Would like to hear comments on generalized characteristics of the e203 airfoil. This is for a combat plane <3lbs, high aspect, 60" ws, 420 sq. in wing. 1 degree of washout built in. I'm looking for a stable, quick turning, relatively high speed (80-90mph), yet non stalling efficient design. 8" root, 5" tip 1 3/16" loft at root with a straight trailing edge.

Ollie, are you out there?

So far, the airfoil is unaltered, straight from the source.