Blade-Geometry Considerations in Analytical Gust-Airfoil Interaction Noise Models
Author:
Affiliation:
1. École Centrale de Lyon
2. Airbus
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2010-3799
Reference15 articles.
1. High frequency thin-airfoil theory for subsonic flow
2. Acoustic radiation from an airfoil in a turbulent stream
3. Advanced turboprop noise prediction based on recent theoretical results
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