Page 249 - Biaxial Multiaxial Fatigue and Fracture
P. 249

Fatigue Analysis of Muitiaxially Loaded Components with the FE-Pospmcessor FEMFAT-MAX   233

          A NEW METHOD TO TAKE INTO ACCOUNT PHASE SHIFTS

          Integral methods have a disadvantage: They would deliver different results also for uniaxial
          bending and torsional loading. But the numerical results are good and should not be affected.
          Therefore we propose to change the S/N-curve in dependence of a multiaxiality parameter. This
          parameter could be simply the phase shift. But in practice this is not a good choice, because a
          phase shift can be defined only for monofrequentic signals. It should be possible to define such
          a parameter which can be applied for stochastic signals too.  A solution has been implemented
          in FEMFAT, which was proposed by Chu et a1 [I 11. The stress state is considered for each time
          step in  the stress space (Fig.  14). The ratio of  the axis lengths of  the inertia ellipsoid in the
          stress space can be used as degree of multiaxiality d~. It is a value in the range from 0 to 1. For
          the combined  load case with 90 degree phase shift, as it can be seen  in  Fig.  10, we would
          obtain a value of  dfi0.58 or, if we scale the shear stress by a damage equivalent factor of 6
          (= ratio  tensionkhear  fatigue limit), a  value of  dpl, respectively. For  all  other  load cases
          (uniaxial and combined without phase shift) we will get a value of dp0. Now the local fatigue
          limit can be modified by the approximate formula





          SM denotes the  sensitivity of  multiaxiality, which  is  a material parameter. Using a value of
          Sp0,26 for the considered tempering steel, a good result is obtained for the combined load
          case with phase shift for the fatigue limit (see Fig. 15). An  additional minor correction of  the
          cycle limit of  endurance could lead to an even better result for the finite life domain.






                                                             , ... ..
                                                            . . .. .::
                                                             .*
                                                            . .. ..:  ;, t.;  .   -- 0
                                                                  -  **
                                                               ;::*,
                                                             ...*. .
                                                             . ..*.>,  +:*;   *


                         Almost uniaxial                   Strongly multiaxial
                        stress-distribution                stress-distribution


          Fig. 14: Local stress state history
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