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Experimental study of flow characteristics of an oblique impinging jet

机译:斜撞击射流流动特性的实验研究

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An experimental study has been performed by using particle image velocimetry to investigate the effect of nozzle-to-plate separation distance (L) and jet impingement angle on the flow characteristics of an obliquely inclined submerged water jet. Measurements were taken for L = 1D, 2D, 4D and 6D (where D is the diameter of the nozzle) for the jet impingement angle (theta) of 45 degrees and 26 degrees, and the flow characteristics in the uphill and the downhill regions are investigated at Reynolds number of 2600 (based on the nozzle diameter D and the jet velocity Uo). It is observed that surface spacing has an opposite effect in the uphill and the downhill regions in terms of wall jet flow. In the uphill region, the tendency of the wall jet to grow increases with increase in L/D. However, in the downhill region, the jet velocity and its thickness are observed to reduce as the separation distance is increased. The distance between the stagnation point and the geometric centre is observed to decrease with increase in L/D because of jet-ambient fluid interaction in the uphill region. The jet width is observed to grow for theta = 45 degrees in the downstream of the plate due to enhanced jet-ambient fluid interaction. Flow at theta = 26 degrees shows that after impingement the entire jet deviates towards the downhill side, which indicates the existence of a critical impingement angle below which there is no flow of the jet in the uphill region. RMS velocity fluctuations and shear stress show an increased turbulence level downstream of the plate in the downhill region for smaller impinging distance implying higher jet-ambient fluid interaction and increased jet width. They, along with the negative turbulence production term, reveal the region of flow separation and reattachment. The decrease in the peak value of Nusselt number can be related to the drop in the jet momentum at the stagnation point with increase in the surface spacing.
机译:通过使用粒子图像速度来研究喷嘴到板分离距离(L)和喷射冲击角对倾斜倾斜水射流的流动特性的影响进行了实验研究。用于L = 1d,2d,4d和6d(其中d是喷嘴的直径)进行测量,用于45度和26度的喷射冲击角(θ),并且上坡和下坡区域的流动特性是在Reynolds的2600(基于喷嘴直径D和喷射速度UO)上进行研究。观察到,在壁射流方面,表面间距在上坡和下坡区域具有相反的效果。在上坡区域中,壁射流的趋势随着L / D的增加而增加。然而,在下坡区域中,观察喷射速度及其厚度以减少随着分离距离而减少。由于上坡区域中的喷射环境流体相互作用,观察到停滞点和几何中心之间的距离以随着L / D的增加而降低。由于增强的射流环境流体相互作用,观察到喷射宽度在板的下游生长= 45度。 Theta = 26度的流程表明,在冲击后,整个射流朝向下坡侧偏离,这表明存在临界撞击角的存在下,在上坡区域中没有喷射流动的流动。 RMS速度波动和剪切应力示出了下坡区域中板下游下游的湍流水平,以较小的撞击距离,这意味着更高的喷射环境流体相互作用和增加的喷射宽度。与负湍流生产术语一起,揭示了流动分离和重新附着的区域。 NUSERET数的峰值的减小可以与滞留点的喷射动量的下降有关,随着表面间隔的增加。

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