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Extending Acoustic Liner Bandwidth with Simple Embedded SeptaAn acoustic liner design incorporating single-hole perforate septa was evaluated by the NASA Langley Liner Physics Team. The design, termed the ‘Simplified Septa’ concept, incorporates embedded septa as found in traditional, multidegree-of-freedom liners. Generally, such septa are composed of multihole perforates or porous mesh, whereas this concept uses septa with one hole per cell. An optimization scheme was employed to determine septa placement and hole diameters based on a target impedance cost function. Versions of the concept are tested in the NASA Langley Normal Incidence Tube (NIT) to determine impedance and absorption spectra for swept tonal excitation at 120 and 140 dB. Experimental results are compared to predictions from a liner model based on the Zwikker-Kosten Transmission Line (ZKTL) code and show good agreement for no-flow conditions.
Document ID
20240004795
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Brian M Howerton
(Langley Research Center Hampton, Virginia, United States)
Jordan Kreitzman
(Langley Research Center Hampton, United States)
Chelsea Solano
(Florida State University Tallahassee, United States)
Date Acquired
April 17, 2024
Subject Category
Acoustics
Meeting Information
Meeting: 30th AIAA/CEAS Aeroacoustics
Location: Rome
Country: IT
Start Date: June 4, 2024
End Date: June 7, 2024
Sponsors: Council of European Aerospace Societies, American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 081876.02.07.19.01.02.01
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
NASA Technical Management
Keywords
acoustics
liner
perforate
2DOF
MDOF
Septum
NIT
impedance
optimization
viscous dissipation
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