I feel kind of silly asking this seeing as how the KR-2S is a well proven design and all, however; I read on another site (can't remember where) that he was a little unsure of the torsional strength of the KR-2S wing due to the skin only being glued to the spars. Like I said, I know the design it quite well proven, but has anyone got any figures or engineering data to show just how much strength is really there?
Side note- I'm really enjoying reading the old posts here. Lots of good info and it's nice to find a group not afraid to really live up to the EXPERIMENTAL placard :) -Todd
