Generating an airfoil wing from a cross-sectional profile at the base and rails defined by the wing's intended leading and trailing edges

 From:  scarab (SPUNAR)
10361.2 In reply to 10361.1 
Hello LarryV,
try to improve your curves, as they have a lot of segments. You need as smooth curve as possible. In this simple design there are sharp leading & trailing edges of your wing, so simple mirroring of upper surface and lower surface can be used. I have used only curves from your model. Sweep command with tangency work quite easily.