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pro vyhledávání: '"Artyom A. Levikhin"'
Publikováno v:
Naučno-tehničeskij Vestnik Informacionnyh Tehnologij, Mehaniki i Optiki, Vol 22, Iss 5, Pp 1016-1024 (2022)
A numerical method for calculating the thrust of a wide-range rocket engine nozzle has been developed. This type of engine is equipped with an annular nozzle with a flat central body and is designed to operate in the upper atmosphere and in vacuum. T
Externí odkaz:
https://doaj.org/article/f9a6461919c7493d88797c86d6f0ed76
