s8066 Airfoil

Selig airfoil for Q-40 pylon racing (10%)

s8066 Airfoil (x,y) Co-ordinates

1 0
0.99805784 0.00016694
0.99241629 0.0007361
0.98324599 0.00170716
0.97064675 0.0031525
0.95481854 0.00514625
0.93598311 0.00770781
0.9143869 0.01083619
0.8902947 0.0144931
0.86398584 0.01861136
0.83574798 0.02308345
0.80587355 0.02776144
0.77465139 0.03234905
0.74207529 0.03662024
0.70813055 0.04059213
0.67306054 0.044282
0.63708355 0.04764434
0.60040608 0.05064086
0.56322909 0.05322136
0.52576064 0.05533743
0.48820767 0.05695361
0.4507588 0.05805093
0.41359357 0.05860808
0.37690109 0.05862167
0.3408726 0.05811834
0.30570768 0.05712917
0.27161334 0.05567576
0.23879064 0.05378345
0.20743553 0.05147406
0.17773239 0.04877194
0.14985548 0.04570354
0.12396889 0.04230027
0.10022708 0.03859257
0.07876779 0.0346132
0.05971673 0.0304014
0.04319141 0.02599727
0.02932066 0.02141578
0.01814221 0.01666974
0.00962621 0.01179741
0.00377942 0.00686645
0.00050486 0.00215925
0.00040015 -0.00190425
0.0037424 -0.0058366
0.01000901 -0.01003232
0.01904333 -0.01414349
0.03083419 -0.0180791
0.04537528 -0.02177464
0.06259549 -0.02518123
0.08241656 -0.0282864
0.10473918 -0.03108836
0.12944176 -0.03357639
0.15637301 -0.03575136
0.185362 -0.03760732
0.21622281 -0.03913285
0.24876296 -0.04031035
0.28278053 -0.0411263
0.31806434 -0.04155576
0.35441709 -0.04157116
0.3916452 -0.04116782
0.42954378 -0.04033576
0.46791669 -0.03907517
0.5065862 -0.0374361
0.54533427 -0.03548212
0.58388963 -0.03326482
0.62198484 -0.03079922
0.65933657 -0.02805848
0.69586476 -0.02491428
0.7315707 -0.02149949
0.76622359 -0.01811914
0.79950677 -0.01491085
0.83111435 -0.0119663
0.86074948 -0.0093475
0.88812801 -0.00708747
0.91298289 -0.00519757
0.93506737 -0.00366457
0.95415554 -0.00244912
0.97008032 -0.00146344
0.98278932 -0.00066776
0.99218813 -0.00015994
0.99801945 9.6636E-06
1 4E-18

s8066 Airfoil CAD files

DOWNLOAD FROM HERE

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