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A Multiaxial Fatigue Life Criterion for Non-Symmetrical and Non-Proportional Elasto-Plastic ...   389







           For an elastic-plastic  axial strain, E,  = E:  + E!',  one has:




           where  vel and  vp, are respectively the elastic and plastic Poisson's  ratio. This would imply
           that a material model should be used to separate the elastic and plastic strains once the total
           strain is given. Instead, a simplified approach will be adopted here. In order to determine the
           material function  K in  the general case, it is found useful to introduce an effective Poisson
           ratio  v , defined in the elastic-plastic range as following:





           where E  is the Young's  modulus and  E,,   is the secant modulus. With this definition
           one always can write  E,. = E, = -vex. The equivalent stress amplitude, beq, may be determined
           by  setting the equivalent strain amplitude, Eq. (2), in the uniaxial cyclic stress-strain  curve,
           that is described in mathematical form by the Ramberg-Osgood  equation:






             For  numerically determining the  value of  the material function  K  for each  value  of  the
           effective shear strain  yeri, Eq. (lo), a convergent iterative procedure has to be employed. First,
           an  initial  guess  value of  v = vel is set, by  which the transverse strains may be evaluated as
           E, = E, = -vE~, for a given value of longitudinal strain. Then, the equivalent strain is calculated
           and, by employing the cyclic stress-strain  curve, Eq. (15),  the equivalent stress and the secant
           modulus  E,? are determined. Finally, the new estimated value of the effective Poisson ratio is
           calculated, Eq.  (14). The procedure is repeated, by employing the calculated value as initial
           guess, until the difference between the guess and the obtained value is sufficiently small.
             Values of  K calculated for a range of effective shear strain amplitudes are shown as hollow
           circles in Fig. 3-a,  b and c, for the Inconel 718 alloy, the Mild Steel and the SAE 1045 steel,
           respectively. Until the material response is elastic, a constant value of  K, i.e.  K,, , Eq. (13), is
           achieved while in the plastic region  K  is a decreasing function of the strain.
             In order to speed up the evaluation of the parameter  K when predicting the fatigue life, the
           following interpolating expression has been adopted for defining the material function K:
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