Application of the Source Term Method and Fan-Shaped Hole for Cooling Performance Improvement in a High-Pressure Turbine

This study presents the arrangement design of the cooling hole and the application of a fan-shaped hole to improve the cooling performance of the high-pressure turbine. To this end, the first stage nozzle vane of the energy efficient engine (E3) was selected as the base model, and for efficient desi...

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Autores principales:	Sangook Jun, Dong-Ho Rhee, Young Seok Kang, Heeyoon Chung, Jae-Hwan Kim
Formato:	Artigo
Lenguaje:	Inglês
Publicado:	MDPI AG 2022-09-01
Colección:	Energies
Materias:	cooling design fan-shaped film cooling hole cooling hole arrangement design source term method approximate model turbine nozzle
Acceso en línea:	https://www.mdpi.com/1996-1073/15/19/6943
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