1. Reference problem#
1.1. Geometry and loading#
We consider a Compact Tension specimen (\(\mathit{CT}\)) with a thickness of \(25\mathit{mm}\). The geometry includes a rigid pin to which the load is applied.

Figure 1: Geometry
1.2. Material properties#
To describe the behavior of the axisymmetric specimen material (bulk material), an elastoplastic behavior law with isotropic work hardening is used (law VMIS_ISOT_TRAC).
We take: \(E\mathrm{=}207\mathit{GPa}\) and \(\nu \mathrm{=}0.3\) and the work hardening curve used is given below:

Figure 2: Isotropic work hardening curve of solid material.
For interface elements the following parameters are used in law CZM_TRA_MIX:
\({\sigma }_{c}\mathrm{=}1800\mathit{MPa}\), \({G}_{c}\mathrm{=}150\mathit{MPa}\mathrm{\cdot }\mathit{mm}\), \({\delta }_{e}\mathrm{=}0.01\mathit{mm}\), \({\delta }_{p}\mathrm{=}0.06\mathit{mm}\), \({\delta }_{c}\mathrm{=}0.117\mathit{mm}\)
The resulting law is shown schematically below.

Figure 3: Law of behavior of interface elements.
NB: Only half of the crack is modelled thanks to the symmetry of the problem, the toughness of the material is \(2{G}_{c}\).
Finally, the rigid pin has elastic behavior (law ELAS) with: \(E\mathrm{=}1\mathrm{\times }{10}^{9}\mathit{MPa}\), \(\nu \mathrm{=}0.3\)
1.3. Boundary conditions and loading#
The limit conditions imposed on the pin are as follows:
move to \(X\) blocked,
imposed displacement \(l\) in the \(Y\) direction.
The evolution of displacement \(l\) over time is given in the following table:
Time \(\mathrm{[}s\mathrm{]}\) |
0 |
0.4 |
Displacement \(l\) \(\mathrm{[}\mathit{mm}\mathrm{]}\) |
0 |
1.6 |
The cohesive zone is represented by the interface elements on the test piece ligament. The boundary conditions on the interface elements are:
displacement in \(X\) imposed identical on both lips of the cohesive zone,
\(Y\) movement stuck on the lower lip.