Investigation of Noise Generated by a DU96 Airfoil
Author:
Affiliation:
1. Technological Institute of Aeronautics (ITA)
2. Stanford University
3. General Electric Company
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2012-2055
Reference47 articles.
1. Trailing edge noise prediction from measured surface pressures
2. A review of the theory of trailing edge noise
3. Broadband Self Noise from Loaded Fan Blades
4. Effect of Airfoil Aerodynamic Loading on Trailing Edge Noise Sources
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