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8.10  Factors that Affect Fatigue Life  •  279

                                 to a discussion of these factors and to measures that may be taken to improve the fatigue
                                 resistance of structural components.
                                 Mean Stress
                                 The dependence of fatigue life on stress amplitude is represented on the S–N plot. Such
                                 data are taken for a constant mean stress s m , often for the reversed cycle situation (s m    0).
                                 Mean stress, however, also affects fatigue life; this influence may be represented by a  series
                                 of S–N curves, each measured at a different s m , as depicted schematically in Figure 8.25. As
                                 may be noted, increasing the mean stress level leads to a decrease in fatigue life.

                                 Surface Effects
                                 For many common loading situations, the maximum stress within a component or
                                 structure occurs at its surface. Consequently, most cracks leading to fatigue failure
                                   originate at surface positions, specifically at stress amplification sites. Therefore, it has
                                 been  observed that fatigue life is especially sensitive to the condition and configuration
                                 of the component surface. Numerous factors influence fatigue resistance, the proper
                                 management of which will lead to an improvement in fatigue life. These include design
                                 criteria as well as various surface treatments.

                                    Design Factors
                                    The design of a component can have a significant influence on its fatigue character-
                                 istics. Any notch or geometrical discontinuity can act as a stress raiser and fatigue crack
                                 initiation site; these design features include grooves, holes, keyways, threads, and so on.
                                 The sharper the discontinuity (i.e., the smaller the radius of curvature), the more severe the
                                 stress concentration. The probability of fatigue failure may be reduced by avoiding (when
                                 possible) these structural irregularities or by making design modifications by which sudden
                                 contour changes leading to sharp corners are eliminated—for example, calling for rounded
                                 fillets with large radii of curvature at the point where there is a change in diameter for a
                                 rotating shaft (Figure 8.26).
                                    Surface Treatments
                                    During machining operations, small scratches and grooves are invariably intro-
                                 duced into the workpiece surface by cutting-tool action. These surface markings can
                                 limit the fatigue life. It has been observed that improving the surface finish by polishing
                                 enhances fatigue life significantly.
                                    One of the most effective methods of increasing fatigue performance is by imposing
                                 residual compressive stresses within a thin outer surface layer. Thus, a surface tensile




                                  >    m >
                                 m        m
                                 3   2    1
               Stress amplitude,    a         m 1                                      Fillet





                                             m
                                             m  2
                                             3
                                                               (a)                    (b)
                                                         Figure 8.26  Demonstration of how design can reduce
                           Cycles to failure, N          stress amplification. (a) Poor design: sharp corner. (b) Good
                           (logarithmic scale)           design: fatigue lifetime is improved by incorporating a rounded
              Figure 8.25  Demonstration of the influence   fillet into a rotating shaft at the point where there is a change
              of mean stress s m  on S–N fatigue behavior.  in diameter.
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