Numerical Investigation on the Performance of a Transonic Axial Compressor with Inlet Distortion and Low Reynolds Number

Numerical Investigation on the Performance of a Transonic Axial Compressor with Inlet Distortion and Low Reynolds Number

The performance and stability of the transonic fan stage with a nonuniform inflow is a key issue in aero engine operation, and the coupling of inlet distortion and low Reynolds numbers at high altitude creates more severe challenges to aero engines. This work used computational methods to explore th...

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Bibliographic Details
Main Authors: Zhiping Li, Xingyu Zhu, Zhaoqi Yan, Tianyu Pan
Format: Article
Language:English
Published: MDPI AG 2022-05-01
Series:Energies
Subjects:
aero-engine
compressor
distortion
low Reynolds number
numerical simulation
Online Access:https://www.mdpi.com/1996-1073/15/10/3612

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