Reynolds number effect on the heat transfer mechanisms in aircraft hot air anti-ice system.

Detalhes bibliográficos
Autor(a) principal: Jean Fernando Bertão Machado
Data de Publicação: 2008
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=1158
Resumo: The primary means of preventing ice formation on wings and engine inlets for modern commercial transport aircraft is by extracting hot air from the compressor and blowing it on the inside surface of the leading edge through small holes drilled in the so-called piccolo tube system. A critical aspect in the design of such system is the prediction of heat transfer of the impinging jets from the piccolo tube. The correct evaluation of the heat transfer rate in such devices is of great interest to optimize both the anti-icing performance and the hot air bleeding from the high-pressure compressor. The history of research in the anti-icing area is rather narrow. A review of the literature reveals that only few experimental and theoretical/numerical studies have been carried out to study the heat transfer and flow in the internal hot-air region. There are some experimental and numerical studies that developed correlations for the average Nusselt number. However, most of the research was performed using a single jet or a group of jets impinging on a flat slat, which is different from the jet impingement on concave surfaces, as the inside surface of a wing. Therefore, the objective of the present work is use the commercial CFD software FLUENT to perform a parametric study of the jet impingement on concave surfaces. The main goal is determine the effect of the Reynolds number on the heat transfer process. At the end of the work, a correlation for the average Nusselt number which account for the Reynolds number is presented.
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spelling Reynolds number effect on the heat transfer mechanisms in aircraft hot air anti-ice system.Sistema anti-geloTransferência de calorJatos incidentesNúmero de ReynoldsTermodinâmicaDinâmica dos fluidos computacionalSegurança de aeronavesFormação de geloEngenharia aeronáuticaThe primary means of preventing ice formation on wings and engine inlets for modern commercial transport aircraft is by extracting hot air from the compressor and blowing it on the inside surface of the leading edge through small holes drilled in the so-called piccolo tube system. A critical aspect in the design of such system is the prediction of heat transfer of the impinging jets from the piccolo tube. The correct evaluation of the heat transfer rate in such devices is of great interest to optimize both the anti-icing performance and the hot air bleeding from the high-pressure compressor. The history of research in the anti-icing area is rather narrow. A review of the literature reveals that only few experimental and theoretical/numerical studies have been carried out to study the heat transfer and flow in the internal hot-air region. There are some experimental and numerical studies that developed correlations for the average Nusselt number. However, most of the research was performed using a single jet or a group of jets impinging on a flat slat, which is different from the jet impingement on concave surfaces, as the inside surface of a wing. Therefore, the objective of the present work is use the commercial CFD software FLUENT to perform a parametric study of the jet impingement on concave surfaces. The main goal is determine the effect of the Reynolds number on the heat transfer process. At the end of the work, a correlation for the average Nusselt number which account for the Reynolds number is presented.Instituto Tecnológico de AeronáuticaCláudia Regina de AndradeJean Fernando Bertão Machado2008-03-25info:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/masterThesishttp://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=1158reponame:Biblioteca Digital de Teses e Dissertações do ITAinstname:Instituto Tecnológico de Aeronáuticainstacron:ITAenginfo:eu-repo/semantics/openAccessapplication/pdf2019-02-02T14:02:34Zoai:agregador.ibict.br.BDTD_ITA:oai:ita.br:1158http://oai.bdtd.ibict.br/requestopendoar:null2020-05-28 19:35:32.146Biblioteca Digital de Teses e Dissertações do ITA - Instituto Tecnológico de Aeronáuticatrue
dc.title.none.fl_str_mv Reynolds number effect on the heat transfer mechanisms in aircraft hot air anti-ice system.
title Reynolds number effect on the heat transfer mechanisms in aircraft hot air anti-ice system.
spellingShingle Reynolds number effect on the heat transfer mechanisms in aircraft hot air anti-ice system.
Jean Fernando Bertão Machado
Sistema anti-gelo
Transferência de calor
Jatos incidentes
Número de Reynolds
Termodinâmica
Dinâmica dos fluidos computacional
Segurança de aeronaves
Formação de gelo
Engenharia aeronáutica
title_short Reynolds number effect on the heat transfer mechanisms in aircraft hot air anti-ice system.
title_full Reynolds number effect on the heat transfer mechanisms in aircraft hot air anti-ice system.
title_fullStr Reynolds number effect on the heat transfer mechanisms in aircraft hot air anti-ice system.
title_full_unstemmed Reynolds number effect on the heat transfer mechanisms in aircraft hot air anti-ice system.
title_sort Reynolds number effect on the heat transfer mechanisms in aircraft hot air anti-ice system.
author Jean Fernando Bertão Machado
author_facet Jean Fernando Bertão Machado
author_role author
dc.contributor.none.fl_str_mv Cláudia Regina de Andrade
dc.contributor.author.fl_str_mv Jean Fernando Bertão Machado
dc.subject.por.fl_str_mv Sistema anti-gelo
Transferência de calor
Jatos incidentes
Número de Reynolds
Termodinâmica
Dinâmica dos fluidos computacional
Segurança de aeronaves
Formação de gelo
Engenharia aeronáutica
topic Sistema anti-gelo
Transferência de calor
Jatos incidentes
Número de Reynolds
Termodinâmica
Dinâmica dos fluidos computacional
Segurança de aeronaves
Formação de gelo
Engenharia aeronáutica
dc.description.none.fl_txt_mv The primary means of preventing ice formation on wings and engine inlets for modern commercial transport aircraft is by extracting hot air from the compressor and blowing it on the inside surface of the leading edge through small holes drilled in the so-called piccolo tube system. A critical aspect in the design of such system is the prediction of heat transfer of the impinging jets from the piccolo tube. The correct evaluation of the heat transfer rate in such devices is of great interest to optimize both the anti-icing performance and the hot air bleeding from the high-pressure compressor. The history of research in the anti-icing area is rather narrow. A review of the literature reveals that only few experimental and theoretical/numerical studies have been carried out to study the heat transfer and flow in the internal hot-air region. There are some experimental and numerical studies that developed correlations for the average Nusselt number. However, most of the research was performed using a single jet or a group of jets impinging on a flat slat, which is different from the jet impingement on concave surfaces, as the inside surface of a wing. Therefore, the objective of the present work is use the commercial CFD software FLUENT to perform a parametric study of the jet impingement on concave surfaces. The main goal is determine the effect of the Reynolds number on the heat transfer process. At the end of the work, a correlation for the average Nusselt number which account for the Reynolds number is presented.
description The primary means of preventing ice formation on wings and engine inlets for modern commercial transport aircraft is by extracting hot air from the compressor and blowing it on the inside surface of the leading edge through small holes drilled in the so-called piccolo tube system. A critical aspect in the design of such system is the prediction of heat transfer of the impinging jets from the piccolo tube. The correct evaluation of the heat transfer rate in such devices is of great interest to optimize both the anti-icing performance and the hot air bleeding from the high-pressure compressor. The history of research in the anti-icing area is rather narrow. A review of the literature reveals that only few experimental and theoretical/numerical studies have been carried out to study the heat transfer and flow in the internal hot-air region. There are some experimental and numerical studies that developed correlations for the average Nusselt number. However, most of the research was performed using a single jet or a group of jets impinging on a flat slat, which is different from the jet impingement on concave surfaces, as the inside surface of a wing. Therefore, the objective of the present work is use the commercial CFD software FLUENT to perform a parametric study of the jet impingement on concave surfaces. The main goal is determine the effect of the Reynolds number on the heat transfer process. At the end of the work, a correlation for the average Nusselt number which account for the Reynolds number is presented.
publishDate 2008
dc.date.none.fl_str_mv 2008-03-25
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=1158
url http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=1158
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 Sistema anti-gelo
Transferência de calor
Jatos incidentes
Número de Reynolds
Termodinâmica
Dinâmica dos fluidos computacional
Segurança de aeronaves
Formação de gelo
Engenharia aeronáutica
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