How to use the NACA airfoil data profile
usin the direct entery way to deal with NACA airfoil data profile is a nightmare so this is a better and more efficient way to to the job.
Using MS Excel inter the profile data in a worksheet, the profile is a ratio of the wing cord, so you need to multiply the values by the cord to get the real airfoil dimisions.
then copy the resulted values to a new worksheet
Save the worksheet as Tab delimited txt file after omitting any thing but the profile data
In solidworks Start a new part project and go to the Features tab page
choose Curves button then Curve through XYZ points
As the curve File Window popup click Browse button