Permeable Structures for Leading Edge Noise Reduction
Author:
Affiliation:
1. Aalen University
2. University of Erlangen-Nürnberg
3. Brandenburg University of Technology
4. University of Southampton
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2021-2192
Reference42 articles.
1. Reduction of blade-vortex interaction noise through porous leading edge
2. Experimental assessment of the noise generated at the leading edge of porous airfoils using microphone array techniques
3. Reduction of Airfoil Turbulence-Impingement Noise by Means of Leading-Edge Serrations and/or Porous Material
4. Reduction of Turbulence Interaction Noise Through Airfoils With Perforated Leading Edges
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2. Experimental Investigations of the Aeroacoustic Interactions of Fan Blade Skew, Leading Edge Serrations and Inflow Turbulence;30th AIAA/CEAS Aeroacoustics Conference (2024);2024-05-30
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