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Digital Holographic Analysis of the Near Field of Aerated-Liquid Jets in Crossflow

机译:横流中气液射流近场的数字全息分析

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摘要

Inline digital holographic microscopy is used to study the rapidly developing region near the injector of several sprays in subsonic crossflow. Pure liquid jets are compared to aerated-liquid jets for crossflow Mach numbers of 0.3 and 0.6. Gas-to-liquid ratios of 0,4, and 8% with a fixed momentum flux ratio (based on liquid flow rate) of 10 are investigated. Three-dimensional representations of the present test cases of aerated injection in crossflow are produced for the first time for the rapidly developing near-injector region (15-25 injector diameters downstream) owing to the capability of holographic diagnostics in probing nonspherical droplets typical of those present in this region. The results are also presented for the stable far-field region of the injector (at 50 and 100 injector diameters downstream). The results include droplet equivalent-diameter distributions, Sauter mean diameter distributions, and droplet velocities.
机译:在线数字全息显微镜用于研究亚音速错流中几种喷雾的喷射器附近快速发展的区域。将纯液体射流与充气液体射流进行比较,得出错流马赫数为0.3和0.6。研究了固定动量通量比(基于液体流速)为10的气液比0.4和8%。由于全息诊断具有探测典型的非球形液滴的能力,因此对于快速发展的近注入器区域(下游15-25注入器直径)首次产生了横流加气注入当前测试案例的三维表示。目前在该地区。还显示了稳定的喷油器远场区域(下游50和100喷油器直径)的结果。结果包括液滴等效直径分布,Sauter平均直径分布和液滴速度。

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  • 来源
    《Journal of propulsion and power》 |2014年第6期|1636-1645|共10页
  • 作者单位

    Oklahoma State University, Stillwater, Oklahoma 74078;

    Oklahoma State University, Stillwater, Oklahoma 74078;

    Taitech, Inc., Beavercreek, Ohio 45433;

    U.S. Air Force Research Laboratory, Wright-Patterson Air Force Base, Ohio 45433;

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  • 正文语种 eng
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