Abstract:
A two-dimensional unsteady mathematical model of a continuous spinning detonation wave in a supersonic incoming flow in an annular combustor is formulated. The wave dynamics in a combustor filled by a gaseous hydrogen-oxygen mixture is studied. The possibility of continuous spin detonation with a supersonic flow velocity at the diffuser entrance is demonstrated numerically for the first time; the structure of transverse detonation waves and the range of their existence depending on the Mach number are studied.
Citation:
S. A. Zhdan, “Mathematical model of continuous detonation in an annular combustor with a supersonic flow velocity”, Fizika Goreniya i Vzryva, 44:6 (2008), 83–91; Combustion, Explosion and Shock Waves, 44:6 (2008), 690–697
\Bibitem{Zhd08}
\by S.~A.~Zhdan
\paper Mathematical model of continuous detonation in an annular combustor with a supersonic flow velocity
\jour Fizika Goreniya i Vzryva
\yr 2008
\vol 44
\issue 6
\pages 83--91
\mathnet{http://mi.mathnet.ru/fgv1449}
\elib{https://elibrary.ru/item.asp?id=11846396}
\transl
\jour Combustion, Explosion and Shock Waves
\yr 2008
\vol 44
\issue 6
\pages 690--697
\crossref{https://doi.org/10.1007/s10573-008-0104-z}
Linking options:
https://www.mathnet.ru/eng/fgv1449
https://www.mathnet.ru/eng/fgv/v44/i6/p83
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