Page 450 - Biaxial Multiaxial Fatigue and Fracture
P. 450

434                        Z ITOH AND Z MIYAZQKI






             On the other hand, in the tests of Case 3 and 4, dl and dll have the same value but the strain waves
             on I and 11-planes have not only the main large strain amplitude but also a small one, since the
             strain paths  are crossing at angles which are not right angles in the El(t)-C(t)  diagram (81.6
             degrees in Case 3 and 4).  In this case, d1 and drr can be expressed by







             Here, in the tests of Case 1, 2 and Case 3,4, taking into account that the relationship between dl
             and d11 can be expressed by

                                                            (for  Case 1,  2)
                                                                                  (12)
                                                             (for  Case 3.4)


             the total damage for cruciform straining can be rewritten as


                                                             (for  Case 1 - 4)    (13)






             Box and circular loading.  In tests with box (Case 10-12) and circular (Case 14) straining, dl and
             dll are given by Eq.( IO)  as in the cruciform straining tests.  In addition, the relationship between
             d1 and dI1 is expressed in Case 10, 12 and  14 by Eq.( 12), so that the total damage is given by
             Eq.(13).  In these  cases,  however, the  value of  the  nonproportional intensity factor, f~p, is
             approximately doubled in comparison with those of  the cruciform straining tests as listed in
             Table 2, resulting in the larger total damage.


             Step loading.  In the step straining tests (Case 6-9), the strain path is basically composed by one
             main  strain  range  with  large  amplitude on  the  I-plane and several  strain ranges with  small
              amplitudes on the 11-plane.  As for example shown in Fig.6, the strain path of Case 7 consists of
              the maximum strain amplitude with one cycle on the I-plane, and the medium strain amplitude
              with three cycles, and further small strain amplitudes with two cycles on the 11-plane.  In this
              case, the damages on I and II-planes can be expressed by,
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