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This article is cited in 13 scientific papers (total in 13 papers)
Dynamic characteristics of a resonant gas-dynamic system for ignition of a fuel mixture
K. J. Arefyevab, A. V. Voronetskiib, M. A. Il'chenkoa a Baranov Central Institute of Aviation Motors, Moscow, 111116, Russia
b Bauman Moscow State Technical University, Moscow, 105005, Russia
Abstract:
Results of an experimental study of specific features of operation of a resonant gas-dynamic ignition system, as applied to initiation of liquid-propellant thrusters, are reported. Dynamic characteristics of the initiation process are determined. The behavior of the spectral characteristics of pressure oscillations in the combustor of a testbench model of a liquid-propellant thruster with ignition of the fuel mixture by the gas-dynamic system is considered.
Keywords:
ignition system, pressure oscillations, gas-dynamic resonance, liquid-propellant thruster, Hartmann oscillator.
Received: 29.01.2013
Citation:
K. J. Arefyev, A. V. Voronetskii, M. A. Il'chenko, “Dynamic characteristics of a resonant gas-dynamic system for ignition of a fuel mixture”, Fizika Goreniya i Vzryva, 49:6 (2013), 41–46; Combustion, Explosion and Shock Waves, 49:6 (2013), 657–661
Linking options:
https://www.mathnet.ru/eng/fgv82 https://www.mathnet.ru/eng/fgv/v49/i6/p41
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