Optimization of A Swirl with Impingement Compound Cooling Unit for A Gas Turbine Blade Leading Edge

In this article, a compound unit of swirl and impingement cooling techniques is designed to study the performance of flow and heat transfer using multi-conical nozzles in a leading-edge of a gas turbine blade. Reynolds Averaged Navier-Stokes equations and the Shear Stress Transport model are numeric...

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Bibliographic Details
Main Authors: Hamza Fawzy, Qun Zheng, Naseem Ahmad, Yuting Jiang
Format: Article
Language:English
Published: MDPI AG 2020-01-01
Series:Energies
Subjects:
Online Access:https://www.mdpi.com/1996-1073/13/1/210