Cargando...
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...
Guardado en:
| Autores principales: | , , |
|---|---|
| Formato: | Artigo |
| Lenguaje: | Inglês |
| Publicado: |
Elsevier
2022-06-01
|
| Colección: | Case Studies in Thermal Engineering |
| Materias: | |
| Acceso en línea: | http://www.sciencedirect.com/science/article/pii/S2214157X22002519 |
| Etiquetas: |
Agregar Etiqueta
Sin Etiquetas, Sea el primero en etiquetar este registro!
|