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1. Identity statement
Reference TypeConference Paper (Conference Proceedings)
Sitemtc-m16c.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier8JMKD3MGP8W/33DJFH5
Repositorysid.inpe.br/mtc-m18@80/2008/07.04.12.41
Last Update2008:12.17.11.50.05 (UTC) administrator
Metadata Repositorysid.inpe.br/mtc-m18@80/2008/07.04.12.41.35
Metadata Last Update2018:06.04.04.05.19 (UTC) administrator
Secondary KeyINPE--PRE/
Citation KeySantos:2008:DiSiHy
TitleDirect simulation of hybrid power-law leading edge in hypersonic flow
FormatPapel
Year2008
Access Date2024, Apr. 26
Secondary TypePRE CI
Number of Files1
Size915 KiB
2. Context
AuthorSantos, Wilson Fernando Nogueira
GroupLCP-CTE-INPE-MCT-BR
AffiliationInstituto Nacional de Pesquisas Espaciais (INPE)
e-Mail Addressignes@lcp.inpe.br
Conference NameSimpósio de Mecânica Computacional, 8 (SIMMEC).
Conference LocationBelo Horizonte, MG
Date25-27 jun.
PublisherPUC Minas
Book TitleProceedings
Tertiary TypePaper
OrganizationPUC Minas
History (UTC)2008-12-17 11:50:06 :: ignes@lcp.inpe.br -> administrator ::
2018-06-04 04:05:19 :: administrator -> marciana :: 2008
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
KeywordsDSMC
hypersonic flow
rarefied flow
power-law shape
aerodynamic heating
AbstractABSTRACT: The aerodynamic characteristics of a family of hybrid power-law leading edges immersed in high-speed rarefied flow are examined by using the Direct Simulation MOnte Carlo (DSMC) method. The work is motivated by the fact that power-law leading edge shapes have characteristics of a sharp body (infinite body slope) and of a blunt body (zero radius of curvature) at the nose. The aerodynamic surface quantities for hybrid power-law shapes are compared to those for symmetric power-law shapes. The results presented highlight the sensitivity of the heat transfer coefficient, pressure coefficient, skin friction coefficient, total drag and total lift due to changes on the power-law exponent of the upper surface shape of the leading edges. Interesting features for sharp and blunt leading edges were noted on the computational results for the aerodynamic surface quantities. It was found that the stagnation point heating for hybrid power-law leading edges are smaller than that for symmetric power-law leading edges. The analysis also indicated that the total drag for the symmetric power-law leading edges is smaller than for hybrid power-law leading edges under the range of conditions investigated.
AreaCOMB
Arrangementurlib.net > BDMCI > Fonds > Produção anterior à 2021 > LABCP > Direct simulation of...
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4. Conditions of access and use
data URLhttp://urlib.net/ibi/8JMKD3MGP8W/33DJFH5
zipped data URLhttp://urlib.net/zip/8JMKD3MGP8W/33DJFH5
Languageen
Target Filedirect.pdf
User Groupadministrator
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Visibilityshown
5. Allied materials
Next Higher Units8JMKD3MGPCW/3ET38CH
Citing Item Listsid.inpe.br/bibdigital@80/2006/04.07.15.50.13 2
Host Collectionsid.inpe.br/mtc-m18@80/2008/03.17.15.17
6. Notes
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7. Description control
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