Determination of Ranges of Unstable Operation of Axial Compressor for Aircraft Turbine Engines

Currently, strict requirements are set for aircraft turbine engine performance, which requires introducing larger, more complex, and more loaded compressors. In sub-assemblies designed in this manner, a vital challenge is to maintain stable compressor operation across wide range of operating conditi...

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Bibliographic Details
Main Authors: Adam KOZAKIEWICZ, Maciej ADAMCZYK, Maciej MAJCHER
Format: Article
Language:English
Published: Military University of Technology, Warsaw 2022-03-01
Series:Problemy Mechatroniki
Subjects:
Online Access:http://promechjournal.pl/gicid/01.3001.0015.8103