| 1. Identity statement | |
| Reference Type | Journal Article |
| Site | mtc-m16.sid.inpe.br |
| Holder Code | isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S |
| Identifier | 6qtX3pFwXQZsFDuKxG/AuGDb |
| Repository | sid.inpe.br/marciana/2003/12.18.12.57 (restricted access) |
| Last Update | 2013:04.18.17.51.50 (UTC) administrator |
| Metadata Repository | sid.inpe.br/marciana/2003/12.18.12.57.49 |
| Metadata Last Update | 2021:02.11.18.10.16 (UTC) administrator |
| Secondary Key | INPE--PRE/ |
| DOI | 10.1080/10407780490424307 |
| ISSN | 1040-7782 1521-0634 |
| Citation Key | MarchiLaroSilvHinc:2004:NuSoFl |
| Title | Numerical solutions of flows in rocket engines with regenerative cooling  |
| Year | 2004 |
| Access Date | 2024, May 05 |
| Secondary Type | PRE PI |
| Number of Files | 1 |
| Size | 301 KiB |
| 2. Context | |
| Author | 1 Marchi, Carlos Henrique 2 Laroca, Fernando 3 Silva, António Fábio Carvalho da 4 Hinckel, José Nivaldo |
| Group | 1 2 3 4 DMC-INPE-MCT-BR |
| Affiliation | 1 Department of Mechanical Engineering, Federal University of Paraná, Curitiba, PR, Brazil 2 Federal University of Paraná , Curitiba, PR, Brazil 3 Department of Mechanical Engineering, Federal University of Santa Catarina, Florianópolis, SC, Brazil 4 Instituto Nacional de Pesquisas Espaciais (INPE) |
| Journal | Numerical Heat Transfer. Part A: Applications |
| Volume | 45 |
| Pages | 699–717 |
| History (UTC) | 2012-11-24 01:54:21 :: administrator -> banon :: 2003 2013-02-04 17:46:28 :: banon -> administrator :: 2003 2013-02-22 16:48:04 :: administrator -> marciana :: 2003 2013-04-18 17:51:51 :: marciana -> administrator :: 2003 -> 2004 2021-02-11 18:10:16 :: administrator -> marciana :: 2004 |
| 3. Content and structure | |
| Is the master or a copy? | is the master |
| Content Stage | completed |
| Transferable | 1 |
| Content Type | External Contribution |
| Abstract | A one-dimensional mathematical model is presented for flows in a rocket engine that has a regenerative cooling system. The problem involves the flow of a gas in a convergingdiverging nozzle, the flow of a coolant in channels distributed around the engine, and the heat conduction through a wall between the gas and the coolant. The numerical model adopted is based on the finite-volume method with a second-order scheme. It was noted that it is important to use variable properties in order to predict the maximum wall temperature in the rocket engine and the drop in pressure of the coolant as it moves along the channels, whereas the thrust of the engine can be calculated with constant properties. |
| Area | ETES |
| Arrangement | urlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Numerical solutions of... |
| 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 | 10407780490424307.pdf |
| User Group | administrator banon marciana |
| Visibility | shown |
| Archiving Policy | denypublisher denyfinaldraft12 |
| Read Permission | deny from all and allow from 150.163 |
| Update Permission | not transferred |
| 5. Allied materials | |
| Next Higher Units | 8JMKD3MGPCW/446AF4B |
| Dissemination | WEBSCI; PORTALCAPES. |
| Host Collection | sid.inpe.br/banon/2003/08.15.17.40 |
| 6. Notes | |
| Empty Fields | alternatejournal archivist callnumber copyholder copyright creatorhistory descriptionlevel e-mailaddress electronicmailaddress format isbn keywords label lineage mark mirrorrepository month nextedition notes number 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 | |