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TABLE 4.3
Transfer Matrix for a Beam Element, Part a:
Definitions:
k )/
λ =
k
/
EI ,
η =
k
/(
k s GA
)
,
ζ = (
N
EI
Sign Convention 1
e 1 + ζ
e 3
e 2
e 4 /
EI
+ (
e 2 + ζ
e 4 )/
k s GA
e 3 /
EI
λ
e 4
e 1 η
e 3
e 3 /
EI
(
e 2 η
e 4 )/
EI
U i
=
λ
EI
(
e 2 + ζ
e 4 ) λ
EIe 3
e 1 + ζ
e 3
λ
e 4
λ
EIe 3
EI
(
e 0 η
e 2 )
e 2
e 1 η
e 3
0
b
w
w
V
M
0
b
V b
M b
θ
U i z a +
z i
z i
z b =
z
=
=
p a e 5 + p
p
w
0
b
= (
e 6 +
m a e 4 + m
e 5 )/
p a (
e 3 + ζ
e 5 )/
(
e 4 + ζ
e 6 )/
EI
k s GA
k s GA
M Ta e 3 + M T
(
e 4 )/
;
EI
[ p a e 4 + p
θ
0
b
=−
e 5 +
m a (
e 3 η
e 5 ) + m
(
e 4 η
e 6 )
/
+
[ M Ta (
e 2 η
e 4 )
]
EI
+ M T
(
e 3 η
e 5 )
]
/
EI
;
e 4 ) p
e 4 M T
V b =−
m a e 5 + m
p a (
e 2 + ζ
(
e 3 + ζ
e 5 ) + λ(
e 6 )
M Ta λ
λ
e 5 ;
p a e 3 p
M b =−
e 4 ) m
e 4
m a (
e 2 η
(
e 3 η
e 5 ) +
M Ta (
e 1
1
η
e 3 )
+ M T
(
e 2 η
e 4 )
M Tb
M Ta
p
=
p b
p a
m b
m a
M T
m
=
=
b
a
b
a
b
a
p a
is the magnitude of the distributed applied force at x
=
a (force/length).
m a
is the magnitude of the distributed applied moment at x
=
a (force-length/length).
p
is the gradient of the distributed applied force, linearly varying in the x direction
(force/length 2 ).
m
is the gradient of the distributed applied moment, linearly varying in the x direction
(force-length/length 2 ).
k s
is the shear form factor.
is the Winkler (elastic) foundation modulus (force/length 2 ).
k
k
is the rotary foundation modulus (force-length/length).
N
is a compressive axial force.
E
is the modulus of elasticity of the material.
I
is the moment of inertia taken about the neutral axis.
G
is the shear modulus of elasticity.
A
is the cross-sectional area.
M Ta
is the magnitude of the distributed thermal moment at x
=
a
.
M T /
is the gradient of the thermal moment, linearly varying in the x -direction. The moment
is defined as follows:
M T =
E
α
TzdA
A
where
T is the temperature change and
α
is the coefficient of thermal expansion.
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