Abstract:
Results of an experimental study of continuous detonation of a hydrogen-air mixture in a flow-type annular combustor $306$ mm in diameter in the regime of air self-ejection are reported. The regime of pulsed detonation is also obtained. Stable regimes of continuous detonation with one and two transverse detonation waves having velocities $D = 1.48-1.16$ km/sec are observed in experiments. The frequency of the pulsed detonation wave is $\approx1.4$ kHz. The known condition for the continuous detonation regime (good mixing for the formation of a detonable layer) is validated. The size of the slot for air ejection, providing a necessary flow rate for detonation and a necessary ratio of the species in the mixture, is determined. Some methods for estimating the air flow rate are presented.
Citation:
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”, Fizika Goreniya i Vzryva, 47:2 (2011), 102–111; Combustion, Explosion and Shock Waves, 47:2 (2011), 217–225
\Bibitem{BykZhdVed11}
\by F.~A.~Bykovskii, S.~A.~Zhdan, E.~F.~Vedernikov
\paper Continuous detonation in the regime of self-oscillatory ejection of the oxidizer. 2. Air as an oxidizer
\jour Fizika Goreniya i Vzryva
\yr 2011
\vol 47
\issue 2
\pages 102--111
\mathnet{http://mi.mathnet.ru/fgv1088}
\elib{https://elibrary.ru/item.asp?id=16364783}
\transl
\jour Combustion, Explosion and Shock Waves
\yr 2011
\vol 47
\issue 2
\pages 217--225
\crossref{https://doi.org/10.1134/S0010508211020110}
Citation in format AMSBIB
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