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http://bura.brunel.ac.uk/handle/2438/28488Full metadata record
| DC Field | Value | Language |
|---|---|---|
| dc.contributor.author | Bhardwaj, M | - |
| dc.contributor.author | Woodhead, PC | - |
| dc.contributor.author | Scholz, MM | - |
| dc.contributor.author | Chong, TP | - |
| dc.date.accessioned | 2024-03-07T17:55:04Z | - |
| dc.date.available | 2024-03-07T17:55:04Z | - |
| dc.date.issued | 2023-06-08 | - |
| dc.identifier | ORCiD: Philip C. Woodhead https://orcid.org/0000-0002-8116-858X | - |
| dc.identifier | ORCiD: Tze Pei Chong https://orcid.org/0000-0002-5272-3943 | - |
| dc.identifier | AIAA 2023-3223 | - |
| dc.identifier.citation | Bhardwaj, M. et al. (2023) 'Noise Characterisation of Multi-Propeller in Hovering and Transitional Configurations Under Static Condition', AIAA AVIATION 2023 Forum, San Diego, CA and Online, 12-16 June, AIAA 2023-3223, pp. 1 - 13. doi: 10.2514/6.2023-3223. | en_US |
| dc.identifier.isbn | 978-1-62410-704-7 | - |
| dc.identifier.uri | https://bura.brunel.ac.uk/handle/2438/28488 | - |
| dc.description | Session: Advanced Air Mobility Noise I (joint AA/TF) - Modeling | en_US |
| dc.description | View Video Presentation: https://doi.org/10.2514/6.2023-3223.vid | - |
| dc.description | Correction: The following statement should be appended at the end of the conclusion section: Future publications will include an extended expansion of the existing study, providing deeper insights and a more comprehensive understanding of the subject matter. | - |
| dc.description.abstract | This paper represents an experimental study on the aeroacoustics behaviours of multi propellers. Two propellers are distributed in various spatial configurations to mimic some of the configurations that resemble a typical eVTOL (electrical Vertical Take-Off and Landing) aircraft. The interdependence for various influencing parameters for the acoustic radiations, such as the longitudinal and transverse displacements between a reference propeller and another propeller, as well as the different rotational speeds, was investigated in a specially constructed test rig inside an anechoic chamber under a quiescent condition. Statistical quantities such as the power spectral density and overall sound pressure level are presented. | en_US |
| dc.format.extent | 1 - 13 | - |
| dc.format.medium | Electronic | - |
| dc.language.iso | en_US | en_US |
| dc.publisher | American Institute of Aeronautics and Astronautics | en_US |
| dc.relation.uri | https://doi.org/10.2514/6.2023-3223.vid | - |
| dc.rights | This is the accepted manuscript version of a conference paper which has been published in final form on 8 June 2023 AIAA Electronic Library at https://doi.org/10.2514/6.2023-3223, Copyright © 2023 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.uri | https://www.aiaa.org/publications/Open-Access | - |
| dc.source | AIAA AVIATION 2023 Forum | - |
| dc.source | AIAA AVIATION 2023 Forum | - |
| dc.title | Noise Characterisation of Multi-Propeller in Hovering and Transitional Configurations Under Static Condition | en_US |
| dc.title.alternative | Noise Characterization of Multi-Propeller Under Static Conditions in Hover | - |
| dc.type | Conference Paper | en_US |
| dc.identifier.doi | https://doi.org/10.2514/6.2023-3223 | - |
| dc.relation.isPartOf | AIAA AVIATION 2023 Forum | - |
| pubs.publication-status | Published | - |
| dc.rights.holder | American Institute of Aeronautics and Astronautics, Inc. | - |
| Appears in Collections: | Dept of Mechanical and Aerospace Engineering Research Papers | |
Files in This Item:
| File | Description | Size | Format | |
|---|---|---|---|---|
| FullText.pdf | This is the accepted manuscript version of a conference paper which has been published in final form on 8 June 2023 AIAA Electronic Library at https://doi.org/10.2514/6.2023-3223, Copyright © 2023 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. | 3.3 MB | Adobe PDF | View/Open |
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