Загрузка...
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...
Сохранить в:
| Главные авторы: | , , |
|---|---|
| Формат: | Artigo |
| Язык: | Inglês |
| Опубликовано: |
Elsevier
2022-06-01
|
| Серии: | Case Studies in Thermal Engineering |
| Предметы: | |
| Online-ссылка: | http://www.sciencedirect.com/science/article/pii/S2214157X22002519 |
| Метки: |
Добавить метку
Нет меток, Требуется 1-ая метка записи!
|