Benchmark solution ===================== Calculation method ----------------- The reference results are obtained by another Aster calculation. Reference quantities and results ----------------------------------- The displacements, the reaction forces at different nodes of the mesh are evaluated, as well as the local stress values for different cells. These values are obtained for three moments :math:`t`: formula formula :math:`t=1`, formula formula, formula :math:`t=2`, formula :math:`t=10`. +---------------------------------------------------------------------------+------------------+-------------------+---------+ |**Identification** |**Reference type**|**Reference value** | + + +-------------------+---------+ | | |Instant |Value | +---------------------------------------------------------------------------+------------------+-------------------+---------+ |Formula point :math:`\mathrm{N05}` Formula travel :math:`\mathrm{DZ}` |'AUTRE_ASTER' |1 |-7.06E-01| + + +-------------------+---------+ | | |2 |-1.41E+00| + + +-------------------+---------+ | | |10 |-6.50E+00| +---------------------------------------------------------------------------+------------------+-------------------+---------+ |Formula point :math:`\mathrm{N06}` Formula travel :math:`\mathrm{DZ}` |'AUTRE_ASTER' |1 |-4.81E-01| + + +-------------------+---------+ | | |2 |-9.63E-01| + + +-------------------+---------+ | | |10 |-4.86E+00| +---------------------------------------------------------------------------+------------------+-------------------+---------+ |Formula point :math:`\mathrm{N01}` Force Nodale formula :math:`\mathrm{DX}`|'AUTRE_ASTER' |1 |-6.35E+09| + + +-------------------+---------+ | | |2 |-1.27E+10| + + +-------------------+---------+ | | |10 |-6.33E+10| +---------------------------------------------------------------------------+------------------+-------------------+---------+ |Formula point :math:`\mathrm{N01}` Force Nodale formula :math:`\mathrm{DY}`|'AUTRE_ASTER' |1 |-6.07E+09| + + +-------------------+---------+ | | |2 |-1.21E+10| + + +-------------------+---------+ | | |10 |-6.12E+10| +---------------------------------------------------------------------------+------------------+-------------------+---------+ |Formula point :math:`\mathrm{N01}` Force Nodale formula :math:`\mathrm{DZ}`|'AUTRE_ASTER' |1 |5.72E+08 | + + +-------------------+---------+ | | |2 |1.14E+09 | + + +-------------------+---------+ | | |10 |4.18E+09 | +---------------------------------------------------------------------------+------------------+-------------------+---------+ Constraints in the mesh that models the membrane_grid at Gauss point number 1. .. csv-table:: "", "Sigxx for rebar meshes oriented according to :math:`\mathrm{OX}` ", "Sigxx for rebar meshes oriented according to :math:`\mathrm{OY}`" "Instant", "Reference Value", "Reference Value" "1", "2.94E+10", "2.00E+11" "2", "5.88E+10", "2.20E+11" "10", "2.15E+11", "3.80E+11" Cumulative plasticity in the mesh that models the membrane_grid at the Gauss point number 1. .. csv-table:: "", "Internal variables V1 for rebar meshes oriented according to :math:`\mathrm{ox}` ", "Internal variables v1 for rebar meshes oriented according to :math:`\mathrm{oY}`" "Instant", "Reference Value", "Reference Value" "2", "", "9.00E-01" "10", "6.73E-01", "4.06E+04" Stresses in the hexa8 concrete mesh at the Gauss point number 1: mesh :math:`\mathit{BMA1}` +-------+---------------------------------+--------+---------+--------+ | |Constraints: Hexa8-point mesh (1) | +-------+---------------------------------+--------+---------+--------+ |Instant|Reference value | + +---------------------------------+--------+---------+--------+ | |SIXX |SIYY |SIZZ |SIXZ | +-------+---------------------------------+--------+---------+--------+ |1 |2.41E+10 |2.41E+10|-3.52E+09|3.96E+08| +-------+---------------------------------+--------+---------+--------+ |2 |4.82E+10 |4.82E+10|-7.04E+09|7.91E+08| +-------+---------------------------------+--------+---------+--------+ |10 |2.44E+11 |2.44E+11|-2.57E+10|2.89E+09| +-------+---------------------------------+--------+---------+--------+