Page 72 - Biaxial Multiaxial Fatigue and Fracture
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Multiaxial Fatigue Assessment of Welded Structures by Local Approach   51

          The analysis of  the influence of  the residual stresses level on the fatigue strength of  butt
        welded joints  subjected to  alternate cyclic load has been  carried out  by  the proposed local
        approach. These calculations were done with the mean measured geometry of the welds.
          Figure  14 shows the influence of  the residual stresses on  the fatigue strength of  the butt
        welds.  The  different  curves  are  examined  from  the  left  side  to  the  right  side,  Le.  in  the
        increasing order of the fatigue strength.

















                              experimental results   -nil   SIG-res
                           -maximis&   SIG-res     -minimum   SIG-res  measured
                           --maximum   SIG-res  measured   -SIG-res   shot peening
                          1   1  !  l!l!l   1   I  I  lI!/l/   i   I   I  i  I  Ill!   I   I  l  l
                  1 E+4         1 E+5         1 E+6         1 E+7        1 E+8
                                          Number of cycles


         Fig. 14. Influence of residual stresses on predicted alternate tensile fatigue strength (R = -1)
                                       of butt welds


          The lowest S-N curve has been  obtained with the maximised residual stresses, it is to say
            =
                  =
        qOng otrans 140 MPa. The second S-N  curve was  plotted by  considering the  maximum
        measured values of residual stresses which correspond to: qOng = 70 MPa and om,,, = 60 MPa.
          These two assessed S-N curves are found to be quite conservative. The minimum measured
        residual  stresses  (along  =  15 MPa  and  om,,  = -20  ma) lead  approximately  to  the  same
        simulation results  as  the  calculation carried  out  accounting for  no  residual  stresses. These
        assumptions seem to be a little optimistic regarding to the experimental S-N curve. The last S-
        N curve was obtained assuming that residual stresses are compressive and reach the maximum
        absolute value, i.e. along = otran, = -100 MPa. This assumption brings quite non conservative
        predictions. It is similar in fact to the effect of pre-stressed shot peening.
          As a conclusion, there is clearly a very considerable effect of residual stresses on the fatigue
        strength  of  aluminium  alloy  welded  joints.  The  influence  is  beneficial  in  the  case  of
        compressive residual stresses and detrimental in the other case. A pre-stress shot peening type
        finishing treatment makes strongly increase the fatigue strength of welded joints.
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