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On the Modelling of Evaporating Sprays Impinging onto Solid Surfaces

dc.contributor.authorRodrigues, Christian
dc.contributor.authorBarata, Jorge M M
dc.contributor.authorSilva, André
dc.date.accessioned2022-04-04T11:13:43Z
dc.date.embargo2060-01-03
dc.date.issued2015-01-03
dc.description.abstractThe present paper presents a numerical study on evaporating droplets impinging onto a solid surface through a crossflow. The characteristics of the initial spray are established by employing an empirical procedure, which relies on a comprehensive set of free spray measurements. Distinct wall and crossflow temperatures are analysed systematically to evaluate the in fluence of droplets evaporation on the nal outcome of spray impingement, and, particularly, on the distribution of the thin liquid lm over the surface. The present computational model already proved to deliver accurate predictions of the spray/wall interactions under different conditions. In this work, the conditions are extrapolated to a heated environment, which reproduce more adequately what is found in in-cylinder situations. The computational model is adapted to meet the new requirements and perform within the range of conditions for which it is now formulated. The analysis shows that higher temperatures lead to smaller impinging droplets, an increase in the number of depositing droplets but a decrease in the fraction of mass of particles contributing to the liquid film; and a more uniform distribution of the liquid layer over the surface.pt_PT
dc.description.sponsorshipFundação para a Ciência e a Tecnologiapt_PT
dc.description.versioninfo:eu-repo/semantics/publishedVersionpt_PT
dc.identifier.citationChristian Rodrigues, Jorge M. Barata, Andre R. Silva On the Modeling of Evaporating Sprays Impinging onto Solid Surfaces 53rd AIAA Aerospace Sciences Meeting, SciTech 2015, Kissmmee, FL, EUA, 5-9 janeiro, 2015 DOI: 10.2514/6.2015-0710pt_PT
dc.identifier.doi10.2514/6.2015-0710pt_PT
dc.identifier.isbn978-1-62410-343-8
dc.identifier.urihttp://hdl.handle.net/10400.6/12170
dc.language.isoengpt_PT
dc.peerreviewedyespt_PT
dc.publisherAmerican Institute of Aeronautics and Astronautics Incpt_PT
dc.relationMODELLING OF A BIOFUEL SPRAY WALL IMPINGEMENT
dc.relation.publisherversionhttps://arc.aiaa.org/doi/10.2514/6.2015-0710pt_PT
dc.rights.urihttp://creativecommons.org/licenses/by/4.0/pt_PT
dc.subjectVelocity Profilespt_PT
dc.subjectHomogeneous Charge Compression Ignitionpt_PT
dc.subjectSauter Mean Diameterpt_PT
dc.subjectNumber of Particlespt_PT
dc.subjectRadial Velocitypt_PT
dc.subjectWeber Numberpt_PT
dc.subjectProbability Density Functionspt_PT
dc.subjectCombustion Efficiencypt_PT
dc.subjectSurface Roughnesspt_PT
dc.subjectWall Temperaturept_PT
dc.subjectDroplet evaporationpt_PT
dc.subjectEvaporating sprayspt_PT
dc.subjectLiquid layerpt_PT
dc.subjectSolid surfacept_PT
dc.subjectThin liquid filmpt_PT
dc.titleOn the Modelling of Evaporating Sprays Impinging onto Solid Surfacespt_PT
dc.typejournal article
dspace.entity.typePublication
oaire.awardTitleMODELLING OF A BIOFUEL SPRAY WALL IMPINGEMENT
oaire.awardURIinfo:eu-repo/grantAgreement/FCT//SFRH%2FBD%2F77651%2F2011/PT
oaire.citation.conferencePlaceKissimmee, Floridapt_PT
oaire.citation.title53rd AIAA Aerospace Sciences Meetingpt_PT
person.familyNameGomes Rodrigues
person.familyNameMartins Barata
person.familyNameResende Rodrigues da Silva
person.givenNameChristian
person.givenNameJorge Manuel
person.givenNameAndré
person.identifierhFY_5JYAAAAJ&hl
person.identifierJ-4185-2012
person.identifier.ciencia-id7F16-AA19-E5AA
person.identifier.ciencia-idF611-BBCC-DAA8
person.identifier.ciencia-id8219-4B2B-E1C7
person.identifier.orcid0000-0002-8177-4483
person.identifier.orcid0000-0001-9014-5008
person.identifier.orcid0000-0002-4901-7140
person.identifier.ridR-9636-2016
person.identifier.scopus-author-id55341335400
person.identifier.scopus-author-id11439470600
person.identifier.scopus-author-id11440407500
project.funder.identifierhttp://doi.org/10.13039/501100001871
project.funder.nameFundação para a Ciência e a Tecnologia
rcaap.embargofctCopyright © 2015 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.pt_PT
rcaap.rightsembargoedAccesspt_PT
rcaap.typearticlept_PT
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relation.isAuthorOfPublicationc4346556-933d-4f70-9b6d-8e1670d57be6
relation.isAuthorOfPublication908e150d-3890-457c-b5da-09c84671cb93
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