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Publikováno v:
Havacılık ve Uzay Teknolojileri Dergisi, Vol 17, Iss 2, Pp 89-106 (2024)
The priority technological direction of thermal protection of hot section components, basically turbine parts is the development of thermal barrier coatings (TBCs) in order to improve the operational performance of aero gas turbine engines (GTEs). Th
Externí odkaz:
https://doaj.org/article/8b2b4fa75d1540cd833c9560a95ecb97