n64015

NACA 64(2)-015 airfoil

n64015 Airfoil (x,y) Coordinates

0 0
0.005 0.01208
0.0075 0.01456
0.0125 0.01842
0.025 0.02528
0.05 0.03504
0.075 0.0424
0.1 0.04842
0.15 0.05785
0.2 0.0648
0.25 0.06985
0.3 0.07319
0.35 0.07482
0.4 0.07473
0.45 0.07224
0.5 0.0681
0.55 0.06266
0.6 0.0562
0.65 0.04895
0.7 0.04113
0.75 0.03296
0.8 0.02472
0.85 0.01677
0.9 0.0095
0.95 0.00346
1 0
0.95 -0.00346
0.9 -0.0095
0.85 -0.01677
0.8 -0.02472
0.75 -0.03296
0.7 -0.04113
0.65 -0.04895
0.6 -0.0562
0.55 -0.06266
0.5 -0.0681
0.45 -0.07224
0.4 -0.07473
0.35 -0.07482
0.3 -0.07319
0.25 -0.06985
0.2 -0.0648
0.15 -0.05785
0.1 -0.04842
0.075 -0.0424
0.05 -0.03504
0.025 -0.02528
0.0125 -0.01842
0.0075 -0.01456
0.005 -0.01208
0 0

n64015 Airfoil CAD files

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