Large Eddy and RANS simulations of flows with adverse pressure gradients

Detalhes bibliográficos
Autor(a) principal: Antonio Batista de Jesus
Data de Publicação: 2015
Tipo de documento: Tese
Idioma: eng
Título da fonte: Biblioteca Digital de Teses e Dissertações do ITA
Texto Completo: http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=3310
Resumo: Large Eddy Simulations (LES) are performed to study flows with adverse pressure gradients (APG) produced by different two-dimensional bumps profiles installed on the bottom wall of a flat channel with parallel plates. An initial study considers a bump profile for which previous direct numerical simulation (DNS) results are available at the Reynolds number Re? = 617, based on the channel inlet friction velocity. The results obtained showed that LES is an adequate methodology for that type of simulation, being capable of reproducing accurately DNS results in terms of mean flow variables, Reynolds stresses profiles and turbulent stresses balances, with refinement levels much coarser than those from DNS. Particularly, LES results reproduce the steep increase in wall friction coefficients and strong peaks in Reynolds stresses in the adverse pressure gradient regions of both bottom and top walls of the channel which are observed in DNS results and linked to instability modes of the near wall streaks. LES is used to study the same bump profile at higher Reynolds numbers, Re? = 950 and Re? = 2000, and the results obtained are very similar to those at Re? = 617, including the steep increase in wall friction coefficients and strong peaks in Reynolds stresses at the APG region for both attached and mildly separated flows. Additional bump profiles are generated by modifying the rear portion of the initial bump configuration, which is elongated in order to produce a longer adverse pressure gradient (APG) region and promote smoother curvature changes as compared to the original profile. As in previous cases, a steep increment in Reynolds stresses values is observed at the APG region along with an augmentation of skin friction values. LES results indicate that the near wall streaks instability observed in previous DNS is characteristic of adverse pressure gradient regions located downstream of an initial favorable pressure gradient (FPG). All configurations studied with LES are also analyzed by Reynolds-average Navier-Stokes(RANS) computations with various turbulence closures. In all cases analyzed with LES it is observed that in the initial FPG region the streamwise component of the Reynolds stresses is increased while the other turbulent stresses are strongly reduced which creates a pattern analogous to the pre-transitional stages of a laminar boundary layer, which becomes unstable in the APG region. This strong non-equilibrium conditions present a great challenge for RANS models which is approximately captured by models sensitized for laminar-turbulent transition prediction.
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spelling Large Eddy and RANS simulations of flows with adverse pressure gradientsTurbulênciaGradientesDinâmica dos fluidos computacionalModelos matemáticosFísicaLarge Eddy Simulations (LES) are performed to study flows with adverse pressure gradients (APG) produced by different two-dimensional bumps profiles installed on the bottom wall of a flat channel with parallel plates. An initial study considers a bump profile for which previous direct numerical simulation (DNS) results are available at the Reynolds number Re? = 617, based on the channel inlet friction velocity. The results obtained showed that LES is an adequate methodology for that type of simulation, being capable of reproducing accurately DNS results in terms of mean flow variables, Reynolds stresses profiles and turbulent stresses balances, with refinement levels much coarser than those from DNS. Particularly, LES results reproduce the steep increase in wall friction coefficients and strong peaks in Reynolds stresses in the adverse pressure gradient regions of both bottom and top walls of the channel which are observed in DNS results and linked to instability modes of the near wall streaks. LES is used to study the same bump profile at higher Reynolds numbers, Re? = 950 and Re? = 2000, and the results obtained are very similar to those at Re? = 617, including the steep increase in wall friction coefficients and strong peaks in Reynolds stresses at the APG region for both attached and mildly separated flows. Additional bump profiles are generated by modifying the rear portion of the initial bump configuration, which is elongated in order to produce a longer adverse pressure gradient (APG) region and promote smoother curvature changes as compared to the original profile. As in previous cases, a steep increment in Reynolds stresses values is observed at the APG region along with an augmentation of skin friction values. LES results indicate that the near wall streaks instability observed in previous DNS is characteristic of adverse pressure gradient regions located downstream of an initial favorable pressure gradient (FPG). All configurations studied with LES are also analyzed by Reynolds-average Navier-Stokes(RANS) computations with various turbulence closures. In all cases analyzed with LES it is observed that in the initial FPG region the streamwise component of the Reynolds stresses is increased while the other turbulent stresses are strongly reduced which creates a pattern analogous to the pre-transitional stages of a laminar boundary layer, which becomes unstable in the APG region. This strong non-equilibrium conditions present a great challenge for RANS models which is approximately captured by models sensitized for laminar-turbulent transition prediction.Instituto Tecnológico de AeronáuticaJoão Luiz Filgueiras de AzevedoAntonio Batista de Jesus2015-07-08info:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/doctoralThesishttp://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=3310reponame:Biblioteca Digital de Teses e Dissertações do ITAinstname:Instituto Tecnológico de Aeronáuticainstacron:ITAenginfo:eu-repo/semantics/openAccessapplication/pdf2019-02-02T14:05:10Zoai:agregador.ibict.br.BDTD_ITA:oai:ita.br:3310http://oai.bdtd.ibict.br/requestopendoar:null2020-05-28 19:41:39.736Biblioteca Digital de Teses e Dissertações do ITA - Instituto Tecnológico de Aeronáuticatrue
dc.title.none.fl_str_mv Large Eddy and RANS simulations of flows with adverse pressure gradients
title Large Eddy and RANS simulations of flows with adverse pressure gradients
spellingShingle Large Eddy and RANS simulations of flows with adverse pressure gradients
Antonio Batista de Jesus
Turbulência
Gradientes
Dinâmica dos fluidos computacional
Modelos matemáticos
Física
title_short Large Eddy and RANS simulations of flows with adverse pressure gradients
title_full Large Eddy and RANS simulations of flows with adverse pressure gradients
title_fullStr Large Eddy and RANS simulations of flows with adverse pressure gradients
title_full_unstemmed Large Eddy and RANS simulations of flows with adverse pressure gradients
title_sort Large Eddy and RANS simulations of flows with adverse pressure gradients
author Antonio Batista de Jesus
author_facet Antonio Batista de Jesus
author_role author
dc.contributor.none.fl_str_mv João Luiz Filgueiras de Azevedo
dc.contributor.author.fl_str_mv Antonio Batista de Jesus
dc.subject.por.fl_str_mv Turbulência
Gradientes
Dinâmica dos fluidos computacional
Modelos matemáticos
Física
topic Turbulência
Gradientes
Dinâmica dos fluidos computacional
Modelos matemáticos
Física
dc.description.none.fl_txt_mv Large Eddy Simulations (LES) are performed to study flows with adverse pressure gradients (APG) produced by different two-dimensional bumps profiles installed on the bottom wall of a flat channel with parallel plates. An initial study considers a bump profile for which previous direct numerical simulation (DNS) results are available at the Reynolds number Re? = 617, based on the channel inlet friction velocity. The results obtained showed that LES is an adequate methodology for that type of simulation, being capable of reproducing accurately DNS results in terms of mean flow variables, Reynolds stresses profiles and turbulent stresses balances, with refinement levels much coarser than those from DNS. Particularly, LES results reproduce the steep increase in wall friction coefficients and strong peaks in Reynolds stresses in the adverse pressure gradient regions of both bottom and top walls of the channel which are observed in DNS results and linked to instability modes of the near wall streaks. LES is used to study the same bump profile at higher Reynolds numbers, Re? = 950 and Re? = 2000, and the results obtained are very similar to those at Re? = 617, including the steep increase in wall friction coefficients and strong peaks in Reynolds stresses at the APG region for both attached and mildly separated flows. Additional bump profiles are generated by modifying the rear portion of the initial bump configuration, which is elongated in order to produce a longer adverse pressure gradient (APG) region and promote smoother curvature changes as compared to the original profile. As in previous cases, a steep increment in Reynolds stresses values is observed at the APG region along with an augmentation of skin friction values. LES results indicate that the near wall streaks instability observed in previous DNS is characteristic of adverse pressure gradient regions located downstream of an initial favorable pressure gradient (FPG). All configurations studied with LES are also analyzed by Reynolds-average Navier-Stokes(RANS) computations with various turbulence closures. In all cases analyzed with LES it is observed that in the initial FPG region the streamwise component of the Reynolds stresses is increased while the other turbulent stresses are strongly reduced which creates a pattern analogous to the pre-transitional stages of a laminar boundary layer, which becomes unstable in the APG region. This strong non-equilibrium conditions present a great challenge for RANS models which is approximately captured by models sensitized for laminar-turbulent transition prediction.
description Large Eddy Simulations (LES) are performed to study flows with adverse pressure gradients (APG) produced by different two-dimensional bumps profiles installed on the bottom wall of a flat channel with parallel plates. An initial study considers a bump profile for which previous direct numerical simulation (DNS) results are available at the Reynolds number Re? = 617, based on the channel inlet friction velocity. The results obtained showed that LES is an adequate methodology for that type of simulation, being capable of reproducing accurately DNS results in terms of mean flow variables, Reynolds stresses profiles and turbulent stresses balances, with refinement levels much coarser than those from DNS. Particularly, LES results reproduce the steep increase in wall friction coefficients and strong peaks in Reynolds stresses in the adverse pressure gradient regions of both bottom and top walls of the channel which are observed in DNS results and linked to instability modes of the near wall streaks. LES is used to study the same bump profile at higher Reynolds numbers, Re? = 950 and Re? = 2000, and the results obtained are very similar to those at Re? = 617, including the steep increase in wall friction coefficients and strong peaks in Reynolds stresses at the APG region for both attached and mildly separated flows. Additional bump profiles are generated by modifying the rear portion of the initial bump configuration, which is elongated in order to produce a longer adverse pressure gradient (APG) region and promote smoother curvature changes as compared to the original profile. As in previous cases, a steep increment in Reynolds stresses values is observed at the APG region along with an augmentation of skin friction values. LES results indicate that the near wall streaks instability observed in previous DNS is characteristic of adverse pressure gradient regions located downstream of an initial favorable pressure gradient (FPG). All configurations studied with LES are also analyzed by Reynolds-average Navier-Stokes(RANS) computations with various turbulence closures. In all cases analyzed with LES it is observed that in the initial FPG region the streamwise component of the Reynolds stresses is increased while the other turbulent stresses are strongly reduced which creates a pattern analogous to the pre-transitional stages of a laminar boundary layer, which becomes unstable in the APG region. This strong non-equilibrium conditions present a great challenge for RANS models which is approximately captured by models sensitized for laminar-turbulent transition prediction.
publishDate 2015
dc.date.none.fl_str_mv 2015-07-08
dc.type.driver.fl_str_mv info:eu-repo/semantics/publishedVersion
info:eu-repo/semantics/doctoralThesis
status_str publishedVersion
format doctoralThesis
dc.identifier.uri.fl_str_mv http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=3310
url http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=3310
dc.language.iso.fl_str_mv eng
language eng
dc.rights.driver.fl_str_mv info:eu-repo/semantics/openAccess
eu_rights_str_mv openAccess
dc.format.none.fl_str_mv application/pdf
dc.publisher.none.fl_str_mv Instituto Tecnológico de Aeronáutica
publisher.none.fl_str_mv Instituto Tecnológico de Aeronáutica
dc.source.none.fl_str_mv reponame:Biblioteca Digital de Teses e Dissertações do ITA
instname:Instituto Tecnológico de Aeronáutica
instacron:ITA
reponame_str Biblioteca Digital de Teses e Dissertações do ITA
collection Biblioteca Digital de Teses e Dissertações do ITA
instname_str Instituto Tecnológico de Aeronáutica
instacron_str ITA
institution ITA
repository.name.fl_str_mv Biblioteca Digital de Teses e Dissertações do ITA - Instituto Tecnológico de Aeronáutica
repository.mail.fl_str_mv
subject_por_txtF_mv Turbulência
Gradientes
Dinâmica dos fluidos computacional
Modelos matemáticos
Física
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