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Fizika Goreniya i Vzryva, 2019, Volume 55, Issue 3, Pages 35–42
DOI: https://doi.org/10.15372/FGV20190304
(Mi fgv581)
 

This article is cited in 9 scientific papers (total in 9 papers)

Determination of the fuel concentration distribution in a supersonic combustion chamber

M. A. Goldfeld, A. V. Starov

Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Branch of the Russian Academy of Sciences, Novosibirsk, 630090, Russia
Full-text PDF (394 kB) Citations (9)
Abstract: Kerosene concentration distributions measured in the combustion chamber of a hotshot wind tunnel in the attached pipeline regime with the input Mach number of 2.89 are reported. Kerosene is injected through 12 jet injectors at an angle to the flow from the wall upstream of a cavity. The measurements are performed in three cross sections. Data on the kerosene concentration distribution in the initial region of the combustion chamber and its dependence on the ratio of the jet and main flow momenta are obtained. It is demonstrated that the absence of intense combustion in a model combustor under these conditions is caused by the fact that the local equivalence ratios are insufficient for ignition.
Keywords: supersonic flow, sampling tube, mixing, kerosene, combustion.
Funding agency Grant number
Program of fundamental scientific research of the State Academies of Sciences АААА-А17-117030610126-4
Received: 04.12.2017
Revised: 14.11.2018
Accepted: 28.11.2018
English version:
Combustion, Explosion and Shock Waves, 2019, Volume 55, Issue 3, Pages 274–281
DOI: https://doi.org/10.1134/S0010508219030043
Bibliographic databases:
Document Type: Article
UDC: 533.6.07;533.69
Language: Russian
Citation: M. A. Goldfeld, A. V. Starov, “Determination of the fuel concentration distribution in a supersonic combustion chamber”, Fizika Goreniya i Vzryva, 55:3 (2019), 35–42; Combustion, Explosion and Shock Waves, 55:3 (2019), 274–281
Citation in format AMSBIB
\Bibitem{GolSta19}
\by M.~A.~Goldfeld, A.~V.~Starov
\paper Determination of the fuel concentration distribution in a supersonic combustion chamber
\jour Fizika Goreniya i Vzryva
\yr 2019
\vol 55
\issue 3
\pages 35--42
\mathnet{http://mi.mathnet.ru/fgv581}
\crossref{https://doi.org/10.15372/FGV20190304}
\elib{https://elibrary.ru/item.asp?id=38170615}
\transl
\jour Combustion, Explosion and Shock Waves
\yr 2019
\vol 55
\issue 3
\pages 274--281
\crossref{https://doi.org/10.1134/S0010508219030043}
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  • https://www.mathnet.ru/eng/fgv/v55/i3/p35
  • This publication is cited in the following 9 articles:
    Citing articles in Google Scholar: Russian citations, English citations
    Related articles in Google Scholar: Russian articles, English articles
    Fizika Goreniya i Vzryva Fizika Goreniya i Vzryva
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