privryan84
2nd Nov 2005, 04:42 pm
I want to draw an airfoil for a wing design. Airfoils come is standard shapes by the NACA. The airfoil I want to draw is a NACA 4412. The way the wings are designed is they have a mean line which has an equation based on the chord length or width of the wing and then above and below that mean line there is a thickness distribution also goverened by an equation. This website explains it in more detail: http://www.ae.su.oz.au/aero/naca45/naca45.html
Is it going to be possible to use these equations in AutoCAD 2002 to make the shape?
Is it going to be possible to use these equations in AutoCAD 2002 to make the shape?