Unsteady thermodynamic computational fluid dynamics simulations of aircraft wing anti-icing operation

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University of Toronto, Toronto, Ont. M3H 5T6, Canada [1 ]
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Journal of Aircraft | 1600年 / 44卷 / 04期
关键词：
A three-dimensional unsteady thermodynamic simulation model is developed to describe the dynamic response of an aircraft wing anti-icing system. This computational fluid dynamics based model involves a complete wing segment including a thermal anti-icing bay inside the leading edge. The unsteady; integrated internal/external thermal flow simulation is presented with heat conductivity through the solid skin in a structured mesh. The calculated skin temperature results are satisfactory in their good match with flight test data. The presented research work indicates a strong potential of using computational fluid dynamics in dynamic wing anti-icing system model development and validation;
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Conference article (CA)
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页码：1113 / 1117
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