Flow structure and cooling behavior of air impingement on a target plate

Adnan A. Abdul Rasool, F. Hamad
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引用次数: 2

Abstract

An experimental data of flow field, pressure coefficient and heat transfer of a jet impinging normally on a flat target plate are presented. The measurements of temperatures and static pressures were carried out for flow from three orifices of 5, 10 and 20 mm diameter for orifice-to-target plate distances of 5, 10, 25, 50, 70, 100 and 120 mm from the orifice exit. The axial development of flow structure of the jet from the orifice was investigated by measuring the radial jet velocity distributions at the same axial distances used to measure heat transfer and static pressure. The results show that pressure coefficients distributions on the target plate are similar to the velocity distributions in the impinging jet which indicates the strong relationship between the two parameters. The pressure coefficients from large orifice diameter are higher than the values from the small orifice diameter for same orifice-to-target plate distance. The results also show a nonlinear increase of heat transfer rate with orifice size and the ratio of axial distance to orifice diameter (X/d). The nonlinear behaviour may be attributed to the complex nature of flow structure at the stagnation region. The high velocity gradients at the stagnation zone leads to higher turbulence and comparatively higher values of heat transfer rates for large orifice diameter.
空气撞击靶板的流动结构与冷却行为
给出了射流在平面靶板上正常撞击时的流场、压力系数和传热的实验数据。对直径分别为5、10和20 mm的三个孔板进行了温度和静压测量,孔板与靶板的距离分别为5、10、25、50、70、100和120 mm。通过测量与测量传热和静压相同轴向距离的径向射流速度分布,研究了孔口射流的轴向流动结构发展。结果表明,靶板上的压力系数分布与冲击射流中的速度分布相似,表明两者之间存在较强的相关性。在相同的孔距下,大孔径的压力系数高于小孔径的压力系数。换热率随孔尺寸和轴向距离与孔直径之比(X/d)呈非线性增加。这种非线性行为可归因于滞止区流动结构的复杂性。滞止区的高速度梯度导致较大的湍流和相对较高的换热率值。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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