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I84                          T LAGODA ETAL.

              distribution  (cruciform specimens and  thin-walled cylinders), the criterion  of  the maximum
              normal strain energy in the critical plane, including the positive energy parameter under tension
              and the negative energy parameter under torsion was a suitable quantity for describing the test
              results of  lOHNAP and SUS304 steels. All  the analyses were based on  a parameter of strain
              energy density which has been presented in details in [IO,  11 1.
                In  [12 - 141 the mesoscopic approach to  fatigue life estimation was proposed. The papers
              concern  uniaxial  tension-compression  with  torsion  in  cylindrical  solid  specimens  made  of
              35NCD16 steel, and the proposed approach is based on the concepts of Orowan [15], Papado-
              pulos [16] and Dang-Vang [17]. In this paper the authors will reanalyse the former test results
              of 35NCD16 steel and assess if the proposed energy parameter can correlate these experimental
              data.
                As it results from the previous papers [4 - 91,  this parameter seems to be very efficient for
              correlation of the experimental data obtained for steels IOHNAP, 18G2A, SUS304 and 12010.3
              as well as cast irons GGG40 and GGG60.
              FATIGUE TESTS

              The tested 35NCDl6 steel has the following chemical composition: Si - 0.37%,  Mn - 0.39%,
              P-O.O1%,S-<o.oO3%,Ni-3.81%,Cr-1.7%,Mo-O.28%,C-O.364%, therestFe. Young’s
              modulus is E = 205 GPa and Poisson’s ratio is v = 0.3, the yield point is R0.2 = 930 MPa, ten-
              sile strength R,  = 1070 MPa, contraction Z = 20.7 %.  Cylindrical specimens were tested under
              constant and variable-amplitude loading. In the case of constant amplitude loading, tests were
              performed  under  tension-compression  and  pure  torsion.  In  the  case  of  variable-amplitude
              loading, tests were performed under tension-compression, combined proportional tension with
              torsion for the ratio of shear and normal stress T(t)/b(t) = 0.5 and pure torsion [I2 - 141. All the
              fatigue tests were realized under controlled force and twisting moment. Basing on the tests un-
              der constant amplitude uniaxial tension-compression it was possible to determine the regres-
              sion models of the fatigue characteristic according to [18]

                                         logN,  =A-m.logo,                        (1)

                Parameters of the determined Wohler curve are as follows: A = 21.07, m = 5.86, the fatigue
              limit oaf= 450 MPa, and the corresponding number of cycles No = 3.328 . lo5. The results of
              fatigue tests under torsion were approximated by a similar regression model:


                                        logN, =A, -m,-log.c,                      (2)
              where  A, = 44.51,  mt = 15.08, the  fatigue  limit  z,f  = 330 MPa,  and  the  corresponding cycle
              number Not = 3.395  lo6.
                It is important to note that the numbers of cycles No and Not for the analysed material differ
              by one order. The results for variable-amplitude loading are shown in Table 1. In the tests the
              standard course CARLOS - lateral - Car Loading Sequence with 95180 cycles in a block was
              used. The cycles with low amplitudes were eliminated so as to obtain the block of fl type (with
              a high reduction of low amplitudes) and f2 type (with a low reduction of low amplitudes). The
              loading of CARLOS type is a typical loading used in tests of car elements realized in France
              and Germany (specially LBF Darmstadt). Its course is characterised by a high irregularity coef-
              ficient.
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