Study of the Microstructure of the Gas Turbine Internal Blade

High Pressure Turbine (HPT) first stage blade is the most important rotational components of aero-engine. It operatesat high temperature and under conditions of extreme environmental attack such as oxidation and corrosion, isespecially subjected to degradation by oxidation, corrosion and wear. Du...

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Bibliographic Details
Main Author: Ahmad, Nurul Najat
Format: Final Year Project
Language:English
Published: Universiti Teknologi Petronas 2011
Subjects:
Online Access:http://utpedia.utp.edu.my/8605/1/2011%20-%20Study%20of%20the%20microstructure%20of%20the%20gas%20turbine%20internal%20blade.pdf
http://utpedia.utp.edu.my/8605/
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