Analysis of the thermal insulation performance of turbine blade thermal barrier coatings considering inlet non-uniformity

The gases discharged from the new generation of lean-burn combustors usually have hot streaks (HS) and swirls. The thermal performance of rotor thermal barrier coatings (TBCs) exhibits significant non-constant behavior due to inlet non-uniformity and blade row interaction. To investigate the non-con...

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Detalhes bibliográficos

Principais autores:	Wei Liu, Gang Yan, Cong Li, Zhiyuan Liu, Li Yang, Yichun Zhou
Formato:	Artigo
Idioma:	Inglês
Publicado em:	Elsevier 2024-01-01
coleção:	Case Studies in Thermal Engineering
Assuntos:	Thermal barrier coatings Hot streak Swirl Hot spot Thermal insulation effectiveness
Acesso em linha:	http://www.sciencedirect.com/science/article/pii/S2214157X23011784
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