B modeling ============== Characteristics of modeling ----------------------------------- .. image:: images/Object_16.svg :width: 624 :height: 206 .. _RefImage_Object_16.svg: Characteristics of the mesh ---------------------------- Number of knots: 43 Number of meshes and type: 10 QUAD4 Tested values --------------- +------------------------------------------------------------------------------------+------------------+-----------+-------------+---------+----------------+ | |**Identification**|**Moments**|**Reference**|**Aster**|**% difference**| + .. image:: images/Object_17.svg + + + + + + | :width: 624 | | | | | | + :height: 206 + + + + + + | | | | | | | + + + + + + + | | | | | | | +------------------------------------------------------------------------------------+------------------+-----------+-------------+---------+----------------+ |5 |ETA_PILOTAGE |5 |1.0 |1.0837 |8.37 | +------------------------------------------------------------------------------------+------------------+-----------+-------------+---------+----------------+ |25 |ETA_PILOTAGE |25 |1.0 |1.0998 |9.98 | +------------------------------------------------------------------------------------+------------------+-----------+-------------+---------+----------------+ notes --------- In this analysis, an imposed displacement type resolution technique ('DDL_IMPO') is used to find the solution. This method provides for each imposed displacement value, a load multiplier coefficient ('ETA_PILOTAGE'). The value of the load imposed in 'AFFE_CHAR_MECA' is equal to the limit pressure, therefore the reference value of the parameter 'ETA_PILOTAGE' is equal to 1. The calculations were stopped when the value of parameter ETA_PILOTAGE stabilized. The reference being taken in relation to the beam solution with 50 elements, we observe an improvement in the DKT QUAD4 results when the mesh is refined.