Materials Transactions, Vol. 56, No. 7 (2015) pp. 963 to 972 Special Issue on Long-Period Stacking Ordered Structure and Its Related Materials II © 2015 The Japan Institute of Metals and Materials Crystal Plasticity Analysis of Development of Intragranular Misorientations due to Kinking in HCP Single Crystals Subjected to Uniaxial Compressive Loading Tsuyoshi Mayama1,+, Tetsuya Ohashi2, Yuichi Tadano3 and Koji Hagihara4 1 Department of Materials Science and Engineering, Kumamoto University, Kumamoto 860-8555, Japan Mechanical Engineering, Kitami Institute of Technology, Kitami 090-8507, Japan 3 Department of Mechanical Engineering, Saga University, Saga 840-8502, Japan 4 Department of Adaptive Machine Systems, Osaka University, Suita 565-0871, Japan 2 The mechanism and the effective factors for the development of intragranular misorientations due to kinking is studied by a crystal plasticity finite element method. A single crystal with hexagonal close-packed (HCP) structure in which only basal slip system is activated is used as a model material. To activate basal slip system, the initial crystal orientations are set to be the ones whose basal planes are slightly deviated from the compressive direction. The result shows that basal slip and the development of intragranular misorientations are sometimes localized near the center of the specimen depending on the initial deviation angle, strain hardening rate, and strain rate sensitivity. The mechanism is discussed in terms of the nonuniform stress distribution and lattice rotation. The effect of slight changes in the boundary conditions shows significant effect on the positions of slip localization. In summary, the present numerical results suggest that there are a number of effective factors for the development of the intragranular misorientations due to kinking including initial crystal orientation, material parameters, and boundary conditions. [doi:10.2320/matertrans.MH201403] (Received December 25, 2014; Accepted February 13, 2015; Published March 27, 2015) Keywords: crystal plasticity, finite element analysis, kinking, single crystal 1. Introduction The electron backscatter diffraction (EBSD) technique has been used widely to measure intragranular misorientations in crystal grains and detailed features of microstructure in deformed metals were examined.14) Pantleon et al.1) characterized the anisotropy of orientation distributions within individual grains in cold-rolled aluminium. Scheriau and Pippan2) reported the influence of grain size on orientation change in polycrystalline copper, nickel and iron. The orientation gradient around a hard particle in a warm-rolled Fe3Al-based alloy3) and the distribution of geometrically necessary dislocations in dual-phase steels4) were studied by three-dimensional EBSD. These results suggest that intragranular misorientation is a key indicator for material properties and microstructure evolution. However, the detailed mechanism and effective factors in the development of intragranular misorientation has not been clarified. Intragranular misorientations evolve when the plastic slip deformation is spatially nonuniform and different amount of lattice rotation take place. While in polycrystals the mutual interactions between grains lead to inhomogeneous deformation, numerical studies on single crystals510) show that deformation can also be inhomogeneous depending on boundary conditions and initial fluctuations. Therefore, inhomogeneous deformation of single crystals is considered to be an essential point for the understanding of the development mechanism of intragranular misorientations. Among several deformation modes that lead to inhomegeneous deformation of single crystals, kinking often induces large intragranular misorientations.9,10) While kinking is one of common deformation modes in metals,1116) intensive studies have been made on hexagonal close-packed (HCP) crystals where basal slip system was dominantly activated.1724) Orowan considered kinking as third fundamental + Corresponding author, E-mail: [email protected] deformation mechanism as well as slip and twinning.17) In contrast, Hess and Barrett18) made a careful observation of compressed Zn single crystals and proposed a simple model of kink formation by an array of dislocations. Jillson19) also concluded that kinks developed after gliding or slip processes from experimental results obtained for Zn single crystals. Hess and Barrett18) discussed that the positions of kink formation varied depending on boundary conditions and defects. Meanwhile, Gilman22) showed that kinks tended to form near the center of specimen, which disagreed with the results by Hess and Barrett.18) Gilman22) also showed that the formation of kink depended on crystal orientation. Whereas these intensive experimental researches, it is still difficult to specify which are the dominant factors for development of intragranular misorientations because the experimental results suffer influences from various origins and unavoidable initial imperfections. While kinking is mentioned in several theoretical and/or numerical researches,810,25) detailed investigation of the influences of various parameters on the development of intragranular misorientations has not been reported. In this study, we try to gain fundamental understandings of the development of intragranular misorientation due to kinking. We employ HCP crystals for a model material in which only basal slip system is activated. A crystal plasticity finite element method is used to evaluate the effects of initial crystal orientation, strain rate sensitivity and strain hardening rate on the development of intragranular misorientations and kinking. Mechanism of the development of intragranular misorientations, abrapt drops in the stress-strain response during kinking and the influence of slight change in boundary conditions are discussed. 2. Overview of the Intragranular Misorientations Due to Kinking Figure 1 shows the typical kink bands experimentally 964 T. Mayama, T. Ohashi, Y. Tadano and K. Hagihara (a) (b) 1010 -2110 0001 (d) (e) 0001 -2110 (c) 25 (h) (g) L1 L2 100 μm 20 μm Misorientation from the origin, degrees (°) (f) 20 L1 15 10 L2 5 0 0 5 10 15 Distance from the origin, l/μm Fig. 1 Typical kink bands experimentally observed in Zn single crystal and polycrystalline Mg-based 18R LPSO phase. (a) Shape of direction at room temperature. The observed direction of the deformed Zn single crystal after 20% compressive strain along the ½0110 (b) Crystal orientation map examined by SEM-EBSD pattern analysis in specimen after 3% compressive specimen is parallel to ½21 10. and (0001) pole strain. The boundaries across which the lattice is rotated more than 5 degree are drawn by black lines. (c)(e) f21 10g figures taken at the positions marked AC in Fig. 1(b), respectively. (f ) Surface morphology of directionally solidified Mg-based 18R LPSO phase alloy after compressive loading along nearly parallel to basal plane. (g) Crystal orientation map in the deformed Mg-based 18R LPSO phase alloy. (h) Line profiles indicating the variations in crystal orientation along L1 and L2 in Fig. 1(g). observed in Zn single crystal and directionally-solidified (abbreviated as DS, hereafter) polycrystalline Mg-based 18R LPSO (long period stacking ordered) phase alloy with the composition of Mg85Zn6Y9 (at%).26) Figure 1(a) shows an optical micrograph of kink bands in a Zn single crystal specimen compressed 20% plastic strain along the ½0110 direction. The observation direction was parallel to the direction. A significant change in the shape of the ½21 10 specimen is observed. Black lines in Fig. 1(a) correspond to the trace of basal planes those were introduced by chemical etching. They are sharply bent at localized regions near the top and bottom ends and kink bands accompany with these lattice rotations. The microstructures in the Zn single crystal specimen in the early stages of deformation were examined by electron backscatter diffraction (EBSD) pattern analysis with scanning electron microscopy (SEM). Figure 1(b) shows the crystal orientation map after 3% compressive strain. The observation direction. Boundaries direction was parallel to the ½21 10 across which lattice rotation was larger than 5° were drawn by black lines. A wide kink band introduced by deformation appeared in the center of the image shown in Fig. 1(b). and (0001) pole figures taken Figures 1(ce) display f21 10g at positions AC in Fig. 1(b), respectively. These demonstrate that a large crystal rotation was caused by the formation axis that was perpendicular of a kink band along the ½21 10 to the normal to the (0001) basal slip plane. Crystal rotations across the sites A and B, and B and C are about 34° and 32°, respectively. Note that these lattice rotation angles are not constant and the value is different in each deformation band. Moreover, some boundaries terminate within the crystal, as indicated by arrows in Fig. 1(b). Although the basal slip is the easiest deformation mode in the Zn single crystal, the contributions of non-basal slip and twinning cannot be completely avoided. While it was recently reported that in the Mg-based LPSO phase DS crystal only basal slip system was predominantly activated compared to the other slip systems in deformation at room temperature.26,27) Because of this fact, contributions from non-basal slips and twinning to kinking should be limited in the case of this alloy system. Figures 1(f ) and (g) shows an optical micrograph of the surface morphology and the crystal orientation map in the deformed LPSO phase DS crystal. The specimen was compressed at room temperature along the growth direction where the basal plane was almost parallel to the loading axis in most of the grains (vertical direction in the Fig. 1(g)). A number of sharp bends of basal plane are observed and these are considered to be developed by superimpose of smaller and ridge-shaped kink bands. Figure 1(h) shows the line profiles of misorientation angle from the origin along L1 and L2 indicated in Fig. 1(g). Although there are significant changes in crystal orientation near the both kinked regions, the transitions of crystal orientation along L1 and L2 are quite different. The transitions along L1 and L2 are step-like and triangular, respectively. Crystal Plasticity Analysis of Development of Intragranular Misorientations due to Kinking in HCP Single Crystals In these ways, experimentally observed deformation microstructure by kinking are considerably complicated. In the LPSO phase polycrytalline specimen, the effect of interactions between grains cannot be excluded. Additionally, in any experimental studies, effects of frictions on loading surfaces and initial imperfections are usually contained. To exclude such effects to kinking and to clarify the formation mechanism of deformation microstructure, numerical analysis using a crystal plasticity finite element method is useful. In the present study, kink band formation behavior was examined by using HCP single crystals with no initial imperfections those deform by only basal slip system. 3. (a) (b) θ ini c z z y x (c) θ ini c BSL1 c y BSL3 BSL2 z θ ini x BSL3 BSL2 BSL1 (d) z y x BSL3 965 BSL2 z z BSL1 15° z x x y x y x y y Fig. 2 Schematic diagrams of analysis model. (a) Model geometry and 10, (c) ½0110 and (d) intermediate boundary conditions. For near (b) ½12 compressive loadings, the definitions of initial deviation angle ªini and deformation modes. Numerical Procedure 3.1 Crystal plasticity finite element method In this study, the rate-dependent finite strain crystal plasticity model proposed by Peirce et al.6) was used. The crystal plasticity model was implemented into each gauss point in a large-deformation finite element scheme as a constitutive law and the development of heterogeneous distributions of slip accumulation and crystal orientation were calculated. After the proposal of the rate-dependent finite strain crystal plasticity model, considerable developments in crystal plasticity model have been made with implementation of geometrically necessary dislocation (GND) density based on strain gradient.2830) When the kink deformation takes place, GND density should significantly increase with the development of sharp bending of slip plane. At the same time, back stresses3133) and additional dissipations due to the development of strain gradient or the evolution of plastic curvature and torsion33,34) and other factors associated with GNDs will be important issues to be discussed. However, thorough discussions of these effects are beyond the objective of this study. Instead, classical crystal plasticity model is used to gain primary understandings of the effects including the initial crystal orientation, strain hardening rate, rate sensitivity and boundary conditions in kinking. In the present paper, the shear slip rate £_ ðiÞ for deformation mode i was calculated by ðiÞ 1=m ¸ ð1Þ £_ ðiÞ ¼ £_ 0 sgnð¸ ðiÞ Þ ðiÞ : g Here, sgnðxÞ ¼ 1 if x 0 and sgnðxÞ ¼ 1 if x < 0; £_ 0 and m are the reference shear strain rate and the strain rate sensitivity parameter, respectively. The ¸ ðiÞ and gðiÞ are the resolved shear stress (RSS) and reference stress for deformation mode i, respectively. The following equation was used for gðiÞ in this study: X g_ ðiÞ ¼ hðijÞ j£_ ðjÞ j ð2Þ j ðijÞ where h is the strain hardening rate. A constant value of h was used for hðijÞ for simplicity, although the strain hardening rate should depend, in general, on various parameters, including the loading history, the reactions of dislocations, temperature, and so forth. For numerical integration of the constitutive model, the rate-tangent modulus method proposed by Peirce et al.6) was used. To ensure stable calculations even when the slip is localized, an r-minimum strategy35,36) was employed to control the increment of time. 3.2 Analysis model Figure 2 shows the schematic diagrams of analysis model. The model is a square prism with dimensions of 10 © 10 © 20 µm. The model is uniformly divided into 10 © 10 © 20 finite elements of 20-node solid type. Reduced integration is adopted and the number of integration points for each element is eight. The boundary conditions are illustrated in Fig. 2(a). The displacement in the z-direction at the bottom surface is fixed and a uniform compressive displacement in the z-direction is applied at the top surface. The displacements in the x- and y-directions at the top and bottom surfaces are not fixed; this corresponds to a condition under which there is no friction between the compressive jig and the specimen. The lateral surfaces of the model are traction-free. To induce a single slip of the basal slip system, the loading 10 direction. When the direction was set to be near the ½12 loading direction is exactly the ½1210 direction, the basal slip system is not activated because the Schmid factors for the basal slip system become zero. To make the Schmid factors of the basal slip system nonzero, the loading direction should 10 direction. The initial deviation angle deviate from the ½12 ªini, defined as the angle between the loading direction and the basal plane as shown in Fig. 2(b), was introduced in the model. That is, the initial crystal orientation was set so that it 10 direction by a rotation of ªini about deviated from the ½12 the x-axis (½1010 axis). For every Gauss point, the same initial crystal orientation was allocated. In Fig. 2(b), the definitions of the deformation modes are also shown. Here, the three modes of basal slip systems are named as BSL1, BSL2 and BSL3. The effects of the initial deviation angle ªini and the finite element mesh are discussed in Sec. 4.1. In Sec. 4.5, effects of slight changes in the constraints on the top or/and bottom surfaces are discussed. Deformation of specimens where the compressive direc direction and tions were slightly deviated from the ½0110 were also intermediate direction between ½1210 and ½0110 made in Sec. 4.6. The initial orientations and deformation modes are schematically illustrated in Figs. 2(c) and (d). 966 T. Mayama, T. Ohashi, Y. Tadano and K. Hagihara Table 1 Model parameters used in crystal plasticity analysis. Section (Fig.) g(basal) [MPa] E [GPa] ¯ ªini 4.1 (Figs. 3, 4, 6 and 7) 45 0.35 3, 4 or 5 100 0.02 10 © 10 © 20 10 © 10 © 20 10 4.2 (Fig. 8) 45 0.35 3 50, 100, 200 or 300 0.02 10 © 10 © 20 10 © 10 © 20 10 4.3 (Fig. 9) 45 0.35 3 100 0.01, 0.02, 0.05 or 0.1 10 © 10 © 20 10 © 10 © 20 10 4.4 (Fig. 10) 45 0.35 3 100 0.02 10 © 10 © 10, 10 © 10 © 20 or 10 © 10 © 40*1 10 © 10 © 10, 10 © 10 © 20 or 10 © 10 © 40*1 10 4.5, 4.6 and 5.1 (Figs. 4*2, 11, 12 and 13*3) 45 0.35 3 100 0.02 10 © 10 © 20 10 © 10 © 20 10 h [MPa] Mesh discretization [element] m Mesh geometry [µm] *1The initial size of each element for all models is 1 © 1 © 1 µm. *2Lattice rotation is suppressed in gray dashed-dotted line in Fig. 4. *3The initial crystal orientations of the results in Figs. 13(b) and (c) are different from the others by rotating about c-axis as shown in Figs. 2(c) and (d). 4. Numerical Results 4.1 Effect of initial deviation angle Figure 3 shows the development of intragranular misorientations during compressive loading. To visualize the variation of the crystal orientation, the deviation angle ¦ª from ªini is defined as shown in Fig. 3(a). Here, a positive value of ¦ª indicates an increase in the deviation angle between the loading direction and basal plane. In Fig. 3(a), distributions of ¦ª at nominal strains ¾zz = ¹0.5, ¹0.6 and ¹0.7% in the model with ªini = 3° are illustrated. In Fig. 3(a), ¦ª continuously increases near the center of the model. Figure 3(b) shows the relationship between the maximum ¦ª at each strain and the nominal compressive strain. The model with ªini = 3° show rapid increase in ¦ª around compressive strain of 0.5%. In contrast, the change in ¦ª in the model with ªini = 5° is much more gradual. Figure 4 shows the calculated stress-strain curves of single crystals with ªini of 3, 4 and 5°. The nominal stress-strain curves differ significantly with the initial crystal orientation; that is, when ªini = 3°, the stress rapidly decreases during deformation, whereas the stress gradually decreases for ªini = 5°. The smaller the initial deviation angle ªini, the larger the amount and the rate of the decrease in stress. The peak stress immediately before the decrease in stress also (a) (b) 20 z θini = 3° Maximum Δθ (°) θ ini+ Δθ z εzz = -0.5% εzz = -0.6% εzz = -0.7% x y Δθ [°] : 0 13.5 15 θini = 4° θini = 5° 10 5 0 0 0.2 0.4 0.6 0.8 1 Nominal compressive strain (%) Fig. 3 Change in crystal orientation during compressive loading. (a) Distributions of ¦ª in the model with ªini = 3°. (b) Changes in the maximum ¦ª at each strain in the model with ªini of 3, 4 and 5°. Nominal compressive stress, σ / MPa 3.3 Deformation mode and material parameters basal slip is the sole mode of plastic The ð0001Þh1120i deformation considered in the present analysis. The initial value of the reference stress gðiÞ for the basal slip system is set to be 10 MPa. Young’s modulus E, Poisson’s ratio ¯, rate sensitivity factor m and strain hardening rate h were set to be the experimentally reported values for conventional polycrystalline Mg alloys at room temperature.37,38) The effects of the variation in strain hardening rate and strain rate sensitivity are discussed in Sec. 4.2 and 4.3, respectively. Apparent causes of non-uniform deformation such as initial fluctuations of material parameters, geometrical imperfection are not included in this paper. Parameters used in the calculations in each section are summarized in Table 1. 350 Without lattice rotation (θ ini = 3°) 300 250 B 200 A C 150 100 θ ini = 3° θ ini = 4° θ ini = 5° 50 0 0 0.2 0.4 0.6 0.8 1 Nominal compressive strain (%) Fig. 4 Variations in calculated stress-strain curves with the initial deviation angle ªini of 3, 4 and 5°. depends on the initial crystal orientation. The different peak stresses are the result of different initial Schmid factors, which in turn depend on the crystal orientation. It was confirmed that the difference in the maximum RSS values at the peak stresses in single crystals with ªini of 3, 4 and 5 is within 1%. The comparison between Fig. 3(b) and Fig. 4 indicate that the significant decrease in stress for smaller ªini is associated with the rapid and pronounced change in crystal orientation. The mechanism of the decrease in stress and localization is discussed in Sec. 5.1. 250 (a) 967 (b) 25 z 200 Misorientation Δθ (°) Nominal compressive stress, σ / MPa Crystal Plasticity Analysis of Development of Intragranular Misorientations due to Kinking in HCP Single Crystals 150 100 10 × 10 × 10 elements 10 × 10 × 20 elements 50 10 × 10 × 10 elements 20 15 10 × 10 × 20 elements l 10 × 10 × 40 elements y 10 x 5 10 × 10 × 40 elements 0 0 0.2 0.4 0.6 0.8 0 1 0 0.2 0.4 0.6 0.8 1 Normalized position in z-direction x3 / l Nominal compressive strain (%) Fig. 5 Effect of finite element mesh resolution on the macroscopic stress-strain curves and on the distribution of ¦ª in the model with ªini = 3°. (a) Stress-strain curves. (b) Line profiles of ¦ª at ¾zz = ¹1%. z x θ ini = 3° y θ ini = 5° θ ini = 4° γ acc : 0 0.36 Fig. 6 Distribution of the accumulation of shear slip of the basal slip system, BSL2, at ¾zz = ¹1% in models with ªini = 3, 4 and 5°. (a) 25 (b) z x θ ini = 3° y θ ini = 4° Δθ [°] : 0 θ ini = 5° Misorientation Δθ (°) As is well known, the calculations of localization by the classical finite element method show mesh dependence.39) Figures 5(a) and (b) show the effects of the mesh resolution on nominal stress-strain curves and the change in the crystal orientation when the nominal compressive strain is ¾zz = ¹1% in the model with ªini = 3°. In Fig. 5(b), the line profiles of ¦ª at the center of x-y plane along z-direction are compared. Here, normalized position in z-direction is defined by x3 (coordinate value in z) divided by model length l. The line profiles show triangular transition of crystal orientation which are similar to the experimental result of L2 in Fig. 1(h). The results for meshes uniformly divided into 10 © 10 © 10, 10 © 10 © 20 and 10 © 10 © 40 elements, in which the geometry of the analysis model is fixed to 10 © 10 © 20 µm, are compared. Although the stress-strain curves are almost the same, as shown in Fig. 5(a), the line profile of ¦ª clearly depends on the mesh resolution. The finer meshes exhibit more significant variation of ¦ª near the center of the model as shown in Fig. 5(b). Additionally, the result of the finer mesh shows that the variation of ¦ª is localized in the narrower width compared with the results of the coarser mesh. As shown above, the results of localization clearly depend on the finite element mesh resolution. Therefore, careful attention should be paid on finite element mesh when quantitative evaluation. In the present study, the influences of parameters are examined by using the same finite element mesh. As discussed in literatures,32) higher order theory of plasticity could be possible to avoid such mesh dependency. In the all results as shown above, the accumulations of shear slip by BSL1 and BSL3 are less than 1% of that for BSL2 at a nominal compressive strain of ¾zz = ¹1%. That is, the single-crystal model is deformed by the approximately single slip of BSL2. Figure 6 shows the effect of ªini on the distribution of the accumulation of shear slip of basal slip system BSL2 when the nominal compressive strain is ¾zz = ¹1%. The distribution strongly depends on ªini. In the models with smaller ªini, more basal slip is accumulated near the center of the model. With the localized accumulation of basal slip, the model becomes bent. Figure 7 shows the dependence of ªini on the variation of crystal orientation when the nominal compressive strain is ¾zz = ¹1%. Figure 7(a) shows the distributions of ¦ª in the θ ini = 3° 20 θini = 4° θ ini = 5° 15 10 5 18 0 0 0.2 0.4 0.6 0.8 1 Normalized position in z-direction x3 / l Fig. 7 Effect of ªini on development of intragranular misorientation. (a) Distributions of ¦ª at ¾zz = ¹1% in the model with ªini of 3, 4, and 5°. (b) Line profiles of ¦ª at ¾zz = ¹1%. models with ªini of 3, 4 and 5°. The distributions clearly indicate that more pronounced intragranular misorientations are introduced in the models with smaller ªini. In the center region of the model with ªini = 3°, the value of ¦ª varies significantly. Comparing Fig. 6 with Fig. 7(a), it is found that the distributions of the accumulations of basal slip and ¦ª are qualitatively very similar. This similarity arises as a result of lattice rotation caused by basal slip as discussed in Sec. 5.1. Figure 7(b) show the line profiles of ¦ª at the nominal compressive strain is ¾zz = ¹1%. With decrease in ªini, significant misorientation is introduced at the narrow region near the center especially in the case of ªini = 3 and 4°. On the other hand, the model with ªini = 5° shows the larger change in the ¦ª near top and bottom regions compared with those in the model with ªini = 3 and 4°. The axis of lattice rotation in all models in Fig. 7 is the x axis (½1010 axis) as explained in Sec. 5.1. The lattice rotation about the x-axis leads to the bending of basal planes. T. Mayama, T. Ohashi, Y. Tadano and K. Hagihara 300 25 (a) (b) h = 300 MPa 250 Misorientation Δθ (°) Nominal compressive stress, σ / MPa 968 h = 200 MPa 200 150 h = 100 MPa 100 h = 50 MPa 50 0 0 0.2 0.4 0.6 0.8 Nominal compressive strain (%) 1 h = 50 MPa 20 h = 100 MPa h = 200 MPa 15 h = 300 MPa 10 5 0 0 0.2 0.4 0.6 0.8 1 Normalized position in z-direction x3 / l Fig. 8 Effect of strain hardening rate of basal slip on macroscopic stress-strain curves and on the distribution of ¦ª in the model with ªini = 3°. (a) Variation in stress-strain curves. (b) Line profiles of ¦ª at ¾zz = ¹1%. The intragranular misorientations revealed in this calculation can be interpreted as kink bands because the boundaries of intragranular misorientations are not parallel to the slip direction of the active slip plane. In other words, the boundaries should be ideally parallel to shear direction when the boundaries are formed by slip banding or twinning. 4.2 Effect of strain hardening rate In the previous section, the calculations were performed with a strain hardening rate h of 100 MPa. In this section, the effect of the strain hardening rate on the distribution of intragranular misorientations is discussed. While experiments on HCP single crystals indicate a very low strain hardening rate of the basal slip system, the strain hardening rate significantly increases with the introduction of a slight lowangle boundary into single crystals.40) Therefore, it is valuable to study the effect of the strain hardening rate on the development of intragranular misorientations. Figure 8(a) shows the effect of the strain hardening rate on the nominal stress-strain curve in the model with ªini = 3°. Here, the strain hardening parameter h is set to 50, 100, 200, or 300 MPa. Stress-strain curves for h smaller than 300 MPa show a decrease in the flow stress from the peak stress, whereas the stress continuously increases when h = 300 MPa. Figure 8(b) shows the line profiles of ¦ª at a nominal compressive strain of ¾zz = ¹1% for different values of h. Significant intragranular misorientations are developed near the center of the model when h is 50 or 100 MPa. In contrast, the difference in ¦ª is slight except near the top and the bottom in the model when h is 200 or 300 MPa. 4.3 Effect of strain rate sensitivity In eq. (1), m is the strain rate sensitivity parameter. The strain rate sensitivity is dependent on the material, microstructure, temperature, slip system, and so forth. Even among HCP metals, strain rate sensitivities are significantly different. While beryllium and zinc show significant strain rate dependence even at room temperature,41,42) the strain rate sensitivity of magnesium at room temperature is relatively low.43) In this section, to clarify the effect of strain rate sensitivity on the development of intragranular misorientations, the numerical results for four different strain rate sensitivities are compared. Figure 9(a) shows the effect of the strain rate sensitivity on the nominal stress-strain curve in the model with ªini = 3°. Here, a strain rate sensitivity parameter m of 0.02, 0.05, 0.1 or 0.2 is used. The rate of the decrease in stress from the peak stress decreases with increasing m. This trend is qualitatively consistent with the numerical results reported by Peirce et al.30) Figure 9(b) shows the line profiles of ¦ª at a nominal compressive strain of ¾zz = ¹1%. A smaller m leads to significant intragranular misorientations while the results with larger m show the smaller difference in ¦ª. As in a number of previous researches1822) and in the Sec. 2, Zn single crystals frequently show significant kinking even though the strain rate sensitivity at room temperature is relatively large. One possible reason for the frequent kinking in Zn would be the high ratio of lattice constants c/a. Due to twinning is geometrically prevented the high ratio, f1012g under the loading in the parallel direction to basal plane.44) In that case, kinking should accommodate the compressive strain in the parallel to basal plane in place of f1012g twinning. The other possible reasons are the influences of several effective factors including strain hardening rate and boundary conditions as discussed in the present study. However, to discuss the detailed mechanism of kinking in Zn is beyond the scope of the present study because the activity of non-basal slip system and the interaction between basal and non-basal slip systems cannot be ignored for Zn even at room temperature. 4.4 Effect of aspect ratio The effect of aspect ratio of the analysis model is examined. Figures 10(a) and (b) show the effects of the aspect ratio on the nominal stress-strain curves and the line profiles of ¦ª at a nominal compressive strain of ¾zz = ¹1% in the model with ªini = 3°. In the calculations, models with geometries of 10 © 10 © 10, 10 © 10 © 20 and 10 © 10 © 40 µm are used. These models are uniformly divided into 10 © 10 © 10, 10 © 10 © 20 and 10 © 10 © 40 elements with the same initial size of each element of 1 © 1 © 1 µm. Although the stress-strain curves are almost the same, as shown in Fig. 10(a), the line profiles of ¦ª show a dependence on the model geometry as shown in Fig. 10(b). The model with the higher aspect ratio exhibits more significant intragranular misorientations near the center of the model. The misorientation is more localized in the narrower region in the result with higher aspect ratio compared with the result with lower aspect ratio. The reason of this aspect ratio dependency will be discussed in Sec. 5.1. 300 (b) 250 200 m = 0.1 150 m = 0.05 m = 0.02 100 50 0 0 0.2 0.4 0.6 0.8 969 25 m = 0.2 (a) Misorientation Δθ (°) Nominal compressive stress, σ / MPa Crystal Plasticity Analysis of Development of Intragranular Misorientations due to Kinking in HCP Single Crystals m = 0.05 m = 0.1 15 m = 0.2 10 5 0 1 m = 0.02 20 0 Nominal compressive strain (%) 0.2 0.4 0.6 0.8 1 Normalized position in z-direction x3 / l 250 25 (a) (b) 200 Misorientation Δθ (°) Nominal compressive stress, σ / MPa Fig. 9 Effect of strain rate sensitivity on the macroscopic stress-strain curves and on the distribution of ¦ª in the model with ªini = 3°. (a) Variation in stress-strain curves. (b) Line profiles of ¦ª at ¾zz = ¹1%. 150 100 10 × 10 × 10 μm 10 × 10 × 20 μm 50 10 × 10 × 10 μm 20 10 × 10 × 20 μm 15 10 × 10 × 40 μm 10 5 10 × 10 × 40 μm 0 0 0.2 0.4 0.6 0.8 0 1 0 0.2 0.4 0.6 0.8 1 Normalized position in z-direction x3 / l Nominal compressive strain (%) Fig. 10 Effect of aspect ratio of specimen on stress-strain curves and on the distribution of ¦ª in the model with ªini = 3°. (a) Stress-strain curves. (b) Line profiles of ¦ª at ¾zz = ¹1%. 4.5 Effect of boundary conditions The deformed Zn single crystal in Fig. 1(a) shows that kink bands are formed near the top and bottom regions of the specimen, while the kink bands calculated in the present analyses are formed in the center of the model. With the aim of more realistically simulating the experimental observation in Fig. 1, constraints on the displacement at the top or/and bottom surfaces are introduced into the model subjected to compression with ªini = 3° (TB-free model) as near-½1120 shown in the previous sections. Figure 11(a) shows schematic diagrams of three boundary conditions; T-fixed, B-fixed and TB-fixed conditions. Constraints on the displacement in the direction perpendicular to the loading direction are added to the TB-free model in Fig. 11(a). In the T-fixed model, the displacements in the xand y-directions of all nodes at the top surface are set to zero. In the B-fixed model, the displacements in the x- and ydirections of all nodes at the bottom surface are set to zero. In the TB-fixed model, the displacements in the x- and ydirections of all nodes at the top and bottom surfaces are set to zero. These additional constraints correspond to the boundary conditions due to friction between the specimen and the compressive jig. Figure 11(b) shows the distributions of ¦ª at a nominal compressive strain of ¾zz = ¹1%. The distributions change significantly with a slight change in the boundary conditions. The distributions for the T-fixed and B-fixed models are similar when one of them is rotated 180° about the x-axis. In both distributions, significant variations of crystal orientation (a) (b) z z x T-fixed y B-fixed TB-fixed x y T-fixed B-fixed Δθ [°] : -3 TB-fixed 19 Fig. 11 Effect of boundary conditions on distribution of ¦ª. (a) Boundary conditions for T-fixed, B-fixed and TB-fixed models. (b) Distributions of ¦ª at ¾zz = ¹1%. are introduced near the fixed end. In the TB-fixed model, the crystal orientation clearly varies near both ends. These results indicate that the additional constraints on the top and/or bottom surfaces lead to intragranular misorientations near the top or/and bottom surfaces. Additionally, in the TB-fixed model, there are regions with slightly negative values of ¦ª near the top and bottom ends. The numerical result of the TB-fixed model shows similar to experimental result shown in Fig. 1(a) while the other numerical results presented in this study are quite different from the experimental result. One possible reason of the similarity is friction on top and bottom surfaces in the real experimental condition. Even in experiment, similar results to TB-free model have been reported17,18) where the effect of end constraints has been avoided by using longer specimens compared with the one in Fig. 1(a). 970 T. Mayama, T. Ohashi, Y. Tadano and K. Hagihara 4.6 Compressive loading under double slip In this section, calculations of compressive loading near ½0110 direction and near-intermediate direction between and ½0110 directions are shown. In these loading ½1120 direction, two basal slip modes are activated. The geometry of the model, the finite element mesh and the boundary conditions are the same as those shown in Fig. 2(a). Only the crystal orientation is changed in accordance with the loading direction. The initial deviation angle is set to be ªini = 3°. Figure 2(c) and (d) show schematic illustrations of the crystal orientations. The boundary condition for these models is TB-free. Figure 12(a), (b) and (c) show the distributions of ¦ª after compression of ¾zz = ¹1% nominal strain in near-½1120, and near-intermediate directions, respectively. near-½0110 compression in Fig. 12(b), the distribuFor the near-½0110 compression as shown tion is similar to that for near-½1120 in Fig. 12(a) whereas the deformation modes are single slip compression and double slip in the in the case of near-½1120 compression. In contrast, as shown in case of near-½0110 Fig. 12(c), the distribution of ¦ª for compression in near and ½0110 directions intermediate direction between ½1120 compression and nearis clearly different from near-½1120 compression. The result of near-intermediate com½0110 pression shows orientation gradient along x-direction while the orientation gradient along x-direction is negligible in the results of near-½1120 compression and near-½0110 compression. The orientation gradient for near-intermediate compression would be caused by different activities for nonequivalent basal slip modes. 5. 5.1 Discussion Mechanism of development of intragranular misorientations In the results of the calculations shown above, local crystal orientations are significantly changed during compression in single crystals. The use of the model without initial fluctuations or imperfections is a crucial difference from previous crystal plasticity analyses on kinking.8,10) When the values of ªini, h and m are small, more significant intragranular misorientations develop. Figures 6 and 7 indicate that the distributions of accumulation of basal slip and intragranular misorientations are very similar. Here, the mechanism of the development of intragranular misorientations is discussed in detail. Figures 13(a)³(c) show the distributions of RSS for BSL2 at points A, B, and C indicated in Fig. 4. The ranges of the contours are adjusted for each point. At point C, the RSS is clearly concentrated in the center of the model. At point B, the distribution of RSS is also nonuniform while the concentration of RSS in the center of the model is weaker. Even at point A, where the stress is increasing almost linearly, the distribution of RSS is not uniform but the difference between the maximum and minimum values of RSS is small. The nonuniform distributions of RSS in Figs. 13(a)³(c) are caused by the nonuniform stress components. Only stress components ·yy, ·yz and ·zz contribute to the RSS for BSL2 because the slip direction and slip plane normal direction for (a) (b) y Δθ [°] : 0 (c) z x 18 Fig. 12 Distribution of ¦ª at ¾zz = ¹1% in TB-free model compressed direction, (b) near-½0110 in (a) near-½1120 direction and (c) near and ½0110. intermediate direction between ½1120 (a) (b) (c) 9.4268 11.1 16.1 (d) Lower z x 9.4262 [MPa] 10.7 [MPa] Absolute stress value 9.1 [MPa] Higher σ zz y Fig. 13 Distributions of the resolved shear stress (RSS) on the basal slip system BSL2 when the nominal compressive strain is at (a) A: 0.4%, (b) B: 0.46% and (c) C: 0.48% in Fig. 4, respectively. (d) Schematic diagram of distribution of stress component ·zz by enhancing the change in the shape when the macroscopic stress is at point A in Fig. 4. BSL2 lie on the y-z plane. It was confirmed that the stress component ·zz shows the most significant heterogeneity in the stress distribution at point A. Figure 13(d) shows a schematic diagram of distribution of stress component ·zz by enhancing the change in the shape of specimen. The reason for this nonuniform distribution of stress component ·zz can be explained in terms of the change in the shape of the specimen. The slip direction and slip plane normal direction of BSL2 in the model with ªini = 3° are s(BSL2)(0, ¹0.05234, 0.99863) and m(BSL)(0, ¹0.99863, ¹0.05234), respectively. The Schmid tensor P(BSL2) for BSL2 is 1 PðBSL2Þ ¼ ðsðBSL2Þ mðBSL2Þ þ mðBSL2Þ sðBSL2Þ Þ 2 0 1 0 0 0 B C ¼ @ 0 0:05226 0:49726 A: ð3Þ 0 0:49726 0:05226 Because of the small deviation angle ªini between the loading direction and the basal plane, the Schmid factor in the loading direction (zz component of P(BSL2)) is nonzero, as indicated in eq. (3). With compressive loading, the basal slip system is activated, even at point A in Fig. 4, because the slip rate £_ calculated by eq. (1) is nonzero when the RSS is nonzero due to the nonzero Schmid factor in the loading direction. Once the basal slip system BSL2 is activated, the shape of the specimen is changed by plastic strain. The plastic strain rate Dp is calculated by _ ðBSL2Þ : Dp ¼ £P ð4Þ From £_ and eqs. (3) and (4), the yz component of shear strain is induced. Owing to the yz component of shear strain, the original square prism shape of the model is changed to an oblique square prism shape as shown in Fig. 13(d), in which broken lines show the original undeformed shape. The oblique planes on both sides of the model, as shown in Crystal Plasticity Analysis of Development of Intragranular Misorientations due to Kinking in HCP Single Crystals Fig. 13(d), lead to nonuniform stress distributions in the model to satisfy the balance of moments. It has been confirmed by elastic plane stress finite element analysis that similar distributions of stress components are induced in a parallelogram subjected to uniform compressive displacement, corresponding to the two-dimensional model schematically shown in Fig. 13(d). Next, the significance of lattice rotation in slip localization is confirmed by the suppression of lattice rotation. In Fig. 4, gray dashed-dotted line shows the calculated stress-strain curve without lattice rotation. Without lattice rotation, stress continues to increase. The significant difference between the results with and without lattice rotation is caused by geometrical softening.45) In the present crystal plasticity model, the slip direction s(¡) and slip plane normal direction m(¡) are updated by _ ð¡Þ ¼ W mð¡Þ : s_ð¡Þ ¼ W sð¡Þ and m ð5Þ In eq. (5), W* is the nonplastic (i.e., elastic and rigid body) spin tensor given by W ¼ W Wp ; ð6Þ where W and Wp are the continuum and plastic spin tensors, respectively. When the plastic deformation Wp is caused by a single slip of BSL2, the plastic spin tensor becomes £_ Wp ¼ ðsðBSL2Þ mðBSL2Þ mðBSL2Þ sðBSL2Þ Þ 20 1 0 0 0 B C ¼ £_ @ 0 0 0:5 A: ð7Þ 0 0:5 0 When the plastic spin due to the BSL2 slip is sufficiently large compared with the macroscopic spin W, W* is approximately calculated by W ¼ Wp : ð8Þ During compressive loading, £_ ðBSL2Þ becomes positive according to eqs. (3) and (4). From eqs. (5), (7) and (8), it is found that the deviation angle ª between the compressive direction and the basal plane increases owing to the activation of basal slip BSL2. When the deviation angle ª is less than 45°, the lattice rotation due to basal slip BSL2 increases the Schmid factor of the basal slip system, which accelerates the activity of basal slip BSL2. Even after large lattice rotation, the Schmid factor of BSL2 is the largest among the three modes of the basal slip system. Therefore, the dominant activity of BSL2 continues. The effect of geometrical softening is especially pronounced in the case of smaller ªini. When ªini is smaller, the Schmid factor in the loading direction becomes smaller. In the present case, from eqs. (3) and (4), a larger slip rate £_ is required in a model with a smaller Schmid factor in the zdirection (zz component of P(BSL2)) to induce a macroscopic compressive plastic strain rate in the z-direction (zz component of Dp). From eqs. (5), (7) and (8), a larger slip rate leads to significant lattice rotation. The significant lattice rotation results in the rapid increase in the Schmid factor discussed in the previous paragraph. With the rapid increase in the Schmid factor, the stress required to obtain the same RSS decreases, which results in softening. 971 The dependence of the aspect ratio of model on intragranular misorientation as shown in Sec. 4.4 can be explained by the above mentioned mechanism. When the same amount of shear strain is induced for the models with different aspect ratios, the displacement in y-direction on the top surface as shown in Fig. 13(d) is dependent on the aspect ratio. That is, the model with higher aspect ratio should show larger displacement in y-direction on the top surface, which lead to more significant nonuniform stress distributions as shown in Fig. 13(d). As the result, the development of intragranular misorientation is dependent on the aspect ratio of the model as shown in Fig. 10. From the similar consideration as discussed above, it is found that lattice rotations in the opposite directions cancelled out owing to the activation of two equivalent compression in Sec. 4.6. basal slip modes for near-½0110 Consequently, the axis of lattice rotation became the same in compression and the sample coordinates for both near-½1120 compression. near-½0110 5.2 Suggested influences of present and potential effective factors Figures 4, 7, 8, 9 and 10 show variations of stress-strain responses and the line profiles of developed intragranular misorientations depending on the effective factors. One common feature is that slight changes in parameters result in significant change in the development of intragranular misorientation. The changes are especially significant from ªini = 4° to ªini = 5° as shown in Fig. 7(b), from h = 100 MPa to h = 200 MPa as shown in Fig. 8(b) and from m = 0.05 to m = 0.1 as shown in Fig. 9(b). This fact suggests that threshold values for each parameter to develop significant misorientations could be exist. The other interesting feature as shown in Figs. 4, 7, 8, 9 and 10 is the influence of effective factors on the shape of the line profile of crystal orientation. The initial crystal orientation and material parameters (hardening rate and strain rate sensitivity) similarly affect the transitions of crystal orientation as shown in line profiles even though the changes in stress-stress response are qualitatively very different. Contrary, the effect of aspect ratio on the transition of crystal orientation is qualitatively different to the effect of other parameters. Therefore, due to the superposition of effects of geometry and the other parameters could lead to more variations of development of intragranular misorientation as well as the significant influences of boundary condition and activity of each deformation mode as shown in the Sec. 4.5 and 4.6. In the results of the present analysis, the transitions of crystal orientations due to kinking are triangular which is similar to the experimental result of “L2” in Fig. 1(h). As pointed out in Sec. 2, the step-like transitions as “L1” in Fig. 1(h) are frequently observed in the experiments. To reproduce the step-like transitions, the numerical approaches other than the present approach might be required. As mentioned in Sec. 3.1, in the present study, non-local effects are not taken into account. With the non-local effects, strain hardening behaviour near kinked region should be very different due to the development of non-local back stress because there are pronounced slip gradient as shown in Fig. 6, which affects slip distributions and intergranular 972 T. Mayama, T. Ohashi, Y. Tadano and K. Hagihara misorientations. Relating to this, with the non-local effects, the prediction of size dependence in kinking is also expected. For further profound investigations with the aim of direct comparisons to experimental results, therefore, non-local effect should be included in the numerical method. Another point to note is that the present crystal plasticity analysis is performed based on the implicit assumption of the existence of enough initial dislocations to induce heterogeneous deformation field. This assumption is not adequate for the kinking at smaller scale where the initial dislocation density is not enough without nucleation of dislocations. In that case, alternative or additional mechanisms should be considered based on discrete approaches such as molecular dynamics simulations.46) 6. Conclusions In this study, the development of intragranular misorientations in single crystals due to the dominant activity of the basal slip system was investigated by a crystal plasticity finite element method. The effects of the initial crystal orientation, strain hardening rate, and strain rate sensitivity on the development of intragranular misorientations were numerically evaluated. The mechanism of the development of intragranular misorientations in models with no initial fluctuations or imperfections was discussed in terms of the nonuniform stress distribution and geometrical softening. The effects of a slight change in the boundary conditions on intragranular misorientations were also examined. The results of the present numerical study are summarized as follows. (1) Even in the case of no initial fluctuations or imperfections, basal slip accumulated locally in a single crystal. The localization originated from the nonuniform stress distribution caused by changes in the shape from a square prism to an oblique square prism due to the activation of the basal slip system. As a result of the localized accumulation of basal slip, significant intragranular misorientations developed owing to the continuous lattice rotation in the same direction. (2) Without lattice rotation, basal slip accumulated much more uniformly than in the case of localized accumulation with lattice rotation. The localized accumulation of basal slip was accelerated by lattice rotation because the lattice rotation due to basal slip increases the Schmid factor for active basal slip systems. (3) The initial deviation angle between the basal plane and the compressive direction, the strain hardening rate, and the rate sensitivity affected the development of intragranular misorientations. Smaller deviation angles, a lower strain hardening rate and lower rate sensitivity resulted in more significant development of intragranular misorientations. Acknowledgments This work was partially supported by a Grants-in-Aid for Scientific Research from MEXT (No. 26109717 and No. 26420020), JSPS Core-to-Core Program B, JSPS Program for Advancing Strategic International Networks to Accelerate the Circulation of Talented Researchers, and the Corporative Research Program of “Network Joint Research Center for Materials and Devices”. REFERENCES 1) W. Pantleon, W. He, T. P. Johansson and C. Gundlach: Mater. Sci. Eng. A 483484 (2008) 668671. 2) S. Scheriau and R. Pippan: Mater. Sci. Eng. A 493 (2008) 4852. 3) J. Konrad, S. Zaefferer and D. Raabe: Acta Mater. 54 (2006) 1369 1380. 4) M. Calcagnotto, D. Ponge, E. Demir and D. Raabe: Mater. Sci. Eng. A 527 (2010) 27382746. 5) D. Peirce, R. J. Asaro and A. Needleman: Acta Metall. 30 (1982) 1087 1119. 6) D. Peirce, R. J. Asaro and A. Needleman: Acta Metall. 31 (1983) 1951 1976. 7) S. V. Harren, H. E. Dève and R. J. Asaro: Acta Metall. 36 (1988) 2435 2480. 8) T. Ohashi: Mater. 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