In essence I am trying to make a NACA 0018 aerofoil, with a 50 mm chord 9 mm maximum thickness and 200 mm span.  I was hoping to use a foam core, with around a 0.25/0.5 mm outer carbon fiber skin, to keep the overall mass to a minimum. But this is subject to me finishing my calculations.  My question is how would I go about doing making this design, and would this be a sensible approach.  Would the laminating starter kit below be suitable, or would this be the wrong approach for this application?  I was thinking of wither wrapping the carbon fiber directly around the foam, or making a mould to manufacture the outer skins first.