s8064 Airfoil

Selig airfoil for Q-500 (Q500) pylon racing (12.33%)

s8064 Airfoil (x,y) Co-ordinates

1 0
0.997927 0.000125
0.991844 0.000661
0.98195 0.001759
0.968438 0.003565
0.951588 0.006193
0.931716 0.009686
0.909164 0.014035
0.884293 0.019168
0.857469 0.024954
0.829053 0.031198
0.79939 0.03763
0.768826 0.04376
0.737098 0.049161
0.703928 0.053909
0.669588 0.05818
0.634301 0.061961
0.598271 0.065229
0.561701 0.067947
0.524799 0.070079
0.487769 0.071601
0.450799 0.0725
0.414069 0.072755
0.37777 0.072374
0.342087 0.071387
0.307218 0.069831
0.273369 0.067736
0.240738 0.065134
0.209521 0.062054
0.1799 0.058531
0.15205 0.0546
0.126136 0.050302
0.102312 0.045678
0.080718 0.040772
0.061481 0.035636
0.044723 0.030322
0.030576 0.024873
0.019091 0.01931
0.010271 0.01367
0.004145 0.008047
0.000637 0.002692
0.000328 -0.001911
0.003568 -0.006325
0.009851 -0.011082
0.018933 -0.015812
0.030792 -0.020402
0.045404 -0.024768
0.062686 -0.02886
0.082555 -0.032657
0.104908 -0.036143
0.12962 -0.039299
0.156536 -0.042118
0.185485 -0.044585
0.216282 -0.046683
0.248732 -0.048388
0.282633 -0.04968
0.317775 -0.05053
0.353959 -0.050905
0.390991 -0.050795
0.428663 -0.050184
0.466779 -0.049071
0.505162 -0.047491
0.543597 -0.045496
0.581815 -0.043133
0.619551 -0.040409
0.656518 -0.03728
0.69267 -0.033539
0.728117 -0.029328
0.762681 -0.025064
0.796024 -0.020943
0.827817 -0.017097
0.857738 -0.013617
0.885475 -0.010558
0.91073 -0.007944
0.933228 -0.005769
0.952715 -0.003991
0.969006 -0.002502
0.982067 -0.001257
0.99181 -0.000404
0.997911 -0.000042
1 0

s8064 Airfoil CAD files

DOWNLOAD FROM HERE

Leave a Reply