Civil Engineering Reference
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of
α
to them.The design buckling resistance
N
b
,
Rd
is then given by
N
b
,
Rd
=
χ
N
y
/γ
M
1
(3.22)
inwhich
γ
M
1
isthepartialfactorformemberinstability,whichhasarecommended
value of 1.0 in EC3.
The dimensionless compressive design buckling resistances
N
b
,
Rd
/
N
y
for
α
=
0.13, 0.21, 0.34, 0.49, and 0.76, which represent the EC3 compression member
curves(a
0
),(a),(b),(c),and(d),respectively,areshowninFigure3.13.Members
with higher initial crookedness have lower strengths due to premature yielding,
andtheseareassociatedwithhighervaluesof
α
.Ontheotherhand,memberswith
lower initial crookedness are not as greatly affected by premature yielding, and
have lower values of
α
assigned to them.
3.5.2 Elastic buckling load
Althoughthedesignbucklingresistance
N
b
,
Rd
givenbyequation3.22wasderived
byusingtheexpressionfortheelasticbucklingload
N
cr
givenbyequation3.2fora
pin-endedcompressionmember,equation3.22isalsousedforothercompression
members by generalising equation 3.2 to
N
cr
=
π
2
EI
/
L
cr
(3.23)
in which
L
cr
is the effective length (referred to as the buckling length in EC3).
The elastic buckling load
N
cr
varies with the member geometry, loading, and
restraints,butthereisnoguidancegiveninEC3fordeterminingeither
N
cr
or
L
cr
.
Section3.6followingsummarisesmethodsofdeterminingtheeffectsofrestraints
ontheeffectivelength
L
cr
,whileSection3.7discussesthedesignofcompression
members with variable sections or loading.
3.5.3 Effects of local buckling
Compression members containing thin-plate elements are likely to be affected by
local buckling of the cross-section (see Chapter 4). Local buckling reduces the
resistances of short compression members below their squash loads
N
y
and the
resistances of longer members which fail by flexural buckling.
Local buckling of a short compression member is accounted for by using a
reducedeffectivearea
A
eff
insteadofthegrossarea
A
,asdiscussedinSection4.7.1.
Local buckling of a longer compression member is accounted for by using
A
eff
instead of
A
and by reducing the generalised slenderness to
λ
=
A
eff
f
y
/
N
cr
(3.24)
but using the gross cross-sectional properties to determine
N
cr
.
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