Brief Description: Wing redesigned for correct airfoils
Redesigned wing for correct dimensions of NACA 0016 airfoils - equation-driven spline curves per NACA 0016 formula - several errors in SW sketches need to be corrected (i.e. WS 60 & 108) - aileron ribs included to maintain profile
Need to taper LE Need to finish TE at root & tip Need to include AIleron spars & v-ribs
