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Digital Holographic Analysis of the Breakup of Aerated Liquid Jets in Supersonic Crossflow

机译:超声交叉流动液体喷气机分解的数字全息分析

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Inline digital holographic microscopy is used to study the spray structure in the near-injector region of three different injectors in supersonic crossflow. Aerated liquid jets at different gas-to-liquid ratio (by mass) are compared to pure liquid jets for a crossflow Mach number of 2. Three-dimensional representations of the present test cases of aerated injection in supersonic crossflow are produced for the first time for the rapidly developing, near-injector region, owing to the capability of holographic diagnostics in probing non-spherical droplets (typical of 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 distributions of droplet equivalent-diameter and Sauter mean diameter, droplet velocities, spray penetration height, and plume width.
机译:内联数字全息显微镜用于研究超声波横流的三种不同注射器的近喷射器区域中的喷雾结构。将不同的气体与液体比(按质量)不同的液体喷射器与纯液体喷射进行比较,用于十字草马赫的纯液体喷射器2.第一次产生超声波横向流中的空气喷射注射的本试验情况的三维表示对于快速发展的近喷射器区域,由于全息诊断在探测非球形液滴(典型的该区域)中的能力。结果还呈现用于喷射器的稳定,远场区域(在下游50和100喷射器直径)。结果包括液滴等效直径和燃烧器平均直径,液滴速度,喷涂渗透高度和羽流宽度的分布。

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