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The Number of Subgrain Boundaries in the Airfoils of Heat-Treated Single-Crystalline Turbine Blades

In the present study, the dendrites deflection mechanism from the mold walls were subjected to verification regarding its heat-treated turbine rotor blades. The number of macroscopic low-angle boundaries created on the cross-section of the blades’ airfoil near the tip was experimentally determined a...

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Detalles Bibliográficos
Autores principales: Krawczyk, Jacek, Bogdanowicz, Włodzimierz, Sieniawski, Jan
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2020
Materias:
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC7792965/
https://www.ncbi.nlm.nih.gov/pubmed/33375104
http://dx.doi.org/10.3390/ma14010008