naca0024 Airfoil

 NACA 0024 airfoil

naca0024 Airfoil (x,y) Coordinates

1 0.00252
0.95 0.01613
0.9 0.02896
0.8 0.05247
0.7 0.07328
0.6 0.09127
0.5 0.10588
0.4 0.11607
0.3 0.12004
0.25 0.11883
0.2 0.11475
0.15 0.10691
0.1 0.09365
0.075 0.084
0.05 0.07109
0.025 0.05229
0.0125 0.03788
0 0
0.0125 -0.03788
0.025 -0.05229
0.05 -0.07109
0.075 -0.084
0.1 -0.09365
0.15 -0.10691
0.2 -0.11475
0.25 -0.11883
0.3 -0.12004
0.4 -0.11607
0.5 -0.10588
0.6 -0.09127
0.7 -0.07328
0.8 -0.05247
0.9 -0.02896
0.95 -0.01613
1 -0.00252

naca0024 Airfoil CAD files

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