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
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
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