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Heat transfer in two-component internal mist cooling Part I. Experimental investigation

机译:两组分内部雾冷却中的热传递第一部分。实验研究

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An experimental investigation was conducted to examine steady, internal, nozzle-generated, gas/liquid mist cooling in vertical channels. The ideal primary cooling mechanism in this situation is surface evaporation of an ultra-thin, subcooled liquid film that forms on the heated surface. The aim was to quantify the effects of various operating and design parameters on the cooling effectiveness. Parameters tested included the liquid atomization nozzle design, inlet flow condition (liquid mass fraction; carrier gas velocity, temperature and humidity; liquid temperature; liquid droplet size distribution; and gas/liquid combination), channel characteristics (cross-section geometry, length and surface wettability), and flow direction. Interest in this research has been motivated by the need for a highly efficient cooling mechanism in high-power lasers for inertial fusion reactor applications. A fully instrumented experimental test facility that included three cylindrical and two rectangular electrically heated test sections with different cross-sections and unheated entry lengths was used. The channel hydraulic diameters covered the range 16-26.7 mm, and the heated length-to-hydraulic-diameter ratio varied in the range from 23.3 to 51. Water was used as the mist liquid, with airorheliumas the carrier gas. Three types of mist generating nozzles with significantly different spray characteristics were used. Local heat transfer coefficients, defined based on the temperature difference between the heated surface and the bulk gas, were obtained along the channels for a wide range of operating conditions. The data indicate that mist cooling can increase the heat transfer coefficient by more than an order of magnitude compared to forced convection using only the carrier gas.
机译:进行了一项实验研究,以检查垂直通道内喷嘴产生的稳定的内部气/液雾冷却情况。在这种情况下,理想的一次冷却机制是在加热表面上形成的超薄,过冷的液膜的表面蒸发。目的是量化各种操作和设计参数对冷却效率的影响。测试的参数包括液体雾化喷嘴的设计,入口流量条件(液体质量分数;载气速度,温度和湿度;液体温度;液滴尺寸分布;以及气/液组合),通道特性(横截面几何形状,长度和表面润湿性)和流向。对惯性聚变反应堆应用的大功率激光器需要高效的冷却机制,激发了对该研究的兴趣。使用了一个设备齐全的实验测试设施,包括三个具有不同横截面和未加热入口长度的圆柱形和两个矩形电加热测试部分。通道的水力直径范围为16-26.7 mm,加热的长度与液压直径之比在23.3至51的范围内变化。使用水作为雾状液体,并以air气作为载气。使用具有明显不同的喷雾特性的三种类型的雾产生喷嘴。在宽范围的工作条件下,沿着通道获得了基于传热表面和散装气体之间的温差定义的局部传热系数。数据表明,与仅使用载气的强制对流相比,雾冷却可以将传热系数提高一个数量级以上。

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