Fatigue life of unidirectional 90° carbon/epoxy laminates made of conventional and ultra-thin plies varying manufacturing and testing conditions

This is an open access article under the terms of the Creative Commons Attribution License, which permits use, distribution and reproduction in any medium, provided the original work is properly cited

Bibliographic Details
Authors: Sánchez-Carmona, Serafín, Correa Montoto, Elena, Barroso Caro, Alberto, París Carballo, Federico
Format: article
Status:Published version
Publication Date:2023
Country:España
Institution:Universidad de Sevilla (US)
Repository:idUS. Depósito de Investigación de la Universidad de Sevilla
OAI Identifier:oai:idus.us.es:11441/142726
Online Access:https://hdl.handle.net/11441/142726
https://doi.org/doi.org/10.1111/ffe.13966
Access Level:Open access
Keyword:Composites
Fatigue analysis
Fiber/matrix failure
Mechanical testing
Tensile mechanical properties
Ultra-thin prepreg
id ES_0efab00ae04272cbdfd2cf0add01f0dc
oai_identifier_str oai:idus.us.es:11441/142726
network_acronym_str ES
network_name_str España
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spelling Fatigue life of unidirectional 90° carbon/epoxy laminates made of conventional and ultra-thin plies varying manufacturing and testing conditionsSánchez-Carmona, SerafínCorrea Montoto, ElenaBarroso Caro, AlbertoParís Carballo, FedericoCompositesFatigue analysisFiber/matrix failureMechanical testingTensile mechanical propertiesUltra-thin prepregThis is an open access article under the terms of the Creative Commons Attribution License, which permits use, distribution and reproduction in any medium, provided the original work is properly citedUnidirectional 90° laminates (UD-90) have been tested under tension–tension loading (R = 0.1) to comprehend the effect of different conditions on their fatigue life. Four different case studies have been evaluated: the existence of porosity using two different UD-90 laminates cured at different pressures in an autoclave, the importance of the surface finishing when a pressure plate is used, the effect of load frequency, and the relevance of the prepreg thickness comparing 190 and 50 g/m2 prepregs while keeping the total thickness of the laminates constant. All these case studies have been analyzed employing S–N curves as the starting point of the authors' current research for the prediction of the onset of transverse damages in ultra-thin plies in the assessment of different cross-ply laminates under cyclic loading.Universidad de Sevilla VIPPIT-2018-II.2Consejería de Economía y Conocimiento, Junta de Andalucía P18-FR-3360Ministerio de Ciencia, Innovación y Universidades PID2021-126279OB-I00John Wiley & Sons Ltd.Mecánica de Medios Continuos y Teoría de EstructurasTEP131: Elasticidad y Resistencia de MaterialesUniversidad de SevillaConsejería de Economía y Conocimiento, Junta de AndalucíaMinisterio de Ciencia, Innovación y Universidades (MICINN). España2023info:eu-repo/semantics/articleinfo:eu-repo/semantics/publishedVersionapplication/pdfapplication/pdfhttps://hdl.handle.net/11441/142726https://doi.org/doi.org/10.1111/ffe.13966reponame:idUS. Depósito de Investigación de la Universidad de Sevillainstname:Universidad de Sevilla (US)InglésFatigue & Fracture of Engineering Materials & Structures (2023), 46, 1837–1847VIPPIT-2018-II.2P18-FR-3360PID2021-126279OB-I00https://onlinelibrary.wiley.com/doi/full/10.1111/ffe.13966info:eu-repo/semantics/openAccessoai:idus.us.es:11441/1427262026-06-17T12:51:07Z
dc.title.none.fl_str_mv Fatigue life of unidirectional 90° carbon/epoxy laminates made of conventional and ultra-thin plies varying manufacturing and testing conditions
title Fatigue life of unidirectional 90° carbon/epoxy laminates made of conventional and ultra-thin plies varying manufacturing and testing conditions
spellingShingle Fatigue life of unidirectional 90° carbon/epoxy laminates made of conventional and ultra-thin plies varying manufacturing and testing conditions
Sánchez-Carmona, Serafín
Composites
Fatigue analysis
Fiber/matrix failure
Mechanical testing
Tensile mechanical properties
Ultra-thin prepreg
title_short Fatigue life of unidirectional 90° carbon/epoxy laminates made of conventional and ultra-thin plies varying manufacturing and testing conditions
title_full Fatigue life of unidirectional 90° carbon/epoxy laminates made of conventional and ultra-thin plies varying manufacturing and testing conditions
title_fullStr Fatigue life of unidirectional 90° carbon/epoxy laminates made of conventional and ultra-thin plies varying manufacturing and testing conditions
title_full_unstemmed Fatigue life of unidirectional 90° carbon/epoxy laminates made of conventional and ultra-thin plies varying manufacturing and testing conditions
title_sort Fatigue life of unidirectional 90° carbon/epoxy laminates made of conventional and ultra-thin plies varying manufacturing and testing conditions
dc.creator.none.fl_str_mv Sánchez-Carmona, Serafín
Correa Montoto, Elena
Barroso Caro, Alberto
París Carballo, Federico
author Sánchez-Carmona, Serafín
author_facet Sánchez-Carmona, Serafín
Correa Montoto, Elena
Barroso Caro, Alberto
París Carballo, Federico
author_role author
author2 Correa Montoto, Elena
Barroso Caro, Alberto
París Carballo, Federico
author2_role author
author
author
dc.contributor.none.fl_str_mv Mecánica de Medios Continuos y Teoría de Estructuras
TEP131: Elasticidad y Resistencia de Materiales
Universidad de Sevilla
Consejería de Economía y Conocimiento, Junta de Andalucía
Ministerio de Ciencia, Innovación y Universidades (MICINN). España
dc.subject.none.fl_str_mv Composites
Fatigue analysis
Fiber/matrix failure
Mechanical testing
Tensile mechanical properties
Ultra-thin prepreg
topic Composites
Fatigue analysis
Fiber/matrix failure
Mechanical testing
Tensile mechanical properties
Ultra-thin prepreg
description This is an open access article under the terms of the Creative Commons Attribution License, which permits use, distribution and reproduction in any medium, provided the original work is properly cited
publishDate 2023
dc.date.none.fl_str_mv 2023
dc.type.none.fl_str_mv info:eu-repo/semantics/article
info:eu-repo/semantics/publishedVersion
format article
status_str publishedVersion
dc.identifier.none.fl_str_mv https://hdl.handle.net/11441/142726
https://doi.org/doi.org/10.1111/ffe.13966
url https://hdl.handle.net/11441/142726
https://doi.org/doi.org/10.1111/ffe.13966
dc.language.none.fl_str_mv Inglés
language_invalid_str_mv Inglés
dc.relation.none.fl_str_mv Fatigue & Fracture of Engineering Materials & Structures (2023), 46, 1837–1847
VIPPIT-2018-II.2
P18-FR-3360
PID2021-126279OB-I00
https://onlinelibrary.wiley.com/doi/full/10.1111/ffe.13966
dc.rights.none.fl_str_mv info:eu-repo/semantics/openAccess
eu_rights_str_mv openAccess
dc.format.none.fl_str_mv application/pdf
application/pdf
dc.publisher.none.fl_str_mv John Wiley & Sons Ltd.
publisher.none.fl_str_mv John Wiley & Sons Ltd.
dc.source.none.fl_str_mv reponame:idUS. Depósito de Investigación de la Universidad de Sevilla
instname:Universidad de Sevilla (US)
instname_str Universidad de Sevilla (US)
reponame_str idUS. Depósito de Investigación de la Universidad de Sevilla
collection idUS. Depósito de Investigación de la Universidad de Sevilla
repository.name.fl_str_mv
repository.mail.fl_str_mv
_version_ 1869403428282695680
score 15,300724

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