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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...
Autores principales: | Decang, Lou, Mengjun, Wang, Jinhua, Liang, Jun, Zeng, Xiaoyang, Huang, Along, Chen |
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Formato: | Online Artículo Texto |
Lenguaje: | English |
Publicado: |
Elsevier
2023
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Materias: | |
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 |
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