Data file(s):
case 1 (± 45° plies): plyuni-m020-1.dat
case 2 (0° plies): plyuni-m020-2.dat
Analysis type: Non linear static analysis
Keywords: Damage Ply material
The structure consists of a two-dimensional square sample. The sample is loaded under traction loads in function of time. Its length is 1 mm and its thickness 1 mm. Two stacking sequences are considered:± 45° plies (case 1) and 0° plies (case 2). As we use a unit thickness, the normal force in the membrane will be equal to the mean stress.
The applied traction loads are defined in function of time as shown in figure 2.
The analysis is performed with the non-linear module (MECANO). The command with the standard SAMCEF procedure for this example may be as follows on Unix workstations:
% samcef ba, me plyuni-m020-i n 2
We want to save (.SAI ARCH) the normal force and the upper skin strain tensor (STYP 9437 9445) of element 1 (components 1 and 2) as function of time. This selection has to be done in pre- treatment. The selected quantity will then be available in post-treatment. By default, selected results are saved at any time step.
% samcef bp plyuni-m020-i n 2
The data used to post-process the results is included in the bank files plyuni-m020-1.dat and plyuni-m020-2.dat, after the entry point .POST. It is loaded with:
Bacon>input.POST
Figures 3 and 4 show the axial mean stress in function of the axial and transverse strains. These results are plotted with:
.VIF code 9437 9445 MAI 1 1 COMP 1 1 CHA
code 9437 9445 MAI 1 1 COMP 1 2 SUP
In figure 3, we can see on the loading and unloading paths that there is a residual deformation (plasticity) and a loss of stiffness (damage).
Figure 4 shows that the behavior is different in traction and in compression.
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Last update: 1-Mar-2018
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