Method of calculating the fuel combustion efficiency in the afterburner combustion chamber of a gas turbine dual fuel engine

The problem of reducing the emission of unburned hydrocarbons and carbon monoxide that affect the value of fuel combustion efficiency in the afterburner combustion chamber of a gas turbine engine is considered. An analysis of the causes of hydrocarbon and carbon monoxide formation were carried out a...

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Bibliographic Details

Published in:	Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение
Main Authors:	A. V. Zhuk, T. V. Grasko, A. S. Kolesnikov, V. V. Raznoschikov
Format:	Article
Language:	English
Published:	Samara National Research University 2025-06-01
Subjects:	aviation fuel specific fuel consumption afterburner hydrogen gas vaporized kerosene emission indices
Online Access:	https://journals.ssau.ru/vestnik/article/viewFile/28700/11331