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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...
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| 主要な著者: | , , |
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| フォーマット: | Artigo |
| 言語: | Inglês |
| 出版事項: |
Elsevier
2022-06-01
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| シリーズ: | Case Studies in Thermal Engineering |
| 主題: | |
| オンライン･アクセス: | http://www.sciencedirect.com/science/article/pii/S2214157X22002519 |
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