Repository logo
 
Publication

Variable Density Approach for Modeling of Transcritical and Supercritical Jets

dc.contributor.authorAntunes, Eduardo Luís Santos Farias
dc.contributor.authorSilva, A. R. R.
dc.contributor.authorBarata, Jorge M M
dc.date.accessioned2018-05-14T09:24:45Z
dc.date.available2018-05-14T09:24:45Z
dc.date.issued2017
dc.description.abstractIn order to study the high pressure and high temperature operating condition of a variety of internal combustion engines such as modern diesel engines, gas turbines and liquid fuel rocket engines, a cryogenic nitrogen jet injected into supercritical chamber conditions was simulated numerically. The favre averaged navier-stokes equations were employed together with a “k-ε” Turbulence Model and using instead of an ideal gas equation of state, the Amagat’s law in an approach originally conceived for gaseous turbulent jets with variable density. The present study describes the assessment of the capabilities of the approach by comparison against experimental data as well as numerical simulation performed by other researcher. The obtained results show an acceptable agreement with experiments for the axial density distribution, failing slightly in the prediction of the jet potential core. Good agreement is observed for radial density distribution as well as for the jet spreading rate.pt_PT
dc.description.versioninfo:eu-repo/semantics/publishedVersionpt_PT
dc.identifier.citationEduardo Antunes, Andre Silva and Jorge Barata, 2017. Variable Density Approach for Modeling of Transcritical and Supercritical Jets. Journal of Engineering and Applied Sciences, 12: 5147-5159pt_PT
dc.identifier.doi10.3923/jeasci.2017.5147.5159pt_PT
dc.identifier.issn1816949X
dc.identifier.urihttp://hdl.handle.net/10400.6/4752
dc.language.isoengpt_PT
dc.peerreviewedyespt_PT
dc.publisherMedwell Journalspt_PT
dc.relationNot available
dc.relation.publisherversionhttp://medwelljournals.com/abstract/?doi=jeasci.2017.5147.5159pt_PT
dc.subjectCritical pointpt_PT
dc.subjectCryogenic jetspt_PT
dc.subjectFuel injectionpt_PT
dc.subjectRocket enginespt_PT
dc.subjectSimulationpt_PT
dc.subjectSupercritical flowspt_PT
dc.titleVariable Density Approach for Modeling of Transcritical and Supercritical Jetspt_PT
dc.typejournal article
dspace.entity.typePublication
oaire.awardTitleNot available
oaire.awardURIinfo:eu-repo/grantAgreement/FCT/5876/UID%2FEMS%2F50022%2F2013/PT
oaire.awardURIinfo:eu-repo/grantAgreement/FCT//SFRH%2FBD%2F87822%2F2012/PT
oaire.citation.endPage5159pt_PT
oaire.citation.issue20pt_PT
oaire.citation.startPage5147pt_PT
oaire.citation.titleJournal of Engineering and Applied Sciencespt_PT
oaire.citation.volume12pt_PT
oaire.fundingStream5876
person.familyNameResende Rodrigues da Silva
person.familyNameMartins Barata
person.givenNameAndré
person.givenNameJorge Manuel
person.identifierJ-4185-2012
person.identifierhFY_5JYAAAAJ&hl
person.identifier.ciencia-id8219-4B2B-E1C7
person.identifier.ciencia-idF611-BBCC-DAA8
person.identifier.orcid0000-0002-4901-7140
person.identifier.orcid0000-0001-9014-5008
person.identifier.scopus-author-id11440407500
person.identifier.scopus-author-id11439470600
project.funder.identifierhttp://doi.org/10.13039/501100001871
project.funder.identifierhttp://doi.org/10.13039/501100001871
project.funder.nameFundação para a Ciência e a Tecnologia
project.funder.nameFundação para a Ciência e a Tecnologia
rcaap.rightsopenAccesspt_PT
rcaap.typearticlept_PT
relation.isAuthorOfPublication908e150d-3890-457c-b5da-09c84671cb93
relation.isAuthorOfPublicationc4346556-933d-4f70-9b6d-8e1670d57be6
relation.isAuthorOfPublication.latestForDiscoveryc4346556-933d-4f70-9b6d-8e1670d57be6
relation.isProjectOfPublicationc1eae78f-3c5c-4b94-92c2-54af6896833d
relation.isProjectOfPublication9d36dd10-f00f-472f-a768-4126341f880f
relation.isProjectOfPublication.latestForDiscoveryc1eae78f-3c5c-4b94-92c2-54af6896833d

Files

Original bundle
Now showing 1 - 1 of 1
No Thumbnail Available
Name:
2017-JEAS-Vol12-No20-pp5147-5159.pdf
Size:
465.96 KB
Format:
Adobe Portable Document Format
License bundle
Now showing 1 - 1 of 1
No Thumbnail Available
Name:
license.txt
Size:
1.71 KB
Format:
Item-specific license agreed upon to submission
Description: