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Whipping in gaseous flow focusing

机译:鞭打气流聚焦

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We study both theoretically and experimentally the whipping instability in axisymmetric gaseous flow focusing realized in a converging-diverging nozzle. The lateral oscillation of both the tapering meniscus and emitted jet is explained in terms of the global linear instability of the lateral mode with the azimuthal number m = 1. A comparison with previous experiments shows good agreement. The distance between the feeding capillary and the nozzle neck hardly affects the m = 1 stability limit for the conditions considered in those experiments. We analyze the influence of the nozzle shape on the parameter conditions leading to whipping. As the nozzle convergence rate (the inverse of the length over which the diameter reduction takes place) increases, the flow becomes more stable under m = 1 perturbations. The above results are in marked contrast with those of the axisymmetric mode m = 0. For the axisymmetric mode, the minimum flow rate increases with the nozzle convergence rate, while the capillary-to-neck distance has considerable influence on the jetting-to-dripping transition. We also conduct experiments with different nozzles and capillary-to-neck distances to examine the effect of those factors on the stability of the jetting regime. The experiments allow us to distinguish between absolute whipping, in which both the tapering meniscus and the emitted jet oscillate, and convective whipping, in which the jet oscillates while the meniscus remains practically steady. Absolute whipping is observed for water and 1-cSt silicone oil focused with the nozzle with the smallest convergence rate and capillary-to-neck distance. The increase of the liquid viscosity stabilizes the liquid meniscus, producing the transition from absolute to convective whipping. In the high-viscosity case, the oscillation of the emitted jet far away from the discharge orifice is considerably affected by the shape of the nozzle in front of its neck. In fact, the increase of the convergence rate and capillary-to-neck distance eliminates the convective whipping as well. The reduction of surface tension enhances absolute whipping. We explain the appearance of the two types of whipping in terms of the flow pattern induced by the nozzle shape in front of the neck. (C) 2020 Elsevier Ltd. All rights reserved.
机译:从理论上看,我们在理论上进行了研究,在轴对称气体流聚焦中实现在趋同的发散喷嘴中的轴对称气体流聚焦。锥形弯月面和发射射流的横向振荡是根据横向模式的全局线性不稳定性,方位角数m = 1。与先前实验的比较显示了良好的一致性。饲养毛细管和喷嘴颈之间的距离几乎不会影响那些实验中考虑的条件的M = 1稳定性极限。我们分析喷嘴形状对导致鞭打的参数条件的影响。随着喷嘴收敛速率(直径减少的长度的倒数)增加,流动在m = 1扰动下变得更稳定。以上结果与轴对称模式M = 0的标记对比度。对于轴对称模式,最小流速随着喷嘴收敛速率而增加,而毛细管 - 颈部距离对喷射到射击率具有相当大的影响滴水过渡。我们还通过不同的喷嘴和毛细管 - 颈部距离进行实验,以检查这些因素对喷射制度稳定性的影响。实验允许我们区分绝对鞭打,其中锥形弯月面和发射的射流振荡,以及对流搅打,其中喷射越振荡,而弯月面仍然稳定。对于水和1-CST硅油的绝对鞭打,其与喷嘴具有最小的收敛速度和毛细管至颈部距离。液体粘度的增加稳定了液体弯月面,从绝对到对流鞭期产生过渡。在高粘度的情况下,远离排放孔的发射射流的振荡受到其颈部前面的喷嘴形状的显着影响。事实上,收敛速率和毛细血管到颈部距离的增加消除了对流鞭打。表面张力的减少增强了绝对鞭打。我们在颈部前喷嘴形状引起的流动模式方面解释了两种类型的鞭打的外观。 (c)2020 elestvier有限公司保留所有权利。

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