Optimal Design and Analysis of a High-Load Supersonic Compressor Based on a Surrogate Model

Optimal Design and Analysis of a High-Load Supersonic Compressor Based on a Surrogate Model

To explore the internal flow mechanism and improve the performance of a supersonic compressor, an efficient global optimization design method was developed for an axial flow compressor and applied in the optimization design of a prototype supersonic compressor. Based on the multiple circular arc (MC...

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Bibliographic Details
Main Authors: Shiji Zhou, Shengfeng Zhao, Chuangxin Zhou, Yunfeng Wu, Hang Yuan, Xingen Lu
Format: Article
Language:English
Published: MDPI AG 2023-04-01
Series:Aerospace
Subjects:
supersonic compressors
aerodynamic optimization
surrogate model
multi-objective optimization
shock loss
boundary layer separation loss
Online Access:https://www.mdpi.com/2226-4310/10/4/364

Internet

https://www.mdpi.com/2226-4310/10/4/364

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