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

机译:发动机真实条件下轴对称物体上冰晶沉积的实验研究

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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.
机译:近年来,已经认识到高海拔大气冰晶对飞行中的飞机发动机构成威胁。记录到的损坏,喘振和停机情况明显高于与过冷水结冰有关的高度。据信,尽管颗粒的确切机理仍知之甚少,但冰粒可能会在核心压缩机内部积聚。为了模拟冰晶的积聚,需要估算撞击在冰面上的水和冰的比例(“粘附效率”)。据信这取决于许多参数,包括颗粒熔体比率和直径,以及表面状况(粗糙或光滑,干燥或湿润,温暖或寒冷)。本文介绍了在加拿大国家研究委员会(NRC)研究海拔测试设施(RATFac)中进行的实验数据。在两个星期的时间内,使用了一个轴对称的测试文章,该文章具有三个可互换的半角不同的锥形“鼻子”。 35°半角鼻子用于马赫数,总含水量(TWC),湿球温度和粒度分布(PSD)的参数研究。在选定的测试条件下,还测试了20°和45°半角鼻。给出了在冰川条件下,Science Engineering Associates WCM-2000多线探针响应的评估,该评估是TWC,粒径和马赫数的函数。阴影摄影技术用于测量鼻子上积冰的增长率,等距相机视图用于对空间均匀性和建造/脱落事件进行定性评估。结果表明,粘着效率对颗粒熔体比率有很强的依赖性,当熔体通常在9-13%之间时,黏附效率达到最大值。侵蚀被证明与粒度,马赫数和表面角相关。提出了新的粘滞概率和侵蚀的半经验模型。

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