Close

1. Identity statement
Reference TypeJournal Article
Sitemtc-m16b.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier6qtX3pFwXQZGivnK2Y/QwPvK
Repositorysid.inpe.br/mtc-m17@80/2007/06.22.18.13   (restricted access)
Last Update2007:06.22.18.13.40 (UTC) administrator
Metadata Repositorysid.inpe.br/mtc-m17@80/2007/06.22.18.13.41
Metadata Last Update2018:06.05.03.34.22 (UTC) administrator
ISSN0100-7386
Citation KeySantos:2007:SiBlLe
TitleSimulation of blunt leading edge aerothermodynamics in rarefied hypersonic flow
Year2007
MonthApr-Jun
Access Date2024, Apr. 27
Secondary TypePRE PI
Number of Files1
Size469 KiB
2. Context
AuthorSantos, Wilson Fernando Nogueira
GroupLCP-INPE-MCT-BR
AffiliationInstituto Nacional de Pesquisas Espaciais (INPE)
JournalJournal of the Brazilian Society of Mechanical Sciences and Engineering
Volume29
Number2
Pages123-135
History (UTC)2007-06-22 18:13:41 :: IGNES -> administrator ::
2018-06-05 03:34:22 :: administrator -> IGNES :: 2007
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Keywordshypersonic flow
rarefied flow
DSMC
blunt leading edge
sharp leading edge
AbstractThe steady-state aerodynamic characteristics of a new family of blunted leading edges immersed in a high-speed rarefied air flow are examined by using a Direct Simulation Monte Carlo (DSMC) Method. A very detailed description of the flow properties has been presented separately at the vicinity of the nose and adjacent to the afterbody surface of the leading edges by a numerical method that properly accounts for non-equilibrium effects that arise near the leading edges and that are especially important at high Mach number. Comparisons based on geometry are made between these new blunt configurations and round leading edge. Some significant differences between these leading edges are noted on the flowfield structure and on the aerodynamic surface quantities. It is found that the upstream effects have different influence on velocity, density, pressure and temperature along the stagnation streamline ahead of the leading edges. The analysis also shows that, despite the seeming advantages of the new blunt leading edge shapes, round leading edge still provides smaller stagnation point heating. Nevertheless, round leading edge provides larger total drag than the new blunt shapes under the range of condition investigated.
AreaCOMB
Arrangementurlib.net > BDMCI > Fonds > Produção anterior à 2021 > LABCP > Simulation of blunt...
doc Directory Contentaccess
source Directory Contentthere are no files
agreement Directory Contentthere are no files
4. Conditions of access and use
Languageen
Target Filesimulation.doc
User GroupIGNES
administrator
Visibilityshown
Archiving Policydenypublisher denyfinaldraft
Read Permissiondeny from all and allow from 150.163
5. Allied materials
Next Higher Units8JMKD3MGPCW/3ET38CH
DisseminationWEBSCI; PORTALCAPES.
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)IGNES
update 


Close