In order to investigate the probability distributions of crack initiation lives N
l under stresses near the endurance limit, S50C specimens having two small transverse holes were tested under cantilever type rotating bending stress. Through the analysis of the data the following conclusions are obtained. (1) The growth of the fatigue crack under the stresses near the endurance limit is very slow, but the crack propagates even after 10
8 cycles, repeating acceleration and deceleration. (2) The S-N
l curve, the relation between the stress σ and the crack initiation life N
l, is thought to be composed of three H^
--, F^
-- and S^
--curves, each of which represents the S-N
l relation resulting from a different crack initiation mechanism, where H^
--curve shows the S-N
l relation at stress levels well above the endurance limit σ
W, F^
--curve appears at stress levels near σ
W, and S^
--curve at still lower stress levels. The apparent scatter of N
l under stresses near σ
W can be explained as a result of the superposition of the respective distributions around these curves.
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