טוען...
Unsteady adiabatic film cooling effectiveness behind shaped holes
Gas turbine as a vital component requires higher inlet temperature to improve its thermal efficiency, and thus a thin coolant film spreads over the blade surface to isolate it from hot gases. However, such coolant intensively interacts with the mainstream, leading to highly unsteady coolant coverage...
שמור ב:
| Main Authors: | , , |
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| פורמט: | Artigo |
| שפה: | Inglês |
| יצא לאור: |
Elsevier
2022-06-01
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| סדרה: | Case Studies in Thermal Engineering |
| נושאים: | |
| גישה מקוונת: | http://www.sciencedirect.com/science/article/pii/S2214157X22002519 |
| תגים: |
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