The stress formula from the Zick analysis looks something like this:
S =-Q/(4*t*(b+1.56*Sqr(Ro*t)))-3*K*Q/(2*t2)
Assuming that you are fixed for most variables such as:
shell thickness, t
shell radius, R
saddle load, Q
That means you can fiddle with the saddle width, b, and the saddle and wear plate angle in order to affect Zick factor K. So if you increase the saddle width and/or increase the saddle and wear plate angles you should be able to reduce the calculated stress.
If this step doesn't reduce the stress sufficiently (and it seems like you have a long way to go to get this stress down) then you'll have to try adding a stiffener ring, or move the saddles closer to the heads so they act as stiffeners, or increase the thickness of the shell.