Numerical study of delamination process of the CFRP composite

A quasi-static approach for an interface damage model, incorporating Rayleigh damping for viscoelastic carbon fiber reinforced polymer composites, is introduced. The interface traction-relative displacement behavior is modeled using a thin adhesive layer, similar to cohesive zone models. The problem...

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Main Authors: Eva Kormanikova, Kamila Kotrasova
Format: Article
Language:English
Published: Gruppo Italiano Frattura 2025-01-01
Series:Fracture and Structural Integrity
Subjects:
Online Access:https://www.fracturae.com/index.php/fis/article/view/5199/4172
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author Eva Kormanikova
Kamila Kotrasova
author_facet Eva Kormanikova
Kamila Kotrasova
author_sort Eva Kormanikova
collection DOAJ
description A quasi-static approach for an interface damage model, incorporating Rayleigh damping for viscoelastic carbon fiber reinforced polymer composites, is introduced. The interface traction-relative displacement behavior is modeled using a thin adhesive layer, similar to cohesive zone models. The problem is solved numerically with a semi-implicit time-stepping method. The cohesive interface model, integrated into the Finite Element Method, was applied to determine the critical force away from the crack tip. Results showed that the numerical delamination under mode I conditions aligned well with experimental data for the cohesive zone formulations studied. The numerical example demonstrates the effectiveness of the proposed model
format Article
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institution Kabale University
issn 1971-8993
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publisher Gruppo Italiano Frattura
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series Fracture and Structural Integrity
spelling doaj-art-45424403bd0e4a3db0f613cd93c2388b2025-01-03T08:51:16ZengGruppo Italiano FratturaFracture and Structural Integrity1971-89932025-01-01197118219210.3221/IGF-ESIS.71.1310.3221/IGF-ESIS.71.13Numerical study of delamination process of the CFRP compositeEva KormanikovaKamila KotrasovaA quasi-static approach for an interface damage model, incorporating Rayleigh damping for viscoelastic carbon fiber reinforced polymer composites, is introduced. The interface traction-relative displacement behavior is modeled using a thin adhesive layer, similar to cohesive zone models. The problem is solved numerically with a semi-implicit time-stepping method. The cohesive interface model, integrated into the Finite Element Method, was applied to determine the critical force away from the crack tip. Results showed that the numerical delamination under mode I conditions aligned well with experimental data for the cohesive zone formulations studied. The numerical example demonstrates the effectiveness of the proposed modelhttps://www.fracturae.com/index.php/fis/article/view/5199/4172delaminationcfrp compositefemmode i
spellingShingle Eva Kormanikova
Kamila Kotrasova
Numerical study of delamination process of the CFRP composite
Fracture and Structural Integrity
delamination
cfrp composite
fem
mode i
title Numerical study of delamination process of the CFRP composite
title_full Numerical study of delamination process of the CFRP composite
title_fullStr Numerical study of delamination process of the CFRP composite
title_full_unstemmed Numerical study of delamination process of the CFRP composite
title_short Numerical study of delamination process of the CFRP composite
title_sort numerical study of delamination process of the cfrp composite
topic delamination
cfrp composite
fem
mode i
url https://www.fracturae.com/index.php/fis/article/view/5199/4172
work_keys_str_mv AT evakormanikova numericalstudyofdelaminationprocessofthecfrpcomposite
AT kamilakotrasova numericalstudyofdelaminationprocessofthecfrpcomposite