Page 81 - Biaxial Multiaxial Fatigue and Fracture
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66                        N  ISOBE AND S.  SAKURAI























                                           Base metal *Weld     metal
                               Fig. 3. Microstructure of welded specimen.


              A servo-hydraulic, axial-torsional machine with an axial load capacity of 245 kN and torque
            capacity of  2.8  kN-m, was used  for  the  strain-controlled multiaxial  fatigue tests.  An  axial
            extensometer with  conical-point quartz extension  rods  that  could independently control and
            measure both the axial and shear strain was used. Its gauge was 25 mm long. Strain-controlled
            multiaxial fatigue tests with combined axial and torsional loading were carried out in several
            von  Mises’  strain  ranges (Ah). Strain  waves  were  in-phase  with  fully  reversed  triangular
            waves at a strain rate of O.l%/s. The principal strain ratios I$, which is the ratio of the minimum
            strain to the maximum principal strain (@=&&I) [4],  employed were -1 (pure torsion), -0.64
            (combined,  E = ,&  ),  and  -0.50  (purely axial). The  strain  measurement point in  the axially
            welded specimen was at a position 90 degrees in the circumferential direction from the weld
            line.
              Specimens were heated by induction heating and tested at 700°C. The failure of a specimen
            was defined as the number of  cycles producing a 25%  reduction in the stress range from the
            saturated value.  Testing was occasionally interrupted to obtain cellulose-acetate film replicas
            and thus observe the growth of fatigue cracks.


            RESULTS AND DISCUSSION
            Results of Low-cycle Fatigue  Testing

            Figure 4 shows the low-cycle fatigue life of base metal and welded specimens. Results for a
            round  bar  specimen with  a  diameter  of  8  mm  are  also  plotted  in  the  figure. The  uniaxial
            fatigue-test result was almost the same as for the round bar [SI, so the failure life of the hollow
            cylindrical specimen was roughly equivalent to that of a round bar. The solid line in the figure
            indicates the fatigue curve for the uniaxial condition. Fatigue lives in the torsional fatigue test
            were 2 to 3 times longer than in the uniaxial test so that the Mises’ equivalent strain was not an
            appropriate parameter for  assessing the fatigue life of  Hastelloy-X. Fatigue lives of  welded
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