1. Reference problem#

1.1. Geometry#

According to the modeling \(\mathrm{2D}\) (plane deformation) or \(\mathrm{3D}\), we consider respectively a rectangle or a bar (see Figure 1.1-1).

_images/100002010000025C000001B9E3FEB8F31B7BFF89.png

Figure 1.1-a : Geometry and Meshing of a rectangle (a) and a bar (b)

1.2. Material properties#

Elasticity:

\(E=190000\text{MPa}\)

Young’s module

\(\mathrm{\nu }=0.3\)

Poisson’s ratio

Work hardening curve:

\(R(\mathrm{\kappa })=488.36+57.13(1-\mathrm{exp}(-8613\mathrm{\kappa }))+238.73(1-\mathrm{exp}(-10.39\mathrm{\kappa }))\)

Ductile damage law GTN:

\({q}_{1}=1.5\)

Model parameter GTN

\({q}_{2}=1.07\)

Model parameter GTN

\({f}_{0}=0.0002i\)

Initial porosity

\({f}_{n}=0\)

Germination Parameter

\({f}_{c}=0.05\)

Coalescence porosity

\(\mathrm{\delta }=3\)

Coalescent acceleration coefficient

\(c=1N\)

Non-local parameter

\(r=5000\mathit{MPa}\)

Lagrange penalty parameter

Norton parameters in the viscoplastic case (C modeling):

\(n=14\)

Exhibitor of Norton’s Law

\(K=150\mathit{MPa}\mathrm{.}{s}^{1/14}\)

Norton’s law coefficient

In particular, the distribution of the initial porosity is not homogeneous. It increases with altitude: \({f}_{0}=0.0002i\) where \(i\) refers to the i-th element layer and \(1\le i\le 10\).

In DEFI_MATERIAU, the following information should be filled in:

ELAS

ECRO_ NL

**** NL

GTN

NON_LOCAL

NORTON

E = 190000

R0= 488.361

Q1 = 1.5

C_ GRAD_VARI = 1

N = 14

NU = 0.3

R1 = 57.133

Q2 = 1.07

PENA_LAGR =5000

K = 150

GAMMA_1 = 8613

PORO_INIT = 0.0002i

R2 = 238.731

COAL_PORO = 0.05

GAMMA_2 =10.386

COAL_ACCE = 3

1.3. Boundary conditions and loads#

For modeling \(2D\) (axisymmetric), the displacements along the \(X\) axis of all the nodes are controlled: \({u}_{x}=1.22x\), the displacements along the \(Y\) axis of the nodes of the same altitude remain uniform, the node \(A\) is blocked along the \(Y\) axis (see Figure 1.1-1 (a) for geometry).

For modeling \(3D\), the movements along the \(X\) axis and the \(Y\) movements of all the nodes are controlled: \({u}_{x}=1.22x\) and \({u}_{y}=1.22y\), the movements along the \(Z\) axis of the nodes of the same altitude remain uniform, the node \(A\) is blocked according to \(Z\). (see Figure 1.1-1 (b) for geometry).

Boundary conditions and loads are imposed this way so that the problem in \(2D\) and the problem in \(3D\) are the same.

The loading is applied at a constant speed for 1000 s. Time steps of 1 s each are imposed.