Civil Engineering Reference
In-Depth Information
Load
N
N
u
Strain-hardening
Fracture
N
pl
E
,
A
N
N
Plastic
L
e
Elastic
Not to scale
Axial extension
e
(b) Axial extension
e
e
y
e
st
(a) Tension member
Figure 2.1
Load-extension behaviour of a perfect tension member.
samewayasdoestheaveragestrain
ε
=
e
/
L
withtheaveragestress
σ
=
N
/
A
,and
sotheload-extensionrelationshipforthemembershowninFigure2.1bissimilar
to the material stress-strain relationship shown in Figure 1.6. Thus the extension
at first increases linearly with the load and is equal to
e
=
NL
EA
,
(2.1)
where
E
is theYoung's modulus of elasticity. This linear increase continues until
the yield stress
f
y
of the steel is reached at the general yield load
N
pl
=
Af
y
(2.2)
whentheextensionincreaseswithlittleornoincreaseinloaduntilstrain-hardening
commences.After this, the load increases slowly until the maximum value
N
u
=
Af
u
(2.3)
is reached, in which
f
u
is the ultimate tensile strength of the steel. Beyond this,
a local cross-section of the member necks down and the load
N
decreases until
fracture occurs.
Thebehaviourofthetensionmemberisdescribedasductile,inthatitcanreach
and sustain the general yield load while significant extensions occur, before it
fractures. The general yield load
N
pl
is often taken as the load capacity of the
member.
Ifthetensionmemberisnotinitiallystressfree,buthasasetofresidualstresses
induced during its manufacture such as that shown in Figure 2.2b, then local
yieldingcommencesbeforethegeneralyieldload
N
pl
isreached(Figure2.2c),and
the range over which the load-extension behaviour is linear decreases. However,
the general yield load
N
pl
at which the whole cross-section is yielded can still
be reached because the early yielding causes a redistribution of the stresses. The
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