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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...

Deskribapen osoa

Gorde:
Xehetasun bibliografikoak
Egile Nagusiak: Mohamed Qenawy, Mohamed Taha, A.H. Abdelbaky Elbatran
Formatua: Artigo
Hizkuntza:Inglês
Argitaratua: Elsevier 2022-06-01
Saila:Case Studies in Thermal Engineering
Gaiak:
Sarrera elektronikoa:http://www.sciencedirect.com/science/article/pii/S2214157X22002519
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