Numerical Analysis of High-Altitude Inlet Air on Boundary Layer Flow Loss in an Aero-Engine Compressor

Numerical Analysis of High-Altitude Inlet Air on Boundary Layer Flow Loss in an Aero-Engine Compressor

A numerical analysis is performed to explore the high altitude and high Mach flight on the effect of wall boundary layer loss in the compressor. The accuracy for solution results by the application of the similarity criterion and parameter definition of the air inlet is compared with the existing ex...

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Bibliographic Details
Main Authors: Feng Wu, Limin Gao, Lu Yang, Aqiang Lin, Hai Zhang
Format: Article
Language:English
Published: MDPI AG 2020-08-01
Series:Energies
Subjects:
compressor
boundary layer
high Mach number
similarity criterion
flow loss
entropy increase
Online Access:https://www.mdpi.com/1996-1073/13/16/4155

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