PSI - Issue 28
Victor Rizov et al. / Procedia Structural Integrity 28 (2020) 1237–1248 Author name / Structural Integrity Procedia 00 (2019) 000–000
1244 8
the crack front. Equations (10), (11), (12) and (14) are used to obtain g , 1 g q , 2 g q and
3 g q . For this purpose, after
replacing of 1 R , , 1 q , 2 q and 3 q , respectively, with 3 g q , the equations should be solved by using the MatLab computer program. After that the complementary strain energy density is obtained by substituting of g and (24) in formula (5). Finally, the strain energy release rate is determined by substituting of * 01 u , * 02 u and * 0 u in (1). The MatLab computer program is used to carry-out the integration in (1). The longitudinal fracture behaviour of the cantilever shown in Fig. 2 is analyzed also by considering the energy balance in order to verify the solution of the strain energy release rate. For this purpose, by assuming a small increase, a , of the crack length, one writes the energy balance as 2 R , g , 1 g q , 2 g q and
a F u U
a Gl a C
,
(27)
where u is the increases of the longitudinal displacement of the free end of the internal crack arm, U is the strain energy cumulated in the bar, C l is the length of the crack front. From (65), one expresses the strain energy release rate as
1
a l u
a U
l G F C
.
(28)
C
Since the length of the crack front is 1 2 l R C ,
(29)
formula (28) is re-written as
R 1 2 1
.
a U
a F u
G
(30)
The integrals of Maxwell-Mohr are used to derive the longitudinal displacement of the free end of the internal crack arm. The result is l a u a g , (31)
The strain energy cumulated in the bar is expressed as 1 0 01 A A l a u dA U a u dA ,
(32)
where 01 u and 0 u are, respectively, the strain energy densities in the internal crack arm and in the un-cracked bar portion, a x l , (Fig.2). The strain energy density in the internal crack arm is obtained by the following formula (Rizov (2019)):
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