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Structural Acoustic Prediction and Interior Noise Control TechnologyThis report documents the results of Task 14, "Structural Acoustic Prediction and Interior Noise Control Technology". The task was to evaluate the performance of tuned foam elements (termed Smart Foam) both analytically and experimentally. Results taken from a three-dimensional finite element model of an active, tuned foam element are presented. Measurements of sound absorption and sound transmission loss were taken using the model. These results agree well with published data. Experimental performance data were taken in Boeing's Interior Noise Test Facility where 12 smart foam elements were applied to a 757 sidewall. Several configurations were tested. Noise reductions of 5-10 dB were achieved over the 200-800 Hz bandwidth of the controller. Accelerometers mounted on the panel provided a good reference for the controller. Configurations with far-field error microphones outperformed near-field cases.
Document ID
20020019842
Acquisition Source
Langley Research Center
Document Type
Contractor Report (CR)
Authors
Mathur, G. P.
(Boeing Co. Long Beach, CA United States)
Chin, C. L.
(Boeing Co. Long Beach, CA United States)
Simpson, M. A.
(Boeing Co. Long Beach, CA United States)
Lee, J. T.
(Boeing Co. Long Beach, CA United States)
Palumbo, Daniel L.
Date Acquired
September 7, 2013
Publication Date
November 1, 2001
Subject Category
Acoustics
Report/Patent Number
NAS 1.26:211247
NASA/CR-2001-211247
Report Number: NAS 1.26:211247
Report Number: NASA/CR-2001-211247
Funding Number(s)
PROJECT: RTOP 706-81-14-01
CONTRACT_GRANT: NAS1-97040
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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