# Molecular Dynamics Modeling of the Effect of Nanotwins on the Superelasticity of Single-Crystalline NiTi Alloys

Authors: Yang Guo; Xiangguo Zeng; Huayan Chen; Tixin Han; Heyi Tian; Fang Wang
Journal: Advances in Materials Science and Engineering
 (2017)

---

## Abstract

The objective of this work is to simulate the superelasticity and shape-memory effect in a single-crystalline nickel-titanium (NiTi) alloy through a molecular dynamics (MD) study. Cooling and heating processes for this material are reproduced to investigate the temperature-induced phase transformation in its microstructure. It is found that the martensitic transformation and its reverse process occur accompanied by an abrupt volume change, and the transformed variants lead to the appearance of the (001) type compound twin. In addition, the transform temperatures for martensite start (Ms) and austenite finish (Af) are determined, respectively. The results indicate that when the temperature is beyond Af during the compressive loading-unloading, the superelastic behavior becomes pronounced, which is attributed to the role of nanotwins on the transformation from the austenitic phase (B2) to martensitic phase (B19′). Compared to existing experimental data, a reasonable agreement is achieved through the modeling results, highlighting the importance of the compound twins for dominating the superelasticity of nanostructured NiTi alloys.


---

## Body

## 1. Introduction

Shape-memory alloys (SMAs) have important applications involving miniactuators, microelectromechanical systems, robotics, biomedicine, and even smart clothing [1] because of their ability of recovering their original shape under heating conditions and sustaining large elastic strains. Such two behaviors are recognized as the shape-memory effect (SME) and the superelasticity (SE), respectively. In recent years, these alloy materials are widely accepted and used as a functional material in the field of the automotive and aerospace industries. Among the many different types of SMAs, a nickel-titanium (NiTi) alloy has gained widespread attention owing to its excellent inherent advantages, such as mechanical properties, corrosion resistance, biocompatibility, and phase transformation close to room temperature. There is an evidence that demonstrates that the SME and SE in the NiTi alloy are caused by the martensitic transition (MT) and its reversible one (i.e., austenitic transition (AT)) between cubic B2 (austenite) and monoclinic B19′ (martensite), respectively [2], which are induced by environmental temperature and applied stress. To meet the specific requirements of safe design, whether and how such behaviors occur in very small length scale system are of growing interest.In the last decade, much effort had been focused on investigating the SME and SE in the NiTi alloy at the nanoscale [2]. Based on experimental observations, it was shown that a stress-induced reversible transformation between the two ordered phases resulted in the strain recovery under isothermal conditions [3]. A constitutive law containing the superelastic effect subjected to multiaxial loading was obtained through direct mechanical experiments [4]. In situ X-ray diffraction was employed to record the atomic configuration of phase transformations during tensile loading-unloading [5]. With regard to the temperature-induced phase transformation, the grain size dependence of phase transition temperature was observed through the transmission electron microscopy (TEM) [6]. Besides, it is justified that atomistic simulations can be regarded as a tool for investigating the MT, SME, and SE by providing more structural details and mechanistic insights at the atomic scale. For example, MD simulations exhibit a possibility of describing the phase structures derived from temperature- and stress-induced phase transformation [7, 8]. In the MD method, several characteristics of phase transformation in the NiTi alloy had been revealed through a semiempirical pair potential [9]. Liang and Zhou [10] conducted an atomistic simulation and successfully achieved the SME in single-crystalline fcc Cu nanowires. It was found that when a thermomechanical load was applied in a martensitic NiAl system, the total recovery of deformation could be obtained by MD under the condition of periodic boundaries [11]. Considering the complexity of microstructure of martensite, the semiempirical potential-based atomistic simulation approach is expected to play an important role in bridging a link between experiments and numerical models for understanding the transformation mechanism in SMAs [12–14].It is well known that the evolution of twinning behavior is of great importance for the martensitic phase transformation in SMAs [3]. Twin martensites are conventionally classified into three categories: type I (i.e., the twin plane is a rational crystal plane), type II (i.e., the twin shear is a rational crystallographic direction), and compound twin (both the twin plane and twin shear are rational), the detailed definitions of which are described in the review [15]. Krishnan and Singh found a new type of B19′ martensite in the thermally cycled NiTi alloy, and the (001) compound twin was shaped [16]. Also, the occurrence and disappearance of microtwins had been confirmed by in situ TEM during mechanical cycles [17]. Some reports claimed that the stress-induced martensite transformation would occur accompanied with deformation twinning when the alloy was subjected to plastic deformation in the austenite state [18]. Zhong et al. performed an in-depth study on the structure and geometrical limit of nanoscale twins in NiTi by combining the crystallographic theory with atomistic simulations [19]. However, the role of atomic interactions involved during structural transformations, such as twinning and size effect as well as the temperature-dependent behavior, is not yet well understood. Moreover, a physical mechanism is still required to explain the characteristics of both temperature- and stress-induced phase transformations.The numerical simulation performed in the present work differs from those of other studies. The motivation behind previous investigations has been to study phase transformations in a single-crystalline NiTi alloy under uniaxial compression loading. It should be emphasized that our investigation is primarily focused on conducting numerical analysis for interatomic motions by using MD simulations coupled with an effective potential [21]. Considering that the twinning structure always appears inside the gain, an initial model is prepared as a single crystal NiTi with the B2 structure. Compared with available experimental information, the role of nanotwins in the atomistic behavior is further examined as well. This study is expected to provide a more comprehensive understanding of the temperature- and stress-induced phase transformation mechanisms for this kind of material from the perspective of atomic scale.


## 2. Materials and Methods

### 2.1. 2NN MEAM Potential

It is widely accepted that the embedded-atom method (EAM) can be employed to characterize the interatomic potential [27]. Besides, a modified embedded-atom method (MEAM) combined with an angular dependent term has been proposed by Baskes [22]. Comparatively speaking, MEAM potentials are well suited for simulations of multicomponent systems composed of elements with different ground states, because they allow for characterizing a wide range of phases (fcc, bcc, hcp, diamond-structured, and even gases) using a common mathematical function [28]. However, Ko et al. [21] strongly recommended the use of second nearest-neighbor modified embedded-atom method (2NN MEAM) when choosing an interatomic potential in the NiTi binary alloy. Furthermore, a comparison of the predicted results with the experimental ones [3] indicated that such a model could be available for representing the characteristics of the low temperature martensitic structure (B19′).The total potential energy of the 2NN MEAM is expressed as follows:(1)E=∑iFiρ-i+12∑j≠isijϕijRij,where Fi is the embedding energy, which is a function of background electron density ρ-i. Sij is the screening function and ϕijRij is the pair interaction between atoms i and j separated by a distance Rij. In fact, what the nicest feature the improved MEAM has is that it accounts for the second nearest-neighbor interactions when calculating the embedding energy, while the original MEAM merely considers the first nearest-neighbor interactions through a strong many-body screening function. A detailed formulation of the 2NN MEAM formalism was provided in literature [29, 30].Figure1 shows the calculated cohesive energy Ec (eV/atom) and equilibrium lattice constants a0 (Å) of the B2 structure under the framework of 2NN MEAM potential.Figure 1
Atomic energyEc (eV) versus unit cell lattice constant a0 (Å).When the lattice constant varies from 2.5 to 4 Å, the atom energy for each instantaneous equilibrium state is calculated, and then the cohesive energy is achieved by minimizing all the atom energies. In this work, the computed energy is 5.05 eV corresponding to an equilibrium lattice constant ofa0 = 2.999 Å, and these values conform to other potentials [20]. Some other calculated physical properties of equiatomic NiTi compounds are presented in Table 1. Compared with experimental data and other potentials, it is demonstrated that the parameters obtained from such a potential could be used in our subsequent simulations for investigating the phase transformations induced by temperature and stress.Table 1
Comparison of calculated and experimental physical constants for the B2 phase.
Property
2NN MEAM potential
Experiments
Literature potential [22]
DFT simulations
Elastic constants (GPa)
C11
143
162 [23]
206
138 [24]
C12
128
129 [23]
136
169 [24]
C44
80
35 [23]
47
40 [24]
Bulk modulus, B
133
140 [23]
159
159 [24]
Cohesive energy (eV)
−5.05
−4.95 [25]
−5.022
−4.99 [26]
Lattice constant (Å)
2.999
3.01 [25]
3.008
2.96 [26]


### 2.2. Physical Structures

For the equiatomic NiTi alloy, the geometric structure of austenitic phase is the cubic B2 (with space group ofPm3-m) structure, while the B19′ structure (with space group of P21/m) is remarkably characterized by a monoclinic angle (β = 96.8°) and shuffling of Ni and Ti atoms on the 110B2 plane [3]. Figure 2 shows the lattice structures for B2 and B19′, respectively.Figure 2
Schematic of the structure of B2 and B19′.


### 2.3. MD Simulations

In this study, the open source software LAMMPS (Large scale Atomic/Molecular Massively Parallel Simulator) [25] developed at Sandia National Laboratories, USA (http://lammps.sandia.gov/), is used to conduct MD simulations. The atomic configuration viewer Ovito [24] (http://ovito.org/) is utilized to analyze microstructural evolutions during phase transformations, and local atomic arrangements are visualized by the common neighbor analysis (CNA) [7].Firstly, the single crystal of B2 type unit cells (witha0=2.999 Å) was produced by the atomic positions of the basis atoms: Ni ≡ (0 0 0) and Ti ≡ (0.5 0.5 0.5). An investigation of the temperature-induced phase transition was performed to study the martensitic transformation mechanism. The initial model was set as the B2 structure, with the length of 20 cells, width of 20 cells, and thickness 5 cells. The total atoms were 4000. Several corresponding MD simulations were employed starting with supercells ranging in sizes from 4000 to 16000 atoms. The single crystal supercell of B2 structure was firstly equilibrated at 550 K, using an isobaric-isothermal ensemble (NPT) at zero pressure. All the simulations were carried out in the temperature range from 550 to 50 K with a cooling rate of 1 K/ps and heating from 50 to 550 K with the same rate. Periodic boundary conditions were applied along all three dimensions for the purpose of computational efficiency [26]. Cell dimensions, cell angles, and individual atomic positions were allowed to relax. Then, the changes in atomic volumes were carefully recorded to observe the occurrence of phase transitions.For the purpose of simplicity only, a pillar was prepared as a single crystal consisting of the B2 structure with dimensions of 9.0 × 8.5 × 2.1 nm and 12000 atoms when simulating the stress-induced phase transition. The sides of the pillar were{110}-type surfaces, and the longitudinal direction was aligned to the [001] direction in the structure. After these steps, the transition temperatures under a zero-stress state were obtained, and then Ms and Af were calculated to be 240 and 440 K, respectively. After that, the pillar was equilibrated to 450 K. It was emphasized that this temperature was slightly higher than Af (440 K), which could be responsible for maintaining the B2 phase under a zero-stress state. Finally, a compressive loading was applied by adjusting the stress along the longitudinal direction of the samples. Under the temperature of 450 K, the compressive stresses increases from 0 to 2.1 GPa and completely decreases. A constant loading rate of ±3.5 MPa/ps was maintained. MD simulations were performed using a time step of 2 fs.


## 2.1. 2NN MEAM Potential

It is widely accepted that the embedded-atom method (EAM) can be employed to characterize the interatomic potential [27]. Besides, a modified embedded-atom method (MEAM) combined with an angular dependent term has been proposed by Baskes [22]. Comparatively speaking, MEAM potentials are well suited for simulations of multicomponent systems composed of elements with different ground states, because they allow for characterizing a wide range of phases (fcc, bcc, hcp, diamond-structured, and even gases) using a common mathematical function [28]. However, Ko et al. [21] strongly recommended the use of second nearest-neighbor modified embedded-atom method (2NN MEAM) when choosing an interatomic potential in the NiTi binary alloy. Furthermore, a comparison of the predicted results with the experimental ones [3] indicated that such a model could be available for representing the characteristics of the low temperature martensitic structure (B19′).The total potential energy of the 2NN MEAM is expressed as follows:(1)E=∑iFiρ-i+12∑j≠isijϕijRij,where Fi is the embedding energy, which is a function of background electron density ρ-i. Sij is the screening function and ϕijRij is the pair interaction between atoms i and j separated by a distance Rij. In fact, what the nicest feature the improved MEAM has is that it accounts for the second nearest-neighbor interactions when calculating the embedding energy, while the original MEAM merely considers the first nearest-neighbor interactions through a strong many-body screening function. A detailed formulation of the 2NN MEAM formalism was provided in literature [29, 30].Figure1 shows the calculated cohesive energy Ec (eV/atom) and equilibrium lattice constants a0 (Å) of the B2 structure under the framework of 2NN MEAM potential.Figure 1
Atomic energyEc (eV) versus unit cell lattice constant a0 (Å).When the lattice constant varies from 2.5 to 4 Å, the atom energy for each instantaneous equilibrium state is calculated, and then the cohesive energy is achieved by minimizing all the atom energies. In this work, the computed energy is 5.05 eV corresponding to an equilibrium lattice constant ofa0 = 2.999 Å, and these values conform to other potentials [20]. Some other calculated physical properties of equiatomic NiTi compounds are presented in Table 1. Compared with experimental data and other potentials, it is demonstrated that the parameters obtained from such a potential could be used in our subsequent simulations for investigating the phase transformations induced by temperature and stress.Table 1
Comparison of calculated and experimental physical constants for the B2 phase.
Property
2NN MEAM potential
Experiments
Literature potential [22]
DFT simulations
Elastic constants (GPa)
C11
143
162 [23]
206
138 [24]
C12
128
129 [23]
136
169 [24]
C44
80
35 [23]
47
40 [24]
Bulk modulus, B
133
140 [23]
159
159 [24]
Cohesive energy (eV)
−5.05
−4.95 [25]
−5.022
−4.99 [26]
Lattice constant (Å)
2.999
3.01 [25]
3.008
2.96 [26]


## 2.2. Physical Structures

For the equiatomic NiTi alloy, the geometric structure of austenitic phase is the cubic B2 (with space group ofPm3-m) structure, while the B19′ structure (with space group of P21/m) is remarkably characterized by a monoclinic angle (β = 96.8°) and shuffling of Ni and Ti atoms on the 110B2 plane [3]. Figure 2 shows the lattice structures for B2 and B19′, respectively.Figure 2
Schematic of the structure of B2 and B19′.


## 2.3. MD Simulations

In this study, the open source software LAMMPS (Large scale Atomic/Molecular Massively Parallel Simulator) [25] developed at Sandia National Laboratories, USA (http://lammps.sandia.gov/), is used to conduct MD simulations. The atomic configuration viewer Ovito [24] (http://ovito.org/) is utilized to analyze microstructural evolutions during phase transformations, and local atomic arrangements are visualized by the common neighbor analysis (CNA) [7].Firstly, the single crystal of B2 type unit cells (witha0=2.999 Å) was produced by the atomic positions of the basis atoms: Ni ≡ (0 0 0) and Ti ≡ (0.5 0.5 0.5). An investigation of the temperature-induced phase transition was performed to study the martensitic transformation mechanism. The initial model was set as the B2 structure, with the length of 20 cells, width of 20 cells, and thickness 5 cells. The total atoms were 4000. Several corresponding MD simulations were employed starting with supercells ranging in sizes from 4000 to 16000 atoms. The single crystal supercell of B2 structure was firstly equilibrated at 550 K, using an isobaric-isothermal ensemble (NPT) at zero pressure. All the simulations were carried out in the temperature range from 550 to 50 K with a cooling rate of 1 K/ps and heating from 50 to 550 K with the same rate. Periodic boundary conditions were applied along all three dimensions for the purpose of computational efficiency [26]. Cell dimensions, cell angles, and individual atomic positions were allowed to relax. Then, the changes in atomic volumes were carefully recorded to observe the occurrence of phase transitions.For the purpose of simplicity only, a pillar was prepared as a single crystal consisting of the B2 structure with dimensions of 9.0 × 8.5 × 2.1 nm and 12000 atoms when simulating the stress-induced phase transition. The sides of the pillar were{110}-type surfaces, and the longitudinal direction was aligned to the [001] direction in the structure. After these steps, the transition temperatures under a zero-stress state were obtained, and then Ms and Af were calculated to be 240 and 440 K, respectively. After that, the pillar was equilibrated to 450 K. It was emphasized that this temperature was slightly higher than Af (440 K), which could be responsible for maintaining the B2 phase under a zero-stress state. Finally, a compressive loading was applied by adjusting the stress along the longitudinal direction of the samples. Under the temperature of 450 K, the compressive stresses increases from 0 to 2.1 GPa and completely decreases. A constant loading rate of ±3.5 MPa/ps was maintained. MD simulations were performed using a time step of 2 fs.


## 3. Results and Discussion

### 3.1. Temperature-Induced Phase Transition

Figure3 shows the temperature dependence of atomic volumes for a cell combined with 4000 atoms. It is evident that the obtained volumes for the austenitic and martensitic structures at room temperature (~300 K) are 13.64 Å3 and 13.73 Å3, respectively, which are in good accordance with those of experiment values (13.70 Å3 and 13.80 Å3) [31]. From this figure, it is distinctly demonstrated that the martensite start temperature (Ms) is 270 K from the discrete positive change, which yield a closer fit to the experimental data when performing a comparison with the previous study [20]. Besides, the discrete decrease during the reheating process marks that the martensite phase transforms back into the austenite at the temperature of 390 K. It is obvious that both martensitic and reverse transformation (i.e., austenite) occur in the process of cooling and heating. The physical reason hiding behind such phenomena is believed to be due to the difference of atomic volume between B2 and B19′.Figure 3
The atomic volume dependence on temperature during cooling (blue circle) and heating (red triangle) process for NiTi alloy with 4000 atoms. The discrete jumps indicated by the arrows represent the occurrence of phase transitions.Figure4 depicts atomic configurations of a simulated supercell before and after a martensitic transition. As shown in Figure 4(b), a twinned structure with finely dispersed compound twin boundaries (001) is observed in the transformed martensite. In previous studies, it was found that such a behavior does exist in the nanocrystalline structure [32].Figure 4
Atomic structures of (a) the initial B2 phase and (b) the transformed B19′ phase including (001) compound twin boundaries. Ni and Ti atoms are represented by blue and red, respectively. Note that the twinning direction and twinning plane (010) are showed by the coordinate of B2 phase.
(a)
(b)Figure5(a) shows the transition temperatures calculated using the 16000-atom supercell. From the results, Ms is about 255 K, which is lower than the one (270 K) of the 4000-atom supercell. This could be attributed to the fact that the undercooling shows an increasing trend with enlarging the supercell sizes. Compared with the 4000-atom supercell (390 K), Af is found to be a higher value of 445 K of 16000 atoms. Furthermore, the larger supercell exhibits a considerably wider thermal hysteresis, which is on account of the increasing of the number of atoms in twin zones. Figure 5(b) shows that more compound twins emerge in the 16000-atom supercell, accompanied by a twinning direction of [010]. These results indicate that the twin direction is not fixed but could vary with cell sizes. Additionally, it is evident that the average width of twin is in nanometer magnitude, which agrees well with experimental data [32]. However, it must be pointed out that the size effect on the transformation temperatures and the nanotwin formations disappears when the specimen is sufficiently large [21].Figure 5
(a) The atomic volume dependence of temperature during cooling and heating and (b) the twinned martensite B19′ phase with 16000 atoms.
(a)
(b)


### 3.2. Stress-Induced Phase Transition

#### 3.2.1. Stress-Strain Behavior

Figure6 illustrates a resultant stress-strain response of the pillar subjected to longitudinal compressive deformations at 450 K. In this figure, the phase transition onset in loading/unloading is represented by an arrow. It is clear that the stress shows an increasing tendency with the applied strain at the beginning of loading, which is known as the elastic stage of martensitic structure. Due to the occurrence of phase transformation from B2 to B19′, a plateau appears in the stress-strain curve. The phase transformation occurred at the stress level of 1339 MPa, which was in agreement with the experimental data (1 GPa) achieved from in situ TEM tests [33]. As the applied load increases, another elastic stage (austenite) emerges with the end of martensitic transformation. During the unloading process, B19′ will directly back into B2. From the figure, it is shown that the full recovery of the initial B2 structure arises after a load cycle, which exhibits the superelastic behavior. In other words, the NiTi alloy allows for sustaining large elastic strains.Figure 6
Simulated stress-strain response of a single crystal NiTi at 450 K. Note that the positive values mean the compressive strain values.


#### 3.2.2. Reversible Phase Transformation

Figure7 shows the atomistic snapshots of the NiTi single crystal during various deformation stages at 450 K. For the purpose of hiding the periodic atoms on the boundaries, a few of the outmost surface layers are not visualized. As expected, only the elastic compression deformation occurs at the initial elastic strain (from 0 to about 5%). In other words, the crystal structure remains unchanged, which is similar to the initial structure (with B2 unit cells). When the stress level reaches 1339 MPa, it seems that the atoms take a considerable rearrangement. Some austenitic lattices (with B2 unit cells) gradually transform into the monoclinic martensitic lattices. With continuing compression, the volume fraction of B19′ increases. The martensitic transformation is verified by a careful inspection for the lattice structure within the phase transformation regions, which is illustrated in Figure 8. In examining this figure, the monoclinic unit cell structure with monoclinic angle β = 97° is in stark contrast with the B2 lattice. Moreover, the newly transformed B19′ variants along different directions create multiple mirrored strips, that is, the twinned structures. This phenomenon is the direct evidence of the (001) type compound twins of B19′, consistent with the behavior observed by TEM [16].Figure 7
Snapshots of the nano-NiTi during the compressive loading and the unloading process. The color of the atoms is scaled according to the common neighbor analysis (CNA) pattern [20]. In each snapshot, blue atoms correspond to the B2 structure and gray atoms to the B19′ structure. A few of the outmost surface layers (thickness of 0.5 nm) are not visualized for clarity.Figure 8
Atomic structure of (110) compound twins, and the white parallelogram indicates a monoclinic unit cell with the monoclinic angleβ≈97°. The mirror twin plane (dashed line) is located on the pure Ni layer. A few of the outmost surface layers (thickness of 0.5 nm) are not visualized for clarity. Ni and Ti atoms are represented by blue and red, respectively.The internal twinning behavior continues until the crystal fully converts into the martensitic phase (with internally twinned B19′ lattice), which occurs at about 20% applied strain. Afterwards, the continuation of applied loading leads to an elastic strain of the twinned martensite, corresponding to the rising portion of stress-strain curve (from 20 to 26%). The final crystal structure (at about 26% applied strain) is characterized by multiple internal twins, seen in Figure7.During the unloading, the deformation in the crystal embedded with twinned martensite fully recovers when the total strain is 26%, which may be expected as a result of a combination of elastic relaxation and a reverse phase transformation (from B19′ to B2). In Figure7, the atomistic snapshots indicate a gradual reduction in volume fractions of the twinned B19′, and B19′ diminishes at the lower stress plateau. It is suggested that the internally twinned martensitic structure remains stable only when the stress level is high. However, the removal of applied stress serves to cause the phase transformation from B19′ to B2.


#### 3.2.3. Dependency of Transformation Stress on Temperature

The relationship between the environmental temperature and transformation stress/strain under stress-controlled compressive loading is provided in Figure9, which shows that, based on 0.2% offset method, the transformation stress increases from 1339 to 2300 MPa as the temperature increases from 450 to 950 K, while the corresponding strain decreases from 18.5 to 13.6% for the same temperature magnitude. These observations from the simulations are in general agreement with experimental findings [3]. The temperature effect could be rationalized on the basis of the thermodynamics of transforming alloys [12]. The twinned monoclinic B19′ structure that constitutes the martensitic phase becomes unstable at an elevated temperature. In order to complete the phase transformation from B2 to B19′, an additional driving force is needed to be applied. As a result, the transformation stress level continues to increase with increasing temperature, which is absolutely different from any conventional alloy that would undergo a decreasing flow stress. When the temperature is sufficiently high (above 950 K), any transformation strain no longer appears in the parent B2 behaviors, demonstrating the temperature-dependent plastic deformation of austenitic phase.Figure 9
Calculated values of transformation stress and strain for the NiTi austenite compressed in001B2 direction when the temperature ranges from 450 to 950 K.


## 3.1. Temperature-Induced Phase Transition

Figure3 shows the temperature dependence of atomic volumes for a cell combined with 4000 atoms. It is evident that the obtained volumes for the austenitic and martensitic structures at room temperature (~300 K) are 13.64 Å3 and 13.73 Å3, respectively, which are in good accordance with those of experiment values (13.70 Å3 and 13.80 Å3) [31]. From this figure, it is distinctly demonstrated that the martensite start temperature (Ms) is 270 K from the discrete positive change, which yield a closer fit to the experimental data when performing a comparison with the previous study [20]. Besides, the discrete decrease during the reheating process marks that the martensite phase transforms back into the austenite at the temperature of 390 K. It is obvious that both martensitic and reverse transformation (i.e., austenite) occur in the process of cooling and heating. The physical reason hiding behind such phenomena is believed to be due to the difference of atomic volume between B2 and B19′.Figure 3
The atomic volume dependence on temperature during cooling (blue circle) and heating (red triangle) process for NiTi alloy with 4000 atoms. The discrete jumps indicated by the arrows represent the occurrence of phase transitions.Figure4 depicts atomic configurations of a simulated supercell before and after a martensitic transition. As shown in Figure 4(b), a twinned structure with finely dispersed compound twin boundaries (001) is observed in the transformed martensite. In previous studies, it was found that such a behavior does exist in the nanocrystalline structure [32].Figure 4
Atomic structures of (a) the initial B2 phase and (b) the transformed B19′ phase including (001) compound twin boundaries. Ni and Ti atoms are represented by blue and red, respectively. Note that the twinning direction and twinning plane (010) are showed by the coordinate of B2 phase.
(a)
(b)Figure5(a) shows the transition temperatures calculated using the 16000-atom supercell. From the results, Ms is about 255 K, which is lower than the one (270 K) of the 4000-atom supercell. This could be attributed to the fact that the undercooling shows an increasing trend with enlarging the supercell sizes. Compared with the 4000-atom supercell (390 K), Af is found to be a higher value of 445 K of 16000 atoms. Furthermore, the larger supercell exhibits a considerably wider thermal hysteresis, which is on account of the increasing of the number of atoms in twin zones. Figure 5(b) shows that more compound twins emerge in the 16000-atom supercell, accompanied by a twinning direction of [010]. These results indicate that the twin direction is not fixed but could vary with cell sizes. Additionally, it is evident that the average width of twin is in nanometer magnitude, which agrees well with experimental data [32]. However, it must be pointed out that the size effect on the transformation temperatures and the nanotwin formations disappears when the specimen is sufficiently large [21].Figure 5
(a) The atomic volume dependence of temperature during cooling and heating and (b) the twinned martensite B19′ phase with 16000 atoms.
(a)
(b)


## 3.2. Stress-Induced Phase Transition

### 3.2.1. Stress-Strain Behavior

Figure6 illustrates a resultant stress-strain response of the pillar subjected to longitudinal compressive deformations at 450 K. In this figure, the phase transition onset in loading/unloading is represented by an arrow. It is clear that the stress shows an increasing tendency with the applied strain at the beginning of loading, which is known as the elastic stage of martensitic structure. Due to the occurrence of phase transformation from B2 to B19′, a plateau appears in the stress-strain curve. The phase transformation occurred at the stress level of 1339 MPa, which was in agreement with the experimental data (1 GPa) achieved from in situ TEM tests [33]. As the applied load increases, another elastic stage (austenite) emerges with the end of martensitic transformation. During the unloading process, B19′ will directly back into B2. From the figure, it is shown that the full recovery of the initial B2 structure arises after a load cycle, which exhibits the superelastic behavior. In other words, the NiTi alloy allows for sustaining large elastic strains.Figure 6
Simulated stress-strain response of a single crystal NiTi at 450 K. Note that the positive values mean the compressive strain values.


### 3.2.2. Reversible Phase Transformation

Figure7 shows the atomistic snapshots of the NiTi single crystal during various deformation stages at 450 K. For the purpose of hiding the periodic atoms on the boundaries, a few of the outmost surface layers are not visualized. As expected, only the elastic compression deformation occurs at the initial elastic strain (from 0 to about 5%). In other words, the crystal structure remains unchanged, which is similar to the initial structure (with B2 unit cells). When the stress level reaches 1339 MPa, it seems that the atoms take a considerable rearrangement. Some austenitic lattices (with B2 unit cells) gradually transform into the monoclinic martensitic lattices. With continuing compression, the volume fraction of B19′ increases. The martensitic transformation is verified by a careful inspection for the lattice structure within the phase transformation regions, which is illustrated in Figure 8. In examining this figure, the monoclinic unit cell structure with monoclinic angle β = 97° is in stark contrast with the B2 lattice. Moreover, the newly transformed B19′ variants along different directions create multiple mirrored strips, that is, the twinned structures. This phenomenon is the direct evidence of the (001) type compound twins of B19′, consistent with the behavior observed by TEM [16].Figure 7
Snapshots of the nano-NiTi during the compressive loading and the unloading process. The color of the atoms is scaled according to the common neighbor analysis (CNA) pattern [20]. In each snapshot, blue atoms correspond to the B2 structure and gray atoms to the B19′ structure. A few of the outmost surface layers (thickness of 0.5 nm) are not visualized for clarity.Figure 8
Atomic structure of (110) compound twins, and the white parallelogram indicates a monoclinic unit cell with the monoclinic angleβ≈97°. The mirror twin plane (dashed line) is located on the pure Ni layer. A few of the outmost surface layers (thickness of 0.5 nm) are not visualized for clarity. Ni and Ti atoms are represented by blue and red, respectively.The internal twinning behavior continues until the crystal fully converts into the martensitic phase (with internally twinned B19′ lattice), which occurs at about 20% applied strain. Afterwards, the continuation of applied loading leads to an elastic strain of the twinned martensite, corresponding to the rising portion of stress-strain curve (from 20 to 26%). The final crystal structure (at about 26% applied strain) is characterized by multiple internal twins, seen in Figure7.During the unloading, the deformation in the crystal embedded with twinned martensite fully recovers when the total strain is 26%, which may be expected as a result of a combination of elastic relaxation and a reverse phase transformation (from B19′ to B2). In Figure7, the atomistic snapshots indicate a gradual reduction in volume fractions of the twinned B19′, and B19′ diminishes at the lower stress plateau. It is suggested that the internally twinned martensitic structure remains stable only when the stress level is high. However, the removal of applied stress serves to cause the phase transformation from B19′ to B2.


### 3.2.3. Dependency of Transformation Stress on Temperature

The relationship between the environmental temperature and transformation stress/strain under stress-controlled compressive loading is provided in Figure9, which shows that, based on 0.2% offset method, the transformation stress increases from 1339 to 2300 MPa as the temperature increases from 450 to 950 K, while the corresponding strain decreases from 18.5 to 13.6% for the same temperature magnitude. These observations from the simulations are in general agreement with experimental findings [3]. The temperature effect could be rationalized on the basis of the thermodynamics of transforming alloys [12]. The twinned monoclinic B19′ structure that constitutes the martensitic phase becomes unstable at an elevated temperature. In order to complete the phase transformation from B2 to B19′, an additional driving force is needed to be applied. As a result, the transformation stress level continues to increase with increasing temperature, which is absolutely different from any conventional alloy that would undergo a decreasing flow stress. When the temperature is sufficiently high (above 950 K), any transformation strain no longer appears in the parent B2 behaviors, demonstrating the temperature-dependent plastic deformation of austenitic phase.Figure 9
Calculated values of transformation stress and strain for the NiTi austenite compressed in001B2 direction when the temperature ranges from 450 to 950 K.


## 3.2.1. Stress-Strain Behavior

Figure6 illustrates a resultant stress-strain response of the pillar subjected to longitudinal compressive deformations at 450 K. In this figure, the phase transition onset in loading/unloading is represented by an arrow. It is clear that the stress shows an increasing tendency with the applied strain at the beginning of loading, which is known as the elastic stage of martensitic structure. Due to the occurrence of phase transformation from B2 to B19′, a plateau appears in the stress-strain curve. The phase transformation occurred at the stress level of 1339 MPa, which was in agreement with the experimental data (1 GPa) achieved from in situ TEM tests [33]. As the applied load increases, another elastic stage (austenite) emerges with the end of martensitic transformation. During the unloading process, B19′ will directly back into B2. From the figure, it is shown that the full recovery of the initial B2 structure arises after a load cycle, which exhibits the superelastic behavior. In other words, the NiTi alloy allows for sustaining large elastic strains.Figure 6
Simulated stress-strain response of a single crystal NiTi at 450 K. Note that the positive values mean the compressive strain values.


## 3.2.2. Reversible Phase Transformation

Figure7 shows the atomistic snapshots of the NiTi single crystal during various deformation stages at 450 K. For the purpose of hiding the periodic atoms on the boundaries, a few of the outmost surface layers are not visualized. As expected, only the elastic compression deformation occurs at the initial elastic strain (from 0 to about 5%). In other words, the crystal structure remains unchanged, which is similar to the initial structure (with B2 unit cells). When the stress level reaches 1339 MPa, it seems that the atoms take a considerable rearrangement. Some austenitic lattices (with B2 unit cells) gradually transform into the monoclinic martensitic lattices. With continuing compression, the volume fraction of B19′ increases. The martensitic transformation is verified by a careful inspection for the lattice structure within the phase transformation regions, which is illustrated in Figure 8. In examining this figure, the monoclinic unit cell structure with monoclinic angle β = 97° is in stark contrast with the B2 lattice. Moreover, the newly transformed B19′ variants along different directions create multiple mirrored strips, that is, the twinned structures. This phenomenon is the direct evidence of the (001) type compound twins of B19′, consistent with the behavior observed by TEM [16].Figure 7
Snapshots of the nano-NiTi during the compressive loading and the unloading process. The color of the atoms is scaled according to the common neighbor analysis (CNA) pattern [20]. In each snapshot, blue atoms correspond to the B2 structure and gray atoms to the B19′ structure. A few of the outmost surface layers (thickness of 0.5 nm) are not visualized for clarity.Figure 8
Atomic structure of (110) compound twins, and the white parallelogram indicates a monoclinic unit cell with the monoclinic angleβ≈97°. The mirror twin plane (dashed line) is located on the pure Ni layer. A few of the outmost surface layers (thickness of 0.5 nm) are not visualized for clarity. Ni and Ti atoms are represented by blue and red, respectively.The internal twinning behavior continues until the crystal fully converts into the martensitic phase (with internally twinned B19′ lattice), which occurs at about 20% applied strain. Afterwards, the continuation of applied loading leads to an elastic strain of the twinned martensite, corresponding to the rising portion of stress-strain curve (from 20 to 26%). The final crystal structure (at about 26% applied strain) is characterized by multiple internal twins, seen in Figure7.During the unloading, the deformation in the crystal embedded with twinned martensite fully recovers when the total strain is 26%, which may be expected as a result of a combination of elastic relaxation and a reverse phase transformation (from B19′ to B2). In Figure7, the atomistic snapshots indicate a gradual reduction in volume fractions of the twinned B19′, and B19′ diminishes at the lower stress plateau. It is suggested that the internally twinned martensitic structure remains stable only when the stress level is high. However, the removal of applied stress serves to cause the phase transformation from B19′ to B2.


## 3.2.3. Dependency of Transformation Stress on Temperature

The relationship between the environmental temperature and transformation stress/strain under stress-controlled compressive loading is provided in Figure9, which shows that, based on 0.2% offset method, the transformation stress increases from 1339 to 2300 MPa as the temperature increases from 450 to 950 K, while the corresponding strain decreases from 18.5 to 13.6% for the same temperature magnitude. These observations from the simulations are in general agreement with experimental findings [3]. The temperature effect could be rationalized on the basis of the thermodynamics of transforming alloys [12]. The twinned monoclinic B19′ structure that constitutes the martensitic phase becomes unstable at an elevated temperature. In order to complete the phase transformation from B2 to B19′, an additional driving force is needed to be applied. As a result, the transformation stress level continues to increase with increasing temperature, which is absolutely different from any conventional alloy that would undergo a decreasing flow stress. When the temperature is sufficiently high (above 950 K), any transformation strain no longer appears in the parent B2 behaviors, demonstrating the temperature-dependent plastic deformation of austenitic phase.Figure 9
Calculated values of transformation stress and strain for the NiTi austenite compressed in001B2 direction when the temperature ranges from 450 to 950 K.


## 4. Conclusions

Compared with previous studies, a deeper understanding of compression in the NiTi alloy is gained by crystallographic calculations on the formation of nanotwinned martensitic structures in a single-crystalline NiTi alloy in the present work. The 2NN MEAM potential is testified by a comparison of the calculated properties and experimental results, such as elastic constant, melting temperature, cohesive energy, and equilibrium lattice constant. Molecular dynamics method is employed to investigate the stress-induced and temperature-induced martensitic phase transformation in NiTi at the nanometer scale. The simulations indicate that the twinning structure has a crucial impact on the phase transformation temperature. The martensite start temperature (Ms) and austenite finish temperature (Af) of the NiTi alloy are obtained and found to provide a reasonable agreement with experimental data. In addition, the superelastic behavior is reproduced through numerical modeling. From the results of the stress-induced phase transition under the 100B2 compressive loading, it could be concluded that a full recovery of the shape occurs after a loading-unloading cycle. Also, the results demonstrate that the stress-induced phase transformation (from austenite to martensite) does exist in single crystal NiTi alloy, the size of which is below 100 nm. This phenomenon was previously observed by in situ TEM nanocompressive tests. The atomic screenshots of the compression specimen indicate that there are multiple B19′ variants of small misorientations with each other and they form the nanotwins. Importantly, the relationship between the environmental temperature and transformation behavior is established through numerical simulations. However, a more precise calibration of the model, capable of accounting for a polycrystalline NiTi alloy and its cyclic behavior, would have to be considered in further study.



---

*Source: 7427039-2017-09-17.xml*