Towards the determination of optimal 3D initiation crack shapes

An approach is proposed to determine the optimal initiation crack shapes when using the Coupled Criterion (CC) to assess 3D debonding initiation at a fiber-matrix interface. The optimal crack shapes are determined among potential crack shapes described by their length along the fiber-matrix interface, their angle at the free surface and the shape of the debonding front. The optimal crack shapes actually correspond to the crack shapes maximizing the energy criterion, regardless of the interface fracture properties. Stress-isocontours fail to replicate the debonding shapes that were experimentally observed on the side of a single glass fiber-transparent epoxy sample, unlike the energy-based crack shapes. Both methods yield similar interface strength identification, however, the energy-based shapes result in larger identified critical energy release rates.

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Publication Details

Journal
Comptes Rendus Mécanique
Published
2025-07-25
DOI
https://doi.org/10.5802/crmeca.309
Primary Topic
Mechanical Behavior of Composites
Type
article
Field-Weighted Citation Impact
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article

Towards the determination of optimal 3D initiation crack shapes

Jérôme Bikard, Behrad Koohbor, Renaud G. Rinaldi, Hugo Girard et al.
Comptes Rendus Mécanique
Mechanical Behavior of Composites
article

Towards the determination of optimal 3D initiation crack shapes

Jérôme Bikard, Behrad Koohbor, Renaud G. Rinaldi, Hugo Girard, Nathalie Godin, Aurélien Doitrand, Milena Tosti Umemura
article en

Abstract

An approach is proposed to determine the optimal initiation crack shapes when using the Coupled Criterion (CC) to assess 3D debonding initiation at a fiber-matrix interface. The optimal crack shapes are determined among potential crack shapes described by their length along the fiber-matrix interface, their angle at the free surface and the shape of the debonding front. The optimal crack shapes actually correspond to the crack shapes maximizing the energy criterion, regardless of the interface fracture properties. Stress-isocontours fail to replicate the debonding shapes that were experimentally observed on the side of a single glass fiber-transparent epoxy sample, unlike the energy-based crack shapes. Both methods yield similar interface strength identification, however, the energy-based shapes result in larger identified critical energy release rates.

Comptes Rendus MécaniqueVol. 353(G1)
Université Claude Bernard Lyon 1 (FR), Centre National de la Recherche Scientifique (FR), Matériaux Ingénierie et Science (FR), Hôpital Saint-Michel (FR), Rowan University (US), Institut National des Sciences Appliquées de Lyon (FR)
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Openalex Percentile: Top 77%
Mechanical Behavior of Composites
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