Fatigue damage mechanism and failure prevention in fiberglass reinforced plastic
Damaging of composite laminates was monitored during fatigue tests, revealing the formation and propagation stages for compressive, tensile, or alternate cyclic loading. Two different laminate stacking sequences, with different number of layers, were tested. The laminates consisted of E-glass fibers...
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Associação Brasileira de Metalurgia e Materiais (ABM); Associação Brasileira de Cerâmica (ABC); Associação Brasileira de Polímeros (ABPol)
2005-03-01
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Online Access: | http://www.scielo.br/scielo.php?script=sci_arttext&pid=S1516-14392005000100009 |
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doaj-423bfef037dd44c4aac70d254630a2eb2020-11-24T23:27:29ZengAssociação Brasileira de Metalurgia e Materiais (ABM); Associação Brasileira de Cerâmica (ABC); Associação Brasileira de Polímeros (ABPol)Materials Research1516-14392005-03-0181454910.1590/S1516-14392005000100009Fatigue damage mechanism and failure prevention in fiberglass reinforced plasticRaimundo Carlos Silverio Freire Jr.Eve Maria Freire de AquinoDamaging of composite laminates was monitored during fatigue tests, revealing the formation and propagation stages for compressive, tensile, or alternate cyclic loading. Two different laminate stacking sequences, with different number of layers, were tested. The laminates consisted of E-glass fibers reinforced orthoftalic polyester resin (FGRP) shaped as mats or (bi-direction) woven fabric textile. Preliminary density, calcination tests and static compressive and tensile mechanical tests were carried out. Then, tensile (R = 0.1), compressive (R = 10) and alternate axial (R = - 1) fatigue tests were performed at different maximum stresses. Tensile cyclic loading resulted in crack formation and propagation confirming the findings reported in other studies. On the other hand, damage from alternate and compressive fatigue depicted peculiar features. Less extended damage and better fatigue resistance were observed for the laminate with symmetrically distributed layers.http://www.scielo.br/scielo.php?script=sci_arttext&pid=S1516-14392005000100009fatiguelaminatesFRP compositesdamage formation and propagation diagrams |
collection |
DOAJ |
language |
English |
format |
Article |
sources |
DOAJ |
author |
Raimundo Carlos Silverio Freire Jr. Eve Maria Freire de Aquino |
spellingShingle |
Raimundo Carlos Silverio Freire Jr. Eve Maria Freire de Aquino Fatigue damage mechanism and failure prevention in fiberglass reinforced plastic Materials Research fatigue laminates FRP composites damage formation and propagation diagrams |
author_facet |
Raimundo Carlos Silverio Freire Jr. Eve Maria Freire de Aquino |
author_sort |
Raimundo Carlos Silverio Freire Jr. |
title |
Fatigue damage mechanism and failure prevention in fiberglass reinforced plastic |
title_short |
Fatigue damage mechanism and failure prevention in fiberglass reinforced plastic |
title_full |
Fatigue damage mechanism and failure prevention in fiberglass reinforced plastic |
title_fullStr |
Fatigue damage mechanism and failure prevention in fiberglass reinforced plastic |
title_full_unstemmed |
Fatigue damage mechanism and failure prevention in fiberglass reinforced plastic |
title_sort |
fatigue damage mechanism and failure prevention in fiberglass reinforced plastic |
publisher |
Associação Brasileira de Metalurgia e Materiais (ABM); Associação Brasileira de Cerâmica (ABC); Associação Brasileira de Polímeros (ABPol) |
series |
Materials Research |
issn |
1516-1439 |
publishDate |
2005-03-01 |
description |
Damaging of composite laminates was monitored during fatigue tests, revealing the formation and propagation stages for compressive, tensile, or alternate cyclic loading. Two different laminate stacking sequences, with different number of layers, were tested. The laminates consisted of E-glass fibers reinforced orthoftalic polyester resin (FGRP) shaped as mats or (bi-direction) woven fabric textile. Preliminary density, calcination tests and static compressive and tensile mechanical tests were carried out. Then, tensile (R = 0.1), compressive (R = 10) and alternate axial (R = - 1) fatigue tests were performed at different maximum stresses. Tensile cyclic loading resulted in crack formation and propagation confirming the findings reported in other studies. On the other hand, damage from alternate and compressive fatigue depicted peculiar features. Less extended damage and better fatigue resistance were observed for the laminate with symmetrically distributed layers. |
topic |
fatigue laminates FRP composites damage formation and propagation diagrams |
url |
http://www.scielo.br/scielo.php?script=sci_arttext&pid=S1516-14392005000100009 |
work_keys_str_mv |
AT raimundocarlossilveriofreirejr fatiguedamagemechanismandfailurepreventioninfiberglassreinforcedplastic AT evemariafreiredeaquino fatiguedamagemechanismandfailurepreventioninfiberglassreinforcedplastic |
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