Page 213 - Biaxial Multiaxial Fatigue and Fracture
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Estimation of the Fatigue Life of High Strength Steel  Under ...   197


           The calculations were made for coefficients a =1, 0.81, 0.64. The best agreement with the ex-
           perimental results is obtained when a = 0.81. In such a case we obtain the mean error  18%.
           Moreover,  assuming lower amplitudes leads to incomct estimation of  the fatigue life and a
           greater error in the life calculation. In Fig.6 the calculated and experimental fatigue lives for
           uniaxial tension-compression are compared. It can be seen that the calculation results for a =
           0.81 are included in the scatter band with a factor 2, and for 0.64 2 a 5  1 in the scatter band
           with a factor 3.
                   t























                                                            0 PM(a=l)
                                                                  PM(a=O.25)
                                                            0 SK(a=l)
                                                            0     SK(a=0.81)
                    I/                                      0     SK(~=O.M)
                   l///                                   Nb,exp  [blocks]





               10   1  Y    I    I   I  l  l  1  1  1  ~  I   I   I   I l l l l
                   10                        100                       1000


            Fig.6. Comparison of the calculated fatigue life with experimental data for uniaxial variable
                                   amplitude tension-compression

             Basing on the previous calculations, we performed further calculations for all the tests real-
           ized under variable amplitude loading. The calculation results for damage accumulation ac-
           cording to the Serensen-Kogayev linear hypothesis, including the energy parameter amplitudes
           81%  of  the fatigue limit expressed in energy are shown in Table 4. These calculated fatigue
           lives are compared with the experimental lives in Fig.7. In the case of variable amplitude tor-
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