Numerical Study Of Heat Transfer In Cooling Passages Of Turbine Blade

Numerical Study Of Heat Transfer In Cooling Passages Of Turbine Blade

As the temperature of combustion gases is higher than the melting temperature of the turbine materials, cooling of turbine parts in a gas turbine engine is necessary for safe operation. Cooling methods investigated in this computational study included cooling flow losses. Film-cooling is one typica...

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Bibliographic Details
Main Authors:	Ahmed F. Khudheyer, Hussein T. Dhaiban
Format:	Article
Language:	English
Published:	University of Baghdad 2023-05-01
Series:	Journal of Engineering
Subjects:	heat and mass transfer, gas turbine cooling
Online Access:	https://joe.uobaghdad.edu.iq/index.php/main/article/view/2076

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