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Publikováno v:
Авіаційно-космічна техніка та технологія, Vol 0, Iss 3, Pp 30-36 (2022)
The subject of research in this article is the process of turning on the afterburner combustion chamber of a modern turbojet bypass engine. The parameters of switching in the afterburner were studied: pressure pulsations of the gas flow between the h
Externí odkaz:
https://doaj.org/article/c2f0d609633d427699f44952050f0e07
Publikováno v:
Aerospace technic and technology. :30-36
The subject of research in this article is the process of turning on the afterburner combustion chamber of a modern turbojet bypass engine. The parameters of switching in the afterburner were studied: pressure pulsations of the gas flow between the h