Glenn,
I think it would be better for you to consult your senior engineer, and read the UKOOA code specifically chapter 3 of part3.
UKOOA's code:
PDm/4t < f1f2f3*LTHP
for anisotropic material: f3=1-(2Sab/r*f1*LTHS), this factor involves the relation between pressure induced axial stress and pressure induced hoop stres, which means 50% of avaliable axial strength is available for additional loadings.
Thus, CAESAR uses:
Sab(f2/r) + PDm/4t < f1f2LTHS/2.0 (you can derive this by using simple equations from the code)
For the rest, you have to read the text.
Goodluck!
Edited by ichigo (11/25/08 05:37 PM)