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Fig. 3.1 Reference element
shape functions on the
reference element K
Furthermore, for i, j =
1 , 2 there holds
a l (N j
K l ,N i K l )
( A l ) ij =
α(x)∂ x N j
K l N i K l d x
β(x)∂ x N j
γ(x)N j
K l x N i K l +
K l N i K l +
=
K l
h l
2
α K l (ξ ) 4
h l N j N i + β K l (ξ ) 2
h l N j N i +
γ K l (ξ )N j N i
=
d ξ,
K
where
α F K l (ξ ) ,
β F K j (ξ ) ,
γ F K l (ξ ) .
β K l (ξ )
α K l (ξ )
:=
:=
γ K l (ξ )
:=
For later purpose, it is useful to split the integral into three parts
( A l ) ij = ( S l ) ij + ( B l ) ij + ( M l ) ij ,
(3.22)
where
2
h l
K α K l N j N i d ξ,
K β K l N j N i d ξ,
( S l ) ij
=
( B l ) ij =
h l
2
γ K l N j N i d ξ.
( M l ) ij
=
K
For general coefficients α(x) , β(x) and γ(x) , these integrals cannot be computed
exactly. Hence, they have to be approximated by a numerical quadrature
1
p
w (p)
j
f(ξ (p)
j
f(ξ) d ξ
),
1
j =
1
using a p -point quadrature rule with quadrature weights w (p)
j
and quadrature points
ξ (p)
j
1 ,...,p .
It remains to construct the stiffness matrix A . The idea is to express the global ba-
sis functions b i (x) in terms of the local shape functions. We have for i
(
1 , 1 ) , j
=
=
1 ,...,N ,
N K i +
N K i + 1 , 0 (x)
N K 1 , N + 1 (x)
N K N + 1 .
=
=
=
b i (x)
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