Experimental Studies of Ice Crystal Accretion on an Axisymmetric Body at Engine-Realistic Conditions

Alexander Bucknell, M. McGilvray, D. Gillespie, Geoffrey Jones, Alasdair Reed, Benjamin Collier
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引用次数: 17

Abstract

It has been recognised in recent years that high altitude atmospheric ice crystals pose a threat to aircraft engines in flight. Instances of damage, surge and shutdown have been recorded at altitudes significantly greater than those associated with supercooled water icing. It is believed that ice particles can accrete inside the core compressor, although the exact mechanism by which this occurs remains poorly understood. In order to model ice crystal accretion, an estimate of the proportion of the impinging ice and water that sticks to a surface (the ‘sticking efficiency’) is required. This is believed to be dependent upon a number of parameters including particle melt ratio and diameter, and surface condition (rough or smooth, dry or wetted, warm or cold). This paper presents data from experiments undertaken in the National Research Council of Canada’s (NRC) Research Altitude Test Facility (RATFac). An axisymmetric test article, which featured three interchangeable cone ‘noses’ of varying half-angle, was used over a period of two weeks. A 35° half-angle nose was used for a parametric study of Mach number, Total Water Content (TWC), wet bulb temperature and particle size distribution (PSD). At selected test conditions, 20° and 45° half-angle noses were also tested. An assessment of the response of the Science Engineering Associates WCM-2000 multiwire probe in glaciated condition is presented, as a function of TWC, particle size and Mach number. A shadowgraphy technique was used to measure the ice accretion growth rate on the nose, with isometric camera views for qualitative assessments of spatial uniformity and build/shed events. The results show that sticking efficiency has a strong dependency on particle melt ratio, with maximum values attained when melt is typically between 9-13%. Erosion is shown to be correlated with particle size, Mach number and surface angle. New semi-empirical models are presented for sticking probability and erosion.
轴对称体上冰晶吸积的实验研究
近年来,人们已经认识到高空大气中的冰晶对飞行中的飞机发动机构成威胁。损坏、浪涌和停机的情况在海拔高度的记录明显高于与过冷水结冰相关的情况。据信,冰粒可以在核心压缩器内积聚,尽管这种情况发生的确切机制尚不清楚。为了模拟冰晶的吸积,需要估计碰撞的冰和水粘在表面上的比例(“粘滞效率”)。这被认为取决于许多参数,包括颗粒熔化比和直径,以及表面状况(粗糙或光滑,干燥或潮湿,温暖或寒冷)。本文介绍了在加拿大国家研究委员会(NRC)研究高度测试设施(RATFac)进行的实验数据。在两周的时间里,使用了一个轴对称测试件,它的特点是三个可互换的半角锥形“鼻子”。采用35°半角机头对马赫数、总含水量(TWC)、湿球温度和粒径分布(PSD)进行参数化研究。在选定的试验条件下,还对20°和45°半角鼻进行了试验。对WCM-2000型多线探针在冰川条件下的响应进行了评估,并将其作为TWC、粒径和马赫数的函数。使用阴影成像技术来测量鼻子上的冰堆积增长率,并使用等距相机视图对空间均匀性和建造/脱落事件进行定性评估。结果表明,粘接效率与颗粒熔体比有很强的相关性,当熔体比在9-13%之间时达到最大值。侵蚀与颗粒大小、马赫数和表面角度有关。提出了新的粘着概率和侵蚀的半经验模型。
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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