Repository logo
 
Publication

Computational characterization of the temperature field in coaxial nitrogen injection under supercritical conditions

dc.contributor.authorMagalhães, Leandro
dc.contributor.authorSilva, A. R. R.
dc.contributor.authorBarata, Jorge M M
dc.date.accessioned2023-08-28T09:18:17Z
dc.date.embargo2025-08-09
dc.date.issued2023-08-09
dc.description.abstractThe modeling of fluids in the supercritical regime is addressed at conditions characteristic of liquid-propelled rocket engines, whose increasing performance demands paved the way for supercritical conditions. In the present document, nitrogen is used as a surrogate for the commonly encountered oxygen-hydrogen mixture so that turbulence mixing can be looked into without influences from combustion and chemically reacting effects. The temperature field validation on nitrogen coaxial injection at supercritical conditions, with high-velocity ratios (outer-to-inner), where the main (inner) stream is recessed relative to the outer stream, is of paramount importance in the flame stabilization operation of liquid rocket motors. The temperature field is analyzed taking into account varying momentum and velocity ratios, whose increased leads to a reduction of potential core lengths, increasing jet spreading. The results also depict a fundamental influence of thermal effects, dominating over the transport of momentum. The experimental data and large eddy simulation solvers from the literature agree with the estimate of injection velocities at several conditions and comparable to the space shuttle main engine pre-burner.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.M. Barata, "Computational characterization of the temperature field in coaxial nitrogen injection under supercritical conditions", Acta Astronautica Volume 212, November 2023, Pages 329-338, DOI: 10.1016/j.actaastro.2023.08.004pt_PT
dc.identifier.doi10.1016/j.actaastro.2023.08.004pt_PT
dc.identifier.issn0094-5765
dc.identifier.issn1879-2030
dc.identifier.urihttp://hdl.handle.net/10400.6/13406
dc.language.isoengpt_PT
dc.peerreviewedyespt_PT
dc.publisherElsevierpt_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://pdf.sciencedirectassets.com/271447/1-s2.0-S0094576523X00095/1-s2.0-S0094576523004022/main.pdf?X-Amz-Security-Token=IQoJb3JpZ2luX2VjEPD%2F%2F%2F%2F%2F%2F%2F%2F%2F%2FwEaCXVzLWVhc3QtMSJHMEUCICMyeRHW%2FnJI6MQXEz9IxdtvIll4egs4mUJa2oPbYZeYAiEAkPyeNJNfjsW8JjZHrNyUbb4i8YZTua5gehyh%2Bn3XnIQquwUIqf%2F%2F%2F%2F%2F%2F%2F%2F%2F%2FARAFGgwwNTkwMDM1NDY4NjUiDNef5D8kHlJNwDkX%2FyqPBWzmzLaCmKSdllcTDc6O%2BA4o%2Fn%2FEST50OypZJ8p1G4qiq2%2B4whlfSuWenIzc2%2F7R5ZRs5lo7%2FZ0Ldr9B3j1Z1Z6Q1JsC8R69nSTFnn0Y7rUPJQtCM1UEA%2BH6UE0c%2FEJODZm0COofgFQkXyfFqJJy4XSQNGl73%2FRAFz1yN98cVNSji7rcYbsDVgcQYDjrLZmdlOULWoxa%2Fql%2BZnydee%2BH8VtsxCTq2lDhYiQVuj6tRsG5N5Gvbyg8bwsN3nzBUZ02a%2BuJsszMIlkkL3wz9UMy2wFxSyE%2BUiIh%2FAgx0%2FXWDYgWnslbQOzHPm9QwhoxQQdMEwUwm7HMr%2BSQKuqPVkmfvZmtTDAlAfwcpkWedtLGiC1NQe1hRm0lgUJwI5HwU4eO%2BrD2xWVAKzGgN5Q45N7jwXOAnygDmLnkunpbfFT%2Fd%2BthdETfipghESZ1LS4bS%2FzOrUZviyJ4EItuvnE4PyoZGudsqA4BVHS86iXYHgqf9UjHR6P22r1ID2az%2FxTj9buDEzXNqBCl94LTc8LItXCmigiXWkie57sSZXcLqddtSWOjpMdJ6st%2Bo0pTLR1KAt7dnM10YZkaD59D8002zON6pN0WmmFV3uQQlEIEGBICatMrnEUFMp1c0VFFgc0bqbqcPPM1jxZAGbc8Nm3dVJn8OhtrNUx7cgnp%2BBMYMbxp994g0UzJ%2B28EIZQ3GIJqb1plo0TuKLyjt8tPIknNL6AObNE7f3kSaWRjXQipQsoIVQNtTwLp%2BwNwk0ysotNYGZROnzmjMdu0SJpmoSrTMSgqimfu6%2BfpkGc4%2FfWmxQLI6PhALqIOeZqPh4Zantnvu%2F%2B5k6f6q6ngVXYU4UPiwpsKOMxkiHhliSNg264FDEE8798wrcGDpwY6sQFUdKkhQcfqDEwDajCC6elnahZeYLBlZrzP0G26Au35k6MVV2%2FdbTY2LHHjL%2FfJwBTmHGkHiEohJy8Z%2B8Y9DkZJ93Vvt1GH8sTCSwOAdPK6fHvzMMfKJ%2FPC3TqHMGNi2HmrXanYDvbPNCTAbsApf0zW1rhg9cb3WFd5%2F73oFmtR%2BFg9E%2B7oEEuNGExkIRAcbEclyUG2W2cDtd6989Xkx7su5rOE3bDy0HfSF05g8prtdzo%3D&X-Amz-Algorithm=AWS4-HMAC-SHA256&X-Amz-Date=20230819T161502Z&X-Amz-SignedHeaders=host&X-Amz-Expires=300&X-Amz-Credential=ASIAQ3PHCVTY3WDHRTOU%2F20230819%2Fus-east-1%2Fs3%2Faws4_request&X-Amz-Signature=e1837c7c03eb5ee1cfcb84f131dd93bcaf6ad65d50ea08934bbca8337d9acc10&hash=c5ba6e7dc4cb85429e83ed059d43ae758218417b82cb2b79ebc287cd3d2b2e9f&host=68042c943591013ac2b2430a89b270f6af2c76d8dfd086a07176afe7c76c2c61&pii=S0094576523004022&tid=spdf-3d29578a-73bc-4f7d-a495-26765c52ab8b&sid=3c1df7e483e077479d6a4e04f6a5637b4a5egxrqb&type=client&tsoh=d3d3LnNjaWVuY2VkaXJlY3QuY29t&ua=15135807585407545554&rr=7f93b167ddf7dd3b&cc=ptpt_PT
dc.rights.urihttp://creativecommons.org/licenses/by/4.0/pt_PT
dc.subjectTranscritical mixingpt_PT
dc.subjectSupercritical mixingpt_PT
dc.subjectLiquid rocket enginespt_PT
dc.titleComputational characterization of the temperature field in coaxial nitrogen injection under 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.endPage338pt_PT
oaire.citation.startPage329pt_PT
oaire.citation.titleActa Astronauticapt_PT
oaire.citation.volume212pt_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.embargofct© 2023 IAA. Published by Elsevier Ltd. All rights reserved. Publicação sem custospt_PT
rcaap.rightsembargoedAccesspt_PT
rcaap.typearticlept_PT
relation.isAuthorOfPublicationfd0c95ba-3a60-42d1-a382-f37a714962b9
relation.isAuthorOfPublication908e150d-3890-457c-b5da-09c84671cb93
relation.isAuthorOfPublicationc4346556-933d-4f70-9b6d-8e1670d57be6
relation.isAuthorOfPublication.latestForDiscoveryfd0c95ba-3a60-42d1-a382-f37a714962b9
relation.isProjectOfPublicationd3f48e72-49da-44e7-b054-cbdb0644e04d
relation.isProjectOfPublication85282b9c-1a98-4958-9e7f-e94c1835cadd
relation.isProjectOfPublication.latestForDiscoveryd3f48e72-49da-44e7-b054-cbdb0644e04d

Files

Original bundle
Now showing 1 - 1 of 1
No Thumbnail Available
Name:
1-s2.0-S0094576523004022-main.pdf
Size:
1.63 MB
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: