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An Experimental Investigation on Spray Characteristics Emanating from Liquid-Liquid Coaxial Swirl Atomizer

机译:液液同轴旋流雾化器喷雾特性的实验研究

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Liquid fuel/oxidizer atomization is extensively used in rocket engines for exploiting their high mixing efficiency. An experimental investigation is performed to explore the characteristics of sprays produced by a liquid-liquid coaxial swirl atomizer in a non-combusting environment. Investigation data will be used to correlate between liquid properties, atomizer geometric dimension, and atomization spray characterization. The idea is design the atomizer, fabricate, cold flow test and analyze the result. This atomizer is divided into two parts which is the inner atomizer and the outer atomizer. There also has two liquid inlet points where one inlet is meant for inner nozzle while the other inlet is meant for the outer nozzle. Two water supplies of the same kind will be supplied into the atomizer. As compared to basic conventional atomizer design, this atomizer sprays two liquid simultaneously at different angles and different swirl directions, but at the same axis. In this paper, it described the characteristics of spray for outer and inner atomizer. As the result, it was found that the outer atomizer have high value of spray cone angle compared to inner atomizer.
机译:液体燃料/氧化剂雾化广泛用于火箭发动机,用于利用它们的高混合效率。进行实验研究以探讨液 - 液同轴旋流雾化器在非燃烧环境中产生的喷雾特性。调查数据将用于液体性质,雾化器几何尺寸和雾化喷涂表征之间的相关性。该思想是设计雾化器,制造,冷流量测试并分析结果。该雾化器分为两部分,是内雾化器和外雾化器。还有两个液体入口点,其中一个入口用于内喷嘴,而另一个入口是用于外喷嘴的。同一种类的两种供水将被提供给雾化器。与基本的常规雾化器设计相比,该雾化器以不同的角度和不同的旋流装置同时喷射两个液体,但是在相同的轴上。本文描述了外部和内雾化器喷雾的特性。结果,发现外雾剂与内雾化器相比具有高值的喷雾锥角。

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