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The response of a turbulent boundary layer to different shaped transverse grooves

机译:湍流边界层对不同形状的横向沟槽的响应

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The response of a turbulent boundary layer to three different shaped transverse grooves was investigated at two values of momentum thickness Reynolds numbers ( R (theta)=1000 and 3000). A 20-mm wide square, semicircular and triangular groove with depth to width ( d / w) ratio of unity was used. In general, the effects of the grooves are more significant at the higher R (theta), with the most pronounced effects caused by the square groove. An increase in wall shear stress tau(w) was observed just downstream of the groove for all three shapes. The increase in tau(w) is followed by a small decrease in tau(w) below the smooth-wall value before it relaxes back to the corresponding smooth-wall value at x / delta(0)approximate to3. At the higher R (theta), the maximum increase in tau(w) for the square groove is about 50% higher than for the semicircular groove and almost twice that for the triangular groove. The effect of the square groove on U / U-0, u '/ U-0 and v '/ U-0 is much more significant than the effect of the semicircular and triangular grooves. There is an increase in the bursting frequency ( f (+)(B)) on the grooved-wall compared to the smooth-wall case. The distribution of f(B)(+) downstream of the different shaped grooves is similar to the tau(w) distribution. [References: 33]
机译:在两个动量厚度雷诺数(Rθ= 1000和3000)的值下研究了湍流边界层对三个不同形状的横向沟槽的响应。使用20毫米宽的正方形,半圆形和三角形凹槽,深度与宽度(d / w)的比率为1。通常,在较高的R(θ)下,凹槽的影响更为明显,而最明显的影响是由方形凹槽引起的。对于这三种形状,仅在凹槽的下游观察到壁切应力tau(w)的增加。在tau(w)增加之后,tau(w)在光滑壁面值以下有小幅下降,然后才松弛回到x / delta(0)近似为3的相应光滑壁面值。在较高的R(θ)处,方形凹槽的tau(w)最大增加量比半圆形凹槽高约50%,几乎是三角形凹槽的两倍。方形凹槽对U / U-0,u'/ U-0和v'/ U-0的影响比半圆形和三角形凹槽的影响大得多。与光滑壁的情况相比,开槽壁的爆裂频率(f(+)(B))增加。不同形状的凹槽下游的f(B)(+)分布类似于tau(w)分布。 [参考:33]

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