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Assessment of Acoustic Behavior for Perforate-Over-Large-Cell LinersThis study explores the effects of increasing the cell size for large-cell acoustic liners. Tests are conducted in the NASA Langley Grazing Flow Impedance Tube to evaluate liners with increasingly larger cell dimensions (up to 2” x 4” cross-section). Conventional impedance eduction confirms that liners with 2” x 3” cells (or larger) must be evaluated using nonlocally reacting assumptions. In addition, due to the sound propagation within cavities, the liners must be modeled using higher fidelity techniques. Thus, grazing flow duct and acoustic liner are modeled simultaneously using finite element methods. The
facesheet is modeled using a transfer impedance, while the rest of the domain is modeled using the convected Helmholtz equation. The acoustic pressures predicted are shown to compare favorably with those measured in the Grazing Flow Impedance Tube.
Document ID
20230005980
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Martha C. Brown
(Langley Research Center Hampton, Virginia, United States)
Chelsea Solano
(Langley Research Center Hampton, Virginia, United States)
Jordan R. Kreitzman
(Langley Research Center Hampton, Virginia, United States)
Michael G. Jones
(Langley Research Center Hampton, Virginia, United States)
Date Acquired
April 18, 2023
Subject Category
Acoustics
Meeting Information
Meeting: AIAA AVIATION Forum and Exposition
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
large diameter
large cell liner
large cavity
acoustics
acoustic liners
COMSOL
ACTRAN
ACTRAN/TM
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