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This article is cited in 1 scientific paper (total in 1 paper)
Numerical simulation of gas flows around aircraft with allowance for the flow/exhaust jet interaction
D. A. Zabarkoa, V. I. Zubovbc, V. P. Koteneva, V. M. Krivtsovcb, Yu. A. Polezhaeva a Research and Production Association of Machine Constructing, ul. Gagarina 33, Reutov, Moscow oblast, 143966, Russia
b Dorodnicyn Computing Center, Federal Research Center "Computer Science and Control" of Russian Academy of Sciences, ul. Vavilova 40, Moscow, 119333, Russia
c Moscow Institute of Physics and Technology, Institutskii per. 9, Dolgoprudnyi, Moscow oblast, 141700, Russia
Abstract:
Three-dimensional steady gas flow around aircraft in the presence of an exhaust jet are considered. The mathematical flow model 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 model is described. Numerical examples are given.
Key words:
mathematical simulation of gas flows around aircraft, turbulence, exhaust jet, compressible Navier–Stokes equation, aircraft nozzle.
Received: 23.09.2014
Citation:
D. A. Zabarko, V. I. Zubov, V. P. Kotenev, V. M. Krivtsov, Yu. A. Polezhaev, “Numerical simulation of gas flows around aircraft with allowance for the flow/exhaust jet interaction”, Zh. Vychisl. Mat. Mat. Fiz., 55:4 (2015), 681–694; Comput. Math. Math. Phys., 55:4 (2015), 677–689
Linking options:
https://www.mathnet.ru/eng/zvmmf10194 https://www.mathnet.ru/eng/zvmmf/v55/i4/p681
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Abstract page: | 287 | Full-text PDF : | 65 | References: | 50 | First page: | 11 |
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