Three dimensional flow simulations with the finite element technique over a multi-stage rocket

Detalhes bibliográficos
Autor(a) principal: Scalabrin,L. C.
Data de Publicação: 2004
Outros Autores: Azevedo,J. L. F., Teixeira,P. R. F., Awruch,A. M.
Tipo de documento: Artigo
Idioma: eng
Título da fonte: Journal of the Brazilian Society of Mechanical Sciences and Engineering (Online)
Texto Completo: http://old.scielo.br/scielo.php?script=sci_arttext&pid=S1678-58782004000200001
Resumo: Aerodynamic flow simulations over the first Brazilian satellite launch vehicle, VLS, during its first-stage flight are presented. The three dimensional compressible flow is modeled by the Euler equations and a Taylor-Galerkin finite element method with artificial dissipation is used to obtain the numerical solution. Transonic and supersonic results for zero angle-of-attack are presented and compared to available experimental results. The influence of mesh refinement and artificial dissipation coeffcient on the transonic flow results are discussed. The results obtained for the supersonic simulations present good agreement with experimental data. The transonic simulation results capture the correct trends but they also indicate that this flight condition requires more refined meshes.
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spelling Three dimensional flow simulations with the finite element technique over a multi-stage rocketAeronautical engineeringcomputational fluid dynamicsfinite element techniqueTaylor-Galerkin methodtransonic flowssupersonic flowsAerodynamic flow simulations over the first Brazilian satellite launch vehicle, VLS, during its first-stage flight are presented. The three dimensional compressible flow is modeled by the Euler equations and a Taylor-Galerkin finite element method with artificial dissipation is used to obtain the numerical solution. Transonic and supersonic results for zero angle-of-attack are presented and compared to available experimental results. The influence of mesh refinement and artificial dissipation coeffcient on the transonic flow results are discussed. The results obtained for the supersonic simulations present good agreement with experimental data. The transonic simulation results capture the correct trends but they also indicate that this flight condition requires more refined meshes.Associação Brasileira de Engenharia e Ciências Mecânicas - ABCM2004-06-01info:eu-repo/semantics/articleinfo:eu-repo/semantics/publishedVersiontext/htmlhttp://old.scielo.br/scielo.php?script=sci_arttext&pid=S1678-58782004000200001Journal of the Brazilian Society of Mechanical Sciences and Engineering v.26 n.2 2004reponame:Journal of the Brazilian Society of Mechanical Sciences and Engineering (Online)instname:Associação Brasileira de Engenharia e Ciências Mecânicas (ABCM)instacron:ABCM10.1590/S1678-58782004000200001info:eu-repo/semantics/openAccessScalabrin,L. C.Azevedo,J. L. F.Teixeira,P. R. F.Awruch,A. M.eng2004-08-12T00:00:00Zoai:scielo:S1678-58782004000200001Revistahttps://www.scielo.br/j/jbsmse/https://old.scielo.br/oai/scielo-oai.php||abcm@abcm.org.br1806-36911678-5878opendoar:2004-08-12T00:00Journal of the Brazilian Society of Mechanical Sciences and Engineering (Online) - Associação Brasileira de Engenharia e Ciências Mecânicas (ABCM)false
dc.title.none.fl_str_mv Three dimensional flow simulations with the finite element technique over a multi-stage rocket
title Three dimensional flow simulations with the finite element technique over a multi-stage rocket
spellingShingle Three dimensional flow simulations with the finite element technique over a multi-stage rocket
Scalabrin,L. C.
Aeronautical engineering
computational fluid dynamics
finite element technique
Taylor-Galerkin method
transonic flows
supersonic flows
title_short Three dimensional flow simulations with the finite element technique over a multi-stage rocket
title_full Three dimensional flow simulations with the finite element technique over a multi-stage rocket
title_fullStr Three dimensional flow simulations with the finite element technique over a multi-stage rocket
title_full_unstemmed Three dimensional flow simulations with the finite element technique over a multi-stage rocket
title_sort Three dimensional flow simulations with the finite element technique over a multi-stage rocket
author Scalabrin,L. C.
author_facet Scalabrin,L. C.
Azevedo,J. L. F.
Teixeira,P. R. F.
Awruch,A. M.
author_role author
author2 Azevedo,J. L. F.
Teixeira,P. R. F.
Awruch,A. M.
author2_role author
author
author
dc.contributor.author.fl_str_mv Scalabrin,L. C.
Azevedo,J. L. F.
Teixeira,P. R. F.
Awruch,A. M.
dc.subject.por.fl_str_mv Aeronautical engineering
computational fluid dynamics
finite element technique
Taylor-Galerkin method
transonic flows
supersonic flows
topic Aeronautical engineering
computational fluid dynamics
finite element technique
Taylor-Galerkin method
transonic flows
supersonic flows
description Aerodynamic flow simulations over the first Brazilian satellite launch vehicle, VLS, during its first-stage flight are presented. The three dimensional compressible flow is modeled by the Euler equations and a Taylor-Galerkin finite element method with artificial dissipation is used to obtain the numerical solution. Transonic and supersonic results for zero angle-of-attack are presented and compared to available experimental results. The influence of mesh refinement and artificial dissipation coeffcient on the transonic flow results are discussed. The results obtained for the supersonic simulations present good agreement with experimental data. The transonic simulation results capture the correct trends but they also indicate that this flight condition requires more refined meshes.
publishDate 2004
dc.date.none.fl_str_mv 2004-06-01
dc.type.driver.fl_str_mv info:eu-repo/semantics/article
dc.type.status.fl_str_mv info:eu-repo/semantics/publishedVersion
format article
status_str publishedVersion
dc.identifier.uri.fl_str_mv http://old.scielo.br/scielo.php?script=sci_arttext&pid=S1678-58782004000200001
url http://old.scielo.br/scielo.php?script=sci_arttext&pid=S1678-58782004000200001
dc.language.iso.fl_str_mv eng
language eng
dc.relation.none.fl_str_mv 10.1590/S1678-58782004000200001
dc.rights.driver.fl_str_mv info:eu-repo/semantics/openAccess
eu_rights_str_mv openAccess
dc.format.none.fl_str_mv text/html
dc.publisher.none.fl_str_mv Associação Brasileira de Engenharia e Ciências Mecânicas - ABCM
publisher.none.fl_str_mv Associação Brasileira de Engenharia e Ciências Mecânicas - ABCM
dc.source.none.fl_str_mv Journal of the Brazilian Society of Mechanical Sciences and Engineering v.26 n.2 2004
reponame:Journal of the Brazilian Society of Mechanical Sciences and Engineering (Online)
instname:Associação Brasileira de Engenharia e Ciências Mecânicas (ABCM)
instacron:ABCM
instname_str Associação Brasileira de Engenharia e Ciências Mecânicas (ABCM)
instacron_str ABCM
institution ABCM
reponame_str Journal of the Brazilian Society of Mechanical Sciences and Engineering (Online)
collection Journal of the Brazilian Society of Mechanical Sciences and Engineering (Online)
repository.name.fl_str_mv Journal of the Brazilian Society of Mechanical Sciences and Engineering (Online) - Associação Brasileira de Engenharia e Ciências Mecânicas (ABCM)
repository.mail.fl_str_mv ||abcm@abcm.org.br
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