Fatigue Crack Paths 2003
fully reversed torsion tests
out on V-shaped
carried
a)
φ 12.5
φ 20
specimens, all characterised by a
R 40
notch tip radius equal to 0.5
60
80
60
mm.
90
Fatigue crack nucleation and
propagation phases are analysed
b)
φ 20
in detail by means of optical and
electronic microscopy. Despite
R 0.5
p = 0.5, 2, 4
R 0.5
the differences due to notch
shape and load level, all fatigue
c)
φ 28
φ 20
p = 4
2800
strength data are summarised in
terms of the Notch Stress
60
60
Figure 1. Geometry of the specimens.
Intensity Factor (N-SIF). Such
factors are calculated on the
basis of the stress distribution
related
to the uncracked
geometry, the notch being modelled simply as a re-entrant corner. N-SIF includes the
influence of notch dept and the size effect. Despite the complexity of the fatigue
phenomena, N-SIF are seen able to summarise the fatigue strength data in a single band
with a very limited scatter. This makes the N-SIF a useful and powerful tool in fatigue
life assessments in the presence of small value of the notch tip radius.
M A T E R I A LN DG E O M E TORFYS P E C I M E N S
The geometry of smooth and notched specimens is shown in Fig. 1. With reference to V
shaped notches (Fig. 1b), the V-notch depth ranges from 0.5 to 4 mm.The height of the
shoulder (Fig. 1c) is 4.0 mm. In all notched specimens the notch tip radius was kept
constant and equal to 0.5 mm. Such a value makes it difficult any correlation between
the theoretical stress concentration factor Kt and the fatigue trength reduction f, since he no ch s sitivi y index
exhibits a large scatter. Finite element analyses car i d out by using the
A N S Y S ®code gave a theoretical stress concentration factor (referr d to the net
area) equal to 1.94, 2.03 and 1.73 for the
symmetric V-notches with a depth equal to
4.0 mm, 2.0 m m and 0.50 mm, respectively. On the other hand, the
geometry with shoulders is characterised by a K net= 1.82.
Figure 2. Microstructure of the C40 steel
(normalised state).
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