1968 Volume 11 Issue 48 Pages 958-962
Following the previous paper (under reversed bending and torsion), fatigue damage of 7 : 3 brass specimens under combined stress is researched by 'annealing-electropolishing method'. Standard damage life, N0, is decided under two stress levels respectively. According to the results, fatigue damage concentrates on the surface of the specimen. N0 becomes shorter rapidly, as σn becomes greater, which is normal stress on the plane of maximum shearing stress. If the ratio of number of stress repetitions to N0 is constant, then the depth of fatigue damage layer is constant also under various stress states. Knowing N0 under reversed torsion, the depth of fatigue damage is decided using an emprical formula, under various stress states.
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