Have a look at:
Roark’s Formulas for Stress and Strain 7th ed.
TABLE 11.4 Formulas for flat plates with straight boundaries and constant thickness
Case No. 18: Right-angle isosceles triangle; all edges simply supported
18a: Uniform over entire plate
The equations are quite simple.
i.e. Sigma (max) = 0.262qa^2/t^2 where q is the load, a is the height of the triangle, t thickness.