Biomedical Engineering Reference
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2
4
3
5 ¼
2
4
3
5
2
4
3
5
2
4
3
5
r 1 00
0 r 2 0
00r 3
n 11
n 12
n 13
r xx
r xy
r xz
n 11
n 21
n 31
n 21
n 22
n 23
r yx
r yy
r yz
n 12
n 22
n 32
n 31
n 32
n 33
r zx
r zy
r zz
n 13
n 23
n 33
ð 2 : 34 Þ
The principal stresses and principal directions characterize the stress in P and
are independent of the orientation of the coordinate system.
2.1.2 Constitutive Equations
The following relation between the stress rate and the strain rate is assumed,
dr ¼ c de
ð 2 : 35 Þ
The material constitutive matrix is defined by c and if material nonlinear
relations exists between r and e, then c ¼ c ep . With Eq. ( 2.35 ) the following
relation can be established,
de ¼ c 1
dr
ð 2 : 36 Þ
being s ¼ c 1
and defined for the three-dimensional case as,
2
4
3
5
t yx
E yy
t zx
E zz
1
E xx
000
t xy
E xx
t zy
E zz
1
E yy
000
t xz
E xx
t yz
E yy
1
E zz
000
s ¼
ð 2 : 37 Þ
1
G xy
0
0
0
00
0
0
0
0
1
G yz
0
1
G zx
0
0
0
0
0
The material constitutive matrix c is obtained by inverting the material com-
pliance matrix s, which is here defined for an three-dimensional anisotropic
material. The elements on matrix s are obtained experimentally. E ii is the Young
modulus in direction i, t ij is the Poisson ratio which characterizes the deformation
rate in direction j when a force is applied in direction i, G ij is the shear modulus
which characterizes the variation angle between directions i and j. Due to sym-
metry the following relation can be established,
E i t ji ¼ E j t ij
ð 2 : 38 Þ
For the two-dimensional case the plane stress and plane strain [ 5 ] deformation
theory assumptions can be presumed. Considering the plane stress assumptions,
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