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Flow regime identification in microgravity two-phase flows using void fraction signals

机译:利用空隙率信号识别微重力两相流中的流态

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A concave parallel plate capacitance sensor has been developed to measure the two-phase flow void fraction for the purpose of objectively identifying flow regimes. The sensor has been used in conjunction with a two-phase flow loop onboard the NASA Lewis DC-9 microgravity aircraft, and data was recently collected. The void fraction time trace and probability density function, along with high speed video images of the flow were used to determine a more objective method of flow regime identification than what is possible through examination of video images alone. A set of criteria was developed to allow the identification of the flow regimes and their transitions through the examination of the void fraction probability density function. Against these criteria, flow regime transition models in the literature for microgravity gas-liquid two-phase flows were evaluated.
机译:为了客观地识别流动状态,已经开发了凹面平行板电容传感器来测量两相流动空隙率。该传感器已与NASA Lewis DC-9微重力飞机上的两相流回路配合使用,并且最近已收集了数据。与单独检查视频图像相比,无效分数时间轨迹和概率密度函数以及该流的高速视频图像可用于确定一种更客观的流态识别方法。开发了一组标准,以允许通过检查空隙率概率密度函数来确定流态及其过渡。根据这些标准,评估了文献中微重力气液两相流的流态转换模型。

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