Page 406 - Biaxial Multiaxial Fatigue and Fracture
P. 406

390                          M. FILIPPINI ET AL.

             For the three materials considered in this paper, the values of the constants used to define the
             material function K are shown in Table 1. The interpolating curves are shown in Fig. 3.




                                                                          SAE 1045 steel






                                                              1%   OW   00,   0015  om  0  s  om  om
                  EIIechresheersnaur[mmfmrn]   Ekbve shear strain [mm4nrn]   EIIechre shears(rain [mmhn]
                       (4                      (b)                     (c)
             Fig.  3.  Values  of  the  material   function^  for  Inconel 718  alloy  (a),  Mild  Steel  (b)  and
             SAJ?  1045 steel (c)


             Table 1. Constants used in the definition of the material fimction K
              Material     CI         A,          BK          C,         DK
              INCONEL 71 8   1 655     1.06.10-5   -2.35      1 .26.102   -1.46
              MILD STEEL   1.655      3.36.10'    -9.49.10'   9.75.104    -1.44
              SAE 1045     1.667       1.05.10'   -8.29.1 0-'   8.851O4   -1.44


             With the above development the procedure for the fatigue life prediction under fully reversed
             loading  is summarised  in three  steps;  first calculate  y&@ through  Eqs (9) and (lo),  second
             evaluate an equivalent axial strain  cwp = KY~,~ with  K given by Eq. (16) and third, introduce
             cwP in the Manson-Cofin relationship in the place of E,  and solve for the number of loading
             cycles.  It is noticed that the experimental data upon which the above procedure is based are
             limited in:  1)  the cyclic stress-strain  curve, which serves to establish the material function  K
             and,  2)  in the Manson-Coffin  curve, which allows estimating the number of load cycles to
             crack initiation.


             Mean strain effects

             For predicting the fatigue life in the intermediate life range up to the high-cycle fatigue regime,
             the new criterion has to take  into account the effect of a superimposed mean strain. If for a
             given multiaxial loading the mean strains are not zero, the strain cycles may be partitioned into
             their  mean  and  alternating  components,  so  that  two effective shear strains,  y&#,  ye'errm are
             calculated.  In  order  to  take  into  account  the  effect  of mean  strain  components,  a general
             formula,  obtained as a second order power expansion in terms of the effective shear strains,
             may be tentatively proposed:
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