Optimization of heat transfer on thermal barrier coated gas turbine blade

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Optimization of heat transfer on thermal barrier coated gas turbine blade

In the field of Aerospace Propulsion technology, material required to resist the maximum temperature. In this paper, using thermal barrier coatings (TBCs) method in gas turbine blade is used to protect hot section component from high-temperature effect to extend the service life and reduce the ma...

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Bibliographic Details
Main Authors:	Aabid, Abdul, Khan, Sher Afghan
Format:	Proceeding Paper
Language:	English English
Published:	Institute of Physics Publishing 2018
Subjects:	TA401 Materials of engineering and construction TJ Mechanical engineering and machinery
Online Access:	http://irep.iium.edu.my/65970/ http://irep.iium.edu.my/65970/1/65970_Optimization%20of%20Heat%20Transfer%20on%20Thermal%20Barrier_conference%20article.pdf http://irep.iium.edu.my/65970/2/65970_Optimization%20of%20Heat%20Transfer%20on%20Thermal%20Barrier_scopus.pdf

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