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1. Identity statement
Reference TypeConference Paper (Conference Proceedings)
Sitemtc-m16d.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier8JMKD3MGP7W/37KD4U8
Repositorysid.inpe.br/mtc-m19@80/2010/06.04.12.10
Last Update2010:06.04.12.10.13 (UTC) administrator
Metadata Repositorysid.inpe.br/mtc-m19@80/2010/06.04.12.10.14
Metadata Last Update2018:06.05.04.36.44 (UTC) administrator
Secondary KeyINPE--PRE/
Citation KeySampaioSant:2010:CoAnAe
TitleComputational analysis of the aerodynamic heating and drag of a reentry Brazilian satellite
Year2010
Access Date2024, May 08
Secondary TypePRE CI
Number of Files1
Size516 KiB
2. Context
Author1 Sampaio, Pedro Andrey C.
2 Santos, Wilson Fernando Nogueira
Group1
2 LCP-CTE-INPE-MCT-BR
Affiliation1
2 Instituto Nacional de Pesquisas Espaciais (INPE)
e-Mail Addressignes@lcp.inpe.br
Conference NameCongresso Nacional de Engenharia Mecânica/National Congress of Mechanical Engineering, CONEM, 6.
Conference LocationCampina Grande, PA
Date18-21 Aug.
PublisherABCM
Publisher CityRio de Janeiro, RJ
Book TitleAnais
Tertiary TypePaper
OrganizationABCM
History (UTC)2010-07-07 20:24:23 :: ignes@lcp.inpe.br -> marciana :: 2010
2010-07-15 15:36:02 :: marciana -> administrator :: 2010
2018-06-05 04:36:44 :: administrator -> marciana :: 2010
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
KeywordsDSMC
rarefie flow
hypersonic flow
aerodynamic heating
reentry
AbstractAbstract The aim of the work reported here is to present a computational investigation on the small ballistic reentry Brazilian vehicle SARA (acronym for SAtélite de Reentrada Atmosférica). Chemical equilibrium and thermal non-equilibrium hypersonic flow over the vehicle SARA at zero-degree angle of attack is modeled by the Direct Simulation Monte Carlo (DSMC) method. The emphasis of this paper is to examine the behavior of the aerodynamic surface quantities during the high altitude portion of the SARA reentry. In this fashion, pressure, skin friction, heat transfer and drag coefficients are investigated for altitudes of 100, 95, 90 and 85 km. In addition, comparisons based on geometry are made by considering axisymmetric and planar two-dimensional configurations. The analysis showed that the stagnation region is a thermally stressed zone. The peak value for the heat flux was attained at the stagnation point. It was also found that the stagnation region is a zone of strong compression, high wall pressure.
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
data URLhttp://urlib.net/ibi/8JMKD3MGP7W/37KD4U8
zipped data URLhttp://urlib.net/zip/8JMKD3MGP7W/37KD4U8
Languageen
Target Filecomputational.pdf
User Groupadministrator
ignes@lcp.inpe.br
marciana
Visibilityshown
5. Allied materials
LinkingTrabalho Vinculado à Tese/Dissertação
Mirror Repositorysid.inpe.br/mtc-m19@80/2009/08.21.17.02.53
Next Higher Units8JMKD3MGPCW/3ET38CH
Citing Item Listsid.inpe.br/bibdigital@80/2006/04.07.15.50.13 1
Host Collectionsid.inpe.br/mtc-m19@80/2009/08.21.17.02
6. Notes
Empty Fieldsarchivingpolicy archivist callnumber copyholder copyright creatorhistory descriptionlevel dissemination documentstage doi edition editor electronicmailaddress format isbn issn label lineage mark nextedition notes numberofvolumes orcid pages parameterlist parentrepositories previousedition previouslowerunit progress project readergroup readpermission resumeid rightsholder schedulinginformation secondarydate secondarymark serieseditor session shorttitle sponsor subject type url versiontype volume
7. Description control
e-Mail (login)marciana
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