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5/6/2013
1
DEVELOPMENT OF CONSTITUTIVE MATERIAL MODEL FOR COMPOSITE WITH
NONLINEAR FIBERS AND MATRIX
Liva Pupure1, Roberts Joffe1,2 and Janis Varna1
1Luleå University of Technology, S-97187 Luleå, SWEDEN2Swerea SICOMP, S-94126 Piteå, SWEDEN
6th International Conference on Composites Testing and Model Identification,
April 22-24, 2013, Alborg, Denmark
2
Outline
• Introduction
• Objectives
• Materials and Manufacturing
• Material model
• Damage
• Visco-plasticity
• Visco-elasticity
• Summary
• Acknowledgments
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3
Introduction
• Advantages: High specific properties, renewable, recyclable, good insulation and damping properties 0
50
100
150
200
250
300
350
0 1 2 3 4 5 6 7
Str
ess
(MP
a)
Strain (%)
Flax UD
Cordenka UD
• Disadvantages: Poor adhesion between fiber and matrix, limited fiber length, difficult to control fiber alignment and orientation, sensitivity to moisture and temperature, limited processing temperature, low impact strength, high non-linearity, variability of properties.
4
Objectives
• Ultimate objective of my work:– Develop accurate models that can predict behavior of
whole bio-based structural composites, based on properties of constituents
• This work demonstrates methodology for identification of input parameters required time-dependent material model
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5
Materials and Manufacturing• Epobiox: epoxidized pine oil based resin ~75% bio-
based (Amroy Finland); curing agent Amroy Ca35Tghardener (mixing ratio 100:27)
• Regenerated cellulose fibers (RCF) used in this studywere Cordenka 700 Super 3
Manufacturing
• Fiber roving was winded on steel plates
using a filament winding machine (2 layers)
• The fiber preforms were impregnated
using vacuum infusion with resin heated
to 50˚C and afterwards cured for 2h at 80˚C
6
Materials and manufacturing
Material E, GPa σmax, MPa εσmax, %
EpoBioX 3.6 56.8 1.8
RCF 22.6 654.4 8.9
RCF/EpoBioX 15.0 246.1 4.9
RH=41%
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7
Material model
max
0max
E
Ed
mm
mCS
exp1
t
a
dt
0
'
Damage Visco-elastic
Visco-plastic
td
d
gdSgd VP
t
,2
010max
mt
MVPVP dC
0
8
Material modelVarna J, Rozite L, Joffe R and Pupurs A, Nonlinearbehavior of PLA based flax composites. Plast RubberCompos, 2012
Giannadakis K, Mannberg P, Joffe R and Varna J, Thesource of inelastic behavior of Glass Fibre /Vinilesternon-crimp fabric [±45]s laminates. J Reinf Plast Comp2011
Rozite L, Varna J, Joffe R and Pupurs A, Analysis of nonlinear behavior oflignin based flax composites, Mechanics of Composite Materials, 2012(accepted).
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9
Material model
Fibermodel
Matrixmodel Composite
model
10
Damage
max
0max
E
Ed
0
2
4
6
8
10
12
14
16
0 1 2 3 4 5 6
E m
od
ulu
s (G
Pa
)
Strain (%)
Normalized E modulus evolution in UD Cordenka
Load
Load, after 9 days
Unload
Unload, after 9 days
Ramp history of loading-unloading experiment to characterize damage
in fiber composite
Reversible or irreversible?
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11
Visco-plasticity
• By performing multiple step creep test at different stress levels
0
0,5
1
1,5
2
2,5
3
0 10000 20000 30000 40000 50000 60000
Str
ain
(%
)
Time (s)
RCF/EpoBioX
160 MPa140 MPa120 MPa100 MPa
mt
MVPVP dC
0
mMVP
m
VP CAt
tAconst 0*
)(.
No loading history and
12
Visco-plasticity
mM
VP
m
VP
CAt
tA
const
0
*
)(
.
0
0.2
0.4
0.6
0.8
1
1.2
0 0.2 0.4 0.6 0.8 1 1.2
Str
ain
(%
)
Time t/t*
Plastic strain development RCF
Modeling250MPa200MPa150MPa100MPa
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13
Visco-plasticity
mM
VP
m
VP
CAt
tA
const
0
*
)(
.
14
Visco-plasticity
• High scatter between samples from the same batch, material demanding test (large number of specimens required).
**2
*1
***2
2*1
1 ......t
t
t
t
t
t
t
t
t
t
t
t
t
tC nknnM
nnM
n
m
nMn
MMVPVP
Parameter Different samples
Onesample
m 0.26 0.26
M 14.1 14
CVP (%) 1.69·10-9 1.36·10-9
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15
Visco-elasticity
• By performing one step creep test at different stress levels (scatter between samples from one batch, sensitivity to moisture, tests in knee region)
• VP-strain can be removed from curve in order to obtain pure VE behavior
16
Visco-elasticity
• Finding of the Cm and τm by mathematical fit for all samples separately
• Choosing reference sample and corresponding Cm and τm
1,1
2
,210
expexp1
exp1
tVPii i
irec
tVPi i
icreep
tt
a
tCg
a
tCgg
10
1
1
g
a
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17
creep
creep
creep
Stra
in (
%)
Stra
in (
%)
Stra
in (
%)
Time (sec)
Time (sec)
Time (sec)
creep
creep
creep
Stra
in (
%)
Stra
in (
%)
Stra
in (
%)
Time (sec)
Time (sec)
Time (sec)
Visco-elasticityREF: 100MPa REF: 120MPa
100
MP
a12
0 M
Pa
160
MP
a
18
Visco-elasticity
• Finding master curve for aσ
EpoBioX RCF/EpoBioX
1a
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19
Visco-elasticity
• Finding master curve for aσ (RCF)1a
20
Visco-elasticity
• Using reference sample and master curve for aσ
find functions g1 and g2
0
0.2
0.4
0.6
0.8
1
1.2
20 25 30 35 40 45 50
g2
Stress, MPa
g2
from fit of experimental data
fitting curve0
0.4
0.8
1.2
1.6
2
20 25 30 35 40 45 50
g1
Stress, MPa
g1
from fit of experimental data
fitting curve
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Summary
• Constitutive model to predict behavior of highly non-linearbio-based composite is in development. Main inputparameters are identified.
• Comprehensive experimental program has been carried outto characterize RCF and their composites. Results showedhigh scatter of data within one batch of specimens. Thisproblem can be solved by use of one specimen to identify allparameters.
• High sensitivity of these materials to moisture complicatesanalysis, since dependents of input parameters on moisturecontent should be accounted for.
22
Summary
• It has been observed that Cm and τm obtained from fittingexperimental data from lowest or highest stress level showsunacceptable fit at different stress levels. Reference samplewith corresponding Cm and τm must be chosen fromintermediate stress levels, which showed best overall fit forall samples.
• The shape of master curve aσ can be seen from dataobtained using several samples as a reference sample. Aftermaster curve has been defined and reference samplechosen, parameters g1 and g2 can be identified by fitting.
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Acknowledgments
• Runar Långström, Birgitha Nyström and PeterMannberg (Swerea SICOMP) for supplyingmaterials
• Newsha Doroudgarian for help with experiments
• My studies has been financially supported byInterreg IV Nord project ANACOMPO (fundingby EU and local government)
24
Thank you for your attention!