Abstract
Hypersonic MHD air flow past a blunt body in the presence of an external magnetic field is considered. The MHD effect on the flow consists in a significant increase in the shock wave stand-off from the body surface and a significant reduction in the heat flux to the wall (up to 50%). It is shown that even in the presence of a strong Hall effect the intensity of the magnetohydrodynamic interaction in the plasma behind the shock wave remains at a high level commensurable with the ideal case of the absence of a Hall effect.
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Translated from Izvestiya Rossiiskoi Academii Nauk, Mekhanika Zhidkosti i Gaza, No. 5, 2006, pp. 188–203.
Original Russian Text Copyright © 2006 by Bityurin and Bocharov.
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Bityurin, V.A., Bocharov, A. Magnetohydrodynamic interaction in hypersonic air flow past a blunt body. Fluid Dyn 41, 843–856 (2006). https://doi.org/10.1007/s10697-006-0100-5
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DOI: https://doi.org/10.1007/s10697-006-0100-5