Zobrazeno 1 - 6
of 6
pro vyhledávání: '"I. S. Zubkov"'
Autor:
V. L. Blinov, I. S. Zubkov
Publikováno v:
Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, Vol 22, Iss 1, Pp 51-62 (2023)
The paper presents the results of one of the stages of creating a model of assessing and forecasting the operating characteristics of a transonic compressor due to erosive wear. A numerical model of a transonic compressor stage is constructed and ver
Externí odkaz:
https://doaj.org/article/b6ff4777157a4d1d8c7072fde7d35634
Publikováno v:
Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, Vol 20, Iss 4, Pp 7-19 (2022)
The paper presents the results of a stage of development of an analytical model for assessing the impact of various defects on the operation of an axial-flow compressor. Some recommendations on setting the numerical models for carrying out gas dynami
Externí odkaz:
https://doaj.org/article/f8e8623476cd4c3498f0d50613f13cb6
Publikováno v:
Известия высших учебных заведений: Проблемы энергетики, Vol 23, Iss 4, Pp 66-83 (2021)
THE PURPOSE. To study the issues of air intake system’s performance as the part of the gas turbines. To estimate the possibility of modeling different performance factors of air intake systems with numerical simulation methods. To develop the recom
Externí odkaz:
https://doaj.org/article/8cfbea5765d04cc4b6bdb73620cfe579
Autor:
V L Blinov, I S Zubkov
Publikováno v:
J. Phys. Conf. Ser.
Journal of Physics: Conference Series
Journal of Physics: Conference Series
This paper presents the compressor blade algorithm for predicting the defect influence on the characteristics of the stage, axial compressor or GTU as a whole. The developed model is based on the use of Bezier curves, with the control point coordinat
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::94023cf58aa557ed2ee5e29364e50aef
https://hdl.handle.net/10995/102306
https://hdl.handle.net/10995/102306
Publikováno v:
IOP Conference Series: Earth and Environmental Science. 990:012057
The current work presents the intermediate results of model development to assess the impact of various defects on the axial compressor operation. Recommendations for adjusting computational models are proposed to conduct gas-dynamic and strength stu
Autor:
I S Zubkov, V L Blinov
Publikováno v:
IOP Conference Series: Materials Science and Engineering. 1089:012004
The paper presents the key stages of developing a geometric model of the axial compressor blade. The model is based on Bezier curves, which are used to design the parts of airfoil and allow making local changes to the airfoil and blade geometry. This