Combustion of methane injected into an air flow with high subsonic velocities by different methods


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An important stage of the development of promising engine and propulsion systems is provision of an effective process of hydrocarbon fuel combustion. There are many publications with numerical and experimental data on combustion of various gaseous hydrocarbons under laboratory conditions, but there is a lack of data on effective combustion of hydrocarbons in short combustion chambers with a large number of injectors. Results of systematic experimental studies of natural gas (methane) combustion in a high-velocity subsonic air flow in an air-breathing model combustor with a rectangular cross section are presented in this paper.

作者简介

R. Albegov

Baranov Central Institute of Aviation Motors

Email: slavavino@ciam.ru
俄罗斯联邦, Moscow, 111116

V. Vinogradov

Baranov Central Institute of Aviation Motors

编辑信件的主要联系方式.
Email: slavavino@ciam.ru
俄罗斯联邦, Moscow, 111116

Yu. Shikhman

Baranov Central Institute of Aviation Motors

Email: slavavino@ciam.ru
俄罗斯联邦, Moscow, 111116

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