Please use this identifier to cite or link to this item: http://bura.brunel.ac.uk/handle/2438/28653
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dc.contributor.authorChong, TP-
dc.contributor.authorMuhammad, C-
dc.date.accessioned2024-03-28T15:21:08Z-
dc.date.available2024-03-28T15:21:08Z-
dc.date.issued2024-04-26-
dc.identifierORCiD: Tze Pei Chong https://orcid.org/0000-0002-5272-3943-
dc.identifierORCiD: C. Muhammad https://orcid.org/0009-0008-5243-5379-
dc.identifier045157-
dc.identifier.citationChong, T.P. and Muhammad, C. (2024) 'On the Enhancement and Suppression of Turbulent Wall Pressure by Large Eddy Break Up Devices', Physics of Fluids, 36 (4), 045157, pp . 1 - 15. doi: 10.1063/5.0195041.en_US
dc.identifier.issn1070-6631-
dc.identifier.urihttps://bura.brunel.ac.uk/handle/2438/28653-
dc.descriptionAcknowledgement: A CC BY or equivalent licence is applied to the Author Accepted Manuscript arising from this submission, in accordance with the grant’s open access conditions. The authors would also like to thank the PhD studentship sponsored by the Thomas Gerald Gray Charitable Trust in the United Kingdom.en_US
dc.descriptionData Availability: The data that support the findings of this study are available from the corresponding author upon reasonable request.-
dc.description.abstractAn experimental study is presented on the application of Large Eddy BreakUp (LEBU) on a flat plate as a sourcetargeting device to perturb the wall pressure fluctuations of a turbulent boundary layer. When interacting with a LEBU wake, the wall pressure spectra can establish a self-similar behaviour against s′, which is a normalised separation distance between the LEBU’s trailing edge and the targeted location for aeroacoustics noise source mitigation. It is found that s′ >3is neededto achieve an overall reduction in the wall pressure fluctuations. The fundamental mechanism by which the LEBUcanreducethewall pressure fluctuation is investigated by studying the spatio-temporal evolution of turbulent spots. When the emanated LEBU wake is interacted with the outer part of turbulent spot, the shielding effect can always inhibit the turbulent fluids ejection from the spot’s leading edge. However, incursion of the high momentum f luids wall-sweeping event at the spot’s trailing edge can only be effectively prevented when s′ > 3.en_US
dc.description.sponsorshipThis research was funded, in whole or in part, by the Engineering and Physical Sciences Research Council in the United Kingdom through research grant No. EP/K002309/1 (Quiet Aerofoils of the Next Generation).en_US
dc.format.extent1 - 15-
dc.format.mediumPrint-Electronic-
dc.language.isoen_USen_US
dc.publisherAmerican Institute of Physicsen_US
dc.rightsCopyright © 2024 Author(s). Published under an exclusive license by AIP Publishing. This article may be downloaded for personal use only. Any other use requires prior permission of the author and the American Institute of Physics. The following article appeared in Chong, T.P. and Muhammad, C. (2024) 'On the Enhancement and Suppression of Turbulent Wall Pressure by Large Eddy Break Up Devices', Physics of Fluids, 36 (4), 045157, pp . 1 - 15, and may be found at https://doi.org/10.1063/5.0195041. A CC BY (or equivalent licence) is applied to the Author Accepted Manuscript arising from this submission, in accordance with the grant’s open access conditions (https://creativecommons.org/licenses/by/4.0/).-
dc.rights.urihttps://creativecommons.org/licenses/by/4.0/-
dc.titleOn the Enhancement and Suppression of Turbulent Wall Pressure by Large Eddy Break Up Devicesen_US
dc.typeArticleen_US
dc.date.dateAccepted2024-03-20-
dc.identifier.doihttps://doi.org/10.1063/5.0195041-
dc.relation.isPartOfPhysics of Fluids-
pubs.issue4-
pubs.publication-statusPublished-
pubs.volume36-
dc.identifier.eissn1089-7666-
dc.rights.licensehttps://creativecommons.org/licenses/by/4.0/legalcode.en-
dc.rights.holderThe Author(s)-
Appears in Collections:Dept of Mechanical and Aerospace Engineering Research Papers

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