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pro vyhledávání: '"Yue-Fang Hsiao"'
Autor:
Yue-Fang Hsiao, Yui-Chuin Shiah
Publikováno v:
Aerospace, Vol 10, Iss 10, p 885 (2023)
The modeling of the turbine blades in aero-parts presents difficulties in conventional domain solution techniques, especially when internal cooling air passages and a thermal barrier coating (TBC) are applied. This paper presents a very efficient 3D
Externí odkaz:
https://doaj.org/article/887dc603835e4760ae351b678d90c39f
