Lj. An et A. Peirce, A WEAKLY NONLINEAR-ANALYSIS OF ELASTO-PLASTIC-MICROSTRUCTURE MODELS, SIAM journal on applied mathematics, 55(1), 1995, pp. 136-155
At certain critical values of the hardening modulus, the governing equ
ations of elasto-plastic how may lose their hyperbolicity and exhibit
two modes of ill-posedness: shear-band and flutter ill-posedness. Thes
e modes of ill-posedness are characterized by the uncontrolled growth
of modes at infinitely fine scales, which ultimately violates the cont
inuum assumption. In previous work [L. An and A. Peirce, SIAM J. Appl.
Math., 54(1994), pp. 708-730], a continuum model accounting for micro
scale deformations was built. Linear analysis demonstrated the regular
izing effect of the microstructure and provided a relationship between
the width of the localized instabilities and the microlength scale. I
n this paper a weakly nonlinear analysis is used to explore the immedi
ate postcritical behavior of the solutions. For both one-dimensional a
nd anti-plane shear models, post-critical deformations in the plastic
regions are shown to be governed by the Boussinesq equation (one of th
e completely integrable PDEs having soliton solutions), which describe
s the Essential coupling between the focusing effect of the nonlineari
ty and the dispersive effect of the microstructure terms. The soliton
solution in the plastic region is patched to the solution in the elast
ic regions to provide a special solution to the weakly nonlinear syste
m. This solution is used to derive a relation between the width of the
shear band and the length scale of the microstructure. A multiple sca
le analysis of the constant displacement solution is used to reduce th
e perturbed problem to a nonlinear Schrodinger equation in the amplitu
de functions-which turn out to be unstable for large time scales. Stab
ility analyses of more complicated special solutions show that the low
wave number solutions are unstable even on the fast time scales while
the high wave numbers are damped by the dispersive microstructure ter
ms. These theoretical results are corroborated by numerical evidence.
This pervasive instability in the strain-softening regime immediately
after failure, indicates that the material will rapidly move to a lowe
r residual stress state with well-defined shear bands.