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Influence of jet-jet interaction on droplet size and jet instability in immiscible liquid-liquid system

机译:不可混溶液液系统中射流相互作用对液滴尺寸和射流不稳定性的影响

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This work investigates the effects of multiple jet interactions and single jet instability on jet breakup and droplet size using experimental and computational techniques. In particular, the jet separation distance, jet breakup length and droplet diameter were measured as a function of initial nozzle separation distance and jet volumetric flow rate. It was found that the two jets moved closer to each other to reach an equilibrium separation distance that was approximately 70% of the spacing between the two nozzles. The distance at which the instabilities were first observed on the surface of the jet was also a function of the initial separation distance. However, it was weakly dependent on the jet velocity. The jet breakup length and resultant droplet diameter were both influenced by flow rate and nozzle separation distance. The jet breakup length was found to decrease with reduction in nozzle spacing at the high flow rates. Interestingly, a linear relationship between droplet diameter and breakup length was found that was largely independent of nozzle spacing and consist with conventional Rayleigh jet breakup theory. The implications of the experimental observations on the design of multi jet systems are discussed. Furthermore, computational fluid dynamics simulations were also used to identify the mechanism and dynamics of jet instability in the single jet systems. The simulation results were analysed to study the effect of instability on various parameters such as jet breakup, droplet formation and size of emulsion droplets, It was found that at higher volumetric flow rates, the droplets size increased during the jet breakup due to an asymmetric instability. The asymmetric instability was caused by the pressure gradient in the continuous phase and was prevented in double jet systems. (C) 2014 Elsevier Ltd. All rights reserved.
机译:这项工作使用实验和计算技术研究了多次射流相互作用和单次射流不稳定性对射流破裂和液滴尺寸的影响。特别地,根据初始喷嘴分离距离和喷射体积流量来测量喷射分离距离,喷射破碎长度和液滴直径。发现两个喷嘴彼此靠近,以达到平衡分离距离,该距离约为两个喷嘴之间间距的70%。第一次在喷射流表面观察到不稳定性的距离也是初始分离距离的函数。但是,它几乎不依赖于射流速度。射流的破裂长度和所得的液滴直径均受流速和喷嘴分离距离的影响。发现在高流速下,随着喷嘴间距的减小,射流破裂长度减小。有趣的是,发现液滴直径与破碎长度之间的线性关系在很大程度上与喷嘴间距无关,并且与传统的瑞利射流破碎理论一致。讨论了实验观察对多喷嘴系统设计的影响。此外,还使用计算流体动力学模拟来确定单喷嘴系统中喷嘴不稳定的机理和动力学。分析了仿真结果以研究不稳定性对各种参数的影响,如射流破裂,液滴的形成和乳液液滴的尺寸,发现在较高的体积流量下,由于不对称的不稳定性,液滴尺寸在射流破裂期间增加了。不对称的不稳定性是由连续相中的压力梯度引起的,在双喷系统中可以避免这种不稳定性。 (C)2014 Elsevier Ltd.保留所有权利。

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