PSI - Issue 2_B
Maria Kashtalyan et al. / Procedia Structural Integrity 2 (2016) 3377–3384 Author name / Structural Integrity Procedia 00 (2016) 000–000
3379
3
Fig. 2. (a) Schematics showing a composite sample with multiple cracks in the ceramic layer;(b) representative segment bounded by two cracks without crack widening; (c) representative segment bounded by two cracks with crack widening l 2 . The equilibrium equations in terms of layer stresses, i.e. stresses averaged across the thickness of the layer and the depth of the sample, have the form
c ~ ~ ( ) ( ) m
ij (1 ) , ,
1,2,
h h /
i j
(1a)
ij
ij
m c
~
~
h
w
1
2 ( ) 22 c c 2
1 ( ) 12 c c 2
d
d
c
~
c ( )
c ( )
x x x dx dx 1 2 3 1 3 ( , , )
,
,
(1b)
0
0
ij
ij
2
wh
dx h
dx h
c
w
h
c
where 1 2 , are the interface shear stresses at the metal/ceramics interface. Assuming that out-of-plane shear stresses vary linearly with 3 x and in the metal layer this variation is restricted to the shear layer of thickness s h , i.e. , 1, 2 ), ( ; , 3 3 ( ) 3 3 3 ( ) 3 j h h x h x h h h x x h h s c c s c s j m j c c j c j (2) the interface shear stresses 1 2 , can be expressed in terms of the in-plane displacements ~ , ~ , 1,2 ( ) ( ) j u u m j c j , and shear moduli c m G G , of the ceramic and metal phases as
c m (1 (1 ) / 2) 3 G G
(3)
c ), ( ~ ~ ( ) ( )
m K u u
,
h h /
K
j
j
j
j
j
s
m
h G
m c h G
c m
The constitutive equations in terms of layer strains and stresses are ( ) 12 ( ) 22 ( ) 11 ( ) 66 ( ) 22 ( ) 12 ( ) 12 ( ) 11 ( ) 12 ( ) 22 ( ) 11 ~ ~ ~ 0 0 0 0 ~ ~ ~ c c c c c c c c c c c S S S S S , ( ) 22 ( ) 12 ( ) 12 ( ) 11 ( ) 12 ( ) 22 ( ) 11 0 0 ~ ~ ~ m m m m m m m S S S S S
~ ~ ~
( ) m
0 0
11
( ) m
(4)
22
( ) m
( ) 66 m
12
( ) 11 ~ ~ m c , and crack surfaces are stress-free, i.e. 0 11 ( )
In addition, it is also assumed that
~
0, ~ (5) Equations (1)-(4) can be reduced to two uncoupled second-order ordinary differential equations with respect to in-plane layer stresses in the ceramic layer. 0 ~ ~ 0, ~ ~ 12 ( ) 12 ( ) 12 ( ) 2 2 ( ) 12 2 22 ( ) 22 11 ( ) 11 ( ) 22 ( ) 1 2 ( ) 22 2 c c c c c c c c c L dx d L dx d (6) Solutions of these equations satisfying specified boundary conditions (5) are found as ( ) s l ( ) c 12 ( ) s l ( ) c 22 2 2 x x
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