Experimental investigations and development of physico-mathematical model of an aerodynamic surface icing in air flow carrying droplets and crystals

The icing of aircraft parts during flight in mixed clouds (containing droplets and crystals) is one of important and, at the same time, insufficiently studied cases. In the present work, the effect of melting ratio on icing intensity of wing leading edge is experimentally studied. A physical and mat...

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Bibliographic Details
Published in:Journal of physics. Conference series 2020-06, Vol.1560 (1), p.12066
Main Authors: Zhbanov, V A, Kashevarov, A V, Miller, A B, Potapov, Yu F, Tokarev, O D, Stasenko, A L
Format: Article
Language:English
Subjects:
Air flow
Aircraft components
Aircraft icing
Aircraft parts
Crystals
Deposition
Droplets
Mathematical analysis
Mathematical models
Physics
Citations: Items that this one cites
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Summary:The icing of aircraft parts during flight in mixed clouds (containing droplets and crystals) is one of important and, at the same time, insufficiently studied cases. In the present work, the effect of melting ratio on icing intensity of wing leading edge is experimentally studied. A physical and mathematical model of crystals accretion on the surface due to their deformation and destruction is proposed.
ISSN:1742-6588
1742-6596
DOI:10.1088/1742-6596/1560/1/012066