The effect of tip clearance on the rotor-stator interaction and noise of marine 1.5-stage compressor
Author:
Affiliation:
1. College of Power and Energy Engineering, Harbin Engineering University, Harbin, People’s Republic of China
2. Department of Naval Architecture, Ocean & Marine Engineering, University of Strathclyde, Glasgow, UK
Funder
Fundamental Research Funds for the Central Universities
Publisher
Informa UK Limited
Subject
Ocean Engineering
Link
https://www.tandfonline.com/doi/pdf/10.1080/20464177.2023.2255337
Reference39 articles.
1. On the effect of the tip-clearance ratio on the aeroacoustics of a diffuser-augmented wind turbine
2. Active control of wind turbines through varying blade tip sweep
3. Effect of the rotor–stator gap variation on the tonal noise generated by axial-flow fans
4. Leakage Noise and Related Flow Pattern in a Low-Speed Axial Fan with Rotating Shroud
5. Experimental study of the effect of the rotor-stator gap variation on the tonal noise generated by low-speed axial fans
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1. Simulation research on aerodynamic noise characteristics of a compressor under different working conditions;The Journal of the Acoustical Society of America;2024-04-01
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