文章基本信息

标题：Aerodynamic Characteristics of Multi-Element Iced Airfoil – CFD Simulation
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作者：A. Hyll ; V. Horák
期刊名称：Advances in Military Technology
印刷版ISSN：1802-2308
电子版ISSN：2533-4123
出版年度：2013
卷号：8
期号：1
语种：English
出版社：University of Defence
摘要：The phenomenon of the in-flight icing can affect all types of aircraft. Presence of the ice accretion on wings can lead to performance degradation. Thus,it is important to understand how the different ice shapes affect aerodynamic characteristics. The prediction of the ice accretion on the wing with flaps of different position was made by the in-house code ICE 4.1. The two-dimensional CFD simulation was used for the study of aerodynamic performance degradation of multi-element iced airfoil. The results are discussed and some of them are compared with the wind tunnel testing.
关键词：Aerodynamics;aircraft icing;performance degradation