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Proceedings of the Institute for System Programming of the RAS, 2021, Volume 33, Issue 6, Pages 241–252
DOI: https://doi.org/10.15514/ISPRAS-2021-33(6)-17 (Mi tisp658) 		 
Development of the flagmanfoam solver for modeling aircraft icing in conditions of small droplet inflow

K. A. Vatutina, M. V. Kraposhina, M. A. Kudrovb, A. B. Millerc, V. G. Melnikovaad, S. M. Sautkinaad, A. O. Morozovb, A. A. Shevelyovad

a Ivannikov Institute for System Programming of the RAS
b Moscow Institute of Physics and Technology
c Central Aerohydrodynamic Institute
d Bauman Moscow State Technical University
Full-text PDF (660 kB)
DOI: https://doi.org/10.15514/ISPRAS-2021-33(6)-17
Abstract: This work is devoted to the creation of the flagmanFoam software package developed on the basis of the OpenFOAM v2012 package. A solver has been developed to simulate icing in conditions of small droplet in-flow, with a characteristic droplet size of up to 40 microns, which corresponds to Appendix C of the Aviation Regulations AP-25. Computational models implemented in the solver are presented: the Euler-Euler approach is used to describe the dynamics of a gas-droplet flow, the Myers thermodynamic model is used to describe the growth of a liquid film and ice, the Coupled Level Set - VoF method is used to move the interface, to take into account the interaction between liquid and body, the immersed boundary method is used, the turbulent viscosity is calculated using the k-w SST turbulence model. The results of modeling on test problems and comparison with experimental data are presented.
Keywords: icing, supercooled droplets, ice accretion, simulation, multiphase environment, surface.
Funding agency
The work is supported by ICE GENESIS project with financial support from the Ministry of Industry and Trade of the Russian Federation, unique project identifier 824310
Document Type: Article
Language: Russian
Citation: K. A. Vatutin, M. V. Kraposhin, M. A. Kudrov, A. B. Miller, V. G. Melnikova, S. M. Sautkina, A. O. Morozov, A. A. Shevelyov, “Development of the flagmanfoam solver for modeling aircraft icing in conditions of small droplet inflow”, Proceedings of ISP RAS, 33:6 (2021), 241–252
Citation in format AMSBIB
\Bibitem{VatKraKud21}
\by K.~A.~Vatutin, M.~V.~Kraposhin, M.~A.~Kudrov, A.~B.~Miller, V.~G.~Melnikova, S.~M.~Sautkina, A.~O.~Morozov, A.~A.~Shevelyov
\paper Development of the flagmanfoam solver for modeling aircraft icing in conditions of small droplet inflow
\jour Proceedings of ISP RAS
\yr 2021
\vol 33
\issue 6
\pages 241--252
\mathnet{http://mi.mathnet.ru/tisp658}
\crossref{https://doi.org/10.15514/ISPRAS-2021-33(6)-17}
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