Abstract

The intrinsic feature of graphene honeycomb lattice is defined by its chiral index (𝑛,𝑚), which can be taken into account when using molecular dynamics. However, how to introduce the index into the continuum model of graphene is still an open problem. The present manuscript adopts the continuum shell model with single director to describe the mechanical behaviors of graphene. In order to consider the intrinsic features of the graphene honeycomb lattice—chiral index (𝑛,𝑚), the chiral-tube vectors of graphene in real space have been used for construction of reference unit base vectors of the shell model; therefore, the formulations will contain the chiral index automatically, or in an explicit form in physical components. The results are quite useful for future studies of graphene mechanics.

1. Introduction

A one-atom-thick layer of graphite called graphene is the “mother” of all graphitic forms. Graphene is a 2D building material for carbon materials of all other dimensionalities. It can be wrapped up to 0D buckyballs, rolled into 1D nanotubes, or stacked into 3D graphite [13]. Figure 1 is a famous picture take on from [3].

The graphene has attracted attention because of its unusual two-dimensional structure and potential for applications. Owing to its exceptional mechanical properties and low mass density, graphene is an ideal material for use in nanoelectromechanical systems (NEMS), which are of great interest both for fundamental studies of mechanics at the nanoscale and for a variety of applications, including force, position, mass, and gas sensing [4].

Graphene research has developed at a truly relentless pace. Several papers appear every day; comprehensive reviews have been done by the graphene pioneers [2, 3]. Geometrically, the graphene can be considered as an “almost” 2D material due to its very small thickness at only one-atom. The 2D feature of the graphene makes it possible to directly use well-formulated 2D continuum shell model to simulate its deformation, vibration, and buckling [13].

Although many features of the graphene can be described by relativistic quantum mechanics and molecular dynamics, the continuum modeling is still useful and crucial for rational device design and interpretation of experimental results. Because experiments at the nanoscale are extremely difficult and atomistic modelling remains prohibitively expensive for large-sized atomic system, it has been accepted that continuum models will continue to play an essential role in the study of carbon nanotube [5]. The validity of using continuum models for nanotube and graphene has been supported by both experimental results and molecular-dynamics simulation, all previous investigations on nanotube have indicated that the laws of continuum mechanics are still valid to some extent even in nanoscale. The success of continuum models to nanotube gives us confidence to predict that contunuum modelling is going to be also valid for graphene mechanics analysis [6, 7].

Within the frame of classic continuum mechanics, there is a well-formulated branch-theory of shell [814]. It deals with a special 3D continuum shell; its thickness is very much smaller than its width and length. The deformation of the thinner 3D shell can be considered as a 2D middle surface with a small thickness, and all off-middle surface quantities can be presented in terms of middle surface. In this way, the 3D thinner shell problem is being converted into a 2D surface problem with a small thickness. Based on this understanding, it is to believe that the shell theory should be the best continuum mechanics model for graphene mechanics.

Regarding the mechanics modeling of the graphene, most of literature considered the graphene as a 2D pre-stretched membrane with zero thickness [1518], and some considered the graphene bending properties [1922]. Since monolayer graphene is very thin, to some extent the membrane theory could be very simple and quite good estimate model, but for tiny and delicated NEMS devices, any small thing must be taken into account as it might has a significant impact on graphene, for instance, graphene’s thickness [3, 6].

Although graphene’s thickness is very small, one layer graphene thickness is 0.335 nm [5], but it cannot be ignored as zero, because the thickness plays a key role to supply a bending stiffness. The graphene should be modelled as a very thinner 3D object by shell theory [814].

The current shell theory [814] can be directly applied to the deformation analysis of nanostructures, for instance, [7, 22]. Reference [22] considered the effects of surface tension on the elastic properties of nanostructures, and [7] discussed a promised nanomaterials nanotorus. However, how to introduce the chiral index (𝑛,𝑚) into continuum model of the graphene is still an open problem. The present manuscript adopts the continuum shell model with single director to describe the mechanical behaviors of graphene. In order to consider the intrinsic features of the graphene honeycomb lattice-chiral index (𝑛,𝑚), the chiral-tube vectors of graphene in real space have been used for construction of reference unit base vectors of the shell model; therefore, the formulations will contain the chiral index automatically, or in explicit form in physical components. The results are quite useful for future studies of graphene mechanics.

The paper is organized as follows. Some elasticity concepts and kinematics of a deformable surface will be introduced in Section 2; the parameterization of single director shell and deformation mode will be demonstrated in Sections 3 and 4. The basis vectors will be established in Section 5. The deformation gradient for both with and without predeformation will be formulated in Sections 6 and 7. The explicit form of the chiral index (𝑛,𝑚) in the physical components will be shown in the Section 8.

2. Some Elasticity Concepts

2.1. Configuration, Deformation, and Parametrization

Let 𝐵 represent the stress-free or reference placement of the physical body with boundary 𝜕𝐵. Points of B are indentified by 𝐗𝐵. Let B be parametrized by the one to one point mapping function Φ, such that 𝐵={𝐗=Φ(𝜉1,𝜉2,𝜉3)𝑅3(𝜉1,𝜉2,𝜉3)Ω} where Ω𝑅3 2 is the parametric image of the body under the inverse mapping Φ1. Denote the deformed configuration of the body by 𝑆 with the boundary of 𝑆 given by 𝜕𝑆. Points in S are identified by 𝐱𝑆. The time-dependent configurations are parametrized by one to one point mapping function Φ, such that 𝑆={𝐱=Φ(𝜉1,𝜉2,𝜉3,𝑡)𝑅3(𝜉1,𝜉2,𝜉3)Ω,𝑡[0,𝑇],𝐱𝜕𝑑𝑆=𝐱} where Φ(𝜉1,𝜉2,𝜉3,𝑡)𝑡=0Φ0(𝜉1,𝜉2,𝜉3) and 𝐱 is the prescribed placement of points on the boundary 𝜕𝑑𝑆 where the placement is given. The deformation mapping 𝝌𝐗𝐵𝐱𝑆 is given parametrically by 𝝌(𝐗,𝑡)=ΦΦ01.  Note that 𝝌(𝐗,0)=𝟏 is the identity mapping.

2.2. Tangent Basis Vectors and the Deformation Gradient

By differentiating the mapping function 𝐱 with respect to curvilinear coordinate (convected coordinate) function 𝜉𝑖(𝑖=1,2,3), the tangent basis vectors are obtained 𝐠𝑖(𝜉1,𝜉2,𝜉3,𝑡)=𝐱,𝑖(𝜉1,𝜉2,𝜉3,𝑡). The fact that the tangent basis vectors are linearly independent is expressed by the relationship 𝐠1(𝐠2×𝐠3)>0. The reference or undeformed tangent basis vectors 𝐆𝑖 are obtained by particularizing the current basis vectors to 𝑡=0, hence 𝐆𝑖=𝐗,𝑖(𝜉1,𝜉2,𝜉3). The dual basis vectors 𝐠𝑖 and 𝐆𝑖 are defined by the orthogonality condition 𝐠𝑖𝐠𝑗=𝛿𝑖𝑗, 𝐆𝑖𝐆𝑗=𝛿𝑖𝑗. The deformation gradient is the mapping 𝐅𝑅3𝑅3 and is obtained by taking the material gradient of the deformation mapping 𝝌 as 𝐅=𝑇𝝌GL+(3), where GL+(3)={𝐅𝑅3×3det(𝐅)>0}. In terms of the parametrization, F is given by 𝐅=𝑇𝝌=Δ𝐱Δ𝐗1. Using the above relations, the deformation gradient F can be given in terms of the current tangent basis vectors and the reference dual basis vectors by 𝐅=𝐠𝑖𝐆𝑖or in a coordinate format as 𝐅=𝐹𝑖𝐽𝐠𝑖𝐆𝐽, where 𝐹𝑖𝐽=𝜕𝑥𝑖/𝜕𝑋𝐽, with relations 𝐅𝑇=𝐆𝑖𝐠𝑖, 𝐅1=𝐆𝑖𝐠𝑖, and 𝐅𝑇=𝐠𝑖𝐆𝑖. Then, the determinant of the deformation gradient 𝐽 is given by 𝐽=det𝐅=𝑗/𝑗0, 𝑗=detΔ𝐱=𝐠1(𝐠2×𝐠3), 𝑗0=detΔ𝐗=𝐆1(𝐆2×𝐆3). Since the current and reference tangent basis vectors are linearly independent, so have 𝑗0>0,𝑗>0,𝐽>0.

3. Parameterization of Graphene Shell Model

The variable pair (r, d) is chosen normally as kinematic variable, in which r is the position vector and d is the director field of mid-surface. Since they are vectors, so the calculations corresponding to these quantities also operate in vector space.

The reasonable parameterization of director field plays a central role in development of shell models. The director field is decomposed into a positive magnitude parameter 𝜆 and the inextensible component or unit director field t, 𝐝=𝜆𝐭, where 𝜆=|𝐝|, 𝐭𝐭=1, 𝑡=𝐝/𝜆. The unit director field t is parameterized by two independent angles, that is, 𝐭=𝐭(𝜓1,𝜓2)={sin𝜓1cos𝜓2sin𝜓1sin𝜓2cos𝜓1}. The advantage of this kind of representation of t is that the variational calculation is very simple, for instance, 𝛿𝐭=𝐭,1𝛿𝜓1+𝐭,2𝛿𝜓2.

4. Single Director Kinematic Modelling of Graphene

The variable pair (r, d) is chosen normally as kinematic variable, in which r is the position vector and d is the director field of deforemed mid-surface and denoting R and D being the position vector and single director on the middle surface of undeformed configuration.

According to the long tradition of shell research [814], the single director field in reference or undeformed configuration can be written as 𝜉𝐗=𝐑1,𝜉2𝜉,𝑡+𝜉𝐃1,𝜉2,𝑡.(1) The single director field in current configuration can be written as 𝜉𝐱=𝐫1,𝜉2𝜉,𝑡+𝜉𝐝1,𝜉2,𝑡.(2) Thus, the points in the body are indentified as the mid-surface mapping r or R plus the distance 𝜉 along the director d or D.

The deformation mode of shell is such that points intially defined along straight fibers, that is, indentified as the distance 𝜉 above or below the mid-surface along the line defined by the initial director D, remain a straight fibers. From the physical point of view, the solution to the shell problem, under the single director kinematic assumption, can be considered as the solution for the shell mid-surface plus the solution for the director which orients points along thickness fibers.

Let us now check, from geometric understanding, whether the single director kinematic assumption could capture the main characteristics of shell deformation. Finite membrane stretch is captured by the deformation of the mid-surface map r; finite bending strains are modeled by the spatial gradient of the director d; transverse shear strain is accounted for by measuring the relative rotation of the director d with respect to the normal to the mid-surface. The thickness change can be represented by the difference of magnitude of initial and current director.

5. Establishment of Unit Base Vectors in the Reference State (Undeformed Graphene Sheet)

The way the graphene sheet is wrapped is represented by a pair of indices (𝑛,𝑚) called the chiral vector. The integers 𝑛 and 𝑚 denote the number of unit vectors along two directions in the honeycomb crystal lattice of graphene. If 𝑚=0, the nanotubes are called “zigzag”. If 𝑛=𝑚, the nanotubes are called “armchair”. Otherwise, they are called “chiral”.

The orthogonal base vectors in the reference state of the grapheme can defined as follows: let a 1 be a base vector e 1, normal base vector of the grapheme plane is 𝐞3=𝐚1×𝐚2/|𝐚1×𝐚2|=(2/3)(𝐚1×𝐚2), and then 𝐞2=(2/3)𝐚2(1/3)𝐚1. The chiral vector 𝐂 can be expressed as follows in terms of orthogonal base vectors: 𝐂=(𝑛+(3/2)𝑚)𝐞1+(3/2)𝑚𝐞2. The tube axes vector T is orthogonal to the chiral vectors, that is, 𝐓𝐂=0, then we have 𝐓=(3/2)𝑚𝐞1(𝑛+(3/2)𝑚)𝐞2.The no-orthogonal base vectors {𝐚1,𝐚2,𝐞3}can be represented by orthogonal base vectors {𝐞1,𝐞2,𝐞3}.

Since T and 𝐂 are orthogonal each other, we can form another chiral-tube base vectors {𝐂,𝐓,𝐄3}, where the normal vector or single director field in undeformed grapheme plane is 𝐄=𝐂×𝐓=(𝑛2+𝑚3)𝐞3.

Up to now, from unit vectors of grapheme in real space, we have formulated two base vectors {𝐞1,𝐞2,𝐞3} and {𝐂,𝐓,𝐄}. In order to capture more information about the deformed grapheme sheet, we will try to formulate its shell model based on the chiral-tube base vectors{𝐂,𝐓,𝐄}; this work has not been found in the literature. For tensor calculation, we introduce 𝐄𝑖 to represent the chiral-tube base vectors as follows: 𝐄1=𝐂,𝐄2=𝐓,𝐄3=𝐄.(3) Corresponding to the chiral-tube unit base vectors {𝐂,𝐓,𝐄}, we can define three axes 𝜉𝑖(𝑖=1,2,3), for instance, the any point in the graphene plane can be expressed as follows: 𝜉1𝐂+𝜉2𝐓=𝜉1𝐄1+𝜉2𝐄2 and any point out of the graphene plane is 𝜉2=𝜉1𝐄1+𝜉2𝐄2+𝜉𝐄.

6. Tangent Basis and Deformation Gradient of Graphene without Predeformation

If the grapheme sheet has no any predeformation, it will be like a plane. Since 𝐄,𝛼=𝜕𝐄/𝜕𝜉𝛼=0, we have the tangent basis vectors in the undeformed configuration as follows: 𝐆𝛼=𝐄𝛼,𝐆3=𝐄3.(4) After the deformation, the convected tangent basis vectors in current graphene shell configuration is defined by 𝐠𝛼=𝐱,𝛼=𝐫,𝛼+𝜉𝐝,𝛼,𝐠3=𝐱,𝟑=𝐝.(5) The dual basis vectors are also defined by the relationships 𝐠𝑖𝐠𝑗=𝛿𝑖𝑗 and 𝐄𝐼𝐄𝐽=𝛿𝐼𝐽.

Then, tangent of deformation or deformation gradient F can be defined by 𝐅=𝐠𝑖𝐆𝑖=𝐫,𝛼𝐄𝛼+𝐝𝐄3+𝜉𝐝,𝛼𝐄𝛼.(6) If we put 𝜉=0 in (5), then the basis vectors of the mid-surface in the current configuration can be obtained; 𝐚𝑖=𝐠𝑖𝜉=0 that is, 𝐚𝛼=𝐫,𝛼,𝐚3=𝐝,(7) and the corresponding dual basis vectors in the mid-surface are defined by 𝐚𝑖𝐚𝑗=𝛿𝑖𝑗.

7. Deformation Gradient of Graphene with Pre-Deformation

If 2D graphene is being wrapped up to 0D nanodot, 1D nanotube, 3D stacked graphite, or been prestressed and then undergo deformation, it means that the graphene got pre-deformation.

After the pre-deformation, the convected tangent basis vectors in predeformation configuration are defined by 𝐆𝛼=𝐗,𝛼=𝐑,𝛼+𝜉𝐃,𝛼,𝐆3=𝐗,3=𝐃.(8) The dual basis vectors are also defined by the relationships 𝐆𝑖𝐆𝑗=𝛿𝑖𝑗.

The predeformation gradient 𝐅prewill be 𝐅pre=𝐆𝑖𝐆𝑖=𝐑,𝛼𝐄𝛼+𝐃𝐄3+𝜉𝐃,𝛼𝐄𝛼.(9) The after deformation gradient 𝐅def will be 𝐅after=𝐠𝑖𝐆𝑖=𝐫,𝛼𝐆𝛼+𝐝𝐆3+𝜉𝐝,𝛼𝐆𝛼.(10) According to the superposition of deformation gradient, the total deformation gradient will be 𝐅Total=𝐅def𝐅pre=𝐠𝑖𝐆𝑖𝐆𝑖𝐆𝑖=𝐠𝑖𝐆𝑖=𝐫,𝛼𝐄𝛼+𝐝𝐄𝟑+𝝃𝐝,𝛼𝐄𝛼.(11) The associated Jacobian determinants are given by 𝑗𝐽=det(𝐅)=𝑗0,𝑗=𝐠1×𝐠2𝐠3,𝑗0=𝐄1×𝐄2𝐄3,(12) and from (8) and (9), and if we denote the director field gradient as 𝐝,𝛼=𝜅𝛽𝛼𝐚𝛽+𝜅3𝛼𝐝,𝐃,𝛼=𝐾𝛽𝛼𝐀𝛼+K3𝛼𝐃.(13) then, we have ̂𝑗𝑗=1+2𝜉+𝜉2𝜅,̂𝑗=𝑗𝜉=0=𝐫,1×𝐫,2𝐝,̃𝑗𝑗=1+2𝜉𝐻+𝜉2𝐾,̃𝑗=𝑗𝜉=0=𝐑,1×𝐑,2𝐃,(14) where =(1/2)(𝜅11+𝜅22),𝜅=𝜅11𝜅22𝜅12𝜅21 can be thought of as the mean and Gaussian curvature in the deformed configuration, and 𝐻=(1/2)(𝐾11+𝐾22),𝐾=𝐾11𝐾22𝐾21𝐾12 can be thought of as mean and Gaussian curvature in the pre-deformation configuration. Since no deformation in the undeformed graphene plane exists, so both its mean and Gaussian curvature are zero.

For instance, the cylindrical pre-deformation [21],𝑥1=𝑅sin(2𝜋(𝑋1/𝐿)),𝑥2=𝑋2,𝑥3=𝑅𝑅cos(2𝜋(𝑋1/𝐿)), where L is the width of the grapheme sheet before rolling and R is the nanotube radius. The pre-deformation gradient in this case is 𝐅pre=2𝜋𝑅𝐿𝑋cos2𝜋1𝐿02𝜋𝑅𝐿𝑋sin2𝜋1𝐿010.(15)

8. Physical Components of Some Quantities in Terms of Chiral Index (𝑛,𝑚)

The chiral index (𝑛,𝑚) is an intrinsic parameter of graphene. With our chiral-tube basis vectors, the influence of the chiral index (𝑛,𝑚) has been introduced into deformation gradient and can be shown explicitly in physical components.

Before going to discuss the physical components of tensor, let us here make a remark about the physical components of physical quantities. We should remember that the tensor (vector) components of a physical quantity which is referred to a particular curvilinear coordinate system may or may not have the same physical dimensions. In this case a great convenience arises because we would like to keep our freedom in choosing arbitrary curvilinear coordinates. For this reason, we must distinguish the tenos components from the “physical components”, which must have uniform physical dimensions, but they do not transfer conveniently under coordinate transformations.

First of all, let us consider the physical components of a vector 𝐮=𝑢𝑖𝐠𝑖=𝐮𝑖𝐠𝑖. It is clearly that the base vectors 𝐠𝑖and𝐠𝑖 are in general not unit vectors. In fact, their lengths are |𝐠𝑖|=𝐠𝑖𝐠𝑖=𝑔𝑖𝑖,|𝐠𝑖|=𝐠𝑖𝐠𝑖=𝑔𝑖𝑖, i not in summation. Then ̂𝐠𝑖=𝐠𝑖/𝑔𝑖𝑖,̂𝐠𝑖=𝐠𝑖/𝑔𝑖𝑖 are unit vectors. With the notation of the unit vectors, the vector can be rewriten as 𝐮=𝑢𝑖𝐠𝑖=𝑢𝑖𝑔𝑖𝑖̂𝐠𝑖̂𝑢𝑖̂𝐠𝑖=𝑢𝑖𝐠𝑖=𝑢𝑖𝑔𝑖𝑖̂𝐠𝑖̂𝑢𝑖̂𝐠𝑖,(16) where ̂𝑢𝑖=𝑢𝑖𝑔𝑖𝑖,̂𝑢𝑖=𝑢𝑖𝑔𝑖𝑖 will have the same physical dimensions. It is seen that ̂𝑢𝑖 are the components of v resolved in the direction of unit vectors ̂𝐠𝑖 which are tangent to the coordinate lines, and that ̂𝑢𝑖 are the components of u resolved in the direction of unit vectors ̂𝐠i which are perpendicular to the coordinate planes. So the components ̂𝑢𝑖and̂𝑢𝑖 are called the physical components of the vector u, and ̂𝐠𝑖̂𝐠and𝑖 are physical base vectors. This means that that the physical components of a vector u can be defined as the components of u resolved in the directions of a set of unit vectors which are parallel either to the set of base vectors or to the set of reciprocal base vectors.

Similarly, for the reference or undeformed state, then 𝐄𝑖=𝐄𝑖/𝐺𝑖𝑖,𝐄𝑖=𝐄𝑖/𝐺𝑖𝑖. For tensor calculation, we define the chiral-tube unit physical base vectors as 𝐄1=𝐂||𝐂||,𝐄2=𝐓||𝐓||,𝐄3=𝐄3||𝐄3||,(17) where |𝐂|=𝐂𝐂=(𝑛+(3/2)𝑚)2+((3/2)𝑚)2, |𝐓|=(𝑛+(3/2)𝑚)2+((3/2)𝑚)2, and |𝐄3|=(𝑛2+𝑚3). It is indicated in (14) that chiral index has been included into the physical components of base vectors. Since all quantities and variables must be established on the base vectors, all of them will be represented by the chiral index. This is the beauty of this work. For “zigzag” with 𝑚=0, we have 𝐄1=𝐂𝐄/𝑛,2𝐄=𝐓/𝑛,3=𝐄3/𝑛2; for “archair” with 𝑛=𝑚, we have 𝐄1=2𝐂𝑛7+23,𝐄2=2𝐓𝑛7+23,𝐄3=𝐄3𝑛21+3.(18)

Using the above physical component in (14), for instance, the 2nd Piola-stress tensor of the shell model can be written in physical component form: 𝐒=𝐽𝐅1𝝈𝐅𝑇=𝐽𝜎𝑖𝑗𝐄𝑖𝐄𝑗=𝐽𝜎𝑖𝑗𝐸𝑖𝑖𝐺𝑗𝑗𝐄𝑖𝐄𝑗𝑆𝑖𝑗𝐄𝑖𝐄𝑗.(19) Similarly, all other quantities can be explicitly expressed in terms of the chiral index (𝑛,𝑚).

9. Conclusion

This paper investigates the possibility of introducing the chiral index (𝑛,𝑚) into the deformation formulation of graphene continuum shell model. For this purpose, we established a chiral-tube basis vectors from graphene unit vectors in real space and formulated graphene deformation gradient for both with and without predeformation. The importance of the chiral index on the deformation and stress has been shown explicitly in the physical components.

Acknowledgments

This work was supported by South Africa National Research Foundation. This support is gratefully acknowledged. The author would like to express his thankfulness to the constructive comments and insightful suggestions given by three anonymous referees.