Design and Acoustic Efficacy of a Broadband Liner for the Inlet of the DGEN Aero-propulsion Research Turbofan
Author:
Affiliation:
1. NASA Glenn Research Center
2. NASA Langley Research Center
Publisher
American Institute of Aeronautics and Astronautics
Reference25 articles.
1. Nark, D. M., Jones, M. G., Sutliff, D. L., Ayle, E., and Ichihashi, F. "Improved Broadband Liner Optimization Appliedtothe AdvancedNoiseControlFan,"AIAA Paper2014-3103, 2014.
2. Modeling of Broadband Liners Applied to the Advanced Noise Control Fan
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