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Proceedings of the Institute for System Programming of the RAS, 2017, Volume 29, Issue 6, Pages 271–288
DOI: https://doi.org/10.15514/ISPRAS-2017-29(6)-17 (Mi tisp287) 		 
Software package to calculate the aerodynamic characteristics of aircrafts

V. N. Koterovab, V. M. Krivtsovba, V. I. Zubovab

a Dorodnicyn Computing Centre FRC CSC RAS
b Moscow Institute of Physics and Technology (State University)
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DOI: https://doi.org/10.15514/ISPRAS-2017-29(6)-17
Abstract: The software package to calculate parameters of three-dimensional steady and unsteady gas flows in complex devices is presented. The mathematical flow model used in package is based on the Reynolds-averaged Navier Stokes equations for a two-component equilibrium turbulent medium and a two-parameter semiempirical turbulence model. A numerical implementation of the software package to modelling three complex flows in modern devices is described.
Keywords: software package, mathematical simulation, gas flows, turbulence, exhaust jet, Navier Stokes equations, aircraft nozzle.
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Document Type: Article
Language: English
Citation: V. N. Koterov, V. M. Krivtsov, V. I. Zubov, “Software package to calculate the aerodynamic characteristics of aircrafts”, Proceedings of ISP RAS, 29:6 (2017), 271–288
Citation in format AMSBIB
\Bibitem{KotKriZub17}
\by V.~N.~Koterov, V.~M.~Krivtsov, V.~I.~Zubov
\paper Software package to calculate the aerodynamic characteristics of aircrafts
\jour Proceedings of ISP RAS
\yr 2017
\vol 29
\issue 6
\pages 271--288
\mathnet{http://mi.mathnet.ru/tisp287}
\crossref{https://doi.org/10.15514/ISPRAS-2017-29(6)-17}
\elib{https://elibrary.ru/item.asp?id=32309080}
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