Fan Noise Reduction with Increased Bypass Nozzle Area
Author:
Affiliation:
1. NASA Glenn Research Center, Cleveland, Ohio 44135
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.19359
Reference19 articles.
1. Effect of Inflow Control on Inlet Noise of a Cut-on Fan
2. The effect of throttling on forward radiated fan noise
3. An Improved Correlation for the Broadband Noise of High-speed Fans
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