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Digital holographic diagnostics of aerated-liquid jets in a subsonic crossflow.

机译:亚音速错流中充气液体射流的数字全息诊断。

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Scope and method of study. Different methods of digital holography were investigated to determine their ability to measure the properties of a spray produced by an aerated-liquid jet. The chosen method was then used to observe the properties of the spray at different downstream locations. Different test conditions of: 1 mm and 0.5 mm injector exit diameters, 4% and 8% GLR, 25 and 50 jet diameters downstream, and jet-to-freestream momentum ratios of 0.74 and 4, were observed to determine their effects. The observations were made by producing maps of the Sauter mean diameter distribution throughout the spray, as well as volume fraction plots showing the concentration of the droplets within the spray.; Findings and conclusions. An aerated jet in crossflow was studied and it was found that digital holographic microscopy was the best method for resolving the smallest droplets within the spray. Using this technique Sauter mean diameter maps were produced and the different effects could be investigated. It was found that the gas-to-liquid mass flow rate ratio had the most effect on droplet sizes, and the SMD could be normalized by this film thickness to produce comparable SMD sizes across different test conditions. This was in contrast to the effect of jet diameter which had little effect on the spray. It was also found that the jet-to-freestream momentum ratio strongly affected the penetration height of the spray into the crossflow while having a small effect on the droplet sizes. Evidence of secondary breakup was also found between the two downstream locations. This evidence was the reduction in droplet sizes, and a study of the aerodynamic forces on the droplets in this area. It was found that at the 4% GLR conditions secondary breakup is likely occurring due to the larger droplets produced at this condition.
机译:研究范围和方法。研究了数字全息术的不同方法,以确定它们测量由充气液体射流产生的喷雾的性能的能力。然后使用选择的方法在不同下游位置观察喷雾的性质。观察到不同的测试条件:1 mm和0.5 mm的喷油器出口直径,4%和8%的GLR,下游的25和50的喷嘴直径以及0.74和4的自由流动量比,以确定它们的效果。通过产生整个喷雾中索特平均直径分布的图以及表示喷雾中液滴浓度的体积分数图来进行观察。结论和结论。对错流的充气射流进行了研究,发现数字全息显微镜是解决喷雾中最小液滴的最佳方法。使用此技术,可以生成Sauter平均直径图,并可以研究不同的影响。发现气液质量流速比对液滴尺寸影响最大,并且可以通过该膜厚将SMD标准化,以在不同测试条件下产生可比较的SMD尺寸。这与喷嘴直径的影响相反,后者对喷雾几乎没有影响。还发现射流与自由流的动量比强烈影响喷雾进入错流的渗透高度,同时对液滴尺寸影响很小。在两个下游位置之间也发现了二次破裂的证据。该证据是液滴尺寸的减小,以及对该区域上液滴的空气动力的研究。发现在4%GLR条件下,由于在此条件下产生较大的液滴,可能发生二次破裂。

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