The rupture of the member when the net c/s member reaches ultimate stress

Plates- Tdn=$\frac{0.9Anfu}{\gamma m l}$

Single Angles -Tdn=$\frac{0.9 Axfu}{\gamma ml}+\frac{\beta.Agofy}{\gamma mo}$

$\frac{Gross \ section}{Tdg}=\frac{Agfy}{\gamma mo}$

block shear-Segment of block of material at the end of member shear act due to the possible use of high bearing …