Experimental and numerical investigations on non-synchronous vibration and frequency lock-in of transonic compressor rotor blades
Author:
Funder
National Major Science and Technology Projects of China
Publisher
Elsevier BV
Reference31 articles.
1. Aeroelastic vibration analysis of a 1.5 stage compressor;Zheng;Propuls. Power Res.,2020
2. Influence of rotor-stator axial clearance on compressor rotating stall characteristics;Li;Aerosp. Sci. Technol.,2023
3. Evolution of the flow instabilities in an axial compressor rotor with large tip clearance: an experimental and URANS study;Wang;Aerosp. Sci. Technol.,2020
4. Tip flow on rotating instability on an axial compressor with different tip clearance;Yang;Aerosp. Sci. Technol.,2023
5. Self- excited blade vibration experimentally investigated in transonic compressors—acoustic resonance;Holzinger;ASME J. Turbomach.,2016
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