n63010a Airfoil

NACA 63-010A airfoil

n63010a Airfoil (x,y) Co-ordinates

0 0
0.005 0.00816
0.0075 0.00983
0.0125 0.0125
0.025 0.01737
0.05 0.02412
0.075 0.02917
0.1 0.03324
0.15 0.0395
0.2 0.044
0.25 0.04714
0.3 0.04913
0.35 0.04995
0.4 0.04968
0.45 0.04837
0.5 0.04613
0.55 0.04311
0.6 0.03943
0.65 0.03517
0.7 0.03044
0.75 0.02545
0.8 0.0204
0.85 0.01535
0.9 0.0103
0.95 0.00525
1 0.00021
0.95 -0.00525
0.9 -0.0103
0.85 -0.01535
0.8 -0.0204
0.75 -0.02545
0.7 -0.03044
0.65 -0.03517
0.6 -0.03943
0.55 -0.04311
0.5 -0.04613
0.45 -0.04837
0.4 -0.04968
0.35 -0.04995
0.3 -0.04913
0.25 -0.04714
0.2 -0.044
0.15 -0.0395
0.1 -0.03324
0.075 -0.02917
0.05 -0.02412
0.025 -0.01737
0.0125 -0.0125
0.0075 -0.00983
0.005 -0.00816
0 0

n63010a Airfoil CAD files

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