Optimization Turbine Blade Cooling by Applying Jet Impingement Cooling Channels

Optimization Turbine Blade Cooling by Applying Jet Impingement Cooling Channels

The aim of this paper is to optimize turbine blade cooling channels by applying jet impingement Method. The selection of experiment data for NASA 3CX turbine blade, and 3D model using solidworks software and create computational fluid dynamics (CFD) simulations used to model the coolant flow and tem...

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Bibliographic Details
Main Authors: Elmenshawy Adham Ahmed Awad Elsayed, Alomar Iyad, Arshad Ali
Format: Article
Language:English
Published: Sciendo 2023-06-01
Series:Transport and Telecommunication
Subjects:
conjugate heat transfer
thermal performance
turbine blade cooling channels
Online Access:https://doi.org/10.2478/ttj-2023-0026

Internet

https://doi.org/10.2478/ttj-2023-0026

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