Noise and Surface Pressure Response of an Airfoil to Incident Turbulence
Author:
Affiliation:
1. United Technologies Research Center, East Hartford, Conn.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.58845
Reference39 articles.
1. Airfoil Theory for Non-Uniform Motion
2. The influence of solid boundaries upon aerodynamic sound
3. Sources of noise in axial flow fans
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