An Investigation of the Promotion of the Aerodynamic Performance of a Supersonic Compressor Cascade Using a Local Negative-Curvature Ramp

An Investigation of the Promotion of the Aerodynamic Performance of a Supersonic Compressor Cascade Using a Local Negative-Curvature Ramp

Shockwaves induce considerable flow separation loss; it is essential to reduce this using the flow control method. In this manuscript, a method for suppressing flow separation in turbomachinery through a constant adverse-pressure gradient was investigated. The first-passage shock was split into a co...

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Bibliographic Details
Main Authors: Yongzhen Liu, Zhen Fan, Weiwei Cui, Qiang Zhou, Jianzhong Xu
Format: Article
Language:English
Published: MDPI AG 2025-05-01
Series:Applied Sciences
Subjects:
negative-curvature profile
constant adverse-pressure gradient
shockwave/boundary layer interaction
supersonic compressor cascade
Online Access:https://www.mdpi.com/2076-3417/15/10/5664
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