In an example problem (wall aspect ratio of 4), using your sheet thickness (t = 2.657 mm), w in my previous post turned out to be too high and should instead be w = 0.116*(1-mu)*rho*a*h^2, where I assumed mu = 0.30 for a solid substance or mu = 0 for water. So that covers the middle rib midspan stress (for this particular sheet thickness).
However, I found that the maximum stress occurs at the midpoint of the bottom edge of the wall, which (in my example problem) turned out to be sigma1 = 0.0830*(1-mu)*rho*a*(h^3)/(t^2).
(Note that both of these results are fairly specific to only the stated sheet thickness, t = 2.657 mm, and probably wouldn't extrapolate to greatly different values of sheet thickness.)
Even though (1-mu)*rho could be refined to obtain a more accurate pressure distribution, what we can get out of this is, the maximum stress occurs at the midpoint of the bottom edge and can be fairly high because it's just a thin sheet there, in the vertical direction, under a relatively high bending moment about the bottom edge.