Experimental Study on the Turbomachinery Trailing Edge Noise Reduction Based on Linear Cascade Test with Phased Array
Author:
Affiliation:
1. Northwestern Polytechnical University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2015-2824
Reference13 articles.
1. Observations on Fan Rotor Broadband Noise Characteristics
2. Fan Broadband Self Noise Prediction Model
3. A study of the silent flight of the owl
4. Aerodynamic noise of a serrated trailing edge
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3. Aeroacoustic investigation of asymmetric oblique trailing-edge serrations enlighted by owl wings;Physics of Fluids;2022-01
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