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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