Determination of CTOD C in Fibre Metal Laminates by ASTM and Schwalbe Methods
Autor(a) principal: | |
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Data de Publicação: | 2002 |
Outros Autores: | , , |
Tipo de documento: | Artigo |
Idioma: | eng |
Título da fonte: | Materials research (São Carlos. Online) |
Texto Completo: | http://old.scielo.br/scielo.php?script=sci_arttext&pid=S1516-14392002000200006 |
Resumo: | Fibre Metal Laminates (FMLs) have arisen as a demand of the aeronautical industry to use thin sheets with high resistance to fatigue crack growth, high damage tolerance, corrosion resistance and high specific strength. Considering these requirements, FMLs are an advantageous choice when compared to metal alloys currently used. In order to employ FMLs in aircraft structures, designers must hold a deep knowledge of a wide set of their properties including fracture toughness. The aim of this work was to evaluate the available methodologies to measure fracture toughness at instability (CTOD C) in unidirectional fibre metal laminates reinforced with aramid fibres (ARALL®). To achieve this, tests were performed to obtain traditional and Schwalbe CTODs by using experimental ASTM based techniques, especially adapted to these laminates. Results achieved point out that Schwalbe method is more appropriate and also that there are differences between both CTOD parameters. |
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Determination of CTOD C in Fibre Metal Laminates by ASTM and Schwalbe Methodsfibre metal laminatescrack tip opening displacementcompositesFibre Metal Laminates (FMLs) have arisen as a demand of the aeronautical industry to use thin sheets with high resistance to fatigue crack growth, high damage tolerance, corrosion resistance and high specific strength. Considering these requirements, FMLs are an advantageous choice when compared to metal alloys currently used. In order to employ FMLs in aircraft structures, designers must hold a deep knowledge of a wide set of their properties including fracture toughness. The aim of this work was to evaluate the available methodologies to measure fracture toughness at instability (CTOD C) in unidirectional fibre metal laminates reinforced with aramid fibres (ARALL®). To achieve this, tests were performed to obtain traditional and Schwalbe CTODs by using experimental ASTM based techniques, especially adapted to these laminates. Results achieved point out that Schwalbe method is more appropriate and also that there are differences between both CTOD parameters.ABM, ABC, ABPol2002-06-01info:eu-repo/semantics/articleinfo:eu-repo/semantics/publishedVersiontext/htmlhttp://old.scielo.br/scielo.php?script=sci_arttext&pid=S1516-14392002000200006Materials Research v.5 n.2 2002reponame:Materials research (São Carlos. Online)instname:Universidade Federal de São Carlos (UFSCAR)instacron:ABM ABC ABPOL10.1590/S1516-14392002000200006info:eu-repo/semantics/openAccessCastrodeza,E.M.Rodrigues Touça,J.M.Perez Ipiña,J.E.Bastian,F.L.eng2002-09-05T00:00:00Zoai:scielo:S1516-14392002000200006Revistahttp://www.scielo.br/mrPUBhttps://old.scielo.br/oai/scielo-oai.phpdedz@power.ufscar.br1980-53731516-1439opendoar:2002-09-05T00:00Materials research (São Carlos. Online) - Universidade Federal de São Carlos (UFSCAR)false |
dc.title.none.fl_str_mv |
Determination of CTOD C in Fibre Metal Laminates by ASTM and Schwalbe Methods |
title |
Determination of CTOD C in Fibre Metal Laminates by ASTM and Schwalbe Methods |
spellingShingle |
Determination of CTOD C in Fibre Metal Laminates by ASTM and Schwalbe Methods Castrodeza,E.M. fibre metal laminates crack tip opening displacement composites |
title_short |
Determination of CTOD C in Fibre Metal Laminates by ASTM and Schwalbe Methods |
title_full |
Determination of CTOD C in Fibre Metal Laminates by ASTM and Schwalbe Methods |
title_fullStr |
Determination of CTOD C in Fibre Metal Laminates by ASTM and Schwalbe Methods |
title_full_unstemmed |
Determination of CTOD C in Fibre Metal Laminates by ASTM and Schwalbe Methods |
title_sort |
Determination of CTOD C in Fibre Metal Laminates by ASTM and Schwalbe Methods |
author |
Castrodeza,E.M. |
author_facet |
Castrodeza,E.M. Rodrigues Touça,J.M. Perez Ipiña,J.E. Bastian,F.L. |
author_role |
author |
author2 |
Rodrigues Touça,J.M. Perez Ipiña,J.E. Bastian,F.L. |
author2_role |
author author author |
dc.contributor.author.fl_str_mv |
Castrodeza,E.M. Rodrigues Touça,J.M. Perez Ipiña,J.E. Bastian,F.L. |
dc.subject.por.fl_str_mv |
fibre metal laminates crack tip opening displacement composites |
topic |
fibre metal laminates crack tip opening displacement composites |
description |
Fibre Metal Laminates (FMLs) have arisen as a demand of the aeronautical industry to use thin sheets with high resistance to fatigue crack growth, high damage tolerance, corrosion resistance and high specific strength. Considering these requirements, FMLs are an advantageous choice when compared to metal alloys currently used. In order to employ FMLs in aircraft structures, designers must hold a deep knowledge of a wide set of their properties including fracture toughness. The aim of this work was to evaluate the available methodologies to measure fracture toughness at instability (CTOD C) in unidirectional fibre metal laminates reinforced with aramid fibres (ARALL®). To achieve this, tests were performed to obtain traditional and Schwalbe CTODs by using experimental ASTM based techniques, especially adapted to these laminates. Results achieved point out that Schwalbe method is more appropriate and also that there are differences between both CTOD parameters. |
publishDate |
2002 |
dc.date.none.fl_str_mv |
2002-06-01 |
dc.type.driver.fl_str_mv |
info:eu-repo/semantics/article |
dc.type.status.fl_str_mv |
info:eu-repo/semantics/publishedVersion |
format |
article |
status_str |
publishedVersion |
dc.identifier.uri.fl_str_mv |
http://old.scielo.br/scielo.php?script=sci_arttext&pid=S1516-14392002000200006 |
url |
http://old.scielo.br/scielo.php?script=sci_arttext&pid=S1516-14392002000200006 |
dc.language.iso.fl_str_mv |
eng |
language |
eng |
dc.relation.none.fl_str_mv |
10.1590/S1516-14392002000200006 |
dc.rights.driver.fl_str_mv |
info:eu-repo/semantics/openAccess |
eu_rights_str_mv |
openAccess |
dc.format.none.fl_str_mv |
text/html |
dc.publisher.none.fl_str_mv |
ABM, ABC, ABPol |
publisher.none.fl_str_mv |
ABM, ABC, ABPol |
dc.source.none.fl_str_mv |
Materials Research v.5 n.2 2002 reponame:Materials research (São Carlos. Online) instname:Universidade Federal de São Carlos (UFSCAR) instacron:ABM ABC ABPOL |
instname_str |
Universidade Federal de São Carlos (UFSCAR) |
instacron_str |
ABM ABC ABPOL |
institution |
ABM ABC ABPOL |
reponame_str |
Materials research (São Carlos. Online) |
collection |
Materials research (São Carlos. Online) |
repository.name.fl_str_mv |
Materials research (São Carlos. Online) - Universidade Federal de São Carlos (UFSCAR) |
repository.mail.fl_str_mv |
dedz@power.ufscar.br |
_version_ |
1754212656950018048 |