Flexible membrane type non-linear liner
Flexible membrane type non-linear liner
Acoustic liners are widely used passive noise reduction technology for aero-engine noise control. Traditional acoustic liners installed in an aero-engine are usually modelled as a Helmholtz resonator, an air-filled cavity sandwiched between a perforated plate and an acoustically rigid back sheet. For wavelengths much greater than the liner's geometrical dimensions, the air-filled cavity is regarded as a spring, and the volume of air inside the perforations of the face sheet as a mass, acting as a Single-Degree-Of-Freedom (SDOF). Such an SDOF liner design typically provides a narrow absorption bandwidth at a resonance frequency lower than a simple quarter-wave resonator. In this preliminary work, the acoustic properties of a novel liner concept called flexible slanted septum core have been studied experimentally. An overall increase in the absorption coefficient and a significant shift in the frequency range towards lower frequencies have been observed at moderate sound pressure levels (SPL). The shift in absorption frequency bandwidth is mainly attributed to the elastic constant and intrinsic damping of the flexible membrane-based perforated face sheet and slanted septum. Additionally , when excited with a high SPL sound source, the flexible liner concept showed much improved sound absorption with broadened frequency bandwidth, acting as a "non-linear" flexible membrane type liner.
Palani, Suresh
62cb4236-3b73-412f-9bee-8064a6e494c7
Subramanyam, Ramesh Raja
7ffe1b2a-a3ac-4433-9090-76babf8dafc4
Paruchuri, Chaitanya
5c1def64-6347-4be3-ac2d-b9f6a314b81d
Joseph, Phillip
9c30491e-8464-4c9a-8723-2abc62bdf75d
12 July 2023
Palani, Suresh
62cb4236-3b73-412f-9bee-8064a6e494c7
Subramanyam, Ramesh Raja
7ffe1b2a-a3ac-4433-9090-76babf8dafc4
Paruchuri, Chaitanya
5c1def64-6347-4be3-ac2d-b9f6a314b81d
Joseph, Phillip
9c30491e-8464-4c9a-8723-2abc62bdf75d
Palani, Suresh, Subramanyam, Ramesh Raja, Paruchuri, Chaitanya and Joseph, Phillip
(2023)
Flexible membrane type non-linear liner.
29th International Congress on Sound and Vibration, , Prague, Czech Republic.
09 Jul - 13 Aug 2023.
Record type:
Conference or Workshop Item
(Paper)
Abstract
Acoustic liners are widely used passive noise reduction technology for aero-engine noise control. Traditional acoustic liners installed in an aero-engine are usually modelled as a Helmholtz resonator, an air-filled cavity sandwiched between a perforated plate and an acoustically rigid back sheet. For wavelengths much greater than the liner's geometrical dimensions, the air-filled cavity is regarded as a spring, and the volume of air inside the perforations of the face sheet as a mass, acting as a Single-Degree-Of-Freedom (SDOF). Such an SDOF liner design typically provides a narrow absorption bandwidth at a resonance frequency lower than a simple quarter-wave resonator. In this preliminary work, the acoustic properties of a novel liner concept called flexible slanted septum core have been studied experimentally. An overall increase in the absorption coefficient and a significant shift in the frequency range towards lower frequencies have been observed at moderate sound pressure levels (SPL). The shift in absorption frequency bandwidth is mainly attributed to the elastic constant and intrinsic damping of the flexible membrane-based perforated face sheet and slanted septum. Additionally , when excited with a high SPL sound source, the flexible liner concept showed much improved sound absorption with broadened frequency bandwidth, acting as a "non-linear" flexible membrane type liner.
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Published date: 12 July 2023
Venue - Dates:
29th International Congress on Sound and Vibration, , Prague, Czech Republic, 2023-07-09 - 2023-08-13
Identifiers
Local EPrints ID: 480688
URI: http://eprints.soton.ac.uk/id/eprint/480688
PURE UUID: 2250dd52-90e0-435e-a57e-f05d84315042
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Date deposited: 08 Aug 2023 16:49
Last modified: 09 Aug 2023 01:57
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Contributors
Author:
Suresh Palani
Author:
Ramesh Raja Subramanyam
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