Please use this identifier to cite or link to this item: http://bura.brunel.ac.uk/handle/2438/31370
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dc.contributor.authorWoodhead, P-
dc.contributor.authorChong, TP-
dc.contributor.authorJoseph, P-
dc.contributor.authorWissink, J-
dc.contributor.authorChaitanya, P-
dc.date.accessioned2025-06-02T07:10:13Z-
dc.date.available2025-06-02T07:10:13Z-
dc.date.issued2025-
dc.identifierORCiD: Philip Woodhead https://orcid.org/0000-0002-8116-858X-
dc.identifierORCiD: Tze Pei Chong https://orcid.org/0000-0002-5272-3943-
dc.identifierORCiD: Jan Wissink https://orcid.org/0000-0002-3608-7449-
dc.identifier.citationWoodhead, P. et al. (2025) 'On the slit trailing edges for aerofoil self-noise reduction', Journal of Fluid Mechanics, 0 (accepted, in press)en_US
dc.identifier.issn0022-1120-
dc.identifier.urihttps://bura.brunel.ac.uk/handle/2438/31370-
dc.description...en_US
dc.description.abstract...en_US
dc.description.sponsorshipThis work is supported by the UK Engineering and Physical Sciences Research Council (EPSRC) research grant (EP/N018737/1) “Quiet aerofoils of the next-generation”. We would also like to express our appreciation for the PhD studentship funded by the EPSRC Doctoral Training Partnership (DTP) awarded to the first author.en_US
dc.format.medium1 - 32-
dc.format.mediumPrint-Electronic-
dc.language.isoenen_US
dc.publisherCambridge University Pressen_US
dc.titleOn the slit trailing edges for aerofoil self-noise reductionen_US
dc.typeArticleen_US
dc.relation.isPartOfJournal of Fluid Mechanics-
pubs.issue00-
pubs.publication-statusAccepted-
pubs.volume0-
dc.identifier.eissn1469-7645-
Appears in Collections:Dept of Mechanical and Aerospace Engineering Embargoed Research Papers

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