TY - JOUR
T1 - The Rotary Bending Fatigue of a Eutectoid Steel (1st Report, Effects of Surface Finish and Defects on Fatigue Limit)
AU - Harada, Shoji
AU - Nishida, Shin Ichi
AU - Endo, Tatsuo
AU - Suehiro, Kenjiro
AU - Fukushima, Yoshihiro
AU - Yamaguchi, Hiroyuki
PY - 1987
Y1 - 1987
N2 - To examine the effects of the surface finish and defects on fatigue limit, specimens differently finished, i.e., sand paper(Grade #600, #80) finish and electrolytic polish, were prepared. Moreover, to simulate surface defects, a small artificial hole of which diameter is varied from 40 to 200 μm is introduced on the specimen surface. Both as-received and annealed specimens were applied so as to extract the effect of the work-hardened surface layer on the fatigue limit. Through examination of the fatigue limit and the non-propagating crack the following results are obtained: (1) The surface roughness slightly influences the fatigue limit, while the work-hardened surface layer has a primary effect on the fatigue limit. (2) An increase in the diameter of the small hole decreases the fatigue limit and results in the prolongation of the non-propagating crack. (3) For the non-propagating crack, the threshold stress intensity factor range ΔKth decreases with a decrease in the crack length.
AB - To examine the effects of the surface finish and defects on fatigue limit, specimens differently finished, i.e., sand paper(Grade #600, #80) finish and electrolytic polish, were prepared. Moreover, to simulate surface defects, a small artificial hole of which diameter is varied from 40 to 200 μm is introduced on the specimen surface. Both as-received and annealed specimens were applied so as to extract the effect of the work-hardened surface layer on the fatigue limit. Through examination of the fatigue limit and the non-propagating crack the following results are obtained: (1) The surface roughness slightly influences the fatigue limit, while the work-hardened surface layer has a primary effect on the fatigue limit. (2) An increase in the diameter of the small hole decreases the fatigue limit and results in the prolongation of the non-propagating crack. (3) For the non-propagating crack, the threshold stress intensity factor range ΔKth decreases with a decrease in the crack length.
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U2 - 10.1299/kikaia.53.401
DO - 10.1299/kikaia.53.401
M3 - Article
AN - SCOPUS:0023311364
SN - 0387-5008
VL - 53
SP - 401
EP - 409
JO - Nihon Kikai Gakkai Ronbunshu, A Hen/Transactions of the Japan Society of Mechanical Engineers, Part A
JF - Nihon Kikai Gakkai Ronbunshu, A Hen/Transactions of the Japan Society of Mechanical Engineers, Part A
IS - 487
ER -