Civil Engineering Reference
In-Depth Information
x
L
f
z
y
Figure 3.24
Torsional buckling of a cruciform section.
Acompression member of doubly symmetric cross-section may buckle elasti-
cally by twisting at a torsional buckling load (see Section 3.11) given by
GI
t
+
π
2
EI
w
L
cr
,
T
N
cr
,
T
=
1
i
0
(3.54)
in which
GI
t
and
EI
w
are the torsional and warping rigidities (see Chapter 10),
L
cr
,
T
is the distance between inflexion points of the twisted shape, and
i
0
=
i
p
+
y
0
+
z
0
(3.55)
in which
y
0
,
z
0
are the shear centre coordinates (which are zero for doubly
symmetric sections, see Section 5.4.3), and
i
p
=
√
{
(
I
y
+
I
z
)/
A
}
(3.56)
is the polar radius of gyration. For most rolled steel sections, the minor axis
buckling load
N
cr
,
z
is less than
N
cr
,
T
, and the possibility of torsional buckling
can be ignored. However, short members which have low torsional and warping
rigidities (such as thin-walled cruciforms) should be checked. Such members can
bedesignedbyusingFigure3.23withthevalueof
N
cr
,
T
substitutedfortheelastic
buckling load
N
cr
.
Monosymmetric and asymmetric section members (such as thin-walled tees
and angles) may buckle in a combined mode by twisting and deflecting. This
action takes place because the axis of twist through the shear centre does not
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