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             to the difference in tack weld positions. In the simulation it was found that the positions of the first few
             tacks were decisive for the general deformation mode as the influence of the succeeding tack welds is
             insufficient to cause large alterations once the deformation mode has been initiated.
             The  computation  time  used  for  each model  is  120 hrs  on a  HP  55000 workstation,  including  the
             thermal  and  the  mechanical  simulation  for  both  fillets.  Holding  the  capability  of  the  workstation
             against the standards of today, a considerable reduction in computation time is realistic.

             4  THE LOCAL/GLOBAL TEMPLATE

             The  efficiency  obtained  by  graded  elements and  moving  mesh  algorithms  is  inadequate  when  the
             objective is simulation of welding in large structures such as ship sections. The essential  problem of
             dynamic  mesh  refinement  is  that  the  structure  should  be  discretised  at  least  to  the  level  where
              geometry, stresses and deformation can be represented with adequate accuracy at ambient temperature.
              More precisely, unwelded regions should be discretised to represent geometry and restraints properly.
             The welded regions should also hold the stresses and deformations accumulated in welding and, hence,
              further discretisation  is  required.  As  a  result  the  number  of  DOFs necessary  to  represent  a  given
              structure  at  the  coarsest  refinement  level  increases  very  quickly  beyond  what  is  computationally
              attainable when the size of the structure grows.

              In the present context a template is defined by a bundle of techniques for welding simulation in large
              structures. Generally, templates are based on hrther approximations compared to the full simulation.
              The essence is how these approximations are chosen and how they affect the accuracy of the prediction.
              To predict the distortions of an assembly rather extensive requirements are imposed on the template to
              be developed.  In  addition  to the  factors essential  to the  local modelling,  it is necessary  further  to
              account for the stiffness of the surrounding structure and to inched the stress and deformation caused
              by preceding welding on the assembly. These factors are central to a template capable of predicting the
              effect of different welding  sequences. A template denoted the LocaVGlobal template or just the UG
              template has been developed for the purpose in Andersen (2000,2001b).
              The subassembly chosen for analysis is a part of a transverse web frame in a container vessel and is
              particularly interesting as it has caused significant problems in production due to welding deformations.
              The global model of the subassembly is shown in Figure 4(a) and is composed of linear elastic shell
              elements.

              As the global shell model is not suited for welding simulation, each weld line is represented by a local
              solid model, equivalent to the dynamically meshed models shown previously. The idea behind the L/G
              template is to link the local models to the global and thus enable a proper representation  of both the
              boundary  conditions  for  the  local  models  and  the  accumulated  distortions  in  the  global  model.
              Moreover, it is exploited that at large part of the structure can be modelled by substructures due to its
              linear elastic response at low temperatures. The steps in the L/G template may be described briefly as
              follows:  The global  model  is substructured  and included  as boundary  conditions for  the first  local
              model as illustrated by Figure 4@). The welding response is calculated and the deformations are used
              to update the distortions of the global shell model as shown in Figure 4(c). The deformed global model
              is  used  to  establish  the  boundary  conditions  in  the  modelling  of  the  next  weld  line  so that  the
              interaction between  weld  lines is included in the modelling  and the effect of welding sequence can
              therefore  be  accounted  for. The  specific  calculation  steps  of the  template  and  issues  such  as  the
              updating of geometry, the combination of shells and solids, the extraction of boundary conditions and
              substructuring are addresses in detail in Andersen (2000,2001 b).
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