Biomedical Engineering Reference
In-Depth Information
which can be developed as,
dL
1
¼
Z
X
dB
T
rdX
þ
Z
B
T
drdX ¼ K
T
du
ð
2
:
84
Þ
X
Using Eqs. (
2.35
) and (
2.70
) the following relation is obtained,
dr ¼ cBdu
ð
2
:
85
Þ
In the deforma
ti
on matrix B only the nonlinear part dB
NL
is dependent of u,
Eq. (
2.80
), thus dB ¼ dB
NL
and therefore,
dL
1
¼
Z
X
dB
NL
r dX
þ
Z
X
B
T
c B dX
ð
2
:
86
Þ
Where the stiffness matrix can be presented as,
K
T
¼ K
r
þ
K
0
þ
K
NL
ð
2
:
87
Þ
Being,
K
r
¼
Z
X
dB
NL
r dX
ð
2
:
88
Þ
K
0
¼
Z
X
B
0
cB
0
dX
ð
2
:
89
Þ
K
NL
¼
Z
X
ffi
dX
B
0
cB
NL
þ
B
NL
cB
NL
þ
B
NL
cB
0
ð
2
:
90
Þ
The initial stress matrix or geometric matrix K
r
is defined as,
K
r
du ¼
Z
X
G
T
dA
T
r dX
ð
2
:
91
Þ
The variation of matrix A in order to u can be defined as,
2
4
3
5
dh
x
0
3
1
0
3
1
dh
y
0
3
1
dh
z
½
½
½
0
3
1
dh
y
0
3
1
dh
x
dh
z
0
3
1
dA
T
¼
ð
2
:
92
Þ
½
½
½
0
3
1
0
3
1
dh
z
0
3
1
dh
y
dh
x
½
½
½