Please use this identifier to cite or link to this item: http://bura.brunel.ac.uk/handle/2438/22829
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dc.contributor.authorWoodhead, PC-
dc.contributor.authorChong, TP-
dc.contributor.authorJoseph, P-
dc.contributor.authorVathylakis, A-
dc.date.accessioned2021-06-12T12:40:40Z-
dc.date.available2021-06-12T12:40:40Z-
dc.date.issued2021-07-05-
dc.identifier152-
dc.identifier.citationWoodhead, P.C., Chong, T.P., Joseph, P.F. and Vathylakis, A. (2021) 'Aerofoil self-noise radiations subjected to serration flap angles' Experiments in Fluids, 62, 152, pp. 1-22. doi: 10.1007/s00348-021-03239-y.en_US
dc.identifier.issn0723-4864-
dc.identifier.urihttps://bura.brunel.ac.uk/handle/2438/22829-
dc.description.abstractCopyright © 2021 The Author(s). Besides the investigation of the aeroacoustics responses of an asymmetric aerofoil subjected to serrated trailing edge flap angles from negative (flap-down) to positive (flap-up), this paper also provides a new perspective on the physical mechanisms of broadband noise reduction by a serrated trailing edge. The blade-loading effect, which is a function of the length and flap angle for a straight/non-serrated trailing edge flat plate, plays a considerable role in the self-noise radiation that is hitherto less recognised. When the same trailing edge flat plate is cut into a sawtooth serration shape, the self-noise reduction will be underpinned simultaneously by both the serration effect (dominant) and the blade-loading effect. The results demonstrate that the far-field radiation of a serrated aerofoil can be manipulated significantly depending on the direction of the flap angle. In the flap-down configuration, the blade-loading will become a negative factor that causes a deterioration of the noise reduction performance across the entire frequency range. In the flap-up configuration, three spectral frequencies zones can be defined. At the low-frequency zone, the diminished cross-flow at the sawtooth gaps will impede the noise reduction capability. At the central-frequency zone, the re-distribution of the turbulence sources and reduction in the turbulence spanwise length scales will enhance the noise reduction performance. Improvement in the noise performance can also be achieved at the high-frequency zone owing to the lack of interaction between the cross-flow and sawtooth structure. A new concept is positively demonstrated by varying the serration flap angle as a periodic function across the spanwise direction (spanwise wavy serration). When compared to a non-flap serrated trailing edge, the spanwise wavy serration is found to further increase the noise reduction level between the central and high-frequency regions. [Graphical abstract available on full text].-
dc.description.sponsorshipUK Engineering and Physical Sciences Research Council (EPSRC)en_US
dc.description.sponsorshipUK Engineering and Physical Sciences Research Council (EPSRC) research grant (EP/N018737/1) “Quiet aerofoils of the next-generation”; EPSRC Doctoral Training Partnership (DTP) PhD studentships (first and fourth authors).-
dc.format.extent1 - 22 (22)-
dc.format.mediumPrint-Electronic-
dc.language.isoenen_US
dc.publisherSpringer Natureen_US
dc.rightsCopyright © The Author(s) 2021. Open Access: This article is licensed under a Creative Commons Attribution 4.0 International License, which permits use, sharing, adaptation, distribution and reproduction in any medium or format, as long as you give appropriate credit to the original author(s) and the source, provide a link to the Creative Commons licence, and indicate if changes were made. The images or other third party material in this article are included in the article's Creative Commons licence, unless indicated otherwise in a credit line to the material. If material is not included in the article's Creative Commons licence and your intended use is not permitted by statutory regulation or exceeds the permitted use, you will need to obtain permission directly from the copyright holder. To view a copy of this licence, visit https://creativecommons.org/licenses/by/4.0/.-
dc.rights.urihttps://creativecommons.org/licenses/by/4.0/-
dc.titleAerofoil Self Noise Radiations Subjected to Serration Flap Anglesen_US
dc.typeArticleen_US
dc.identifier.doihttps://doi.org/10.1007/s00348-021-03239-y-
dc.relation.isPartOfExperiments in Fluids: experimental methods and their applications to fluid flow-
pubs.publication-statusPublished online-
pubs.volume62-
dc.identifier.eissn1432-1114-
Appears in Collections:Dept of Mechanical and Aerospace Engineering Research Papers

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