n64108 Airfoil

NACA 64-108 airfoil

n64108 Airfoil (x,y) Coordinates

0 0
0.00472 0.00682
0.00719 0.00828
0.01215 0.01058
0.0246 0.01457
0.04956 0.02032
0.07455 0.02471
0.09955 0.02832
0.14958 0.03405
0.19962 0.03835
0.24968 0.04152
0.29974 0.0437
0.3498 0.04494
0.39987 0.04528
0.44994 0.04431
0.5 0.04236
0.55005 0.03959
0.6001 0.03617
0.65013 0.03219
0.70015 0.02777
0.75016 0.02302
0.80015 0.01802
0.85013 0.01297
0.9001 0.00808
0.95005 0.00364
1 0
0.94995 -0.00048
0.8999 -0.00292
0.84987 -0.00625
0.79985 -0.01006
0.74984 -0.01406
0.69985 -0.01805
0.64987 -0.02189
0.5999 -0.02545
0.54995 -0.02863
0.5 -0.03132
0.45006 -0.03335
0.40013 -0.03456
0.3502 -0.03464
0.30026 -0.03398
0.25032 -0.03256
0.20038 -0.03039
0.15042 -0.02733
0.10045 -0.02316
0.07545 -0.02047
0.05044 -0.01716
0.0254 -0.01271
0.01285 -0.0095
0.00781 -0.00758
0.00528 -0.00632
0 0

n64108 Airfoil CAD files

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