constitutive modeling of viscoelastic behavior of cnt/polymer composites k. yazdchi 1, m. salehi 2...
TRANSCRIPT
Constitutive modeling of viscoelastic behavior of CNT/Polymer composites
K. Yazdchi1, M. Salehi2
1- Multi scale Mechanics (MSM), Faculty of Engineering Technology, University of Twente, Enschede, The Netherlands
[email protected] Mechanical engineering Department, Amirkabir University of
Technology, Tehran, Iran
Presentation Outline
• Geometric Structure, Mechanical Properties
and Applications of SWCNTs
• Micromechanical analysis
• Predicting mechanical properties, using
equivalent continuum model (ECM)
• Numerical results
• Conclusions
Geometric Structure of SWCNTs
Source: http://www.photon.t.u-tokyo.ac.jp/~maruyama/agallery/agallery.html
Geometric Structure of SWCNTs
21 manaCh
22
1
2
3sin
nmnm
m
O
C
ArmchairZigzag
Wrapping (10,0) SWNT (Zigzag)
Ch = (10,0)
Wrapping (10,10) SWNT (Armchair)
Ch = (10,10)
Wrapping (10,5) SWNT (Chiral)
Ch = (10,5)
Mechanical Properties of CNTs
High Elastic Modulus (1 TPa)
Strength 100 times greater than steel (up to 50
GPa) at one sixth the Weight
High Strain to Failure (10%-30%)
High Electrical and Thermal Conductivity
High Aspect Ratio (1000)
Excellent Resilience and Toughness
Excellent Optical and Transport Properties
Low Density (1.3 g/cm^3)
CNTs Applications
Reinforcement Elements
Aerospace, Automobile, Medicine, or
Chemical Industry
Sensors and Actuators
Space Elevator
CNT Nano-Gear and Puncher
CNT Transistor
Defect and Junction Devices
Micromechanical analysis
Representative Volume Element (RVE)
Macroscale Microscale
Zoom
Inclusions Voids
Micromechanical analysis (Modeling Procedures)
Step 1
Step 2
Step 3
Homogenization scheme
Micromechanical analysis (Stress & Strain Averages)
,1w
wdVx
V
ww
dVxV
1
Inclusions
Matrix
00
0
11
1
01
11
wwV
w
V
www
dVxdVxV
dVxV
0101 wwwvv
00
0
11
1
01
11
wwV
w
V
www
dVxdVxV
dVxV
01
01 wwwvv
Micromechanical analysis (Homogenized elastic operator)
0101
:1::1: 01110111 w
el
w
el
w
el
w
el
wCvCvCvCv
Assume that each phase of this RVE obeys Hooke’s law:
1
1
1
:0 v
Avww
w
On the other hand:
w
el
w
elelel
wCACCvC :::0110
ACCvCC elelelel:0110 ?
Micromechanical analysis (Voigt Assumption)
01 www
elelel
w
elel
wCvCvCCvCv 01110111 1:1
4IAVoigt
0 0Upper Bound
Micromechanical analysis (Reuss Assumption)
01 www
0 0
01
11 1:wwww
el
wvvD
01
:1: 0111 w
el
w
el
wDvDv
elelelDvDvD 0111 1
11
01
1
11 1
elelelCvCvC
Lower Bound
Micromechanical analysis (Mori Tanaka (M-T) scheme)
• The most popular
• For composites with moderate volume fractions of inclusions (25% - 30%)
• Takes into account the interaction between inclusions
Heterogeneous RVE
Step 1
Step 2
Associated Isolated Inclusion Medium
0 //0
//0
• For composites with transversely isotropic, spheroidal inclusions, unidirectional reinforcements
Equivalent Homogeneous Medium
Micromechanical analysis (Viscoelasticity )
Dynamic Correspondence Principle (DCP):
Elastic Solution Viscoelastic Solution
ssEs^^^
E
Time Domain Frequency Domain
LCT
Inverse LCT iws
Numerical Results• Straight NTs (Effects of Waviness is ignored)
• Perfectly aligned or completely randomly oriented
nanotubes
• Matrix is linearly viscoelastic and isotropic and
effective continuum fiber is elastic and transversely
isotropic
• Perfect bounding between NT and polymer
• Assume a SWCNT, the non-bulk local polymer around
the NT, and the NT/polymer interface layer collectively as
an effective continuum fiber
• Mechanical properties of NT and polymer are
independent from temperature
Numerical Results (Analytical Formulation)
,2
,2
,2
,
,
,
31
^
44
^
31
^
23
^
23
^
22
^
23
^
66
^
23
^
12
^
44
^
12
^
33
^
22
^
22
^
23
^
11
^
12
^
33
^
33
^
23
^
22
^
22
^
11
^
12
^
22
^
33
^
12
^
22
^
12
^
11
^
11
^
11
^
L
LLL
L
LLL
LLL
LLL
Transversely isotropic
^^^^^^
2,2,,,2 pmnlkL
,,,
,,
12
^^
23
^^
11
^^
12
^^
23
^^
GpGmLn
LlKk
Numerical Results (Modeling the interphase region)
Bulk polymer
Interphase
CNT
R
05.0
fr
t
1
fr
t
Carbon fibers
Carbon Nanotubes!!
Numerical Results (Modeling the interphase region)
Multiscale modeling
Numerical Results (Completely randomly oriented nanotubes)
0.4
0.5
0.6
0.7
0.8
0.9
1
1.1
0 5 10
t (hour)
1/E
(1/
GP
a)
Aspect ratio = 5
Aspect ratio = 50
Aspect ratio = 5000
0.2
0.4
0.6
0.8
1
1.2
1.4
0 5 10
t (hour)
1/G
(1/
GP
a)
CNT volumefraction = 1%
CNT volumefraction = 5%
CNT volumefraction = 10%
Isotropic composites
^^
,GK
44
^
11
^
,LLOR
Numerical Results (Perfectly aligned)
0
0.2
0.4
0.6
0.8
1
1.2
1.4
0 2 4 6 8 10
t (hour)
Cre
ep C
omp
lian
ce (
1/G
Pa)
M22, CNT Volumefraction = 1%
M22, CNT Volumefraction = 5%
M22, CNT Volumefraction = 10%
k23, CNT Volumefraction = 1%
k23, CNT Volumefraction = 5%
k23, CNT Volumefraction = 10%
M44, CNT Volumefraction = 1%
M44, CNT Volumefraction = 5%
M44, CNT Volumefraction = 10%
Transversely isotropic composites
Numerical Results (Perfectly aligned)
Transversely isotropic composites
0.01
0.02
0.03
0.04
0.05
0.06
0.07
0 2 4 6 8 10
t (hour)
Cre
ep C
ompl
ianc
e (1
/GP
a)
M11, CNT Volumefraction = 1%
M11, CNT Volumefraction = 5%
M11, CNT Volumefraction = 10%
Numerical Results (Perfectly aligned)
Transversely isotropic composites
0.10.150.2
0.250.3
0.350.4
0.450.5
0.55
0 2 4 6 8 10
t (hour)
Cre
ep C
ompl
ianc
e (1
/GP
a) M22, Aspect ratio = 5
M22, Aspect ratio = 50
M22, Aspect ratio = 500
k23, Aspect ratio = 5
k23, Aspect ratio = 50
k23, Aspect ratio = 500
Numerical Results (Perfectly aligned)
Transversely isotropic composites
0
0.2
0.4
0.6
0.8
1
1.2
1.4
0 2 4 6 8 10
t (hour)
Cre
ep C
ompl
ianc
e (1
/GP
a) M11, Aspect ratio = 5
M11, Aspect ratio = 50
M11, Aspect ratio = 500
M44, Aspect ratio = 5
M44, Aspect ratio = 50
M44, Aspect ratio = 500
Conclusions
The parameters which affect the mechanical properties of NTRPCs are NT aspect ratio, volume fraction and orientation.
For composites having unidirectionally aligned nanotubes (transversely isotropic), numerical results indicate that the increase of the nanotube aspect ratio and volume fraction significantly enhances their axial creep resistance but has insignificant influences on their transverse, shear and plane strain bulk creep compliances.
The effect of the nanotube orientation on the shear compliances is negligibly small.
Conclusions
For composites with aligned or randomly oriented nanotubes, all the compliances are found to decrease monotonically with the increase of the nanotube volume fraction.
For composites having randomly oriented NTs (isotropic) with increasing the aspect ratio or NT volume fraction, the axial and shear creep compliances will decreases also the effect of aspect ratio in comparison with volume fraction is negligible.
The model proposed in the foregoing is simple and very economical to employ, particularly in viscoelastic behaviour of nanocomposites, compared with other methods.
Suggestions
The effects of NT waviness and agglomeration and also temperature on the viscoelastic behavior of NTRPCs.
Find new methods in modeling the interphase region (such as MD, etc).
The effect of anisotropic properties of CNTs, 3D modelling, end caps and any possible relative motion between individual shells or tubes in a MWNT and an NT bundle Voids and Defects will be studied in the future.
Use other Micromechanical models and compare the results with experimental data.
Thank you for your attention
Any Questions?