Increased CL. to 1.6 max without Flaps. Maintained low CD ~.01, increased wing stiffness and strength. Wings now quickly interchangable, greatly reduced wing flex.. Cut turning radius at increased flight dynamics. Lowered piloting skills required to fly airplane. Improved Lift by increasing wing area by 59%. Steep Climbs now possible. Flight time enhanced. Increased flying speed envelope. Increased weight capacity while lowering landing and stall speeds. Extended range and lowered risk of crashing. Improved stability in windy flying conditions. Lowered Aspect Ratio and CM (moment) of wing - both work to stabilize flight characteristics of the aircraft. .
A Clark-Y or E-205 (Eppler) airfoil selection forms the external shape of the wings. Internally, each wing is undergoing calcs to determine the material composition and structure.
See the pdf file for preliminary information.