Bio-Inspired Finlets for the Reduction of Marine Rotor Noise
Author:
Affiliation:
1. Virginia Polytechnic Institute and State University
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2017-3867
Reference16 articles.
1. Aerodynamic noise of a serrated trailing edge
2. Reduction of Wind Turbine Noise Using Optimized Airfoils and Trailing-Edge Serrations
3. Experimental Investigations in Low-Noise Trailing Edge Design.
4. The Silent Flight of Owls
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