F. A. Bykovskii, S. A. Zhdan, E. F. Vedernikov, “Continuous detonation in the regime of self-oscillatory ejection of the oxidizer. 1. Oxygen as a oxidizer”, Fizika Goreniya i Vzryva, 46:3 (2010), 116–124; Combustion, Explosion and Shock Waves, 46:3 (2010), 344

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Fizika Goreniya i Vzryva, 2010, Volume 46, Issue 3, Pages 116–124 (Mi fgv1200)

This article is cited in 10 scientific papers (total in 10 papers)

Continuous detonation in the regime of self-oscillatory ejection of the oxidizer. 1. Oxygen as a oxidizer

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

Lavrent’ev Institute of Hydrodynamics, Siberian Division, Russian Academy of Sciences, Novosibirsk, 630090, Russia

Citations (10)

Abstract: Results of an experimental study of continuous spin and pulsed detonation of hydrogen-oxygen and acetylene-oxygen mixtures in a flow-type annular combustor $10$ cm in diameter with channel expansion in the regime of oxidizer ejection are presented. Through comparisons with the mechanical analogy of a piston-driven pump, it is found that the detonation wave serves as a pump for the oxidizer, and the rarefaction wave serves as a suction piston. Stable regimes of continuous spin detonation with one transverse wave are observed under the test conditions used; the wave velocity is $D=1.76-1.6$ km/sec for hydrogen and $D=1.46-1.2$ km/sec for acetylene. The frequency of the pulsed detonation wave is $7.3$–$5$ kHz in the $\mathrm{H}_2$–$\mathrm{O}_2$ mixture and approximately $2.5$ kHz in the $\mathrm{C}_2\mathrm{H}_2$–$\mathrm{O}_2$ mixture.

Keywords: oxidizer ejection, continuous spin detonation, pulsed detonation, flow-type combustor, flow structure.

Received: 01.07.2009

English version:
Combustion, Explosion and Shock Waves, 2010, Volume 46, Issue 3, Pages 344–351
DOI: https://doi.org/10.1007/s10573-010-0047-z

Bibliographic databases:

Document Type: Article

UDC: 536.8, 536.46

Language: Russian

Citation: F. A. Bykovskii, S. A. Zhdan, E. F. Vedernikov, “Continuous detonation in the regime of self-oscillatory ejection of the oxidizer. 1. Oxygen as a oxidizer”, Fizika Goreniya i Vzryva, 46:3 (2010), 116–124; Combustion, Explosion and Shock Waves, 46:3 (2010), 344–351

Citation in format AMSBIB

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\by F.~A.~Bykovskii, S.~A.~Zhdan, E.~F.~Vedernikov

\paper Continuous detonation in the regime of self-oscillatory ejection of the oxidizer. 1. Oxygen as a oxidizer

\jour Fizika Goreniya i Vzryva

\yr 2010

\vol 46

\issue 3

\pages 116--124

\mathnet{http://mi.mathnet.ru/fgv1200}

\elib{https://elibrary.ru/item.asp?id=15056322}

\transl

\jour Combustion, Explosion and Shock Waves

\yr 2010

\vol 46

\issue 3

\pages 344--351

\crossref{https://doi.org/10.1007/s10573-010-0047-z}

Linking options:

https://www.mathnet.ru/eng/fgv1200

https://www.mathnet.ru/eng/fgv/v46/i3/p116

Cycle of papers

Continuous detonation in the regime of self-oscillatory ejection of the oxidizer. 1. Oxygen as a oxidizer
F. A. Bykovskii, S. A. Zhdan, E. F. Vedernikov
Fizika Goreniya i Vzryva, 2010, 46:3, 116–124
Continuous detonation in the regime of self-oscillatory ejection of the oxidizer. 2. Air as an oxidizer
F. A. Bykovskii, S. A. Zhdan, E. F. Vedernikov
Fizika Goreniya i Vzryva, 2011, 47:2, 102–111

This publication is cited in the following 10 articles:

E V Simonov, S A Zhdan, “Calculation of continuous spin detonation of a hydrogen-oxygen mixture in an annular combustor with oxygen ejection”, J. Phys.: Conf. Ser., 1404:1 (2019), 012069
Vijay Anand, Ephraim Gutmark, “Rotating detonation combustors and their similarities to rocket instabilities”, Progress in Energy and Combustion Science, 73 (2019), 182
Vijay Anand, Ephraim Gutmark, “Rotating Detonations and Spinning Detonations: Similarities and Differences”, AIAA Journal, 56:5 (2018), 1717
Matthew L. Fotia, John Hoke, Frederick Schauer, Shock Wave and High Pressure Phenomena, Detonation Control for Propulsion, 2018, 1
F A Bykovskii, S A Zhdan, E F Vedernikov, A N Samsonov, E L Popov, “Detonation of a hydrogen-oxygen gas mixture in a plane-radial combustor with exhaustion toward the periphery in the regime of oxygen ejection”, J. Phys.: Conf. Ser., 1128 (2018), 012075
Chenglong Yang, Xiaosong Wu, Hu Ma, Lei Peng, Jian Gao, “Experimental research on initiation characteristics of a rotating detonation engine”, Experimental Thermal and Fluid Science, 71 (2016), 154
Matthew L. Fotia, Fred Schauer, Tom Kaemming, John Hoke, “Experimental Study of the Performance of a Rotating Detonation Engine with Nozzle”, Journal of Propulsion and Power, 32:3 (2016), 674
Piotr Wolański, “Detonative propulsion”, Proceedings of the Combustion Institute, 34:1 (2013), 125
F. A. Bykovskii, S. A. Zhdan, E. F. Vedernikov, “Continuous detonation in the regime of self-oscillatory ejection of the oxidizer. 2. Air as an oxidizer”, Combustion, Explosion and Shock Waves, 47:2 (2011), 217–225
F. A. Bykovskii, S. A. Zhdan, E. F. Vedernikov, “Continuous detonation in the air ejection mode. Domain of existence”, Combustion, Explosion and Shock Waves, 47:3 (2011), 330–334

Citing articles in Google Scholar: Russian citations, English citations
Related articles in Google Scholar: Russian articles, English articles

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