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Experimental Study of the Collision Zone of a Boundary Layer with a Wall Jet

2012-06-15Journal article Embargoed access
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dc.contributor.authorBarata, Jorge M M
dc.contributor.authorRibeiro, Samuel Dinis Galvão
dc.contributor.authorSantos, Pedro
dc.contributor.authorSilva, André
dc.date.accessioned2022-04-11T11:22:32Z
dc.date.embargo2060-06-15
dc.date.issued2012-06-15
dc.description.abstractLaser-Doppler measurements are presented for a highly curved flow resulting from the collision of plane turbulent wall jet with a boundary layer. This configuration can be found in the case of impinging jets of a V/STOL aircraft operating in ground vicinity. The experiments were carried out for boundary layer to wall jet velocity ratio of 0.5. The results include mean and turbulent velocity characteristics of the flow field as well as the characterization of the vorticity. The results revealed the existence of very small recirculation zones located upstream the separation point that co-exist and interact with the very well known VSTOL ground vortex. Copyright © 2009 by the American Institute of Aeronautics and Astronautics, Inc.pt_PT
dc.description.sponsorshipFundação para a Ciência e a Tecnologiapt_PT
dc.description.versioninfo:eu-repo/semantics/publishedVersionpt_PT
dc.identifier.citationSilva, A.R.R., Durão, D.F.G., Barata, J.M.M., Santos, P., Ribeiro, S. Experimental Study of the Collision Zone of a Boundary Layer with a Wall Jet 47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition, Orlando, Florida, EUA, 5-8 janeiro, 2009 DOI: 10.2514/6.2009-335pt_PT
dc.identifier.doi10.2514/6.2009-335pt_PT
dc.identifier.isbn978-1-60086-973-0
dc.identifier.isbn978-156347969-4
dc.identifier.urihttp://hdl.handle.net/10400.6/12200
dc.language.isoengpt_PT
dc.peerreviewedyespt_PT
dc.publisherAmerican Institute of Aeronautics and Astronautics Incpt_PT
dc.relation.publisherversionhttps://arc.aiaa.org/doi/10.2514/6.2009-335pt_PT
dc.rights.urihttp://creativecommons.org/licenses/by/4.0/pt_PT
dc.subjectVortex Flowpt_PT
dc.subjectBoundary Layer Thicknesspt_PT
dc.subjectReynolds Stresspt_PT
dc.subjectAircraft Fuselagespt_PT
dc.subjectJet Flowpt_PT
dc.subjectNormal Stresspt_PT
dc.subjectWind Tunnelspt_PT
dc.subjectAerodynamic Instabilitypt_PT
dc.subjectTurbulence Intensitypt_PT
dc.subjectCharacteristic Velocitypt_PT
dc.titleExperimental Study of the Collision Zone of a Boundary Layer with a Wall Jetpt_PT
dc.typejournal article
dspace.entity.typePublication
oaire.citation.conferencePlaceOrlando, Floridapt_PT
oaire.citation.title47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Expositionpt_PT
person.familyNameMartins Barata
person.familyNameResende Rodrigues da Silva
person.givenNameJorge Manuel
person.givenNameAndré
person.identifierhFY_5JYAAAAJ&hl
person.identifierJ-4185-2012
person.identifier.ciencia-idF611-BBCC-DAA8
person.identifier.ciencia-id8219-4B2B-E1C7
person.identifier.orcid0000-0001-9014-5008
person.identifier.orcid0000-0002-4901-7140
person.identifier.scopus-author-id11439470600
person.identifier.scopus-author-id11440407500
rcaap.embargofctCopyright © 2009 by the American Institute of Aeronautics and Astronautics, Inc.pt_PT
rcaap.rightsembargoedAccesspt_PT
rcaap.typearticlept_PT
relation.isAuthorOfPublicationc4346556-933d-4f70-9b6d-8e1670d57be6
relation.isAuthorOfPublication908e150d-3890-457c-b5da-09c84671cb93
relation.isAuthorOfPublication.latestForDiscovery908e150d-3890-457c-b5da-09c84671cb93

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