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Zhurnal Vychislitel'noi Matematiki i Matematicheskoi Fiziki, 2018, Volume 58, Number 2, Pages 291–303
DOI: https://doi.org/10.7868/S0044466918020151 (Mi zvmmf10683) 		 
This article is cited in 2 scientific papers (total in 2 papers)

High-order multioperator compact schemes for numerical simulation of unsteady subsonic airfoil flow

A. D. Savel'ev

Dorodnicyn Computing Center, Federal Research Center “Computer Science and Control”, Russian Academy of Sciences, Moscow, Russia
Citations (2)
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DOI: https://doi.org/10.7868/S0044466918020151
Abstract: On the basis of high-order schemes, the viscous gas flow over the NACA2212 airfoil is numerically simulated at a free-stream Mach number of $0.3$ and Reynolds numbers ranging from $10^3$ to $10^7$. Flow regimes sequentially varying due to variations in the free-stream viscosity are considered. Vortex structures developing on the airfoil surface are investigated, and a physical interpretation of this phenomenon is given.
Key words: numerical simulation, high-order compact schemes, airfoil, boundary layer separation.
Received: 03.07.2017
English version:
Computational Mathematics and Mathematical Physics, 2018, Volume 58, Issue 2, Pages 274–285
DOI: https://doi.org/10.1134/S0965542518020148
Bibliographic databases:
Document Type: Article
UDC: 519.634
Language: Russian
Citation: A. D. Savel'ev, “High-order multioperator compact schemes for numerical simulation of unsteady subsonic airfoil flow”, Zh. Vychisl. Mat. Mat. Fiz., 58:2 (2018), 291–303; Comput. Math. Math. Phys., 58:2 (2018), 274–285
Citation in format AMSBIB
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    • This publication is cited in the following 2 articles:
    Citing articles in Google Scholar: Russian citations, English citations
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    		Журнал вычислительной математики и математической физики Computational Mathematics and Mathematical Physics
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