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Effect of deformation conditions on compression phase transformation of AZ31

  • Qianhua Yang , Bowen Yang , Zhibing Chu EMAIL logo , Chun Xue , Yugui Li , Leifeng Tuo and Hong Gao
Published/Copyright: July 5, 2022
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Abstract

In this article, the compression simulation of AZ31 magnesium alloy is simulated by the molecular dynamics method. The effects of loading mode, temperature, and strain rate on the compression behavior are analyzed. The lattice distortion, mechanical behavior, structural evolution, and dislocation evolution in the compression process are deeply analyzed, and the results of different loading modes are obtained. The hexagonal close-packed (HCP) → face-centered cubic (FCC) phase transformation mechanism of AZ31 magnesium alloy during compression at temperature and strain rate, which is related to the mechanical behavior, has been studied completely. This article perfects the research on the compression behavior of magnesium alloys, excavates the application potential of magnesium alloys, and provides a new idea for improving the processing technology and developing high-performance magnesium alloys.

1 Introduction

Magnesium and magnesium alloys have excellent physical and mechanical properties, high specific strength, good thermal conductivity, and some more properties. They are important and excellent materials for automotive and aerospace industry structures [1,2,3,4,5,6,7,8,9]. Mg–Al–Zn magnesium alloy is currently one of the most widely used magnesium alloy series [10], of which the most representative is AZ31 wrought magnesium alloy. However, the large-scale commercial application of mg-based alloys still faces some obstacles [11,12,13]. To further improve the strength of magnesium alloy, it is necessary to fully understand the influence of microstructure and dislocation evolution on the strength [14]. Magnesium alloys have a hexagonal closely packed structure [15], and its deformation mechanism is closely related to stress/strain state, temperature, and strain rate. Plastic deformation still plays a key role in the strengthening of the hexagonal close-packed (HCP) phase [16,17]. Grain refinement of magnesium alloys, especially magnesium–aluminum (Mg–Al) alloys, is the most effective method to improve strength [18].

Integrated computational material engineering has become a reliable tool to establish the relationship between structure, process, and properties, which will promote the development and the application of new magnesium alloys to a great extent [19,20,21]. Among them, molecular dynamics (MD) simulation, as an important method in the study of plastic deformation mechanism at micro- and nano-scale in metal materials [22,23,24,25], can predict the effects of grain size, grain boundaries, stacking faults, and dislocations on the deformation behavior of materials at the atomic level [26,27,28,29,30,31,32,33,34,35,36,37]. MD simulations show that grain boundaries are the origin of dislocations in nanomaterials [38]. The nucleation and diffusion of some Shockley dislocations are caused by grain boundary (GB) deformation, that is, the position migration under the action of atomic phase transformation and stress [39,40]. Therefore, the study of dislocation evolution mechanism and phase transformation mechanism is of great significance to the total plastic deformation [41].

Rajput and Paul [42] studied the effect of uniaxial and plane strain tensile deformation on the mechanical behavior of nanocrystalline copper and found that the yield of the material begins with the nucleation of Shockley partial dislocations, and the subsequent deformation leads to the increase of dislocation line length in the material. The nucleation and diffusion of dislocations and stacking faults jointly control the strain hardening behavior of materials. The uneven distribution of atomic strain and dislocation was observed in uniaxial and plane strain tensile deformation. Higher GB migration was observed during uniaxial tensile deformation. Vlasova [43] investigated the deformation characteristics of nanocrystalline magnesium under high-speed deformation by MD simulation. Uniaxial compression and plane strain compression (PSC) of [0001]-nanocrystalline magnesium were carried out, and the effects of loading methods on the deformation and strength properties of [0001]-nanocrystalline magnesium were investigated. Paul et al. [44] studied the deformation mechanism and pore nucleation of nanocrystalline aluminum under uniaxial and plane strain loading. Compared with uniaxial loading, nanocavities nucleate earlier under plane strain loading. Zhang et al. [45] studied the micro-mechanical behavior of Cu/Ti laminated composites during uniaxial tension and PSC by the MD method and revealed the microdeformation mechanism of closely packed hexagonal metal laminated composites.

To sum up, the compression simulation of AZ31 magnesium alloy is simulated by the MD method, the effects of loading mode, temperature, and strain rate on the compression behavior are analyzed, the lattice distortion, mechanical behavior, structural evolution, and dislocation evolution in the compression process are deeply analyzed, and different loading modes are obtained. The HCP → face-centered cubic (FCC) phase transformation mechanism of AZ31 magnesium alloy during compression at temperature and strain rate, which is related to the mechanical behavior, has been studied completely. This article studies the compression behavior of magnesium alloys, excavates the application potential of magnesium alloys, and provides a new idea for improving the processing technology and developing high-performance magnesium alloys.

2 Simulation method

The potential function is a mathematical function that describes the total energy E and particle coordinates (r) of the model particles in the study of MD [46,47,48,49]. The modified embedded atomic method potential function can be used to calculate the pairwise interactions of various materials, which is more suitable for the calculation of metals and alloys with FCC, body-centered cubic (BCC), HCP, and diamond structures [50,51,52,53,54,55,56]. Eq. (1) for modified embedded atom method is given as follows:

(1) E = i F i ( ρ ¯ i ) + 1 2 i j ϕ ij ( γ ij ) .

In Eq. (1), E is the total energy of atom i, F is the embedded energy and is the function of atomic electron density ρ, ρ is the atomic electron density, γ and ϕ is a pair of potential interactions, and α and β is the element type of atoms i and j.

The model of AZ31 magnesium alloy was established by Atomsk [57], and the X-axis, Y-axis, and Z-axis were set to correspond to [1̅21̅0], [1̅010], and [0001], respectively. The model is imported into large-scale atomic/molecular massively parallel simulator (LAMMPS) [58] for MD simulation. The potential function developed by Stukowski [59] can be used to study the deformation and recrystallization characteristics of Mg–Al–Zn alloy in the whole processing temperature range, and so this potential function is used for calculation. X, Y, and Z are all periodic boundary conditions, constant-pressure, constant-temperature (NPT) ensemble is adopted, and the time step is 0.001 ps. The NPT ensemble and the nose-hoover thermostat maintain the stability of the entire system at constant pressure and temperature. The conjugate gradient algorithm is used to minimize the model energy to obtain the equilibrium structure at a given temperature in the NPT ensemble. Therefore, the model is first relaxed 10 ps under constant temperature and pressure, and then different deformation conditions are imposed, the deformation time is 20 ps, and the final deformation of magnesium alloy reaches 20%. The deformation Eq. (2) is expressed as follows:

(2) ε = L 1 L 2 L 1 × 100 % .

In Eq. (2), ε is strain; L 1 is the initial length of the model in [0001] crystal direction; and L 2 is the length of the model compressed along the [0001] crystal direction.

The results are imported into the visualization software OVITO for analysis. Common neighbor analysis (CNA) can observe the face-centered cubic, body-centered cubic, closely packed hexagonal (HCP) structure, and other structure (GB atoms) in the metal. DXA (dislocation analysis) can determine the Burgers vector of each dislocation and identify the dislocation junction. Grain segmentation can observe the grain changes in the simulation process. Construct surface mesh can identify the cavity and calculate the cavity area [60,61,62,63,64,65].

3 Results and analysis

3.1 Influence of compression mode on phase transition

The model of AZ31 magnesium alloy with a size of 192.6 Å × 222.395 Å × 208.4 Å is established, in which 96% are Mg atoms, 3% are Al atoms, and 1% are Zn atoms. The model contains 20 grains, and the X-axis, Y-axis, and Z-axis are set to correspond to the crystal directions of [1̅21̅0], [1̅010], and [0001], respectively. Import the model into LAMMPS and then assign the potential function developed by Hyo-Sun Jang to the model. X, Y, and Z are all periodic boundary conditions, and the time step is 0.001 ps. The model energy is minimized and 10 ps is relaxed at 300 K. The temperature change in the relaxation process is shown in Figure 1a. The model is uniformly compressed 20 ps along the Z-axis ([0001] direction) at 300 K with the strain rate of 0.01 ps−1, and the uniaxial compression simulation (UC) is realized. The process diagram is shown in Figure 1b.

Figure 1 
                  Uniaxial compression: (a) the change of temperature during relaxation and (b) process diagram.
Figure 1

Uniaxial compression: (a) the change of temperature during relaxation and (b) process diagram.

The model of AZ31 magnesium alloy with a size of 200 Å × 200 Å × 200 Å is established, in which 96% are Mg atoms, 3% are Al atoms, and 1% are Zn atoms. The model contains 20 grains, and the X-axis, Y-axis, and Z-axis are set to correspond to the crystal directions of [1̅21̅0], [1̅010], and [0001], respectively. The MD simulation is carried out by LAMMPS, and the potential function developed by Jang is assigned to the model. X, Y, and Z are all periodic boundary conditions, the time step is 0.001 ps, and the 10 ps is relaxed at 300 K. The change of temperature during the relaxation process is shown in Figure 2a. Keeping the size of the Y-axis model unchanged, the model is uniformly compressed 20 ps along the Z-axis ([0001] direction) at the strain rate of 0.01 ps−1 at 300 K, and the PSC simulation is realized. The process diagram is shown in Figure 2b.

Figure 2 
                  Plane strain compression: (a) the change of temperature during relaxation and (b) process diagram.
Figure 2

Plane strain compression: (a) the change of temperature during relaxation and (b) process diagram.

Figure 3 shows the grain change, Figure 3a shows the grain number curve, Figure 3b shows the grains at different strains under PSC, and Figure 3c shows the grains at different strains under UC. It can be seen that under PSC, the grain number is more, the grain volume is smaller, the grain refinement is more obvious, and the grain refinement occurs earlier.

Figure 3 
                  Grain change: (a) grain number curve, (b) grain change under PSC, and (c) grain change under UC.
Figure 3

Grain change: (a) grain number curve, (b) grain change under PSC, and (c) grain change under UC.

Figure 4 shows parameter changes during compression. Figure 4a shows the stress–strain curve. The yield stress under PSC is 2.85 GPa, and the yield stress under UC is 1.92 GPa, which increases by 48.43%. The yield strain under PSC is 10.2%, and the yield strain under UC is 9.6%, with an increase of 6.25%. The elastic modulus of PSC is larger, which means that PSC can improve the plasticity of AZ31 magnesium alloy. Figure 4b shows the dislocation density curve. The dislocation occurs earlier, and the dislocation density is higher in AZ31 magnesium alloy under PSC.

Figure 4 
                  Parameter changes during compression: (a) stress–strain curve and (b) dislocation density curve.
Figure 4

Parameter changes during compression: (a) stress–strain curve and (b) dislocation density curve.

Figure 5 shows cavity evolution. Figure 5a shows the curve of the cavity area, Figure 5b shows the evolution of the cavity under PSC, and Figure 5c shows the evolution of the cavity under UC. It can be found that cavity appears earlier in magnesium alloys under PSC, the time of cavity appearing is almost consistent with the time of dislocation increase, and the cavty area formed under PSC is larger. Therefore, in the PSC process, because the Y direction is fixed, the atomic position changes faster, forming dislocations and cavity, and at the same time, the yield stress of magnesium alloy increases.

Figure 5 
                  Cavity evolution: (a) cavity area curve, (b) cavity evolution under PSC, and (c) cavity evolution under UC.
Figure 5

Cavity evolution: (a) cavity area curve, (b) cavity evolution under PSC, and (c) cavity evolution under UC.

Figure 6 shows GB evolution. Figure 6a shows the atomic fraction curve within the grain, and Figure 6b shows the atomic fraction curve of the GB. The GB diffusion of magnesium alloy occurs earlier under PSC, and the rate and degree of diffusion are higher than that of UC. Figure 6c and d are CNA diagrams of PSC and UC, respectively, in which the red atom is the HCP structure, the green atom is FCC structure, and the white atom is GB atom. It is obvious that with the increase in compression, the number of atoms in the GB increases, the GB diffuses, and the atoms of the FCC structure increase gradually, and the FCC stacking faults increase. The FCC stacking fault first forms at the GB and then expands into the grain. The formation principle is as follows: due to the compression, the position of the HCP structure atom changes and becomes the GB atom. With the increase in the squeezing amount, the GB atom forms an FCC stacking fault.

Figure 6 
                  Grain boundary evolution: (a) fraction curve of GI atoms, (b) fraction curve of GB atoms (c) figure of CNA under PSC and (d) figure of CNA in UC.
Figure 6

Grain boundary evolution: (a) fraction curve of GI atoms, (b) fraction curve of GB atoms (c) figure of CNA under PSC and (d) figure of CNA in UC.

Figure 7 shows structural evolution. Figure 7a–c shows the fractional curve of HCP, FCC, and BCC structure, respectively. It can be seen that the change of grain internal (GI) atoms curve is mainly caused by HCP structure and FCC structure, while the proportion of the BCC structure is very small. The structural change of PSC is earlier than that of UC, and the number of BCC atoms in PSC is slightly more than that of UC. The changes of HCP structure and FCC structure are earlier than the occurrence of plastic deformation. In the process of compression, the atoms of the HCP structure first become GB atoms. With the increase in the amount of compression, the position of GB atoms continues to change, and some atoms form FCC stacking faults. Figure 7d–f shows the evolution diagram of each structure under PSC, and Figure 7g–i shows the evolution diagram of each structure under UC. It can be seen that under PSC, the occurrence of FCC stacking fault is earlier than that of UC and the occurrence of the BCC structure is earlier than that of UC. The FCC stacking fault occurs between the HCP structure and the GB, so that the phase structure transformation of HCP → GB → FCC occurs during compression.

Figure 7 
                  Structural evolution: (a) HCP structure fraction curve, (b) FCC structure fraction curve, (c) BCC structure fraction curve, (d)–(f) structural evolution diagram under PSC, and (g)–(i) structural evolution diagram under UC.
Figure 7

Structural evolution: (a) HCP structure fraction curve, (b) FCC structure fraction curve, (c) BCC structure fraction curve, (d)–(f) structural evolution diagram under PSC, and (g)–(i) structural evolution diagram under UC.

Figure 8 shows dislocation evolution. Figure 8a and b shows the dislocation evolution diagrams under PSC and UC, respectively. With the increase in the amount of squeezing, the atomic position changes, and the dislocation density increases. Figure 8c and d shows the dislocation density curves under PSC and UC, respectively. It is found that the dislocations in the model are mainly other dislocations and 1 3 1 ¯ 100 dislocations. Under PSC, the dislocation density in magnesium alloy is significantly higher than that in UC. This is because the Y-axis is fixed, and the atom can only move to the X-axis, resulting in more 1 3 1 ¯ 100 dislocations and other dislocations, resulting in more FCC stacking faults. The change of other dislocation density is almost the same as that of GB atom, and the change of 1 3 1 ¯ 100 dislocation is almost the same as that of FCC stacking fault. Table 1 presents the Bergson markings of common dislocations in closely packed hexagonal crystals. Among them, A B 1 3 11 2 ¯ 0 is the basal complete dislocation, T S ( [ 0001 ] ) is the cylindrical complete dislocation, S A / T B 1 3 11 2 ¯ 3 is the incomplete dislocation, and A σ ( A σ 1 3 1 ¯ 100 ) is the Shockley incomplete dislocation [66]. The strain corresponding to the increase of dislocation density is consistent with that when the atomic fraction of FCC structure begins to increase, so that there is a positive correlation between Shockley partial dislocations and FCC stacking faults.

Figure 8 
                  Dislocation evolution: (a) dislocation evolution diagram under PSC, (b) dislocation evolution diagram under UC, (c) dislocation density curve under PSC, and (d) dislocation density curve under UC.
Figure 8

Dislocation evolution: (a) dislocation evolution diagram under PSC, (b) dislocation evolution diagram under UC, (c) dislocation density curve under PSC, and (d) dislocation density curve under UC.

Table 1

Bergson marks of common dislocations in hexagonal close packed crystals [67]

Mark A B T S S A / T B A σ σ S A S
b 1 3 11 2 ¯ 0 [ 0001 ] 1 3 11 2 ¯ 3 1 3 1 ¯ 100 1 2 [ 0001 ] 1 6 2 ¯ 203

3.2 Effect of temperature on phase transition under PSC

The AZ31 magnesium alloy model with a size of 200 Å × 200 Å × 200 Å is imported into LAMMPS, then the potential function is assigned to the model, X, Y, and Z are all set as periodic boundary conditions, NPT ensemble is adopted, the time step is 0.001 ps, and the 10 ps is relaxed under 300–700 K, respectively. The change of temperature during the relaxation process is shown in Figure 9. Then, keeping the size of the Y-axis model unchanged, the PSC is realized by uniformly compressing 20 ps along the Z-axis ([0001] direction) at the strain rate of 0.01 ps−1.

Figure 9 
                  Temperature change during relaxation.
Figure 9

Temperature change during relaxation.

Figure 10 shows the grain evolution, Figure 10(a) shows the grain diagram, and Figure 10(b) shows the grain curve. It can be seen that the change in the number of grains is not very obvious with the change of temperature, and the number of grains at different temperatures is roughly the same. Therefore, it is speculated that temperature has little effect on grain refinement.

Figure 10 
                  Grain evolution: (a) grain diagram and (b) grain number curve.
Figure 10

Grain evolution: (a) grain diagram and (b) grain number curve.

Figure 11 shows the force–energy parameter curve under PSC, and Figure 11a shows the stress–strain curve. With the increase in temperature, the initial stress increases, the yield stress decreases, and the elastic modulus decreases. In the PSC process, with the increase in temperature, the potential energy of AZ31 magnesium alloy increases and plastic deformation occurs more easily, so the yield stress and yield strain decrease with the increase in temperature. Figure 11b shows the potential energy curve. The higher the temperature is, the more energy is obtained and the greater the potential energy is. Figure 11c is a volume curve. With the increase in the amount of compression, the elastic deformation first occurs and the volume decreases. When the strain reaches the yield strain, the volume begins to increase when the strain reaches the plastic stage. The higher the temperature is, the shorter the elastic stage is and the smaller the volume change is. Figure 11d shows the total dislocation density curve. With the increase in the amount of compression, the atomic position changes, and the total dislocation density increases.

Figure 11 
                  Force energy parameter curve: (a) stress–strain curve, (b) potential energy curve, (c) volume curve, and (d) total dislocation density curve.
Figure 11

Force energy parameter curve: (a) stress–strain curve, (b) potential energy curve, (c) volume curve, and (d) total dislocation density curve.

Figure 12 shows the evolution of the cavity, Figure 12a shows the cavity, and Figure 12b shows the cavity curve. It can be seen that cavityies appear at the same time as the yield time of magnesium alloy; so in the process of compression, cavities are generated with the change of atomic position, and at the end of elastic deformation, magnesium alloys begin to yield and enter the plastic stage, the number of cavity increases, and the area increases, increasing the overall volume of magnesium alloys.

Figure 12 
                  Cavity evolution: (a) cavity diagram and (b) cavity curve.
Figure 12

Cavity evolution: (a) cavity diagram and (b) cavity curve.

Figure 13 shows the evolution of grain boundaries under PSC, and Figure 13a shows the diagram of CNA. It is obvious that with the increase in compression, the number of atoms in the FCC structure increases, and the number of atoms in grain boundaries increases. When ε = 10 % , a large number of FCC stacking faults have occurred in the model. Figure 13b shows the GI atomic curve, and Figure 13c shows the GB atomic curve. It can be seen that the atomic fraction of GB decreases with the increase in compression, and the higher the temperature is, the higher the atomic fraction of GB is. When the atomic fraction of GB increases, the strain is about 4.5% smaller than the yield strain, so the phase transformation of magnesium alloy is earlier than plastic deformation.

Figure 13 
                  Grain boundary evolution under PSC: (a) CNA diagram, (b) GI atomic curve, and (c) GB atomic curve.
Figure 13

Grain boundary evolution under PSC: (a) CNA diagram, (b) GI atomic curve, and (c) GB atomic curve.

Figure 14 shows the structure evolution, Figure 14a shows the CNA diagram of HCP structure, Figure 14b shows the CNA diagram of the FCC structure, Figure 14c shows the CNA diagram of the BCC structure, Figure 14d shows the atomic curve of the HCP structure, Figure 14e shows the atomic curve of FCC structure, and Figure 14f shows the atomic curve of the BCC structure. It can be seen that the higher the temperature is, the earlier the atomic fraction of HCP begins to change, and the smaller the atomic fraction of the BCC structure is. When ε = 20 % , the atomic fraction curve of the FCC structure tends to be smooth. The higher the temperature is, the greater the potential energy of magnesium alloy is, the more active the atom is, and the position of magnesium alloy is easier to change. The earlier the HCP structure decreases, so the higher the temperature is, the smaller the yield strength is.

Figure 14 
                  Structural evolution: (a) CNA diagram of HCP structure, (b) CNA diagram of FCC structure, (c) CNA diagram of BCC structure, (d) atomic curve of HCP structure, (e) atomic curve of FCC structure, and (f) atomic curve of BCC structure.
Figure 14

Structural evolution: (a) CNA diagram of HCP structure, (b) CNA diagram of FCC structure, (c) CNA diagram of BCC structure, (d) atomic curve of HCP structure, (e) atomic curve of FCC structure, and (f) atomic curve of BCC structure.

Figure 15 shows the evolution of dislocations, Figure 15a shows the dislocation lines, and Figure 15b–f shows the dislocation density curves at different temperatures. With the increase in compression, the number of dislocation lines increases, the dislocation lines become longer, and the dislocation density increases. Among them, the dislocations with the highest dislocation densities are 1 3 1 ¯ 100 dislocations (Shockley partial dislocations) and other dislocations. With the increase in temperature, the densities of 1 3 1 ¯ 100 dislocations (Shockley partial dislocations) and other dislocations decrease. The strain corresponding to the increase of 1 3 1 ¯ 100 dislocation density is consistent with that when the atomic fraction of the FCC structure begins to increase, so that there is a positive correlation between Shockley partial dislocations and FCC stacking faults.

Figure 15 
                  Dislocation evolution: (a) dislocation line diagram and (b)–(f) dislocation density curve.
Figure 15

Dislocation evolution: (a) dislocation line diagram and (b)–(f) dislocation density curve.

3.3 Effect of strain rate on phase transformation under PSC

The AZ31 magnesium alloy model with a size of 200 Å × 200 Å × 200 Å is imported into LAMMPS, and the potential function is assigned to the model. X, Y, and Z are all periodic boundary conditions, using NPT ensemble, the time step is 0.001 ps, and the 10 ps is relaxed at 300 K. The change of temperature during the relaxation process is shown in Figure 16. Keeping the size of the Y-axis model unchanged, the model was uniformly compressed 20 ps along the Z-axis ([0001] direction) at 300 K at the strain rate of 0.001–0.1 ps−1 to achieve PSC.

Figure 16 
                  Temperature change during relaxation.
Figure 16

Temperature change during relaxation.

Figure 17 shows the grain evolution, Figure 17a shows the grain diagram, and Figure 17b presents the grain curve. It can be seen that there is no obvious rule in the number of grains at different strain rates, so it is inferred that the strain rate has no significant effect on the grain refinement of magnesium alloys.

Figure 17 
                  Grain evolution: (a) grain diagram and (b) grain curve.
Figure 17

Grain evolution: (a) grain diagram and (b) grain curve.

Figure 18 shows the force–energy parameter curve under PSC, and Figure 18a shows the stress–strain curve. When ε ̇ 0.01 ps 1 , the yield stress and elastic modulus increase gradually with the increase in the strain rate. When ε ̇ > 0.01 ps 1 , the magnesium alloy no longer yielded. Figure 18b shows a potential energy curve. The higher the strain rate is, the greater the potential energy of magnesium alloy is, and the greater the rate of potential energy increase is. Figure 18c shows a volume curve. When ε ̇ 0.01 ps 1 , as the number of compression increases, the elastic deformation first occurs and the volume decreases, and the larger the strain rate is, the greater the rate of volume reduction is. When the strain reaches yield strain, the volume begins to increase when the strain reaches the plastic stage. When ε ̇ > 0.01 ps 1 , the volume decreases all the time and the decreasing rate increases with the increase in the strain rate. Figure 18d shows the curve of total dislocation density, which increases with the increase in compression. However, the change of total dislocation density of ε ̇ > 0.01 ps 1 is different from that of ε ̇ 0.01 ps 1 .

Figure 18 
                  Force energy parameter curve: (a) stress–strain curve, (b) potential energy curve, (c) volume curve, and (d) total dislocation density curve.
Figure 18

Force energy parameter curve: (a) stress–strain curve, (b) potential energy curve, (c) volume curve, and (d) total dislocation density curve.

Figure 19 shows the evolution of cavitys, Figure 19a shows cavities, and Figure 19b shows cavitys curve. It can be seen that the time of appearance of the cavity is the same as the yield time of magnesium alloy, and so in the process of compression, with the change of atomic position, cavity is produced, at the end of elastic deformation, magnesium alloys begin to yield and enter the plastic stage, the number of cavity increases, and the volume increases, increasing the overall volume of magnesium alloys. With the increase in the strain rate, the cavity area decreases, and when ε ̇ = 0.1 ps 1 , there will be no more cavity in the model.

Figure 19 
                  Cavity evolution: (a) cavity diagram and (b) cavity curve.
Figure 19

Cavity evolution: (a) cavity diagram and (b) cavity curve.

Figure 20 shows the evolution of the GB, and Figure 20a shows the CNA diagram. It is obvious that with the increase in the amount of compression, the number of atoms in the FCC structure increases, and the number of atoms in the GB increases. With the increase in the strain rate, the FCC stacking fault occurs later. Figure 20b shows the GI atomic curve, and Figure 20c shows the GB atomic curve. It can be seen that the fraction of GB atoms increases with the increase in compression. The higher the strain rate, the later the growth of GB atoms and the greater the growth rate, so the strain rate affects the time and degree of phase transformation. The higher the rate is, the later the phase transformation is, and the greater the degree of phase transformation is.

Figure 20 
                  Grain boundary evolution: (a) CNA diagram, (b) GI atomic curve, and (c) GB atomic curve.
Figure 20

Grain boundary evolution: (a) CNA diagram, (b) GI atomic curve, and (c) GB atomic curve.

Figure 21 is the structure evolution under PSC, Figure 21a shows the CNA diagram of the HCP structure, Figure 21b shows the CNA diagram of the FCC structure, Figure 21c shows the CNA diagram of the BCC structure, Figure 21d shows the atomic curve of the HCP structure, Figure 21e shows the atomic curve of the FCC structure, and Figure 21f shows the atomic curve of the BCC structure. It can be seen that the higher the strain rate is, the later the atomic fraction of HCP begins to change. This is because the larger the strain rate is, the smaller the potential energy is, the less the atom is, and the position of the atom is not easy to change. The smaller the pore area is, the higher the strain rate is, the greater the yield strain is, and the greater the yield strength is. With the increase in the strain rate, the atomic fraction curves of the HCP structure and the FCC structure change later, while the strain phase of the BCC structure changes. The atomic fraction of the BCC structure increases with the increase in the strain rate. Therefore, the strain rate mainly affects the phase transition time and the degree of phase transformation.

Figure 21 
                  Structural evolution: (a) CNA diagram of HCP structure, (b) CNA diagram of FCC structure, (c) CNA diagram of BCC structure, (d) atomic curve of HCP structure, (e) atomic curve of FCC structure, and (f) atomic curve of BCC structure.
Figure 21

Structural evolution: (a) CNA diagram of HCP structure, (b) CNA diagram of FCC structure, (c) CNA diagram of BCC structure, (d) atomic curve of HCP structure, (e) atomic curve of FCC structure, and (f) atomic curve of BCC structure.

Figure 22 shows the evolution of dislocations, Figure 22a shows the dislocation lines, and Figure 22b–f shows the dislocation density curves at different temperatures. It can be seen that the dislocation densities at all strain rates increase with the increase in compression. In the process of compression, the dislocations with the highest dislocation density are still 1 3 1 ¯ 100 dislocations (Shockley partial dislocations) and other dislocations. The strain corresponding to the increase of 1 3 1 ¯ 100 dislocation density is still the same as that when the atomic fraction of the FCC structure begins to increase, so there is still a strong correlation between HCP transition FCC phase transition and Shockley partial dislocations.

Figure 22 
                  Dislocation evolution: (a) dislocation line diagram and (b)–(f) dislocation density curve.
Figure 22

Dislocation evolution: (a) dislocation line diagram and (b)–(f) dislocation density curve.

4 Conclusion

In this article, the compression simulation of AZ31 magnesium alloy is simulated by the MD method. The effects of loading mode, temperature, and strain rate on the compression behavior are analyzed. The lattice distortion, mechanical behavior, structural evolution, and dislocation evolution in the compression process are deeply analyzed, and the results of different loading modes are obtained. The HCP → FCC phase transformation mechanism of AZ31 magnesium alloy during compression at temperature and strain rate, which is related to the mechanical behavior, has been studied completely. The main results are as follows:

  1. PSC can improve the plasticity of AZ31 magnesium alloy and produce more severe grain refinement, GB diffusion, and phase transformation earlier, and the dislocation density is significantly higher than that of UC.

  2. The plastic deformation mechanism of magnesium alloy changes into GB diffusion due to the increase of temperature, which has no obvious effect on grain refinement and dislocation evolution. With the increase in temperature, the potential energy of magnesium alloy increases and plastic deformation occurs more easily, so the yield stress and yield strain decrease.

  3. The strain rate affects the time and degree of phase transformation. The higher the strain rate is, the later the phase transformation is, and the greater the degree of phase transformation is, the greater the yield strength and yield strain are.

  4. The phase transformation of HCP → GB → FCC occurs in AZ31 magnesium alloy during compression. With the increase in compression amount, the number of atoms in GB increases, the number of atoms in GB diffuses, the number of atoms in the FCC structure increases gradually, and the number of FCC stacking faults increases. Due to the compression, the position of the HCP structure atom changes and becomes the GB atom, resulting in Shockley partial dislocations. As the squeezing continues to increase, the GB atom becomes an FCC stacking fault.

  5. The phase transformation is before the specific plastic deformation in the compression process of magnesium alloy, and the yield occurs during the formation of the cavity. With the increase in the amount of compression, the elastic deformation of magnesium alloy occurs at first, the volume decreases, the atomic position changes gradually, and the phase transformation occurs. When a cavity occurs in the magnesium alloy, it begins to yield and enters the plastic stage, and the volume begins to increase.

  6. There is a strong correlation between Shockley partial dislocations and FCC stacking faults. The corresponding strain when the density of Shockley partial dislocations increases is consistent with that when the atomic fraction of FCC structure begins to increase.

Acknowledgments

This work was supported by the National Key Research and Development Project (2018YFB1307902), Shanxi Province Joint Student Training Base Talent Training Project (No. 2018JD33), Shanxi young top talent project, Shanxi Province Science Foundation for Youths (201901D211312), Excellent young academic leaders in Shanxi colleges and universities (No. 2019045), Excellent Achievements Cultivation Project of Shanxi Higher Education Institutions (No. 2019KJ028), Shanxi Province emerging industry leader talent project, Shanxi Graduate Education Innovation Project (No. 2019SY482).

  1. Funding information: This work was supported by the National Key Research and Development Project (2018YFB1307902), Shanxi Province Joint Student Training Base Talent Training Project (No. 2018JD33), Shanxi young top talent project, Shanxi Province Science Foundation for Youths (201901D211312), Excellent young academic leaders in Shanxi colleges and universities (No. 2019045), Excellent Achievements Cultivation Project of Shanxi Higher Education Institutions (No. 2019KJ028), Shanxi Province emerging industry leader talent project, Shanxi Graduate Education Innovation Project (No. 2019SY482).

  2. Author contributions: Q.H. Yang ideated, designed the study and analyzed the results. Q.H. Yang carried out the MC/MD structure evolution analysis, dislocation visualization analysis and making the figures. Z.B. Chu contributed to the overall guidance for the work and provided financial support. C. Xue, B.W. Yang, Y.G. Li, L.F. Tuo and H. Gao provided ideas. All authors have accepted responsibility for the entire content of this manuscript and approved its submission.

  3. Conflict of interest: The authors declare that they have no conflict of interest.

  4. Data availability statement: The datasets generated during and/or analyzed during the current study are available from the corresponding author on reasonable request.

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Received: 2021-09-15
Revised: 2021-11-03
Accepted: 2022-02-17
Published Online: 2022-07-05

© 2022 Qianhua Yang et al., published by De Gruyter

This work is licensed under the Creative Commons Attribution 4.0 International License.

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  115. Achieving excellent oxidation resistance and mechanical properties of TiB2–B4C/carbon aerogel composites by quick-gelation and mechanical mixing
  116. Microwave-assisted sol–gel template-free synthesis and characterization of silica nanoparticles obtained from South African coal fly ash
  117. Pulsed laser-assisted synthesis of nano nickel(ii) oxide-anchored graphitic carbon nitride: Characterizations and their potential antibacterial/anti-biofilm applications
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  119. Benzaldehyde derivatives on tin electroplating as corrosion resistance for fabricating copper circuit
  120. Mechanical and heat transfer properties of 4D-printed shape memory graphene oxide/epoxy acrylate composites
  121. Coupling the vanadium-induced amorphous/crystalline NiFe2O4 with phosphide heterojunction toward active oxygen evolution reaction catalysts
  122. Graphene-oxide-reinforced cement composites mechanical and microstructural characteristics at elevated temperatures
  123. Gray correlation analysis of factors influencing compressive strength and durability of nano-SiO2 and PVA fiber reinforced geopolymer mortar
  124. Preparation of layered gradient Cu–Cr–Ti alloy with excellent mechanical properties, thermal stability, and electrical conductivity
  125. Recovery of Cr from chrome-containing leather wastes to develop aluminum-based composite material along with Al2O3 ceramic particles: An ingenious approach
  126. Mechanisms of the improved stiffness of flexible polymers under impact loading
  127. Anticancer potential of gold nanoparticles (AuNPs) using a battery of in vitro tests
  128. Review Articles
  129. Proposed approaches for coronaviruses elimination from wastewater: Membrane techniques and nanotechnology solutions
  130. Application of Pickering emulsion in oil drilling and production
  131. The contribution of microfluidics to the fight against tuberculosis
  132. Graphene-based biosensors for disease theranostics: Development, applications, and recent advancements
  133. Synthesis and encapsulation of iron oxide nanorods for application in magnetic hyperthermia and photothermal therapy
  134. Contemporary nano-architectured drugs and leads for ανβ3 integrin-based chemotherapy: Rationale and retrospect
  135. State-of-the-art review of fabrication, application, and mechanical properties of functionally graded porous nanocomposite materials
  136. Insights on magnetic spinel ferrites for targeted drug delivery and hyperthermia applications
  137. A review on heterogeneous oxidation of acetaminophen based on micro and nanoparticles catalyzed by different activators
  138. Early diagnosis of lung cancer using magnetic nanoparticles-integrated systems
  139. Advances in ZnO: Manipulation of defects for enhancing their technological potentials
  140. Efficacious nanomedicine track toward combating COVID-19
  141. A review of the design, processes, and properties of Mg-based composites
  142. Green synthesis of nanoparticles for varied applications: Green renewable resources and energy-efficient synthetic routes
  143. Two-dimensional nanomaterial-based polymer composites: Fundamentals and applications
  144. Recent progress and challenges in plasmonic nanomaterials
  145. Apoptotic cell-derived micro/nanosized extracellular vesicles in tissue regeneration
  146. Electronic noses based on metal oxide nanowires: A review
  147. Framework materials for supercapacitors
  148. An overview on the reproductive toxicity of graphene derivatives: Highlighting the importance
  149. Antibacterial nanomaterials: Upcoming hope to overcome antibiotic resistance crisis
  150. Research progress of carbon materials in the field of three-dimensional printing polymer nanocomposites
  151. A review of atomic layer deposition modelling and simulation methodologies: Density functional theory and molecular dynamics
  152. Recent advances in the preparation of PVDF-based piezoelectric materials
  153. Recent developments in tensile properties of friction welding of carbon fiber-reinforced composite: A review
  154. Comprehensive review of the properties of fly ash-based geopolymer with additive of nano-SiO2
  155. Perspectives in biopolymer/graphene-based composite application: Advances, challenges, and recommendations
  156. Graphene-based nanocomposite using new modeling molecular dynamic simulations for proposed neutralizing mechanism and real-time sensing of COVID-19
  157. Nanotechnology application on bamboo materials: A review
  158. Recent developments and future perspectives of biorenewable nanocomposites for advanced applications
  159. Nanostructured lipid carrier system: A compendium of their formulation development approaches, optimization strategies by quality by design, and recent applications in drug delivery
  160. 3D printing customized design of human bone tissue implant and its application
  161. Design, preparation, and functionalization of nanobiomaterials for enhanced efficacy in current and future biomedical applications
  162. A brief review of nanoparticles-doped PEDOT:PSS nanocomposite for OLED and OPV
  163. Nanotechnology interventions as a putative tool for the treatment of dental afflictions
  164. Recent advancements in metal–organic frameworks integrating quantum dots (QDs@MOF) and their potential applications
  165. A focused review of short electrospun nanofiber preparation techniques for composite reinforcement
  166. Microstructural characteristics and nano-modification of interfacial transition zone in concrete: A review
  167. Latest developments in the upconversion nanotechnology for the rapid detection of food safety: A review
  168. Strategic applications of nano-fertilizers for sustainable agriculture: Benefits and bottlenecks
  169. Molecular dynamics application of cocrystal energetic materials: A review
  170. Synthesis and application of nanometer hydroxyapatite in biomedicine
  171. Cutting-edge development in waste-recycled nanomaterials for energy storage and conversion applications
  172. Biological applications of ternary quantum dots: A review
  173. Nanotherapeutics for hydrogen sulfide-involved treatment: An emerging approach for cancer therapy
  174. Application of antibacterial nanoparticles in orthodontic materials
  175. Effect of natural-based biological hydrogels combined with growth factors on skin wound healing
  176. Nanozymes – A route to overcome microbial resistance: A viewpoint
  177. Recent developments and applications of smart nanoparticles in biomedicine
  178. Contemporary review on carbon nanotube (CNT) composites and their impact on multifarious applications
  179. Interfacial interactions and reinforcing mechanisms of cellulose and chitin nanomaterials and starch derivatives for cement and concrete strength and durability enhancement: A review
  180. Diamond-like carbon films for tribological modification of rubber
  181. Layered double hydroxides (LDHs) modified cement-based materials: A systematic review
  182. Recent research progress and advanced applications of silica/polymer nanocomposites
  183. Modeling of supramolecular biopolymers: Leading the in silico revolution of tissue engineering and nanomedicine
  184. Recent advances in perovskites-based optoelectronics
  185. Biogenic synthesis of palladium nanoparticles: New production methods and applications
  186. A comprehensive review of nanofluids with fractional derivatives: Modeling and application
  187. Electrospinning of marine polysaccharides: Processing and chemical aspects, challenges, and future prospects
  188. Electrohydrodynamic printing for demanding devices: A review of processing and applications
  189. Rapid Communications
  190. Structural material with designed thermal twist for a simple actuation
  191. Recent advances in photothermal materials for solar-driven crude oil adsorption
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