Comparison between aluminum and all composite AL5 aircraft fuselage.
Autor(a) principal: | |
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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=1160 |
Resumo: | This work demonstrate the decision that lead the responsible team for the AL5 aircraft to recommend more dedicated study, on using composite materials on the constant section barrel of the fuselage, to the next design team. The recommendation where made after the mass comparison of a composite fuselage and an equivalent aluminum fuselage, both estimated through methodologies described on the books of Bruhn and Niu. |
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Biblioteca Digital de Teses e Dissertações do ITA |
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Comparison between aluminum and all composite AL5 aircraft fuselage.Projeto de aeronavesMateriais compósitosFuselagensEstruturas de aeronavesEngenharia de materiaisEngenharia aeronáuticaThis work demonstrate the decision that lead the responsible team for the AL5 aircraft to recommend more dedicated study, on using composite materials on the constant section barrel of the fuselage, to the next design team. The recommendation where made after the mass comparison of a composite fuselage and an equivalent aluminum fuselage, both estimated through methodologies described on the books of Bruhn and Niu.Instituto Tecnológico de AeronáuticaPaulo RizziRodolfo Delatore Alonso2008-03-25info:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/masterThesishttp://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=1160reponame: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:1160http://oai.bdtd.ibict.br/requestopendoar:null2020-05-28 19:35:33.188Biblioteca Digital de Teses e Dissertações do ITA - Instituto Tecnológico de Aeronáuticatrue |
dc.title.none.fl_str_mv |
Comparison between aluminum and all composite AL5 aircraft fuselage. |
title |
Comparison between aluminum and all composite AL5 aircraft fuselage. |
spellingShingle |
Comparison between aluminum and all composite AL5 aircraft fuselage. Rodolfo Delatore Alonso Projeto de aeronaves Materiais compósitos Fuselagens Estruturas de aeronaves Engenharia de materiais Engenharia aeronáutica |
title_short |
Comparison between aluminum and all composite AL5 aircraft fuselage. |
title_full |
Comparison between aluminum and all composite AL5 aircraft fuselage. |
title_fullStr |
Comparison between aluminum and all composite AL5 aircraft fuselage. |
title_full_unstemmed |
Comparison between aluminum and all composite AL5 aircraft fuselage. |
title_sort |
Comparison between aluminum and all composite AL5 aircraft fuselage. |
author |
Rodolfo Delatore Alonso |
author_facet |
Rodolfo Delatore Alonso |
author_role |
author |
dc.contributor.none.fl_str_mv |
Paulo Rizzi |
dc.contributor.author.fl_str_mv |
Rodolfo Delatore Alonso |
dc.subject.por.fl_str_mv |
Projeto de aeronaves Materiais compósitos Fuselagens Estruturas de aeronaves Engenharia de materiais Engenharia aeronáutica |
topic |
Projeto de aeronaves Materiais compósitos Fuselagens Estruturas de aeronaves Engenharia de materiais Engenharia aeronáutica |
dc.description.none.fl_txt_mv |
This work demonstrate the decision that lead the responsible team for the AL5 aircraft to recommend more dedicated study, on using composite materials on the constant section barrel of the fuselage, to the next design team. The recommendation where made after the mass comparison of a composite fuselage and an equivalent aluminum fuselage, both estimated through methodologies described on the books of Bruhn and Niu. |
description |
This work demonstrate the decision that lead the responsible team for the AL5 aircraft to recommend more dedicated study, on using composite materials on the constant section barrel of the fuselage, to the next design team. The recommendation where made after the mass comparison of a composite fuselage and an equivalent aluminum fuselage, both estimated through methodologies described on the books of Bruhn and Niu. |
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=1160 |
url |
http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=1160 |
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 |
Projeto de aeronaves Materiais compósitos Fuselagens Estruturas de aeronaves Engenharia de materiais Engenharia aeronáutica |
_version_ |
1706809266666471424 |