Improved Broadband Liner Optimization Applied to the Advanced Noise Control FanThe broadband component of fan noise has grown in relevance with the utilization of increased bypass ratio and advanced fan designs. Thus, while the attenuation of fan tones remains paramount, the ability to simultaneously reduce broadband fan noise levels has become more desirable. This paper describes improvements to a previously established broadband acoustic liner optimization process using the Advanced Noise Control Fan rig as a demonstrator. 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 liners aimed at producing impedance spectra that most closely match the predicted optimum values. Design selection is based on an acceptance criterion that provides the ability to apply increased weighting to specific frequencies and/or operating conditions. Constant-depth, double-degree of freedom and variable-depth, multi-degree of freedom designs are carried through design, fabrication, and testing to validate the efficacy of the design process. Results illustrate the value of the design process in concurrently evaluating the relative costs/benefits of these liner designs. This study also provides an application for demonstrating the integrated use of duct acoustic propagation/radiation and liner modeling tools in the design and evaluation of novel broadband liner concepts for complex engine configurations.
Document ID
20150000537
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)
Ayle, Earl (Hexcel Corp. Casa Grande, AZ, United States)
Ichihashi, Fumitaka (Hexcel Corp. Casa Grande, AZ, United States)
Date Acquired
January 16, 2015
Publication Date
June 16, 2014
Subject Category
Acoustics
Report/Patent Number
NF1676L-17755Report Number: NF1676L-17755
Meeting Information
Meeting: AIAA/CEAS Aeroacoustics Conference
Location: Atlanta, GA
Country: United States
Start Date: June 16, 2014
End Date: June 20, 2014
Sponsors: Council of European Aerospace Societies, American Inst. of Aeronautics and Astronautics