The ASME Code requirements for the shell and stiffener ring are loosely related through the required shell thickness, "t". However, there is no strict relationship when investigating the MAEP of each component.
The requirement for the shell (UG-28) based on external pressure is for a minimum thickness based on the parameters L, Do, and t (length between lines of support, outside diameter, and nominal thickness of the shell). (And, of course, the material and design temperature.)
The requirement for the stiffener ring (UG-29) is for a minimum moment of inertia based on the shell thickness required for the given pressure.
The MAEP of the shell can be found using the Code rules of UG-28. Typically when doing these calculations by hand a nominal thickness is assumed, then the maximum pressure rating is determined by rules of this paragraph, thus obtaining the shell MAEP. Given enough time and paper, one could "back calculate" the required thickness to just meet the design pressure, thus coming up with the required thickness. COMPRESS does this automatically and reports both the thickness required for the design pressure and the MAEP based on the nominal thickness.
As discussed previously, in "Design" calculation mode COMPRESS calculates the required stiffener ring moment of inertia based on the required thickness of shell for the design external pressure.
In "Rating" calculation mode COMPRESS determines the MAEP of the combined ring-shell section. This can be limited by either of the following:
a) The available shell thickness may limit the ring MAEP. In this case, the thickness required for the ring MAEP is equal to the full shell thickness; this is the thickness applied in the calculation for required moment of inertia.
b) The shell thickness does not limit the ring MAEP. In this case, the required thickness applied in the calculation for required moment of inertia is the thickness required for the ring MAEP.
Tom Barsh
Codeware Technical Support