Civil Engineering Reference
In-Depth Information
This equation states that for equilibrium, the internal moment of resistance
EI
(d
2
v
/d
x
2
) must exactly balance the external disturbing moment
−
N
cr
v
at any
pointalongthelengthofthemember.Whenthisequationissatisfiedatallpoints,
the displaced position is one of equilibrium.
Thesolutionofequation3.58whichsatisfiestheboundaryconditionatthelower
end that
(
v
)
0
=
0is
v
=
δ
sin
π
x
k
cr
L
,
where
1
k
cr
=
N
cr
π
2
EI
/
L
2
,
and
δ
is an undetermined constant. The boundary condition at the upper end that
(
v
)
L
=
0 is satisfied when either
δ
=
0
v
=
0
(3.59)
or
k
cr
=
1
/
n
in which
n
is an integer, so that
N
cr
=
n
2
π
2
EI
/
L
2
,
(3.60)
v
=
δ
sin
n
π
x
/
L
.
(3.61)
The first solution (equations 3.59) defines the straight stable equilibrium position
which is valid for all loads
N
less than the lowest value of
N
cr
, as shown in
Figure 3.2b. The second solution (equations 3.60 and 3.61) defines the buckling
loads
N
cr
atwhichdisplacedequilibriumpositionscanexist.Thissolutiondoesnot
determine the magnitude
δ
of the central deflection, as indicated in Figure 3.2b.
The lowest buckling load is the most important, and this occurs when
n
=
1,
so that
N
cr
=
π
2
EI
/
L
2
,
(3.2)
v
=
δ
sin
π
x
/
L
.
(3.1)
3.8.2 Bending of members with initial curvature
The bending of the compression member with initial curvature shown in
Figure 3.2a can be analysed by considering the differential equilibrium equation
EI
d
2
v
d
x
2
=−
N
(
v
+
v
0
)
,
(3.62)
whichisobtainedfromequation3.58forastraightmemberbyaddingtheadditional
bending moment
−
Nv
0
induced by the initial curvature.
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