Computer Aided Design of a wing.

For any of you Aero boffs out there. I need help with designing a wproject. This is probably in the wrong forum here but since i have browsed this forum for years and years; and respect the fact that there is a lot of knowledge within this forum in aerospace related topics, ive decided il post it here anyway. Id really appreciate it if any of you could help me with the dimensions of the wing for a subsonic glider. designed to fly at 10 m/s with a co-efficient of lift = 0.8. density of the atmosphere being 1.225. mass of the wing = 0.2 kg. it would be great if i could come up with a wing that develops a lift force greater than (0.2*9.81) N. The higher the lift the better. Its a constant cord wing, so its not tapered. Any values on chord vs wingspan would be greatly appreciated. Diagrams would help aswell if your prepared to help. Also I need help with the chamber height of the wing. Thanks in advance!
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Sick from wellbutrin