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Effect of the shape of flow confinement on turbulent slot jet impingement cooling of a heated circular cylinder

机译:流动限制形状对加热圆柱湍流槽喷射撞击的影响

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摘要

In this paper, details of experimental and numerical investigations carried out on slot jet impingement over a heated circular cylinder with and without a flow confinement have been presented. In this study, to enhance heat transfer rate in the rear side of the cylinder, circular, quadrilateral and hexagonal flow confinements with openings at the top and bottom of the confinements are used around the target cylinder. The Reynolds number, Re-D, defined based on the average velocity at the nozzle exit and the cylinder diameter, is varied from 6000 to 20000. The non-dimensional distance between the nozzle exit and the heated cylinder, H/S is varied in range of 2 = H/S = 12. The ratio of the cylinder diameter to the slot width, D/S = 8.5 is fixed in all the cases considered in the present study. The results of present study shows that the bottom surface of the cylinder is substantially cooled when flow confinement walls are used compared to the case of unconfined flow. The overall enhancement in the average Nusselt number over the heated cylinder due the quadrilateral and the hexagonal confinements is in the range of 20-42%.
机译:在本文中,已经介绍了在加热圆柱上的槽喷射冲击的实验和数值研究的细节,其具有和不具有流动限制的加热圆柱体。在本研究中,为了提高圆筒后侧的传热速率,在目标气缸周围使用围绕围绕和底部的开口的圆形,四边形和六边形流动限制。基于喷嘴出口处的平均速度和气缸直径的雷诺数Re-D可从6000到20000变化。喷嘴出口和加热圆筒之间的非尺寸距离,H / S变化2& h / s& = 12的范围。在本研究中考虑的所有情况下,汽缸直径与槽宽的比率为固定在槽宽度,d / s = 8.5。当前研究结果表明,当使用流量限制壁与非整合流动的情况相比,当使用流量限制壁时,汽缸的底表面基本上冷却。由于四边形和六边形约束的加热圆筒上的平均冲击数的整体增强在20-42%的范围内。

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