| 1. Identity statement | |
| Reference Type | Journal Article |
| Site | mtc-m16b.sid.inpe.br |
| Holder Code | isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S |
| Identifier | 6qtX3pFwXQZ3r59YDb/Gk4uP |
| Repository | sid.inpe.br/iris@1917/2005/06.01.18.34 (restricted access) |
| Last Update | 2021:11.18.15.04.06 (UTC) marciana |
| Metadata Repository | sid.inpe.br/iris@1917/2005/06.01.18.34.51 |
| Metadata Last Update | 2021:11.18.15.04.08 (UTC) marciana |
| Secondary Key | INPE--PRE/ |
| ISSN | 0022-4650 |
| Label | self-archiving-INPE-MCTIC-GOV-BR |
| Citation Key | SantosLewi:2005:CaShWa |
| Title | Calculation of shock wave structure over power law bodies in hypersonic flow  |
| Year | 2005 |
| Month | Mar.-Apr. |
| Access Date | 2024, Apr. 28 |
| Secondary Type | PRE PI |
| Number of Files | 1 |
| Size | 735 KiB |
| 2. Context | |
| Author | 1 Santos, Wilson Fernando Nogueira dos 2 Lewis, M. J. |
| Resume Identifier | 1 8JMKD3MGP5W/3C9JJCC |
| Group | 1 LCP-INPE-MCT-BR |
| Affiliation | 1 Instituto Nacional de Pesquisas Espaciais 2 University of Maryland |
| Journal | Journal of Spacecraft and Rockets |
| Volume | 42 |
| Number | 2 |
| Pages | 213-222 |
| History (UTC) | 2005-06-01 18:34:52 :: ignes -> administrator :: 2006-11-09 18:03:20 :: administrator -> ignes :: 2007-07-11 12:04:29 :: ignes -> administrator :: 2012-11-24 01:38:48 :: administrator -> ignes :: 2005 2013-02-20 14:54:13 :: ignes -> administrator :: 2005 2014-08-20 17:42:33 :: administrator -> marciana :: 2005 2014-08-20 17:43:43 :: marciana -> administrator :: 2005 2018-06-05 03:43:37 :: administrator -> marciana :: 2005 |
| 3. Content and structure | |
| Is the master or a copy? | is the master |
| Content Stage | completed |
| Transferable | 1 |
| Content Type | External Contribution |
| Version Type | publisher |
| Keywords | Monte-Carlo blunt simulation |
| Abstract | A numerical study is conducted of power law shaped leading edges situated in a rarefied hypersonic flow. The motivation-is interest in investigating the flowfield structure of power law shaped leading edges as possible candidates for blunting geometries of hypersonic leading edges. The primary aim is to examine in detail the effect of geometry of such leading edges on the shock wave structure. The sensitivity of the shock wave shape, standoff distance, and shock wave thickness to shape variations of the power law class of leading edges is calculated by using the direct simulation Monte Carlo method. Calculations show that the shape of the shock wave is in agreement with that predicted by the analytic hypersonic small disturbance theory for the flow conditions considered. |
| Area | COMB |
| Arrangement | urlib.net > Produção anterior à 2021 > LABCP > Calculation of shock... |
| 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 | calculation.pdf |
| User Group | administrator ignes marciana |
| Visibility | shown |
| Archiving Policy | denypublisher allowfinaldraft |
| Read Permission | deny from all and allow from 150.163 |
| Update Permission | not transferred |
| 5. Allied materials | |
| Next Higher Units | 8JMKD3MGPCW/3ET38CH |
| Dissemination | WEBSCI |
| Host Collection | cptec.inpe.br/walmeida/2003/04.25.17.12 |
| 6. Notes | |
| Empty Fields | alternatejournal archivist callnumber copyholder copyright creatorhistory descriptionlevel doi e-mailaddress electronicmailaddress format isbn lineage mark mirrorrepository nextedition notes orcid parameterlist parentrepositories previousedition previouslowerunit progress project readergroup rightsholder schedulinginformation secondarydate secondarymark session shorttitle sponsor subject tertiarymark tertiarytype typeofwork url |
| 7. Description control | |
| e-Mail (login) | marciana |
| update | |