Recent Developments in the Aerodynamic Heat Transfer and Cooling Technology of Gas Turbines Endwalls

With an increased inlet gas temperature and the homogenization of the combustion chamber outlet temperature, the endwalls of gas turbines are exposed to extremely high heat loads. The complex flow structure of turbine endwalls makes it difficult to cool some regions of the endwalls, which can easily...

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Bibliographic Details
Main Authors: Rongdi Zhang, Pengchao Liu, Xirui Zhang, Wenxiong Xi, Jian Liu
Format: Article
Language:English
Published: MDPI AG 2023-08-01
Series:Aerospace
Subjects:
Online Access:https://www.mdpi.com/2226-4310/10/8/702