Results of conjugate modeling and analysis of the thermal state of a high-pressure turbine blade

Results of conjugate modeling and analysis of the thermal state of a high-pressure turbine blade

Numerical modeling for the purpose of receiving the temperature field of cooled rotor blades and its improvement is an integral process of modern design of gas turbine engines since the issue of cooling at gas temperature at the combustion chamber outlet over 1800-2000 K is becoming one of the key o...

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Bibliographic Details
Main Authors: V. N. Matveev, S. A. Melnikov, G. M. Popov, V. M. Zubanov, I. A. Kudryashov, A. I. Shcherban
Format: Article
Language:English
Published: Samara National Research University 2023-05-01
Series:Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение
Subjects:
aircraft engine
turbine cooling
cooled blades
cooling efficiency coefficient
Online Access:https://journals.ssau.ru/vestnik/article/viewFile/19344/9607

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