The Aerodynamic Profile as Acoustic Noise Generator
Author:
Affiliation:
1. Coleman Engineering Company,
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Link
http://arc.aiaa.org/doi/pdf/10.2514/8.2606
Reference7 articles.
1. The Aerodynamic Forces on Low Aspect Ratio Wings Oscillating in an Incompressible Flow
2. Smilg, B., and Wasserman, L. S., Application of Three-Dimensional Flutter Theory to Aircraft Structures, Air Force Technical Report No. 4798,July, 1942.
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1. Rotating blades and aerodynamic sound;Journal of Sound and Vibration;1973-06
2. Sources of Noise in Axial Flow Fans;The Journal of the Acoustical Society of America;1972-05
3. Problems of helicopter noise estimation and reduction;VTOL Research, Design, and Operations Meeting;1969-02-17
4. Some Experiments Related to the Noise from Boundary Layers;The Journal of the Acoustical Society of America;1957-03
5. Tecnical Notes;Journal of Jet Propulsion;1954-07
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