Please use this identifier to cite or link to this item: http://bura.brunel.ac.uk/handle/2438/29515
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dc.contributor.authorNeedham, DJ-
dc.contributor.authorLangdon, S-
dc.date.accessioned2024-08-07T15:07:41Z-
dc.date.available2024-08-07T15:07:41Z-
dc.date.issued2024-11-05-
dc.identifierORCiD: D.J.Needham https://orcid.org/0000-0002-4958-6976-
dc.identifierORCiD: Stephen Langdon https://orcid.org/00000002-0572-5137-
dc.identifierA61-
dc.identifierarXiv:2402.14028v2 [physics.flu-dyn]-
dc.identifier.citationNeedham, D.J. and Langdon, S. (2024) 'A mathematical model for wind-generated particle-fluid flow fields with an application to the helicopter cloud problem', Journal of Fluid Mechanics, 998, A61, pp. 1 - 40. doi:en_US
dc.identifier.issn0022-1120-
dc.identifier.urihttps://bura.brunel.ac.uk/handle/2438/29515-
dc.descriptionData availability statement: The authors confirm that the data supporting the findings of this study are available within the paper.en_US
dc.descriptionMSC codes 76-10, 76T99, 76M20, 76M45.-
dc.description.abstractWe develop a model for the interaction of a fluid flowing above an otherwise static particle bed, with generally the particles being entrained or detrained into the fluid from the upper surface of the particle bed, and thereby forming a fully two phase fluidized cloud above the particle bed. The flow in this large-scale fluidized region is treated as a two-phase flow, whilst the key processes of entrainment and detrainment from the particle bed are treated by examining the local dynamical force balances on the particles in a thin transition layer at the interface between the fully fluidized region and the static particle bed. This detailed consideration leads to the formation of an additional macroscopic boundary condition at this interface, which closes the two-phase flow problem in the bulk fluidized region above. We then introduce an elementary model of the well-known helicopter brownout problem, and use the theory developed in the first part of the paper to fully analyse this model, both analytically and numerically.en_US
dc.description.sponsorshipThis research received no specific grant from any funding agency, commercial or not-for-profit sectors.en_US
dc.format.extent1 - 40-
dc.format.mediumPrint-Electronic-
dc.language.isoen_USen_US
dc.publisherCambridge University Pressen_US
dc.relation.urihttps://arxiv.org/abs/2402.14028-
dc.relation.urihttps://doi.org/10.48550/arXiv.2402.14028-
dc.rightsAttribution 4.0 International-
dc.rights.urihttps://creativecommons.org/licenses/by/4.0/-
dc.subjectphysics.flu-dynen_US
dc.subjectparticle/fluid flowsen_US
dc.titleA mathematical model for wind-generated particle-fluid flow fields with an application to the helicopter cloud problemen_US
dc.typeArticleen_US
dc.date.dateAccepted2024-07-14-
dc.identifier.doihttps://doi.org/10.1017/jfm.2024.740-
pubs.volume998-
dc.identifier.eissn1469-7645-
dc.rights.licensehttps://creativecommons.org/licenses/by/4.0/legalcode.en-
dc.rights.holderThe Author(s)-
Appears in Collections:Dept of Mathematics Research Papers

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