1. Reference problem#
The damage \(D(t)\) is calculated from the data of the stress tensor \(\sigma (t)\) and the cumulative plastic deformation \(p(t)\) resulting from a thermomechanical calculation. The damage kinetics is given by:
\(\dot{D}=\frac{1}{{(1-D)}^{\mathrm{2s}}}{\left[\frac{1}{\mathrm{3ES}}(1+\nu ){\sigma }_{\mathrm{eq}}^{2}+\frac{3}{\mathrm{2ES}}(1-2\nu ){\sigma }_{H}^{2}\right]}^{s}\dot{p}\) |
if \(p>{p}_{d}\) |
\(D=0\) |
otherwise |
\({\sigma }_{\mathrm{eq}}\) is the equivalent von Mises stress
\({\sigma }_{H}\) is the hydrostatic stress
\({p}_{d}\) represents the damage threshold
\(S\) is a material characteristic (\(\mathrm{MPa}\))
\(s\) is a material characteristic
1.1. Material properties#
\(\mathrm{Temp}(°C)\) |
\(E(\mathrm{MPa})\) |
\(\nu\) |
\(S(\mathrm{MPa})\) |
\({P}_{d}\) |
\(s\) |
|
Case 1 |
Case 2 |
|||||
143006.0E+6 |
0.33 |
7.0 |
1.005E-6 |
0.8 |
1.003 |
|
143006.0E+6 |
0.33 |
7.0 |
1.005E-6 |
0.8 |
1.003 |
|
143006.0E+6 |
0.33 |
7.0 |
1.005E-6 |
0.8 |
1.003 |
Two exponent values
are successively used for the validation of developments in CALC_CHAMP.
1.2. Loading#
The loading corresponds to a tensile test at constant temperature and at a fixed deformation rate. It is defined in paragraph [§2.2].