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3.6.2 Convergence of the Finite Element Method
Assume uniform mesh width h in space and constant time steps k = T/M in time.
We show now that the computed sequence
{ u N }
converges, as h
0 and k
0, to
the exact solution of ( 3.7 ). We have
C 1 (J
H 2 (G))
C 3 (J
H 1 (G)) . Let u m (x)
Theorem 3.6.5
Assume u
;
;
=
u(t m ,x) and u N
θ< 2
S 1
T
be as in ( 3.14 ), with V N =
. Assume for 0
also ( 3.30 ).
Then , the following error bound holds :
M
1
u m + θ
N
u M
u N
2
u m + θ
2
a
L 2 (G) +
k
0
m
=
Ch 2 T
0
Ch 2
2
max
0
T
u(t)
H 2 (G) +
t u(s)
H 1 (G) d s
t
C k 2 0
2
tt u(s)
d s
if 0
θ
1 ,
+
k 4 0
(3.44)
1
2
ttt u(s)
d s
if θ =
2 .
Remark 3.6.6 By the properties ( 3.8 )-( 3.9 ) (with C 3 =
0), the norm
· a in ( 3.28 )
is equivalent to the energy-norm
· V . Thus, we see from ( 3.44 ) that we have
u M
u N V = O
+
k) , i.e. first order convergence in the energy norm, provided
the solution u(t, x) is sufficiently smooth. However, one can also prove second order
convergence in the L 2 -norm, i.e.
(h
u M
u N L 2 (G) = O
(h 2
+
k) ,if θ
∈[
0 , 1
]\{
1 / 2
}
,
u M
u N L 2 (G) = O
(h 2
k 2 ) if θ
and
1 / 2. Hence, for continuous, linear fi-
nite elements, we obtain the same convergence rates as for the finite difference dis-
cretization in Theorem 2.3.8.
+
=
The proof of Theorem 3.6.5 will be given in several steps. We define e N :=
u m
u N
I N denotes nodal interpolant de-
fined in ( 3.24 ). Since we already estimated the consistency error η m
and consider the splitting ( 3.34 ), where now
u m
I N u m ,
=
we focus on ξ N
V N .
ξ N } m are solutions of the θ -scheme :
C 1 (J
Lemma 3.6.7 If u
;
H) , the errors
{
Given ξ N := I N u 0
u 0 N , for m
1 find ξ m + 1
N
=
0 ,...,M
V N such that
v N
V N :
ξ N ,v N ) + a θξ m + 1
θ)ξ N ,v N = (r m ,v N )
k 1 m + 1
N
+ ( 1
(3.45)
N
where the residuals r m
= r 1
+ r 2
+ r 3
are given by
= k 1 (u m + 1
u m + θ ,v N ,
(r 1 ,v N )
u m )
−˙
= k 1 (
u m ), v N ,
I N u m + 1
k 1 (u m + 1
(r 2 ,v N )
I N u m )
(r 3 ,v N )
I N u m + θ
u m + θ ,v N ).
=
a(
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