Hydrogen combustion in an axisymmetric duct with a supersonic air flow |
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Authors: | V A Zabaykin A A Smogolev |
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Affiliation: | (1) Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Division, Russian Academy of Sciences, Novosibirsk, 630090 |
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Abstract: | Results of an experimental study of hydrogen combustion in a supersonic high-enthalpy air flow in axisymmetric ducts with
constant and variable cross sections are described. Conditions of flow reconstruction due to heat addition in ducts of different
geometry are considered. It is demonstrated that a gas-dynamic action ensures stable self-ignition and it becomes possible
to control combustion in expanding ducts with special profiles.
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Translated from Fizika Goreniya i Vzryva, Vol. 43, No. 3, pp. 3–8, May–June, 2007. |
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Keywords: | supersonic flow hydrogen combustion duct geometry |
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