Hi Guys, is there anyone who could help me design an optimum wing aerofoil section for a small pylon class we run in the uk called club 2000, its effectivlly a scaled down version to Q500.

Ive been looking through thease threads on aerodynamics, flow sections, laminer seperation, high reynolds no, etc and im afraid im a complte fish out of water in understanding all of the above, ive tried but its a bit like chucking me in the space shuttle with every warning light on red and 30 seconds to impact.


I can supply all the other info, weight, speed etc..............Hopeing someone can help

Many thanks

Darren