I would like to sketch a NACA wing profile into NX. The easiest way would be to create a script that uses a function to sketch the curve for me, altering the thickness over a specified length.
ie.
For x=0:0.01:1
y=(0.2969sqrt(x)-0.126x-0.3516x^2 +0.2843x^3-0.1015x^4)
end
I am using NX 7.5...