Large Eddy Simulation of Bluff Body Stabilized Turbulent Premixed Flame

Detalhes bibliográficos
Autor(a) principal: Salvador,Nicolas Moisés Cruz
Data de Publicação: 2013
Outros Autores: Mendonça,Márcio Teixeira de, Dourado,Wladimyr Mattos da Costa
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=S2175-91462013000200181
Resumo: ABSTRACT: A turbulent reacting flow in a channel with an obstacle was simulated computationally with large eddy simulation turbulence modeling and the Xi turbulent combustion model for premixed flame. The numerical model was implemented in the open source software OpenFoam. Both inert flow and reactive flow simulations were performed. In the inert flow, comparisons with velocity profile and recirculation vortex zone were performed as well as an analysis of the energy spectrum obtained numerically. The simulation with reacting flow considered a pre-mixture of propane (C 3 H 8) and air such that the equivalence ratio was equal to 0.65, with a theoretical adiabatic flame temperature of 1,800 K. The computational results were compared to experimental ones available in the literature. The equivalence ratio, inlet flow velocity, pressure, flame-holder shape and size, fuel type and turbulence intensity were taken from an experimental set up. The results shown in the present simulations are in good agreement with the experimental data.
id DCTA-1_16a759bccfe76812e467595adfd217b5
oai_identifier_str oai:scielo:S2175-91462013000200181
network_acronym_str DCTA-1
network_name_str Journal of Aerospace Technology and Management (Online)
repository_id_str
spelling Large Eddy Simulation of Bluff Body Stabilized Turbulent Premixed FlameComputational fluid dynamicsReacting flowLarge eddy simulationCombustion modelingABSTRACT: A turbulent reacting flow in a channel with an obstacle was simulated computationally with large eddy simulation turbulence modeling and the Xi turbulent combustion model for premixed flame. The numerical model was implemented in the open source software OpenFoam. Both inert flow and reactive flow simulations were performed. In the inert flow, comparisons with velocity profile and recirculation vortex zone were performed as well as an analysis of the energy spectrum obtained numerically. The simulation with reacting flow considered a pre-mixture of propane (C 3 H 8) and air such that the equivalence ratio was equal to 0.65, with a theoretical adiabatic flame temperature of 1,800 K. The computational results were compared to experimental ones available in the literature. The equivalence ratio, inlet flow velocity, pressure, flame-holder shape and size, fuel type and turbulence intensity were taken from an experimental set up. The results shown in the present simulations are in good agreement with the experimental data.Departamento de Ciência e Tecnologia Aeroespacial2013-06-01info:eu-repo/semantics/articleinfo:eu-repo/semantics/publishedVersiontext/htmlhttp://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462013000200181Journal of Aerospace Technology and Management v.5 n.2 2013reponame:Journal of Aerospace Technology and Management (Online)instname:Departamento de Ciência e Tecnologia Aeroespacial (DCTA)instacron:DCTA10.5028/jatm.v5i2.245info:eu-repo/semantics/openAccessSalvador,Nicolas Moisés CruzMendonça,Márcio Teixeira deDourado,Wladimyr Mattos da Costaeng2017-05-25T00:00:00Zoai:scielo:S2175-91462013000200181Revistahttp://www.jatm.com.br/ONGhttps://old.scielo.br/oai/scielo-oai.php||secretary@jatm.com.br2175-91461984-9648opendoar:2017-05-25T00:00Journal of Aerospace Technology and Management (Online) - Departamento de Ciência e Tecnologia Aeroespacial (DCTA)false
dc.title.none.fl_str_mv Large Eddy Simulation of Bluff Body Stabilized Turbulent Premixed Flame
title Large Eddy Simulation of Bluff Body Stabilized Turbulent Premixed Flame
spellingShingle Large Eddy Simulation of Bluff Body Stabilized Turbulent Premixed Flame
Salvador,Nicolas Moisés Cruz
Computational fluid dynamics
Reacting flow
Large eddy simulation
Combustion modeling
title_short Large Eddy Simulation of Bluff Body Stabilized Turbulent Premixed Flame
title_full Large Eddy Simulation of Bluff Body Stabilized Turbulent Premixed Flame
title_fullStr Large Eddy Simulation of Bluff Body Stabilized Turbulent Premixed Flame
title_full_unstemmed Large Eddy Simulation of Bluff Body Stabilized Turbulent Premixed Flame
title_sort Large Eddy Simulation of Bluff Body Stabilized Turbulent Premixed Flame
author Salvador,Nicolas Moisés Cruz
author_facet Salvador,Nicolas Moisés Cruz
Mendonça,Márcio Teixeira de
Dourado,Wladimyr Mattos da Costa
author_role author
author2 Mendonça,Márcio Teixeira de
Dourado,Wladimyr Mattos da Costa
author2_role author
author
dc.contributor.author.fl_str_mv Salvador,Nicolas Moisés Cruz
Mendonça,Márcio Teixeira de
Dourado,Wladimyr Mattos da Costa
dc.subject.por.fl_str_mv Computational fluid dynamics
Reacting flow
Large eddy simulation
Combustion modeling
topic Computational fluid dynamics
Reacting flow
Large eddy simulation
Combustion modeling
description ABSTRACT: A turbulent reacting flow in a channel with an obstacle was simulated computationally with large eddy simulation turbulence modeling and the Xi turbulent combustion model for premixed flame. The numerical model was implemented in the open source software OpenFoam. Both inert flow and reactive flow simulations were performed. In the inert flow, comparisons with velocity profile and recirculation vortex zone were performed as well as an analysis of the energy spectrum obtained numerically. The simulation with reacting flow considered a pre-mixture of propane (C 3 H 8) and air such that the equivalence ratio was equal to 0.65, with a theoretical adiabatic flame temperature of 1,800 K. The computational results were compared to experimental ones available in the literature. The equivalence ratio, inlet flow velocity, pressure, flame-holder shape and size, fuel type and turbulence intensity were taken from an experimental set up. The results shown in the present simulations are in good agreement with the experimental data.
publishDate 2013
dc.date.none.fl_str_mv 2013-06-01
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=S2175-91462013000200181
url http://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462013000200181
dc.language.iso.fl_str_mv eng
language eng
dc.relation.none.fl_str_mv 10.5028/jatm.v5i2.245
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.5 n.2 2013
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
_version_ 1754732530808913920