n6409 Airfoil

NACA 6409

n6409 Airfoil (x,y) Coordinates

1 0
0.99732 0.00084
0.9893 0.00333
0.97603 0.00737
0.9576 0.01284
0.93423 0.01954
0.90615 0.02724
0.87357 0.03571
0.8369 0.04464
0.79647 0.05378
0.75272 0.06283
0.70608 0.07153
0.6571 0.07961
0.60627 0.08684
0.55413 0.09302
0.50132 0.09796
0.4484 0.10152
0.3959 0.1036
0.34367 0.10352
0.29315 0.10086
0.24502 0.09584
0.19988 0.08874
0.1583 0.07992
0.1208 0.06982
0.0878 0.05889
0.05968 0.04762
0.03677 0.03646
0.0192 0.02581
0.0072 0.01603
0.0008 0.00737
0 0
0.00467 -0.00573
0.01467 -0.00956
0.02973 -0.01157
0.0497 -0.01192
0.07428 -0.0108
0.10317 -0.00844
0.13607 -0.00513
0.17257 -0.00119
0.21235 0.00307
0.25498 0.00729
0.30012 0.01112
0.3473 0.01425
0.39618 0.01639
0.44707 0.01772
0.49868 0.01871
0.5504 0.01925
0.60167 0.01929
0.65193 0.0188
0.70065 0.0178
0.74728 0.01634
0.7913 0.01451
0.83223 0.01241
0.86957 0.01017
0.90288 0.00791
0.9318 0.00576
0.95593 0.00383
0.97503 0.00221
0.98883 0.00101
0.99722 0.00025
1 0

n6409 Airfoil CAD files

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