Please use this identifier to cite or link to this item: http://bura.brunel.ac.uk/handle/2438/28491
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dc.contributor.authorScholz, MM-
dc.contributor.authorArcondoulis, E-
dc.contributor.authorWoodhead, PC-
dc.contributor.authorChong, TP-
dc.contributor.authorSmith, E-
dc.date.accessioned2024-03-08T09:37:19Z-
dc.date.available2024-03-08T09:37:19Z-
dc.date.issued2023-06-08-
dc.identifierORCiD: Philip C. Woodhead https://orcid.org/0000-0002-8116-858X-
dc.identifierORCiD: Tze Pei Chong https://orcid.org/0000-0002-5272-3943-
dc.identifierORCiD: Edward R Smith https://orcid.org/0000-0002-7434-5912-
dc.identifierAIAA 2023-3926-
dc.identifier.citationScholz, M.M. et al. (2023) 'Structured Porous Coated Cylinder Modifications Based on Internal Flow Field Data', AIAA AVIATION 2023 Forum, San Diego, CA and Online, 12-16 June, AIAA 2023-3926, pp. 1 - 17. doi: 10.2514/6.2023-3926.en_US
dc.identifier.isbn978-1-62410-704-7-
dc.identifier.urihttps://bura.brunel.ac.uk/handle/2438/28491-
dc.descriptionSession: Acoustic / Fluid Dynamics Interactions IIen_US
dc.descriptionView Video Presentation: https://doi.org/10.2514/6.2023-3926.vid-
dc.description.abstractPorous coated cylinders have been proven to reduce vortex shedding tones relative to a bare cylinder. However, many porous treatments are based on the use of very complex, open-cell structures to manipulate turbulent flow. Due to complex geometries the physical mechanisms which can be drawn are problematic to investigate due to a typically randomised porous structure. The novel 3D printed Structured Porous Coated Cylinder (SPCC), which mimics the acoustics of open-cell foam's noise closely, absolves this issue thereby allowing improved observability and modifications. This study aims to draw from previous works and to investigate modified SPCCs to further understand the internal flows which attenuate fundamental vortex shedding tones. The initial study highlighted presented a preliminary analysis on the acoustic far-field of cylindrical structures and the validation against prior works. Following on from this, this paper highlights the modifications to the existing SPCC structure to affect the regions of stagnated flow within the porous layers, to investigate how these internal flows have impacted the vortex shedding attenuating capacity of the SPCC. Conducted at Brunel University London, the acoustic data shown confirms the ability of the SPCC to significantly reduce turbulent shedding noise over its bare cylinder counterparts and the three modified SPCCs proved the importance of the streamwise communication in the internal structure of the SPCC and that the stagnation regions as stipulated by earlier studies can be filled which retains the acoustic performance and most likely reduces the drag. Lastly, the removal of the ability for the flow to travel in the spanwise direction within the SPCC has been shown to improve the acoustic far field radiation over the original SPCC.en_US
dc.description.sponsorshipThe authors would like to thank the EPSRC for the financial support from the Doctoral Training Partnership (DTP); Engineering & Physical Sciences Research Council (EP/V006886/1) QUiet Aerofoil with ADaptive PORous Surfaces (QUADPORS).en_US
dc.format.extent1 - 17-
dc.format.mediumElectronic-
dc.language.isoen_USen_US
dc.publisherAmerican Institute of Aeronautics and Astronauticsen_US
dc.relation.urihttps://doi.org/10.2514/6.2023-3926.vid-
dc.rightsThis is the accepted manuscript version of a conference paper which has been published in final form on AIAA Electronic Library at https://doi.org/10.2514/6.2023-3926, Copyright © 2023 by Max Scholz, Elias Arcondoulis, Philip Woodhead, Tze Pei Chong, Edward Smith. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. All rights reserved. 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 ISBN 978-1-62410-704-7 to initiate your request. See also AIAA Rights and Permissions https://www.aiaa.org/randp.-
dc.rights.urihttps://www.aiaa.org/publications/Open-Access-
dc.sourceAIAA AVIATION 2023 Forum-
dc.sourceAIAA AVIATION 2023 Forum-
dc.subjectflow Conditions-
dc.subjectvortex shedding phenomena-
dc.subjectstreamwise velocity-
dc.subjectacoustic measurement-
dc.subjectporous materials-
dc.subject3D printing-
dc.subjectpower spectral density-
dc.subjectshear layers-
dc.subjectsound pressure level-
dc.subjectwind tunnels-
dc.titleStructured Porous Coated Cylinder Modifications Based on Internal Flow Field Dataen_US
dc.typeConference Paperen_US
dc.identifier.doihttps://doi.org/10.2514/6.2023-3926-
dc.relation.isPartOfAIAA AVIATION 2023 Forum-
pubs.publication-statusPublished-
dc.rights.holderMax Scholz, Elias Arcondoulis, Philip Woodhead, Tze Pei Chong, Edward Smith.-
Appears in Collections:Dept of Mechanical and Aerospace Engineering Research Papers

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FullText.pdfThis is the accepted manuscript version of a conference paper which has been published in final form on AIAA Electronic Library at https://doi.org/10.2514/6.2023-3926, Copyright © 2023 by Max Scholz, Elias Arcondoulis, Philip Woodhead, Tze Pei Chong, Edward Smith. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. All rights reserved. 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 ISBN 978-1-62410-704-7 to initiate your request. See also AIAA Rights and Permissions https://www.aiaa.org/randp.9.87 MBAdobe PDFView/Open


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