Comparison of finlet rails and fences for trailing edge noise reduction in NACA0012 aerofoil
Author:
Affiliation:
1. University of Southampton
2. Queen Mary University of London
3. The University of Manchester
4. Virginia Polytechnic Institute and State University
5. Florida Atlantic University
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2022-3015
Reference11 articles.
1. Gruber,M.“Airfoilnoisereductionbyedgetreatments,”Ph.D.thesis,022012.
2. Aerodynamic noise from a poroelastic edge with implications for the silent flight of owls
3. Computational study of the effect of structural compliance on the noise radiated from an elastic trailing-edge
4. Measurement of the noise generation at the trailing edge of porous airfoils
5. Experimental investigation of the impact of porous parameters on trailing-edge noise
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