The effect of non-uniform combustion temperature profile on thermal fatigue cracking of an air-cooled gas turbine vane-Reference-Cited by-同舟云学术

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The effect of non-uniform combustion temperature profile on thermal fatigue cracking of an air-cooled gas turbine vane

Published:2019-11 Issue: Volume:105 Page:766-780
ISSN:1350-6307
Container-title:Engineering Failure Analysis
language:en
Short-container-title:Engineering Failure Analysis

Author:

Yousefabad Elham kamouri,Asadi Saeed,Savadkouhi Payam,Sedaghat Omid,Bakhshi Ali

Publisher

Elsevier BV

Subject

General Engineering,General Materials Science

Reference12 articles.

1. Proceedings of the International Gas Turbine Congress 1999 Kobe;Kouichi,1999

2. Gas Turbine Blade Failures- Causes, Avoidance and Troubleshooting;Meher-Homji,2018

3. Common failures in gas turbine blade: a critical review;Rani;Int. J. Eng. Sci. Res. Technol.,2018

4. Microstructural changes during high temperature service of a cobalt-based superalloy first stage nozzle;Luna Ramirez;Adv. Mater. Sci. Eng.,2016

5. Development of repair mechanism of FSX-414 based 1st stage nozzle of gas turbine;Rahman,2017

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