Parametric Airfoil Design and Sensitivity Analysis for Turbulent Boundary-Layer Trailing-Edge Noise Reduction
Author:
Affiliation:
1. University of California, Davis, California 95616
Funder
Hyundai Motor Company
China Scholarship Council
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J060096
Reference29 articles.
1. BrooksT. F.PopeD. S.MarcoliniM. A. “Airfoil Self-Noise and Prediction,” NASA RP 1218, 1989.
2. Location and quantification of noise sources on a wind turbine
3. Trailing-Edge Noise from Hovering Rotors
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