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Eualuation of Fatigue of Fillet  Welded Joints in  Vehicle Components  Under Multiaxial Service Loads  25



















          Fig. 2. Load configuration on the test rig   Fig. 3. Load sequences, 1 block


          LIFE CALCULATION IN ACCORDANCE WITH THE HOT SPOT STRESS APPROACH


          Finite Element Modelling

          Niemi [8, 91 presents a series of variants for realising the joint between two welded parts in a
          finite element  (FE) model  but  does  not  give a clear recommendation. Figure 4  [8] shows
          various ways to model cover plate endings.
                                 ?I  Is!L-                          Rigid bar
                                               ell elements
                   :  I  ,  ?
              a) double shells connected   b) double shells connected   c) double shells connected
              bv a vertical shell   by a vertical shell and   by rigid bars
                                    inclined shell elements
                         Rigid bar             Solid element


              d)  Elfis3- single shells with offset,   e) solid element modelling
              connected by rigid bars

          Fig. 4. Various modelling approaches for cover plate endings [8]


            To take advantage of the experience from a previous investigation [7] on the applicability
          of  the hot  spot stress approach, simple 4-node shell elements have been  used  to model the
          tube,  8-node volume elements have been  used  for  the  forged  arms. Both  meshes  are  tied
          together  with  constraint  equations.  The  weld  itself  is  modelled  by  increasing  the  shell
          element’s thickness. In accordance with Niemi’s suggestions, the element length has been set
          to 2.5  mm  (=0.4’h, where h  is the shell thickness). Figure 5 shows the finite element mesh
          used together with the load configuration.
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