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pro vyhledávání: '"Дмитрий Викторович Козел"'
Autor:
Дмитрий Викторович Козел
Publikováno v:
Авіаційно-космічна техніка та технологія, Vol 0, Iss 4sup2, Pp 19-28 (2021)
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
Externí odkaz:
https://doaj.org/article/9393cd90f53b4fe18394405d972e19f0
Publikováno v:
Авіаційно-космічна техніка та технологія, Vol 0, Iss 5, Pp 74-82 (2020)
The problem of numerical simulation of the gas flow with the combustion of atomized liquid fuel was solved (the equilibrium combustion model pdf was used along with the partially mixed mixture model) in the annular combustion chamber of a gas turbine
Externí odkaz:
https://doaj.org/article/7a46d7cc67934c9b95558b150426c600