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Experimental Evaluation of Tuned Chamber Core Panels for Payload Fairing Noise ControlAnalytical models have been developed to predict the sound absorption and sound transmission loss of tuned chamber core panels. The panels are constructed of two facesheets sandwiching a corrugated core. When ports are introduced through one facesheet, the long chambers within the core can be used as an array of low-frequency acoustic resonators. To evaluate the accuracy of the analytical models, absorption and sound transmission loss tests were performed on flat panels. Measurements show that the acoustic resonators embedded in the panels improve both the absorption and transmission loss of the sandwich structure at frequencies near the natural frequency of the resonators. Analytical predictions for absorption closely match measured data. However, transmission loss predictions miss important features observed in the measurements. This suggests that higher-fidelity analytical or numerical models will be needed to supplement transmission loss predictions in the future.
Document ID
20160006606
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Schiller, Noah H.
(NASA Langley Research Center Hampton, VA, United States)
Allen, Albert R.
(NASA Langley Research Center Hampton, VA, United States)
Herlan, Jonathan W.
(Mississippi Univ. University, MS, United States)
Rosenthal, Bruce N.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
May 26, 2016
Publication Date
October 27, 2015
Subject Category
Acoustics
Report/Patent Number
NF1676L-22468
Report Number: NF1676L-22468
Meeting Information
Meeting: Aerospace Testing Seminar
Location: Los Angeles, CA
Country: United States
Start Date: October 27, 2015
End Date: October 29, 2015
Sponsors: Aerospace Corp.
Funding Number(s)
WBS: WBS 585777.08.50.66.23.10
Distribution Limits
Public
Copyright
Public Use Permitted.
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