An assessment of three turbulence models for two airfoils on transonic flows using a commercial package
Autor(a) principal: | |
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Data de Publicação: | 2010 |
Tipo de documento: | Dissertação |
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=1324 |
Resumo: | The Computational Fluid Dynamics is extensively employed in aerospace industry, which has become feasible due to the evolution of the computers (increased capacity) and to the relatively low computational cost. A great challenge is the inclusion of viscosity effects in the flow simulations, also using a mesh fine enough to catch all the velocity fluctuations due to turbulence. The demand for computational power makes it unfeasible for aerospace applications. Due to the coming of the turbulence models and Reynolds-averaged Navier-Stokes equations, the use of CFD has become common in aerospace industry, allowing optimization and reducing cycles of wind tunnel testing. This work presents the results of two-dimensional flow simulations made using three different turbulence models, as well as two distinct airfoils - a conventional and a supercritical. The simulated cases were chosen taking into account the availability of data for validation. A discussion concerning the results is presented, as well as the conclusion. |
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Biblioteca Digital de Teses e Dissertações do ITA |
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An assessment of three turbulence models for two airfoils on transonic flows using a commercial packageDinâmica dos fluidos computacionalEscoamento transônicoTurbulênciaAerofóliosAerodinâmicaFísicaEngenharia aeronáuticaAbsorvedores de radiaçãoThe Computational Fluid Dynamics is extensively employed in aerospace industry, which has become feasible due to the evolution of the computers (increased capacity) and to the relatively low computational cost. A great challenge is the inclusion of viscosity effects in the flow simulations, also using a mesh fine enough to catch all the velocity fluctuations due to turbulence. The demand for computational power makes it unfeasible for aerospace applications. Due to the coming of the turbulence models and Reynolds-averaged Navier-Stokes equations, the use of CFD has become common in aerospace industry, allowing optimization and reducing cycles of wind tunnel testing. This work presents the results of two-dimensional flow simulations made using three different turbulence models, as well as two distinct airfoils - a conventional and a supercritical. The simulated cases were chosen taking into account the availability of data for validation. A discussion concerning the results is presented, as well as the conclusion.Instituto Tecnológico de AeronáuticaMarcos Aurélio OrtegaPaulo Afonso de Oliveira SovieroEduardo Rafael Garcia Borota2010-07-16info:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/masterThesishttp://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=1324reponame:Biblioteca Digital de Teses e Dissertações do ITAinstname:Instituto Tecnológico de Aeronáuticainstacron:ITAenginfo:eu-repo/semantics/openAccessapplication/pdf2019-02-02T14:02:39Zoai:agregador.ibict.br.BDTD_ITA:oai:ita.br:1324http://oai.bdtd.ibict.br/requestopendoar:null2020-05-28 19:36:06.952Biblioteca Digital de Teses e Dissertações do ITA - Instituto Tecnológico de Aeronáuticatrue |
dc.title.none.fl_str_mv |
An assessment of three turbulence models for two airfoils on transonic flows using a commercial package |
title |
An assessment of three turbulence models for two airfoils on transonic flows using a commercial package |
spellingShingle |
An assessment of three turbulence models for two airfoils on transonic flows using a commercial package Eduardo Rafael Garcia Borota Dinâmica dos fluidos computacional Escoamento transônico Turbulência Aerofólios Aerodinâmica Física Engenharia aeronáutica Absorvedores de radiação |
title_short |
An assessment of three turbulence models for two airfoils on transonic flows using a commercial package |
title_full |
An assessment of three turbulence models for two airfoils on transonic flows using a commercial package |
title_fullStr |
An assessment of three turbulence models for two airfoils on transonic flows using a commercial package |
title_full_unstemmed |
An assessment of three turbulence models for two airfoils on transonic flows using a commercial package |
title_sort |
An assessment of three turbulence models for two airfoils on transonic flows using a commercial package |
author |
Eduardo Rafael Garcia Borota |
author_facet |
Eduardo Rafael Garcia Borota |
author_role |
author |
dc.contributor.none.fl_str_mv |
Marcos Aurélio Ortega Paulo Afonso de Oliveira Soviero |
dc.contributor.author.fl_str_mv |
Eduardo Rafael Garcia Borota |
dc.subject.por.fl_str_mv |
Dinâmica dos fluidos computacional Escoamento transônico Turbulência Aerofólios Aerodinâmica Física Engenharia aeronáutica Absorvedores de radiação |
topic |
Dinâmica dos fluidos computacional Escoamento transônico Turbulência Aerofólios Aerodinâmica Física Engenharia aeronáutica Absorvedores de radiação |
dc.description.none.fl_txt_mv |
The Computational Fluid Dynamics is extensively employed in aerospace industry, which has become feasible due to the evolution of the computers (increased capacity) and to the relatively low computational cost. A great challenge is the inclusion of viscosity effects in the flow simulations, also using a mesh fine enough to catch all the velocity fluctuations due to turbulence. The demand for computational power makes it unfeasible for aerospace applications. Due to the coming of the turbulence models and Reynolds-averaged Navier-Stokes equations, the use of CFD has become common in aerospace industry, allowing optimization and reducing cycles of wind tunnel testing. This work presents the results of two-dimensional flow simulations made using three different turbulence models, as well as two distinct airfoils - a conventional and a supercritical. The simulated cases were chosen taking into account the availability of data for validation. A discussion concerning the results is presented, as well as the conclusion. |
description |
The Computational Fluid Dynamics is extensively employed in aerospace industry, which has become feasible due to the evolution of the computers (increased capacity) and to the relatively low computational cost. A great challenge is the inclusion of viscosity effects in the flow simulations, also using a mesh fine enough to catch all the velocity fluctuations due to turbulence. The demand for computational power makes it unfeasible for aerospace applications. Due to the coming of the turbulence models and Reynolds-averaged Navier-Stokes equations, the use of CFD has become common in aerospace industry, allowing optimization and reducing cycles of wind tunnel testing. This work presents the results of two-dimensional flow simulations made using three different turbulence models, as well as two distinct airfoils - a conventional and a supercritical. The simulated cases were chosen taking into account the availability of data for validation. A discussion concerning the results is presented, as well as the conclusion. |
publishDate |
2010 |
dc.date.none.fl_str_mv |
2010-07-16 |
dc.type.driver.fl_str_mv |
info:eu-repo/semantics/publishedVersion info:eu-repo/semantics/masterThesis |
status_str |
publishedVersion |
format |
masterThesis |
dc.identifier.uri.fl_str_mv |
http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=1324 |
url |
http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=1324 |
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 |
Dinâmica dos fluidos computacional Escoamento transônico Turbulência Aerofólios Aerodinâmica Física Engenharia aeronáutica Absorvedores de radiação |
_version_ |
1706809268224655360 |