Civil Engineering Reference
In-Depth Information
C
N
M
m
M
N
1
+
=
1
1
+
=
N
1
-
N
/
N
M
b
,
y
,
Rd
cr
,
y
pl
N
1-
N
/
N
M
b
,
y
,
Rd
cr
,
y
pl
M
/
M
1.18
(-
N
/
N
)
1
=
pl
y
Analytical solutions
Analytical solutions
1.0
1.0
M
N
L
i ---- =40
y
0.5
0.5
N
m =1
80
120
M
0
-
L
i ---- =120
y
y
y
0
0
0
0.5
1.0
0
0.5
1.0
M/M
M/M pl
pl
(a) Effect of slenderness
(b) Effect of end moment ratio
Figure 7.11 Interaction formulae.
( L / i y 0), and of some members which are not bent in single curvature (i.e.
β m > 0), as shown, for example, in Figure 7.11b.
Equation 7.21 represents the interaction between buckling and bending which
determinestheresistanceofmoreslendermembers.Ifthecaseofequalandoppo-
siteendmomentsisconsideredfirst( β m =− 1and C m = 1),thenitwillbeseenthat
equation7.21includesthesameapproximateamplificationfactor1 /( 1 N / N cr , y )
as does equation 7.7 for the maximum moments in elastic beam-columns. It is of
a similar form to the first yield condition of equation 7.13, except that a conver-
siontoultimateresistancehasbeenmadebyusingtheultimateresistance N b , y , Rd ,
and moment M pl , y instead of the squash load N y and the yield moment M y .These
substitutions ensure that this interaction formula gives the same limit predictions
for concentrically loaded columns ( M = 0) and for beams ( N = 0) as do the
treatments given in Chapters 3 and 5. The accuracy of equation 7.21 for beam-
columns with equal and opposite end moments ( β m =− 1) is demonstrated in
Figure 7.11a.
The effects of unequal end moments ( β m > 1) on the ultimate resistances of
beam-columns are allowed for approximately in equation 7.21 by the coefficient
C m whichconvertstheunequalendmoments M and β m M intoequivalentequaland
oppositeendmoments C m M .Althoughthisconversionisforin-planebehaviour,it
isremarkablysimilartotheconversionusedforbeamswithunequalendmoments
which buckle out of the plane of bending (see Section 6.2.1.2). The accuracy of
equation 7.21 for beam-columns with unequal end moments is demonstrated in
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