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首页> 外文期刊>Journal of Heat Transfer >Experimental Investigation of Air-Water Mist Jet Impingement Cooling Over a Heated Cylinder
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Experimental Investigation of Air-Water Mist Jet Impingement Cooling Over a Heated Cylinder

机译:加热圆筒冷却冷却空气雾气喷射冲击的实验研究

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摘要

Experimental investigation on heat transfer mechanism of air-water mist jet impingement cooling on a heated cylinder is presented. The target cylinder was electrically heated and was maintained under the boiling temperature of water. Parametric studies were carried out for four different values of mist loading fractions, Reynolds numbers, and nozzle-to-surface spacings. Reynolds number, Re-hyd, defined based on the hydraulic diameter, was varied from 8820 to 17,106; mist loading fraction, f ranges from 0.25% to 1.0%; and nozzle-to-surface spacing, H/d was varied from 30 to 60. The increment in the heat transfer coefficient with respect to air-jet impingement is presented along with variation in the heat transfer coefficient along the axial and circumferential direction. It is observed that the increase in mist loading greatly increases the heat transfer rate. Increment in the heat transfer coefficient at the stagnation point is found to be 185%, 234%, 272%, and 312% for mist loading fraction 0.25%, 0.50%, 0.75%, and 1.0%, respectively. Experimental study shows identical increment in stagnation point heat transfer coefficient with increasing Reynolds number, with lowest Reynolds number yielding highest increment. Stagnation point heat transfer coefficient increased 263%, 259%, 241%, and 241% as compared to air-jet impingement for Reynolds number 8820, 11,493, 14,166, and 17,106, respectively. The increment in the heat transfer coefficient is observed with a decrease in nozzle-to-surface spacing. Stagnation point heat transfer coefficient increased 282%, 248%, 239%, and 232% as compared to air-jet impingement for nozzle-to-surface spacing of 30, 40, 50, and 60, respectively, is obtained from the experimental analysis. Based on the experimental results, a correlation for stagnation point heat transfer coefficient increment is also proposed.
机译:提出了一种加热圆筒的空气 - 水雾喷射冲洗冷却传热机理的实验研究。将目标气缸电加热,并在水的沸腾温度下保持。参数研究进行了四种不同值的雾装载分数,雷诺数和喷嘴到表面间隔。 Reynolds Number,基于液压直径定义的Re-Hyd,从8820到17,106变化;雾装载级分,F范围为0.25%至1.0%;和喷嘴到表面间隔,H / D从30到60变化。传热系数相对于空气喷射冲击的增量以及沿轴向和圆周方向的传热系数的变化呈现。观察到薄雾加载的增加大大增加了传热速率。在停滞点的热传递系数中递增,雾载荷分数为185%,234%,272%和312%,分别为0.25%,0.50%,0.75%和1.0%。实验研究表明,随着雷诺数的增加,停滞点传热系数在滞后点传热系数相同的增量,具有最低的雷诺数,产生最高的增量。与Reynolds 8820,11,493,14,166和17,106的空气喷射冲击相比,停滞点传热系数增加263%,259%,241%和241%。观察热传递系数的增量,随着喷嘴到表面间隔的降低。与实验分析中获得30,40,50和60的空气喷射冲击相比,停滞点传热系数增加282%,248%,239%和232%,从实验分析中获得。基于实验结果,还提出了对停滞点传热系数增量的相关性。

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