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A comparative discrete-dislocation/nonlocal crystal-plasticity

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typeset2:/sco3/jobs1/ELSEVIER/msa/week.17/Pmsa15088y.001 Wed May 16 07:53:37 2001 Page Wed<br />

D. Columbus, M. Grujicic / Materials Science and Engineering A000 (2001) 000–000 13<br />

Fig. 6. (a) The equivalent plastic strain contour plot; (b) the 22 stress<br />

contour plot and (c) the deformed finite element mesh for the<br />

<strong>nonlocal</strong> <strong>crystal</strong> <strong>plasticity</strong> (Model-I) analysis at the onset of crack<br />

extension (K I/K I0=1.18, arrows indicate position of crack tip).<br />

addition, the stress levels in the corresponding three<br />

regions are comparable for the two types of analyses. A<br />

comparison of the distorted finite element mesh resulting<br />

from the <strong>crystal</strong>-<strong>plasticity</strong> analysis, Fig. 6c, with the<br />

corresponding mesh resulting from the <strong>discrete</strong>-<strong>dislocation</strong><br />

analysis, Fig. 3c, indicates very similar crack profiles<br />

in the two cases. However, the deformation bands<br />

observed in Fig. 3c, can not be readily identified in Fig.<br />

6c.<br />

To show the role of the <strong>nonlocal</strong> <strong>crystal</strong>-<strong>plasticity</strong><br />

phenomenon on mode I crack growth behavior, the<br />

equivalent plastic strain, the normal, 22, stress contour<br />

plot, and the distorted mesh obtained from a <strong>crystal</strong>-<strong>plasticity</strong><br />

analysis based on Model-I parameters, but with the<br />

<strong>nonlocal</strong> parameters (c, a0 and a1) turned off, at the same<br />

level of stress intensity factor as in Fig. 6a–c (KI/KI0= 1.18), are shown in Fig. 7a–c. This analysis is referred<br />

to as a local <strong>crystal</strong>-<strong>plasticity</strong> analysis.<br />

The main differences in the distribution of equivalent<br />

plastic strain in local (Fig. 7a) and <strong>nonlocal</strong> (Fig. 6a)<br />

<strong>crystal</strong>-<strong>plasticity</strong> analyses can be summarized as follows:<br />

1. higher values of equivalent plastic strain are observed<br />

in the local-<strong>plasticity</strong> case and the highest<br />

plastic-strain region is located at the crack tip. In<br />

the <strong>nonlocal</strong> <strong>crystal</strong>-<strong>plasticity</strong> case, the highest plastic-strain<br />

region is slightly removed from the crack<br />

tip;<br />

2. the plastic strain bands, while well formed in both<br />

cases, appear to be narrower in the local-<strong>plasticity</strong><br />

case.<br />

A comparison of the local, Fig. 7b, and <strong>nonlocal</strong>,<br />

Fig. 6b, 22 stress distributions indicates that while the<br />

distributions are quite similar, ca. 8% higher tensile<br />

stress levels are attained in the <strong>nonlocal</strong> <strong>crystal</strong>-<strong>plasticity</strong><br />

case.<br />

A comparison of the local, Fig. 7c, and <strong>nonlocal</strong>,<br />

Fig. 6c, deformed finite element meshes indicates significant<br />

differences in the crack profile especially near<br />

the crack tip. In the local <strong>crystal</strong>-<strong>plasticity</strong> case, the<br />

crack tip is quite blunted and no crack advance is<br />

observed. In sharp contrast, the crack tip is considerably<br />

sharp and crack extension is observed in the case<br />

of <strong>nonlocal</strong> <strong>crystal</strong> <strong>plasticity</strong>.<br />

The equivalent plastic strain, the normalized 22 stress contour plot, and the deformed finite element<br />

mesh at the onset of crack extension (KI/KI0=1.53) for<br />

the Model-II <strong>nonlocal</strong> <strong>crystal</strong>-<strong>plasticity</strong> analysis are<br />

shown in Fig. 8a–c, respectively.<br />

A comparison of the equivalent plastic strain distributions<br />

obtained using Model-II (Fig. 8a) and Model-I<br />

(Fig. 6a) <strong>nonlocal</strong> <strong>crystal</strong>-<strong>plasticity</strong> analyses indicates<br />

that higher plastic strain levels are attained in the<br />

former case. In addition, the highest plastic strain region<br />

in the case of Model-II is located at the crack tip.<br />

These findings are consistent with the fact that in order<br />

to delay the onset of crack extension in the Model-II<br />

UNCORRECTED PROOF<br />

crack tip is associated with the highest tensile stress<br />

values while the region behind the crack tip contains<br />

low-magnitude primarily negative 22 stress values.<br />

These observations are fully consistent with the ones<br />

made during the <strong>discrete</strong>-<strong>dislocation</strong> analysis, Fig. 3b. In

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