n64012a Airfoil

NACA 64(1)-012A airfoil

n64012a Airfoil (x,y) Coordinates

0 0
0.005 0.00961
0.0075 0.01158
0.0125 0.01464
0.025 0.02018
0.05 0.02788
0.075 0.03364
0.1 0.03839
0.15 0.0458
0.2 0.05132
0.25 0.05534
0.3 0.05809
0.35 0.05965
0.4 0.05993
0.45 0.05863
0.5 0.05605
0.55 0.05244
0.6 0.04801
0.65 0.04289
0.7 0.03721
0.75 0.03118
0.8 0.025
0.85 0.01882
0.9 0.01263
0.95 0.00644
1 0.00025
0.95 -0.00644
0.9 -0.01263
0.85 -0.01882
0.8 -0.025
0.75 -0.03118
0.7 -0.03721
0.65 -0.04289
0.6 -0.04801
0.55 -0.05244
0.5 -0.05605
0.45 -0.05863
0.4 -0.05993
0.35 -0.05965
0.3 -0.05809
0.25 -0.05534
0.2 -0.05132
0.15 -0.0458
0.1 -0.03839
0.075 -0.03364
0.05 -0.02788
0.025 -0.02018
0.0125 -0.01464
0.0075 -0.01158
0.005 -0.00961
0 0

n64012a Airfoil CAD files

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