Modeling the effect of twinning and detwinning during strain-path changes of magnesium alloy AZ31
International Journal of Plasticity 25 (2009) 861–880
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International Journal of Plasticity 25 (2009) 861–880
Contents lists available at ScienceDirect
International Journal of Plasticity journal homepage: www.elsevier.com/locate/ijplas
Modeling the effect of twinning and detwinning during strain-path changes of magnesium alloy AZ31 Gwénaëlle Proust a,b,*, Carlos N. Tomé a, Ashutosh Jain c, Sean R. Agnew c a
Los Alamos National Laboratory, MST-8, MS G755, Los Alamos, NM 87545, USA University of Sydney, Sydney, NSW 2006, Australia c Department of Materials Science and Engineering, University of Virginia, 116 Engineering Way, Charlottesville, VA 22904, USA b
a r t i c l e
i n f o
Article history: Received 11 December 2007 Received in final revised form 17 May 2008 Available online 14 June 2008 Keywords: Twinning Polycrystal modeling Hardening Hexagonal materials Magnesium
a b s t r a c t Hexagonal materials deform plastically by activating diverse slip and twinning modes. The activation of such modes depends on their relative critical stresses, and the orientation of the crystals with respect to the loading direction. To be reliable, a constitutive description of these materials has to account for texture evolution associated with reorientations due to both dislocation slip and twinning, and for the effect of the twin boundaries as barriers to dislocation propagation. We extend a previously introduced twin model, which accounts explicitly for the composite character of the grain formed by a matrix with embedded twin lamellae, to describe the influence of twinning on the mechanical behavior of the material. The role of the twins as barriers to dislocations is explicitly incorporated into the hardening description of slip deformation via a directional Hall–Petch mechanism. We introduce here an improved hardening law for twinning, which discriminates for specific twin/dislocation interactions, and a detwinning mechanism. We apply this model to the interpretation of compression and tension experiments done in rolled magnesium alloy AZ31B at room temperature. Particularly challenging cases involve strain-path changes that force strong interactions between twinning, detwinning, and slip mechanisms. Ó 2008 Elsevier Ltd. All rights reserved.
* Corresponding author. Address: University of Sydney, School of Civil Engineering, Sydney, NSW 2006, Australia. Tel.: +61 2 9036 5498; fax: +61 2 9351 3343. E-mail address: [email protected] (G. Proust). 0749-6419/$ - see front matter Ó 2008 Elsevier Ltd. All rights reserved. doi:10.1016/j.ijplas.2008.05.005
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1. Introduction The purpose of the present work is twofold: develop a crystallographic model for the plastic response of Mg AZ31, applicable to non-monotonic deformation conditions and, in the process, increase our basic understanding of the role that slip and twin modes play in texture and hardening evolution. Wrought magnesium and magnesium alloys show, especially at room temperature, high asymmetry and anisotropy in their mechanical properties as a result of texture, the polar nature of twinning, and the fact that different deformation modes are active depending on the loading direction (Kelley and Hosford, 1968; Avedesian and Baker, 1999; Jain and Agnew, 2007; Lou et al., 2007). Several studies have been realized to understand the occurrence of the various slip and twin modes and their role onto the hardening behavior and texture evolution of Mg and Mg alloys during monotonic deformation (see for example Klimanek and Potzsch, 2002; Agnew et al., 2003; Agnew and Duygulu, 2005; Jiang et al., 2007). From these studies, it is clear that Mg and its alloys possess two ‘‘easy” deformation modes: hai slip on basal planes and tensile f1012gh 1011i twinning. In particular, tensile twinning has been associated with the increased hardening of the material that is observed when deformation takes place along the main basal component (Kelley and Hosford, 1968; Barnett, 2007a). These two modes alone, however, are insufficient to accommodate arbitrary deformation, and it has been found exper imentally that other slip modes contribute to strain accommodation: pyramidal hai slip f1011gh11 20i (e.g., Schmid and Boas, 1968), prism hai slip f1010gh1120i (e.g., Ward-Flynn et al., 1961) and pyrami (Stohr and Poirier, 1972; Obara et al., 1973; Ando and Tonda, 2000). dal hc + ai slip f1122gh11 23i The relative activity of the various slip and twinning modes described above depends on the specific loading conditions and initial texture; in turn, it determines texture evolution. In addition, hardening depends, in a complex manner, on the texture and interactions between slip and twin modes. Central to this effect is the fact that tensile twins change the texture of the material by reorienting domains of the grain by 86.6°. Moreover, twin boundaries can also act as obstacles to further slip and twinning deformation (Christian and Mahajan, 1995; Serra and Bacon, 1995; Serra et al., 2002). As a consequence, not only the monotonic loading response varies much depending on texture and testing direction and sense, but the mechanical response associated with strain-path changes (such as the ones which take place during forming) cannot be deduced from the knowledge of the monotonic response. This strain-path change behavior has been characterized experimentally for AZ31 Mg by Jain and Agnew (2006) and Lou et al. (2007). These authors observe that in sheet pre-deformed mainly by slip, twinning is not prevented by the presence of dislocations in the material, but the reloading yield strengths are slightly higher than for the annealed material. The influence of twins introduced by pre-straining on the reloading behavior of several magnesium alloys has also been explored (Caceres et al., 2003; Kleiner and Uggowitzer, 2004; Jain and Agnew, 2006; Brown et al., 2007; Lou et al., 2007; Mann et al., 2007; Wang and Huang, 2007). These authors report the phenomenon of detwinning (also referred to as untwinning) upon reversal or strain-path changes: the twins created during preload disappear during reload, and texture evolution is reversed to a large extent. The objective of this paper is to predict the mechanical behavior at room temperature of the Mg alloy AZ31B during strain-path changes. Recently, we published a similar analysis for pure Zr deformed at 76 K, a regime where tensile and compressive twins are active, and where secondary twinning plays an important role in increasing ductility (Proust et al., 2007). In that paper, where we present our new composite grain (CG) twin model, we argue that only a crystallography-based model that accounts for the orientation of slip and twin systems in each grain can describe the mechanical response for arbitrary deformation routes. Mg differs from Zr in that it twins more easily – after only 2% strain, Mg alloys can already exhibit as much as 14% twinned volume fraction (Chino et al., 2008) – and that it has been observe to undergo prolific detwinning. Therefore, it was necessary to extend the previously described CG twin model to properly describe these unique twinning behaviors associated with Mg alloys. In our previous paper (Proust et al., 2007), we provided a comprehensive review of polycrystal models addressing twinning in HCP materials. In short, early models were only concerned with describing texture evolution associated with monotonic loading (Van Houtte, 1978; Tomé et al., 1991; Lebensohn and Tomé, 1993; Philippe et al., 1995). More recently, researchers started developing
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constitutive models that, in addition to texture, also addressed the hardening response due to twinning associated with monotonic loading (Agnew et al., 2001; Kalidindi, 2001; Kaschner et al., 2001; Tomé et al., 2001; Salem et al., 2003, 2005; Staroselsky and Anand, 2003; Barnett et al., 2006; Clausen et al., 2008; Wu et al., 2007). Most of these approaches accounted for twin reorientation and used the concept of latent hardening to capture the role that twin interfaces play in hardening. It is also interesting to notice that models for martensitic transformation in TRIP steels share many commonalities with the crystallography-based twin models described above (Cherkaoui et al., 1998; Cherkaoui, 2003; Kubler et al., 2003) and have been adapted (Cherkaoui, 2003) for modeling twinning in fcc materials. The models described above reasonably predict the stress–strain response and texture evolution of magnesium alloys during monotonic deformation but predicting the mechanical behavior of these materials is more challenging once one considers changes in the loading path. To the best of our knowledge, only one attempt has been made to model the strain-path change behavior of Mg alloys. Jain and Agnew (2006) used the VPSC model (Lebensohn and Tomé, 1993) combined with the predominant twin reorientation (PTR) scheme (Tomé et al., 1991) and fitted the hardening parameters to monotonic deformation data. Although this particular model allows for latent hardening between the various deformation modes, it ignores the hardening directionality due to the microstructure evolution during twinning. The predictions for the strain-path changes did not match the experimental results, which demonstrated the need for a new model. This paper describes the use and extension of the CG twin model to predict the hardening, texture and twin volume fraction evolution of rolled Mg alloy AZ31B during monotonic and strain-path change deformations at room temperature. Although the focus is on modeling issues, we also interpret the experimental data to understand how the various deformation modes interact during strain-path change. We have also made a first attempt at modeling detwinning and our simple initial approach captures the main features associated with that process. 2. Experimental results 2.1. Material Commercial magnesium alloy AZ31B (3 wt% Al, 1 wt% Zn and balance Mg) sheet material was received in the stress relieved H24-temper. The material was annealed for an hour at 345 °C to reduce the presence of mechanical twins. After the heat treatment the microstructure of the material was an equiaxed grain structure with an average grain size of 13 lm. The initial texture was measured by Xray diffraction (XRD) and is shown in Fig. 1a. Compression and tension tests were performed at room temperature with an initial strain rate of 5 103 s1 using a computer controlled MTS screw-driven machine. The final texture of each deformed sample was then measured by electron backscattered diffraction (EBSD). Detailed experimental procedures were published previously (Jain and Agnew, 2006). 2.2. Monotonic deformation Fig. 1b shows the stress–strain response of the alloy deformed monotonically by in-plane tension (IPT), in-plane compression (IPC) and through-thickness compression (TTC). The respective final textures are shown in Fig. 2. As the initial texture is not axisymmetric about the sheet normal direction, some anisotropy was observed for tests along different in-plane directions (Jain and Agnew, 2007); however, the in-plane results reported in the present paper are solely obtained for a load applied parallel to the rolling direction (RD) of the plate. The IPT and TTC samples exhibit the typical hardening behavior associated with slip dominated deformation. During TTC, the material deforms mainly via basal hai and pyramidal hc + ai slip; the latter mechanism was first observed in Mg during c-axis compression of single crystals (Obara et al., 1973). However, recent studies (Koike, 2005; Jiang et al., 2006; compressive twinning, f1011g—f10 double twining and Barnett, 2007b) have shown that f1011g 12g double twinning, can also accommodate compressive strains along the c-axis at room f1013g—f10 12g temperature. However, those twinning systems never grow to reach the size or volume fraction of the f1012g tensile twins (Jiang et al., 2007) and, therefore, do not contribute to the same extent as the
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400
RD
RD
TD
TD
1.0 2.0 4.0 8.0
Stress (MPa)
10 1 0
0002
300 200
IPT TTC IPC
100 0 0.00
0.05
0.10
0.15
0.20
Strain 400
300
Stress (MPa)
Stress (MPa)
400
IPC Reloads
200 100 0 0.00
0.05
0.10
Strain
0.15
0.20
300 200
TTC Reloads
100 0 0.00
Strain-path change Monotonic 0.05
0.10
0.15
0.20
Strain
Fig. 1. (a) Basal and prismatic pole figure showing the texture of the as-annealed AZ31B Mg; (b) stress–strain curves for monotonic IPT, IPC and TTC; (c) strain-path change stress–strain curves for the samples deformed first in TTC to 5% and 10% strain and then deformed in IPC (the monotonic IPC stress–strain curve is represented by the dotted line for comparison); and (d) strain-path change stress–strain curves for the samples deformed first in IPC to 5% and 10% strain and then deformed in TTC (the monotonic TTC stress–strain curve is represented by the dotted line for comparison).
tensile twinning to shear accommodation. As noted by Jain et al. (2008) these twins cause reorientations within the main texture components and do not result in marked texture evolution. Hence, those systems will not be considered in the present simulations, rather it will be assumed that the required shear accommodated by these twins is reasonably approximated by hc + ai slip (Agnew et al., 2006). Before deformation, the material shows a strong basal texture with most of the grains having their c-axes within 40° from the TT direction. After 5% TTC, the basal component of the texture has been reinforced and now most grains have their c-axes within 30° from the TT direction. The spread in the c-axis distribution has been reduced, as can be seen on the texture profile shown in Fig. 3. To obtain the profiles from the experimental the XRD and EBDS texture data, we enforce axisymmetry on the pole figure by averaging the intensity along the azimuthal direction between 0 and 360°. During IPT, basal hai and prismatic hai slip accommodate most of the deformation (Barnett et al., 2006; Jain et al., 2008). But due to the c-axis spread of the initial texture, some grains are favorably oriented for tensile twinning (Jain et al., 2008). In the basal pole figure obtained for the sample deformed 10% in IPT (see Fig. 2), the presence of (0 0 0 2) intensity in the direction perpendicular to both the rolling and TT directions confirms the existence of twins in the material. Integrating the area under the basal pole intensity curve of Fig. 3, gives an estimated 7% volume fraction of twins after 10% deformation. The hardening displayed by the sample deformed in IPC shows the characteristic increase in the hardening rate associated with twinning. The microstructure of the material has been changed drastically, as can be seen in Fig. 4a, showing a micrograph of a sample deformed 7% in IPC. Most of the grains present twin lamellae and some of them are heavily twinned. The texture of the deformed material is also very different from the initial one (see Fig. 2). The basal component along the ND
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Measured 0001
Predicted 10 1 0
0001
10 1 0
5% TTC
10% IPC
10% IPT 0.4 1.0 2.0 5% TTC
4.0
+ 5% IPC
8.0 RD
5%IPC+ 10%TTC TD Fig. 2. Comparison of measured and predicted basal and prismatic pole figures for monotonic and strain-path change deformations. The measured pole figures were obtained by EBSD. IPC and IPT were realized along the RD. The 0.4 intensity line is included in the 10% IPT case to reveal the ‘anomalous’ twinning effect.
has disappeared and now the c-axes of the crystals are aligned with the loading direction due to the 86.6° reorientation caused by tensile twinning. A comparison of the texture profiles obtained for the as-annealed material and the sample deformed in IPC, allows us to identify that there is a separation between the c-axis orientations belonging to the matrix or to the twinned portion of the material at a tilt angle of about 50°. Integrating the intensity profiles between 50° and 90°, and subtracting the initial volume fraction in the same interval, allows us to evaluate the twin volume fractions in deformed samples. Results are reported in Table 1, where it can be seen that after 10% IPC, 90% of the aggregate has twinned. 2.3. Effect of prior slip on subsequent twinning In order to study the effect of dislocation substructure on subsequent deformation dominated by twinning, samples were pre-strained in TTC up to strains of 5% and 10%, and then reloaded in IPC. The stress–strain curves corresponding to these experiments are shown in Fig. 1c. The final texture corresponding to the sample deformed 5% in TTC and then 5% in IPC is shown in Fig. 2. During TTC pre-straining, the material deforms primarily by basal hai and pyramidal hc + ai slip, though there is compressive twinning as noted by Jiang et al. (2006). likely some f1011g
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Measured
Predicted 0.3
Normalized intensity
Normailized Intensity
0.3
0.2
0.1
0.0
0.2
0.1
0.0 0
10
20
30 40 50
60 70
80 90
0
10
angle Initial
20
30 40 50
60 70
80 90
angle 5% TTC
5% TTC+5% IPC
10% IPT
10% IPC
5% IPC +10% TTC
Fig. 3. Comparison of the measured and predicted texture profiles used to estimate the twin volume fractions in the samples deformed by IPC (monotonic or strain-path change) and by IPT. The angle represents the orientation of the c-axis of the various crystals in reference to the normal direction of the plate. The solid black line represents the texture profile of the as-annealed material and is used as the base line in the twin volume fraction calculations.
Fig. 4. Micrographs showing the microstructure of (a) a sample deformed by in-plane compression to a strain of 7% and (b) a sample first deformed by in-plane compression to a strain of 7% and then by through-thickness compression to a strain of 6%.
Table 1 Estimation of the twin volume fraction using the measured and predicted texture profiles shown in Fig. 3 Twin volume fraction
10% IPT 10% IPC 5 IPC + 10% TTC 5% TTC + 5% IPC
Experimental
Prediction
0.07 0.90 0 0.65
0.08 0.86 0 0.72
The IPC reload curve following 5% and 10% TTC pre-load is similar to the monotonic IPC curve: the deformation is still largely accommodated by twinning, as the hardening and texture evolution show, but the onset of twinning happens at a higher stress. The value of the reload yield strength has in-
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creased by 40 and 60 MPa, respectively, and there is a Bauschinger-like transition within the first 2% deformation. In addition, both reload curves show a more extended transition from easy to hard deformation, probably as a result of a more balanced twin and slip activity, which also leads to a slower texture evolution. Lou et al. (2007) proposed that dislocation multiplication affects the twin nucleation stress. In this case, during the preloading, hai and hc + ai dislocations are introduced. These dislocations may act as barriers to twin nucleation or/and twin propagation. This would explain both the increase of the stress corresponding to the onset of twinning with the increase in pre-strain, as well as the more extended hardening plateau associated with twinning. 2.4. Detwinning In order to study the effect of twinning on subsequent deformation, samples were pre-strained in IPC up to strains of 5% and 10%, and then reloaded in TTC. The stress–strain curves corresponding to these experiments are shown in Fig. 1d, and the texture corresponding to 5% IPC followed by 10% TTC is shown in Fig. 2. During pre-straining, the material deforms primarily by tensile twinning, but reverses the twins (detwins) during the reload stage. The integration of the texture profiles is consistent with this understanding; Table 1 indicates that the material is twin free after 10% TTC reload. During monotonic TTC, primarily basal hai and pyramidal hc + ai slip are active; however, once twins have been introduced by previous IPC, the hardening behavior of the material reloaded in TTC changes drastically. The reload flow curves display the sigmoidal shape associated to deformation twinning. The reason is that the grains that have twinned during IPC are now properly oriented to twin again (or detwin) during subsequent TTC since the basal poles are roughly at 90° from the TT direction. The reversal of the texture (see Fig. 2) associated with TTC reloads is a strong indication of detwinning. To prove that detwinning is actually happening during this strain-path change, micrographs of the microstructure were taken after 7% IPC (Fig. 4a) and after 7% IPC followed by 6% TTC (Fig. 4b). By comparing Fig. 4a and b, we see that the amount of twins has decreased during TTC reload and though some twin lamellae are still visible in Fig. 4b, there are many grains that are twin free and very few grains are heavily twinned. Detwinning may not be complete because the test was stopped before full strain reversal (Wu et al., in press). Both reloading curves in Fig. 1d are similar to the monotonic IPC stress–strain curve except for the value of the reload yield strength. After 5% IPC pre-strain, the yield stress upon reloading is actually lower than the initial yield for IPC indicating that detwinning is easier to activate than twinning, as noted previously (Lou et al., 2007). As the amount of pre-straining increases, the yield strength increases. This phenomenon could be explained by the fact that slip is activated inside and around the newly created twins and, as the density of dislocations increases, detwinning becomes harder to activate. 3. Polycrystal model The Visco-Plastic Self Consistent (VPSC) polycrystal model is used as a platform for implementing a mesoscopic Composite Grain (CG) model that accounts for twinning evolution inside the grain. The reader can find a detailed description of VPSC and of the recently proposed CG model in our recent paper (Proust et al., 2007), where the model was applied to describe the response of Zr subjected to strain-path changes. Within the VPSC approach, each grain is regarded as a visco-plastic inclusion embedded in and interacting with the visco-plastic effective medium that represents the aggregate. When the medium is subjected to externally imposed loading conditions, the relative stiffness of grain and medium determine the deformation of the former. The strain rate is assumed to be uniform inside the grain, and is accommodated by the shear rates provided by slip and twin systems. The strain rate of the grain, e_ , is related to the shear rates c_ s contributed by slip and twinning systems through a rate sensitive law
e_ ij ¼
X s
msij c_ s ¼ c_ 0
X s
msij
n ms : r
ss
¼ M sec ijkl rkl :
ð1Þ
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where r is the stress tensor, and ss is the threshold resolved shear stress associated with the system s. Msec is a linearized visco-plastic compliance tensor (secant approximation) that is accurate for a discrete range of rates and stresses. Its evolution with deformation is a complex function of the slip and twinning activity in the grain and is discussed below. 3.1. The composite grain twin model The CG twin model was introduced to describe the strain-path change behavior of Zr at 76 K (Tomé and Kaschner, 2005; Proust et al., 2007). Differences in how twinning operates in Mg by comparison to Zr, forced us to extend the model and revise some of the assumptions used in Proust et al. (2007). We refer the interested reader to the two papers mentioned above, while here we focus on what is new about the model. Fig. 5 illustrates the characteristics of the CG model. During a deformation simulation, the Predominant Twin System (PTS) is identified in each grain, and a layered structure of twins parallel to the twin plane of the PTS is assumed to form and to evolve with twin activity. The interaction between this composite grain and the surrounding effective medium is characterized by the CG effective mechanical properties. The layers are assumed to be equidistant and two parameters are introduced: the separation dc of the center planes of the lamellae, and the maximum volume fraction of the grain that may PTS . Because twins are assumed (as a first approximation) to pose impenbe reoriented by twinning fmax etrable barriers to dislocations or to other twins, the separation of the twin interfaces is relevant to the hardening response, as we will see below. The first adaptation we have introduced in the CG model to reproduce the behavior of Mg concerns the spacing between the twin lamellae. For the Zr we assumed that the parameter dc was constant throughout the entire deformation, which was in agreement with our experimental data showing that by 30% deformation less than 50% of the material had twinned (Proust et al., 2007). In the case of Mg, the experimental data shows that after 10% deformation almost 90% of the material has twinned, and that twins ‘coalesce’ inside the grain. Therefore, it does not seem appropriate to have twin boundaries acting as barriers when almost the entire grain is transformed by twinning. For this reason, the value of dc is made to increase with the PTS volume fraction until reaching a value of one (which corresponds to having only one twin domain), when 70% of the grain has twinned. By creating this layered twin–matrix structure inside grains, we are able to account for the directional barrier effect created by the twin boundaries. If slip is occurring, inside the matrix or inside the twin, on a plane non-parallel to the twin/matrix interface, the dislocation mean free path is reduced
Fig. 5. Schematics of the CG showing the characteristic lengths used in the model and the evolution of these lengths with the PTS volume fraction when the material twins and detwins. (a) The material has not started to twin and the grain is only constituted of a matrix region, (b) when the material starts to twin, several thin lamellae are created, (c) as the PTS volume fraction increases, some lamellae merge together increasing the mean free path (dmfp) for the dislocation motion inside the twinned domains, and (d) the grain has almost completed twinned and we have now a single twinned region.
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due to the barrier effect and that particular slip system will be harder to activate. This idea is implemented in the CG model through a Hall–Petch term that depends on the calculated mean free path for each slip system in the matrix and in the twins. The second change we have introduced in the extended CG twin model concerns the coupling between twin and matrix. In the previous paper presenting the CG model, we introduced two different methods to calculate the deformation of matrix and twin: the coupled and uncoupled twin lamellae. In the former case, continuity of stress and strain is enforced across the twin interface that separates twin and matrix, once the PTS is identified in the grain and the twins are created. In the latter approach, twin and matrix representative ellipsoids are assumed to interact independently with the effective medium, although the volume transfer between matrix and twin and the shape update (due to the evolution of the twin volume fraction, the thickness of the matrix and twin lamellae is changing) are still enforced. To predict the behavior of this Mg alloy we use the coupled deformation scheme at the beginning of deformation, when twins can be regarded as thin lamellae (as in Fig. 4a). When the twin volume fraction inside the grain is higher than 70% and twins coalesce, we transition to the uncoupled scheme. 3.2. Hardening of slip systems Within the CG model, three mechanisms may contribute to the hardening of slip systems inside the matrix and the twin: the evolution of the statistical dislocations with strain, the evolution of geometrically necessary dislocations (GND) and a directional Hall–Petch effect:
ss ¼ ssSTAT þ ssGND þ ssHP :
ð2Þ
Each of these terms is updated incrementally at each straining step. The first term is a classical saturation Voce law associated with statistical dislocations, to which a latent hardening effect has been added:
^s X ss0 s0 ds h Dc ; dC s0 Ch ^s ¼ s0 þ s1 1 exp 0 : where s
DssSTAT ¼
s1
ð3aÞ ð3bÞ
0
Here C is accumulated shear in the grain, Dcs the shear increment in the slip or twinning system s0 0 and hss the latent hardening coefficient, coupling hardening of s due to activity of s0 . While only the barrier effect of the PTS is explicitly accounted for, the other twinning systems can contribute to the hardening of slip systems through the latent hardening parameter. s The second term of Eq. (2) depends on the directional mean free path dmfp defined by the assumed lamellar spacing of the PTS for dislocations on system s. It represents the influence of the GNDs over the threshold stress (Karaman et al., 2000):
DsSGND ¼
HsGND s s dmfp ð STAT þ
s
ssGND Þ
Dcs :
ð4Þ
The last term of Eq. (2) describes the directional Hall–Petch effect:
Hs
HP ssHP ¼ qffiffiffiffiffiffiffiffiffi : s
ð5Þ
dmfp
While the GND contribution is not so relevant at the strains considered here, the Hall–Petch term plays an important role on hardening, especially during strain-path changes. In addition, the Hall– Petch effect introduces length scaling into the model. It has been proposed that originally mobile dislocations will become sessile once the lattice in which they reside has been twinned (Basinski et al., 1997). Basinski et al. further proposed that these ‘‘inherited dislocations” will harden slip inside the twins. However, because the relative effects of these hardening mechanisms have yet to be experimentally differentiated, only the Hall–Petch effect will be used in our model.
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3.3. Hardening of twinning systems When the CG twin model was applied to Zr, the hardening law given by Eq. (2) was used to describe the hardening behavior of both slip and twinning systems. While this hardening law is appropriate to describe the hardening associated with dislocation creation and annihilation, in connection to twinning it should only be regarded as an empirical law that provides a dependence of twin hardening with accumulated shear. We verified that, in the case of Mg, it is not possible to adjust the parameters of such law to the experimental hardening behavior observed during strain-path changes. As a consequence, we present here a ‘deformation mode specific’ law to describe the hardening of twinning systems, of the form: TWS
s
¼s
TWS 0
þ
X M
(
s
M
1 exp
h M CM
sM
!)
;
ð6Þ
where the sum is made over all the slip modes M (basal hai, prism hai, pyramidal hc + ai) that can be activated during deformation, and CM represents the accumulated shear for all the slip systems belonging to the slip mode M. While this new hardening law is empirical, it provides for a selective influence of different deformation modes upon twinning, which is more consistent with the sparse experimental and theoretical information available. For example, it has been proposed by Mendelson (1970) that non-planar dislocation dissociations may be the mechanism of twin nucleation for HCP materials. As a consequence: (a) twin nucleation is delayed until specific dislocation structures develop and (b) such dissociation may be favorable for one type of dislocation but not for another. In what concerns twin growth, atomic scale simulations done for Mg and a-Ti (Serra and Bacon, 1996; Pond et al., 1999) suggest that twin interfaces may propagate (grow) via mixed basal dislocations that, upon arrival at the twin interface, dissociate into dipolar twin dislocations which propagate and advance the interface. As a consequence, twin propagation should be coupled to dislocation activation (Serra and Bacon, 1996). Moreover, during strain-path changes, it was observed that the onset of twinning happens at a higher stress once the material has been deformed by a slip dominated process. Lou and coworkers (Lou et al., 2007) proposed that pyramidal hc + ai dislocations increase the twin nucleation stress. The empirical hardening law that we propose here for tensile twins reflects all these observations. The twinning threshold stress value increases or decreases with the amount of shear accommodated by the various slip modes. The nucleation and growth phases of twinning are simulated by lowering the value of the twinning threshold stress when strain is accommodated by specific slip systems. For this purpose, negative values are given in Eq. (6) to the parameters sM and hM of basal and prism slip. In the case studied here, it is assumed that hai dislocations on basal planes are the most likely to induce twin nucleation and growth, based on atomistic simulations studies (Serra and Bacon, 1996) and the observations that basal slip is easy to activate in most orientations. Tensile twinning and hc + ai dislocations on pyramidal planes are competing mechanisms. However, during strain-path changes, it is possible to have previously induced hc + ai dislocations interact with twins and harden them. In the new hardening law it is possible to describe this phenomenon by giving positive values to the parameters sM and hM. Fig. 6b shows the evolution of the twinning threshold stress with the amount of shear accommodated by each slip mode. The determination of the hardening parameters associated with these curves is explained in Section 4 of this paper. The same hardening laws are applied in the twinned regions to predict the evolution of the slip and twinning threshold stresses as in the matrix. For slip, the same hardening parameters are used in the matrix and in the twin. However, the experimental evidence suggests that detwinning is easier than twinning (Lou et al., 2007); therefore, the hardening parameters, which describe the threshold stress evolution for twinning are different inside the matrix and inside the twins (detwinning), as discussed below. 3.4. Detwinning It has been experimentally observed for Mg that when the loading direction is changed, grains that had previously twinned can detwin easily (Caceres et al., 2003; Kleiner and Uggowitzer, 2004; Lou
871
250
250
200
200
τTWS (MPa)
τS (MPa)
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