Page 402 - Biaxial Multiaxial Fatigue and Fracture
P. 402

386                          M. FILIPPINI ET AL.





                                                                                   (3)
                            +6 (   + A&:  + A&;)]  ' maximized with respect to rime


             The terns A€, , Asq have to be calculated as strain differences between two generic instants tl
             and r2, e.g.  A&,  = E,  (1, ) - E, (r, ) , AE~ sXy (t, ) - cXy (I, ) etc. The equivalent strain range Asq ,
                                           =
             Eq. (3),  is calculated by varying tl  and rz such as to obtain its maximum value. This criterion
             produces  a  lower  equivalent  strain  for  the  out-of-phase  than  for  the  in-phase  loading,
             predicting an increase of the fatigue life,  in contradiction with the experimental results. The
             application of this criterion may lead to unconservative predictions, as shown by Tipton and
             Nelson [14].


             Criterion of Sonsino and Grubisic

             The criterion of Sonsino and Grubisic [I31 assumes that the fatigue damage is caused by the
             interaction of shear strains acting on different elementary material planes, called interference
             planes. An interference plane is completely defined by the spherical coordinates, 29  and  p, of
             its unit normal vector n (Fig. 1).











                                     YAF"





             Fig.  1. Definition of interference plane: dA represents the free material surface; n is the unit
             normal vector of the generic interference plane
                According to Sonsino and Gtubisic [13],  in order to simplify the calculation procedure the
             shear  strain  is  calculated only  on  the  interference planes  defined by  a  constant  value  of
              p = 90°, corresponding to the planes normal to the surface. The shear strain on these planes
             can be obtained at each time in the following way:




             The shear amplitudes yo (e) are calculated for each plane:
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