Email this article The Structure of a Hypersonic Air Flow near a Plane Surface at Various Intensities of Magnetogasdynamic Interaction
- Authors: Fomichev V.P.1, Yadrenkin M.A.1
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Affiliations:
- Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Branch
- Issue: Vol 43, No 12 (2017)
- Pages: 1063-1066
- Section: Article
- URL: https://bakhtiniada.ru/1063-7850/article/view/206713
- DOI: https://doi.org/10.1134/S1063785017120057
- ID: 206713
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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.
About the authors
V. P. Fomichev
Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Branch
Email: yadrenkin@itam.nsc.ru
Russian Federation, Novosibirsk, 630090
M. A. Yadrenkin
Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Branch
Author for correspondence.
Email: yadrenkin@itam.nsc.ru
Russian Federation, Novosibirsk, 630090
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