A beam of rectangular cross-section is welded to a support by means of fillet welds as shown in Fig. 8.34. Determine the size of the welds, if the permissible shear stress in the weld is limited to 75 N/mm².
A beam of rectangular cross-section is welded to a support by means of fillet welds as shown in Fig. 8.34. Determine the size of the welds, if the permissible shear stress in the weld is limited to 75 N/mm².
\text { Given } P=25 kN \quad \tau=75 N / mm ^{2} .
Step I Primary shear stress
The total area of the horizontal and vertical welds is given by
A=2[100 t+150 t]=(500 t) mm ^{2} .
The primary shear stress in the welds is given by
\tau_{1}=\frac{P}{A}=\frac{25000}{(500 t)}=\left(\frac{50}{t}\right) N / mm ^{2} (i).
Step II Bending stress
Referring to Fig. 8.35, the moment of inertia of four welds about the X-axis is given by
I_{x x}=2\left[\frac{b t^{3}}{12}+(b t) \times\left(\frac{d}{2}\right)^{2}\right]+2\left[\frac{t d^{3}}{12}\right] .
Assuming b and d to be large as compared to the throat dimension t and neglecting the terms containing t³, we have
I_{x x}=t\left[\frac{b d^{2}}{2}+\frac{d^{3}}{6}\right] .
Substituting the values,
I_{x x}=t\left[\frac{(100)(150)^{2}}{2}+\frac{(150)^{3}}{6}\right]=\left[(75)(150)^{2}\right] t mm ^{4} .
From Eq. (8.28),
\sigma_{b}=\frac{M_{b} y}{I} (8.28).
\sigma_{b}=\frac{M_{b} y}{I}=\frac{(25000 \times 500)(75)}{(75)(150)^{2} t} .
=\left(\frac{555.55}{t}\right) N / mm ^{2} (ii).
Step III Maximum shear stress
From Eq. (8.29), the maximum shear stress in the weld is given by,
\tau=\sqrt{\left(\frac{\sigma_{b}}{2}\right)^{2}+\left(\tau_{1}\right)^{2}}=\sqrt{\left(\frac{555.55}{2 t}\right)^{2}+\left(\frac{50}{t}\right)^{2}} .
=\frac{282.24}{t} N / mm ^{2} .
Step IV Size of weld
Since the permissible shear stress in the weld is 75 N/mm².
\left(\frac{282.24}{t}\right)=75 \quad \text { or } \quad t=3.76 mm .
\text { and } \quad h=\frac{t}{0.707}=\frac{3.76}{0.707}=5.32 \cong 6 mm .