INVESTIGATION OF REMAINING USEFUL LIFE OF GAS TURBINE BLADE

The aim of this research is to investigate the remaining useful life of gas turbine blade. This investigation was done by predicting the turbine blades service life using Stress Rupture Test (SRT) under accelerated test conditions where the applied stresses to the specimen is between 400 MPa to 600...

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Bibliographic Details
Main Author: Osman, Muhammad Hafizuddin
Format: Final Year Project
Language:English
Published: IRC 2015
Subjects:
Online Access:http://utpedia.utp.edu.my/15717/1/Hafizuddin%2014760%20-%20Final%20Dissertation%20Report.pdf
http://utpedia.utp.edu.my/15717/
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Institution: Universiti Teknologi Petronas
Language: English

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