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Assessment of Radiated Fan Noise Prediction Capabilities Using Static Engine Test DataThis paper describes further assessment of the CDUCT-LaRC code via comparison with static engine test data. In an effort to improve confidence in the use of CDUCT-LaRC for liner optimization studies addressing realistic three-dimensional geometries, inlet radiated fan noise predictions were performed at 54% and 87% engine speed settings. Predictions were then compared with far-field measurements to assess the approach and implementation. The particular configurations were chosen to exercise the three-dimensional capability of CDUCT-LaRC and it s applicability to realistic configurations and conditions. At the 54% engine speed setting, the predictions capture the general directivity and acoustic treatment effects quite well. Comparisons of the predicted and measured directivity at the 87% power setting were more problematic. This was likely due in part to the difficulties in source specification and possibly the nonlinear nature of buzz-saw tones at this engine operating condition. Overall, the approach captured the basic trends and provided a conservative estimate of liner effects from which relative performance metrics could be inferred.
Document ID
20110012468
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Nark, Douglas M.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 8, 2013
Publication Date
June 6, 2011
Subject Category
Acoustics
Report/Patent Number
NF1676L-11679
Report Number: NF1676L-11679
Meeting Information
Meeting: 17th AIAA/CEAS Aeroacoustics Conference
Location: Portland, OR
Country: United States
Start Date: June 6, 2011
End Date: June 8, 2011
Sponsors: National Oceanic and Atmospheric Administraion, American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 561581.02.08.07.18.14
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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