The influences of bypass ratio variation on runway performance of jet airplanes.
Autor(a) principal: | |
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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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Biblioteca Digital de Teses e Dissertações do ITA |
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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 |