在失重状态下注入液体:液滴或间歇泉的形成

S. Collicott, K. D. Kennedy
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引用次数: 0

摘要

在失重状态下向充满气体的容器中注入液体会导致至少两种情况-液滴附着在注射孔周围的壁上,以及液体以连续射流的形式从孔中传播出去。在零重力流体研究几何和航天系统中,都需要设计液体注入来满足一种或另一种条件。其他人先前的实验假设注射孔的边缘是锋利的。本文研究了抛物飞行器失重状态下的倒角孔和圆形孔中液体的流出。与以往的研究结果相比,结果表明,倒角和圆形边缘对划分壁面液滴和间歇泉行为的韦伯数值的影响很小。由于任何制造的孔口都具有有限的钝度,因此这一结论对研究和航天系统都是有用的。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Injecting a Liquid in Weightlessness: Droplet or Geyser Formation
Abstract Injecting a liquid into a gas-filled vessel while in weightlessness can result in at least two conditions–a droplet attached to the wall around the injection orifice and a geyser in which the liquid propagates away from the orifice in a continuous jet. The need to design injection of liquid to accomplish one condition or the other shows up in both zero-g fluids research geometries and spaceflight systems. Previous experiments by others assumed the rim of the injection orifice to be sharp. Liquid flow out of orifices with chamfered and rounded rims during the weightlessness of parabolic aircraft flight are studied in this work. When compared to previous work, results indicate that chamfered and rounded rims have little effect on the value of Weber number dividing the wall-bound droplet and geyser behaviors. Because any manufactured orifice will have finite bluntness, this conclusion is useful for both research and spaceflight systems.
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