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Publikováno v:
Омский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение", Vol 2, Iss 3, Pp 21-25 (2018)
A mathematical model for the interaction of a gas environment with the surfaces of the impeller of turbogenerator compressor is developed. The study of the characteristic of power losses at various rotational speeds of the rotor is provided. Recomm
Externí odkaz:
https://doaj.org/article/e3e8ec1a7fc845659f133621a7c34a9a
