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1. Identity statement
Reference TypeJournal Article
Siteplutao.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier8JMKD3MGP3W/3TEPNBL
Repositorysid.inpe.br/plutao/2019/06.10.16.24   (restricted access)
Last Update2019:06.13.17.05.42 (UTC) administrator
Metadata Repositorysid.inpe.br/plutao/2019/06.10.16.24.13
Metadata Last Update2020:01.06.11.35.23 (UTC) administrator
DOI10.2514/1.T5486
ISSN0887-8722
Labellattes: 4859685163568596 2 LeiteSant:2019:CoAnRa
Citation KeyLeiteSant:2019:CoAnRa
TitleComputational analysis of a rarefied hypersonic flow over backward-facing steps
Year2019
Access Date2024, May 12
Type of Workjournal article
Secondary TypePRE PI
Number of Files1
Size2325 KiB
2. Context
Author1 Leite, Paulo H. M.
2 Santos, Wilson Fernando Nogueira dos
Resume Identifier1
2 8JMKD3MGP5W/3C9JJCC
Group1
2 LABCP-COCTE-INPE-MCTIC-GOV-BR
Affiliation1 Brazilian Army
2 Instituto Nacional de Pesquisas Espaciais (INPE)
Author e-Mail Address1
2 wilson.santos@inpe.br
JournalJournal of Thermophysics And Heat Transfer
Volume2019
History (UTC)2019-06-13 17:05:44 :: lattes -> administrator :: 2019
2020-01-06 11:35:23 :: administrator -> simone :: 2019
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Version Typepublisher
KeywordsDSMC
Hypersonic Flow
Rarefied Flow
Backward-Facing Step
AbstractThis work deals with a numerical study on backward-facing steps situated in a nonreacting low-density hypersonic flow. The work is motivated by the interest in investigating the impact on the aerodynamic surface quantities of surface discontinuities on hypersonic vehicles. Discontinuities are represented by backward-facing steps with boundary-layer thickness larger than the step height at the step position. The primary emphasis is to assess the sensitivity of the heat transfer, pressure, and skin friction coefficients. In doing so, these effects have been investigated by employing the direct simulationMonte Carlo (DSMC) method. The analysis showed that the flow past a backwardfacing step in hypersonic flow is characterized by a strong expansion on the corner of the step, which influences the downstream separation region and the aerodynamics surface properties downstream of the back face. It was found that the recirculation region behind of the steps is a function of the back-face height, for the conditions investigated. In addition, the heat flux to the surface and the wall pressure increased in the reattachment zone downstream of the back face and reached the flat plate values in a smooth fashion. A comparison of the present simulation results with experimental data showed close agreement concerning the heat flux to step surface.
AreaCOMB
Arrangementurlib.net > BDMCI > Fonds > Produção anterior à 2021 > LABCP > Computational analysis of...
doc Directory Contentaccess
source Directory Contentthere are no files
agreement Directory Contentthere are no files
4. Conditions of access and use
Languageen
User Grouplattes
self-uploading-INPE-MCTI-GOV-BR
Visibilityshown
Read Permissiondeny from all and allow from 150.163
Update Permissionnot transferred
5. Allied materials
LinkingTrabalho não Vinculado à Tese/Dissertação
Next Higher Units8JMKD3MGPCW/3ET38CH
DisseminationWEBSCI; SCOPUS.
Host Collectiondpi.inpe.br/plutao@80/2008/08.19.15.01
6. Notes
NotesSetores de Atividade: Pesquisa e desenvolvimento científico.
Empty Fieldsalternatejournal archivingpolicy archivist callnumber copyholder copyright creatorhistory descriptionlevel e-mailaddress format isbn lineage mark mirrorrepository month nextedition number orcid pages parameterlist parentrepositories previousedition previouslowerunit progress project readergroup rightsholder schedulinginformation secondarydate secondarykey secondarymark session shorttitle sponsor subject targetfile tertiarytype url
7. Description control
e-Mail (login)simone
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