Tip leakage flow, tip aerodynamic loading and rotating instability in a subsonic high-speed axial flow compressor rotor
Author:
Funder
National Natural Science Foundation of China
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference56 articles.
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3. Stall inception in an axial flow compressors;Day;J. Turbomach.,1993
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5. Three-dimensional through-flow modelling of axial flow compressor rotating stall and surge;Righi;Aerosp. Sci. Technol.,2018
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