Modeling the set of blade profiles of a gas turbine engine

In the development of gas turbine engines (GTE) it is necessary to simulate the flow section of blade machines (turbines, compressors). At the same time, it is rational to use previously designed profiles and set of profiles with high aerodynamic and efficient performance. This is due to the fact th...

Full description

Bibliographic Details
Main Authors: Vladimir K. Mamaev, Leonid V. Vinogradov, Petr P. Oschepkov
Format: Article
Language:English
Published: Peoples’ Friendship University of Russia (RUDN University) 2019-12-01
Series:RUDN Journal of Engineering Research
Subjects:
Online Access:http://journals.rudn.ru/engineering-researches/article/viewFile/22672/17689