Vortex Noise of Isolated Airfoils
Author:
Affiliation:
1. United Aircraft Research Laboratories, East Hartford, Conn.
2. Sikorsky Aircraft Division, Stratford, Conn.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.60229
Reference15 articles.
1. Sources of noise in axial flow fans
2. On the Aerodynamic Noise of a Rigid Flat Plate Moving at Zero Incidence
3. A Study of Vanes Singing in Water
4. Investigation of the Wing-Wake Frequency with Application of the Strouhal Number
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