Scaling of airfoil self-noise using measured flow parameters
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.8896
Reference13 articles.
1. Trailing edge noise prediction from measured surface pressures
2. Aerodynamic sound generation by turbulent flow in the vicinity of a scattering half plane
3. Discrete tones of isolated airfoils
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