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Winfoil Airfoils - Total Number: 277
Name T/C % Camber % Camber Chord % CL Max CD Min
<< First < Prev 10 11 12 13 14 Next > Last >>
RAF 30 12.56 0.105 0.17 1.065 0.0004
RAF 27 9.7 0 0 0.854 0.0057
RAF 26 6.58 2.13 49.9 1.016 0.0041
RAF 25 6.43 1.043 49.86 0.746 0.0043
RAF 19 10.52 10.065 40 2.23 0.0084
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
0.17 0.63 0.17 -0.53
0.43 1.17 0.43 -1
0.83 1.57 0.83 -1.57
1.25 1.8 1.25 -1.8
2.5 2.48 2.5 -2.48
5 3.46 5 -3.46
10 4.68 10 -4.68
15 5.44 15 -5.44
20 5.94 20 -5.94
30 6.32 30 -6.32
40 6.2 40 -6.2
50 5.66 50 -5.66
60 4.78 60 -4.78
70 3.7 70 -3.7
80 2.5 80 -2.5
90 1.3 90 -1.3
95 0.7 95 -0.7
100 0 100 0
V 1.0