Effect of serrated trailing edge on boundary layer instability noise
Author:
Affiliation:
1. Delft University of Technology
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2015-2363
Reference15 articles.
1. Noise generated by airfoil profiles placed in a uniform laminar flow
2. Flow Field Around a Serrated Trailing Edge at Incidence
3. An experimental study of airfoil instability tonal noise with trailing edge serrations
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1. Experimental Investigation of Airfoil Instability Tonal Noise Reduction Using Structured Porous Trailing Edges;Applied Sciences;2024-04-02
2. Optimization of the Aeroacoustics and Aerodynamics of a Wind Turbine Airfoil with Serrations Using Multi-Criteria Decision Making;2023 10th International Conference on Recent Advances in Air and Space Technologies (RAST);2023-06-07
3. Review of Fluid Dynamic and Acoustic Performance of Biologically Inspired Passive Flow Control Trailing Edge Devices for Design Applications;55th AIAA Aerospace Sciences Meeting;2017-01-05
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