n64012 Airfoil

NACA 64(1)-012 airfoil

n64012 Airfoil (x,y) Coordinates

0 0
0.005 0.00978
0.0075 0.01179
0.0125 0.0149
0.025 0.02035
0.05 0.0281
0.075 0.03394
0.1 0.03871
0.15 0.0462
0.2 0.05173
0.25 0.05576
0.3 0.05844
0.35 0.05978
0.4 0.05981
0.45 0.05798
0.5 0.0548
0.55 0.05056
0.6 0.04548
0.65 0.03974
0.7 0.0335
0.75 0.02695
0.8 0.02029
0.85 0.01382
0.9 0.00786
0.95 0.00288
1 0
0.95 -0.00288
0.9 -0.00786
0.85 -0.01382
0.8 -0.02029
0.75 -0.02695
0.7 -0.0335
0.65 -0.03974
0.6 -0.04548
0.55 -0.05056
0.5 -0.0548
0.45 -0.05798
0.4 -0.05981
0.35 -0.05978
0.3 -0.05844
0.25 -0.05576
0.2 -0.05173
0.15 -0.0462
0.1 -0.03871
0.075 -0.03394
0.05 -0.0281
0.025 -0.02035
0.0125 -0.0149
0.0075 -0.01179
0.005 -0.00978
0 0

n64012 Airfoil CAD files

DOWNLOAD FROM HERE