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EFFECT OF DEFLECTED INFLOW ON FLOWS IN A STRONGLY-CURVED 90 DEGREE ELBOW

机译:弯曲的流量对强弯90度弯头中流量的影响

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Wall pressure measurements and flow visualization were conducted for a 90 degree elbow with an axis curvature radius the same as its inner diameter (125 mm, R_c/D = 1). Reynolds numbers 320,000 and 500,000, based on the inner diameter and bulk velocity, were examined. A deflected inflow, having an almost constant velocity slope, was introduced in the present study. The velocity at the inside was 20% faster than the bulk velocity in the plane one diameter upstream of the elbow inlet. Ensemble averaged pressure distributions showed that no difference of normalized pressure could be found in cases of Reynolds numbers of 320,000 and 500,000. Comparisons with a uniform inlet flow case proved that a low-pressure region at the intrados of the elbow was weakened and that a high-pressure region outside strengthened in the deflected inflow case. The present case had a characteristic pressure distribution that the pressure downstream of the elbow increased at the inside until two diameters downstream from the elbow exit. Flow visualization concluded that the corresponding pressure increase was caused by a collision of a strengthened secondary flow convected from the extrados. The unsteady pressure distribution in the present case showed that a circumferential extent of a strongly fluctuating region in the inside and downstream of the elbow decreased, comparing with the uniform inlet flow case. Power spectral density functions of pressures exhibited that the fluctuation having the Strouhal number (based on the inner diameter and bulk velocity) of 0.6 existed in the downstream region of the elbow, which is 0.1 larger than that of the uniform inflow case.
机译:进行90度弯头的壁面压力测量和流动可视化,其轴曲率半径与其内径相同(125毫米,R_c / D = 1)。根据内径和体积速度,检查了雷诺数320,000和500,000。在本研究中引入了具有几乎恒定的速度斜率的偏转流入。内部的速度比弯头入口上游一直径平面中的整体速度快20%。集合平均压力分布表明,在雷诺数分别为320,000和500,000的情况下,未发现归一化压力的差异。与均匀进水箱的比较证明,在弯曲的进水箱中,弯头内腔处的低压区域被削弱,而外部的高压区则被加强。本例具有特征性的压力分布,肘部下游的压力在内部增加,直到肘部下游的两个直径。流动可视化得出的结论是,相应的压力增加是由从对流层对流的加强次流的碰撞引起的。与均匀的入口流动情况相比,在当前情况下的不稳定压力分布表明,在肘部的内部和下游,强烈波动区域的周向范围减小了。压力的功率谱密度函数表明,在肘部的下游区域存在Strouhal数(基于内径和体速度)为0.6的波动,该波动比均匀流入情况大0.1。

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