Civil Engineering Reference
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s
2
a
s
1
La
w
2
V
Tz
L
2
V
Ty
La
w
2
V
Ty
2
V
L
Throat
2
V
L
V
Ty
2
V
Tz
V
L
V
Tz
(a) Connection
(b) Part weld
Figure 9.21
Fillet welded joint.
weld is reached when
√
σ
w
+
3
τ
w
=
f
uw
(9.25)
in which
f
uw
is the ultimate tensile strength of the weld, which is assumed to be
greaterthanthatoftheplate.Thisequationissimilartoequation1.1usedinSection
1.3.1 to express the distortion energy theory for yield under combined stresses.
Substituting equations 9.23 and 9.24 into equation 9.25 and rearranging leads to
−
2
V
Ty
sin
α
+
V
Tz
cos
α
2
=
(
f
uw
La
)
2
.
V
Ty
+
V
Tz
+
V
L
3
(9.26)
This is often simplified conservatively to
V
R
La
=
f
u
√
3
(9.27)
in which
V
R
is the vector resultant
V
Ty
+
V
Tz
+
V
L
V
R
=
(9.28)
of the applied forces
V
Ty
,
V
Tz
, and
V
L
.
In the simple design method of EC3-1-8 [1] based on equations 9.27 and 9.28,
thedesignweldforces
F
Ty
,
Ed
,
F
Tz
,
Ed
,and
F
L
,
Ed
perunitlengthduetothefactored
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