Textile Composite Damage Analysis Taking into Account the Forming Process
The internal structure of composite materials is modified during manufacturing. The formation of woven prepregs or dry preforms changes the angle between the warp and weft yarns. The damage behaviour of the consolidated composite is modified by these changes of angle. It is important when designing...
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doaj-20f73129eb91400cadb4684c0675fd902020-11-27T08:03:09ZengMDPI AGMaterials1996-19442020-11-01135337533710.3390/ma13235337Textile Composite Damage Analysis Taking into Account the Forming ProcessMarjorie Jauffret0Aldo Cocchi1Naim Naouar2Christian Hochard3Philippe Boisse4INSA-Lyon, LaMCoS CNRS, University de Lyon, 69621 Lyon, FranceLMA CNRS, Aix Marseille University, 13007 Marseille, FranceINSA-Lyon, LaMCoS CNRS, University de Lyon, 69621 Lyon, FranceLMA CNRS, Aix Marseille University, 13007 Marseille, FranceINSA-Lyon, LaMCoS CNRS, University de Lyon, 69621 Lyon, FranceThe internal structure of composite materials is modified during manufacturing. The formation of woven prepregs or dry preforms changes the angle between the warp and weft yarns. The damage behaviour of the consolidated composite is modified by these changes of angle. It is important when designing a composite part to consider this modification when calculating the damage in order to achieve a correct dimensioning. In this paper, a damage calculation approach of the consolidated textile composite that takes into account the change in orientation of the yarns due to forming is proposed. The angles after forming are determined by a simulation of the draping based on a hypoelastic behaviour of the woven fabric reinforcement. Two orthogonal frames based on the warp and weft directions of the textile reinforcement are used for the objective integration of stresses. Damage analysis of the cured woven composite with non-perpendicular warp and weft directions is achieved by replacing it with two equivalent Unidirectional (UD) plies representing the yarn directions. For each ply, a model based on Continuum Damage Mechanics (CDM) describes the progressive damage. Two examples are presented, a bias extension specimen and the hemispherical forming coupon. In both cases, the angles between the warp and weft yarns are changed. It is shown that the damage calculated by taking into account these angle changes is greatly modified.https://www.mdpi.com/1996-1944/13/23/5337damageforminghypoelasticitytextile compositefibre orientation |
collection |
DOAJ |
language |
English |
format |
Article |
sources |
DOAJ |
author |
Marjorie Jauffret Aldo Cocchi Naim Naouar Christian Hochard Philippe Boisse |
spellingShingle |
Marjorie Jauffret Aldo Cocchi Naim Naouar Christian Hochard Philippe Boisse Textile Composite Damage Analysis Taking into Account the Forming Process Materials damage forming hypoelasticity textile composite fibre orientation |
author_facet |
Marjorie Jauffret Aldo Cocchi Naim Naouar Christian Hochard Philippe Boisse |
author_sort |
Marjorie Jauffret |
title |
Textile Composite Damage Analysis Taking into Account the Forming Process |
title_short |
Textile Composite Damage Analysis Taking into Account the Forming Process |
title_full |
Textile Composite Damage Analysis Taking into Account the Forming Process |
title_fullStr |
Textile Composite Damage Analysis Taking into Account the Forming Process |
title_full_unstemmed |
Textile Composite Damage Analysis Taking into Account the Forming Process |
title_sort |
textile composite damage analysis taking into account the forming process |
publisher |
MDPI AG |
series |
Materials |
issn |
1996-1944 |
publishDate |
2020-11-01 |
description |
The internal structure of composite materials is modified during manufacturing. The formation of woven prepregs or dry preforms changes the angle between the warp and weft yarns. The damage behaviour of the consolidated composite is modified by these changes of angle. It is important when designing a composite part to consider this modification when calculating the damage in order to achieve a correct dimensioning. In this paper, a damage calculation approach of the consolidated textile composite that takes into account the change in orientation of the yarns due to forming is proposed. The angles after forming are determined by a simulation of the draping based on a hypoelastic behaviour of the woven fabric reinforcement. Two orthogonal frames based on the warp and weft directions of the textile reinforcement are used for the objective integration of stresses. Damage analysis of the cured woven composite with non-perpendicular warp and weft directions is achieved by replacing it with two equivalent Unidirectional (UD) plies representing the yarn directions. For each ply, a model based on Continuum Damage Mechanics (CDM) describes the progressive damage. Two examples are presented, a bias extension specimen and the hemispherical forming coupon. In both cases, the angles between the warp and weft yarns are changed. It is shown that the damage calculated by taking into account these angle changes is greatly modified. |
topic |
damage forming hypoelasticity textile composite fibre orientation |
url |
https://www.mdpi.com/1996-1944/13/23/5337 |
work_keys_str_mv |
AT marjoriejauffret textilecompositedamageanalysistakingintoaccounttheformingprocess AT aldococchi textilecompositedamageanalysistakingintoaccounttheformingprocess AT naimnaouar textilecompositedamageanalysistakingintoaccounttheformingprocess AT christianhochard textilecompositedamageanalysistakingintoaccounttheformingprocess AT philippeboisse textilecompositedamageanalysistakingintoaccounttheformingprocess |
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