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N 0 , the fa-
Based on the assumption that N is taken from the first order analysis N
miliar
second
order
theory
is
obtained.
The
internal
virtual
work
then
becomes
(Wunderlich, 1976)
u EAu + δw N 0
w + δw EI
w )
δ
W i =
dx
.
u
···
w
x δ
x dEAd x
0
.
u T
=
dx
(11.56)
······
······
.
x dN 0 d x
x d 2 EId x
0
+
k D
u
w with
w + w 0 .
To include the effect of imperfections, replace
The external virtual work is
given by
N 0
w 0 δw +
κδθ )
] b
δ
W e
=
(
p x δ
u
+
p z δw
EI
dx
[ V
δw +
M
δθ
(11.57)
Horizontal
Vertical
Imperfections
Imposed
Concentrated Loads
Distributed
Distributed
Curvature
at the Boundaries
Load
Load
For the conditions of equilibrium to hold,
δ
W
=− δ
W i
δ
W e
=
0
(11.58)
with the internal virtual work of Eq. (11.56) and the external virtual work from Eq. (11.57).
If shear deformation is taken into account, the internal virtual work relationship would
appear as (Chapter 2, Example 2.7).
.
.
x dEAd x
u
········· ······
·········
······
······
x δ
x dN 0 d x
.
.
x dk s GA
δ
W
=
[ u
]
w
dx
=
0
+ x dk s GAd x
······
······
······
······
······
x dEId x
.
.
θ
k s GAd x
+
k s GA
(11.59)
where N 0
0 for tensile axial forces. This expression is applied in Example 11.12, where an
appropriate bifurcation load is found with and without consideration of shear deformation.
>
11.3.2
Beam Element Matrices (Theory of Second Order)
The principle of virtual work can also be used to generate the element stiffness matri-
ces for stability analyses. For a beam the principle of virtual work takes the form of
Eq. (11.58) with the extension term deleted. With the introduction of the shape function
w =
=
N u Gv
Nv , the element contribution for an element of length
with compressive
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