PSI - Issue 17
B. Boukert et al. / Procedia Structural Integrity 17 (2019) 37–43 Author name / Structural Integrity Procedia 00 (2019) 000 – 000
39
3
where:
N z
k
1 Q z z z z z +
(3)
2 3 4 6 (1, , , , , )
1 k z = =
( , , A B D E F H , , ,
)
ij
ij
ij
ij
ij
ij
ij
k
The equation of motion of the third order theory are derived using the principle of virtual displacement. The obtained set of equations are presented below.
xx N N x y Nxy N x y Q Q y
xy
0
+ =
yy
0
+ =
(4)
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
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 development of Navier solutions of simply supported antisymmetric cross-ply laminates using the third order theory are presented below, where the boundary conditions are satisfied by the following expansions. 0 1 1 0 1 1 ( , ), ( , ) , .cos( ).sin( ) ( , ), ( , ) , .sin( ). s( ) x mn mn n m y mn mn n m u x y x y U X x y v x y x y V Y x co y = = = = = =
n m = =
(5)
w x y
mn W x
.sin( ).sin( ) y
( , )
=
0
1 1
where
/ , = = m a
/ m b
:
The mechanical transverse load q(x,y) is also expanded in double Fourier series
0 0 4 ( , ) sin( ) sin( ) a b q x y x ab
mn Q
y dxdy
(6)
=
The coefficients ( U mn ,V mn , W mn , X mn , Y mn ) of the Navier solution are obtained through the resolution of the system given by (7) . 1 1 11 12 13 14 15 2 2 T C mn mn mn T C N N U S S S S S − − −
12 22 23 24 25 13 23 33 34 35 14 24 34 44 45 15 25 35 45 55 S S S S S S S S S S W Q S S S S S X S S S S S Y = − mn mn mn mn V
N
N
−
mn
mn
(7)
mn
T
C
1
1
2 mn M M M M − − T mn
mn
C
2
−
mn
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