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with
0
1
1
/
k s GA
0
0
0
0
0
0
1
/
EI
A
=
P
=
p z
0
k
0
0
0
0
k
N
1
0
As can be observed in Eq. (4.90b), the loading elements z i can be computed if the
transfer matrix U i is available. Since, for a complete solution, it is necessary only to find
U i , we can set p z equal to zero in Eqs. (4.94) and (4.95).
Thus, we seek to solve the homogeneous differential equations
d z
dx =
Az
(4.96)
The solution can be in the form [Eq. (4.90c)]
U i z 0 =
e A z 0
U i z a
z
=
or
z b =
(4.97)
A function of a square matrix A of order n is equal to a polynomial in A of order n
1
.
Hence, for the 4
×
4 matrix A for a beam,
e A =
2
3
c 0 I
+
c 1 A
+
c 2 (
A
)
+
c 3 (
A
)
(4.98)
The Cayley-Hamilton Theorem (“a matrix satisfies its own characteristic equation”) per-
mits A of Eq. (4.98) to be replaced by its characteristic values
λ i .
Thus,
e λ i =
2
3 ,
c 0 +
c 1 λ i +
c 2 i )
+
c 3 i )
i
=
1 , 2 , 3 , 4
(4.99)
represents four equations that can be solved for the functions c 0 , c 1 , c 2 , and c 3 .
Substitution
of these values into Eq. (4.98) leads to the desired transfer matrix.
To find the characteristic values
λ i , substitute e λ i into the homogeneous first order
governing equations, yielding the characteristic equation
| I λ i A |=
0
(4.100)
With A given by Eq. (4.95)
λ i
1
(
1
/
k s GA
)
0
=
0
λ i
0
(
1
/
EI
)
|
I
λ i
A
|=
0
(4.101)
k
0
λ i
0
(
k
)
λ i
0
N
1
The roots
λ 1 ,
λ 2 ,
λ 3 ,
λ 4 = ( ±
n 1 ,
±
in 2 )
, of this determinant are readily found to be
n 1 , 2 = (((ζ + η)
2
/
λ)
1
/
2
± η)/
)
1
/
2
4
2
(4.102)
where
k )/
λ =
k
/
EI,
η =
k
/(
k s GA
)
,
ζ = (
N
EI
Substitute these characteristic values into Eq. (4.99), giving
e n 1 =
2
3
c 0 +
c 1 n 1 +
c 2 (
n 1 )
+
c 3 (
n 1 )
e n 1 =
2
3
c 0
c 1 n 1 +
c 2 (
n 1 )
c 3 (
n 1 )
(4.103)
e in 2 =
c 0 +
ic 1 n 2
c 2 (
n 2 )
2
ic 3 (
n 2 )
3
e in 2 =
2
3
c 0
ic 1 n 2
c 2 (
n 2 )
+
ic 3 (
n 2 )
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