Abstract:
Results of numerical and theoretical studies of supersonic diffusive combustion of a system of plane hydrogen jets in a supersonic air flow are described. It is shown that large–scale vortex structures appear in the mixing zone of the system of hydrogen jets and the cocurrent flow. These vortex structures affect the mechanism of turbulent exchange between the fuel and the oxidizer.
Citation:
U. К. Zhapbasbaev, Y. P. Makashev, “Gas–dynamic structures in supersonic combustion of hydrogen in a system of plane jets in a supersonic flow”, Prikl. Mekh. Tekh. Fiz., 42:1 (2001), 25–32; J. Appl. Mech. Tech. Phys., 42:1 (2001), 21–27
\Bibitem{ZhaMak01}
\by U.~К.~Zhapbasbaev, Y.~P.~Makashev
\paper Gas–dynamic structures in supersonic combustion of hydrogen in a system of plane jets in a supersonic flow
\jour Prikl. Mekh. Tekh. Fiz.
\yr 2001
\vol 42
\issue 1
\pages 25--32
\mathnet{http://mi.mathnet.ru/pmtf2708}
\elib{https://elibrary.ru/item.asp?id=17261991}
\transl
\jour J. Appl. Mech. Tech. Phys.
\yr 2001
\vol 42
\issue 1
\pages 21--27
\crossref{https://doi.org/10.1023/A:1018892024601}
Linking options:
https://www.mathnet.ru/eng/pmtf2708
https://www.mathnet.ru/eng/pmtf/v42/i1/p25
This publication is cited in the following 2 articles:
N. N. Fedorova, O. S. Vankova, “Effect of the ambient medium parameters on ignition and combustion of a supersonic hydrogen jet expanding into a still space”, Combustion, Explosion and Shock Waves, 58:3 (2022), 269–281
V. A. Zabaikin, A. A. Smogolev, “Hydrogen combustion in an axisymmetric duct with a supersonic air flow”, Combustion, Explosion and Shock Waves, 43:3 (2007), 247–252
Citation in format AMSBIB
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