Civil Engineering Reference
In-Depth Information
a
x
b
N
x
y
Figure 14.4
Simply supported rectangular plate uniformly compressed in one direction.
Thus, the expression for the critical value of the compressive force
N
x,cr
can be simplified as
2
π
2
2
D
1
a
b
N
=
m
+
(14.7)
x cr
,
2
2
a
m
Equation 14.7 with
m
= 1 can be represented in the form
π
2
D
N
=
k
(14.8)
x cr
,
2
a
where
k
is a factor depending on the ratio
a
/
b
and is shown in Figure 14.5
by the curve marked
m
= 1. The critical value of the compressive stress σ
cr
is then given by
2
2
N
h
k E h
b
π
x cr
,
σ
=
=
(14.9)
cr
12 1
(
2
)
2
−
ν
where
h
is the thickness of the plate
a
is the length
b
is the width
m
is the number of half-waves in which the plate buckles have been
determined
14.2.2 linear buckling of steel members
14.2.2.1 Buckling of steel structure members
Steel members in compression in a truss structure have to be analyzed for
buckling loads. Usually buckling becomes a governing criterion in struc-
tures like arched bridges, guyed towers, the top chord of a pony truss, or
any other unbraced compression member.
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