Page 439 - Mechanical Behavior of Materials
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Section 9.5  The Physical Nature of Fatigue Damage                         439





























































            Figure 9.19 Stress–life curves for completely reversed bending of smooth specimens, showing
            various stages of fatigue damage in an annealed 99% aluminum (1230-0), and in a hardened
            6061-T6 aluminum alloy. (Adapted from [Hunter 54] and [Hunter 56]; copyright c   ASTM;
            reprinted with permission.)
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