Issue 29
A. Bacigalupo et alii, Frattura ed Integrità Strutturale, 29 (2014) 1-8; DOI: 10.3221/IGF-ESIS.29.01
ˆ
11,1 12,2 1 1 21,1 22,2 2 2 ˆ d d k v u k v u
1 1 u
ˆ k
1 2 u
1,1 m m k u v k u v 2,2 21 1 1 2 2 2 ˆ ˆ ˆ d d k I
I
12
1
(2)
2 1 v
2 2 v
where the stiffnesses ˆ d
d cell k k A and ˆ
cell A being the area of the periodic cell, together with
k k A
are introduced,
cell
M
M
J
J
1 A and
and
, and the micro-inertia terms
, respectively.
the mass densities
I
I
1
2
2
A
A
A
1
2
1
2
cell
cell
cell
cell
i m are the overall stress components, namely the asymmetric stress components and the micro
ij and
In Eq. (2)
cell A
2 2 2 3 cos l
and the following inertial parameters
couples, respectively. In case of hexachiral lattice, one obtains
are obtained
3 sin 2
s
1
24
2 2 3 tan sin l 2 2 3 sin 24 i A 1 24 M s I 2
cell
2 3 J
2
2 sin tan
2
I
l
192 i
2
A
cell
24 s , 1 sin 2
cell A
and the resulting inertia parameters are
For the tetrachiral lattice one obtains
2
2 cos
l
48 s
2 , M
2 J
2
2
1 . To obtain the displacement formulation of the equations of motion, the compatibility equations involving the macrostrain components 11 1,1 u , 22 2,2 u , 12 1,2 u , 21 2,1 u and the curvatures 1 ,1 and 2 ,2 have to be considered together with the constitutive equation. sin I l , 2 2 sin 48 i cell A 2 2 sin tan 2 2 192 i cell I l A
M ICROPOLAR CONSTITUTIVE EQUATION FOR HEXA - AND TETRA - CHIRAL LATTICES
T
he constitutive equation of hexachiral honeycomb corresponds to that obtained in [13, 15] and is written as follows
11 22 12 21 1 2
A A A A
2
0 0 0 0 S 0
0 0 0 0 0 S
11 22
2 A A k A A k
k k
(3)
12
21 1 m m
0 0
0 0
0 0
0 0
2
in which the five elastic moduli
4
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