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Supercritical Injection Modeling by an Incompressible but Variable Density Approach

dc.contributor.authorMagalhães, Leandro
dc.contributor.authorSilva, A. R. R.
dc.contributor.authorBarata, Jorge M. M.
dc.date.accessioned2023-01-30T09:53:31Z
dc.date.available2023-01-30T09:53:31Z
dc.date.issued2023-01-25
dc.description.abstractSupercritical nitrogen jet behavior is modeled using an incompressible but variable density approach developed for variable density jets. Following mechanical and thermal breakup concepts, several injection conditions relevant to liquid rocket propulsion are analyzed, considering heat transfer in the injector. Regarding axial density distributions, different levels of agreement with experimental data are encountered for potential core, subsided core, and plateau formations. Further comparisons with compressible formulations from the literature are a good indicator of the proposed methodology’s suitability for the simulation of supercritical injection behavior.pt_PT
dc.description.sponsorshipFundação para a Ciência e a Tecnologiapt_PT
dc.description.versioninfo:eu-repo/semantics/publishedVersionpt_PT
dc.identifier.citationMagalhães, Leandro B., André R. R. Silva, and Jorge M. M. Barata. 2023. "Supercritical Injection Modeling by an Incompressible but Variable Density Approach" Aerospace 10, no. 2: 114. https://doi.org/10.3390/aerospace10020114pt_PT
dc.identifier.doi10.3390/aerospace10020114pt_PT
dc.identifier.issn2226-4310
dc.identifier.urihttp://hdl.handle.net/10400.6/12818
dc.language.isoengpt_PT
dc.peerreviewedyespt_PT
dc.publisherMDPI AGpt_PT
dc.relationAssociate Laboratory of Energy, Transports and Aeronautics
dc.relationalterado para: “Contribution to the Physical Understanding of Supercritical Fluid Flows: a Computational Perspective”. Computational methods for jet/spray characterization: transcritical and supercritical conditions
dc.relation.publisherversionhttps://www.mdpi.com/2226-4310/10/2/114pt_PT
dc.rights.urihttp://creativecommons.org/licenses/by/4.0/pt_PT
dc.subjectHigh-pressure systemspt_PT
dc.subjectSupercritical injectionpt_PT
dc.subjectLiquid rocket enginespt_PT
dc.subjectVariable density jetspt_PT
dc.titleSupercritical Injection Modeling by an Incompressible but Variable Density Approachpt_PT
dc.typejournal article
dspace.entity.typePublication
oaire.awardTitleAssociate Laboratory of Energy, Transports and Aeronautics
oaire.awardTitlealterado para: “Contribution to the Physical Understanding of Supercritical Fluid Flows: a Computational Perspective”. Computational methods for jet/spray characterization: transcritical and supercritical conditions
oaire.awardURIinfo:eu-repo/grantAgreement/FCT/6817 - DCRRNI ID/UIDB%2F50022%2F2020/PT
oaire.awardURIinfo:eu-repo/grantAgreement/FCT//SFRH%2FBD%2F136381%2F2018/PT
oaire.citation.issue2pt_PT
oaire.citation.startPage114pt_PT
oaire.citation.titleAerospacept_PT
oaire.citation.volume10pt_PT
oaire.fundingStream6817 - DCRRNI ID
person.familyNameMagalhães
person.familyNameResende Rodrigues da Silva
person.familyNameMartins Barata
person.givenNameLeandro
person.givenNameAndré
person.givenNameJorge Manuel
person.identifier2611303
person.identifierJ-4185-2012
person.identifierhFY_5JYAAAAJ&hl
person.identifier.ciencia-id571C-5641-9D78
person.identifier.ciencia-id8219-4B2B-E1C7
person.identifier.ciencia-idF611-BBCC-DAA8
person.identifier.orcid0000-0002-1256-9689
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
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relation.isAuthorOfPublication908e150d-3890-457c-b5da-09c84671cb93
relation.isAuthorOfPublicationc4346556-933d-4f70-9b6d-8e1670d57be6
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