Efficacy of a Multiple Degree of Freedom Acoustic Liner Installed in the Bypass of a Scale Model High Speed Fan
Author:
Affiliation:
1. NASA Glenn Research Center
2. NASA Langley Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2016-3005
Reference15 articles.
1. 1H.H. Hubbard, editor,Aeroacoustics of Flight Vehicles: Theory and Practice: Volume1, NASA Reference Publication 1258, Vol 1, WRDC Technical Report 90-3052.
2. 2D.M. Nark, and M.G. Jones, "Broadband Liner Optimization for the Source Diagnostic Test Fan," AIAA Paper 2012-2195.
3. 3D.M. Nark, F. Farassat, D.S. Pope, and V. Vatsa, "The Development of the Ducted Fan Noise Propagation and Radiation Code CDUCTLaRC", AIAA Paper 2003-3242.
4. 4D.M. Nark, M.G. Jones, and D.L. Sutliff, "Improved Broadband Liner Optimization Applied to the Advanced Noise Control Fan", AIAA-2014-3103.
5. D.L. Sutliff, M.G. Jones, and D.M.Nark, "In-Duct and Far-field Experimental Measurements from the ANCF for the Purpose of Improved Broadband Liner Optimization", AIAA-2014-3231.
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