Zobrazeno 1 - 3
of 3
pro vyhledávání: '"P. N. Brodnev"'
Autor:
Yu. B. Galerkin, A. F. Rekstin, V. B. Semenovskiy, L. N. Marenina, O. A. Solovyeva, A. A. Drozdov, L. N. Rozanov, P. N. Brodnev
Publikováno v:
Омский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение", Vol 6, Iss 2, Pp 9-20 (2022)
The process of designing a new turboexpander unit using the Universal modeling method consists of several stages: preliminary design, optimization, calculation of gas dynamic characteristics. The development of modern computational methods and the
Externí odkaz:
https://doaj.org/article/872ec0ee0c9c4e4e8a5a3ed39f5f14bd
Autor:
A. I. Borovkov, Yu. B. Galerkin, O. A. Solovieva, A. A. Drozdov, A. F. Rekstin, V. B. Semenovsky, P. N. Brodnev
Publikováno v:
Омский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение", Vol 4, Iss 4, Pp 16-27 (2020)
The mathematical model underlying the program for calculating and designing axial compressors is presented. The process of calculating the pressure loss in the elements of the axial compressor stage flow path is described. The loss coefficient cons
Externí odkaz:
https://doaj.org/article/05540d79ad1647558c088ac6eb0b9502
Autor:
Yu. B. Galerkin, A. F. Rekstin, Aleksandr Drozdov, O. A. Solovieva, V. B. Semenovsky, A. I. Borovkov, P. N. Brodnev
Publikováno v:
Journal of Physics: Conference Series. 1891:012019
This paper presents a mathematical model underlying the program for calculating and designing axial compressors. The process of calculating pressure loss in the elements of the axial compressor’s stage flow path is described. The loss coefficient c
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a5b765803e5d3b59620e60876ca365f8
https://doi.org/10.1088/1742-6596/1891/1/012019
https://doi.org/10.1088/1742-6596/1891/1/012019