n64110

NACA 64-110 airfoil

n64110 Airfoil (x,y) Coordinates

0 0
0.00465 0.00844
0.00712 0.01023
0.01207 0.01303
0.0245 0.01793
0.04945 0.025
0.07443 0.03037
0.09944 0.03479
0.14947 0.04178
0.19953 0.047
0.24959 0.05087
0.29967 0.0535
0.34975 0.05495
0.39984 0.05524
0.44992 0.05391
0.5 0.05138
0.55007 0.04786
0.60012 0.04356
0.65016 0.0386
0.70019 0.03313
0.7502 0.02729
0.80019 0.0212
0.85016 0.01512
0.90012 0.00929
0.95006 0.00406
1 0
0.94994 -0.0009
0.89988 -0.00413
0.84984 -0.0084
0.79981 -0.01324
0.7498 -0.01833
0.69981 -0.02341
0.64984 -0.0283
0.59988 -0.03284
0.54993 -0.0369
0.5 -0.04034
0.45008 -0.04295
0.40016 -0.04452
0.35025 -0.04465
0.30033 -0.04378
0.25041 -0.04191
0.20047 -0.03904
0.15053 -0.03506
0.10056 -0.02963
0.07557 -0.02613
0.05055 -0.02184
0.0255 -0.01607
0.01293 -0.01195
0.00788 -0.00953
0.00535 -0.00794
0 0

n64110 Airfoil CAD files

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