s8065 Airfoil

Selig airfoil for Q-40 pylon racing (11%)

s8065 Airfoil (x,y) Co-ordinates

1 0
0.99799345 0.00013081
0.99212025 0.00064886
0.98256076 0.00164927
0.96947079 0.00324812
0.95309102 0.00553995
0.93369244 0.00855997
0.91157321 0.01230522
0.88704959 0.01672247
0.86044882 0.02171353
0.83210011 0.02712528
0.80232754 0.03274588
0.77146147 0.03819146
0.73936403 0.0430992
0.70586712 0.04749618
0.67122309 0.05150364
0.63565123 0.05509625
0.59935637 0.05824451
0.56254033 0.06090266
0.52541205 0.06303144
0.48817588 0.0646042
0.45101815 0.06560211
0.41412023 0.06600298
0.37767163 0.06581018
0.34185932 0.06505252
0.30687944 0.06376417
0.27293839 0.06197182
0.2402362 0.05970469
0.20896727 0.05698898
0.17931487 0.05385452
0.15145325 0.05033324
0.12554665 0.04646182
0.10174937 0.04227597
0.08019908 0.03781531
0.06102294 0.03312597
0.04434007 0.02825462
0.03027875 0.0232372
0.01888699 0.01808694
0.01015598 0.01283432
0.00410702 0.00756621
0.00064601 0.00253375
0.00031731 -0.00175966
0.00347807 -0.00584155
0.00965869 -0.01022987
0.01862646 -0.01455885
0.03037228 -0.01871945
0.04488254 -0.02263404
0.06207826 -0.02625973
0.08188189 -0.02958274
0.10419508 -0.03259589
0.12889336 -0.0352853
0.15582461 -0.03765106
0.18481852 -0.03968576
0.21568836 -0.04137765
0.24824045 -0.04270831
0.28227172 -0.04366318
0.31757006 -0.04421632
0.35393702 -0.04433976
0.3911774 -0.04402775
0.4290824 -0.04326803
0.46745589 -0.04206368
0.50612131 -0.04045605
0.54486168 -0.03850284
0.58340814 -0.03626199
0.62149278 -0.03374911
0.65883359 -0.0309436
0.6953302 -0.02770034
0.7309964 -0.02413705
0.76563239 -0.02057383
0.79891722 -0.017161
0.83054222 -0.01399728
0.86020736 -0.01115019
0.88762502 -0.00865676
0.91252453 -0.00653167
0.93465545 -0.00476354
0.95378729 -0.00331281
0.96975557 -0.00208276
0.982533 -0.00103843
0.99203693 -0.00032137
0.99797259 -2.6896E-05
1 -3.9E-17

s8065 Airoil CAD files

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