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1. Identity statement
Reference TypeJournal Article
Sitemtc-m16c.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier8JMKD3MGP8W/353L2QP
Repositorysid.inpe.br/mtc-m18@80/2009/04.01.12.26   (restricted access)
Last Update2009:04.01.12.26.15 (UTC) administrator
Metadata Repositorysid.inpe.br/mtc-m18@80/2009/04.01.12.26.17
Metadata Last Update2020:04.28.17.48.32 (UTC) administrator
ISSN0022-4650
Citation KeySantos:2009:BlImLi
TitleBluntness impact on lift-to-drag ratio of hypersonic wedge flow
Year2009
Access Date2024, Mar. 29
Secondary TypePRE PI
Number of Files1
Size647 KiB
2. Context
AuthorSantos, Wilson Fernando Nogueira
GroupLCP-CTE-INPE-MCT-BR
AffiliationInstituto Nacional de Pesquisas Espaciais (INPE)
e-Mail Addressignes@lcp.inpe.br
JournalJournal of Spacecraft and Rockets
Volume46
Number2
Pages329-338
Secondary MarkB1_ENGENHARIAS_III B2_ENGENHARIAS_IV B1_INTERDISCIPLINAR
History (UTC)2009-07-14 18:48:26 :: ignes@lcp.inpe.br -> administrator ::
2010-05-11 01:08:14 :: administrator -> ignes@lcp.inpe.br ::
2011-05-24 23:11:51 :: ignes@lcp.inpe.br -> administrator :: 2009
2020-04-28 17:48:32 :: administrator -> simone :: 2009
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Version Typepublisher
AbstractA computational investigation was conducted on rarefied hypersonic flow past truncated wedges at incidence. Positive angle-of-attack effects on the aerodynamic surface quantities have been investigated by employing the direct simulation Monte Carlo method. The results highlight the sensitivity of the heat transfer coefficient, the total drag coefficient, the total lift coefficient, and the lift-to-drag ratio to changes not only on the angle of attack but also on the frontal-face thickness of the leading edges. Some significant differences between sharp and blunt leading edges were noted on the surface quantities. Interesting features observed in these surface properties showed that even small leading-edge thickness, compared with the freestream mean free path, still has important effects on high Mach number leading-edge flows. The analysis is important because it is impossible to achieve ideally sharp leading edges of airframes such as waveriders.
AreaCOMB
Arrangementurlib.net > BDMCI > Fonds > Produção anterior à 2021 > LABCP > Bluntness impact on...
doc Directory Contentaccess
source Directory Contentthere are no files
agreement Directory Contentthere are no files
4. Conditions of access and use
Languageen
Target Filebluntness.pdf
User Groupadministrator
ignes@lcp.inpe.br
marciana
Reader Groupadministrator
marciana
Visibilityshown
Archiving Policydenypublisher allowfinaldraft
Read Permissiondeny from all and allow from 150.163
Update Permissionnot transferred
5. Allied materials
Mirror Repositorysid.inpe.br/mtc-m18@80/2008/03.17.15.17.24
Next Higher Units8JMKD3MGPCW/3ET38CH
Citing Item Listsid.inpe.br/bibdigital@80/2006/04.07.15.50.13 1
DisseminationWEBSCI
Host Collectionsid.inpe.br/mtc-m18@80/2008/03.17.15.17
6. Notes
Empty Fieldsalternatejournal archivist callnumber copyholder copyright creatorhistory descriptionlevel doi electronicmailaddress format isbn keywords label lineage mark month nextedition notes orcid parameterlist parentrepositories previousedition previouslowerunit progress project resumeid rightsholder schedulinginformation secondarydate secondarykey session shorttitle sponsor subject tertiarymark tertiarytype typeofwork url
7. Description control
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