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We know that the displacements at
Now, we
have three equations for five unknowns. Two additional conditions will be required. Recall
that the static boundary conditions are M
ξ =
0 and 1 must be zero. Thus, u 0
=
u 4
=
0
.
0or u 0 =
u 4 =
=
0
) =
M
=
1
) =
0
.
The
central difference expressions are
u 0 = (
h 2
1
/
)(
u
2 u 0 +
u 1 )
1
(27)
u 4 = (
h 2
1
/
)(
u 3
2 u 4 +
u 5 )
Since u 0 =
u 4 =
u 0
=
u 4
=
0 , (27) gives
u
=−
u 1
and
u 5 =−
u 3
(28)
1
Now (26) provides three equations for the three unknowns u 1 ,u 2 , and u 3
.
The somewhat cumbersome treatment of the fictitious node points can be avoided by
using forward and backward difference expressions near the boundary. Thus, if we use
(Table 8.1)
u 1 = (
12 h 2
1
/
)(
11 u 0
20 u 1 +
6 u 2 +
4 u 3
u 4 )
(29a)
for i
=
1 of (26), and
u 3 = (
12 h 2
1
/
)(
u 0 +
4 u 1 +
6 u 2
20 u 3 +
11 u 4 )
(29b)
for i
=
3 of (26), then no nodes occur beyond the ends of the beam. In this case, with
u 0
0 , we again have three equations for three unknowns.
From (28) and (26), we obtain the stiffness-like equations
=
u 4
=
29
16
1
u 1
u 2
u 3
0
.
1125
=−
16
30
16
0
.
1250
1 6
29
0
.
08035
(30)
K
U
=
P
which have the solutions
u 1
=
0
.
013183 ,
2
=
0
.
017617 ,
3
=
0
.
012033
(31)
These correspond to errors of 0.27%, 0.095%, and 0.086%, respectively. This is a significant
improvement over the use of the simple central difference formula for M
.
The better results of the improved difference expression of a higher order scheme are to
be expected, since the error is 0
=
4
h 4
h 2
).
For an arbitrary M, the higher order difference technique, using the central difference
expression (25), provides the general expression
(
)
, while that for the simple central difference is 0
(
M 3
u i 2 +
16 u i 1
30 u i +
16 u i + 1
u i + 2 =−
12 i
(
M
i
)/
(
M
+
i
)
(32)
This will lead to a banded matrix of bandwidth 5.
Multiple Position Difference Method
Choose from Table 8.2 the multiple difference expression for the second derivative
12
h 2 (
u i 1 +
10 u i +
u i + 1 =
u i 1
2 u i
+
u i + 1
)
(33)
Choose four subdivisions (Fig. 8.5b) so that M
=
4 ,h
=
1
/
4 , and
ξ
=
i
/
4
.
From (33),
i
u 0 +
10 u 1 +
u 2 = (
i
=
1:
12
)(
16
)(
u 0
2 u 1 +
u 2 )
u 1 +
10 u 2 +
u 3 = (
i
=
2:
12
)(
16
)(
u 1
2 u 2 +
u 3 )
(34)
u 2 +
10 u 3 +
u 4 = (
i
=
3:
12
)(
16
)(
u 2
2 u 3 +
u 4 )
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