Wird geladen...
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...
Gespeichert in:
| Hauptverfasser: | , , |
|---|---|
| Format: | Artigo |
| Sprache: | Inglês |
| Veröffentlicht: |
Elsevier
2022-06-01
|
| Schriftenreihe: | Case Studies in Thermal Engineering |
| Schlagworte: | |
| Online Zugang: | http://www.sciencedirect.com/science/article/pii/S2214157X22002519 |
| Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|