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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