The influences of bypass ratio variation on runway performance of jet airplanes.

Detalhes bibliográficos
Autor(a) principal: Rodrigo Figueira Mourão
Data de Publicação: 2004
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=612
Resumo: The influences of bypass ratio variation of turbofan engines in airplane runway performance are investigated more deeply in this work utilising a take-off analysis software developed by Ishizuka (2003). An initial study was carried out by Mourão, Negrão and Barbosa (2003). The results are analysed and discussed according to the operational feasibility of operators and technical feasibility of engine manufacturers. The analysis is based on comparisons of gains/losses in take-off distance, accelerate-stop distance and take-off weight for a range of bypass ratio values. Also, suggestions for future studies and researches are given his document is intended also to provide satisfactory background information of the take-off process and its mandatory regulations (FAR Part25, 1998) as much for commercial airplanes as for military airplanes. The aim is to contribute to readers' knowledge interested instudying more deeply the particularities of this specific flight phase and improving its operational safety.
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spelling The influences of bypass ratio variation on runway performance of jet airplanes.Motores TurbofanPistas (de pouso e decolagem)Razão de diluiçãoCorrida de decolagemDesempenho de aeronavesTurbinas a gásEngenharia aeronáuticaEngenharia mecânicaThe influences of bypass ratio variation of turbofan engines in airplane runway performance are investigated more deeply in this work utilising a take-off analysis software developed by Ishizuka (2003). An initial study was carried out by Mourão, Negrão and Barbosa (2003). The results are analysed and discussed according to the operational feasibility of operators and technical feasibility of engine manufacturers. The analysis is based on comparisons of gains/losses in take-off distance, accelerate-stop distance and take-off weight for a range of bypass ratio values. Also, suggestions for future studies and researches are given his document is intended also to provide satisfactory background information of the take-off process and its mandatory regulations (FAR Part25, 1998) as much for commercial airplanes as for military airplanes. The aim is to contribute to readers' knowledge interested instudying more deeply the particularities of this specific flight phase and improving its operational safety.Instituto Tecnológico de AeronáuticaJoão Roberto BarbosaJosé Ricardo Parizi NegrãoRodrigo Figueira Mourão2004-04-15info:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/masterThesishttp://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=612reponame:Biblioteca Digital de Teses e Dissertações do ITAinstname:Instituto Tecnológico de Aeronáuticainstacron:ITAenginfo:eu-repo/semantics/openAccessapplication/pdf2019-02-02T14:01:53Zoai:agregador.ibict.br.BDTD_ITA:oai:ita.br:612http://oai.bdtd.ibict.br/requestopendoar:null2020-05-28 19:33:42.792Biblioteca Digital de Teses e Dissertações do ITA - Instituto Tecnológico de Aeronáuticatrue
dc.title.none.fl_str_mv The influences of bypass ratio variation on runway performance of jet airplanes.
title The influences of bypass ratio variation on runway performance of jet airplanes.
spellingShingle The influences of bypass ratio variation on runway performance of jet airplanes.
Rodrigo Figueira Mourão
Motores Turbofan
Pistas (de pouso e decolagem)
Razão de diluição
Corrida de decolagem
Desempenho de aeronaves
Turbinas a gás
Engenharia aeronáutica
Engenharia mecânica
title_short The influences of bypass ratio variation on runway performance of jet airplanes.
title_full The influences of bypass ratio variation on runway performance of jet airplanes.
title_fullStr The influences of bypass ratio variation on runway performance of jet airplanes.
title_full_unstemmed The influences of bypass ratio variation on runway performance of jet airplanes.
title_sort The influences of bypass ratio variation on runway performance of jet airplanes.
author Rodrigo Figueira Mourão
author_facet Rodrigo Figueira Mourão
author_role author
dc.contributor.none.fl_str_mv João Roberto Barbosa
José Ricardo Parizi Negrão
dc.contributor.author.fl_str_mv Rodrigo Figueira Mourão
dc.subject.por.fl_str_mv Motores Turbofan
Pistas (de pouso e decolagem)
Razão de diluição
Corrida de decolagem
Desempenho de aeronaves
Turbinas a gás
Engenharia aeronáutica
Engenharia mecânica
topic Motores Turbofan
Pistas (de pouso e decolagem)
Razão de diluição
Corrida de decolagem
Desempenho de aeronaves
Turbinas a gás
Engenharia aeronáutica
Engenharia mecânica
dc.description.none.fl_txt_mv The influences of bypass ratio variation of turbofan engines in airplane runway performance are investigated more deeply in this work utilising a take-off analysis software developed by Ishizuka (2003). An initial study was carried out by Mourão, Negrão and Barbosa (2003). The results are analysed and discussed according to the operational feasibility of operators and technical feasibility of engine manufacturers. The analysis is based on comparisons of gains/losses in take-off distance, accelerate-stop distance and take-off weight for a range of bypass ratio values. Also, suggestions for future studies and researches are given his document is intended also to provide satisfactory background information of the take-off process and its mandatory regulations (FAR Part25, 1998) as much for commercial airplanes as for military airplanes. The aim is to contribute to readers' knowledge interested instudying more deeply the particularities of this specific flight phase and improving its operational safety.
description The influences of bypass ratio variation of turbofan engines in airplane runway performance are investigated more deeply in this work utilising a take-off analysis software developed by Ishizuka (2003). An initial study was carried out by Mourão, Negrão and Barbosa (2003). The results are analysed and discussed according to the operational feasibility of operators and technical feasibility of engine manufacturers. The analysis is based on comparisons of gains/losses in take-off distance, accelerate-stop distance and take-off weight for a range of bypass ratio values. Also, suggestions for future studies and researches are given his document is intended also to provide satisfactory background information of the take-off process and its mandatory regulations (FAR Part25, 1998) as much for commercial airplanes as for military airplanes. The aim is to contribute to readers' knowledge interested instudying more deeply the particularities of this specific flight phase and improving its operational safety.
publishDate 2004
dc.date.none.fl_str_mv 2004-04-15
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=612
url http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=612
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 Motores Turbofan
Pistas (de pouso e decolagem)
Razão de diluição
Corrida de decolagem
Desempenho de aeronaves
Turbinas a gás
Engenharia aeronáutica
Engenharia mecânica
_version_ 1706809260834291712

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