Close

1. Identity statement
Reference TypeJournal Article
Sitemtc-m16b.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier6qtX3pFwXQZGivnK2Y/QnqSw
Repositorysid.inpe.br/mtc-m17@80/2007/06.06.12.23   (restricted access)
Last Update2007:06.06.12.23.01 (UTC) administrator
Metadata Repositorysid.inpe.br/mtc-m17@80/2007/06.06.12.23.02
Metadata Last Update2018:06.05.03.34.14 (UTC) administrator
ISSN0103-9733
Citation KeySantos:2007:GaInEf
TitleGas-surface interaction effect on round leading aerothermodynamics
Year2007
MonthJun.
Access Date2024, Apr. 28
Secondary TypePRE PN
Number of Files1
Size1231 KiB
2. Context
AuthorSantos, Wilson Fernando Nogueira
GroupLCP-INPE-MCT-BR
AffiliationInstituto Nacional de Pesquisas Espaciais (INPE)
JournalBrazilian Journal of Physics
Volume37
Number2A
Pages337-348
History (UTC)2007-06-06 12:23:02 :: ignes -> administrator ::
2012-10-23 23:53:22 :: administrator -> ignes :: 2007
2013-02-20 14:54:15 :: ignes -> administrator :: 2007
2018-06-05 03:34:14 :: administrator -> marciana :: 2007
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Keywordsaerothermodynamics
gas flow
surfaces
AbstractABSTRACT: Effects of incomplete surface accommodation in rarefied gas flow have been studied by using the Direct Simulation Monte Carlo (DSMC) method in conjunction with the Cercignani-Lampis-Lord gas surface interaction model. The DSMC calculations examine differences in predictions of aerodynamic forces and heat transfer between full and partial surface accommodation for hypersonic flow past round leading edges at zero incidence. The aerodynamic performance of round leading edges is assessed by using the heat transfer rate, the total drag and the shock wave standoff distance. Twenty-five combinations of nose radius, normal and tangential accommodation coefficients were used in the simulation. For the flow conditions considered, the analysis showed that stagnation point heating, total drag and shock standoff distance are sensitive to changes on either the normal or tangential accommodation coefficient. The results substantiate that it becomes imperative to take surface accommodation into account in order to make accurate predictions of the aerodynamic forces on, and heat transfer rates to, bodies in rarefied hypersonic flow.
AreaCOMB
Arrangementurlib.net > BDMCI > Fonds > Produção anterior à 2021 > LABCP > Gas-surface interaction effect...
doc Directory Contentaccess
source Directory Contentthere are no files
agreement Directory Contentthere are no files
4. Conditions of access and use
Languageen
Target Filegas.pdf
User Groupadministrator
ignes
Visibilityshown
Archiving Policydenypublisher denyfinaldraft12
Read Permissiondeny from all and allow from 150.163
5. Allied materials
Next Higher Units8JMKD3MGPCW/3ET38CH
DisseminationWEBSCI; PORTALCAPES; SCIELO.
Host Collectionlcp.inpe.br/ignes/2004/02.12.18.39
cptec.inpe.br/walmeida/2003/04.25.17.12
6. Notes
Empty Fieldsalternatejournal archivist callnumber copyholder copyright creatorhistory descriptionlevel documentstage doi e-mailaddress electronicmailaddress format isbn label lineage mark mirrorrepository nextedition notes orcid parameterlist parentrepositories previousedition previouslowerunit progress project readergroup resumeid rightsholder schedulinginformation secondarydate secondarykey secondarymark session shorttitle sponsor subject tertiarymark tertiarytype typeofwork url versiontype
7. Description control
e-Mail (login)marciana
update 


Close