Asymmetric Heat Transfer in Aircraft Electrothermal Anti-Icing

نویسندگان

چکیده

Aircraft icing is an important cause of air disasters, and electrothermal anti-icing a common protection method. In this work, the influence meteorological conditions on was studied through wind tunnel experiment fairing. Based finite volume method, transient heat transfer calculation method for proposed. The calculated results were compared with experimental results, heating mode structure layout effect analyzed. show that are in good agreement shows obvious asymmetry. First, during heating, temperature gradient structural profile large, high concentrated layer, distribution layer relatively uniform. During cooling, more uniform, mainly back conduction outer wall increases first then decreases from center to surroundings. Second, when spray turned on, significantly reduced, but hardly changes. Third, uniform can simultaneously raise reduce layer. Fourth, while front affect wall, small. However, one be used control finely.

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ژورنال

عنوان ژورنال: Symmetry

سال: 2023

ISSN: ['0865-4824', '2226-1877']

DOI: https://doi.org/10.3390/sym15030599