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1.0
0.8
0.2
0.5
0.6
1.0
0.4
2.0
0.2
N cr,z / N cr,T = 5.0
0
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0
M cr,MN / M zx
Figure 7.14 Elastic buckling load combinations for beam-columns with equal end moments.
sothat ( 1 N cr , MN / N cr , T )>( 1 N cr , MN / N cr , z )( 1 N cr , MN / N cr , y ) .Inthiscase,
equation 7.39 can be safely approximated by the interaction equation
N cr , MN
N cr , z
1
( 1 N cr , MN / N cr , y )
M cr , MN
M zx
+
= 1.
(7.40)
7.3.1.2 Beam-columns with unequal end moments
The elastic flexural-torsional buckling of simply supported beam-columns with
unequal major axis end moments M and β m M has been investigated numerically,
and many solutions are available [7-11].The conservative interaction equation
2
M / F
M E
N
N cr , z
+
= 1
(7.41)
has also been proposed [9], in which
M E = π 2 EI z GI t / L 2 . (7.42)
Thefactor1/ F inequation7.41varieswiththeendmomentratio β m asshownin
Figure7.15,andallowstheunequalendmomentstobetreatedasequivalentequal
end moments M / F . Thus the elastic buckling of beam-columns with unequal
end moments can also be approximated by modifying equation 7.35 to
( M cr , MN / F ) 2
M zx
1 N cr , MN
N cr , T
1 N cr , MN
N cr , z
=
,
(7.43)
or by a similar modification of equation 7.40.
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