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Hydraulic Characteristics of Liquid Film Generated by Slit Injector

机译:狭缝喷射器产生的液体膜的液压特性

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Liquid film generated by a jet slit injector on a wall was analyzed experimentally. Liquid film characteristics were investigated by measuring the liquid film thickness distribution for various experimental conditions. At first, the distributions were qualitatively analyzed using backlight imaging. Furthermore, quantitative measurements were performed using a liquid film thickness sensor based on the electric conductance method, which was applied to the high-speed wire-mesh method. The injection angle (15, 30, 45 degrees), jet velocity (7, 10.5, 13.5m/s), and injection distance (45, 55, 65mm) were varied, and the responses of the liquid film were observed. Having increased the injection angle, the main stream thickness decreased and the position of the maximum film thickness moved upstream. A faster jet velocity corresponded to a wider liquid film area and larger perturbation of the liquid film. The injection distance did not affect the characteristics of the liquid film considerably. A hydraulic jump effect was also observed, and a large hydraulic jump affected the film thickness distribution of the main stream. The results of this study can be applied to the development of liquid rocket engines or thrusters using the film-cooling method.
机译:通过实验分析由墙壁上的喷射狭缝喷射器产生的液体膜。通过测量各种实验条件的液膜厚度分布来研究液膜特性。首先,使用背光成像进行定性分析分布。此外,使用基于电导法的液体膜厚度传感器进行定量测量,该电导法施加到高速线网格方法。改变注射角(15,30,45度),喷射速度(7,10.5,13.5m / s)和注射距离(45,55,65mm),并且观察到液体膜的响应。增加了注射角度,主流厚度降低,并且最大膜厚度的位置移动上游。更快的射流速度与较宽的液体膜面积相对应,液体膜的较大扰动。注射距离显着影响液体膜的特性。还观察到液压跳跃效果,大的液压跳跃影响了主流的膜厚度分布。该研究的结果可以应用于使用薄膜冷却方法的液体火箭发动机或推进器的开发。

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