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The Background of Fatigue Limit Ratio of Torsional Fatigue to Rotating Bending Fatigue in .__ 301
Table 5. Classification of fatigue limit ratios z ,,,/ u
Characteristics of material Z ,,,/ (T I Example material
Fatigue Crack Age-hardened Al-alloy
limit does
not depend initiates
on defects from
0.65-0.7 I Cast carbon steel
Fatigue Shape 0.75 Steel with a hole
limit
depends on of Connected hole 0.9 Nodular cast iron
defects defect Crack-like defect 1 1 Gray cast iron
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7. Findley, W.N. (1956), “Theory for Combined Bending and Torsion Fatigue with Data for
SAEi4340 Steel”, Int. Con$ Fatigue Metal, Inst. Mech. Eng., 150-157.
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Jpn. SOC. Mech. Eng., Vo1.42, No.359, 1947-1953.
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15. Nisitani, H. and Goto, T. (1976), “Notch Sensitivity in Fatigue of an Al-Alloy”, Trans. Jpn.
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Vo1.40, N0.340,3254-3266.
19. Nisitani, H. (1968), “Fatigue under Two-step Loading in Electropolished Specimen of