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311

being on the order of magnitude comparable with the interatomic distances in silicon

carbide.

A new model, Discrete Fractal Fracture Mechanics (DFFM), is proposed here.

2. PRELIMINARIES. CLASSIC COHESIVE CRACK MODEL

When a cohesive model is designed, the length of the physical crack

c

is extended by

an adding the cohesive zones at both ends of the crack (Fig. 1). Within these zones the

restraining stress

S

counteracts the separation process. If the length of each cohesive zone

is

R

, then the half-length of the extended crack becomes

a

=

c

+

R

. In order to solve the

pertinent mixed boundary value problem one needs to assume the following distribution

of pressure applied along the surface of the extended crack

,0

( )

,

x c

p x

S c x a

σ

σ

≤ ≤

= ⎨ − ≤ ≤

(1)

This is later superposed with the uniform tension

p(x)

= -

σ

thus generating a stress-

free crack with two cohesive zones, in which the

S

-stress is present, Fig. 1. The second

boundary condition is expressed in terms of the displacement component

u

y

, which is set

equal zero along the symmetry axis outside the crack for

x a

. The resulting solution is

the familiar stress field, which in the vicinity of the crack tip contains the dominant term

controlled by the stress intensity factor. This is the singular term, and it will be subject to

annihilation. Such requirement of disappearance of the singular term is know as the

“finiteness condition”.

Figure 1: The distribution of pressure applied along the surface of the extended crack

Before proceed to set up such condition for the crack given in Fig. 1,

K

-factors

associated with stresses

σ

and

S

should be evaluated. The well-known LEFM expression

2 2

0

( )

2

a

I

a p x

K

dx

a x

π

=

(2)

is substitute (1) for the pressure

p

(

x

) to obtain the stress intensity factor for cohesive crack

0

0

2

2

2

2

2

2

2

2

(

)

2

2

2

c

a

a

a

c

c

TOT

a

dx

S dx

a dx

a Sdx

K

a x

a x

a x

a x

σ

σ

σ

π

π

π

− ⎫

⎪ =

+

=

⎪⎩

(3)

It is seen that both

σ

and

S

contribute to the total stress intensity factor. Notating as

2 2

2 2

0

2

2

a

a

S

c

a

dx

a Sdx

K

K

a x

a x

σ

σ

π

π

=

=

(4)

the Eq. (3) is rewritten as follows