Issue 25
A. Spagnoli et alii, Frattura ed Integrità Strutturale, 25 (2013) 94-101; DOI: 10.3221/IGF-ESIS.25.14
T HE KINKED CRACK MODEL Self-balanced microstress field Consider an infinite cracked plate described by the xy coordinate system in Fig. 1, exposed to remote tensile stress ( ) y along the y-axis and shear stress ( ) xy . Assume that material microstructural features create a self-balanced (residual) microstress field, which is characterized by a length scale, d , related to a characteristic material length, and amplitudes e.g. governed by material properties’ dispersion. Further let us assume that such a microstress field is a one-dimensional function (of the x - coordinate), defined by the following stress tensor:
x
x d
T
xy
x,a
xy,a
(1)
(x)
f
y
xy
xy,a
y,a
Without lack of generality, we describe the plane microstress field by taking into account the following two non-zero stress components: y a f(x / d) and xy a f(x / d) . An attempt to correlate the above self-balanced microstress to some heterogeneity features of the material microstructure is presented in Ref. [18].
K I
k I
K II
y
k II
2
2
b
k I
k II
0
1
x
1
a
l
K II
K I
Figure 1 : Nomenclature for the kinked crack in an infinite plate (y-axis of symmetry).
Approximate stress intensity factors in the kinked crack According to the present model, the central crack might kink as a result of both remote and microstess fields (see Fig. 1). As will be shown below, the local stress intensity factors (SIFs) at the crack tips ( I k and II k ) can be expressed as a function of those ( I K and II K ) of a straight crack having length equal to the projected length of the kinked crack [2-7]. The total values of SIFs defined with respect to the projected crack are the sum of two contributions (due to remote and microstress fields, respectively), that is: ( ) I I I ( ) II II II K K K K K K (2) The remote SIFs are defined with respect to the projected crack of semi-length l , aligned with the x - axis (Fig. 1). Hence, under the uniform remote stresses ( ) ( ) y and ( ) ( ) xy , we have :
l
1
l
( ) K 2
( )
( )
dx
l
I
2
2
0
l
x
(3)
l
1
l
( ) K 2
( )
( )
dx
l
II
2
2
0
l
x
95
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