Reference problem ===================== Geometry --------- **A4** **A3** 5 subdivisions Z Y **A1** GRN011 **A2** 0.2 :math:`m` 0.2 :math:`m` 10 subdivisions x The coordinates of the points are given in meters (:math:`m`): .. csv-table:: ":math:`\mathrm{A1}(\mathrm{0,0}\mathrm{,0})` "," :math:`\mathrm{A3}(\mathrm{10,5}\mathrm{,0})`" ":math:`\mathrm{A2}(\mathrm{10,0}\mathrm{,0})` "," :math:`\mathrm{A4}(\mathrm{0,5}\mathrm{,0})`" Material properties ----------------------- A to O models ~~~~~~~~~~~~~~~~~~~~~~ The material has an isotropic elastic behavior: Young's module: :math:`E=\mathrm{200000.MPa}` Poisson's ratio: :math:`\nu \mathrm{=}0.` Density: :math:`\rho \mathrm{=}\mathrm{1000.Kg}\mathrm{/}{m}^{3}` For N modeling, the material is GLRC_DAMAGE with equivalent elastic properties (zero steel modulus). ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ ~~~~~~~~~~~~~~~~~~~~~~~~~~~~ Boundary conditions and loads ------------------------------------- A and B models ~~~~~~~~~~~~~~~~~~~~~~ Edge :math:`A1A4` is embedded. The plate is :math:`\mathrm{0,8}m` thick. The plate is offset from :math:`e=\mathrm{0,4}m`. A :math:`\mathit{Fz}=–1000\text{N}` nodal force is applied to the :math:`A1A2` edge. D, E, F, G, H, H, H, H, I, I, I, J, K, M, and N modeling ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ Edge :math:`A1A4` is embedded. The plate is :math:`\mathrm{0,8}m` thick. The plate is offset from :math:`e=\mathrm{0,4}m`. A distributed transverse nodal force :math:`{F}_{z}=–1000N/m` is applied to the edge :math:`A2A3` and a distributed nodal traction force :math:`{F}_{x}=4000N/m` is applied to the same edge :math:`A2A3`. O modeling ~~~~~~~~~~~~~~~ Edge :math:`A1A4` is embedded. The plate is :math:`\mathrm{0,8}m` thick. The plate is offset from :math:`e=\mathrm{0,4}m`. A :math:`\mathit{Fz}=–1000\text{N}` nodal force is applied to the :math:`A1A2` edge.