Please use this identifier to cite or link to this item: http://bura.brunel.ac.uk/handle/2438/29658
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dc.contributor.authorBhardwaj, M-
dc.contributor.authorChong, TP-
dc.contributor.authorParuchuri, C-
dc.contributor.authorJoseph, P-
dc.coverage.spatialRome, Italy-
dc.date.accessioned2024-09-03T15:13:23Z-
dc.date.available2024-09-03T15:13:23Z-
dc.date.issued2024-05-30-
dc.identifierORCiD: Tze Pei Chong https://orcid.org/0000-0002-5272-3943-
dc.identifierAIAA 2024-3045-
dc.identifier.citationBhardwaj, M. et al. (2024) 'Noise decomposition of dual synchronized propellers in hover', 30th AIAA/CEAS Aeroacoustics Conference, 2024, Rome, Italy, 4-7 June, AIAA 2024-3045, pp. 1 - 11. doi: 10.2514/6.2024-3045.en_US
dc.identifier.isbn978-1-62410-720-7-
dc.identifier.urihttps://bura.brunel.ac.uk/handle/2438/29658-
dc.descriptionPaper no. AIAA 2024-3045, Session: Propeller‚ Rotorcraft and V/STOL Noise IIIen_US
dc.description.abstractThis experimental study investigates the acoustic characteristics of dual propellers in the side-by-side configuration, and addresses the impact of blade tip-to-tip separation distances and relative blade-to-blade phase angles on the tonal noise generation with a specially designed propeller rig. The parametric study of co-rotating and counter-rotating configurations is performed to emphasize the effect and importance of phase synchronization in producing the tonal components, such as the first Blade Pass Frequency (BPF). The linearity of acoustic interference for the side-by-side propellers is investigated through the principle of superimposition. A unique noise decomposition algorithm for various rotation angles is developed to understand the directional behavior of the synchronized propellers. The responses of the first BPF noise radiation as a function of the rotation angle under different combinations of rotating direction and blade-to-blade phase angle have been established.en_US
dc.format.extent1 - 11-
dc.format.mediumElectronic-
dc.languageEnglish-
dc.language.isoen_USen_US
dc.publisherAmerican Institute of Aeronautics and Astronautics, Inc.en_US
dc.rightsThis is the accepted manuscript version of a conference paper which has been published in final form on 30 May 2024 in the AIAA Electronic Library at https://doi.org/10.2514/6.2024-3045, Copyright © 2024 by the American Institute of Aeronautics and Astronautics, Inc. 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.source30th AIAA/CEAS Aeroacoustics Conference (2024)-
dc.source30th AIAA/CEAS Aeroacoustics Conference (2024)-
dc.subjectcounter rotating propellers-
dc.subjectoverall sound pressure level-
dc.subjectunsteady flows-
dc.subjectaerodynamic interference-
dc.subjectpower spectral density-
dc.subjectmicrophone array-
dc.subjectanechoic chambers-
dc.subjectpropeller noise-
dc.subjecttachometer-
dc.subjectelectric vertical take off and landing-
dc.titleNoise decomposition of dual synchronized propellers in hoveren_US
dc.typeConference Paperen_US
dc.date.dateAccepted2024-02-05-
dc.identifier.doihttps://doi.org/10.2514/6.2024-3045-
dc.relation.isPartOf30th AIAA/CEAS Aeroacoustics Conference, 2024-
pubs.finish-date2024-06-07-
pubs.finish-date2024-06-07-
pubs.publication-statusPublished-
pubs.start-date2024-06-04-
pubs.start-date2024-06-04-
dc.rights.holderAmerican Institute of Aeronautics and Astronautics, Inc.-
Appears in Collections:Dept of Mechanical and Aerospace Engineering Research Papers

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