PSI - Issue 13
B. Boukert et al. / Procedia Structural Integrity 13 (2018) 174–180 B.Boukert et al / Structural Integrity Procedia 00 (2018) 000–000
176
3
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
(3)
,
where:
N z
1 Q z z z z z
k
2 3 4 6 (1, , , , , )
(4)
1 k z
( , , A B D E F H , , ,
)
ij
ij
ij
ij
ij
ij
ij
k
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. 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
( , )
.sin( ).sin( ) y
w x y
mn W x
(5)
0
1 1
:
/ , m a
/ m b
where
The mechanical transverse load q(x,y) is also expanded in double Fourrier series
0 0 4 ( , ) sin( ) sin( ) a b q x y x ab
(6)
mn Q
y dxdy
The coefficients ( U mn ,V mn , W mn , X mn , Y mn ) of the Navier solution are obtained by solution of the system (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 where N mn , M mn are given by equations 8-10: 1 , , N z k k k Ti Ti Ti mn mn mn i N M P Q mn mn mn T mn T mn V N
N
mn
mn
(7)
1
1
C
2 mn M M M M mn
mn
2
C
mn
3
( ), T z T z z T z z dz ( ) , ( )
(8)
1 k z k
4 h
Ti
Ti
Ti
mn M M
P
(9)
mn
mn
2
3
0 0 a b
4
i
i
(10)
sin( ) sin( ) x
mn T
T
y dxdy
ab
(11)
( , , ), T x y z C x y z ( , , )
1( , ), 2( , ) sin( ) sin( ) f z T f z C x y
1 1
n m
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