Study of Conservation on Implicit Techniques for Unstructured Finite Volume Navier-Stokes Solvers
Autor(a) principal: | |
---|---|
Data de Publicação: | 2014 |
Outros Autores: | , , |
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. |
id |
DCTA-1_032ce1b00fd907503d0dda0d067606a4 |
---|---|
oai_identifier_str |
oai:scielo:S2175-91462014000300267 |
network_acronym_str |
DCTA-1 |
network_name_str |
Journal of Aerospace Technology and Management (Online) |
repository_id_str |
|
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 |
_version_ |
1754732530883362816 |