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Computational study on coaxial nitrogen-hydrogen injection at supercritical conditions

dc.contributor.authorMagalhães, Leandro
dc.contributor.authorSilva, André
dc.contributor.authorBarata, Jorge M M
dc.date.accessioned2022-04-04T09:36:58Z
dc.date.embargo2060-12-29
dc.date.issued2021-12-29
dc.description.abstractIn the present work, we perform a computational study on the mixing of nitrogen and hydrogen at supercritical conditions. A coaxial injection configuration is considered where nitrogen is injected through the central post with a hydrogen co-flow. The flow in both injectors as well as in the combustion chamber is considered in the computations. This preliminary version presents the radial density profiles maximum of both species and radial density profiles at selected locations.pt_PT
dc.description.sponsorshipFundação para a Ciência e a Tecnologiapt_PT
dc.description.versioninfo:eu-repo/semantics/publishedVersionpt_PT
dc.identifier.citationLeandro B. Magalhães, André R R Silva, Jorge M. Barata Computational study on coaxial nitrogen-hydrogen injection at supercritical conditions AIAA SciTech 2022 Forum and Exposition, Evento Hibrido, San Diego, CA, EUA, 3-7 janeiro, 2022pt_PT
dc.identifier.doi10.2514/6.2022-0877pt_PT
dc.identifier.issn978-162410631-6
dc.identifier.urihttp://hdl.handle.net/10400.6/12154
dc.language.isoengpt_PT
dc.peerreviewedyespt_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://arc.aiaa.org/doi/abs/10.2514/6.2022-0877pt_PT
dc.rights.urihttp://creativecommons.org/licenses/by/4.0/pt_PT
dc.subjectCombustion Chamberspt_PT
dc.subjectHeat Transferpt_PT
dc.subjectViscositypt_PT
dc.subjectGas Constantpt_PT
dc.subjectThermal Conductivitypt_PT
dc.subjectPropellantpt_PT
dc.subjectConservation Equationspt_PT
dc.subjectThermodynamic Propertiespt_PT
dc.subjectRocket Thrust Chamberpt_PT
dc.subjectFinite Volume Methodpt_PT
dc.titleComputational study on coaxial nitrogen-hydrogen injection at supercritical conditionspt_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.conferencePlaceSan Diego, CA & Virtualpt_PT
oaire.citation.titleAIAA SCITECH 2022 Forumpt_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.embargofctAmerican Institute of Aeronautics and Astronautics Inc.. All rights reserved.pt_PT
rcaap.rightsembargoedAccesspt_PT
rcaap.typearticlept_PT
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