Cargando…

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...

Descripción completa

Detalles Bibliográficos
Autores principales: Du, Haifen, Mei, Ziyue, Zou, Jiayao, Jiang, Wei, Xie, Danmei
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2019
Materias:
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC7514218/
http://dx.doi.org/10.3390/e21101007