PSI - Issue 5
B. Boukert et al. / Procedia Structural Integrity 5 (2017) 115–122 B.Boukert/ Structural Integrity Procedia 00 (2017) 000 – 000
118
4
xx N N x y Nxy N x y Q Q y
xy
0
yy
0
2
2
xy P P
2
P
4 (
yy
x
xx
q
2
)
0
2
2
2
x
y
x y
h x
y
3
(4)
2 M M Q x y M M Q x y Where M M P Q Q R h h 2 0 0 4 4 : , 3 xx xy x xy yy y ij ij ij ij ij
ij
The stresses resultants are related to the strains by:
0 1 3
N M B D F P E F H A B E
0 2
Q R D F A D
(5)
,
Where :
N z
k
1 Q z z z z z
2 3 4 6 (1, , , , , )
1 k z
( , , A B D E F H , , ,
(6)
)
ij
ij
ij
ij
ij
ij
ij
k
2.3. The navier solution:
The development of Navier solutions of simply supported antisymmetric cross-ply laminates using the third order theory are bellow where the boundary conditions are satisfied by the following expansions.
1 1 n m n m n m n m n m 1 1 1 1 1 1
u x y
mn U x
cos( ) sin( ) y
( , )
0
v x y
V
sin( ) s( ) x co y
( , )
mn
0
w x y
mn W x
sin( ) sin( ) y
( , )
0
(7)
1 1
( , ) x y
mn X co x
s( ) sin( ) y
x
( , ) x y
Y
sin( ) s( ) x co y
y
mn
where
/ , m a
/ m b
:
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