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...
| Main Authors: | , |
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| Format: | Conference or Workshop Item |
| Language: | English English |
| Published: |
Institute of Physics Publishing
2018
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| Subjects: | |
| Online Access: | http://irep.iium.edu.my/65970/ http://irep.iium.edu.my/65970/ 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 |
Internet
http://irep.iium.edu.my/65970/http://irep.iium.edu.my/65970/
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