Dynamic characteristics of a resonant gas-dynamic system for ignition of a fuel mixture

被引：14

作者：

Aref'ev, K. Yu. ^{[1
,2
]}

Voronetskii, A. V. ^{[2
]}

Il'chenko, M. A. ^{[1
]}

机构：

[1] Baranov Cent Inst Aviat Motors, Moscow 111116, Russia

[2] Bauman Moscow State Tech Univ, Moscow 105005, Russia

来源：

COMBUSTION EXPLOSION AND SHOCK WAVES | 2013年 / 49卷 / 06期

关键词：

ignition system; pressure oscillations; gas-dynamic resonance; liquid-propellant thruster; Hartmann oscillator;

D O I：

10.1134/S0010508213060038

中图分类号：

O414.1 [热力学];

学科分类号：

摘要：

Results of an experimental study of specific features of operation of a resonant gasdynamic 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.

引用

页码：657 / 661

页数：5

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[10]

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