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This article is cited in 117 scientific papers (total in 117 papers)
Continuous detonation of a subsonic flow of a propellant
F. A. Bykovskii, E. F. Vedernikov Siberian Division, Russian Academy of Sciences, Lavrent'ev Institute of Hydrodynamics, Novosibirsk, 630090
Abstract:
The principal possibility of organizing controlled combustion of a subsonic flow of a propellant in longitudinal pulsed and spin detonation waves is experimentally verified. Conditions and reasons for the existence of detonation waves are considered.
Keywords:
propellant, detonation, subsonic flow, combustor, flow structure.
Received: 18.03.2002 Accepted: 10.11.2002
Citation:
F. A. Bykovskii, E. F. Vedernikov, “Continuous detonation of a subsonic flow of a propellant”, Fizika Goreniya i Vzryva, 39:3 (2003), 93–104; Combustion, Explosion and Shock Waves, 39:3 (2003), 323–334
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https://www.mathnet.ru/eng/fgv1881 https://www.mathnet.ru/eng/fgv/v39/i3/p93
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