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...
שמור ב:
| Principais autores: | , , |
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| פורמט: | Artigo |
| שפה: | Inglês |
| יצא לאור: |
Peoples’ Friendship University of Russia (RUDN University)
2019-12-01
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| סדרה: | RUDN Journal of Engineering Research |
| נושאים: | |
| גישה מקוונת: | http://journals.rudn.ru/engineering-researches/article/viewFile/22672/17689 |
| תגים: |
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