Simulation of Ablation in a Composite Thermal Protection System via an Interface Tracking Method

Detalhes bibliográficos
Autor(a) principal: Machado,Humberto Araujo
Data de Publicação: 2012
Tipo de documento: Artigo
Idioma: eng
Título da fonte: Journal of Aerospace Technology and Management (Online)
Texto Completo: http://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462012000300331
Resumo: Abstract: In this work, the two-dimensional computational simulation of the ablative process in a composite used in rocket thermal protection systems via an interface tracking method was presented. The ablative model considers the presence of two simultaneous moving fronts, the pyrolysis and char fronts. The results were compared with some experimental data, showing better agreement than the one-front model. Such procedure will allow a more accurate dimensioning of rocket thermal protection systems, contributing for project optimization.
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spelling Simulation of Ablation in a Composite Thermal Protection System via an Interface Tracking MethodAblationCompositeMoving boundaryComputational simulationAbstract: In this work, the two-dimensional computational simulation of the ablative process in a composite used in rocket thermal protection systems via an interface tracking method was presented. The ablative model considers the presence of two simultaneous moving fronts, the pyrolysis and char fronts. The results were compared with some experimental data, showing better agreement than the one-front model. Such procedure will allow a more accurate dimensioning of rocket thermal protection systems, contributing for project optimization.Departamento de Ciência e Tecnologia Aeroespacial2012-09-01info:eu-repo/semantics/articleinfo:eu-repo/semantics/publishedVersiontext/htmlhttp://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462012000300331Journal of Aerospace Technology and Management v.4 n.3 2012reponame:Journal of Aerospace Technology and Management (Online)instname:Departamento de Ciência e Tecnologia Aeroespacial (DCTA)instacron:DCTA10.5028/jatm.2012.04030312info:eu-repo/semantics/openAccessMachado,Humberto Araujoeng2017-05-24T00:00:00Zoai:scielo:S2175-91462012000300331Revistahttp://www.jatm.com.br/ONGhttps://old.scielo.br/oai/scielo-oai.php||secretary@jatm.com.br2175-91461984-9648opendoar:2017-05-24T00:00Journal of Aerospace Technology and Management (Online) - Departamento de Ciência e Tecnologia Aeroespacial (DCTA)false
dc.title.none.fl_str_mv Simulation of Ablation in a Composite Thermal Protection System via an Interface Tracking Method
title Simulation of Ablation in a Composite Thermal Protection System via an Interface Tracking Method
spellingShingle Simulation of Ablation in a Composite Thermal Protection System via an Interface Tracking Method
Machado,Humberto Araujo
Ablation
Composite
Moving boundary
Computational simulation
title_short Simulation of Ablation in a Composite Thermal Protection System via an Interface Tracking Method
title_full Simulation of Ablation in a Composite Thermal Protection System via an Interface Tracking Method
title_fullStr Simulation of Ablation in a Composite Thermal Protection System via an Interface Tracking Method
title_full_unstemmed Simulation of Ablation in a Composite Thermal Protection System via an Interface Tracking Method
title_sort Simulation of Ablation in a Composite Thermal Protection System via an Interface Tracking Method
author Machado,Humberto Araujo
author_facet Machado,Humberto Araujo
author_role author
dc.contributor.author.fl_str_mv Machado,Humberto Araujo
dc.subject.por.fl_str_mv Ablation
Composite
Moving boundary
Computational simulation
topic Ablation
Composite
Moving boundary
Computational simulation
description Abstract: In this work, the two-dimensional computational simulation of the ablative process in a composite used in rocket thermal protection systems via an interface tracking method was presented. The ablative model considers the presence of two simultaneous moving fronts, the pyrolysis and char fronts. The results were compared with some experimental data, showing better agreement than the one-front model. Such procedure will allow a more accurate dimensioning of rocket thermal protection systems, contributing for project optimization.
publishDate 2012
dc.date.none.fl_str_mv 2012-09-01
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=S2175-91462012000300331
url http://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462012000300331
dc.language.iso.fl_str_mv eng
language eng
dc.relation.none.fl_str_mv 10.5028/jatm.2012.04030312
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 Departamento de Ciência e Tecnologia Aeroespacial
publisher.none.fl_str_mv Departamento de Ciência e Tecnologia Aeroespacial
dc.source.none.fl_str_mv Journal of Aerospace Technology and Management v.4 n.3 2012
reponame:Journal of Aerospace Technology and Management (Online)
instname:Departamento de Ciência e Tecnologia Aeroespacial (DCTA)
instacron:DCTA
instname_str Departamento de Ciência e Tecnologia Aeroespacial (DCTA)
instacron_str DCTA
institution DCTA
reponame_str Journal of Aerospace Technology and Management (Online)
collection Journal of Aerospace Technology and Management (Online)
repository.name.fl_str_mv Journal of Aerospace Technology and Management (Online) - Departamento de Ciência e Tecnologia Aeroespacial (DCTA)
repository.mail.fl_str_mv ||secretary@jatm.com.br
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