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Section 9.6  Trends in S-N Curves                                          443


                                                σ , ksi
                                                 u
                                      20
                           0     Wrought Al alloys  40      60         80   30
                       σ erb  , Fatigue Limit, MPa  100  m = 0.4  σ erb  = 130 MPa  20  σ erb  , ksi
                        200
                        200

                                                                            10


                          0       100     200    e  300    400     500     600 0
                                       σ  , Ultimate Tensile Strength, MPa
                                        u
                                                              8
            Figure 9.25 Fatigue strengths in rotating bending at 5 × 10 cycles for various tempers of
            common wrought aluminum alloys, including 1100, 2014, 2024, 3003, 5052, 6061, 6063,
            and 7075 alloys. The slope m e = σ erb /σ u indicates the average behavior for σ u < 325 MPa.
            (Adapted from R. C. Juvinall, Stress, Strain, and Strength, 1967; [Juvinall 67] p. 215;
            reproduced with permission; c  1967 The McGraw-Hill Companies, Inc.)


               Figures 9.24 and 9.25 apply for a uniaxial state of stress and for zero mean stress, so the values
            need to be adjusted for other situations. For example, for a state of pure shear stress due to torsion,
            the fatigue limit for zero mean stress can be estimated from the bending value by
                                                 √
                                                                                      (9.13)
                                        τ er = σ erb / 3 = 0.577σ erb
               Glass-fiber-reinforced thermoplastics are typically tested under zero-to-maximum tension or
            bending. Such composites may have various reinforcement details, such as continuous unidirec-
            tional fibers, random chopped fiber mats, or short chopped fibers for injection molding. Their S-N
            curves for R ≈ 0 are sometimes approximated by a relationship of the form of Eq. 9.5, namely,

                                         σ max = σ u (1 − 0.1log N f )                (9.14)

            where σ u is the ultimate tensile strength. The constant 0.1 determines the slope of the resulting
            straight line on a log–linear plot. See the paper by Adkins (1988) in the References for more
            detail.
               An important influence on S-N curves that will be considered in some detail later in this chapter
            is the effect of mean stress. For a given stress amplitude, tensile mean stresses give shorter fatigue
            lives than for zero mean stress, and compressive mean stresses give longer lives. Some test data
            illustrating this are shown in Fig. 9.26. Note that such an effect of mean stress lowers or raises the
            S-N curve, so that for a given life, the stress amplitude which can be allowed is lower if the mean
            stress is tensile, or higher if it is compressive.
               Stress raisers (notches) shorten the life—that is, lower the S-N curve—more so if the elastic
            stress concentration factor k t is higher. An example of this effect is shown in Fig. 9.27. Another
            important trend is that notches have a relatively more severe effect on high-strength, limited-ductility
            materials. Notch effects are treated in detail in the next chapter, and also later in Chapter 14.
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