Page 470 - Biaxial Multiaxial Fatigue and Fracture
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454                        M. WEICK AND 1 AKTAA

            the microstructural barriers have a noticeably smaller influence on the crack growth rate at high
            loading levels.
            While the crack propagation in the short cracks regime can be described using the methods of
            the elastic-plastic fracture mechanics (EPFM) [9], approaches of the so-called microstructural
            fracture mechanics (MFM) are needed for the regime of micro cracks [lo]. In the following, a
            model for micro and  short crack propagation will be presented, which was developed on the
            base of  the model by McDowell and Bennet [8] and applied to our multiaxial tests for lifetime
            prediction.


            Microcrack propagation modelling. TO describe the  average crack  growth  rate  in  the  short
            cracks regime, the following elastic-plastic fracture mechanics approach proposed by Hoshide
            and Socie for mixed mode loading [9] is used





            where the crack  growth rate  df~ correlates with the range of  J-integral  AJ. Cj and  m,are
            material and temperature dependent parametexdl  can be calculated in terms of an elastic and
            a plastic part.
                                        AJ=AJ,, +NP,                             (9)

            For mixed mode loading the elastic part is based on the normal stress ranges Aon and the shear
            stress ranges AT  on the plane, where the crack is assumed to nucleate and propagate. This is
            usually  the  plane  of  maximum  shear  strains  18,101.  Neglecting  the  influence  of  plastic
            deformation on the effective crack length the elastic part can be phrased as [9]:





             For the plastic part is given by the formula derived by Hoshide and Socie [9] generalised here
             for the case of multiaxial non-proportional cyclic loading:

                                   AJpl =T(h,n,v)A~; Aoq a                       (1 1)

                                             1-n
                                  with  7 =s(h)-+t,(h)xn
                                             J;;

                                        and  h=-  AT
                                               Acll
             Aoq  denotes  the  von  Mises  equivalent  stress  range.  Its  calculation  is  analogous  to  the
             determination of  A€;.  The dimensionless function 7  takes into account the increased plastic
             deformation  in  front  of  the  crack  tip  in  comparison  to  the  global plastic  deformation. The
             function s(h) takes  into account  the mode mixity of  the crack  loading and  decreases as h
             increases. For pure Mode I loading ( h = 0) s =3.85. For the pure Mode I1 (h -+ -)  s=1,45 [9].
             For a mixed mode loading we propose an interpolation in the following form:
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