I hoped it would be just that -not just a wild shot at the importance of airfoil design
My new project of the Cassutt racing plane - will use a wing shape that is highly tapered and the airfoil will change from a moderate 12% section to an extremely thin tip of 8-9%
The sections are chosen as a best guess of strength as the taper of each panel is 2-1.
I expect very low wing loading to cover the other results desired
they are
1 strength
2 stiffness
3 rapid shift from lifting to stalled to lifting again
The desired AOA for stall is low (quick flick setups)
The low wing loading on the setup should keep accidental snapping at bay