1. Identity statement | |
Reference Type | Journal Article |
Site | mtc-m16b.sid.inpe.br |
Holder Code | isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S |
Identifier | 6qtX3pFwXQZGivnK2Y/QnqSw |
Repository | sid.inpe.br/mtc-m17@80/2007/06.06.12.23 (restricted access) |
Last Update | 2007:06.06.12.23.01 (UTC) administrator |
Metadata Repository | sid.inpe.br/mtc-m17@80/2007/06.06.12.23.02 |
Metadata Last Update | 2018:06.05.03.34.14 (UTC) administrator |
ISSN | 0103-9733 |
Citation Key | Santos:2007:GaInEf |
Title | Gas-surface interaction effect on round leading aerothermodynamics |
Year | 2007 |
Month | Jun. |
Access Date | 2024, Apr. 28 |
Secondary Type | PRE PN |
Number of Files | 1 |
Size | 1231 KiB |
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2. Context | |
Author | Santos, Wilson Fernando Nogueira |
Group | LCP-INPE-MCT-BR |
Affiliation | Instituto Nacional de Pesquisas Espaciais (INPE) |
Journal | Brazilian Journal of Physics |
Volume | 37 |
Number | 2A |
Pages | 337-348 |
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 |
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3. Content and structure | |
Is the master or a copy? | is the master |
Content Stage | completed |
Transferable | 1 |
Content Type | External Contribution |
Keywords | aerothermodynamics gas flow surfaces |
Abstract | ABSTRACT: 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. |
Area | COMB |
Arrangement | urlib.net > BDMCI > Fonds > Produção anterior à 2021 > LABCP > Gas-surface interaction effect... |
doc Directory Content | access |
source Directory Content | there are no files |
agreement Directory Content | there are no files |
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4. Conditions of access and use | |
Language | en |
Target File | gas.pdf |
User Group | administrator ignes |
Visibility | shown |
Archiving Policy | denypublisher denyfinaldraft12 |
Read Permission | deny from all and allow from 150.163 |
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5. Allied materials | |
Next Higher Units | 8JMKD3MGPCW/3ET38CH |
Dissemination | WEBSCI; PORTALCAPES; SCIELO. |
Host Collection | lcp.inpe.br/ignes/2004/02.12.18.39 cptec.inpe.br/walmeida/2003/04.25.17.12 |
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6. Notes | |
Empty Fields | alternatejournal 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 |
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7. Description control | |
e-Mail (login) | marciana |
update | |
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