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Naji, M. |
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Motta, Antonella |
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Aletan, Dirar |
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Mohamed, Tarek |
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Ertürk, Emre |
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Taccardi, Nicola |
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Kononenko, Denys |
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Petrov, R. H. | Madrid |
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Alshaaer, Mazen | Brussels |
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Bih, L. |
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Casati, R. |
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Muller, Hermance |
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Kočí, Jan | Prague |
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Šuljagić, Marija |
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Kalteremidou, Kalliopi-Artemi | Brussels |
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Azam, Siraj |
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Ospanova, Alyiya |
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Blanpain, Bart |
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Ali, M. A. |
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Popa, V. |
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Rančić, M. |
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Ollier, Nadège |
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Azevedo, Nuno Monteiro |
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Landes, Michael |
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Rignanese, Gian-Marco |
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Dorival, Olivier
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Topics
Publications (9/9 displayed)
- 2020Effects of dynamics and trigger on energy absorption of composite tubes during axial crushingcitations
- 2018Experimental and Numerical study of the behavior of hybrid unidirectional/woven composite laminates under impact loading
- 2018Impact damage prediction in thin woven composite laminates-Part I: Modeling strategy and validationcitations
- 2016Experimental results of medium velocity impact tests for reinforced foam core braided composite structurescitations
- 2015Effects of the stacking sequence, material nature and addition of an adhesive film on the delamination resistance of woven composite laminates in mode I and II
- 2015Experimental study of impact energy absorption by reinforced braided composite structures: Dynamic crushing testscitations
- 2015Experimental comparison of impact energy absorption by several reinforced foam composite structures
- 2014Influence of the stacking sequence and crack velocity on fracture toughness of woven composite laminates in mode Icitations
- 2014Change of scale strategy for the microstructural modelling of polymeric rohacell foams
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article
Impact damage prediction in thin woven composite laminates-Part I: Modeling strategy and validation
Abstract
International audience ; An explicit finite element modeling of the 5-harness satin woven composite material is proposed in this paper. It is based on the semi-continuous approach. The bundles are modeled with rod elements and a specific dam-ageable shell element is used to stabilize this truss structure. As the woven pattern geometry plays a key role in damage initiation and propagation, the rods located at the crimp regions where warp and weft yarns cross each other have been offset to represent the bundles undulations. The main objective of the presented modelling strategy is to represent local bending stiffness variations and damage initiation at the crimp regions without using artificial parameters, but only geometric and material parameters. The method has been implemented into the explicit finite element code RADIOSS. The modeling strategy is validated by representing a three-point bending test and a drop weight test. It provides good prediction for the local bending stiffness, the impact force history and the damage size and shape. The strain concentration at the crimp regions is well represented.