Page 224 - Biaxial Multiaxial Fatigue and Fracture
P. 224

208                         A.  VARVANI-FARA HANI


             uniaxial   loading   condition   is   the   well-known   Ramberg-Osgood   relation
                       (  /  *yn*
             (ql =ol1/E+ crII K   ),  which  is  commonly  used  to present  cyclic uniaxial  stress-strain
             curve.
               The  range  of  maximum  shear  stress  and  the  corresponding  normal  stress  range  are
             calculated from the largest stress Mohr’s circle during the first reversal (at the angle 81) and the
             second reversal (at the angle 82) of a cycle as:










             where csl I.  ~22 and 033 are the principal stress values calculated using Eq (3).
             Similarly, the range of maximum shear strain and the corresponding normal strain range on the
             critical plane at which Mohr’s circles are the largest during the first reversal (at the angIe 81)
             and the second reversal (at the angle 82) of a cycle are calculated as:










             where E~I, ~22, and  ~33 are the principal strain values (&11>~22>  ~33) which are calculated using
             Eq (4).


             Proposed fatigue parameter

             In this paper for the convenience of presentation, first the proposed parameter and its capability
             to take into account the effects of out-of-phase strain hardening and mean stress are discussed
             for the load histories with frequency ratio of  -1   [17,23,24] and then the damage model is
             extended for other ratios of 0(=2 and a=3.
                                                                 (2)
                                                                       obtained  from  the
                The  range  of  maximum  shear  stress   and  shear strain  A  ib~
              largest stress and strain Mohr’s circles at angles el and 82 during a cycle and the corresponding
              normal stress range Ao,, and the normal strain range A&,, on that plane are the components of
              the proposed parameter in the present paper.
                Multiaxial fatigue energy-based models have been  long discussed in  terms of  normal and
              shear energy weights. In  Garud’s approach [8] he found that  an  empirical weighting factor
              equal  to  C=0.5  in  the  shear  energy part  of  his  model  (Eq  10) gave  a  good correlation  of
              multiaxial  fatigue results for  1% Cr Mo V  steel for both in-phase and out-of-phase loading
             conditions:
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