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DC Field | Value | Language |
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dc.contributor.author | Langdon, S | - |
dc.contributor.author | Needham, D | - |
dc.coverage.spatial | Las Vegas, USA | - |
dc.date.accessioned | 2025-06-07T10:23:54Z | - |
dc.date.available | 2025-06-07T10:23:54Z | - |
dc.date.issued | 2025-07-16 | - |
dc.identifier | ORCiD: Stephen Langdon https://orcid.org/0000-0002-0572-5137 | - |
dc.identifier.citation | Langdon, S. and Needham, D. (2025) 'Modelling visibility in particle-fluid flow fields generated by helicopter rotors', AIAA Aviation Forum, Las Vegas, NE, USA, 21-25 July. AIAA 2025-3824, pp. 1 - 16. doi: 10.2514/6.2025-3824. | en_US |
dc.identifier.isbn | 978-1-62410-738-2 (ebk) | - |
dc.identifier.uri | https://bura.brunel.ac.uk/handle/2438/31412 | - |
dc.description | Paper presented at the AIAA Aviation Forum and Ascend, Las Vegas, NE, USA, 21-25 July, Session: Multiphase Flows I. | en_US |
dc.description.abstract | As a helicopter descends towards a bed of sand, a high velocity particle laden cloud can form around the helicopter body, a phenomenon known as “brownout”, and a consequence of which can potentially be a significant deterioration in visibility for the helicopter pilot. Here we consider a recently developed physically based rational mathematical model for the generation of wind-driven particle flow fields from otherwise static particle beds, one application of which is the scenario considered here. We introduce a directional opacity measure, defined for each observation angle from the helicopter cockpit, and show how visibility may vary in the model as certain parameters are varied. In particular, we demonstrate a counterintuitive result suggesting that, with specific yet potentially realistic parameter choices, pilot visibility may be improved in some viewing directions if the helicopter were hovering at a lower altitude. | en_US |
dc.description.sponsorship | ... | en_US |
dc.format.extent | 1 - 16 | - |
dc.format.medium | Print-Electronic | - |
dc.language.iso | en_US | en_US |
dc.publisher | American Institute of Aeronautics and Astronautics (AIAA) | en_US |
dc.rights | This is the accepted manuscript version of an article which has been published in final form on AIAA Electronic Library at https://doi.org/10.2514/6.2025-3824, Copyright © 2025 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. All requests for copying and permission to reprint should be submitted to CCC at https://www.copyright.com; employ the eISSN 1533-385X to initiate your request. See also AIAA Rights and Permissions https://www.aiaa.org/randp. | - |
dc.rights.uri | https://www.aiaa.org/randp | - |
dc.source | AIAA Aviation Forum | - |
dc.source | AIAA Aviation Forum | - |
dc.title | Modelling visibility in particle-fluid flow fields generated by helicopter rotors | en_US |
dc.type | Conference Paper | en_US |
dc.identifier.doi | https://doi.org/10.2514/6.2025-3824 | - |
pubs.finish-date | 2025-07-25 | - |
pubs.finish-date | 2025-07-25 | - |
pubs.publication-status | Published | - |
pubs.start-date | 2025-07-21 | - |
pubs.start-date | 2025-07-21 | - |
dc.rights.holder | American Institute of Aeronautics and Astronautics | - |
Appears in Collections: | Dept of Mathematics Research Papers |
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File | Description | Size | Format | |
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FullText.pdf | This is the accepted manuscript version of an article which has been published in final form on AIAA Electronic Library at https://doi.org/10.2514/6.2025-3824, Copyright © 2025 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. All requests for copying and permission to reprint should be submitted to CCC at https://www.copyright.com; employ the eISSN 1533-385X to initiate your request. See also AIAA Rights and Permissions https://www.aiaa.org/randp. | 909.48 kB | Adobe PDF | View/Open |
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