From the Blade Geometry to Prediction of Tonal Noise Component in Hover
Author:
Affiliation:
1. Technion Israel Institute of Technology
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2022-3076
Reference38 articles.
1. Noise due to turbulent flow past a trailing edge
2. Acoustic radiation from an airfoil in a turbulent stream
3. Towards a non-empirical trailing edge noise prediction model
4. Transient analysis of blade-vortex interaction noise
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