Prediction of Surface Pressure Spectrum at the Aerofoil Trailing Edge Treated With Canopies
Author:
Affiliation:
1. University of Southampton
2. Queen Mary University of London
3. Brunel University London
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2024-3286
Reference14 articles.
1. Bio-inspired canopies for the reduction of roughness noise
2. Bioinspired Trailing-Edge Noise Control
3. Turbulent boundary-layer wall-pressure fluctuations on smooth and rough walls
4. Blake,W.K."Chapter2-EssentialsofTurbulent WallPressureFluctuations,"Mechanicsof Flow-Induced Sound and Vibration, Volume2(Second Edition), edited by W. K. Blake,Academic Press, 2017, secondedition ed., pp.81-177. https://doi.org/https://doi.org/10.1016/B978-0-12-809274-3.00002-7, URL https://www.sciencedirect.com/science/article/pii/ B9780128092743000027.
5. Analytical models of the wall-pressure spectrum under a turbulent boundary layer with adverse pressure gradient
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