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High-Order Multioperator Compact Schemes for Numerical Simulation of Unsteady Subsonic Airfoil Flow

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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 103 to 107. 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.

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Authors and Affiliations

  1. Dorodnicyn Computing Center, Federal Research Center “Computer Science and Control,”, Russian Academy of Sciences, Moscow, 119333, Russia

    A. D. Savel’ev

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  1. A. D. Savel’ev
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Correspondence to A. D. Savel’ev.

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Dedicated to the 100th birthday of Academician N.N. Moiseev

Original Russian Text © A.D. Savel’ev, 2018, published in Zhurnal Vychislitel’noi Matematiki i Matematicheskoi Fiziki, 2018, Vol. 58, No. 2, pp. 291–303.

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Savel’ev, A.D. High-Order Multioperator Compact Schemes for Numerical Simulation of Unsteady Subsonic Airfoil Flow. Comput. Math. and Math. Phys. 58, 274–285 (2018). https://doi.org/10.1134/S0965542518020148

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  • DOI: https://doi.org/10.1134/S0965542518020148

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