Effect of casing treatment to switch the type of instability inception in a high-speed axial compressor
Author:
Funder
National Natural Science Foundation of China
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference26 articles.
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2. A theory of post-stall transients in axial compression systems: part II—application;Greitzer;J. Eng. Gas Turbines Power,1986
3. A method for assessing effects of circumferential flow distortion on compressor stability;Hynes;J. Turbomach.,1987
4. Active suppression of aerodynamic instabilities in turbomachines;Epstein;J. Propuls. Power,1989
5. Stall inception in axial compressors;McDougall;J. Turbomach.,1990
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