Downstream Perforations for the Reduction of Turbulence-Aerofoil Interaction Noise: Part II - Theoretical Investigation
Author:
Affiliation:
1. University of Cambridge
2. University of Southampton
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2021-2147
Reference21 articles.
1. Reduction of Airfoil Turbulence-Impingement Noise by Means of Leading-Edge Serrations and/or Porous Material
2. A Semi-analytic and Experimental Study of Porous Leading Edges
3. Aerodynamic noise from a poroelastic edge with implications for the silent flight of owls
4. On the noise prediction for serrated leading edges
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1. Aeroacoustics research in Europe: The CEAS-ASC report on 2022 highlights;Journal of Sound and Vibration;2024-01
2. Effect of porosity on Curle’s dipolar sources on an aerofoil in turbulent flow;Journal of Sound and Vibration;2023-01
3. Downstream porosity for the reduction of turbulence–aerofoil interaction noise;Journal of Sound and Vibration;2022-12
4. Investigation of Curle's Dipolar Sources on a Porous Airfoil Interacting with Incoming Turbulence;28th AIAA/CEAS Aeroacoustics 2022 Conference;2022-06-13
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