Study of Damage in Woven Composite Materials Subjected to Impact

This study focuses on modeling the low-velocity impact behaviour of textile-shaped composites. Textile preforms are modeled using Texgen software. Six types of fabrics are considered: Twill (2/2) [0]4, twill (2/2) sequence [0/30/-30/0], twill (2/2) sequence [0/45/-45/0], and plain weave [0]4, plain weave sequence [0/30/-30/0], plain weave sequence [0/45/-45/0]. For the study of fabric damage under impact, the commercial finite element software Ls-dyna is used in transient regime. The "automatic-surface to-surface" approach is employed to model the contact between the impactor and the laminate, while the contact between fibres and the matrix is modeled using the "contact automatic surface to surface tiebreak" technique. Results from the modeling are graphically represented over the impact time. With increasing impact velocity, the contact force, displacement at the impact point, and impact energy increase accordingly.

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Publication Details

Journal
Acta Mechanica Slovaca
Published
2025-03-30
DOI
https://doi.org/10.21496/ams.2024.027
Primary Topic
Textile materials and evaluations
Type
article
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article

Study of Damage in Woven Composite Materials Subjected to Impact

Zahi Rachid, Habib Achache, M. Djilali Beida
3 links
Acta Mechanica Slovaca
Textile materials and evaluations
article

Study of Damage in Woven Composite Materials Subjected to Impact

Zahi Rachid, Habib Achache, M. Djilali Beida
article en

Abstract

This study focuses on modeling the low-velocity impact behaviour of textile-shaped composites. Textile preforms are modeled using Texgen software. Six types of fabrics are considered: Twill (2/2) [0]4, twill (2/2) sequence [0/30/-30/0], twill (2/2) sequence [0/45/-45/0], and plain weave [0]4, plain weave sequence [0/30/-30/0], plain weave sequence [0/45/-45/0]. For the study of fabric damage under impact, the commercial finite element software Ls-dyna is used in transient regime. The "automatic-surface to-surface" approach is employed to model the contact between the impactor and the laminate, while the contact between fibres and the matrix is modeled using the "contact automatic surface to surface tiebreak" technique. Results from the modeling are graphically represented over the impact time. With increasing impact velocity, the contact force, displacement at the impact point, and impact energy increase accordingly.

Acta Mechanica SlovacaVol. 29(1)
Sustainable cities and communities
Openalex Percentile: Top 85%
Textile materials and evaluations
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