Page 278 - Failure Analysis Case Studies II
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                             Table 1
                             Bend stress incurred in the adjustment pin at each weight stack
                             setting

                             Weight stack            Fatigue bend stress
                             Ob)                     (MW
                              15                      19
                              30                      38
                              45                      58
                              60                      17
                              75                      96
                              90                     115
                             105                     135
                             120                     154
                             135                     173
                             150                     192
                             I65                     212
                             180                     23 1
                             195                     250
                             210                     269
                             225                     289
                             240                     308
                             255                     327
                             270                     346
                             285                     366






       2.6. Bending stresses

          From the previous section, we see that individuals use varying weight stack settings. Each weight
       stack setting produces a unique bending stress in the adjustment pin. For each weight stack setting,
       the bend stress was calculated using equation (2) and multiplied by the fatigue stress concentration
       at the pin shoulder. The corrected bending stresses for each weight stack setting are summarized
       in Table 1.
       2.7.  Full reuersed loading

          The expected number of cycles to failure for each bending stress were estimated using Basquin’s
       law [5], where,

            om  = A(NJb.                                                                       (4)
       However,  Basquin’s law is only valid for the case of  fully reversed loading. In the case of  the
       adjustment pin,  it was being loaded from zero to various values. Therefore, the cyclic bending
       stresses were converted to equivalent fully reversed stresses. This was done using the Goodman
       mean stress correction [6],
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