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Behavior of a Horizontal Gas-Liquid Two-Phase Flow under Microgravity (Flow pattern and Film Construction in Annular Flow Region)

机译:微重力下水平气液两相流的行为(环形流动区域的流型和薄膜结构)

摘要

In order to predict various phenomena related to flow and heat transfer in space,it is necessary to carry out experiments under microgravity. In this paper,we describe the behavior of a horizontal two-phase flow under microgravity utilizing a drop tower 6.1m in height,which realizes microgravity conditions of less than 0.02G(G=g/go)for about one second when the capsule is falling down. The experiment was carried out in a horizontal transparent acrylic resin tube of 10mm I.D. and 250mm length,using Freon-22 and water as the working fluid,in a superficial gas velocity range of 0.021m/s to 5.05m/s(ReG=58ï½ 1.4Ã 10^4)and a superficial water velocity of 0.022m/s to 0.456m/s(ReL=246ï½ 5.1Ã 10^3). The flow patterns obtained under microgravity were compared with other data under actual microgravity utilizing a drop tower. Furthermore,the base liquid film thickness,the height of waves and the period of waves in the region of annular flow,were obtained from a measured shape of waves. Then,the relationship between these values,gas Reynolds number and liquid film Reynolds number was obtained. Also,the void fraction under microgravity could be expressed using the distribution parameter and the Martinelli parameter.
机译:为了预测与空间中的流动和热传递有关的各种现象,有必要在微重力下进行实验。在本文中,我们描述了利用高度为6.1m的下降塔在微重力作用下水平两相流的行为,当胶囊处于水平状态时,该过程实现了小于0.02G(G = g / go)的微重力条件约一秒钟。掉下来。实验在内径为10mm的水平透明丙烯酸树脂管中进行。长度为250mm,使用Freon-22和水作为工作流体,表观气速范围为0.021m / s至5.05m / s(ReG = 58×1/2 1.4×10 ^ 4),表观水速为0.022m / s s至0.456m / s(ReL = 246×1/2 5.1×10 ^ 3)。利用滴塔将在微重力下获得的流动模式与实际微重力下的其他数据进行比较。此外,从测量的波浪形状获得基础液体膜的厚度,波浪高度和在环形流动区域中的波浪周期。然后,得到这些值,气体雷诺数和液膜雷诺数之间的关系。同样,微重力下的空隙率可以用分布参数和马丁内利参数表示。

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