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Winfoil Airfoils - Total Number: 277
Name T/C % Camber % Camber Chord % CL Max CD Min
<< First < Prev 4 5 6 7 8 Next > Last >>
RAF 15 6.45 2.564 30 1.282 0.0059
AG455ct -02f rot. 6.47 1.846 31.8804 1.009 0.0078
AG17 6.49 2.013 45.4997 0.959 0.0072
RAF 26 6.58 2.13 49.9 1.016 0.0041
AG26 Bubble Dancer DLG by 6.84 2.547 44.0913 1.056 0.0071
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
1.25 1.85 1.25 -0.79
2.5 2.55 2.5 -1.04
5 3.47 5 -1.34
10 4.59 10 -1.47
15 5.2 15 -1.28
20 5.52 20 -0.9
30 5.56 30 -0.35
40 5.31 40 -0.29
50 4.88 50 -0.54
60 4.33 60 -0.85
70 3.66 70 -1.06
80 2.84 80 -0.97
90 1.8 90 -0.79
95 1.19 95 -0.65
100 0 100 0
V 1.0