A. A. Davydov, T. V. Konstantinovskaya, A. E. Lutsky, A. M. Kharitonov, A. M. Shevchenko, A. S. Shmakov, “Simulation of a supersonic flowfield in the tip vortex core at Mach number of 6”, Mat. Model., 24:6 (2012), 67–82; Math. Models Comput. Simul., 5:1 (2013), 25

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Matematicheskoe modelirovanie, 2012, Volume 24, Number 6, Pages 67–82 (Mi mm3285)

This article is cited in 5 scientific papers (total in 5 papers)

Simulation of a supersonic flowfield in the tip vortex core at Mach number of 6

A. A. Davydov^a, T. V. Konstantinovskaya^a, A. E. Lutsky^a, A. M. Kharitonov^b, A. M. Shevchenko^b, A. S. Shmakov^b

^a Keldysh Institute of Applied Mathematics of Russiаn Асаdеmу of Sciепсеs, Moscow
^b Khristianovich Institute of Theoretical and Applied Mechanics SB RAS

Full-text PDF (799 kB) Citations (5)

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Abstract: In this work there are presented: numerical simulations of the wing-tip vortex for various attack angles of the wing, comparing the resulting flow regimes among themselves and with the experimental data. Numerical simulations were executed using the turbulence model of Spalart–Allmaras in the Keldysh Institute of Applied Mathematics RAS. Experiments were realized in Khristianovich Institute of Theoretical and Applied Mechanics SB RAS.

Keywords: wing-tip vortex, numerical simulations, supersonic flow, turbulence model of Spalart–Allmaras.

Received: 31.10.2011

English version:
Mathematical Models and Computer Simulations, 2013, Volume 5, Issue 1, Pages 25–36
DOI: https://doi.org/10.1134/S2070048213010031

Bibliographic databases:

Document Type: Article

UDC: 519.6

Language: Russian

Citation: A. A. Davydov, T. V. Konstantinovskaya, A. E. Lutsky, A. M. Kharitonov, A. M. Shevchenko, A. S. Shmakov, “Simulation of a supersonic flowfield in the tip vortex core at Mach number of 6”, Mat. Model., 24:6 (2012), 67–82; Math. Models Comput. Simul., 5:1 (2013), 25–36

Citation in format AMSBIB

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\by A.~A.~Davydov, T.~V.~Konstantinovskaya, A.~E.~Lutsky, A.~M.~Kharitonov, A.~M.~Shevchenko, A.~S.~Shmakov

\paper Simulation of a supersonic flowfield in the tip vortex core at Mach number of 6

\jour Mat. Model.

\yr 2012

\vol 24

\issue 6

\pages 67--82

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\mathscinet{http://mathscinet.ams.org/mathscinet-getitem?mr=3026821}

\elib{https://elibrary.ru/item.asp?id=21276766}

\transl

\jour Math. Models Comput. Simul.

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\pages 25--36

\crossref{https://doi.org/10.1134/S2070048213010031}

\scopus{https://www.scopus.com/record/display.url?origin=inward&eid=2-s2.0-84928997260}

Linking options:

https://www.mathnet.ru/eng/mm3285

https://www.mathnet.ru/eng/mm/v24/i6/p67

This publication is cited in the following 5 articles:

Shmakov A.S., Shevchenko A.M., “Features and Problems of Experimental Study of Supersonic Vortex Flows”, AIP Conference Proceedings, 2125, ed. Fomin V., Amer Inst Physics, 2019, 030108
V. E. Borisov, A. A. Davydov, T. V. Konstantinovskaya, A. E. Lutskii, A. M. Shevchenko, A. S. Shmakov, “Modelirovanie sverkhzvukovogo techeniya v slede za krylom pri $M = 2$ – $4$ ”, Preprinty IPM im. M. V. Keldysha, 2018, 050, 19 pp.
Borisov V.E., Davydov A.A., Konstantinovskaya T.V., Lutsky A.E., Shevchenko A.M., Shmakov A.S., “Numerical and Experimental Investigation of a Supersonic Vortex Wake At a Wide Distance From the Wing”, AIP Conference Proceedings, 2027, ed. Fomin V., Amer Inst Physics, 2018, 030120-1
A. A. Davydov, T. V. Konstantinovskaya, A. E. Lutskii, “Chislennoe modelirovanie vikhrevogo sleda za krylom na bolshikh udaleniyakh ot kryla v sverkhzvukovom potoke”, Preprinty IPM im. M. V. Keldysha, 2017, 095, 15 pp.
A. A. Davydov, A. E. Lutskii, “Chislennoe modelirovanie sverkhzvukovogo techeniya v slede za krylom i ego vzaimodeistviya s peresekayuschimisya udarnymi volnami”, Preprinty IPM im. M. V. Keldysha, 2014, 098, 16 pp.

Citing articles in Google Scholar: Russian citations, English citations
Related articles in Google Scholar: Russian articles, English articles

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Abstract page:	486
Full-text PDF :	145
References:	87
First page:	11

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