Aerodynamic Optimization and Mechanism Investigation on Performance Improvements in a Transonic Compressor Cascade

In this paper, a transonic compressor cascade was optimized to improve its aerodynamic performance. A new blade parameterization method with 16 control variables was first proposed to fit the shapes of the suction and the pressure side, as well as the leading edge. Then, the Kriging surrogate-model-...

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Bibliographic Details
Main Authors: Fanjie Meng, Chaoxuan Gong, Kunhang Li, Jin Xiong, Jingyin Li, Penghua Guo
Format: Article
Language:English
Published: MDPI AG 2023-02-01
Series:Machines
Subjects:
Online Access:https://www.mdpi.com/2075-1702/11/2/244