Study of Conservation on Implicit Techniques for Unstructured Finite Volume Navier-Stokes Solvers

Detalhes bibliográficos
Autor(a) principal: Junqueira-Junior,Carlos
Data de Publicação: 2014
Outros Autores: Scalabrin,Leonardo Costa, Basso,Edson, Azevedo,João Luiz F.
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=S2175-91462014000300267
Resumo: ABSTRACT: The work is a study of conservation on linearization techniques of time-marching schemes for the unstructured finite volume Reynolds-averaged Navier-Stokes formulation. The solver used in this work calculates the numerical flux applying an upwind discretization based on the flux vector splitting scheme. This numerical treatment results in a very large sparse linear system. The direct solution of this full implicit linear system is very expensive and, in most cases, impractical. There are several numerical approaches which are commonly used by the scientific community to treat sparse linear systems, and the point-implicit integration was selected in the present case. However, numerical approaches to solve implicit linear systems can be non-conservative in time, even for formulations which are conservative by construction, as the finite volume techniques. Moreover, there are physical problems which strongly demand conservative schemes in order to achieve the correct numerical solution. The work presents results of numerical simulations to evaluate the conservation of implicit and explicit time-marching methods and discusses numerical requirements that can help avoiding such non-conservation issues.
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spelling Study of Conservation on Implicit Techniques for Unstructured Finite Volume Navier-Stokes SolversComputational fluid dynamicsTime marching methodsFlux vector splitting schemeConservative discretizationABSTRACT: The work is a study of conservation on linearization techniques of time-marching schemes for the unstructured finite volume Reynolds-averaged Navier-Stokes formulation. The solver used in this work calculates the numerical flux applying an upwind discretization based on the flux vector splitting scheme. This numerical treatment results in a very large sparse linear system. The direct solution of this full implicit linear system is very expensive and, in most cases, impractical. There are several numerical approaches which are commonly used by the scientific community to treat sparse linear systems, and the point-implicit integration was selected in the present case. However, numerical approaches to solve implicit linear systems can be non-conservative in time, even for formulations which are conservative by construction, as the finite volume techniques. Moreover, there are physical problems which strongly demand conservative schemes in order to achieve the correct numerical solution. The work presents results of numerical simulations to evaluate the conservation of implicit and explicit time-marching methods and discusses numerical requirements that can help avoiding such non-conservation issues.Departamento de Ciência e Tecnologia Aeroespacial2014-09-01info:eu-repo/semantics/articleinfo:eu-repo/semantics/publishedVersiontext/htmlhttp://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462014000300267Journal of Aerospace Technology and Management v.6 n.3 2014reponame:Journal of Aerospace Technology and Management (Online)instname:Departamento de Ciência e Tecnologia Aeroespacial (DCTA)instacron:DCTA10.5028/jatm.v6i3.371info:eu-repo/semantics/openAccessJunqueira-Junior,CarlosScalabrin,Leonardo CostaBasso,EdsonAzevedo,João Luiz F.eng2017-05-29T00:00:00Zoai:scielo:S2175-91462014000300267Revistahttp://www.jatm.com.br/ONGhttps://old.scielo.br/oai/scielo-oai.php||secretary@jatm.com.br2175-91461984-9648opendoar:2017-05-29T00:00Journal of Aerospace Technology and Management (Online) - Departamento de Ciência e Tecnologia Aeroespacial (DCTA)false
dc.title.none.fl_str_mv Study of Conservation on Implicit Techniques for Unstructured Finite Volume Navier-Stokes Solvers
title Study of Conservation on Implicit Techniques for Unstructured Finite Volume Navier-Stokes Solvers
spellingShingle Study of Conservation on Implicit Techniques for Unstructured Finite Volume Navier-Stokes Solvers
Junqueira-Junior,Carlos
Computational fluid dynamics
Time marching methods
Flux vector splitting scheme
Conservative discretization
title_short Study of Conservation on Implicit Techniques for Unstructured Finite Volume Navier-Stokes Solvers
title_full Study of Conservation on Implicit Techniques for Unstructured Finite Volume Navier-Stokes Solvers
title_fullStr Study of Conservation on Implicit Techniques for Unstructured Finite Volume Navier-Stokes Solvers
title_full_unstemmed Study of Conservation on Implicit Techniques for Unstructured Finite Volume Navier-Stokes Solvers
title_sort Study of Conservation on Implicit Techniques for Unstructured Finite Volume Navier-Stokes Solvers
author Junqueira-Junior,Carlos
author_facet Junqueira-Junior,Carlos
Scalabrin,Leonardo Costa
Basso,Edson
Azevedo,João Luiz F.
author_role author
author2 Scalabrin,Leonardo Costa
Basso,Edson
Azevedo,João Luiz F.
author2_role author
author
author
dc.contributor.author.fl_str_mv Junqueira-Junior,Carlos
Scalabrin,Leonardo Costa
Basso,Edson
Azevedo,João Luiz F.
dc.subject.por.fl_str_mv Computational fluid dynamics
Time marching methods
Flux vector splitting scheme
Conservative discretization
topic Computational fluid dynamics
Time marching methods
Flux vector splitting scheme
Conservative discretization
description ABSTRACT: The work is a study of conservation on linearization techniques of time-marching schemes for the unstructured finite volume Reynolds-averaged Navier-Stokes formulation. The solver used in this work calculates the numerical flux applying an upwind discretization based on the flux vector splitting scheme. This numerical treatment results in a very large sparse linear system. The direct solution of this full implicit linear system is very expensive and, in most cases, impractical. There are several numerical approaches which are commonly used by the scientific community to treat sparse linear systems, and the point-implicit integration was selected in the present case. However, numerical approaches to solve implicit linear systems can be non-conservative in time, even for formulations which are conservative by construction, as the finite volume techniques. Moreover, there are physical problems which strongly demand conservative schemes in order to achieve the correct numerical solution. The work presents results of numerical simulations to evaluate the conservation of implicit and explicit time-marching methods and discusses numerical requirements that can help avoiding such non-conservation issues.
publishDate 2014
dc.date.none.fl_str_mv 2014-09-01
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=S2175-91462014000300267
url http://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462014000300267
dc.language.iso.fl_str_mv eng
language eng
dc.relation.none.fl_str_mv 10.5028/jatm.v6i3.371
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.6 n.3 2014
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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