Preliminary Study of the Effects of Different Drag Laws on Ice Crystal Impingement on Probes Mounted on a Fuselage

A. Carozza, P. L. Vitagliano, G. Mingione
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Abstract

In this work, the effects of different drag laws regarding the ice crystal impingement on the fuselage of a regional aircraft are investigated. Different probes are considered on the surface of interest and simulated like simple segments normal to the fuselage. Along each of these instrumentations, the collection efficiency has been calculated by using a RANS structured solver named UZEN and an Eulerian impingement code IMP3D, both developed internally at CIRA. The solvers are parallelized and well-assessed. The computational grid has been generated with ICEM CFD. Results show the strong influence of the shape considered for the ice crystal particles and how different laws can guide different water concentrations on the probe surface.

Abstract Image

不同阻力定律对安装在机身上的探头上冰晶撞击效果的初步研究
在这项工作中,研究了不同阻力定律对冰晶撞击支线飞机机身的影响。我们考虑了相关表面上的不同探头,并将其模拟为与机身法线平行的简单线段。通过使用名为 UZEN 的 RANS 结构求解器和欧拉撞击代码 IMP3D(均由 CIRA 内部开发),计算了每个仪器的收集效率。这两个求解器都是并行化的,并经过良好评估。计算网格由 ICEM CFD 生成。结果表明,冰晶颗粒的形状对计算结果有很大影响,不同的规律可以引导探头表面不同的水浓度。
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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