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Experimental Investigation on Liquid Film Asymmetry in Air-Water Horizontal Annular Flow

机译:空水水平环形流动液膜不对称的实验研究

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The asymmetry of circumferential liquid film thickness distribution in an air-water horizontal annular flow has been experimentally investigated using superficial gas and liquid velocity of 10 - 40 m/s and 0.025 to 0.4 m/s, respectively. In general, the film at the bottom of the pipe will be thicker than that of the side and the top. The asymmetry parameter could be expressed in the ratio of average film thickness to the bottom film thickness or the ratio of the top-to-bottom film thickness. Measurement using compact multiple probe instrument shows that the circumferential film thickness distribution is strongly affected by superficial gas velocity. The higher gas velocity results in the more uniform liquid film circumferential distribution. In comparison to the existing correlations, the asymmetry parameter resulted from the experiment shows a good agreement. It is also shown from the experiment that a less symmetry of film thickness distribution is resulted when the gravity force is dominant. A more symmetry distribution is resulted when the inertial force takes control.
机译:使用浅表气体和10-40m / s和0.025至0.4m / s的浅表气体和液体速度来实验研究了空气水平环形流动中的周向液膜厚度分布的不对称。通常,管道底部的薄膜将比侧面和顶部的薄膜厚。不对称参数可以以平均膜厚度与底部膜厚度的比率或顶到底膜厚度的比率表示。使用紧凑型多探针仪的测量表明,圆周膜厚度分布受浅表气体速度的强烈影响。较高的气体速度导致更均匀的液体膜周向分布。与现有相关性相比,由实验引起的不对称参数显示出良好的一致性。从实验中也显示出薄膜厚度分布的较小对称性,导致重力力占主导地位。当惯性力控制时,导致更多对称性分布。

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