Civil Engineering Reference
In-Depth Information
β m M
1.0
1.0
N
0.8
0.8
0.6
0.6
N
M
N / N cr,z
0.00
0.25
0.50
0.75
0.95
N / N cr,z
0.4
0.4
0.00
0.25
0.50
0.75
0.95
0.2
0.2
(1- )/2
m
m
(1- )/2
-1.0 -0.5
0
0.5 1.0
-1.0 -0.5
0
0.5 1.0
End moment ratio m
2 EI w /GI t L 2 = 0.09
End moment ratio m
(a)
(b)
2 EI w /GI t L 2 =1.0
Figure 7.16 Flexural-torsional buckling coefficients 1 bc in equation 7.45.
7.3.1.3 Beam-columns with elastic end restraints
Theelasticflexural-torsionalbucklingofsymmetricallyrestrainedbeam-columns
with equal and opposite end moments ( β m =− 1) is analysed in Section 7.6.2.
The particular example considered is one for which the minor axis bending and
end warping restraints are equal. This corresponds to the situation in which both
ends of both flanges have equal elastic restraints whose stiffnesses are such that
Flange end moment
Flange end rotation = EI z
R
1 R
(7.47)
L
inwhichtherestraintparameter R variesfrom0(flangeunrestrained)to1(flange
rigidly restrained).
It is shown in Section 7.6.2 that the elastic buckling values M cr , MN and N cr , MN
oftheendmomentsandaxialloadforwhichtherestrainedbeam-columnbuckles
elastically are given by
1 N cr , MN
N cr , z
1 N cr , MN
N cr , T
M cr , MN
i p N cr , z N cr , T =
(7.48)
in which
N cr , z = π 2 EI z / L cr ,
(7.49)
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