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1. Identity statement
Reference TypeBook Section
Sitemtc-m21b.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier8JMKD3MGP3W34P/3KU87HL
Repositorysid.inpe.br/mtc-m21b/2016/01.11.15.39   (restricted access)
Last Update2016:01.11.15.41.06 (UTC) simone
Metadata Repositorysid.inpe.br/mtc-m21b/2016/01.11.15.39.45
Metadata Last Update2024:01.08.13.43.12 (UTC) simone
Secondary KeyINPE--/
DOI10.1051/eucass/201507369
Citation KeyLeiteSant:2015:CoAnRa
TitleComputational analysis of a rarefied hypersonic flow over combined gap/step geometries
Year2015
Access Date2024, Apr. 24
Secondary TypePRE LN
Number of Files1
Size2875 KiB
2. Context
Author1 Leite, Paulo Henrique Mineiro
2 Santos, Wilson Fernando Nogueira dos
Resume Identifier1
2 8JMKD3MGP5W/3C9JJCC
Group1 PCP-ETES-SPG-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
2 wilson@lcp.inpe.br
EditorKnight, D.
Lipatov, I.
Reijasse, P.
Book TitleProgress in Flight Physics
PublisherEDP Sciences
Pages369-394
History (UTC)2016-01-11 15:41:06 :: simone -> administrator :: 2015
2018-06-04 02:56:01 :: administrator -> simone :: 2015
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Version Typepublisher
KeywordsComputational analysis
hypersonic flow
AbstractThis work describes a computational analysis of a hypersonic §ow over a combined gap/step con¦guration at zero degree angle of attack, in chemical equilibrium and thermal nonequilibrium. E¨ects on the §ow- ¦eld structure due to changes on the step frontal-face height have been investigated by employing the Direct Simulation Monte Carlo (DSMC) method. The work focuses the attention of designers of hypersonic con- ¦gurations on the fundamental parameter of surface discontinuity, which can have an important impact on even initial designs. The results high- light the sensitivity of the primary §ow¦eld properties, velocity, density, pressure, and temperature due to changes on the step frontal-face height. The analysis showed that the upstream disturbance in the gap/step con- ¦guration increased with increasing the frontal-face height. In addition, it was observed that the separation region for the gap/step con¦gura- tion increased with increasing the step frontal-face height. It was found that density and pressure for the gap/step con¦guration dramatically increased inside the gap as compared to those observed for the gap con- ¦guration, i. e., a gap without a step.
AreaCOMB
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4. Conditions of access and use
Languageen
Target FileProgress_in_Flight_Physics_07_0369(2015).pdf
User Groupsimone
Reader Groupadministrator
simone
Visibilityshown
Read Permissiondeny from all and allow from 150.163
Update Permissionnot transferred
5. Allied materials
Mirror Repositorysid.inpe.br/mtc-m21b/2013/09.26.14.25.22
Next Higher Units8JMKD3MGPCW/3ET38CH
8JMKD3MGPCW/3F35D8B
Citing Item Listsid.inpe.br/mtc-m21/2012/07.13.15.01.58 1
sid.inpe.br/bibdigital/2013/10.14.22.36 1
DisseminationBNDEPOSITOLEGAL
Host Collectionsid.inpe.br/mtc-m21b/2013/09.26.14.25.20
6. Notes
Empty Fieldsarchivingpolicy archivist callnumber city copyholder copyright creatorhistory descriptionlevel e-mailaddress edition format isbn issn label lineage mark nextedition notes numberofvolumes orcid parameterlist parentrepositories previousedition previouslowerunit progress project rightsholder schedulinginformation secondarydate secondarymark serieseditor seriestitle session shorttitle sponsor subject tertiarymark tertiarytype translator url volume
7. Description control
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