Suppression of Delamination in CFRP Laminates with Ply Discontinuity Using Polyamide Mesh

Carbon fiber-reinforced plastics (CFRPs) offer excellent in-plane mechanical performance, but their relatively low interlaminar fracture toughness makes them vulnerable to delamination, particularly around intralaminar discontinuities such as resin-rich regions or fiber gaps. This study investigates the effectiveness of polyamide (PA) mesh inserts in improving interlaminar toughness and suppressing delamination in CFRP laminates with such features. Two PA mesh configurations were evaluated: a fully embedded continuous layer and a 20 mm cut mesh strip placed between continuous and discontinuous plies near critical regions. Fracture toughness tests showed that PA mesh insertion improved interlaminar toughness approximately 2.4-fold compared to neat CFRP, primarily due to a mechanical interlocking mechanism that disrupts crack propagation and enhances energy dissipation. Uniaxial tensile tests with digital image correlation revealed that while initial matrix cracking occurred at similar stress levels, the stress at which complete delamination occurred was approximately 60% higher in specimens with a 20 mm mesh and up to 92% higher in specimens with fully embedded mesh. The fully embedded mesh provided consistent delamination resistance across the laminate, while the 20 mm insert localized strain redistribution and preserved global mechanical performance. These findings demonstrate that PA mesh is an effective interleaving material for enhancing damage tolerance in CFRP laminates with internal discontinuities.

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Publication Details

Journal
Journal of Composites Science
Published
2025-08-04
DOI
https://doi.org/10.3390/jcs9080414
Citations
6
Primary Topic
Mechanical Behavior of Composites
Type
article
Field-Weighted Citation Impact
5.18
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article

Suppression of Delamination in CFRP Laminates with Ply Discontinuity Using Polyamide Mesh

Jun Koyanagi, M. J. Mohammad Fikry, Satoru Yoneyama, Vladimir Vinogradov et al.
6 citations
Journal of Composites Science
Mechanical Behavior of Composites
5.18
article

Suppression of Delamination in CFRP Laminates with Ply Discontinuity Using Polyamide Mesh

Jun Koyanagi, M. J. Mohammad Fikry, Satoru Yoneyama, Vladimir Vinogradov, Shinji Ogihara, Hayato NAKATANI, Keisuke Iizuka
article en
6 citations

Abstract

Carbon fiber-reinforced plastics (CFRPs) offer excellent in-plane mechanical performance, but their relatively low interlaminar fracture toughness makes them vulnerable to delamination, particularly around intralaminar discontinuities such as resin-rich regions or fiber gaps. This study investigates the effectiveness of polyamide (PA) mesh inserts in improving interlaminar toughness and suppressing delamination in CFRP laminates with such features. Two PA mesh configurations were evaluated: a fully embedded continuous layer and a 20 mm cut mesh strip placed between continuous and discontinuous plies near critical regions. Fracture toughness tests showed that PA mesh insertion improved interlaminar toughness approximately 2.4-fold compared to neat CFRP, primarily due to a mechanical interlocking mechanism that disrupts crack propagation and enhances energy dissipation. Uniaxial tensile tests with digital image correlation revealed that while initial matrix cracking occurred at similar stress levels, the stress at which complete delamination occurred was approximately 60% higher in specimens with a 20 mm mesh and up to 92% higher in specimens with fully embedded mesh. The fully embedded mesh provided consistent delamination resistance across the laminate, while the 20 mm insert localized strain redistribution and preserved global mechanical performance. These findings demonstrate that PA mesh is an effective interleaving material for enhancing damage tolerance in CFRP laminates with internal discontinuities.

Journal of Composites ScienceVol. 9(8)
Osaka Gakuin University (JP), Aoyama Gakuin University (JP), Tokyo University of Science (JP), Newcastle University (GB)
Openalex Percentile: Top 4%
Mechanical Behavior of Composites
5.18
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