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Applied Mathematics and Nonlinear Sciences
Volume 9 (2024): Numero 1 (Gennaio 2024)
Accesso libero
Optimization of CDA Blade Based on Surrogate Model
Weishuai Meng
Weishuai Meng
Sino-European Institute of Aviation Engineering, Civil Aviation University of China
Tianjin, China
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Meng, Weishuai
,
Shuming Li
Shuming Li
Aeronautical Engineering Institute, Civil Aviation University of China
Tianjin, China
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Li, Shuming
,
Hong Zhang
Hong Zhang
Sino-European Institute of Aviation Engineering, Civil Aviation University of China
Tianjin, China
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Zhang, Hong
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Qingguo Kong
Qingguo Kong
Sino-European Institute of Aviation Engineering, Civil Aviation University of China
Tianjin, China
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Kong, Qingguo
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Qiang Zhao
Qiang Zhao
Sino-European Institute of Aviation Engineering, Civil Aviation University of China
Tianjin, China
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Zhao, Qiang
05 nov 2024
Applied Mathematics and Nonlinear Sciences
Volume 9 (2024): Numero 1 (Gennaio 2024)
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Pubblicato online:
05 nov 2024
Ricevuto:
28 giu 2024
Accettato:
28 set 2024
DOI:
https://doi.org/10.2478/amns-2024-3048
Parole chiave
Surrogate model
,
Compressor
,
CDA blade
,
Performance prediction
,
Blade optimization
© 2024 Weishuai Meng et al., published by Sciendo
This work is licensed under the Creative Commons Attribution 4.0 International License.
