Fatigue Crack Paths 2003
A non-linear dependency from loads of relative displacement of the crack lips during
opening can be noticed; but this will not affect the overall deflection behaviour which
always resulted quite linear.
The behaviour is obviously different when approaching the end of the crack (in
points B 31 and B39) where the relative movementof the crack lips is strongly reduced,
so that the gauges do not fail anymore or fail at very high loads.
An overview of lips opening in all measuring points is given in Fig. 9: the measured
strains displacements have been distributed symmetrically with respect to the crack.
46000
load A
load B
2000
]
load C
S t r a i n [
0
load D
-2000
load E
-4000
-6000
B.31 B 3 2 B 3 3 B 3 4 B 3 5 B 3 6 B 3 7 B 3 8 B 3 9
Strain gauge
Figure 9. The opening of crack lips as measured by the series of B gauges.
T H ESIMPLIFIEMD O D E L
The model used for calculating the breathing behaviour and the reduced stiffness of the
cracked shaft is described in detail in [1]. Here only some results are recalled. The
model of the breathing mechanism allows to evaluate with high accuracy, if compared
with 3D non linear calculations, the open and closed parts of the crack. It is then
assumed that only the closed parts together with the integer parts of the cracked cross
section contribute to the resisting area and to its second moments of area. The values of
the second moments of area are then used for evaluating the stresses due to the bending
moment, in the same manner as it would have been in a constant cross section beam,
which is obviously totally unrealistic. The highly non-linear stress distribution is not
considered.
The crack closure effect has been simulated with an external bending momentwhich
tends to hold the crack closed, generating a maximumof 140 micro-strains of
compressive strain.
These strain values have been corrected with the stress intensity factors of Fig. 4.
N o wa comparison is possible between calculated results and experimental results,
taking account of crack closure effects and stress intensity factors.
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