Civil Engineering Reference
In-Depth Information
Approximationsforthemaximummoments M max inbeam-columnswithtrans-
verse loads can be obtained by using
M max = δ M max ,0
(7.9)
in which M max ,0 is the maximum moment when N = 0,
δ = γ m ( 1 γ s N / N cr )
( 1 γ n N / N cr ) ,
(7.10)
N cr = π 2 EI /( k cr L 2 ) ,
(7.11)
and k cr = L cr / L is the effective length ratio. Expressions for M max ,0 and values
of γ m , γ n , γ s , and k cr are given in Figure 7.5 for beam-columns with central
concentrated loads Q and in Figure 7.6 for beam-columns with uniformly dis-
tributedloads q .Aworkedexampleoftheuseoftheseapproximationsisgivenin
Section 7.7.1.
Themaximumstress σ max inthebeam-columnisthesumoftheaxialstressand
themaximumbendingstresscausedbythemaximummoment M max .Itistherefore
given by
σ max = σ ac + σ bcy M max
M
(7.12)
m
n
s
Beam-column
First-order moment ( N =0)
k
M max , 0
cr
Q
QL
/4
QL
---------
1.0
1.0
1.0 0.18
+
4
L /2
L /2
Q
2.0
1.0
1.0 0.19
QL
-
QL
Q
5
QL
/32
3
QL
+
3
-------- QL
5
6
---------
------
1.0
1.0 0.45
-
16
16
3
QL
/16
L /2
L /2
Q
5
QL
/32
+
3
-------- QL
0.7
1.0
1.0 0.28
-
16
3
QL
/16
L /2
L /2
Q
Q
5
QL
/32
3
-------- QL
+
+
1.0
1.0
0.49 0.14
-
16
L
/2
L /2 L /2 L /2
3
QL
/16
QL
/8
Q
QL
QL
+
QL
---------
---------
1.0
1.0
1.0 0.62
---------
-
-
8
8
8
QL
/8
/8
L /2
L /2
Q
QL
Q L
+
0.5
1.0
1.0
0.18
---------
-
-
8
L /2
L /2
QL
/8
Figure 7.5 Approximations for beam-columns with central concentrated loads.
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