Analysis of Gas Turbine Blade Cooling System

Amir Hossein Ghanizadeh, Amir Hossein (2009) Analysis of Gas Turbine Blade Cooling System. [Final Year Project] (Unpublished)

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As the turbine inlet temperature increases, the heat transferred to the turbine blade also increases. The operating temperatures are far above the permissible metal temperatures. Therefore, there is a critical need to cool the blades for safe operation. The cooling methods currently implemented in the turbine industry can be classified into two types: internal cooling and external cooling.

Item Type: Final Year Project
Subjects: T Technology > TJ Mechanical engineering and machinery
Departments / MOR / COE: Engineering > Mechanical
Depositing User: Users 5 not found.
Date Deposited: 11 Jan 2012 12:18
Last Modified: 25 Jan 2017 09:44

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