Film Cooling Performance and Superposition Method of an Actual Turbine Vane at High Freestream Turbulence

This study aims to enhance the understanding of film cooling performance in an actual turbine vane by investigating influencing factors and developing more precise numerical prediction methods. Pressure sensitive paint (PSP) testing and Reynolds-Averaged Navier–Stokes (RANS) simulations were conduct...

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Detalles Bibliográficos

Principais autores:	Peng Chu, Yongfeng Sui, Bin Dai, Jibing Lan, Wenyang Shao, Binbin Xue, Xiliang Xu, Zhenping Feng
Formato:	Artigo
Idioma:	Inglês
Publicado:	MDPI AG 2025-06-01
Series:	Aerospace
Assuntos:	gas turbine film cooling fan-shaped holes multirow superposition method numerical simulation
Acceso en liña:	https://www.mdpi.com/2226-4310/12/6/533
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