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Nonclassical Transonic Boundary Layers: Toward Overcoming Dead-End Situations in High-Speed Aerodynamics

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Abstract

Analytical models of unsteady free viscous-inviscid interaction of gas flows at transonic speeds, i.e., a transonic boundary layer with self-induced pressure (nonclassical boundary layer) are considered. It is shown that an adequate flow model can be constructed by applying methods of singular perturbations. The results of a comparative analysis of classical and regularized stability models for a boundary layer with self-induced pressure in the case of interaction at transonic speeds are overviewed.

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Authors and Affiliations

  1. Research Institute of Mechanics, Moscow State University, Moscow, 119991, Russia

    A. N. Bogdanov

  2. Moscow Institute of Physics and Technology, Dolgoprudnyi, Moscow oblast, 141700, Russia

    V. N. Diesperov

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

    V. I. Zhuk

Authors
  1. A. N. Bogdanov
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  2. V. N. Diesperov
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  3. V. I. Zhuk
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Correspondence to A. N. Bogdanov.

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

Original Russian Text © A.N. Bogdanov, V.N. Diesperov, V.I. Zhuk, 2018, published in Zhurnal Vychislitel’noi Matematiki i Matematicheskoi Fiziki, 2018, Vol. 58, No. 2, pp. 270–280.

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Bogdanov, A.N., Diesperov, V.N. & Zhuk, V.I. Nonclassical Transonic Boundary Layers: Toward Overcoming Dead-End Situations in High-Speed Aerodynamics. Comput. Math. and Math. Phys. 58, 254–263 (2018). https://doi.org/10.1134/S0965542518020033

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  • DOI: https://doi.org/10.1134/S0965542518020033

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