Investigation of straightforward impedance eduction method on single-degree-of-freedom acoustic liners
Investigation of straightforward impedance eduction method on single-degree-of-freedom acoustic liners
In order to address the current aircraft noise problem, the knowledge of impedance of acoustic liners subjected to high-intensity sound and grazing flow is of crucial importance to the design of high-efficiency acoustic nacelles. To this end, the present study is twofold. Firstly, the StraightForward impedance eduction Method (SFM) is evaluated by the strategy that the impedance of a liner specimen is firstly experimentally educed on a flow duct using the SFM, and then its accuracy is checked by comparing the numerical prediction with the measured wall sound pressure of the flow duct. Secondly, the effects of grazing flow and high-intensity sound on the impedance behavior of two single-layer liners are investigated based on comparisons between educed impedance and predictions by three impedance models. The performance of the SFM is validated by showing that the educed impedance leads to excellent agreement between the simulation and the measured wall sound pressure for different grazing flow Mach numbers and Sound Pressure Levels (SPLs) and over a frequency range from 3000 Hz down to 500 Hz. The grazing flow effect generally has the tendency that the acoustic resistance exhibits a slight decrease before it increases linearly with an increase in Mach, predicted successfully by the sound-vortex interaction theoretical model and the Kooi semi-empirical impedance model. However, the Goodrich semi-empirical impedance model gives only a simple linear relation of acoustic resistance starting from Mach zero. Additionally, when the SPL increases from 110 to 140 dB in the present investigation, the acoustic resistance exhibits a significant increase at all frequencies in the absence of flow; however, the resistance decreases slightly under a grazing flow of Mach 0.117. It indicates that the SPL effect can be greatly inhibited when flow is present, and the grazing flow effect can be reduced partly as well at a relatively high SPL.
Acoustic liner, Experimental validation, Grazing flow effect, High sound intensity effect, Impedance eduction, Numerical evaluation, Straightforward impedance eduction method
2221-2233
Qiu, Xianghai
28fa27ed-5fbb-4545-8bd3-22925a18f2e4
Xin, Bo
b6e7200e-6589-48ea-acc8-e7f287bb7c5c
Wu, Long
9787473b-a81a-47ce-a696-22afa8c2204b
Meng, Yang
da00d8a9-6a60-426b-90e2-90d77d5190c8
Jing, Xiaodong
9bd7313a-4ab2-4387-839e-4c1583f61531
Qiu, Xianghai
28fa27ed-5fbb-4545-8bd3-22925a18f2e4
Xin, Bo
b6e7200e-6589-48ea-acc8-e7f287bb7c5c
Wu, Long
9787473b-a81a-47ce-a696-22afa8c2204b
Meng, Yang
da00d8a9-6a60-426b-90e2-90d77d5190c8
Jing, Xiaodong
9bd7313a-4ab2-4387-839e-4c1583f61531
Qiu, Xianghai, Xin, Bo, Wu, Long, Meng, Yang and Jing, Xiaodong
(2018)
Investigation of straightforward impedance eduction method on single-degree-of-freedom acoustic liners.
Chinese Journal of Aeronautics, 31 (12), .
(doi:10.1016/j.cja.2018.08.014).
Abstract
In order to address the current aircraft noise problem, the knowledge of impedance of acoustic liners subjected to high-intensity sound and grazing flow is of crucial importance to the design of high-efficiency acoustic nacelles. To this end, the present study is twofold. Firstly, the StraightForward impedance eduction Method (SFM) is evaluated by the strategy that the impedance of a liner specimen is firstly experimentally educed on a flow duct using the SFM, and then its accuracy is checked by comparing the numerical prediction with the measured wall sound pressure of the flow duct. Secondly, the effects of grazing flow and high-intensity sound on the impedance behavior of two single-layer liners are investigated based on comparisons between educed impedance and predictions by three impedance models. The performance of the SFM is validated by showing that the educed impedance leads to excellent agreement between the simulation and the measured wall sound pressure for different grazing flow Mach numbers and Sound Pressure Levels (SPLs) and over a frequency range from 3000 Hz down to 500 Hz. The grazing flow effect generally has the tendency that the acoustic resistance exhibits a slight decrease before it increases linearly with an increase in Mach, predicted successfully by the sound-vortex interaction theoretical model and the Kooi semi-empirical impedance model. However, the Goodrich semi-empirical impedance model gives only a simple linear relation of acoustic resistance starting from Mach zero. Additionally, when the SPL increases from 110 to 140 dB in the present investigation, the acoustic resistance exhibits a significant increase at all frequencies in the absence of flow; however, the resistance decreases slightly under a grazing flow of Mach 0.117. It indicates that the SPL effect can be greatly inhibited when flow is present, and the grazing flow effect can be reduced partly as well at a relatively high SPL.
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More information
Accepted/In Press date: 17 May 2018
e-pub ahead of print date: 5 September 2018
Additional Information:
Funding Information:
The research work was co-supported by the National Natural Science Foundation of China (No. 51576009) and the Projects of International Cooperation and Exchanges National Natural Science Foundation of China (Nos. 11661141020 and 51711530036).
Keywords:
Acoustic liner, Experimental validation, Grazing flow effect, High sound intensity effect, Impedance eduction, Numerical evaluation, Straightforward impedance eduction method
Identifiers
Local EPrints ID: 485878
URI: http://eprints.soton.ac.uk/id/eprint/485878
ISSN: 1000-9361
PURE UUID: 5ff09c08-6c6f-4596-8cbe-88a5a105cd0a
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Date deposited: 03 Jan 2024 19:33
Last modified: 18 Mar 2024 03:51
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Author:
Xianghai Qiu
Author:
Bo Xin
Author:
Long Wu
Author:
Yang Meng
Author:
Xiaodong Jing
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