thread1259-190836
My name is Antonio, I have a doubt concerning to the stress due to internal pressure:
The report mentions the stress at lug edge due to pressure:
Circunferential: P*Ri/t and longitudinal: P*Ri/2t.
In this case: P= 10,02 Kgf/cm²; Ri=1550mm; t(shell)=(16-3,0)=13mm...
