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Supercooled Water Droplet Impingement and Icing Region Prediction on a Rotating Fan Blade

机译:旋转风扇叶片上的过冷水滴撞击和结冰区域预测

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Ice accretion on the aero-engine fan degrades the engine performance and even causes accidents, and the physical processes involved in ice accumulation on the rotating blade are complex and challenging. So developing high accuracy numerical method and simulating the icing process on the rotating fan blade is necessary and worth studying. In the present study, the flow field of transonic fan rotor67 was simulated and water impingement characteristic was obtained with ANSYS Fluent by the Eulerian approach. The impact region and collection efficiency of different median volume diameters were compared and analyzed. The heat transfer between air and water droplet was also considered to obtain the impingement temperature of water droplets. Results showed that the water droplet temperature in some regions exceeds the freezing point and icing will not occur in these regions. Combining the impingement region, droplet temperature, wall temperature and evaporating rate on the blade surface, the pressure side of the blade is divided into four parts. Features of these regions were analyzed and possible icing area was presented. The method proposed herein is suitable for the icing prediction of high speed rotating axial fans and provides guidance for further research.
机译:航空发动机风扇上积冰会降低发动机性能,甚至导致事故,而且旋转叶片上积冰所涉及的物理过程非常复杂且具有挑战性。因此,开发高精度数值方法并模拟旋转风扇叶片的结冰过程是必要的,值得研究。在本研究中,模拟了跨音速风扇转子67的流场,并通过欧拉方法利用ANSYS Fluent获得了水冲击特性。比较和分析了不同中值体积直径的撞击区域和收集效率。还考虑了空气和水滴之间的热传递以获得水滴的撞击温度。结果表明,某些区域的水滴温度超过冰点,并且在这些区域不会结冰。结合叶片表面的撞击区域,液滴温度,壁温和蒸发速率,将叶片的压力侧分为四个部分。分析了这些区域的特征,并提出了可能的结冰区域。本文提出的方法适用于高速旋转轴流风机的结冰预测,并为进一步研究提供指导。

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