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IMPINGING JET HEAT TRANSFER IN THE TRANSITIONAL WALL JET REGION

机译:在过渡壁射流区域中撞击喷射热传递

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Convective heat transfer to an impinging air jet is known to yield high local and area averaged heat transfer coefficients. Such jets are of interest in the cooling of electronic components and of turbine blades and in manufacturing processes such as grinding. The current research is concerned with the measurement of heat transfer to an impinging air jet over a wide range of test parameters. These include Reynolds numbers, Re, from 10000 to 30000 and nozzle to impingement surface distance, H/D, from 0.5 to 8. The current research reports both mean and fluctuating heat transfer distributions up to 6 diameters from the geometric centre of the jet. The heat transfer results are compared to local velocity data. At low nozzle to impingement surface spacings the heat transfer distributions exhibit peaks at a radial location that varies with both Re and H/D. These peaks are shown to be due to an abrupt increase in turbulence in the wall jet boundary layer. At certain test configurations vortices that initiate in the shear layer impinge on the surface and move along the wall jet before being broken down into smaller scale turbulence. The effects of the vortical flow on the heat transfer mechanisms in an impinging jet flow are discussed.
机译:已知对撞击空气射流的对流热传递得到高局部和面积平均传热系数。这种喷射对电子元件和涡轮叶片的冷却以及诸如研磨的制造过程感兴趣。目前的研究涉及在各种测试参数上测量传热到撞击空气喷射。这些包括reynolds数字,从10000到30000和喷嘴到冲击表面距离,h / d从0.5到8。目前的研究报告了从射流的几何中心的均值和波动传热分布。将传热结果与局部速度数据进行比较。在低喷嘴处于冲击表面间隔,传热分布在径向位置显示峰值,其与RE和H / D都变化。这些峰被认为是由于壁喷射边界层中的湍流突然增加。在某些测试配置中,在剪切层中发起的涡流撞击表面并在分解成较小的湍流之前沿着壁射流移动。讨论了涡流对撞击喷射流动中传热机制的影响。

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