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Mechanical modelling of reinforcement fabrics using a virtual fiber approach with hybrid elements

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DEPARTMENT OF MATERIALS TEXTILES AND CHEMICAL ENGINEERING (MATCH) CENTRE FOR TEXTILE SCIENCE AND ENGINEERING (CTSE)

MECHANICAL MODELLING OF

REINFORCEMENT FABRICS USING A VIRTUAL FIBRE APPROACH WITH

HYBRID ELEMENTS

Lode DAELEMANS; B. Tomme; T.D. Dinh; B. Caglar; V. Michaud; J. Van Stappen; V. Cnudde; M. Boone and W. Van Paepegem

January 2021

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In this presentation

Framework that allows the kinematic and mechanical modelling of reinforcement (woven) fabrics based on hybrid virtual fibres

2

Virtual fibres Textile modelling Predictive simulations

Woven fabrics Through-thickness

compressive loading

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The concept of virtual fibre modelling

3

Fibrous nature of yarns Virtual fibres at yarn scale 3D modelling of textiles

Near-fibre scale precision Fibres realign under load

Differences to traditional FEM modeling

# virtual fibres determines accuracy;

Transversal material behaviour follows from the virtual fibers and is not explicitly defined;

Consider contact friction between virtual fibers.

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Advantages of this near-microscale modelling approach

4

Fibrous nature of yarns Virtual fibres at yarn scale 3D modelling of textiles

No need for a priori shape assumptions or µCT model extraction

Direct implementation of yarn parameters possible (twist, fibre type, …) Determination of input parameters for mesoscale modelling tools

Extreme deformation modes (discontinuous) possible, e.g. unravelling, splitting, …

(5)

State-of-the-art in virtual fibre modelling

Initially conceived around 2000 by Wang et al.

Several research groups currently using this method, for example

5

SOME DIFFERENCES BETWEEN STUDIES Truss elements OR Beam elements

Kinematics OR Mechanics

Proprietary code OR Implemented in commercial FEA

Physics based input parameters OR Inversely determined input parameters

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Our approach to virtual fibre modelling

6

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7

INPUT APPROACH APPLICATIONS

Datasheet values Fiber diameter;

Fiber linear density;

Fiber Young’s modulus;

Yarn tex;

Crimp;

Yarn count;

Weave schematic.

Experimental input

Non-elastic material properties;

Friction;

Bending stiffness.

High fidelity

50 – 100 virtual fibres per yarn;

Most-realistic approach.

Homogenised (simple)

Yarn properties without transversal behaviour;

Manufacturing

Virtual testing

Microstructural analysis

Cord twisting Tufting Weave compaction

Forming Coated fabrics Tensile, shear, flexure, …

Physics-based framework within commercial FEA software

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Actual implementation

Each virtual fibre is a chain of truss-like elements

8

Software

ABAQUS commercial FEA software Explicit solver

General contact algorithm

T3D2 truss elements, B31 beam elements

Hybrid truss-beam elements for bending stiffness

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Assumptions

9

Cross-sectional area virtual yarn equals that of real yarn.

1.

Mechanical properties of virtual fibre equal those real fibre, except for bending stiffness.

2.

Initial fabric microstructure is generated based on weave schematic and yarn crimp.

3.

𝐴

𝑣𝑦

= 𝑛

𝑣𝑓

𝜋

4 𝐷

𝑣𝑓2

= 𝐴

𝑟𝑦

= 𝑛

𝑟𝑓

𝜋

4 𝐷

𝑟𝑓2

→ 𝐷

𝑣𝑓

1

𝑛

𝑣𝑓

𝐸

𝑏𝑒𝑎𝑚

𝐼

𝑣𝑓,𝑏𝑒𝑎𝑚

= (𝐸𝐼 )

𝑚𝑒𝑎𝑠𝑢𝑟𝑒𝑑

1

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In-plane virtual testing of a 3D woven fabric

10

Tensile testing Shear testing

Finite element simulation of the woven geometry and mechanical behaviour of a 3D woven dry fabric under tensile and shear loading using the digital element method

L Daelemans, J Faes, S. Allaoui, G. Hivet, M. Dierick, L. Van Hoorebeke, W. Van Paepegem Composites Science and Technology (2016), 137, 177-187

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Through-thickness compression

11

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From the experimental side

12

2x2 twill weave Interglass E-glass fibres

390 g/m² Fabric

Through-thickness compression set-up

Compliance calibration procedure

In-situ µCT measurements

Uncertainty range

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From the numerical side

13 Prof. Y. Wang

Kansas State University

Based on work of (Green et al. 2014)

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Amount of virtual fibres per yarn

14

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Through-thickness compression simulation

15

Dominating deformation mechanisms Fibre realignment

Fibre and yarn bending Transversal compaction

Very difficult loading to achieve predictive simulations

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“Mesh convergence”

16

61 virtual fibres per yarn Length-over-diameter ratio 1

L

D

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Importance of virtual fibre bending stiffness

17

Correct kinematics AND mechanics only with hybrid fibres

Experiment

Hybrid virtual fibres

Truss-only fibres

Truss-only fibres Truss-only fibres Hybrid virtual fibres

Hybrid virtual fibres

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Which value of bending stiffness should we implement?

18

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Which value of bending stiffness should we implement?

19

Measured bending stiffness (Peirce’s method) seems to give correct order of magnitude.

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20

Which value of friction

Simulated compressive response aligns well with the experimental measured one.

Typical glass-glass yarn friction values found in literature: 0.2 – 0.4

How to deal with decrease in surface area in virtual yarns?

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Hysteresis

21

Losses upon unloading are captured well by the simulations

Experiment Hysteresis losses

(J/m²) 6.72 ± 0.24 Simulation # virtual

fibers

𝑳/𝑫 𝑬𝑰 𝝁

61 1 𝐸𝐼𝑚𝑒𝑎𝑠 0.2 7.62

61 1 𝐸𝐼𝑚𝑒𝑎𝑠 0.35 8.04

61 1 𝐸𝐼𝑚𝑒𝑎𝑠 0.6 7.15

61 1 𝐸𝐼𝑚𝑒𝑎𝑠 0.8 7.06

61 1 2𝐸𝐼𝑚𝑒𝑎𝑠 0.35 7.92

1

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Conclusions

22

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23

Hybrid fibres offer a viable strategy for virtual fibre

modelling of the (out-of-plane) mechanical behaviour of textiles in commercial FEA packages

Accurate measurements of the platen-to-platen distance during compression

CONCLUSION

FUTURE WORK

Improved test method to determine yarn bending stiffness Friction law in function of the number of virtual fibres

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Acknowledgments

Research Foundation – Flanders (FWO) FWO grant 12ZR520N

FCWO – UGent project G.0041.15N

Ghent University Special Research Fund BOF.EXP.2017.0007

Swiss Competence Center for Energy Research (SCCER) Mobility of the Swiss Innovation Agency (Innosuisse)

Swiss National Science Foundation SNF - 182669

24

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DEPARTMENT OF MATERIALS TEXTILES AND CHEMICAL ENGINEERING CENTRE FOR TEXTILE SCIENCE AND ENGINEERING

Lode DAELEMANS

Professor

CENTRE FOR TEXTILE SCIENCE AND ENGINEERING, DEPARTMENT OF MATERIALS, TEXTILES AND

CHEMICAL ENGINEERING (MATCH)

E LODE.DAELEMANS@UGENT.BE

T +32 9 264 57 51

WEBSITE HTTPS://WWW.TEXTILES.UGENT.BE

@UGENT_TEXTILES

@LDAELEMA

LODE DAELEMANS

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