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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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Resumo

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.

Sobre autores

V. Fomichev

Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Branch

Email: yadrenkin@itam.nsc.ru
Rússia, Novosibirsk, 630090

M. Yadrenkin

Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Branch

Autor responsável pela correspondência
Email: yadrenkin@itam.nsc.ru
Rússia, Novosibirsk, 630090

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Declaração de direitos autorais © Pleiades Publishing, Ltd., 2017