Effect of rotor axial blade loading distribution on compressor stability
Author:
Funder
National Natural Science Foundation of China
Academic Excellence Foundation of BUAA for PHD Students
National Major Science and Technology Projects of China
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference43 articles.
1. Numerical investigations of the separated transitional flow over compressor blades with different loading distributions;Wang;Aerosp. Sci. Technol.,2020
2. Tip leakage flow, tip aerodynamic loading and rotating instability in a subsonic high-speed axial flow compressor rotor;Chen;Aerosp. Sci. Technol.,2021
3. Loss reduction in axial-flow compressors through low-speed model testing;Wisler;J. Eng. Gas Turbines Power,1985
4. Blade loading and rotation effects on compressor rotor wake near end walls;Lakshminarayana;AIAA J.,1983
5. Effect of impeller blade loading on compressor stage performance in a high specific speed range;Shibata;J. Turbomach.,2012
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