Aircraft engine nozzle guide vane surface temperature optimization

An optimization method based on the sensitivity of global and local geometric parameters is proposed to improve the cooling efficiency of E3 engine nozzle guide vane. For 29 geometric parameters that affect the vane maximum temperature in the cooling design, the sensitivity ranking of them is firstl...

Descripción completa

Detalles Bibliográficos
Autores principales: Decang, Lou, Mengjun, Wang, Jinhua, Liang, Jun, Zeng, Xiaoyang, Huang, Along, Chen
Formato: Online Artículo Texto
Lenguaje:English
Publicado: Elsevier 2023
Materias:
Research Article
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC10559985/
https://www.ncbi.nlm.nih.gov/pubmed/37809483
http://dx.doi.org/10.1016/j.heliyon.2023.e20222

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC10559985/
https://www.ncbi.nlm.nih.gov/pubmed/37809483
http://dx.doi.org/10.1016/j.heliyon.2023.e20222

Ejemplares similares