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H 0 (G) , and if V N =
S 1
T
Ch 2 as h
V =
, we obtain λ A
0. Hence, we get stabil-
ity provided the CFL type stability condition
θ< 1
2
Ch 2 /( 1
k
2 θ),
0
1
holds. For
2
θ
1, the θ -scheme is stable without any time step restriction.
3.6 Error Estimates
Let u m (x)
u(t m ,x) , u N
=
be as in ( 3.14 ) and assume V N consists of linear finite
S 1
T
elements, i.e. V N
=
.For m
=
0 ,...,M
1, we want to estimate the error
e N (x)
u m (x)
u N (x) . Therefore, we split the error
e N = (u m
:=
I N u m ) + ( I N u m
u N ) =: η m
+ ξ N ,
(3.34)
where
I N :
V
V N is the interpolant as defined in ( 3.24 ). For a fixed time point
t m , η m (x)
=
u(t m ,x)
(
I N u)(t m ,x)
V is a consistency error for which we now
give an error estimate.
3.6.1 Finite Element Interpolation
We prove error estimates of the interpolation error u
I N u .
Proposition 3.6.1 Let
I N : V V N be the interpolant as defined in ( 3.24 ). Then ,
the following error estimates hold :
N +
1
h 2 ( n)
i
I N u) (n)
2
u ()
2
(u
L 2 (G)
C
L 2 (K i ) ,n
=
0 , 1 ,
=
1 , 2 .
(3.35)
i =
1
In particular , if the mesh is uniform , i . e . h i =
h ,
Ch n
I N u) (n)
u ()
(u
L 2 (G)
L 2 (G) ,n
=
0 , 1 ,
=
1 , 2 .
(3.36)
u c H 1 (G) for c = 1
Proof Consider G = ( 0 , 1 ) and
u H 2 (G) . Then,
0 u .
By the Poincaré inequality ( 3.4 ), which also holds for the space H 1 (G) (see ( 3.5 )),
u c L 2 (G) C u L 2 (G) .
(3.37)
With
x
I N
u
:=
u( 0 )
+
c d x
=
u( 0 )
+
cx,
0
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