Page 304 - Biaxial Multiaxial Fatigue and Fracture
P. 304

288                       T FUKUDA AND H. MISITAMI
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                          Fig. 1. Principal stress and principal shear stress in torsion


             the relation between both fatigue limits of bending and torsion becomes  cJ,=Z,   in torsion.
            Then, the fatigue limit ratio of torsional fatigue to bending fatigue is obtained by the following
            equation:




             This  equation  corresponds to  the  maximum  tensile stress  criterion, which  is  related  to  the
             macroscopic criterion of yielding ( Zs/(7,=  1).
               A defective material, which contains sharp defects like gray cast iron, mostly follows the
             Eq.(l).  However, in  the  artificial defects of  small circular  holes or  nodular cast irons,  it  is
             necessary to consider the stress concentration of a circular hole. Since the maximum stress due
             to the stress concentration of a circular hole is equal to approximately 3 0  in bending and 4 t
             in torsion ( (J   Z   the ratio of fatigue limits is reduced to the following equation:



             Nisitani  presented some experimental results for an  annealed rolled carbon steel bar  with  a
             small hole [13]. In the case of a single hole specimen,  Z J (J,was  equal to approximately 0.75,
             whereas  it was  equal to  about 0.9  in  the case  of  the  connected hole  specimen, It  was also
             shown  that   TI,,,'^^ was  equal to approximately 0.9  (not 0.75)  for  a nodular cast  iron. This
             means that spheroidal graphite is not always independently distributed and is regarded as a
             kind of connected hole.
               As is mentioned above, the fatigue limit of a defective material including cast iron is mainly
             controlled by the maximum tensile stress, and the value of  fatigue limit ratio Z J 0,  follows
             Eq.(3),  depending on the type or distribution of defects, etc.

                                        Z,/(7,=0.75  - 1                          (3)


             In  the  case  where  the  fatigue  limit  is  controlled  by  the  maximum  shear  stress  only
             (non-defective material)

             If the cracks once initiated do not stop propagating, the fatigue limit is determined by whether
             a crack initiates or not. According to  the successive observations by  Nisitani, age-hardened
             Al-alloy corresponds to this case [15]. In this material a crack initiates in a fairly small region
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