1 Introduction

High-entropy alloys (HEAs) show great potential in breaking the property limits of metals and provide a flexible model to accelerate the development of physical metallurgy.[1,2] Recently, heterogeneous grain structure (HGS) has shown a great chance in balancing the strength and ductility of metals and alloys.[3,4,5] This efficient strengthening approach has also been applied to enhance the mechanical properties of HEAs.[6,7] Broadly speaking, multiscale-grain HEAs,[8,9,10] eutectics HEAs,[11,12,13] and precipitation-hardened HEAs[14,15,16,17] can also be viewed as HGS HEAs. Such combinations of HGS strengthening strategy and multiprincipal alloys design concept have achieved remarkable properties, opening an effective way to overcome strength–ductility trade-off.[18,19,20,21]

Meanwhile, it is widely recognized that the HGS can be obtained by partial recrystallization, which is the handiest and most economical thermal–mechanical processing (TMP).[5] Recrystallization refers to the transformation of a metastable deformation state to a stable recrystallization state.[22] However, the reported TMP processes to get partially recrystallized samples are inefficient. It relies on a time-consuming trial-and-error approach, especially in the choice of annealing temperature and time. For example, HGS with 39 pct recrystallized fraction and 76 pct recrystallized fraction were obtained when annealed at 600 for 1 and 4 hours, respectively, in the single-phase NiCoCr HEA with 70 pct reduction in thickness.[9] Similar HGS microstructure was also obtained in Al0.1CoCrFeNi at 600 °C for 1 hour of annealing.[23] A full recrystallization microstructure can be obtained in NiCoCr by annealing for 1 hour at temperatures higher than 700 °C.[9] These works showed that annealing temperature and time significantly influenced the recrystallization volume, but related quantified study describing the relationship among these three parameters is still limited. In addition, HGS was retained in Ti and Al doped NiCoCr HEA when annealed at 900 °C for 1 hour, indicating that the addition of Ti and Al changed the recrystallization kinetics.[8] The higher recrystallization temperature caused by the addition of Ti and Al was also be found in NiCoCrFeMn HEA.[24] It is, therefore, obvious that the recrystallized kinetics varied with the chemical compositions of HEAs. However, the origin of this composition dependence is still not fully understood. In light of the above two points, the quantified study on recrystallization kinetics of HEAs becomes the prerequisite for precisely adjusting of HGS.

As for the recrystallization kinetics of HEAs, Annasamy et al.[25,26] reported that NiCoCrFeAlx exhibited a decreased rate of recrystallization comparing with traditional alloys because of a high activation energy (549 kJ·mol−1). This high activation energy was attributed to the distorted lattice, sluggish diffusion, and the interaction between Al–Ni rich precipitates and recrystallization. A low activation energy of ~ 232.7 kJ·mol−1 was obtained in single-phase HEA NiCoCrFeN0.7.[27] It was again attributed to the sluggish diffusion effect of HEAs. However, the sluggish diffusion effect has been debated in recent years.[28,29,30] On the other hand, stacking fault energy has been suggested to play a role in the recrystallization of HEAs. For example, the recrystallization kinetics of Fe50Mn30Co10Cr10 were enhanced by the reverse transformation of strain-induced martensite. Meanwhile, an even lower recrystallization activation energy of 108 kJ·mol−1 was obtained for this HEA. The authors argued that the low stacking fault energy (SFE) of the Fe50Mn30Co10Cr10 HEA led to the phase transformation and thus low recrystallization activation energy.[31] In addition, Wu et al.[32] also reported that SFE could profoundly affect the recrystallization kinetics of HEAs. Despite these pioneering works, two important issues concerning the recrystallization of HEAs remain unclear. Firstly, the recrystallization kinetics of single-phase HEAs, which are the most used systems in obtaining HGS, are still limited. Secondly, how SFE affects the recrystallization behavior of HEAs is still confusing.

Therefore, we in the current study investigated the static recrystallization behaviors of two single-phase HEAs of NiCoCrFe and Ni2CoCrFe with different SFE[33,34,35] using the metallographic method. The recrystallization kinetics of the two HEAs were analyzed using the Arrhenius equation and Johnson–Mehl–Avrami–Kolmogorov (JMAK) model which applies to describe the kinetics of materials.[36] Scanning electron microscope (SEM), electron backscattered diffraction (EBSD), transition electron microscope (TEM) were used to characterize deformed microstructures and to uncover the effect of SFE on the recrystallization kinetics of single-phase HEAs.

2 Experiments

Samples of NiCoCrFe and Ni2CoCrFe were produced by arc melting pure (> 99.5 pct) constituent metals under an argon atmosphere in which Ti getter was employed to prevent potential oxygen contamination and then casted into a copper mold with the dimension of 50 mm × 10 mm × 5 mm. Each sample was remelted for four times to promote the chemical homogeneity. Ingots were further homogenized for 2 hours at 1200 °C followed by water quenching. After homogenized treatment, HEAs were cold-rolled to ~ 1.5 mm (~ 70 pct thickness reduction). The recrystallization heat treatment was carried out at 575, 600, and 650 °C from 5 to 300 minutes unequally and quenched in water to keep the recrystallized microstructure. Selection of the annealing temperature was based on the empirical recrystallization temperature ~ 0.6 Tm (melting point), which was an appropriate temperature to study the recrystallization kinetics and ensure the fully recrystallization within an acceptable and controllable annealing time (the melting point was calculated by the JMatPro with the Nickel-based Superalloy database in Figure 8). Considering the requirement of annealing time and accuracy of experiment, 575 °C and 650 °C were also chosen to study the recrystallization kinetics since the activation energy can be obtained from the Arrhenius equation of different temperatures. Selection of the annealing time was random from 5 to 300 minutes and interval of annealing time became larger with time increasing.

The X-ray diffraction (XRD) patterns of the homogenized, cold-rolled and annealed samples were obtained by Rigaku d/max-2550 with monochromator. The SEM samples were initially grinded to 2500-grit SiC paper, then electron-polished in a solution of perchloric acid and alcohol (50:450 mL) with a direct voltage of 30 V for 8–10 seconds at ambient temperature, and finally analyzed by SEM (Tescan MIRA3) equipped with back scattered electron (BSE) and EBSD detectors (Oxford Instruments). The method described in Reference [37] was adopted here to obtain recrystallized fraction and the average value of three images with view field of 800 μm was used as one data point. TEM (JEOL 2100F) was used to identify the deformation microstructures under 200 kV. A twin-jet polishing technique was used to prepare the TEM specimens. Sheet samples with the thickness of 0.5 mm were first cut from the center of the samples by electrical discharged machining (EDM) and then mechanically ground to a thickness of ~ 50 μm using SiC papers. Then the samples were punched into 3-mm-diameter disks and further thinned in a mixture of a 10 pct volume percent perchloric acid and 90 pct alcohol at – 30 °C with 50 V. The dog-bone specimens with gauge dimension of 12.5 × 1.2 × 3 mm3 were prepared for the tensile test with a strain rate of 1 × 10−3 s−1 at ambient temperature.

3 Results and Discussion

XRD patterns of the initial and annealed microstructures of NiCoCrFe and Ni2CoCrFe are presented in Figure 1. NiCoCrFe is denoted as A and Ni2CoCrFe is denoted as B; meanwhile H, CR and PRX are used to represent homogenized state, cold-rolled state, partially recrystallized state. PRX samples, NiCoCrFe and Ni2CoCrFe are annealed for 53 and 61 minutes under 600 °C, respectively. From the characteristic peaks, fcc structure can be clearly identified, indicating that all the microstructures of homogenized, cold-rolled, and partially recrystallized states are single-phase fcc structure.

Fig. 1
figure 1

XRD patterns of NiCoCrFe and Ni2CoCrFe under cold-rolled, homogenized and partially recrystallized states

The representative images for different stages of the recrystallization process, i.e., the begin of recrystallization (< 10 pct), low recrystallization fraction (10–30 pct), high recrystallization fraction (50–70 pct), and almost full recrystallization (> 90 pct) are shown in Figures 2 and 3. Figure 2 shows the representative partially recrystallized microstructures of NiCoCrFe. As shown in Figure 2(a), deformed NiCoCrFe starts to recrystallize after 11 minutes annealing at 600 °C. The recrystallized grains are featured by clear boundary and uniform contrast under BSE mode. The fraction of recrystallized area increases as the annealing time increases (Figures 2(b) and (c)). The microstructure of NiCoCrFe after annealed for 75 minutes at 600 °C in Figure 2(d) shows that recrystallized fraction reaches up to 95 pct. A similar microstructure evolution is observed in Ni2CoCrFe (Figures 3(a) through (d)). The quantified recrystallized fractions as a function of annealing time at different temperatures are presented in Figure 4, and the representative microstructures used for measuring the recrystallized volume fractions can be seen in Electronic Supplementary Figures S1, S2, S3, S4, S5, S6, S7, S8, S9, S10, S11, S12, S13, S14, S15, S16, S17, S18, S19, S20, S21, S22, S23, S24, S25, and S26. It is intriguing that the two HEAs show significant difference in recrystallization kinetics even though the compositions of the two HEAs are highly similar and undergo the same thermal–mechanical processing. For example, according to Figure 4(b), at 600 °C the 50 pct recrystallized fraction need ~ 20 minutes for NiCoCrFe, while more than 40 minutes is required for Ni2CoCrFe. A similar trend in recrystallization kinetics of the two HEAs is also observed at 575 °C and 650 °C in Figures 4(a) and (c). All kinetics curves show that NiCoCrFe owns a faster rate of recrystallization than Ni2CoCrFe.

Fig. 2
figure 2

Partially recrystallized microstructures of NiCoCrFe under 600 °C. (a) 11 min, (b) 14 min, (c) 60 min, and (d) 75 min

Fig. 3
figure 3

Partially recrystallized microstructures of Ni2CoCrFe under 600 °C. (a) 5 min, (b) 25 min, (c) 35 min, and (d) 75 min

Fig. 4
figure 4

Recrystallized fraction of NiCoCrFe and Ni2CoCrFe vs. time under different temperatures. (a) 575 °C, (b) 600 °C, and (c) 650 °C

Here the JMAK model is adapted to quantitatively understand the recrystallization behaviors of the studied HEAs[22]:

$$X= 1-\mathrm{exp}\left(-B{t}^{n}\right),$$
(1)

where \(X\) represents the recrystallized fraction of alloys \((\mathrm{pct})\), \(t\) is the annealing time at the fixed temperature, \(B\) is a constant, and \(n\) is the Avrami exponent related with nucleation and growth pattern of the recrystallization. From the slopes of the Avrami plots, i.e., \(\mathrm{log}\left[\mathrm{ln}(1/(1-X))\right]\) vs. \(\mathrm{log}\left[\mathrm{ln}t\right]\) in Figures 5(a) and (b), the values of \(n\) can be calculated, whose values of NiCoCrFe and Ni2CoCrFe locate in 1.24 to 1.72 and 1.24 to 1.83, respectively. According to fitted \(B\) and \(n\), Figures 5(c) and (d) show the recrystallized fractions of both NiCoCrFe and Ni2CoCrFe, from which it is obvious to find that both single-phase HEAs exhibit sigmoidal forms and short incubation periods of ~ 2 minutes at the investigated temperatures. After the incubation period, the recrystallization rate gradually increases up to 50 pct recrystallized fraction (midpoint), after which rate would decrease and stop at almost fully recrystallized fraction (~ 95 pct). According to the traditional definition of the recrystallization temperature (at which the material has 50 pct recrystallized fraction in 1 hour heating treatment),[22] recrystallization temperatures of 70 pct cold-rolled NiCoCrFe and Ni2CoCrFe are around 600 °C.

Fig. 5
figure 5

Recrystallization kinetics of NiCoCrFe and Ni2CoCrFe under cold-rolled 70 pct. (a, b) JMAK plots, and (c, d) recrystallized fraction vs. time plots

By comparing the two HEAs’ recrystallization behaviors, it is surprising that the recrystallization rate of NiCoCrFe is faster than that of Ni2CoCrFe under the same deformation and annealing conditions, which means a higher stored energy in NiCoCrFe. To understand the difference between the recrystallization kinetics of the two HEAs, the activation energies of recrystallization are analyzed using Arrhenius equation[22]:

$$\frac{1}{t}=A\mathrm{exp}\left(-\frac{Q}{RT}\right),$$
(2)

where \(t\) is the time of reaching the specific recrystallized fraction (50 pct was adopted here, \({t}_{0.5}\)), \(R\) and \(T\) are the universal gas constant and annealing temperature, respectively, \(A\) is the pre-exponential factor, and \(Q\) is the activation energy of recrystallization (kJ·mol−1), which can be extracted from the slopes of the curves in Figure 6: 234 and 221 kJ·mol−1 for NiCoCrFe and Ni2CoCrFe, respectively.

Fig. 6
figure 6

Recrystallization activation energy of NiCoCrFe (Q1) and Ni2CoCrFe (Q2) under 70 pct cold-rolled deformation

In the classical theory,[22] there are four main factors affecting the recrystallization kinetic, (a) initial grain size; (b) degree of deformation; (c) temperature of annealing; and (d) compositions of alloys, among which the prior three factors can be easily excluded since that (a) two alloys owned the same initial grain size of ~ 1 mm (Figure 7); (b) deformation degree had been strictly controlled around ~ 70 pct; (c) two alloys were under the same temperature and annealing circumstances.

Fig. 7
figure 7

BSE images of homogenized microstructures at 1200 °C for 2 h. (a) NiCoCrFe, and (b) Ni2CoCrFe

Thus, it is rational to consider the composition factor that affects recrystallization kinetic. Traditionally, composition variation of alloys will mainly affect its properties: (1) melting point; (2) diffusivity; (3) stacking fault energy.

(1) Melting point, the heating temperature of 873 K (600 °C) is referred to as the 0.522Tm for NiCoCrFe (melting point is around 1400 °C) and 0.513Tm for Ni2CoCrFe (melting point of is around 1426 °C). Melting points of two alloys were calculated here by JMatPro software according to the Nickel-based Superalloy database in Figure 8 with a small difference of 26 °C. After transforming the Centigrade to Kelvin temperature, the heating temperature of 873 K (600 °C) is referred to as the 0.522Tm for NiCoCrFe and 0.513Tm for Ni2CoCrFe. Essentially, shear modulus correlated with melting points determines the value of stored energy and higher melting point means higher stored energy.[22] However, interestingly, NiCoCrFe owns a higher stored energy but lower melting point than Ni2CoCrFe and the melting point difference cannot explain such phenomenon.

Fig. 8
figure 8

Calculated phase diagrams of two alloys based on TTNi8 database. (a) NiCoCrFe and (b) Ni2CoCrFe

(2) Diffusivity, activation energies for bulk diffusion of each element in the NiCoCrFe HEA sample are listed in Table I where Cr has the highest activation energy (323 kJ mol−1) and Co has the lowest one (240 kJ mol−1). Interestingly, the QRX extracted from the slope of the curve in Figure 6 amounts to 234 kJ mol−1 for NiCoCrFe, which are slightly less than the activation energy of bulk diffusion of Co (240 kJ mol−1). With the increase of Ni content, corresponding values for Ni2CoCrFe has not been provided. According to Vaidya’s report,[31] configuration of the constituents has a huge impact on the atomic diffusion and activation energy. In this regard, the average enthalpy of mixing for all individual components in the NiCoCrFe and Ni2CoCrFe have been calculated from the following expression.[31] Here, mixing enthalpy of binary pairs of elements of the multicomponent alloys are listed in Table II. Ideally, Ni2CoCrFe is viewed as the equiatomic alloy which each element’s mixing enthalpy is the same as NiCoCrFe.

Table I Activation Energies (kJ mol−1) for Bulk Diffusion of Each Constituent Elements in NiCoCrFe[28]
Table II Mixing Enthalpy of Binary Pairs of Elements of the Multicomponent Alloys[28]
$$\Delta {H}_{\mathrm{avg}}^{i}=\frac{\sum_{\begin{array}{c}j=1\\ j\ne i\end{array}}^{n}\Delta {H}_{\mathrm{mix}\left(ij\right)}}{n}.$$
(3)

\(\Delta {H}_{\mathrm{mix}\left(ij\right)}\) is the binary mixing enthalpy of ith and jth element that was listed in Table III with the consideration of each element volume fraction.[31] A more negative value of \(\Delta {H}_{\mathrm{avg}}^{\mathrm{all}}\) in Ni2CoCrFe (− 2.6) than NiCoCrFe (− 2.5) suggests a relatively strong binding of composed elements and hence an increased activation barrier for diffusion in Ni2CoCrFe. However, the extrapolated recrystallization activation energies show the reverse result compared with the analyzed diffusion activation, implying bulk diffusion cannot control the recrystallization process in Ni–Co–Cr–Fe alloys which means the effect of diffusivity can also be excluded.

Table III Average Enthalpies of Mixing (\(\Delta {H}_{\mathrm{avg}}^{i}\)) for All Constituents in NiCoCrFe and Ni2CoCrFe With the Consideration of Element Volume Fraction

(3) Stacking fault energy, related studies have shown that the lower content of Ni causes a lower SFE in Ni–Co–Cr–Fe system,[33,34,35] it is, therefore, reasonable to assume that the deformed state, which is significantly influenced by SFE, might be responsible for the difference in recrystallization kinetics of two HEAs. As shown in Figures 9(a) and (b), it is also obvious that two alloys exhibit different deformation microstructures. The deformed NiCoCrFe shows many fringes with lighter contrast, which are hardly observed in deformed Ni2CoCrFe. This difference in deformed microstructures between the two HEAs is confirmed by high-magnification BSE images in Figures 9(c) and (d).

Fig. 9
figure 9

BSE images of deformed microstructures after cold-rolled 70 pct. (a, c) NiCoCrFe, and (b, d) Ni2CoCrFe

To further understand these deformed microstructures, high-resolution EBSD and TEM analysis are carried out. Figures 10(a) and (c) respectively show the inverse pole figure (IPF) images of deformed NiCoCrFe and Ni2CoCrFe, from which deformation twins (60 deg misorientation regions) are found in NiCoCrFe. As a contrast, there are only small misorientation changes in Ni2CoCrFe across the profile line in Figures 10(b) and (d). The unindexed areas in Figure 10(c) are caused by the highly localized deformation in the slip bands and beyond the resolution limit required for reliable EBSD indexing.

Fig. 10
figure 10

EBSD images of deformed microstructures of NiCoCrFe and Ni2CoCrFe cold-rolled ~ 70 pct. (a) IPF image of NiCoCrFe, (b) cumulative disorientation image of NiCoCrFe, (c) IPF image of Ni2CoCrFe, and (d) cumulative disorientation image of Ni2CoCrFe

These characters of the two HEAs are also confirmed by TEM. Both bight field (BF) and dark field (DF) graphs of the same area are obtained with selected area diffraction pattern (SAD) (Figure 11(a)), confirming the existence of typical deformation twins. However, there are only dislocation cells detected in BF with single set of diffraction pattern in Ni2CoCrFe (Figure 11(b)). The different deformation mechanisms also result in distinct strain hardening behaviors. As shown in Figure 12, tensile stress of initial homogenized microstructure of NiCoCrFe is always higher than Ni2CoCrFe. The different deformation mechanisms of the two HEAs are fully understandable since the decrease of Ni content can decrease the SFE and thus promote deformation twinning.[34,38] Therefore, in the following, our discussion will focus on the effect of deformation twins on the recrystallization kinetics of HEAs.

Fig. 11
figure 11

TEM images of deformed microstructures of NiCoCrFe and Ni2CoCrFe under cold-rolled 70 pct. (a) Bright field image of NiCoCrFe, the insets are the dark field image and the SAD corresponding to the same area. (b) Bright field image of Ni2CoCrFe, the inset is the corresponding SAD

Fig. 12
figure 12

Multi-tensile tests of the strength of NiCoCrFe and Ni2CoCrFe under homogenized state

On the one hand, it has been found that the deformation twins will hinder the dislocation movement and thus improve the storied energy of driving the recrystallizations.[39,40,41] According to Bailey–Hirsch relationship,[42] \(\sigma ={\sigma }_{\mathrm{y}}+MG\alpha b\sqrt{\rho }\) where the strain hardening ability is proportional to the square root of dislocation density, so it is reasonable to argue that a higher strain hardening may correspond to a higher dislocation density. As shown in Figure 12, the homogenized NiCoCrFe (σy ~ 188 MPa, σUTS ~ 479 MPa) shows a similar yield strength but higher ultimate stress during deformation compared with Ni2CoCrFe (σy ~ 174 MPa, σUTS ~ 429 MPa). Therefore, there is a higher dislocation density of the homogenized NiCoCrFe, which is induced by its characteristic deformation twins compared with the homogenized Ni2CoCrFe.

On the other hand, deformation twins can also significantly affect microstructural inhomogeneity,[43,44] which will act as the preferred nucleation sites of recrystallization. For instance, it has been found in α-titanium[43] that twin boundaries and twinning-induced crystallographic lattice reorientation can improve the microstructural inhomogeneity, leading to a promoted static recrystallization process. In addition, more nucleation sites were also found in shear bands, grain boundaries and triple junctions of the Fe–Mn–C alloys,[44] which were all inhomogeneities with localized orientation gradients. Similarly, in the present study, the deformation twins can also increase the heterogeneity of microstructure and act as the preferential nucleation sites for recrystallization.

Figure 13 shows the partially recrystallized microstructure of NiCoCrFe annealing for 53 minutes and Ni2CoCrFe annealing for 61 minutes both under 600 °C. The nucleation patterns can be deduced from these characteristic partially recrystallized areas. As Figures 13(a) and (d) demonstrated, both two alloys nucleate at grain boundaries because grain boundary owns quantities of defects and high stored energy. The curve divides the recrystallized area and non-recrystallized area. In Figures 13(b) and (c), the distinct microstructures show different intragranular nucleation methods of two alloys. Figure 13(b) presents the intersection recrystallization areas in which the straight lines show the nucleation of twins and the curves show the nucleation of slip bands. Because of the existence of deformation twins, there are more potential nucleation sites in NiCoCrFe. In Ni2CoCrFe, only slip bands nucleation area exists which is circled by curves. Other characteristic nucleation areas under higher magnification in Figures 13(c) and (d) also prove the existence of nucleation methods of deformation twins and slip bands in NiCoCrFe, while only slip bands nucleation in Ni2CoCrFe. These recrystallization nucleation modes are also supported by Avrami exponent. In Figure 5, Avrami exponent of NiCoCrFe varies between 1.24 and 1.72, and that of Ni2CoCrFe varies between 1.24 and 1.83. These values indicate that the investigated HEAs do not follow the traditional site-saturated nucleation or random nucleation mechanisms, for which the Avrami exponents separately equal to 3 or 4.[43,45] Such deviation of n from the classic values should be due to the heterogeneous recrystallization nucleation in Figure 13.[45] Through the comparison of nucleation methods for two alloys, it indicates that more potential nucleation sites provided by twins cause a higher recrystallization rate and lead to faster recrystallization kinetics for NiCoCrFe consequently.

Fig. 13
figure 13

BSE images of partially recrystallized microstructures of NiCoCrFe at 600 °C, 53 min and Ni2CoCrFe at 600 °C, 61 min. (a) Grain boundary nucleation of NiCoCrFe, (b, c) intragranular nucleation of NiCoCrFe, (d) grain boundary nucleation of Ni2CoCrFe, and (e, f) intragranular nucleation of Ni2CoCrFe

As a summary of former discussion, the role of deformation twins playing in the faster kinetics of recrystallization of NiCoCrFe can be concluded from two aspects. (1) Deformation twins result in higher stored energy by enhancing strain hardening capacity. (2) Deformation twins provide more potential nucleation sites for recrystallization.

4 Conclusion

In the present work, the recrystallization kinetics of single-phase Ni–Co–Cr–Fe HEAs with different SFE were investigated. The major motivations of the current study were the lack of the quantified recrystallization kinetics as well as the unclarified mechanism of SFE effect the on recrystallization of HEAs. With the aid of SEM, EBSD, and TEM, we demonstrated that the increased stacking fault energy in Ni–Co–Cr–Fe-based single-phase HEAs can slow the recrystallization kinetics. Related deformation behaviors of two alloys had been studied and the recrystallization mechanism were discussed. The following conclusions can be made:

  • Recrystallization kinetics curves of the single-phase Ni–Co–Cr–Fe HEAs show favorable coincidences with the JMAK model. The Avrami exponent of NiCoCrFe varies between 1.24 and 1.72, and that of Ni2CoCrFe varies between 1.24 and 1.83.

  • Under 70 pct cold-rolled deformation and 600 °C annealing temperature, NiCoCrFe shows higher recrystallization kinetics compared with Ni2CoCrFe, though two HEAs have almost identical activation energies of 234 and 221 kJ·mol−1 based on the Arrhenius equation.

  • Profound deformation twins are found in NiCoCrFe while hardly detected in Ni2CoCrFe by EBSD boundary disorientation analysis and the selected area diffraction pattern in TEM.

  • Deformation twins result in higher local stored strain energy by enhancing strain hardening capacity and providing more potential nucleation sites, accelerating the recrystallization rate of NiCoCrFe. Based on these findings, the kinetics of recrystallization of HEAs can be controlled by adjusting the SFE of HEAs.