n63412 Airfoil

NACA 63(1)-412 airfoil

n63412 Airfoil (x,y) Coordinates

0 0
0.00336 0.01071
0.00567 0.0132
0.01041 0.01719
0.02257 0.0246
0.04727 0.03544
0.07218 0.04379
0.09718 0.05063
0.14735 0.06138
0.19765 0.06929
0.248 0.07499
0.2984 0.07872
0.34882 0.08059
0.39924 0.08062
0.44964 0.07894
0.5 0.07567
0.55031 0.07125
0.60057 0.06562
0.65076 0.05899
0.70087 0.05153
0.75089 0.04344
0.80084 0.03492
0.8507 0.02618
0.90049 0.01739
0.95023 0.00881
1 0
0.94977 0.0033
0.89951 0.00329
0.8493 0.00074
0.79916 -0.00308
0.74911 -0.00764
0.69913 -0.01265
0.64924 -0.01799
0.59943 -0.02278
0.54969 -0.02745
0.5 -0.03164
0.45035 -0.03514
0.40076 -0.03778
0.351118 -0.03939
0.3016 -0.03984
0.252 -0.03919
0.20235 -0.03745
0.15265 -0.03446
0.10282 -0.02995
0.07782 -0.02685
0.05273 -0.0228
0.02743 -0.01716
0.01459 -0.01291
0.00933 -0.0104
0.00664 -0.00871
0 0

n63412 Airfoil CAD files

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