This project was a group mission to design a 20 inch long NACA 0012 wing with around 6° of taper. The goal was to make the lightest possible wing that could withstand both static and dynamic load cases. My main role was to manufacture the wing and assist deriving the Rayleigh Ritz deflection code. Unfortunately, the wing kinda sucked, but I blame that on the epoxy saturation, still cool though! Note: If you’re checking this out on mobile, the embedded pdf gets a little sluggish. I suggest just clicking the Download Report PDF button.