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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Main Authors: Raimundo Carlos Silverio Freire Jr., Eve Maria Freire de Aquino
Format: Article
Language:English
Published: Associação Brasileira de Metalurgia e Materiais (ABM); Associação Brasileira de Cerâmica (ABC); Associação Brasileira de Polímeros (ABPol) 2005-03-01
Series:Materials Research
Subjects:
Online Access:http://www.scielo.br/scielo.php?script=sci_arttext&pid=S1516-14392005000100009
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spelling 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
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