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射流撞壁形成液膜的形态和厚度试验

袁韦韦 黄勇 章宏宙 黎露

袁韦韦, 黄勇, 章宏宙, 等. 射流撞壁形成液膜的形态和厚度试验[J]. 航空动力学报, 2022, 37(11):2524-2533 doi: 10.13224/j.cnki.jasp.20220232
引用本文: 袁韦韦, 黄勇, 章宏宙, 等. 射流撞壁形成液膜的形态和厚度试验[J]. 航空动力学报, 2022, 37(11):2524-2533 doi: 10.13224/j.cnki.jasp.20220232
YUAN Weiwei, HUANG Yong, ZHANG Hongzhou, et al. Experiment on shape and thickness of liquid film formed by impinging jets on solid walls[J]. Journal of Aerospace Power, 2022, 37(11):2524-2533 doi: 10.13224/j.cnki.jasp.20220232
Citation: YUAN Weiwei, HUANG Yong, ZHANG Hongzhou, et al. Experiment on shape and thickness of liquid film formed by impinging jets on solid walls[J]. Journal of Aerospace Power, 2022, 37(11):2524-2533 doi: 10.13224/j.cnki.jasp.20220232

射流撞壁形成液膜的形态和厚度试验

doi: 10.13224/j.cnki.jasp.20220232
详细信息
    作者简介:

    袁韦韦(1992−),男,博士生,主要从事液膜流动及其稳定性研究。E-mail:BY1904059@buaa.edu.cn

    通讯作者:

    黄勇(1964−),男,教授、博士生导师,博士,主要从事燃油雾化及燃烧室点火熄火机理研究。E-mail:yhuang@buaa.edu.cn

  • 中图分类号: V434+.3

Experiment on shape and thickness of liquid film formed by impinging jets on solid walls

  • 摘要:

    为了研究射流撞壁形成液膜的主要特征,采用基于紫外线发光二极管灯-诱导荧光法(UVLED-induced fluorescence,LEDIF)和高速相机的测试方法对液膜形状和厚度进行了实验研究。结果表明,曲面和平面液膜长度和宽度均随射流速度增加而增加。随着气流速度增加,平面和曲面液膜均长度增加,宽度都减小。随着壁面曲率半径的增加,液膜宽度稍有增加,而液膜长度增加较为明显。随着射流速度的增加,平面和曲面液膜厚度整体上都逐渐减小。而当射流速度进一步增加时,转捩现象开始出现,此时液膜厚度均会迅速增加。曲面液膜的转捩临界速度为19.10~25.08 m/s,而平面液膜转捩速度约为25.08~35.92 m/s。随着气流速度的增加,平面液膜厚度逐渐减小,而曲面液膜厚度在x=0~55 mm时随气流速度增加而增加,在x>55 mm时随气流速度增加而减小。对不同的曲率半径,液膜厚度沿Ψ1圆周方向呈“W”形,而随着曲率半径的增加,“W”逐渐变得扁平,但是位于中间( Ψ1=0°)的厚度基本不变。

     

  • 图 1  试验装置示意图

    Figure 1.  Schematic diagram of the experimental device

    图 2  试验测试方法原理示意图

    Figure 2.  Schematic diagram of the principle of the test method

    图 3  光强-厚度标定示意图

    Figure 3.  Schematic diagram of light intensity- thickness calibration

    图 4  测试方法处理流程

    Figure 4.  Process of the measurement method

    图 5  典型斜射流撞壁液膜图像

    Figure 5.  Typical image of the liquid film formed by oblique jets impinging on a wall

    图 6  射流速度对平面液膜形态的影响

    Figure 6.  Effect of the jet velocity on the shape of the flat wall liquid film

    图 7  射流速度对曲面液膜形态的影响(R=30 mm)

    Figure 7.  Effect of the jet velocity on the shape of the curved wall liquid film (R=30 mm)

    图 8  横向气流速度对平面液膜形态的影响(U0=13.2 m/s)

    Figure 8.  Effect of the airflow velocity on the shape of the flat wall liquid film (U0=13.2 m/s)

    图 9  横向气流速度对曲面液膜形态的影响(U0=13.2 m/s,R=30 mm)

    Figure 9.  Effect of the airflow velocity on the shape of the curved wall liquid film (U0=13.2 m/s, R=30 mm)

    图 10  曲率半径对曲面液膜形态的影响 (U0=13.2 m/s)

    Figure 10.  Effect of the radius of curvature on the shape of the curved wall liquid film ( U0=13.2 m/s)

    图 11  射流速度对平面液膜厚度的影响(α=30°)

    Figure 11.  Effect of the jet velocity on the thickness of the flat wall liquid film (α=30°)

    图 12  射流速度对曲面液膜厚度的影响(R=30 mm)

    Figure 12.  Effect of the jet velocity on the thickness of the curved wall liquid film (R=30 mm)

    图 13  气流速度对平面液膜厚度的影响

    Figure 13.  Effect of the airflow velocity on the thickness of the flat wall liquid film

    图 14  气流速度对曲面液膜厚度的影响(R=30 mm)

    Figure 14.  Effect of the airflow velocity on the thickness of the curved wall liquid film (R=30 mm)

    图 15  曲率半径对曲面液膜厚度的影响(U0=13.2 m/s)

    Figure 15.  Effect of the radius of curvature on the thickness of the curved wall liquid film (U0=13.2 m/s)

    表  1  试验参数及工况表

    Table  1.   Experimental parameters and test conditions

    序号Uair/(m/s)U0/(m/s)R/mm
    109.630, ∞
    2013.230, ∞
    3019.130, ∞
    4025.0830, ∞
    5035.9230, ∞
    61013.230, ∞
    72013.230, ∞
    83013.230, ∞
    94013.230, ∞
    105013.230, ∞
    11013.220
    12013.240
    下载: 导出CSV
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  • 收稿日期:  2022-04-22
  • 网络出版日期:  2022-09-09

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