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This article is cited in 2 scientific papers (total in 2 papers)
Vortex structures in combustion of hydrogen in a supersonic cocurrent air stream
S. S. Vorontsov, V. A. Zabaikin, A. A. Smogolev, P. K. Tret'yakov Siberian Division, Russian Academy of Sciences, Institute of Theoretical and Applied Mechanics, Novosibirsk, 630090
Abstract:
The existence of vortex zones at the outer boundary of the hydrogen plume in a cocurrent air flow is confirmed. An analysis of experimental results and a comparison with available calculations show that the formation of such zones can be associated with the wave structure arising in the case of nonisobaric outflow of the air stream. The size of vortex zones of combustion increases along the plume, and these zones can improve mixing of the fuel and air jets.
Keywords:
supersonic nonisobaric jet, hydrogen combustion, vortex structures.
Received: 23.05.2002
Citation:
S. S. Vorontsov, V. A. Zabaikin, A. A. Smogolev, P. K. Tret'yakov, “Vortex structures in combustion of hydrogen in a supersonic cocurrent air stream”, Fizika Goreniya i Vzryva, 39:2 (2003), 3–8; Combustion, Explosion and Shock Waves, 39:2 (2003), 119–123
Linking options:
https://www.mathnet.ru/eng/fgv1853 https://www.mathnet.ru/eng/fgv/v39/i2/p3
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