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Fizika Goreniya i Vzryva, 2020, Volume 56, Issue 5, Pages 49–56
DOI: https://doi.org/10.15372/FGV20200505
(Mi fgv707)
 

This article is cited in 7 scientific papers (total in 7 papers)

Continuous detonation of CH4/H2–air mixtures in an annular combustor with varied geometry

F. A. Bykovskii, S. A. Zhdan, E. F. Vedernikov

Lavrentyev Institute of Hydrodynamics of Siberian Branch of the Russian Academy of Sciences, 630090, Novosibirsk, Russia
Full-text PDF (303 kB) Citations (7)
Abstract: Regimes of continuous detonation of CH4/H2–air mixtures with mass fractions of H2 in the fuel equal to 01/5 are obtained in an annular combustor 503 mm in diameter with variation of the combustor geometry. The influence of the combustor geometry on the velocity and number of transverse detonation waves, pressure in the combustor, and specific impulse is considered. It is found that three-fold constriction of the combustor exit cross area allows obtaining two-wave regimes of continuous spin detonation in the pure methane-air mixture. Based on stagnation pressures measured at the combustor exit, the specific impulses in the case of continuous detonation are determined for different compositions of the fuel.
Keywords: continuous spin detonation, methane, hydrogen, air, transverse detonation waves, geometry of the annular combustor, fuel injection system, photorecording, flow structure, thrust characteristics.
Funding agency Grant number
Russian Foundation for Basic Research 19-01-00270a
Received: 07.10.2019
Revised: 23.01.2020
Accepted: 19.02.2020
English version:
Combustion, Explosion and Shock Waves, 2020, Volume 56, Issue 5, Pages 537–544
DOI: https://doi.org/10.1134/S0010508220050056
Bibliographic databases:
Document Type: Article
UDC: 534.222.2, 544.454.3
Language: Russian
Citation: F. A. Bykovskii, S. A. Zhdan, E. F. Vedernikov, “Continuous detonation of CH4/H2–air mixtures in an annular combustor with varied geometry”, Fizika Goreniya i Vzryva, 56:5 (2020), 49–56; Combustion, Explosion and Shock Waves, 56:5 (2020), 537–544
Citation in format AMSBIB
\Bibitem{BykZhdVed20}
\by F.~A.~Bykovskii, S.~A.~Zhdan, E.~F.~Vedernikov
\paper Continuous detonation of $\mathrm{CH}_4/\mathrm{H}_2$--air mixtures in an annular combustor with varied geometry
\jour Fizika Goreniya i Vzryva
\yr 2020
\vol 56
\issue 5
\pages 49--56
\mathnet{http://mi.mathnet.ru/fgv707}
\crossref{https://doi.org/10.15372/FGV20200505}
\elib{https://elibrary.ru/item.asp?id=43939924}
\transl
\jour Combustion, Explosion and Shock Waves
\yr 2020
\vol 56
\issue 5
\pages 537--544
\crossref{https://doi.org/10.1134/S0010508220050056}
Linking options:
  • https://www.mathnet.ru/eng/fgv707
  • https://www.mathnet.ru/eng/fgv/v56/i5/p49
  • This publication is cited in the following 7 articles:
    1. Qiaodong Bai, Han Qiu, Jiaxiang Han, Yuwen Wu, Fang Wang, Chunsheng Weng, “Effect of ethylene-rich gas temperature on rotating detonation auto-initiation process”, Experimental Thermal and Fluid Science, 158 (2024), 111246  crossref
    2. Lei Bai, Fangming Cheng, Yuting Dong, “Experimental Investigation and Chemical Kinetics Analysis of Carbon Dioxide Inhibition on Hydrogen-Enriched Liquefied Petroleum Gas (LPG) Explosions”, Energies, 17:21 (2024), 5351  crossref
    3. Zhenmin Luo, Shangyong Zhou, Tao Wang, Bin Su, Ruikang Li, “The weakening effect of the inhibition of CO2 on the explosion of HCNG with the increase of hydrogen: Experimental and chemical kinetic research”, International Journal of Hydrogen Energy, 48:82 (2023), 32179  crossref
    4. Bin Su, Zhenmin Luo, Jun Deng, Tao Wang, Litao Liu, Shangyong Zhou, Kunlun Lu, Jiang Zhang, Lu Liu, “Comparative study on methane/air deflagration with hydrogen and ethane additions: Investigation from macro and micro perspectives”, Process Safety and Environmental Protection, 174 (2023), 561  crossref
    5. F. A. Bykovskii, S. A. Zhdan, E. F. Vedernikov, “Parameters of continuous multifront detonation of a methane mixture with heated air in an annular cylindrical combustor”, Combustion, Explosion and Shock Waves, 58:2 (2022), 149–158  mathnet  mathnet  crossref  crossref
    6. V.S. Ivanov, S.M. Frolov, A.E. Zangiev, V.I. Zvegintsev, I.O. Shamshin, “Updated conceptual design of hydrogen/ethylene fueled detonation ramjet: Test fires at Mach 1.5, 2.0, and 2.5”, Aerospace Science and Technology, 126 (2022), 107602  crossref
    7. F. A. Bykovskii, S. A. Zhdan, E. F. Vedernikov, “Continuous multifront detonation of kerosene–air mixture in an annular combustor with variations of its geometry”, Shock Waves, 31:8 (2021), 829  crossref
    Citing articles in Google Scholar: Russian citations, English citations
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