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Preliminary Design of a Distributed Facesheet Acoustic Liner for Broadband Acoustic AttenuationThe purpose of this study is to investigate the acoustic performance of a liner with a distributed facesheet and a uniform depth core for broadband attenuation. The distributed facesheet is comprised of a cluster of three distinct cell resonators of varying hole diameter and porosity replicated over the active liner treatment area. A target frequency range of 1000 to 2000 Hz and an attenuation metric of 10 dB are chosen. An optimizer is used to determine the optimal facesheet designs for flow conditions of Mach 0.0 and Mach 0.3. The samples are tested in the Grazing Flow Impedance Tube at NASA Langley Research Center. The two liners are shown to achieve at least 10 dB attenuation over frequency ranges of 700 and 400 Hz, respectively, when tested at their respective designed flow speeds. This study demonstrate that a distributed facesheet with a uniform depth core can be successfully used to achieve broadband sound absorption.
Document ID
20230006773
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Martha C. Brown
(Langley Research Center Hampton, Virginia, United States)
Douglas M. Nark
(Langley Research Center Hampton, Virginia, United States)
Michael G. Jones
(Langley Research Center Hampton, Virginia, United States)
Date Acquired
May 3, 2023
Subject Category
Acoustics
Meeting Information
Meeting: AIAA AVIATION Forum 2023
Location: San Diego, CA
Country: US
Start Date: June 12, 2023
End Date: June 16, 2023
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 081876.02.07.50.10.02.03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
NASA Peer Committee
Keywords
acoustic liners
distributed facesheet
variable facesheet
broadband liner
broadband attenuation
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