This article is cited in 131 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.

UDC: 536.8, 536.46

Received: 18.03.2002
Accepted: 10.11.2002

 English version: Combustion, Explosion and Shock Waves, 2003, 39:3, 323–334

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