n64212ma Airfoil

NACA-NASA/AMES/Hicks 63(1)-212 MOD A airfoil

n64212ma Airfoil (x,y) Coordinates

0 0
0.0017515 0.0139677
0.0048357 0.0209074
0.0088714 0.0263278
0.0138847 0.0315286
0.0188679 0.0352297
0.0288103 0.041432
0.0387467 0.0473345
0.0486491 0.0515373
0.0617421 0.0581767
0.0917591 0.0646775
0.1164151 0.0696854
0.165692 0.075501
0.2149875 0.0788158
0.2642925 0.08113
0.3135933 0.0827444
0.3628836 0.0828386
0.4121608 0.082293
0.4614075 0.0797175
0.5105944 0.0756329
0.5597372 0.0703291
0.6088307 0.0640261
0.6578783 0.0568937
0.7068729 0.0490923
0.7558185 0.0407918
0.8047181 0.032162
0.8535675 0.0234733
0.9023817 0.0149853
0.9511766 0.0070179
1 0
0.9508063 0.0012641
0.9015374 -0.0007209
0.8522694 -0.0041262
0.8030236 -0.0083921
0.7538183 -0.013079
0.7046501 -0.0178766
0.6555237 -0.0225549
0.6064432 -0.0269042
0.5574017 -0.0307641
0.5084032 -0.0339448
0.4594425 -0.036226
0.410535 -0.0373181
0.3616514 -0.0367204
0.3127909 -0.0349728
0.253167 -0.0318697
0.2139372 -0.0296847
0.1747054 -0.0275996
0.1354696 -0.0257145
0.0962359 -0.0237295
0.0570021 -0.0217444
0.032482 -0.0204537
0.0226835 -0.0194576
0.012909 -0.0172616
0.0080518 -0.014664
0.004194 -0.0111861
0.0013356 -0.0068281
0 0

n64212ma Airfoil CAD files

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