Help naca 0012

Hi all,

I need some help. This should be trivial but I've been doing battle with my cad software for days and just can't seem to get there.

I want a table of offsets every 100 mm for a naca 0012 or similar 1 meter long and (obviously) 120 wide. Can someone help me out ?

Every package I have that I can create the curve I can't get the dimensions. Every package I have that I can force the dimensions I can't create or import the curve.

I'm making a mould to make some floats for my rowing shell (trainer wheels), so it will be a trimaran...manadatory multihull content

Thank you in advance.

 

Maybe post it in hydrodynamics and aerodynamics ?

 

Maybe these data are useful for you :

 

Try this :
Airfoil plotter (n63412-il) http://www.airfoiltools.com/plotter/index
you can generate .csv plot files

 

The formulation and its coefficients for the 4 digits Naca airfoil is given in this NASA document , page 3 :
https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19970008124.pdf

 

Thank you, I knew there had to be a simple solution.