5. D modeling#
In this modeling, the linear elements of modeling A have been replaced by quadratic elements. Everything else is the same.
5.1. Characteristics of the mesh#
These are the same modeling characteristics as for modeling A but we transformed the linear element mesh into a quadratic element mesh using the CREA_MAILLAGE/LINE_QUAD command. The structure is thus meshed with hexahedra with 20 knots.
5.2. Tested features#
These are the same tested functionalities as those of modeling A.
5.3. Tested sizes and results#
The POST_MAIL_XFEM operator makes it possible to mesh the cracks represented by the X- FEM method. The operator POST_CHAM_XFEM then makes it possible to export the results X- FEM to this new mesh. These two operators should only be used after the calculation in post-processing views. They allow nodes to be generated just below and above the interface and to show their movements.
For each lateral face of the structure (\(y=0\) and \(y=\mathrm{LY}\)), we test the movements of the nodes located just above and just below the level set.
5.3.1. Compression loading (pressure loading)#
Identification |
Reference |
\(\mathrm{DY}\) for all nodes on the left surface located just below the interface |
10-6 |
\(\mathrm{DY}\) for all nodes on the left surface located just above the interface |
10-6 |
\(\mathrm{DY}\) for all nodes on the right surface located just below the interface |
-10-6 |
\(\mathrm{DY}\) for all nodes on the right surface located just above the interface |
-10-6 |
5.3.2. Compression loading/traction (pressure loading)#
Identification |
Reference |
\(\mathrm{DY}\) for all nodes on the left surface located just below the interface |
-10-6 |
\(\mathrm{DY}\) for all nodes on the left surface located just above the interface |
10-6 |
\(\mathrm{DY}\) for all nodes on the right surface located just below the interface |
10-6 |
\(\mathrm{DY}\) for all nodes on the right surface located just above the interface |
-10-6 |
5.3.3. Compression loading (surface force loading)#
Identification |
Reference |
\(\mathrm{DY}\) for all nodes on the left surface located just below the interface |
10-6 |
\(\mathrm{DY}\) for all nodes on the left surface located just above the interface |
10-6 |
\(\mathrm{DY}\) for all nodes on the right surface located just below the interface |
-10-6 |
\(\mathrm{DY}\) for all nodes on the right surface located just above the interface |
-10-6 |
5.3.4. Compression/tensile loading (surface force loading)#
Identification |
Reference |
\(\mathrm{DY}\) for all nodes on the left surface located just below the interface |
-10-6 |
\(\mathrm{DY}\) for all nodes on the left surface located just above the interface |
10-6 |
\(\mathrm{DY}\) for all nodes on the right surface located just below the interface |
10-6 |
\(\mathrm{DY}\) for all nodes on the right surface located just above the interface |
-10-6 |
To test all the nodes at once, we test the MIN and the MAX of the column.