Question:
I work in a small sheet metal shop. We make cylindrical vessels (up to 4 ft in radius) that can hold up to a few psi.
The usual formula I use - which was given to me by the chief engineer - for wall thickness is PR/t=stress (Hoop stress) or t=PR/Allowable stress at temperature.
I then throw in about 40-60% extra thickness for a margin of error.
Do I have to add in axial stress (PR/2t) [which is perpendicular] and/or shear?
My understanding is that since hoop stress is the largest, it alone is sufficient.
This is not an ASME shop.
My understanding is that you do not add the hoop, axial, and shear stresses, but but go for the maximum, which in our case is hoop stress.
I work in a small sheet metal shop. We make cylindrical vessels (up to 4 ft in radius) that can hold up to a few psi.
The usual formula I use - which was given to me by the chief engineer - for wall thickness is PR/t=stress (Hoop stress) or t=PR/Allowable stress at temperature.
I then throw in about 40-60% extra thickness for a margin of error.
Do I have to add in axial stress (PR/2t) [which is perpendicular] and/or shear?
My understanding is that since hoop stress is the largest, it alone is sufficient.
This is not an ASME shop.
My understanding is that you do not add the hoop, axial, and shear stresses, but but go for the maximum, which in our case is hoop stress.