Simultaneous Ultra-Small-Angle X-Ray Scattering and X-Ray Transmission Measurements of a Liquid Jet in Crossflow With Film Atomization

Brandon A. Sforzo, J. Ilavsky, C. Powell
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Abstract

Aircraft atomizers generally rely on multiple physical phenomena to introduce, distribute, and mix liquid fuel with the continuous air flow. Many such devices use plain jets for high liquid flow rates and film shear atomization to encourage droplet formation. To further characterize the near-field of processes, experiments were conducted to examine multiphase development of a liquid jet issuing into a subsonic crossflow. The jet impinged on a wall and the liquid subsequently filmed and convected downstream until reaching the end of the splitter plate, where it broke up by shear forces. X-ray diagnostics were used to interrogate different regions of the flow at the Advance Photon Source at Argonne National Laboratory 9-ID beamline. The projected liquid mass distribution was measured through x-ray absorption correlations using the collimated beam. The light was conditioned for Ultra-Small-Angle-X-ray-Scattering measurements, which were collected simultaneously with the transmission signal. These transmission and scattering signals were used to compute the projected mass and path-specific surface area of the spray, which were combined to calculate Satuer mean diameter. Though the transmission is typically collected using focused beam with a finer spatial resolution during a separate experimental campaign, the near-simultaneous acquisition allowed for more accurate registration between the signals and control of the operating condition. The transmission mapping confirmed the liquid path length of the unbroken liquid jet issuing into the domain and the interaction point with the wall. The spreading and flowing of the liquid down the plate and shedding from the trailing edge of the plate revealed an order of magnitude greater liquid path length, indicating the spreading of the film. X-ray scattering results indicate surface wave formation on the liquid jet and the initial stripping of droplets from the column. Furthermore, the scattering was enhanced for droplets rebounding due to splashing from the plate. The combined signals were used to calculate the droplet diameters in the shear breakup region trailing the splitter plate. These combined measurements provide detailed breakup information to inform inputs required to initialize Lagrangian spray calculations, as well as validate high-fidelity atomization simulations.
膜雾化横流中液体射流的超小角x射线散射和x射线透射测量
航空雾化器一般依靠多种物理现象来引入、分配和混合液体燃料与连续气流。许多这样的装置使用纯射流来实现高液体流速和膜剪切雾化来促进液滴的形成。为了进一步表征近场过程,进行了实验来研究液体射流进入亚音速交叉流的多相发展。射流撞击壁面,液体随后形成薄膜并向下游流动,直到到达分离器板的末端,在剪切力的作用下破碎。在阿贡国家实验室9-ID光束线的先进光子源上,使用x射线诊断来询问流动的不同区域。通过准直光束的x射线吸收相关性测量了投影液体的质量分布。该光被用于超小角度x射线散射测量,该测量与传输信号同时收集。这些传输和散射信号用于计算喷雾的投影质量和路径比表面积,并将其结合计算土星平均直径。虽然传输通常是在单独的实验活动中使用具有更精细空间分辨率的聚焦光束收集的,但近乎同时的采集允许信号之间更精确的登记和操作条件的控制。透射图确定了喷流进入区域的液路长度以及与壁面的相互作用点。液体沿平板向下扩散和流动,以及从平板后缘脱落,表明液路长度增加了一个数量级,表明薄膜的扩散。x射线散射结果表明,液体射流表面波形成,液滴从柱中剥离。此外,由于溅射引起的液滴反弹增强了散射。利用组合信号计算剪切破碎区液滴直径。这些综合测量提供了详细的分解信息,为初始化拉格朗日喷雾计算所需的输入提供了信息,并验证了高保真的雾化模拟。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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