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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| Autores principales: | , , |
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| Formato: | Artigo |
| Lenguaje: | Inglês |
| Publicado: |
Peoples’ Friendship University of Russia (RUDN University)
2019-12-01
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| Colección: | RUDN Journal of Engineering Research |
| Materias: | |
| Acceso en línea: | http://journals.rudn.ru/engineering-researches/article/viewFile/22672/17689 |
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