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Fizika Goreniya i Vzryva, 2008, Volume 44, Issue 3, Pages 95–108 (Mi fgv1402)  

This article is cited in 18 scientific papers (total in 18 papers)

Continuous spin detonation of hydrogen-oxygen mixtures. 2. Combustor with an expanding annular channel

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

Lavrent’ev Institute of Hydrodynamics, Siberian Division, Russian Academy of Sciences, Novosibirsk, 630090
Citations (18)
Abstract: A comprehensive numerical and experimental study of continuous spin detonation of a hydrogen-oxygen mixture in an annular combustor with the components supplied through injectors is performed. The hydrogen-oxygen mixture is burned in the regime of continuous spin detonation in an annular combustor 4 cm in diameter with subsequent channel expansion. The flow structure is considered for varied flow rates of the components of the mixture and the counterpressure of the ambient medium. The dynamics of the transverse detonation wave is numerically studied in a two-dimensional unsteady gas-dynamic statement of the problem with the geometric parameters of the combustor consistent with experimental ones. Reasonable agreement with experiments is reached in terms of the shape of detonation fronts, detonation velocity, and height of the wave front. The optimal point of channel expansion beginning is chosen, which ensures the maximum specific impulse in the spin detonation regime.
Keywords: continuous spin detonation, combustor, transverse detonation waves, flow structure, mathematical modeling.
Received: 20.07.2007
Accepted: 06.12.2007
English version:
Combustion, Explosion and Shock Waves, 2008, Volume 44, Issue 3, Pages 330–342
DOI: https://doi.org/10.1007/s10573-008-0041-x
Bibliographic databases:
Document Type: Article
UDC: 536.8, 536.46
Language: Russian
Citation: F. A. Bykovskii, S. A. Zhdan, E. F. Vedernikov, “Continuous spin detonation of hydrogen-oxygen mixtures. 2. Combustor with an expanding annular channel”, Fizika Goreniya i Vzryva, 44:3 (2008), 95–108; Combustion, Explosion and Shock Waves, 44:3 (2008), 330–342
Citation in format AMSBIB
\Bibitem{BykZhdVed08}
\by F.~A.~Bykovskii, S.~A.~Zhdan, E.~F.~Vedernikov
\paper Continuous spin detonation of hydrogen-oxygen mixtures. 2.~Combustor with an expanding annular channel
\jour Fizika Goreniya i Vzryva
\yr 2008
\vol 44
\issue 3
\pages 95--108
\mathnet{http://mi.mathnet.ru/fgv1402}
\elib{https://elibrary.ru/item.asp?id=11846349}
\transl
\jour Combustion, Explosion and Shock Waves
\yr 2008
\vol 44
\issue 3
\pages 330--342
\crossref{https://doi.org/10.1007/s10573-008-0041-x}
Linking options:
  • https://www.mathnet.ru/eng/fgv1402
  • https://www.mathnet.ru/eng/fgv/v44/i3/p95
    Cycle of papers
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    3. Jianping Zhou, Feilong Song, Shida Xu, Xingkui Yang, Yongjun Zheng, “Investigation of Rotating Detonation Fueled by Liquid Kerosene”, Energies, 15:12 (2022), 4483  crossref
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    5. Xiao-Jian He, Xiang-Yang Liu, Jian-Ping Wang, “On the mechanisms of the multiplicity and bifurcation of detonation waves in 3D rotating detonation engines”, Aerospace Science and Technology, 130 (2022), 107874  crossref
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    7. Yepan Zhong, Yun Wu, Di Jin, Xin Chen, Xingkui Yang, Shunli Wang, “Effect of channel and oxidizer injection slot width on the rotating detonation fueled by pre-combustion cracked kerosene”, Acta Astronautica, 165 (2019), 365  crossref
    8. Brent A. Rankin, Joshua R. Codoni, Kevin Y. Cho, John L. Hoke, Frederick R. Schauer, “Investigation of the structure of detonation waves in a non-premixed hydrogen–air rotating detonation engine using mid-infrared imaging”, Proceedings of the Combustion Institute, 37:3 (2019), 3479  crossref
    9. S. Hansmetzger, R. Zitoun, P. Vidal, “A study of continuous rotation modes of detonation in an annular chamber with constant or increasing section”, Shock Waves, 28:5 (2018), 1065  crossref
    10. Brent A. Rankin, Daniel R. Richardson, Andrew W. Caswell, Andrew G. Naples, John L. Hoke, Frederick R. Schauer, “Chemiluminescence imaging of an optically accessible non-premixed rotating detonation engine”, Combustion and Flame, 176 (2017), 12  crossref
    11. Brent A. Rankin, Matthew L. Fotia, Andrew G. Naples, Christopher A. Stevens, John L. Hoke, Thomas A. Kaemming, Scott W. Theuerkauf, Frederick R. Schauer, “Overview of Performance, Application, and Analysis of Rotating Detonation Engine Technologies”, Journal of Propulsion and Power, 33:1 (2017), 131  crossref
    12. Brent A. Rankin, Joshua R. Codoni, Kevin Y. Cho, John Hoke, Frederick R. Schauer, 55th AIAA Aerospace Sciences Meeting, 2017  crossref
    13. Brent A. Rankin, Christopher A. Fugger, Daniel R. Richardson, Kevin Y. Cho, John Hoke, Andrew W. Caswell, James R. Gord, Frederick Schauer, 54th AIAA Aerospace Sciences Meeting, 2016  crossref
    14. Frank K. Lu, Eric M. Braun, “Rotating Detonation Wave Propulsion: Experimental Challenges, Modeling, and Engine Concepts”, Journal of Propulsion and Power, 30:5 (2014), 1125  crossref
    15. Frank Lu, Eric Braun, Luca Massa, Donald Wilson, 47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 2011  crossref
    16. Eric Braun, Nathan Dunn, Frank Lu, 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, 2010  crossref
    17. F. A. Bykovskii, S. A. Zhdan, E. F. Vedernikov, “Realization and modeling of continuous spin detonation of a hydrogen-oxygen mixture in flow-type combustors. 2. Combustors with expansion of the annular channel”, Combustion, Explosion and Shock Waves, 45:6 (2009), 716–728  mathnet  mathnet  crossref
    18. F. A. Bykovskii, E. F. Vedernikov, “Continuous spin detonation of hydrogen-oxygen mixtures. 3. Methods of measuring flow parameters and flow structure in combustors of different geometries”, Combustion, Explosion and Shock Waves, 44:4 (2008), 451–460  mathnet  mathnet  crossref
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