Please use this identifier to cite or link to this item: http://bura.brunel.ac.uk/handle/2438/31412
Full metadata record
DC FieldValueLanguage
dc.contributor.authorLangdon, S-
dc.contributor.authorNeedham, D-
dc.coverage.spatialLas Vegas, USA-
dc.date.accessioned2025-06-07T10:23:54Z-
dc.date.available2025-06-07T10:23:54Z-
dc.date.issued2025-07-16-
dc.identifierORCiD: Stephen Langdon https://orcid.org/0000-0002-0572-5137-
dc.identifier.citationLangdon, 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.isbn978-1-62410-738-2 (ebk)-
dc.identifier.urihttps://bura.brunel.ac.uk/handle/2438/31412-
dc.descriptionPaper presented at the AIAA Aviation Forum and Ascend, Las Vegas, NE, USA, 21-25 July, Session: Multiphase Flows I.en_US
dc.description.abstractAs 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.extent1 - 16-
dc.format.mediumPrint-Electronic-
dc.language.isoen_USen_US
dc.publisherAmerican Institute of Aeronautics and Astronautics (AIAA)en_US
dc.rightsThis 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.urihttps://www.aiaa.org/randp-
dc.sourceAIAA Aviation Forum-
dc.sourceAIAA Aviation Forum-
dc.titleModelling visibility in particle-fluid flow fields generated by helicopter rotorsen_US
dc.typeConference Paperen_US
dc.identifier.doihttps://doi.org/10.2514/6.2025-3824-
pubs.finish-date2025-07-25-
pubs.finish-date2025-07-25-
pubs.publication-statusPublished-
pubs.start-date2025-07-21-
pubs.start-date2025-07-21-
dc.rights.holderAmerican Institute of Aeronautics and Astronautics-
Appears in Collections:Dept of Mathematics Research Papers

Files in This Item:
File Description SizeFormat 
FullText.pdfThis 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 kBAdobe PDFView/Open


Items in BURA are protected by copyright, with all rights reserved, unless otherwise indicated.