n63015a Airfoil

NACA 63-015A airfoil

n63015a Airfoil (x,y) Co-ordinates

0 0
0.005 0.01203
0.0075 0.01448
0.0125 0.01844
0.025 0.02579
0.05 0.03618
0.075 0.04382
0.1 0.04997
0.15 0.05942
0.2 0.06619
0.25 0.07091
0.3 0.07384
0.35 0.07496
0.4 0.07435
0.45 0.07215
0.5 0.06858
0.55 0.06387
0.6 0.0582
0.65 0.05173
0.7 0.04468
0.75 0.03731
0.8 0.02991
0.85 0.02252
0.9 0.01512
0.95 0.00772
1 0.00032
0.95 -0.00772
0.9 -0.01512
0.85 -0.02252
0.8 -0.02991
0.75 -0.03731
0.7 -0.04468
0.65 -0.05173
0.6 -0.0582
0.55 -0.06387
0.5 -0.06858
0.45 -0.07215
0.4 -0.07435
0.35 -0.07496
0.3 -0.07384
0.25 -0.07091
0.2 -0.06619
0.15 -0.05942
0.1 -0.04997
0.075 -0.04382
0.05 -0.03618
0.025 -0.02579
0.0125 -0.01844
0.0075 -0.01448
0.005 -0.01203
0 0

n63015a Airfoil CAD files

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