v3.03.111 SSLS111 - Single plate eccentricity#
Summary:
This test makes it possible to validate the eccentricity of simple plates (that is to say that it is neither a multilayer nor a homogenized behavior).
The models used are:
modeling \(A\) - DST, DSTQ (QUAD4) + MECA_STATIQUE
modeling \(B\) - DKT, DKTG (TRIA3) + MECA_STATIQUE
modeling \(D\) - Q4G, Q4G (QUAD4) + MECA_STATIQUE
modeling \(E\) - Q4G, Q4G (QUAD4) + MECA_STATIQUE
modeling \(F\) - DKT, DKTG (QUAD4) + MECA_STATIQUE
modeling \(G\) - DST, DSQ (QUAD4) + MECA_STATIQUE
modeling \(H\) - DKTG, DKTG (QUAD4) + MECA_STATIQUE
modeling \(I\) - Q4G, Q4G (QUAD4) + MECA_STATIQUE
modeling \(J\) - DKT, DKT (QUAD4) + STAT_NON_LINE
modeling \(K\) - DKTG, DKTG (QUAD4) + STAT_NON_LINE
modeling \(M\) - Q4GG, Q4GG (QUAD4) + STAT_NON_LINE
modeling \(N\) - DKTG, DKTG (QUAD4) + STAT_NON_LINE — GLRC_DAMAGE
modeling \(O\) - DKT. DKT (QUAD4) + STAT_NON_LINE
Models \(A\) and \(B\): we model 2 plates that are eccentric with respect to the mean plane and we compare the results to an analytical solution.
Modeling \(D\), \(E\), \(F\), \(G\), \(H\),,, \(I\), \(J\), \(K\), \(M\), \(N\):
A single plate eccentric with respect to the mean plane is modelled and the results are compared to an analytical solution. Between modeling \(D\) and \(E\), we change the fineness of the mesh
Modeling \(O\):
A single plate eccentric with respect to the mean plane is modelled in order to validate the calculation of the stress components SIXZ and SIYZ. Two calculations are carried out, the first in monolayer serving as a reference and the second in multi-layer.