PSI - Issue 2_B
Marcus Wheel / Procedia Structural Integrity 2 (2016) 174–181
179
Author name / Structural Integrity Procedia 00 (2016) 000–000
6
M 1 +M 2
M
1
d 1
M 2
d
b
a
Figure 1 Composite laminate with delamination of length a
(n-4) layers
(n-3) layers
E B E A
E A
t B
E
t
B
t A
t B
(n-3) layers
(n-4) layers
½.t B
b
½.t B
n odd
b
n even
Figure 2 Details of laminate cross section
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