
202 Applied calculus of variations for engineers
global finite element matrix is then
K =
⎡
⎢
⎢
⎣
K
1
(1, 1) K
1
(1, 2) K
1
(1, 3) 0
K
1
(2, 1) K
1
(2, 2) + K
2
(1, 1) K
1
(2, 3) + K
2
(1, 2) K
2
(1, 3)
K
1
(3, 1) K
1
(3, 2) + K
2
(2, 1) K
1
(3, 3) + K
2
(2, 2) K
2
(2, 3)
0 K
2
(3, 1) K
2
(3, 2) K
2
(3, 3)
⎤
⎥
⎥
⎦
.
The assembled global load vector is similarly obtained:
F =
2
i=1
L
ge
F
g
e,i
=
⎡
⎢
⎢
⎣
F
1
(1)
F
1
(2) + F
2
(1)
F
1
(3) + F
2
(2)
F
2
(3)
⎤
⎥
⎥
⎦
.
The notation convention is the same as in the element matrix assembly.
The global solution is then obtained from the matrix equation
Ku
= F,
where K is the global stiffness matrix and F is the global force vector. The
global solution vector is
u
= K
−1
F =
⎡
⎢
⎢
⎣
u
1
u
2
u
3
u
4
⎤
⎥
⎥
⎦
,
and ...