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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...

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Principais autores: Vladimir K. Mamaev, Leonid V. Vinogradov, Petr P. Oschepkov
Formato: Artigo
Idioma:Inglês
Publicado: Peoples’ Friendship University of Russia (RUDN University) 2019-12-01
Series:RUDN Journal of Engineering Research
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Acceso en liña:http://journals.rudn.ru/engineering-researches/article/viewFile/22672/17689
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