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Analysis of Gas Turbine Blade Cooling System

Amir Hossein Ghanizadeh, Amir Hossein (2009) Analysis of Gas Turbine Blade Cooling System. UNSPECIFIED. (Unpublished)

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Abstract

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
Subject: T Technology > TJ Mechanical engineering and machinery
Divisions: Engineering > Mechanical
Depositing User: Users 5 not found.
Date Deposited: 11 Jan 2012 12:18
Last Modified: 25 Jan 2017 09:44
URI: http://utpedia.utp.edu.my/id/eprint/350

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