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EXPERIMENTAL INVESTIGATIONS OF THE INFLUENCE OF WATER DROPLETS IN COMPRESSOR CASCADES

机译:水滴在压缩机级联水滴影响的实验研究

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This paper presents first results of experiments in a two-phase-flow cascade wind-tunnel. A Phase-Doppler-Anemometry system is used to measure velocity and water droplet-sizes in a compressor cascade. The local velocity with water injected is slower than the air flow without water injection due to droplet inertia and loss of momentum. Ligament formation and breakup caused by Rayleigh-Taylor instabilities is observed at the trailing edge resulting in particle sizes between 20 μm and 30 μm independent of flow velocity and the size of the nozzle used for water injection. Another region in the last third of the suction side is found, where a separation of droplets below 10 μm occurs. A change in flow angle at the cascade outlet is observed depending on water-load and droplet-size in the inlet.
机译:本文介绍了两相流级联风洞中的首先实验结果。相位多普勒 - 气管系统用于测量压缩机级联中的速度和水滴尺寸。由于液滴惯性和动量损失,注入的水的局部速度比空气流量慢慢。在雷格利泰勒不稳定性引起的韧带形成和分解在后缘,导致粒度为20μm和30μm,与用于注水的喷嘴的尺寸无关。找到吸入侧的最后三分之一的另一个区域,其中发生低于10μm以下的液滴的分离。根据入口中的水载和液滴尺寸观察到级联出口处的流动角的变化。

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