Hello, Iām a part of a group trying to assemble the Fun Cub Quad VTOL aircraft. We wanted to know the lift and drag characteristics of the fixed wing plane. If that is not available, does anyone have information about the airfoil section, chord length and span of the wing?
Hi
I and my friends write our thesis about control of fix-wing planes, and we use FunCub as test air-frame.
Part about aerodynamic wrote my friend and is available here https://www.vutbr.cz/www_base/zav_prace_soubor_verejne.php?file_id=82736
unfortunately we wrote in czech language, but if you download package the shut be Matlab/Simulink model with aerodynamic derivatives. Or you can try use translator for full text