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1. Identity statement
Reference TypeConference Paper (Conference Proceedings)
Siteplutao.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
IdentifierJ8LNKAN8RW/3C644CJ
Repositorydpi.inpe.br/plutao/2012/06.21.20.47.13
Last Update2015:03.18.13.30.21 (UTC) administrator
Metadata Repositorydpi.inpe.br/plutao/2012/06.21.20.47.14
Metadata Last Update2018:06.05.00.01.49 (UTC) administrator
Labellattes: 4859685163568596 2 LeiteSant:2012:CoImAe
Citation KeyLeiteSant:2012:CoImAe
TitleCompressibility Impact on the Aerodynamic Surface Quantities of Rarefied Hypersonic Flow over Forward-Facing Steps
FormatDVD
Year2012
Access Date2024, Mar. 28
Secondary TypePRE CN
Number of Files1
Size631 KiB
2. Context
Author1 Leite, Paulo H. Mineiro
2 Santos, Wilson Fernando Nogueira dos
Resume Identifier1
2 8JMKD3MGP5W/3C9JJCC
Group1 LCP-CTE-INPE-MCTI-GOV-BR
2 LCP-CTE-INPE-MCTI-GOV-BR
Affiliation1 Instituto Nacional de Pesquisas Espaciais (INPE)
2 Instituto Nacional de Pesquisas Espaciais (INPE)
Author e-Mail Address1 phmineiro@lcp.inpe.br
2 wilson@lcp.inpe.br
e-Mail Addresswilson@lcp.inpe.br
Conference NameBrazilian Congress of Thermal Sciences and Engineering, 14 (ENCIT).
Conference LocationRio de Janeiro, RJ
DateNov 18-22, 2012
Book TitleProceedings
Tertiary TypePaper
History (UTC)2012-06-22 00:11:01 :: lattes -> secretaria.cpa@dir.inpe.br :: 2012
2013-01-07 12:17:12 :: secretaria.cpa@dir.inpe.br -> administrator :: 2012
2018-06-05 00:01:49 :: administrator -> marciana :: 2012
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
forward-facing step
compressibility effect
AbstractCompressibility effects on hypersonic flow over forward-facing steps have been numerically investigated by using the Direct Simulation Monte Carlo (DSMC) method. The work is motivated by interest in assessing the impact of surface discontinuities on hypersonic configurations in the transition flow regime. The computations were carried out by assuming step frontal-face height from 3 to 5 millimeters and freestream Mach number from 5 to 25 at zero-degree angle of incidence. The results highlight some significant differences on the aerodynamic surface quantities due to variations on the step frontal-face height and on the freestream Mach number. Interesting features observed on pressure, skin friction, and heat transfer coefficients showed that small frontal-face thickness, compared to the freestream mean free path, still has important effects on these properties for the freestream Mach number range investigated.
AreaCOMB
Arrangementurlib.net > BDMCI > Fonds > Produção anterior à 2021 > LABCP > Compressibility Impact on...
doc Directory Contentaccess
source Directory Contentthere are no files
agreement Directory Contentthere are no files
4. Conditions of access and use
data URLhttp://urlib.net/ibi/J8LNKAN8RW/3C644CJ
zipped data URLhttp://urlib.net/zip/J8LNKAN8RW/3C644CJ
Languageen
Target FileLeite_compressibility.pdf
User Grouplattes
marciana
secretaria.cpa@dir.inpe.br
Reader Groupadministrator
marciana
Visibilityshown
Read Permissionallow from all
Update Permissionnot transferred
5. Allied materials
Next Higher Units8JMKD3MGPCW/3ET38CH
Host Collectiondpi.inpe.br/plutao@80/2008/08.19.15.01
6. Notes
NotesSetores de Atividade: Atividades profissionais, científicas e técnicas.
Empty Fieldsarchivingpolicy archivist callnumber copyholder copyright creatorhistory descriptionlevel dissemination doi edition editor isbn issn lineage mark mirrorrepository nextedition numberofvolumes orcid organization pages parameterlist parentrepositories previousedition previouslowerunit progress project publisher publisheraddress rightsholder schedulinginformation secondarydate secondarykey secondarymark serieseditor session shorttitle sponsor subject tertiarymark type url volume
7. Description control
e-Mail (login)marciana
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