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This article is cited in 1 scientific paper (total in 1 paper)
Numerical analysis of combustion kinetics for hydrogen–air mixtures with NH$_3$, CH$_4$, and C$_2$Н$_6$
A. M. Starik, N. S. Titova Russian Federation’s State Scientific Center, Baranov Central Institute of Aviation, Motor-Building, 111250, Moscow
Abstract:
The possibility of reducing the concentration of nitrogen oxides and HNO$_x$-group components with simultaneous shortening of the reaction-zone length during combustion of hydrogen-air mixtures in a supersonic flow behind an oblique shock wave by introducing NH$_3$, CH$_4$, and C$_2$Н$_6$ additives into the mixture is analyzed. A numerical study shows that a small (up to 5%) amount of these additives substantially changes the combustion kinetics behind the shock-wave front, shortens the flame length, and diminishes the NO and NO$_2$ content in the combustion products.
Received: 06.11.1998
Citation:
A. M. Starik, N. S. Titova, “Numerical analysis of combustion kinetics for hydrogen–air mixtures with NH$_3$, CH$_4$, and C$_2$Н$_6$”, Fizika Goreniya i Vzryva, 36:3 (2000), 31–38; Combustion, Explosion and Shock Waves, 36:3 (2000), 310–317
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https://www.mathnet.ru/eng/fgv2199 https://www.mathnet.ru/eng/fgv/v36/i3/p31
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