Please use this identifier to cite or link to this item: http://bura.brunel.ac.uk/handle/2438/29921
Title: Turbulent Noise Sources Reduction by Large-Eddy Breakup Devices and Riblets
Other Titles: Turbulent Noise Sources Reduction by LEBU and Riblets
Authors: Muhammad, C
Chong, TP
Issue Date: 11-Nov-2024
Publisher: American Institute of Aeronautics and Astronautics (AIAA)
Citation: Muhammad, C. and Chong, T.P. (2024) 'Turbulent Noise Sources Reduction by Large-Eddy Breakup Devices and Riblets', AIAA Journal, 0 (ahead of print), pp. 1 - 13. doi: 10.2514/1.J063388.
Abstract: An experimental study is presented on the application of large-eddy breakup (LEBU) on a flat plate as an outer layer source-targeting device to mitigate the wall pressure fluctuations and lateral coherence length scale of a turbulent boundary-layer developed at zero pressure gradient. Both represent the prominent noise sources for the trailing-edge noise radiation. When a LEBU is placed strategically at the outer part of a turbulent boundary-layer, the wall pressure spectra can establish a self-similar behavior against 𝑠′, which is a normalized separation distance between the LEBU’s trailing-edge and the targeted location for noise mitigation. It is found that 𝑠′ has to be greater than 3 to achieve an overall reduction in the wall pressure fluctuations. What appears to be the optimal LEBU configuration for the mitigation of wall pressure fluctuations, however, will not be reciprocated in the lateral coherence length. The combined effect would render the LEBU rather ineffective to reduce the frequency-integrated, overall noise radiation. Our previous study has confirmed that riblets, a near-wall source-targeting device, is more effective in the mitigation of the lateral coherence length. Under the principle of non-interference, a combination of riblets and LEBU demonstrates that reduction of the frequency-integrated, overall noise radiation can be achieved, again at 𝑠′ > 3.
URI: https://bura.brunel.ac.uk/handle/2438/29921
DOI: https://doi.org/10.2514/1.J063388
ISSN: 0001-1452
Other Identifiers: ORCD: Tze Pei Chong https://orcid.org/0000-0002-5272-3943
Appears in Collections:Dept of Mechanical and Aerospace Engineering Research Papers

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FullText.pdfThis is the accepted manuscript version of an article which has been published in final form on AIAA Electronic Library, Published online Open Access 11 November 2024 on AIAA Electronic Library at https://doi.org/10.2514/1.J063388, Copyright © 2024 by Tze Pei Chong. For the purpose of open access, the authors have applied a Creative Commons Attribution 4.0 International License (CC BY) licence to any Author Accepted Manuscript version arising to meet UKRI terms and conditions. Author accepted manuscript self-archived with permission of the AIAA per https://www.aiaa.org/publications/Open-Access. All requests for copying and permission to reprint should be submitted to CCC at https://www.copyright.com; employ the eISSN 1533-385X to initiate your request. See also AIAA Rights and Permissions: https://www.aiaa.org/randp.10.02 MBAdobe PDFView/Open


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