Controlling the position of a stabilized detonation wave in a supersonic gas mixture flow in a plane channel
- 作者: Levin V.1, Zhuravskaya T.1
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隶属关系:
- Institute of Mechanics
- 期: 卷 43, 编号 3 (2017)
- 页面: 316-319
- 栏目: Article
- URL: https://journals.rcsi.science/1063-7850/article/view/204082
- DOI: https://doi.org/10.1134/S1063785017030191
- ID: 204082
如何引用文章
详细
Stabilization of a detonation wave in a stoichiometric hydrogen–air mixture flowing at a supersonic velocity into a plane symmetric channel with constriction has been studied in the framework of a detailed kinetic mechanism of the chemical interaction. Conditions ensuring the formation of a thrust-producing f low with a stabilized detonation wave in the channel are determined. The inf luence of the inf low Mach number, dustiness of the combustible gas mixture supplied to the channel, and output cross-section size on the position of a stabilized detonation wave in the f low has been analyzed with a view to increasing the efficiency of detonation combustion of the gas mixture. It is established that thrust-producing flow with a stabilized detonation wave can be formed in the channel without any energy consumption.
作者简介
V. Levin
Institute of Mechanics
Email: zhuravskaya@imec.msu.ru
俄罗斯联邦, Moscow, 119192
T. Zhuravskaya
Institute of Mechanics
编辑信件的主要联系方式.
Email: zhuravskaya@imec.msu.ru
俄罗斯联邦, Moscow, 119192