PSI - Issue 26
Merazi Mohamed et al. / Procedia Structural Integrity 26 (2020) 129–138 Merazi et al / Structural Integrity Procedia 00 (2020) 000 – 000
134
6
The stress resultants of a the plate can be related to the total strains by
s
N
B D H 0 D D A 0 B s s
k k
s xz s yz
s xz s yz
s 44 0 A A 0
S S
s b
s
s b
=
(16)
=
M M
,
s 55
s
where
b t xy
s t xy
t x y xy N N , N , N = ,
b y b x b M M ,M ,M = 0 , 0 , 0 } , = { , , } , = { , , } ,
s s x s M M ,M ,M = y
(17a)
= {
(17b)
Where ij A , ij D , etc., are the plate stiffness, defined by { 11 11 1 1 1 1 1 1 12 12 1 2 1 2 1 2 and
66 66 6 6 6 6 6 6 } = ∫ 11 (1, 2 , ( ), ( ), 2 ( )) ℎ 2 − − ℎ 2 −
{ 1 1− 2 }
(18a)
(
) (
) s 11
s 22
s 22
s 22
s 11
s 11
11 22 22 A , D , B , D , H A , D , B , D , H = 11
(18b)
h d
2 − − −
2
= = s A A Q g z s
dz
( ) ns
,
(18c)
ns
44
55
55
h d
2
3. Analytical solution
Rectangular plates are generally classified in accordance with the type of support used. We are here concerned with the exact solution for a simply supported FG plate. The following boundary conditions are imposed at the side edges: 0 = = = = = = = = 0 at x= -a/2, a/2 (19a) 0 = = = = = = = = 0 at y= -b/2, b/2 (19b) The equations of motion admit the Navier solutions for simply supported plates. The displacement variables 0 u , 0 v , b w , s w can be written as product of arbitrary parameters and known trigonometric functions by assuming the following variations
V U
y) x) sin( sin( y) x) sin( sin( y) x) cos( sin( y) x) sin( cos(
v u
0 0
mn mn
= = m 1n 1
(20)
=
W
w w
s b
smn bmn
W
n / b = .
mn U , mn V , bmn W , and
smn W are arbitrary parameters to be determined, and
m / a = and
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