PSI - Issue 33
10
Victor Rizov et al. / Procedia Structural Integrity 33 (2021) 402–415 Author name / Structural Integrity Procedia 00 (2019) 000–000
411
n t
2 1
2 1
2 2
e v t UN i 2
1
u
E v t pri UN
n E E
.
(31)
0
1
UN
i
i
pri
i
DRH v and
DUN v , which are involved in (14) and (29) are found in the following way.
The speeds,
5 10 0.0066
Fig. 7. The strain energy release rate in non-dimensional form plotted against 31 q (curve 1 – at
v
rad / sec , curve 2 – at
5 10 0.0132
5 0.02 10
v
v
rad / sec and curve 3 – at
rad / sec ).
First, one equation is written by using the fact that the bending moments in the cross-sections of the right-hand delamination crack arm and the un-cracked beam portion are equal RH i UN i i n i A i n i A UNi i z dA z dA 1 ( ) 1 ( ) 2 1 . (32)
t v DRH and
t v DUN in (6). After
DRH and DUN with
Further one equation is worked-out by replacing of
substituting of stresses, DUN v by using the MatLab computer program. It should be mentioned that equations (32) and (6) can be used to determine DRH v and DUN v at various values of the time. By substituting of (22), (23) and (26) in (22), one obtains the following solution to the strain energy release rate: i and UNi , in (32), equations (32) and (6) are solved with respect to DRH v and
RH i n i 1 ( )
RH i n i 1 ( )
h 1
G
u dA RH 0
u dA i RH 0
.
(33)
i
A
A
i
i
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