Fatigue crack growth resistance and crack closure behavior in two aluminum alloys for aeronautical applications.

Detalhes bibliográficos
Autor(a) principal: Rodrigues, Elenice Maria
Data de Publicação: 2005
Outros Autores: Matias, Adalberto, Godefroid, Leonardo Barbosa, Bastian, Fernando Luiz, Al-Rubaie, Kassim Shamil Fadhil
Tipo de documento: Artigo
Idioma: eng
Título da fonte: Repositório Institucional da UFOP
Texto Completo: http://www.repositorio.ufop.br/handle/123456789/5389
http://dx.doi.org/10.1590/S1516-14392005000300011
Resumo: Aluminum-lithium alloys are candidate materials for many aerospace applications because of their high specific strength and elastic modulus. These alloys have several unique characteristics such as excellent fatigue crack growth resistance when compared with that of the conventional 2000 and 7000 series alloys. In this study, fatigue crack propagation behavior has been examined in a commercial thin plate of Al-Li-Cu-Mg alloy (8090), with specific emphasis at the fatigue threshold. The results are compared with those of the traditional Al-Cu-Mg alloy (2024). Fatigue crack closure is used to explain the different behavior of the compared alloys.
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spelling Rodrigues, Elenice MariaMatias, AdalbertoGodefroid, Leonardo BarbosaBastian, Fernando LuizAl-Rubaie, Kassim Shamil Fadhil2015-05-19T17:29:26Z2015-05-19T17:29:26Z2005RODRIGUES, E. M. et al. Fatigue crack growth resistance and crack closure behavior in two aluminum alloys for aeronautical applications. Materials Research, São Paulo, v. 8, n. 3, p. 287-291, 2005. Disponível em: <http://www.scielo.br/scielo.php?script=sci_arttext&pid=S1516-14392005000300011>. Acesso em: 09 abr. 2015.1516-1439http://www.repositorio.ufop.br/handle/123456789/5389http://dx.doi.org/10.1590/S1516-14392005000300011Aluminum-lithium alloys are candidate materials for many aerospace applications because of their high specific strength and elastic modulus. These alloys have several unique characteristics such as excellent fatigue crack growth resistance when compared with that of the conventional 2000 and 7000 series alloys. In this study, fatigue crack propagation behavior has been examined in a commercial thin plate of Al-Li-Cu-Mg alloy (8090), with specific emphasis at the fatigue threshold. The results are compared with those of the traditional Al-Cu-Mg alloy (2024). Fatigue crack closure is used to explain the different behavior of the compared alloys.FatigueCrack closureAluminum alloysAeronautical applicationsFatigue crack growth resistance and crack closure behavior in two aluminum alloys for aeronautical applications.info:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/articleAutorização concedida ao Repositório Institucional da UFOP pela Materials Research em 25/10/2013 com as seguintes condições: disponível sob Licença Creative Commons que permite copiar, distribuir e transmitir o trabalho desde que sejam citados o autor e o licenciante. Não permite o uso para fins comerciais nem a adaptação.info:eu-repo/semantics/openAccessengreponame:Repositório Institucional da UFOPinstname:Universidade Federal de Ouro Preto (UFOP)instacron:UFOPLICENSElicense.txtlicense.txttext/plain; charset=utf-82636http://www.repositorio.ufop.br/bitstream/123456789/5389/2/license.txtc2ffdd99e58acf69202dff00d361f23aMD52ORIGINALARTIGO_FatigueCrackResistance.pdfARTIGO_FatigueCrackResistance.pdfapplication/pdf1166386http://www.repositorio.ufop.br/bitstream/123456789/5389/1/ARTIGO_FatigueCrackResistance.pdf314d17996e06efa77da2d4cbe16a5465MD51123456789/53892019-07-23 10:59:23.671oai:localhost: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Repositório InstitucionalPUBhttp://www.repositorio.ufop.br/oai/requestrepositorio@ufop.edu.bropendoar:32332019-07-23T14:59:23Repositório Institucional da UFOP - Universidade Federal de Ouro Preto (UFOP)false
dc.title.pt_BR.fl_str_mv Fatigue crack growth resistance and crack closure behavior in two aluminum alloys for aeronautical applications.
title Fatigue crack growth resistance and crack closure behavior in two aluminum alloys for aeronautical applications.
spellingShingle Fatigue crack growth resistance and crack closure behavior in two aluminum alloys for aeronautical applications.
Rodrigues, Elenice Maria
Fatigue
Crack closure
Aluminum alloys
Aeronautical applications
title_short Fatigue crack growth resistance and crack closure behavior in two aluminum alloys for aeronautical applications.
title_full Fatigue crack growth resistance and crack closure behavior in two aluminum alloys for aeronautical applications.
title_fullStr Fatigue crack growth resistance and crack closure behavior in two aluminum alloys for aeronautical applications.
title_full_unstemmed Fatigue crack growth resistance and crack closure behavior in two aluminum alloys for aeronautical applications.
title_sort Fatigue crack growth resistance and crack closure behavior in two aluminum alloys for aeronautical applications.
author Rodrigues, Elenice Maria
author_facet Rodrigues, Elenice Maria
Matias, Adalberto
Godefroid, Leonardo Barbosa
Bastian, Fernando Luiz
Al-Rubaie, Kassim Shamil Fadhil
author_role author
author2 Matias, Adalberto
Godefroid, Leonardo Barbosa
Bastian, Fernando Luiz
Al-Rubaie, Kassim Shamil Fadhil
author2_role author
author
author
author
dc.contributor.author.fl_str_mv Rodrigues, Elenice Maria
Matias, Adalberto
Godefroid, Leonardo Barbosa
Bastian, Fernando Luiz
Al-Rubaie, Kassim Shamil Fadhil
dc.subject.por.fl_str_mv Fatigue
Crack closure
Aluminum alloys
Aeronautical applications
topic Fatigue
Crack closure
Aluminum alloys
Aeronautical applications
description Aluminum-lithium alloys are candidate materials for many aerospace applications because of their high specific strength and elastic modulus. These alloys have several unique characteristics such as excellent fatigue crack growth resistance when compared with that of the conventional 2000 and 7000 series alloys. In this study, fatigue crack propagation behavior has been examined in a commercial thin plate of Al-Li-Cu-Mg alloy (8090), with specific emphasis at the fatigue threshold. The results are compared with those of the traditional Al-Cu-Mg alloy (2024). Fatigue crack closure is used to explain the different behavior of the compared alloys.
publishDate 2005
dc.date.issued.fl_str_mv 2005
dc.date.accessioned.fl_str_mv 2015-05-19T17:29:26Z
dc.date.available.fl_str_mv 2015-05-19T17:29:26Z
dc.type.status.fl_str_mv info:eu-repo/semantics/publishedVersion
dc.type.driver.fl_str_mv info:eu-repo/semantics/article
format article
status_str publishedVersion
dc.identifier.citation.fl_str_mv RODRIGUES, E. M. et al. Fatigue crack growth resistance and crack closure behavior in two aluminum alloys for aeronautical applications. Materials Research, São Paulo, v. 8, n. 3, p. 287-291, 2005. Disponível em: <http://www.scielo.br/scielo.php?script=sci_arttext&pid=S1516-14392005000300011>. Acesso em: 09 abr. 2015.
dc.identifier.uri.fl_str_mv http://www.repositorio.ufop.br/handle/123456789/5389
dc.identifier.issn.none.fl_str_mv 1516-1439
dc.identifier.doi.none.fl_str_mv http://dx.doi.org/10.1590/S1516-14392005000300011
identifier_str_mv RODRIGUES, E. M. et al. Fatigue crack growth resistance and crack closure behavior in two aluminum alloys for aeronautical applications. Materials Research, São Paulo, v. 8, n. 3, p. 287-291, 2005. Disponível em: <http://www.scielo.br/scielo.php?script=sci_arttext&pid=S1516-14392005000300011>. Acesso em: 09 abr. 2015.
1516-1439
url http://www.repositorio.ufop.br/handle/123456789/5389
http://dx.doi.org/10.1590/S1516-14392005000300011
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