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Evaporation Characteristics of n-Heptane Droplet Streams in a Heated Air Channel Flow

机译:加热空气通道流动中正庚烷液滴流的蒸发特性

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An experimental study is presented on the evaporation of diluted droplet-laden two-phase jet flows within a heated air channel co-flow. In this study, n-heptane is pre-atomized by an ultrasonic nozzle to produce droplet cluster with a median diameter of about15μm, and a continuous cold air flow is applied to carry the fuel droplet cluster to emerge from a nozzle tube, producing a free turbulent jet of droplet stream. The droplet stream is then introduced as a central jet into a square-shaped channel with heated air co-flow for evaporation investigations. With flexibilities of the initial properties of droplet stream and surrounding conditions of channel flow, the axial evolution of droplet size is determined to characterize the evaporation behavior of n-heptane droplet stream under various boundary conditions. The equivalence ratios of droplet streams are varied by changing both the carrier-air flow rate and the fuel flow rate. The surrounding temperature of channel co-flow ranges from 40 °C to 240 °C using electrical air heater, and its turbulence intensity is varied by different perforated plate. The laser diffraction technique is employed to measure the droplet size distribution, and the axial evolution of SMD is derived and analyzed concerning the effects of the droplet stream properties and the surrounding channel co-flow conditions.
机译:提出了一种实验研究,蒸发在加热的空气通道混合内的稀释液滴两相射流的蒸发。在该研究中,通过超声喷嘴预雾化N-庚烷以产生具有约15μm的中值直径的液滴簇,并且施加连续的冷空气流量以携带燃料液滴簇从喷嘴管中出现,从而产生自由滴流滴流湍流。然后将液滴流引入中央射流中,进入方形通道,其具有加热的空气流量,用于蒸发研究。对于液滴流的初始性质和通道流动的周围条件的灵活性,确定液滴尺寸的轴向演化是在各种边界条件下表征正庚烷液滴流的蒸发行为。通过改变载体空气流速和燃料流速来改变液滴流的等效比。通道循环的周围温度使用电气加热器的40℃至240℃,其湍流强度由不同的多孔板变化。采用激光衍射技术来测量液滴尺寸分布,并且SMD的轴向演化是关于液滴流性质和周围通道的助流条件的效果的衍生和分析。

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