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Convective heat transfer in supercritical flows of CO2 in tubes with and without flow obstacles

机译:在有和没有流动障碍的情况下,超临界CO2在管中的对流传热

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Heat transfer measurements to CO2-cooled tubes with and without flow obstacles at supercritical pressures were obtained at the University of Ottawa's supercritical pressure test facility. The effects of obstacle geometry (obstacle pitch, obstacle shape, flow blockage) on the wall temperature and heat transfer coefficient were investigated. Tests were performed for vertical upward flow in a directly heated 8 mm ID tube for a pressure range from 7.69 to 8.36 MPa, a mass flux range from 200 to 1184 kg/m(2) s, and a heat flux range from 1 to 175 kW/m(2). The results are presented graphically in plots of wall temperature and heat transfer coefficient vs. bulk specific enthalpy of the fluid. The effects of flow parameters and flow obstacle geometry on supercritical heat transfer for both normal and deteriorated heat transfer are discussed. A comparison of the measurements with leading prediction methods for supercritical heat transfer in bare tubes and for spacer effects is also presented. The optimum increase in heat transfer coefficient was found to be for blunt obstacles, having a large flow blockage, and a short obstacle pitch. (C) 2016 Elsevier B.V. All rights reserved.
机译:渥太华大学的超临界压力测试设备获得了在超临界压力下有无流动障碍的CO2冷却管的传热测量结果。研究了障碍物的几何形状(障碍物间距,障碍物形状,流动障碍)对壁温和传热系数的影响。在直接加热的8 mm内径管中进行垂直向上流动的测试,压力范围为7.69至8.36 MPa,质量通量范围为200至1184 kg / m(2)s,热通量范围为1至175千瓦/米(2)。结果以图形方式显示在壁温和传热系数与流体体积比焓的关系图中。讨论了流动参数和流动障碍物几何形状对正常和恶化传热的超临界传热的影响。还介绍了将测量结果与裸管中超临界传热和间隔效应的领先预测方法进行的比较。发现传热系数的最佳增加是针对钝的障碍物,具有大的流量阻塞和较短的障碍物间距。 (C)2016 Elsevier B.V.保留所有权利。

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