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Title : CFD Analysis & Flow
Company : Fexilon Technologies
Date : 11-Mar-2012
Downloads : 11

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Icing alters the shape and surface characteristics of aircraft components, which results in altered aerodynamic forces and moments caused by air flow over those iced components. The typical effects of icing are increased drag, reduced stall angle of attack , and reduced maximum lift. In this analysis, the leading-edge and the piccolo type thermal anti-icing bay of an aircraft wing is simulated using computational fluid dynamics (CFD) for a range of inlet-temperatures and the flow-rates of the heating fluid.
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