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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Detaylı Bibliyografya
Asıl Yazarlar: Mohamed Qenawy, Mohamed Taha, A.H. Abdelbaky Elbatran
Materyal Türü: Artigo
Dil:Inglês
Baskı/Yayın Bilgisi: Elsevier 2022-06-01
Seri Bilgileri:Case Studies in Thermal Engineering
Konular:
Film cooling
Unsteady flow structure
Fast-PSP
Internal crossflow
Shaped holes
Online Erişim:http://www.sciencedirect.com/science/article/pii/S2214157X22002519
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