Fatigue Crack Paths 2003
O n the other hand, in the case of a slim parabolic notch (i.e. a blunt crack, with 20t=0
and q=2, see Figures 1-2) Eqs 3 coincide with Creager-Paris’ formulation [9]. Only in
this case the distance between the notch tip and the origin of the co-ordinate system is
r0=p/2. Otherwise, the distance r0 varies as a function of q, according to the expression
reported in Figure 2.
For Mode1 problems, the parameter a1 can be correlated to the peak stress value
according to the following expression [21]:
(5
m a x
(4)
3 . 1 :
%1r3‘“1{1+%.+xb,(1—M)+I(1+i1)xd,+x.,l
‘1 I 40-0
P R I N C I P ASLT R E SDSI S T R I B U T IDOUNET OM O DIEL O A CDO N D I T I O N S
IN FINITESIZEC O M P O N E N T S
Equations 3 are valid in the close neighbourhood of the notch tip, where the influence of
the remotely applied stress does not appear. Obviously the crack length can overcome
this region and therefore a correction of such formulas, capable to prolong their range of
validity, is clearly desirable. That would allow us a rapid calculation of the SIF on the
basis of the principal stress distribution of the uncracked body. Following these
guidelines, an analytical approach useful for finite size components under tensile loads
was presented in Ref [28], with reference to the tensile stress 69 I 6:0 :Gy along the notch
bisector (Figure 2). It was given as follows:
6 = — 6 m a4(q_x1) 1+—atan[(r_r°)m]
F +qo)I i W (5)
y 4 ( q — l ) + q 0 ) I
r o m
r0
_ xd,(l+iu)+x.l
where
I
_
6
1 + > H + X(1_b7\I'1)
( )
The coefficient 031 is given in Table 1. Eq. 5 represents an extension of the local stress
distribution given in Ref. [21]:
G m a x
_ i 7cI—l
i III-l
6y —4(q_I)+q0)lI4(q 0L0) +q®1Ir0J I
(7)
Due to its nature, Eq. 5 coincides with Eq. 7 in highly stressed regions but it is also
capable to describe the transition between notch stress zone and the nominal stress zone.
It is worth noting that the parameter m in Eq. 5 can be evaluated on the basis of
equilibrium conditions, without any best fitting of numerical data. A number of
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