The geometric characteristics of the front and the length selection for the combustion chamber of direct flow type

A method has been developed for selecting the geometric characteristics of the front and the length of the direct-flow combustion chamber. Afterburner combustion chambers are of the ramjet type and are used for a short-term increase in the thrust of a gas turbine engine during takeoff, for overcomin...

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Autor principal: Дмитрий Викторович Козел
Formato: article
Lenguaje:EN
RU
UK
Publicado: National Aerospace University «Kharkiv Aviation Institute» 2021
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Acceso en línea:https://doaj.org/article/9393cd90f53b4fe18394405d972e19f0
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