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The Structure of a Hypersonic Air Flow near a Plane Surface at Various Intensities of Magnetogasdynamic Interaction

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Abstract

This Letter presents a systematization of the effects observed in experiments on the magnetogasdynamic interaction near the surface of a plate in a high-speed gas flow. Ranges of the hydromagnetic-interaction parameter determining various levels of influence on the shock-wave structure of the flow are established.

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Authors and Affiliations

  1. Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Branch, Russian Academy of Sciences, Novosibirsk, 630090, Russia

    V. P. Fomichev & M. A. Yadrenkin

Authors
  1. V. P. Fomichev
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  2. M. A. Yadrenkin
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Correspondence to M. A. Yadrenkin.

Additional information

Original Russian Text © V.P. Fomichev, M.A. Yadrenkin, 2017, published in Pis’ma v Zhurnal Tekhnicheskoi Fiziki, 2017, Vol. 43, No. 23, pp. 31–39.

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Fomichev, V.P., Yadrenkin, M.A. The Structure of a Hypersonic Air Flow near a Plane Surface at Various Intensities of Magnetogasdynamic Interaction. Tech. Phys. Lett. 43, 1063–1066 (2017). https://doi.org/10.1134/S1063785017120057

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  • DOI: https://doi.org/10.1134/S1063785017120057

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