Simplified engine/nacelle heat transfer case analysis via CFD modeling for supporting the preliminary design of nacelle cooling/ventilation system.

Detalhes bibliográficos
Autor(a) principal: Ricardo Pereira das Neves
Data de Publicação: 2009
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=861
Resumo: An aeronautical engine is a complex machine composed of different components operating at different temperatures that in conjunction with the nacelle creates a crowded region with the coupled heat transfer mechanisms to be covered by the nacelle cooling/ventilation system. The final configuration of this system is defined through a demanding refinement of the preliminary design. For this reason the preliminary design is considered the key point and as a rule it can be based on the use of similar design scaling or by the use of numerical approaches. The numerical approaches available are the use of a one-dimensional heat transfer analysis or a complete heat transfer analysis via Computational Fluid Dynamics, or CFD. The short lead time usually available to get the nacelle ready leads the using of a more simplified analysis. Even though this simplified analysis is a lesser laborious activity than a more complete heat transfer analysis, it is still a relatively complicated task. Thus this work aims at presenting a simple methodology for supporting the preliminary design of nacelle cooling/ventilation which is basically relies on confirming if such system is really necessary taking into consideration the temperature distribution in the region between the engine/nacelle and the specified limits. In this case, the proposed methodology presented in this work is concerning to the natural convection analysis in a bidimensional engine/nacelle model by the use of CFD. In view of the fact that there is no specific literature reference available about such methodology or the natural convection analysis in an analogous model configuration or even experimental tests results, it was decided to utilize the studies about natural convection in concentric cylinders in the model validation process and to show the suitability of the proposed methodology, it was directly compared to the natural convection analysis in a simplified tridimensional engine/nacelle model by the use of CFD tool which would be performed by the manufacturer.
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spelling Simplified engine/nacelle heat transfer case analysis via CFD modeling for supporting the preliminary design of nacelle cooling/ventilation system.Transferência de calorDinâmica dos fluidos computacionalSistemas de refrigeraçãoVentilaçãoNacelasMotores de aeronavesTermodinâmicaFísicaAn aeronautical engine is a complex machine composed of different components operating at different temperatures that in conjunction with the nacelle creates a crowded region with the coupled heat transfer mechanisms to be covered by the nacelle cooling/ventilation system. The final configuration of this system is defined through a demanding refinement of the preliminary design. For this reason the preliminary design is considered the key point and as a rule it can be based on the use of similar design scaling or by the use of numerical approaches. The numerical approaches available are the use of a one-dimensional heat transfer analysis or a complete heat transfer analysis via Computational Fluid Dynamics, or CFD. The short lead time usually available to get the nacelle ready leads the using of a more simplified analysis. Even though this simplified analysis is a lesser laborious activity than a more complete heat transfer analysis, it is still a relatively complicated task. Thus this work aims at presenting a simple methodology for supporting the preliminary design of nacelle cooling/ventilation which is basically relies on confirming if such system is really necessary taking into consideration the temperature distribution in the region between the engine/nacelle and the specified limits. In this case, the proposed methodology presented in this work is concerning to the natural convection analysis in a bidimensional engine/nacelle model by the use of CFD. In view of the fact that there is no specific literature reference available about such methodology or the natural convection analysis in an analogous model configuration or even experimental tests results, it was decided to utilize the studies about natural convection in concentric cylinders in the model validation process and to show the suitability of the proposed methodology, it was directly compared to the natural convection analysis in a simplified tridimensional engine/nacelle model by the use of CFD tool which would be performed by the manufacturer.Instituto Tecnológico de AeronáuticaCláudia Regina de AndradeRicardo Pereira das Neves2009-11-06info:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/masterThesishttp://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=861reponame:Biblioteca Digital de Teses e Dissertações do ITAinstname:Instituto Tecnológico de Aeronáuticainstacron:ITAenginfo:eu-repo/semantics/openAccessapplication/pdf2019-02-02T14:01:58Zoai:agregador.ibict.br.BDTD_ITA:oai:ita.br:861http://oai.bdtd.ibict.br/requestopendoar:null2020-05-28 19:34:33.815Biblioteca Digital de Teses e Dissertações do ITA - Instituto Tecnológico de Aeronáuticatrue
dc.title.none.fl_str_mv Simplified engine/nacelle heat transfer case analysis via CFD modeling for supporting the preliminary design of nacelle cooling/ventilation system.
title Simplified engine/nacelle heat transfer case analysis via CFD modeling for supporting the preliminary design of nacelle cooling/ventilation system.
spellingShingle Simplified engine/nacelle heat transfer case analysis via CFD modeling for supporting the preliminary design of nacelle cooling/ventilation system.
Ricardo Pereira das Neves
Transferência de calor
Dinâmica dos fluidos computacional
Sistemas de refrigeração
Ventilação
Nacelas
Motores de aeronaves
Termodinâmica
Física
title_short Simplified engine/nacelle heat transfer case analysis via CFD modeling for supporting the preliminary design of nacelle cooling/ventilation system.
title_full Simplified engine/nacelle heat transfer case analysis via CFD modeling for supporting the preliminary design of nacelle cooling/ventilation system.
title_fullStr Simplified engine/nacelle heat transfer case analysis via CFD modeling for supporting the preliminary design of nacelle cooling/ventilation system.
title_full_unstemmed Simplified engine/nacelle heat transfer case analysis via CFD modeling for supporting the preliminary design of nacelle cooling/ventilation system.
title_sort Simplified engine/nacelle heat transfer case analysis via CFD modeling for supporting the preliminary design of nacelle cooling/ventilation system.
author Ricardo Pereira das Neves
author_facet Ricardo Pereira das Neves
author_role author
dc.contributor.none.fl_str_mv Cláudia Regina de Andrade
dc.contributor.author.fl_str_mv Ricardo Pereira das Neves
dc.subject.por.fl_str_mv Transferência de calor
Dinâmica dos fluidos computacional
Sistemas de refrigeração
Ventilação
Nacelas
Motores de aeronaves
Termodinâmica
Física
topic Transferência de calor
Dinâmica dos fluidos computacional
Sistemas de refrigeração
Ventilação
Nacelas
Motores de aeronaves
Termodinâmica
Física
dc.description.none.fl_txt_mv An aeronautical engine is a complex machine composed of different components operating at different temperatures that in conjunction with the nacelle creates a crowded region with the coupled heat transfer mechanisms to be covered by the nacelle cooling/ventilation system. The final configuration of this system is defined through a demanding refinement of the preliminary design. For this reason the preliminary design is considered the key point and as a rule it can be based on the use of similar design scaling or by the use of numerical approaches. The numerical approaches available are the use of a one-dimensional heat transfer analysis or a complete heat transfer analysis via Computational Fluid Dynamics, or CFD. The short lead time usually available to get the nacelle ready leads the using of a more simplified analysis. Even though this simplified analysis is a lesser laborious activity than a more complete heat transfer analysis, it is still a relatively complicated task. Thus this work aims at presenting a simple methodology for supporting the preliminary design of nacelle cooling/ventilation which is basically relies on confirming if such system is really necessary taking into consideration the temperature distribution in the region between the engine/nacelle and the specified limits. In this case, the proposed methodology presented in this work is concerning to the natural convection analysis in a bidimensional engine/nacelle model by the use of CFD. In view of the fact that there is no specific literature reference available about such methodology or the natural convection analysis in an analogous model configuration or even experimental tests results, it was decided to utilize the studies about natural convection in concentric cylinders in the model validation process and to show the suitability of the proposed methodology, it was directly compared to the natural convection analysis in a simplified tridimensional engine/nacelle model by the use of CFD tool which would be performed by the manufacturer.
description An aeronautical engine is a complex machine composed of different components operating at different temperatures that in conjunction with the nacelle creates a crowded region with the coupled heat transfer mechanisms to be covered by the nacelle cooling/ventilation system. The final configuration of this system is defined through a demanding refinement of the preliminary design. For this reason the preliminary design is considered the key point and as a rule it can be based on the use of similar design scaling or by the use of numerical approaches. The numerical approaches available are the use of a one-dimensional heat transfer analysis or a complete heat transfer analysis via Computational Fluid Dynamics, or CFD. The short lead time usually available to get the nacelle ready leads the using of a more simplified analysis. Even though this simplified analysis is a lesser laborious activity than a more complete heat transfer analysis, it is still a relatively complicated task. Thus this work aims at presenting a simple methodology for supporting the preliminary design of nacelle cooling/ventilation which is basically relies on confirming if such system is really necessary taking into consideration the temperature distribution in the region between the engine/nacelle and the specified limits. In this case, the proposed methodology presented in this work is concerning to the natural convection analysis in a bidimensional engine/nacelle model by the use of CFD. In view of the fact that there is no specific literature reference available about such methodology or the natural convection analysis in an analogous model configuration or even experimental tests results, it was decided to utilize the studies about natural convection in concentric cylinders in the model validation process and to show the suitability of the proposed methodology, it was directly compared to the natural convection analysis in a simplified tridimensional engine/nacelle model by the use of CFD tool which would be performed by the manufacturer.
publishDate 2009
dc.date.none.fl_str_mv 2009-11-06
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=861
url http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=861
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 Transferência de calor
Dinâmica dos fluidos computacional
Sistemas de refrigeração
Ventilação
Nacelas
Motores de aeronaves
Termodinâmica
Física
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