1. Identity statement | |
Reference Type | Journal Article |
Site | mtc-m21d.sid.inpe.br |
Holder Code | isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S |
Identifier | 8JMKD3MGP3W34T/4B63C82 |
Repository | sid.inpe.br/mtc-m21d/2024/04.17.15.54 |
Last Update | 2024:04.17.15.54.04 (UTC) simone |
Metadata Repository | sid.inpe.br/mtc-m21d/2024/04.17.15.54.04 |
Metadata Last Update | 2024:05.05.15.16.39 (UTC) administrator |
DOI | 10.1007/s40430-024-04843-9 |
ISSN | 1678-5878 |
Citation Key | CostaMendCostSalv:2024:TwBoLa |
Title | A two-dimensional boundary layer model for combustion chamber simulation |
Year | 2024 |
Month | May |
Access Date | 2024, July 27 |
Type of Work | journal article |
Secondary Type | PRE PN |
Number of Files | 1 |
Size | 1514 KiB |
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2. Context | |
Author | 1 Costa, Erykson Marconny da Silva 2 Mendonça, Márcio Teixeira de 3 Costa, Fernando de Souza 4 Salvador, Cesar A. V. |
Resume Identifier | 1 2 3 8JMKD3MGP5W/3C9JH46 |
ORCID | 1 2 0000-0002-6630-0749 |
Group | 1 PCP-ETES-DIPGR-INPE-MCTI-GOV-BR 2 PCP-ETES-DIPGR-INPE-MCTI-GOV-BR 3 COPDT-CGIP-INPE-MCTI-GOV-BR |
Affiliation | 1 Instituto Nacional de Pesquisas Espaciais (INPE) 2 Instituto Nacional de Pesquisas Espaciais (INPE) 3 Instituto Nacional de Pesquisas Espaciais (INPE) 4 Universidade Federal de Santa Maria (UFSM) |
Author e-Mail Address | 1 ErycksonMarconny@gmail.com 2 marcio_tm@yahoo.com 3 fernando.costa@inpe.br 4 valverde@ufsm.br |
Journal | Journal of the Brazilian Society of Mechanical Sciences and Engineering |
Volume | 46 |
Number | 5 |
Pages | e280 |
Secondary Mark | B1_INTERDISCIPLINAR B1_ENGENHARIAS_III B1_ENGENHARIAS_I B1_CIÊNCIAS_AMBIENTAIS B2_MATERIAIS B2_GEOCIÊNCIAS B2_ENGENHARIAS_IV B2_ENGENHARIAS_II B2_ARQUITETURA_E_URBANISMO B3_SAÚDE_COLETIVA B3_ODONTOLOGIA B3_CIÊNCIA_DE_ALIMENTOS B5_MATEMÁTICA_/_PROBABILIDADE_E_ESTATÍSTICA B5_CIÊNCIAS_BIOLÓGICAS_I C_CIÊNCIA_DA_COMPUTAÇÃO C_ASTRONOMIA_/_FÍSICA |
History (UTC) | 2024-04-17 15:54:04 :: simone -> administrator :: 2024-04-17 15:54:06 :: administrator -> simone :: 2024 2024-04-17 15:54:33 :: simone -> administrator :: 2024 2024-05-05 15:16:39 :: administrator -> simone :: 2024 |
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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 |
Version Type | publisher |
Keywords | Boundary layer Combustion chamber Combustion chamber cooling Propulsion Reactive flow Two phase combustion |
Abstract | Different propulsion systems can be used for launching payloads into orbit and for attitude control, orbit correction and maneuvering of satellites. Liquid bipropellant thrusters are used in applications requiring high specific impulses and high thrust levels and numerical simulation models can reduce development costs and time. This work describes a new 2D numerical model based on the boundary layer equations for the simulation of spray combustion. This model can be applied to the preliminary design of rocket combustion chambers, and allows the determination of droplet vaporization lengths, chemical composition, temperature profile and other thermodynamic and propulsion parameters. The computation time is, in general, lower than more complex 2D and 3D simulation models. Liquid fuel and oxidizer are injected into the combustion chamber with known droplet sizes and a pre-existing gas flow, which represents combustion products recirculation. The governing equations are discretized using centered and backward finite differences and the solution is marched downstream, considering droplet evaporation, mixture and combustion of propellant vapors with pre-existing gases. Burning of unsymmetrical dimethylhydrazine (UDMH) and dinitrogen tetroxide (NTO) was simulated with different mixture conditions and taking into account eleven product species. The model was validated by considering separately the different routines, comparing results of internal boundary layer flows, droplet evaporation and combustion products composition against expected theoretical behavior and results from other models. The influence of the equivalence ratio radial distribution on flow parameters was evaluated. The gas temperatures near the wall remained relatively constant after a certain distance downstream, depending on the local equivalence ratio distribution. The boundary layer remained very thin along the chamber due to the constant addition of combustion products. |
Area | COMB |
Arrangement 1 | urlib.net > BDMCI > Fonds > Produção pgr ATUAIS > PCP > A two-dimensional boundary... |
Arrangement 2 | urlib.net > BDMCI > Fonds > Produção a partir de 2021 > CGIP > A two-dimensional boundary... |
doc Directory Content | access |
source Directory Content | there are no files |
agreement Directory Content | |
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4. Conditions of access and use | |
data URL | http://urlib.net/ibi/8JMKD3MGP3W34T/4B63C82 |
zipped data URL | http://urlib.net/zip/8JMKD3MGP3W34T/4B63C82 |
Language | en |
Target File | s40430-024-04843-9.pdf |
User Group | simone |
Reader Group | administrator simone |
Visibility | shown |
Archiving Policy | allowpublisher allowfinaldraft |
Update Permission | not transferred |
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5. Allied materials | |
Mirror Repository | urlib.net/www/2021/06.04.03.40.25 |
Next Higher Units | 8JMKD3MGPCW/3F35D8B 8JMKD3MGPCW/46KUES5 |
Citing Item List | sid.inpe.br/bibdigital/2013/10.14.22.36 4 sid.inpe.br/bibdigital/2022/04.03.23.11 2 sid.inpe.br/mtc-m21/2012/07.13.14.46.07 1 |
Dissemination | WEBSCI; PORTALCAPES. |
Host Collection | urlib.net/www/2021/06.04.03.40 |
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6. Notes | |
Empty Fields | alternatejournal archivist callnumber copyholder copyright creatorhistory descriptionlevel e-mailaddress format isbn label lineage mark nextedition notes parameterlist parentrepositories previousedition previouslowerunit progress project readpermission rightsholder schedulinginformation secondarydate secondarykey session shorttitle sponsor subject tertiarymark tertiarytype url |
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7. Description control | |
e-Mail (login) | simone |
update | |
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