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1
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commandotom
Materials
- Oct 27, 2012
- 4
Seems like I've been chasing my tail through the code or may be it's just that I can't quite see the forest for the trees. I'd like to be able to determine the Maxmum Allowable Stress for the following.
SA-264; 20% SA-240 316 on SA 285 backing, Specified Tensile strength; 55K. Nominal thickness 0.375", Temp. 600. Ultimately I'll be using the stress to calculate the min. thickness for the heads and shell.
I've been through UCL-11 and UCL-23(c) seems like I get close but just can't quite get to where I need to be. New to this site. Sure hope someone can set me on the right course. Many Thanks in advance.
SA-264; 20% SA-240 316 on SA 285 backing, Specified Tensile strength; 55K. Nominal thickness 0.375", Temp. 600. Ultimately I'll be using the stress to calculate the min. thickness for the heads and shell.
I've been through UCL-11 and UCL-23(c) seems like I get close but just can't quite get to where I need to be. New to this site. Sure hope someone can set me on the right course. Many Thanks in advance.