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Further Development and Assessment of a Broadband Liner Optimization ProcessThe utilization of advanced fan designs (including higher bypass ratios) and shorter engine nacelles has highlighted a need for increased fan noise reduction over a broader frequency range. Thus, improved broadband liner designs must account for these constraints and, where applicable, take advantage of advanced manufacturing techniques that have opened new possibilities for novel configurations. This work focuses on the use of an established broadband acoustic liner optimization process to design a variable-depth, multi-degree of freedom liner for a high speed fan. Specifically, in-duct attenuation predictions with a statistical source model are used to obtain optimum impedance spectra over the conditions of interest. The predicted optimum impedance information is then used with acoustic liner modeling tools to design a liner aimed at producing impedance spectra that most closely match the predicted optimum values. The multi-degree of freedom design is carried through design, fabrication, and testing. In-duct attenuation predictions compare well with measured data and the multi-degree of freedom liner is shown to outperform a more conventional liner over a range of flow conditions. These promising results provide further confidence in the design tool, as well as the enhancements made to the overall design process.
Document ID
20160009094
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Nark, Douglas M.
(NASA Langley Research Center Hampton, VA, United States)
Jones, Michael G.
(NASA Langley Research Center Hampton, VA, United States)
Sutliff, Daniel L.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
July 17, 2016
Publication Date
May 30, 2016
Subject Category
Acoustics
Report/Patent Number
NF1676L-22922
Report Number: NF1676L-22922
Meeting Information
Meeting: AIAA/CEAS Aeroacoustis Conference
Location: Lyon
Country: France
Start Date: May 30, 2016
End Date: June 1, 2016
Sponsors: American Inst. of Aeronautics and Astronautics, National Oceanic and Atmospheric Administration
Funding Number(s)
WBS: WBS 081876.02.07.03.01.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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