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Conjugate Heat Transfer Investigation on Swirl-Film Cooling at the Leading Edge of a Gas Turbine Vane

Numerical calculation of conjugate heat transfer was carried out to study the effect of combined film and swirl cooling at the leading edge of a gas turbine vane with a cooling chamber inside. Two cooling chambers (C(1) and C(2) cases) were specially designed to generate swirl in the chamber, which...

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Publicado en:Entropy (Basel)
Autores principales: Du, Haifen, Mei, Ziyue, Zou, Jiayao, Jiang, Wei, Xie, Danmei
Formato: Artigo
Lenguaje:Inglês
Publicado: MDPI 2019
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Acceso en línea:https://ncbi.nlm.nih.gov/pmc/articles/PMC7514218/
https://ncbi.nlm.nih.govhttp://dx.doi.org/10.3390/e21101007
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