Page 101 - Biaxial Multiaxial Fatigue and Fracture
P. 101

86                        L. SUSMEL AND N. PETRONE

            an extension of the Mandell semi-log linear equation and, finally, the criterion due to Smith &
            Pascoe  is  capable  of  modelling  three  different  fatigue  damage  mechanisms:  the  rectilinear
            cracking, the shear deformation along the fibre plane and the combined rectilinear cracking and
            matrix shear deformation.
               These approaches are clearly developed for composites, but when the degree of  anisotropy is
            not so high, different methods are again suggested. The criterion proposed by Lin et al.  [28, 291
             can be mentioned as a valid criterion to apply in this kind of situations. This method is based on an
             original employment of the strain vector.
               Aim of the present paper is the validation of the Susmel and Lazzarin's  criterion on a widely
             used  industrial  aluminium  alloy  showing  a  slight  degree  of  anisotropy  to  confirm  if  the
             employment of specific models for anisotropic materials can be avoided when  subjected to  in-
             phase and out-of-phase multiaxial loadings.


             FUNDAMENTALS OF THE MODIFIED WOHLER CURVES METHOD

             The theoretical frame of  the Susmel and  Lazzarin's  criterion  is based on a combined use  of a
             modified Wohler diagram and the initiation plane concept [21].
               The theory of deformation in single crystal has been employed to give a physical interpretation
             of the fatigue damage: in a polycrystal this depends on the maximum shear stress amplitude, tar
             (determined by the minimum circumscribed circle concept [30]) and on the maximum stress u",,,,~~
             normal to the plane of maximum shear stress amplitude (initiation plane) [21].



                                                       A




                                                                             ZA,Ref(P1)
                                                                             ' ZA,Ref (pi)
                                                                 J
                                                            increasing p     1
                                                                             !
                                                                             I




              Fig. 1.  Frames of reference and definition of   Fig. 2.  Modified Wohler diagram.
              the polar co-ordinates I#  and 9.


               Consider a cylindrical specimen subjected to a multiaxial cyclic load (Figure 1). With reference
             to a maximum shear stress amplitude plane, located by $* and 8* angles, it is possible to define for
             this plane the stress ratio p as follows:
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