Evaluating the Acoustic Benefits of Over-the-Rotor Acoustic Treatments Installed on the Advanced Noise Control Fan
Author:
Affiliation:
1. Air Force Research Laboratory
2. University of Notre Dame
3. NASA Glenn Research Center
4. University of Southampton
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2017-3872
Reference12 articles.
1. Jones, M.G., Parrott, T.L., Sutliff, D.L., and Hughes, C.E. "Assessment of Soft Vane and Metal Foam Engine Noise Reduction Concepts", AIAA-2009-3142.
2. Elliott, D.M., Woodward, R.P., Podboy, G.G. "Acoustic Performance of Novel Fan Noise Reduction Technologies for a High Bypass Model Turbofan at Simulated Flight Conditions," AIAA 2009-3140.
3. Hughes, C.E., Gazzaniga, J.A. "Effect of Two Advanced Noise Reduction Technologies on the Aerodynamic Performance of an Ultra High Bypass Ratio Fan," AIAA 2009-3139.
4. Low-Speed Fan Noise Attenuation from a Foam-Metal Liner
5. High-Speed Turbofan Noise Reduction Using Foam-Metal Liner Over-the-Rotor
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