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8.8 The S–N Curve  •  273

                                                                     Figure 8.19  Stress amplitude (S)
                                                                     versus logarithm of the number of cycles
                                                                     to fatigue failure (N) for (a) a material that
                                                                     displays a fatigue limit and (b) a material that
                  Stress amplitude, S  Fatigue
                                                                     does not display a fatigue limit.



                    limit





                       10 3  10 4  10 5  10 6  10 7  10 8  10 9  10 10
                                       Cycles to failure, N
                                       (logarithmic scale)
                                            (a)


                   Stress amplitude, S




                      S

              Fatigue strength 1
                   cycles
               at N 1
                                                                                            Tutorial Video:
                                                                                          Impact Energy vs.
                                                                                              Temperature
                                                                                            and S–N Graph
                        3     4     Fatigue life  7    8    9     10
                       10    10                10  N 10    10   10
                                                    1
                                    at stress S 1                                                Examples
                                                                                        How do I Interpret the
                                       Cycles to failure, N
                                       (logarithmic scale)                              Cyclical Fatigue Failure
                                            (b)                                          Graphs and Equations?
                                 largest value of fluctuating stress that will not cause failure for essentially an infinite number
                                 of cycles. For many steels, fatigue limits range between 35% and 60% of the tensile strength.
                                    Most nonferrous alloys (e.g., aluminum, copper) do not have a fatigue limit, in that
                                 the S–N  curve continues its downward trend at increasingly greater N  values (Figure
                                 8.19b). Thus, fatigue ultimately occurs regardless of the magnitude of the stress. For
              fatigue strength   these materials, the fatigue response is specified as fatigue strength, which is defined as
                                                                                                        7
                                 the stress level at which failure will occur for some specified number of cycles (e.g., 10
                                 cycles). The determination of fatigue strength is also demonstrated in Figure 8.19b.
                                    Another important parameter that characterizes a material’s fatigue behavior is
              fatigue life       fatigue life N f . It is the number of cycles to cause failure at a specified stress level, as
                                 taken from the S–N plot (Figure 8.19b).
                                    Fatigue S–N curves for several metal alloys are shown in Figure 8.20; data were gen-
                                 erated using rotating-bending tests with reversed stress cycles (i.e., R    1). Curves for
                                 the titanium, magnesium, and steel alloys as well as for cast iron display fatigue limits;
                                 curves for the brass and aluminum alloys do not have such limits.
                                    Unfortunately, there always exists considerable scatter in fatigue data—that is, a vari-
                                 ation in the measured N value for a number of specimens tested at the same stress level.
                                 This variation may lead to significant design uncertainties when fatigue life and/or fatigue
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