benjamin d. jensen, kristopher e. wise - nasa€¦ · effects of atomic-scale structure on the...
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Effects of atomic-scale structure on the
fracture properties of amorphous
carbon – carbon nanotube composites
Benjamin D. Jensen, Kristopher E. WiseNASA Langley Research Center
Gregory M. OdegardMichigan Technological University
13th U.S. National Congress on Computational Mechanics
July 26-30, 2015
https://ntrs.nasa.gov/search.jsp?R=20160006312 2020-06-30T13:27:04+00:00Z
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Overview
Motivation• Carbon nanotubes (CNTs) have high specific stiffness and strength
• Composite design with CNTs will be different than for carbon fibers
• New reactive force field ReaxFF can be applied to model fracture
Objectives1. Estimate maximum CNT composite mechanical properties
2. Compare composite mechanical properties with:
a. Singlewall vs multiwall CNTs
b. Dispersed vs bundled CNT arrangements
c. CNT-matrix crosslinking
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Bond breaking with ReaxFF
Molecular dynamics using ReaxFF:
– Allows bond breaking and formation to be modeled
– Multibody interactions via bond order function
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1 1.5 2 2.5 3
Po
ten
tia
l E
nerg
y (
kca
l/m
ole
)
Distance (Å)
HarmonicReaxFF
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1 1.5 2 2.5 3
Fo
rce
(kca
l/m
ole
−Å
)
Distance (Å)
HarmonicReaxFF
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Modeling Fracture with ReaxFF
New ReaxFFC-2013 parameterization fitted to:
– Diamond strained in the bulk and <001> direction
– Graphene strained in the bulk and axial directions
In-house analysis of ReaxFFC-2013* mechanical properties
of diamond, graphene, amorphous carbon, and CNTs:**
– Improved Poisson contraction response
– Elastic and fracture properties improved over previous
ReaxFFCHO parameterization
*Goverapet Srinivasan, S.; van Duin, A. C. T.; Ganesh, P., J. Phys. Chem. A 2015, 119 (4), 571-580.
**Jensen, B.D.; Wise, K.; Odegard, G.M., Submitted to J. Phys. Chem A
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Simulation Setup
SWNT Array
SWNT Bundle MWNT Array5
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Simulation Setup
1. Continuous/straight CNTs
2. Amorphous carbon (AC) matrix:– Relative simplicity
– High mechanical properties
3. Three CNT arrangements:– SWNT array, MWNT array, SWNT bundle
4. Five crosslinking fractions for each system:– 0%, 5%, 10%, 15%, 20%
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Equilibration Procedure
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1400
E F G O P O P
Po
ten
tia
l E
ne
rgy (
kca
l/m
ol)
Te
mp
era
ture
(K
)
Time (ps)
Equilibration Step
Potential EnergyTemperature
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Results
0
1
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0 0.5 1 1.5 2
gc(r
)
r (nm)
all atomsCNT
AC
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0 0.5 1 1.5 2
gc(r
)
r (nm)
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1
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0 0.5 1 1.5 2g
c(r
)
r (nm)
a) b) c)
Structuring of amorphous carbon at the CNT interface
Nanotube-centered cylindrical distribution functions, zeroed at the exterior nanotube wall
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Results
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Results
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240
0 0.05 0.1 0.15 0.2 0.25
Axia
l S
pecific
Mod
ulu
s(G
Pa/(
g/c
m3)
Degree of Crosslinking
SWNT arrayMWNT array
SWNT bundle
Results
Axial Specific Moduli
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• Templating of the matrix substantially increases
the axial modulus
• Dispersion of crosslink sites does not strongly
influence axial modulus
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Results
Axial Specific Moduli
• Templating of the matrix substantially increases
the axial modulus
• Dispersion of crosslink sites does not strongly
influence axial modulus
120
140
160
180
200
220
240
0 0.05 0.1 0.15 0.2 0.25
Axia
l S
pecific
Mod
ulu
s(G
Pa/(
g/c
m3)
Absolute Degree of Crosslinking
SWNT arrayMWNT array
SWNT bundle
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Results
Transverse Specific Moduli
• Multiwalled CNT resists CNT flattening, increasing
the transverse modulus
• Lack of crosslinks within the bundle limits
effectiveness of crosslinking for transverse stiffness
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50
60
70
0 0.05 0.1 0.15 0.2 0.25
Tra
nsvers
e S
pe
cific
Mo
dulu
s (
GP
a/(
g/c
m3)
Degree of Crosslinking
SWNT arrayMWNT arraySWNT bundle
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Results
Specific Shear Moduli
• SWNT bundle system has lowest specific shear
moduli in both directions
• Inner MWNT walls reinforce circular shape resulting
in higher out-of-plane specific shear modulus
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20
25
30
35
40
0 0.05 0.1 0.15 0.2 0.25
In−
Pla
ne
Sp
ecific
She
ar
Modu
lus (
GP
a/(
g/c
m3)
Degree of Crosslinking
SWNT arrayMWNT arraySWNT bundle
5
10
15
20
25
0 0.05 0.1 0.15 0.2 0.25O
ut−
of−
Pla
ne
Sp
ecific
She
ar
Modu
lus (
GP
a/(
g/c
m3)
Degree of Crosslinking
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0.4
0.5
0.6
0.7
0.8
0 0.05 0.1 0.15 0.2 0.25M
ino
r P
ois
son
’s R
atio
Degree of Crosslinking
SWNT arrayMWNT arraySWNT bundle
0.25
0.3
0.35
0.4
0.45
0 0.05 0.1 0.15 0.2 0.25
Ma
jor
Po
isson
’s R
atio
Degree of Crosslinking
Results
Poisson’s Ratios
• Major Poisson’s ratio largest around 7% crosslinking
• MWNT array resists deformation of the circular
cross-section resulting in lower minor ratios
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SWNT array axial fracture (9% crosslinked)
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MWNT array axial fracture (9% crosslinked)
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SWNT bundle axial fracture (9% crosslinked)
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Results
Specific Ultimate Stress
• Axial specific strength maximized around 4%
crosslinking
• Transverse strength continually improved through
crosslinking
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0 0.05 0.1 0.15 0.2 0.25
Axia
l S
p. U
ltim
ate
Str
ess
(GP
a/(
g/c
m3)
Degree of Crosslinking
SWNT arrayMWNT array
SWNT bundle
4
6
8
10
12
14
16
18
0 0.05 0.1 0.15 0.2 0.25T
ran
s. S
p. U
ltim
ate
Str
ess
(GP
a/(
g/c
m3)
Degree of Crosslinking
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Conclusions
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0 10 20 30 40 50 60 70
Axial
Trans.Sp
. M
od
ulu
s (
GP
a/(
g/c
m3))
Ultimate Sp. Strength (GPa/(g/cm3))
SWNT array
MWNT array
SWNT bundle
AC 2.37 g/cm3
AC 2.82 g/cm3
AC 3.35 g/cm3
Pure CNT array
Multiple data points for each system reflect impact of crosslinks to matrix
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Summary
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0 10 20 30 40 50 60 70
Axial
Trans.Sp
. M
od
ulu
s (
GP
a/(
g/c
m3))
Ultimate Sp. Strength (GPa/(g/cm3))
SWNT array
MWNT array
SWNT bundle
AC 2.37 g/cm3
AC 2.82 g/cm3
AC 3.35 g/cm3
Pure CNT array
Increasing crosslinking
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Multiple data points for each system reflect impact of crosslinks to matrix
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Summary
SWNT vs MWNT– Interface templating has a substantial impact on the matrix properties,
and SWNTs maximize the surface area per CNT mass
– Inner MWNT walls reinforce the circular cross section
Arrays vs bundle– Very weak bonding within bundle reduces the properties that require
transferring load through the bundle
Crosslinking– Crosslinks decrease axial specific modulus, increase transverse
modulus
– Axial specific ultimate strength is maximized around 4% crosslinking
– Transverse specific ultimate strength is continually increased with crosslinking
– Crosslinking may inhibit void nucleation at the CNT/matrix interface
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Acknowledgements
NASA Langley Research Center
- Mia Siochi
- LaRC Nano Incubator Team
Michigan Technological University
- Matthew Radue
- S. Gowtham
- Cameron Hadden
Pennsylvania State University
- Adri van Duin (Penn. State)
- Sriram Srinivasan (Penn. State)
NASA Langley Research CenterFunded in part by
Revolutionary Technological Challenges Program (GRANT NNX09AM50A )
SUPERIOR, a high-performance computing cluster at
Michigan Technological University, was used in
obtaining some of results
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Questions
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Supplemental Slides
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Results
0
15
30
45
60
75
0 0.075 0.15 0.225 0.3 0.375
a)
Sp
. S
tre
ss (
GP
a/(
g/c
m3)
True Strain
Exterior CNTsInterior CNTs
Composite
0
15
30
45
60
75
0 0.075 0.15 0.225 0.3 0.375
b)
Sp
. S
tre
ss (
GP
a/(
g/c
m3)
True Strain
Individual CNT stress-strain responses
within the maximally crosslinked systemsMWNT array SWNT bundle
• Exterior/functionalized CNTs fracture earlier than
interior/unfunctionalized
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Results
0
10
20
30
40
50
60
70
0 50 100 150 200 250
a)
Sp
. S
tre
ss (
GP
a/(
g/c
m3))
Time (ps)
CNTAC
CompositeUltimate
0 50 100 150 200 250
b)
Time (ps)
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70c)
Sp
. S
tress (
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a/(
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d)
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0 0.075 0.15 0.225 0.3 0.375
e)
Sp
. S
tre
ss (
GP
a/(
g/c
m3))
True Strain
0 0.075 0.15 0.225 0.3 0.375
f)
True Strain
Axial stress-strain response
SWNT
array
MWNT
array
SWNT
bundle
Uncrosslinked Maximum crosslinking
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Results
0
5
10
15
20
0 100 200 300 400 500
a)
Sp
. S
tress (
GP
a/(
g/c
m3))
Time (ps)
0 100 200 300 400 500
b)
Time (ps)
0
5
10
15
20c)
Sp
. S
tress (
GP
a/(
g/c
m3))
d)
CNTAC
CompositeUltimate
0
5
10
15
20
0 0.15 0.3 0.45 0.6 0.75
e)
Sp
. S
tre
ss (
GP
a/(
g/c
m3))
True Strain
0 0.15 0.3 0.45 0.6 0.75
f)
True Strain
Transverse specific stress-strain response
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