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60                          R LABESSEJIED ET AL.

            plastic stress response model is also applied for that purpose in the case where the stress levels
            exceed the material yield  stress.  A multiaxial critical plane criterion and the linear Miner's
            damage  summation  technique  are  employed  for  assessing  lifetimes.  The  ratio  between
            predicted results and largely scattered experimental ones are found to be less than 4.
               On the  basis  of  experimental  results  and  lifetimes calculated  by  the  presented  fatigue
            assessment procedure, the following items may be pointed out:
               -  All the geometrical peculiarities of the welded assembly must be considered including
            angular and axial defects generated by the welding. The influence of these parameters is the
            most pronounced one with respect to the fatigue behaviour of the weld,
               -   Fatigue predictions require to take account for S-N curves modifications involved by
            metallurgical thermally dependent changes,
               -   The residual stresses remaining in the vicinity of  the weld  should be considered and
            superimposed to the actual operational stress states existing within the weld,
               -  The cyclic plasticity correction has to be run on when stress states exceed largely the
            initial material yield stress,
               -  A multiaxial fatigue damage model as a fatigue stress-based criterion has to be used in
            order to account for multiaxial stress states generated within the weld.
               The fatigue assessment procedure proposed in this work  is modular and opened so that it
            may  include any  multiaxial  fatigue  criterion, attended  that  the  ductility level  of  materials
             reveals more or less suitability of multiaxial fatigue concepts [13].


            REFERENCES

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