n6400a Airfoil

NACA 64-008A airfoil

n64008a Airfoil (x,y) Coordinates

0 0
0.005 0.00646
0.0075 0.00778
0.0125 0.00983
0.025 0.01353
0.05 0.01863
0.075 0.02245
0.1 0.02559
0.15 0.03047
0.2 0.03414
0.25 0.03681
0.3 0.03866
0.35 0.03972
0.4 0.03998
0.45 0.03921
0.5 0.03757
0.55 0.03524
0.6 0.03234
0.65 0.02897
0.7 0.02521
0.75 0.02117
0.8 0.01698
0.85 0.01278
0.9 0.00858
0.95 0.00438
1 0.00018
0.95 -0.00438
0.9 -0.00858
0.85 -0.01278
0.8 -0.01698
0.75 -0.02117
0.7 -0.02521
0.65 -0.02897
0.6 -0.03234
0.55 -0.03524
0.5 -0.03757
0.45 -0.03921
0.4 -0.03998
0.35 -0.03972
0.3 -0.03866
0.25 -0.03681
0.2 -0.03414
0.15 -0.03047
0.1 -0.02559
0.075 -0.02245
0.05 -0.01863
0.025 -0.01353
0.0125 -0.00983
0.0075 -0.00778
0.005 -0.00646
0 0

n64008a Airfoil CAD files

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