| 1. Identity statement | |
| Reference Type | Conference Paper (Conference Proceedings) |
| Site | mtc-m16.sid.inpe.br |
| Holder Code | isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S |
| Repository | sid.inpe.br/marciana/2004/01.08.13.56 (restricted access) |
| Last Update | 2009:03.11.18.11.21 (UTC) administrator |
| Metadata Repository | sid.inpe.br/marciana/2004/01.08.13.56.39 |
| Metadata Last Update | 2018:06.05.01.20.41 (UTC) administrator |
| Secondary Key | INPE-10377-PRE/5877 |
| Citation Key | SantosLewi:2003:ShWaSt |
| Title | Shock Wave Structure in a Rarefied Hypersonic Flow on Power Law Shaped Leading Edges  |
| Format | On-line |
| Year | 2003 |
| Access Date | 2024, Apr. 27 |
| Secondary Type | PRE CI |
| Number of Files | 1 |
| Size | 437 KiB |
| 2. Context | |
| Author | 1 Santos, Wilson Fernando Nogueira 2 Lewis, Mark J. |
| Group | 1 LCP-INPE-MCT-BR |
| Affiliation | 1 Combustion and Propulsion Laboratory 2 National Institute for Space Research |
| Conference Name | AIAA Aerospace Sciences Meeting and Exhibit, 41. |
| Conference Location | Reno, NV |
| Date | 6-9, 2003 |
| Publisher | AIAA |
| Publisher City | Reston, VA |
| Pages | 1-11 |
| Book Title | Proceedings |
| History (UTC) | 2008-06-10 23:02:09 :: administrator -> marciana :: 2009-03-11 18:11:21 :: marciana -> administrator :: 2018-06-05 01:20:41 :: administrator -> marciana :: 2003 |
| 3. Content and structure | |
| Is the master or a copy? | is the master |
| Content Stage | completed |
| Transferable | 1 |
| Content Type | External Contribution |
| Keywords | propulsão power law shaped leading edges hypersonic flow Direct Simulation Monte Carlo method DSMC |
| Abstract | This work deals with a numerical study on power law shaped leading edges situated in a rarefied hypersonic flow. The work is motivated by 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 of this paper is to examine in details the geometry effect 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 such leading edges is calculated by using a Direct Simulation Monte Carlo method. Calculations show that the shock wave shape is in surprising agreement with that predicted by the hypersonic small disturbance theory for the flow conditions considered. |
| Area | COMB |
| Arrangement | urlib.net > BDMCI > Fonds > Produção anterior à 2021 > LABCP > Shock Wave Structure... |
| 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 | shock.pdf |
| User Group | administrator marciana |
| Visibility | shown |
| Copy Holder | SID/SCD |
| Read Permission | deny from all and allow from 150.163 |
| 5. Allied materials | |
| Next Higher Units | 8JMKD3MGPCW/3ET38CH |
| Host Collection | sid.inpe.br/banon/2003/08.15.17.40 |
| 6. Notes | |
| Notes | (AIAA 2003/1134) |
| Empty Fields | archivingpolicy archivist callnumber copyright creatorhistory descriptionlevel dissemination documentstage doi e-mailaddress edition editor electronicmailaddress identifier isbn issn label lineage mark mirrorrepository nextedition numberofvolumes orcid organization parameterlist parentrepositories previousedition previouslowerunit progress project readergroup resumeid rightsholder schedulinginformation secondarydate secondarymark serieseditor session shorttitle sponsor subject tertiarymark tertiarytype type url versiontype volume |
| 7. Description control | |
| e-Mail (login) | marciana |
| update | |