RESEARCH ARTICLE
Copyright © 2013 American Scientific Publishers
All rights reserved
Printed in the United States of America
Journal of
Computational and Theoretical Nanoscience
Vol. 10, 470–480, 2013
Molecular Dynamic Simulations of Pristine and
Defective Graphene Nanoribbons Under Strain
Burcu Tüzün1 and Şakir Erkoç1 2 ∗
1
Department of Micro and Nano Technology, Middle East Technical University, Ankara 06531, Turkey
2
Department of Physics, Middle East Technical University, Ankara 06531, Turkey
Structural properties of pristine and defective graphene nanoribbons have been investigated by
stretching them under 5 percent and 10 percent uniaxial strain until the nanoribbons fracture. The
stretching process have been carried out by performing molecular dynamics simulations at 1 K
and 300 K to determine the temperature effect on the structure of the graphene nanoribbons.
Results of the simulations indicated that the conformation of the initial graphene nanoribbon model,
temperature, and stretching speed have a considerable effect on the structural properties, however
they have a slight effect on the strain value. The maximum strain at which fracture occurs is found
to be 46.41 percent for zigzag 8 layer pristine graphene nanoribbon at 1 K and fast stretching
process. On the other hand, the defect formation energy is strongly affected from temperature and
nanoribbon type. Stone-Wales formation energy is calculated to be 1.60 eV at 1 K whereas 30.13 eV
at 300 K for armchair graphene nanoribbon.
Keywords: Monovacancy, Divacancy, Stone Wales Defect, Carbon Nanosheet, Graphene,
Nanoribbon, Molecular Dynamics Simulations, Atomistic Potential.
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1. INTRODUCTION
Carbon is an important element in nanoscale because of its
capability of forming different low dimensional structures
such as graphene (2D), carbon nanotubes (CNT) (1D), and
fullerenes (0D) which have superior physical properties.1
A graphene layer is composed of sp2 hybridized carbon
atoms.2
Until 2004, it was thought that films with thickness at nanometer scale are thermodynamically unstable.
However, in 2004, Novoselov and coworkers3 were able to
prepare single layer graphene. Since the isolation of either
single or a few atom thickness graphene layers, it and
its applications arouse interest among scientists because
of its novel properties.4 2D graphene layer can be considered as a building block of different carbon structures.
For example, by rolling the graphene layer and in turn,
creating carbon nanotubes (CNT),1 by wrapping graphene
and forming spherical buckyballs and by putting them one
after the other, graphite can be obtained.4 The popularity
of 2D graphene layer comes from its unique electronic
properties, and there are lots of studies about the electrical
properties of them in literature.5–8 However, mechanical
strength of graphene is also marvelous.9 The study carried
∗
Author to whom correspondence should be addressed.
470
J. Comput. Theor. Nanosci. 2013, Vol. 10, No. 2
by Lee et al. showed that the breaking strength of graphene
is 200 times larger than that of steel.10 It is obvious that
the strength of graphene depends on the number and types
of defects and also edge termination.
There are different types of defects such as dopinginduced defects caused by substitution of non-carbon
atoms in graphene sheet, structural defects, grain boundary
defects, bond rotation defect and non-sp2 carbon defects
resulted by dangling bonds.1 Apart from mechanical
strength, defects also play a crucial role in physicochemical
properties, chemical activity, structure, topology, cavity,1
optical, electronic and thermal properties.2 Moreover, conductance and ductility of graphene based devices are controlled by defect characteristic of graphene. In other words,
structural defects in graphene layer appear during processing or growth has a great effect on the performance
of the graphene based devices. Because of this structural
defects, graphene based devices may lose their functional
quantity or gain superior or new functionalities depending on type, location or size of the defects. For example, graphene is generally used to enhance and improve
the strength of composites. However, research carried out
by Bartolucci and coworkers11 showed that the strength
of graphene-aluminum composites is lower than that of
pure aluminum and aluminum-carbon nanotube composites. The lower mechanical strength is explained by the
1546-1955/2013/10/470/011
doi:10.1166/jctn.2013.2721
Tüzün and Erkoç
Molecular Dynamic Simulations of Pristine and Defective Graphene Nanoribbons Under Strain
Fig. 1. Zigzag and armchair graphene nanoribbon models. The number of layers (L) define the width of the nanoribbon.
J. Comput. Theor. Nanosci. 10, 470–480, 2013
471
RESEARCH ARTICLE
defects which become reaction sites with aluminum and
result in significant amount of aluminum carbide (Al4 C3 )
as points of weakness.11 In some cases, defected graphene
is favorable such as earth metal dispersion on graphene
layer and hydrogen adsorption. Hydrogen has very limited
interaction with graphene12 which results in using metals such as lithium or palladium to adsorb or decompose
hydrogen for sensing.12 13 Metal atoms such as lithium
binding on graphene vacancies with energy higher then
cohesive and cluster forming energy are the active side
for hydrogen adsorption.13 The structure is also affected
from defect due to different hybridization ability of carbon atoms which cause different stable structure such
as carbyne or graphite. Moreover, the flat structure of
graphene layer may be deformed due to non-hexagonal
carbon arrangements when polygons can not satisfy symmetry rules. This local curvature allow reactivity and
Fig. 2. Types of defects in graphene nanoribbons.
adsorption.2
The importance of graphene comes from its large applienergy generation devices due to its electro-catalytic activcation areas. For example, graphene is a very good choice
ity, enzymatic binding capacity, unique electrical propfor fabrication of ultrafast transistors because of its abilerties and low production cost. It can also be possible
ity of outstanding electron transport at room temperature.
to detect the bio-molecules, drugs, heavy metals or catGraphene is also preferred in the biosensors and chemical
alytic surfaces by the help of the presence of the defects
sensors because of its low capacitance resulting in low sigor dopants. However, knowing information concerning
nal to noise ratio, and rapid electron transfer resulting in
defects is crucial to control chemical, electronic, mechanaccurate and selective detection of biomolecules.14 Some
ical and magnetic properties of graphene.1
robust polymer composites (poly-vinyl-alcohol/graphene),
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present study, 2D graphene nanoribbon (GNR) in
high electrical conducting (polystyrene/graphene),
high Tue, 14 Jun
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2016 15:30:28
two
different
geometries, which are zigzag and armchair
thermal conducting polymers (epoxy resins/graphene
comCopyright: American Scientific Publishers
models, have been studied. The GNR models considered
posites) and more thermally stable polymers can be proare shown in Figure 1.
duced by using graphene as fillers during fabrication.15
Although the electronic properties of GNR have been
Moreover, using graphene instead of CNT decrease the
studied extensively, there are limited information in the
production cost and difficulties that stem from reliabilliterature about the mechanical properties of GNRs. The
ity problem due to chirality of CNT.12 15 Graphene is
structural defects considered in the present work, which
suitable to be used as electrode material in capacitors16
are monovacancy, divacancy and Stone-Wales defects, are
and lithium-ion batteries17 because its wide surface area
presented in Figure 2. The other property of defects is
(2630 m2 g−1 ), high electrical conductivity (64 mS cm−1 ),
mobility. Defects are not stationary, they have a certain
stability over vast range of temperature and high elecmobility parallel to the graphene plane. The characteristic
tron mobility (2 × 105 cm2 V−1 s−1 at electron densities
of migration depends on types of defects and temperature.2
of 2 × 1011 cm−2 for 150 nm graphene nano sheet above
In the present simulations the migration of defects have
Si/SiO2 gate) make the graphene a good choice for energy
storage.4 Apart from these, graphene is preferred also in
been also investigated.
Molecular Dynamic Simulations of Pristine and Defective Graphene Nanoribbons Under Strain
RESEARCH ARTICLE
2. METHOD OF CALCULATIONS
Tüzün and Erkoç
3. RESULTS AND DISCUSSION
Molecular dynamics (MD) method, known since 1960, is
The calculated formation energies Efe of the monovacancy,
a very powerful technique to study the materials propdivacancy and Stone-Wales defects for zigzag and armchair
erties at nanoscale. Many interparticle interactions are
GNRs are given in Tables I and II, respectively. Defect fortaken into account by MD technique which can not be
mation energy Efe is defined by the differences between the
ignored at nanoscale as done at macroscale.18 In the
total energies of the pristine and defective GNR with the
present study classical molecular dynamics simulations
condition that they have the same width, length and edge
(MDS) have been performed in a canonical ensemble
form. Namely Efe = ETp − ETd , where ETp is total energy
system to investigate the structural properties of GNRs.
of pristine GNR, and ETd is the total energy of defective
According to canonical ensemble, the temperature is taken
GNR. The formation energies give the information about
as constant and the number of particles is also conthe tendency of the defect formation on the GNRs and stastant. The Verlet algorithm is used for time integration
bility. Defects with low formation energies are more stable
and velocity calculations. The interaction between partithan defects with high formation energies.20 DFT calcucles are calculated according to Tersoff potential energy
lation results for defect formation energies for CNTs and
function parameterized for carbon.19 MDSs have been
graphene sheets are available in the literature.21–23 The
carried out at 1 and 300 K in order to understand the
present results may not be compared with the literature
effect of temperature on the defect mobility and fracture
values because of the definitions of the defect formation
mechanism.
energies and also the different method of calculations.
Before the stretching process, an appropriate working
As seen from Tables I and II the defect formation enercell has been generated by defining the initial position of
gies are different for each defect. Defect formation enercarbon atoms. Periodic boundary conditions are applied in
gies at 1 K for zigzag GNRs are calculated as 21.47, 26.94
the direction which the stretching process is carried out.
and 31.87 eV for monovacancy, Stone-Wales and divaMD relaxation was carried out until the total energy of
cancy defects, respectively. From these values, at 1 K for
the system becomes constant with respect to time. This
zigzag GNR, the defect type can be put in order from
is when the system gets to the state of equilibrium. 105
more stable to less stable as monovacancy, Stone-Wales
MD steps were enough to reach equilibrium for the models
and divacancy. However, Efe at 300 K for zigzag GNR is
considered in the present study. After Delivered
the systemby
reaches
different
than that of the one at 1 K which affects also
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equilibrium the stretching processIP:
starts
with the extension
between defects. At 300 K, Efe of divaPublishers
of the geometry by 5 percent. At eachCopyright:
stretching American
process, Scientific
cancy (32.58
eV) changes slowly whereas Efe of monothe system was relaxed until equilibrium was reached.
vacancy (44.00 eV) and Efe of Stone-Wales (50.59 eV)
Stretching and relaxation processes have been continued
drastically increase by 104.94 percent and 87.79 percent
until some of the bonds are broken and the nanoribbon
respectively. The change in percentage is calculated as
starts to fracture.
Efe300 K − Efe1 K /Efe1 K × 100, where Efe300 K and Efe1 K are
In the present study GNRs with two different chirality
defect formation energies at 300 K and 1 K, respectively.
(zigzag and armchair) and with different layer (the width
Therefore, at 300 K, divacancy defect on zigzag GNR is
of the nanoribbon) have been studied. To see the effect
more stable than monovacancy and Stone-Wales defects
of the width on the strength of the zigzag model GNRs
which is less stable among them. Defect formation enerwith 4, 5, 6, 7, and 8 layers; and armchair model GNRs
gies are not only affected from temperature but they are
with 6, 7, 8, 9, 10, 11, and 12 layers were generated.
also affected from chirality. At 1 K for armchair GNR,
Because of the limited space in the journal papers we have
formation energy of Stone-Wales defect is calculated as
not included the results of all the models generated. We
1.60 eV which is a much smaller value among all defect
just included the results of the largest models considered,
formation energies.
namely 8 layer model for zigzag GNR and 12 layer model
As seen from Table II at 1 K the most stable defect on
for armchair GNR. The width of the armchair and zigzag
armchair GNR is the Stone-Wales defects which is folGNRs was tried to be kept close to each other by taklowed by monovacancy defect (14.58 eV) and divacancy
ing the models at different layers in order to understand
defect (23.52 eV). At 300 K the Efe of Stone-Wales defect
the chirality effect better. For example, the width of the
on arm-chair GNR increase drastically by 1783.2 percent,
zigzag model with 8 layers is close to the width of the
armchair model with 12 layers as seen from Figure 1. In
Table I. Defect formation energies (Efe , in eV) of zigzag 8 layer
the present study, 8 layer zigzag GNR with 24.60 Å initial
graphene nanoribbons.
length and 12 layer armchair GNR with 42.60 Å initial
Defect type
Efe (at 1 K)
Efe (at 300 K)
length were compared to investigate chirality effect on the
Divacancy
31.87
32.58
strength. In order to eliminate the differences in the initial
Monovacancy
21.47
44.00
length, strain values were compared instead of final length
Stone-Wales
26.94
50.59
at which fracture occurs.
472
J. Comput. Theor. Nanosci. 10, 470–480, 2013
Tüzün and Erkoç
Molecular Dynamic Simulations of Pristine and Defective Graphene Nanoribbons Under Strain
Table II. Defect formation energies (Efe , in eV) of armchair 12 layer
graphene nanoribbons.
J. Comput. Theor. Nanosci. 10, 470–480, 2013
473
RESEARCH ARTICLE
Figure 4 shows the results of the simulations for
the defective armchair GNR models. These results were
obtained at 300 K with slow stretching process. As seen
Defect type
Efe (at 1 K)
Efe (at 300 K)
from the figures, the number of runs are the same for monoDivacancy
2352
55.44
vacancy and divacancy defective armchair GNR. Moreover,
Monovacancy
1458
62.34
the topology or shape of the GNRs is also similar for monoStone-Wales
160
30.13
vacancy and divacancy defective armchair GNR. This is not
expected because the absence of two atoms should have a
but it is still the most stable structure among them. At
more significant effect than that of the absence of one atom.
300 K, Efe of monovacancy (62.34 eV) and Efe of divaOn the other hand, Stone-Wales defective armchair
cancy (55.44 eV) increase by 327.57 percent and 135.71
GNR model is stronger than the other defective modpercent, respectively. At 300 K, monovacancy defect is
els. It is an expected result since in Stone-Wales defect
more stable than divacancy defect as in the case of zigzag
the reason of the defect is not the absence of the atoms
GNR at 300 K. Strain values for zigzag and armchair
but the non-hexagonal rings surrounded by hexagonal carGNRs with monovacancy defect and pristine are listed in
bon rings. Moreover, the non-hexagonal ring changes and
Table III. As seen from this table, the maximum strain
becomes a hexagonal ring during the stretching process.
value is obtained as 46.41 for pristine zigzag GNR at 1 K
As a result of stretching a Stone-Wales defective GNR
under fast stretching process, while the minimum value is
changes to a defect-free GNR, namely Stone-Wales defect
obtained as 21.00 for monovacancy defected zigzag GNR
disappears during streching process. See Figure 4.
at 300 K under fast stretching process. As demonstrated
Figure 5 shows the monovacancy defect structure on
from Table III strain values are affected from temperature.
armchair GNRs under stretch at 1 and 300 K. As seen from
For example, for zigzag GNRs strain values obtained at
the figure, the motion of the monovacancy defect at 300 K
300 K are smaller than that of at 1 K, which is valid also
is more remarkable than that of at 1 K. At 300 K before
for armchair model. However, the temperature effect seems
the stretching process, defects can not be seen clearly from
to be make no difference in the strain values of armchair
figure because defect moves toward the edge (a sort of
GNRs for fast stretching process.
diffusion). During stretching, movement of defect continThe stretching results of the defect free armchair model
ues until bond breaking takes place and the nanoribbon
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at 1 and 300 K can be seen in Figure
3. The by
number
fracture.
The side view of the GNR at 300 K looks more
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of runs, namely a complete stretching
process, are differthan2016
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of GNR at 1 K as a result of temperature
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ent for slow and fast stretching processes. For example,
effect. However, the side view of the GNR at 1 K is almost
for 12 layer armchair model at 1 K, the stretching prosmooth.
cess continues until 6 runs for slow stretching and 3 runs
Figure 6 shows the results of the simulations for armfor fast stretching. It is an expected result since extending
chair GNR with divacancy defects under stretch. The interis 5 percent for slow stretching while 10 percent for fast
esting and more remarkable point in this figure is that the
growing the size of the defect at 1 K is more rapidly and
stretching. From Figure 3 the effect of temperature is also
at the end of the stretching process, the final size of the
seen. At 300 K the topology of the GNRs also changes
defect at 1 K is larger than the size of the defect at 300 K.
during the stretching process.
Figures 7 and 8 display the strain energy, or delta energy
(E) versus strain graph of the Stone-Wales defected armTable III. Calculated strain values for various graphene nanoribbons.
chair GNRs. E is defined as the difference between final
Graphene model and
and initial configuration energies, namely E = Ef − Ei .
defect type
Temperature (K)
Stretching type
Strain
Strain is defined as the percent of the length differences,
zz8L-pristine
1
Slow
40.71
namely Strain = 100 × Li − L0 /L0 , where L0 is initial
zz8L-monovacancy
1
Slow
34.00
length, whereas Li is the length of the nanoribbon at ith
zz8L-pristine
1
Fast
46.41
stretching step or run.
zz8L-monovacancy
1
Fast
33.10
The difference in Figures 7 and 8 is very interesting,
zz8L-pristine
300
Slow
27.63
because
the characteristics of E versus strain show oppozz8L-monovacancy
300
Slow
21.55
zz8L-pristine
300
Fast
33.10
site behaviour at low (1 K) and room temperature (300 K)
zz8L-monovacancy
300
Fast
21.00
cases. That is E versus strain changes rapidly for fast
ac12L-pristine
1
Slow
34.01
stretching case than the slow stretching case at 1 K. On
ac12L-monovacancy
1
Slow
34.01
the other hand, E versus strain changes rapidly for slow
ac12L-pristine
1
Fast
33.10
stretching case than the fast stretching case at 300 K.
ac12L-monovacancy
1
Fast
33.10
The results of the zigzag GNR stretching simulations are
ac12L-pristine
300
Slow
27.62
ac12L-monovacancy
300
Slow
21.55
presented in the Figures 9–13. As seen from the Figure 9,
ac12L-pristine
300
Fast
33.10
the pristine zigzag GNR keeps its structure without deforac12L-monovacancy
300
Fast
33.10
mation and fracture sudenly, then we stop stretching at this
Tüzün and Erkoç
RESEARCH ARTICLE
Molecular Dynamic Simulations of Pristine and Defective Graphene Nanoribbons Under Strain
Fig. 3. Structures of armchair 12 layer defect free graphene nanoribbons under stretch.
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Fig. 4. Structures of defected 12 layer armchair graphene nanoribbons.
474
J. Comput. Theor. Nanosci. 10, 470–480, 2013
Tüzün and Erkoç
Molecular Dynamic Simulations of Pristine and Defective Graphene Nanoribbons Under Strain
RESEARCH ARTICLE
Fig. 5. Structures of 12 layer armchair graphene nanoribbons with monovacancy defect under stretch.
point. The same situation does also hold in the armchair
edge atoms at 1 K and bond breaking takes place. On the
other
hand,
at 300 K, deformation and bond breaking starts
pristine GNR.
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It is interesting to note that the deforFigure 10 shows the zigzag GNRs
with monovacancy.
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mation on
the edge at 1 K starts on the edge which is
As seen from this figure the deformation
starts from
the Scientific
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Fig. 6. Structures of 12 layer armchair graphene nanoribbons with divacancy defect under stretch.
J. Comput. Theor. Nanosci. 10, 470–480, 2013
475
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RESEARCH ARTICLE
Molecular Dynamic Simulations of Pristine and Defective Graphene Nanoribbons Under Strain
Fig. 7. Structures of armchair graphene nanoribbons with Stone-Wales defect under stretch of at 1 K. The graph shows the strain energy (E) versus
strain for the corresponding structures.
parallel to the side of the triangular type monovacancy.
the fixed edges of the GNR for monovacancy, whereas the
On the contrary, the side view of the GNR with monoroughness and/or the wavy character are localized close to
vacancy at 300 K is different from the side view of the
divacancy position.
GNR with divacancy at 300 K. As seen from Figure 10
Figures 12 and 13 display the E versus strain graph
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are localized
at
of
Stone-Wales
defected zigzag GNRs. At 1 K the E
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Fig. 8. Structures of armchair graphene nanoribbons with Stone-Wales defect under stretch of at 300 K. The graph shows the strain energy (E)
versus strain for the corresponding structures.
476
J. Comput. Theor. Nanosci. 10, 470–480, 2013
Tüzün and Erkoç
Molecular Dynamic Simulations of Pristine and Defective Graphene Nanoribbons Under Strain
RESEARCH ARTICLE
Fig. 9. Structures of pristine zigzag graphene nanoribbons under stretch of at 1 K and 300 K.
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Fig. 10.
Structures of zigzag graphene nanoribbons with monovacancy defect under stretch of at 1 K and 300 K.
J. Comput. Theor. Nanosci. 10, 470–480, 2013
477
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RESEARCH ARTICLE
Molecular Dynamic Simulations of Pristine and Defective Graphene Nanoribbons Under Strain
Fig. 11.
Structures of zigzag graphene nanoribbons with divacancy defect under stretch of at 1 K and 300 K.
Fig. 12.
Structures of zigzag graphene nanoribbons with Stone-Wales defect under stretch of at 1 K and 300 K.
478
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Molecular Dynamic Simulations of Pristine and Defective Graphene Nanoribbons Under Strain
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Fig. 13. Structures of zigzag graphene nanoribbons with Stone-Wales defect under stretch of at 300 K. The graph shows the strain energy (E)
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versus strain for the corresponding structures.
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no significant effect on the strain value, whereas it has
versus strain graph for both fast and slow stretching look
great effect on the strain energy. However, the strain value
similar. However, they show different charactheristics at
has been affected from both defect and temperature. The
300 K; the E versus strain is larger for slow stretching
number of runs taken until the fracture takes place for
than that of fast stretching.
zigzag GNR is slightly larger than that of the runs for
armchair GNR which can be concluded as zigzag GNR is
4. CONCLUSIONS
more stable (or stronger) than armchair GNR under strain.
The strength and stability of armchair and zigzag GNRs
Acknowledgment: The authors would like to thank
at two different temperatures have been investigated by
Alper Ince for critically reading the manuscript.
MDS. The result of the simulations were used to calculate strain values and defect formation energies. From
the results of the simulations we can conclude that, at
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Received: 19 December 2011. Accepted: 5 January 2012.
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