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1. Identity statement
Reference TypeJournal Article
Sitemtc-m21d.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier8JMKD3MGP3W34T/4B63C82
Repositorysid.inpe.br/mtc-m21d/2024/04.17.15.54
Last Update2024:04.17.15.54.04 (UTC) simone
Metadata Repositorysid.inpe.br/mtc-m21d/2024/04.17.15.54.04
Metadata Last Update2024:05.05.15.16.39 (UTC) administrator
DOI10.1007/s40430-024-04843-9
ISSN1678-5878
Citation KeyCostaMendCostSalv:2024:TwBoLa
TitleA two-dimensional boundary layer model for combustion chamber simulation
Year2024
MonthMay
Access Date2024, July 27
Type of Workjournal article
Secondary TypePRE PN
Number of Files1
Size1514 KiB
2. Context
Author1 Costa, Erykson Marconny da Silva
2 Mendonça, Márcio Teixeira de
3 Costa, Fernando de Souza
4 Salvador, Cesar A. V.
Resume Identifier1
2
3 8JMKD3MGP5W/3C9JH46
ORCID1
2 0000-0002-6630-0749
Group1 PCP-ETES-DIPGR-INPE-MCTI-GOV-BR
2 PCP-ETES-DIPGR-INPE-MCTI-GOV-BR
3 COPDT-CGIP-INPE-MCTI-GOV-BR
Affiliation1 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 Address1 ErycksonMarconny@gmail.com
2 marcio_tm@yahoo.com
3 fernando.costa@inpe.br
4 valverde@ufsm.br
JournalJournal of the Brazilian Society of Mechanical Sciences and Engineering
Volume46
Number5
Pagese280
Secondary MarkB1_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
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Version Typepublisher
KeywordsBoundary layer
Combustion chamber
Combustion chamber cooling
Propulsion
Reactive flow
Two phase combustion
AbstractDifferent 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.
AreaCOMB
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4. Conditions of access and use
data URLhttp://urlib.net/ibi/8JMKD3MGP3W34T/4B63C82
zipped data URLhttp://urlib.net/zip/8JMKD3MGP3W34T/4B63C82
Languageen
Target Files40430-024-04843-9.pdf
User Groupsimone
Reader Groupadministrator
simone
Visibilityshown
Archiving Policyallowpublisher allowfinaldraft
Update Permissionnot transferred
5. Allied materials
Mirror Repositoryurlib.net/www/2021/06.04.03.40.25
Next Higher Units8JMKD3MGPCW/3F35D8B
8JMKD3MGPCW/46KUES5
Citing Item Listsid.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
DisseminationWEBSCI; PORTALCAPES.
Host Collectionurlib.net/www/2021/06.04.03.40
6. Notes
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