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Fizika Goreniya i Vzryva, 2007, Volume 43, Issue 3, Pages 3–8 (Mi fgv1493)  
Hydrogen combustion in an axisymmetric duct with a supersonic air flow

V. A. Zabaikin, A. A. Smogolev

Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Division, Russian Academy of Sciences, Novosibirsk, 630090
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.
Keywords: supersonic flow, hydrogen combustion, duct geometry.
Received: 07.02.2006
English version:
Combustion, Explosion and Shock Waves, 2007, Volume 43, Issue 3, Pages 247–252
DOI: https://doi.org/10.1007/s10573-007-0037-y
Bibliographic databases:
Document Type: Article
UDC: 536.46
Language: Russian
Citation: V. A. Zabaikin, A. A. Smogolev, “Hydrogen combustion in an axisymmetric duct with a supersonic air flow”, Fizika Goreniya i Vzryva, 43:3 (2007), 3–8; Combustion, Explosion and Shock Waves, 43:3 (2007), 247–252
Citation in format AMSBIB
\Bibitem{ZabSmo07}
\by V.~A.~Zabaikin, A.~A.~Smogolev
\paper Hydrogen combustion in an axisymmetric duct with a supersonic air flow
\jour Fizika Goreniya i Vzryva
\yr 2007
\vol 43
\issue 3
\pages 3--8
\mathnet{http://mi.mathnet.ru/fgv1493}
\elib{https://elibrary.ru/item.asp?id=16757049}
\transl
\jour Combustion, Explosion and Shock Waves
\yr 2007
\vol 43
\issue 3
\pages 247--252
\crossref{https://doi.org/10.1007/s10573-007-0037-y}
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