seen to accumulate at the rough wall sections in the flow. Here, locally, the drag is largest and so the drag reducing effect of the bubbles is felt strongest. Therefore, a larger maximum value of bubbly DR is found for the alternating rough and smooth walls compared to the completely rough wall.

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