| 1. Identity statement | |
| Reference Type | Journal Article |
| Site | mtc-m16b.sid.inpe.br |
| Holder Code | isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S |
| Identifier | 6qtX3pFwXQZGivnK2Y/MhR2S |
| Repository | sid.inpe.br/mtc-m17@80/2006/08.28.17.00 (restricted access) |
| Last Update | 2006:08.28.17.00.59 (UTC) administrator |
| Metadata Repository | sid.inpe.br/mtc-m17@80/2006/08.28.17.01.01 |
| Metadata Last Update | 2018:06.05.03.44.00 (UTC) administrator |
| Secondary Key | INPE--PRE/ |
| ISSN | 0100-7386 |
| Citation Key | Santos:2006:EfCoAe |
| Title | Effects of compressibility on aerodynamic surface quantities over low-density hypersonic wedge flow  |
| Year | 2006 |
| Month | Jul.-Sept. |
| Access Date | 2024, Apr. 28 |
| Secondary Type | PRE PI |
| Number of Files | 1 |
| Size | 365 KiB |
| 2. Context | |
| Author | Santos, Wilson Fernando Nogueira |
| Group | LCP-INPE-MCT-BR |
| Affiliation | Instituto Nacional de Pesquisas Espaciais |
| Journal | Journal of the Brazilian Society of Mechanical Sciences and Engineering |
| Volume | 28 |
| Number | 3 |
| Pages | 362-372 |
| History (UTC) | 2006-08-28 17:01:01 :: ignes -> administrator :: 2010-05-11 02:47:24 :: administrator -> ignes :: 2011-05-29 09:18:25 :: ignes -> administrator :: 2012-11-24 01:39:02 :: administrator -> ignes :: 2006 2013-02-20 14:54:14 :: ignes -> administrator :: 2006 2018-06-05 03:44:00 :: administrator -> marciana :: 2006 |
| 3. Content and structure | |
| Is the master or a copy? | is the master |
| Content Stage | completed |
| Transferable | 1 |
| Content Type | External Contribution |
| Keywords | Rarefied flow hypersonic flow DSMC blunt leading edge stagnation point heatung |
| Abstract | Hypersonic flow past truncated wedges at zero incidence in thermal non-equilibrium is investigated for a range of Mach number from 5 to 12. The simulations were performed by using a Direct Simulation Monte Carlo (DSMC) Method. The study focuses the attention of designers of hypersonic configurations on the fundamental parameter of bluntness, which can have an important impact on even initial design. Some significant differences between sharp and blunt leading edges were noted on the heat transfer, pressure and skin friction coefficients as well as on total drag. Interesting features observed in the surface fluxes showed that small leading edge thickness compared to the freestream mean free path still has important effects on high Mach number leading edge flows. The numerical results present reasonable comparison for wall pressure and heat transfer predictions with experiments conducted in a shock tunnel. |
| Area | COMB |
| Arrangement | urlib.net > BDMCI > Fonds > Produção anterior à 2021 > LABCP > Effects of compressibility... |
| doc Directory Content | access |
| source Directory Content | there are no files |
| agreement Directory Content | there are no files |
| 4. Conditions of access and use | |
| Language | en |
| Target File | effects.pdf |
| User Group | administrator ignes |
| Visibility | shown |
| Archiving Policy | denypublisher denyfinaldraft |
| Read Permission | deny from all and allow from 150.163 |
| 5. Allied materials | |
| Next Higher Units | 8JMKD3MGPCW/3ET38CH |
| Dissemination | WEBSCI; PORTALCAPES. |
| Host Collection | lcp.inpe.br/ignes/2004/02.12.18.39 cptec.inpe.br/walmeida/2003/04.25.17.12 |
| 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 secondarymark session shorttitle sponsor subject tertiarymark tertiarytype typeofwork url versiontype |
| 7. Description control | |
| e-Mail (login) | marciana |
| update | |