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Matematicheskoe modelirovanie, 2024, Volume 36, Number 3, Pages 51–66
DOI: https://doi.org/10.20948/mm-2024-03-04 (Mi mm4541) 		 
Numerical simulation of 3D flow past an inlet model

B. N. Chetverushkin, V. E. Borisov, A. E. Lutsky, Ya. V. Khankhasaeva

Keldysh Institute of Applied Mathematics RAS
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DOI: https://doi.org/10.20948/mm-2024-03-04
Abstract: Numerical simulation of supersonic flow of viscous heat-conducting gas past an inlet model for various Mach numbers ($M = 4$ and $5$) and temperatures of the model surface was carried out on the basis of an unsteady Reynolds averaged Navier–Stokes equations system (URANS) with the Spalart–Allmaras (SA) and Menter’s (SST) turbulence model. Three-dimensional features of the flow and heat flux’s dependence on wall temperature were investigated. Comparison of simulation results with experimental data was carried out.
Keywords: engine inlet, RANS, SA, SST, isothermal wall, heat flux density.
Funding agency Grant number
Russian Science Foundation 22-11-00126
Received: 28.11.2023
Revised: 28.11.2023
Accepted: 04.12.2023
English version:
Mathematical Models and Computer Simulations, 2024, Volume 16, Issue 5, Pages 687–697
DOI: https://doi.org/10.1134/S2070048224700327
Document Type: Article
Language: Russian
Citation: B. N. Chetverushkin, V. E. Borisov, A. E. Lutsky, Ya. V. Khankhasaeva, “Numerical simulation of 3D flow past an inlet model”, Mat. Model., 36:3 (2024), 51–66; Math. Models Comput. Simul., 16:5 (2024), 687–697
Citation in format AMSBIB
\Bibitem{CheBorLut24}
\by B.~N.~Chetverushkin, V.~E.~Borisov, A.~E.~Lutsky, Ya.~V.~Khankhasaeva
\paper Numerical simulation of 3D flow past an inlet model
\jour Mat. Model.
\yr 2024
\vol 36
\issue 3
\pages 51--66
\mathnet{http://mi.mathnet.ru/mm4541}
\crossref{https://doi.org/10.20948/mm-2024-03-04}
\transl
\jour Math. Models Comput. Simul.
\yr 2024
\vol 16
\issue 5
\pages 687--697
\crossref{https://doi.org/10.1134/S2070048224700327}
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