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Winfoil Airfoils - Total Number: 277
Name T/C % T/C % Chord Position Camber % Camber Chord % CL Max CD Min
1 2 3 4 5 Next > Last >>
RAF 19 10.52 15 10.065 40 2.23 0.0084
FX63-137 13.67 30.87 5.84 56.53 2.199 0.0076
RAF 6 9.97 29.97 4.541 29.97 1.996 0.0078
RAF 32 12.66 30 5.067 50 1.827 0.0089
EPPLER 1200 16.93 36.11 3.48 40.77 1.818 0.0072
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
1.25 2.7 1.25 -0.8
2.5 4.61 2.5 -1.18
5 7.33 5 -1.07
7.5 9.24 7.5 -0.55
10 10.66 10 0.26
15 12.59 15 2.09
20 13.62 20 3.82
30 14.18 30 5.88
40 13.74 40 6.54
50 12.5 50 6.3
60 10.86 60 5.36
70 8.72 70 4.22
80 6.38 80 2.68
90 3.64 90 1.04
95 1.97 95 0.17
100 0 100 0
X Y
1 0
0.95 0.0197
0.9 0.0364
0.8 0.0638
0.7 0.0872
0.6 0.1086
0.5 0.125
0.4 0.1374
0.3 0.1418
0.2 0.1362
0.15 0.1259
0.1 0.1066
0.075 0.0924
0.05 0.0733
0.025 0.0461
0.0125 0.027
0 0
0 0
0.0125 -0.008
0.025 -0.0118
0.05 -0.0107
0.075 -0.0055
0.1 0.0026
0.15 0.0209
0.2 0.0382
0.3 0.0588
0.4 0.0654
0.5 0.063
0.6 0.0536
0.7 0.0422
0.8 0.0268
0.9 0.0104
0.95 0.0017
1 0
X Y
100 0
95 1.97
90 3.64
80 6.38
70 8.72
60 10.86
50 12.5
40 13.74
30 14.18
20 13.62
15 12.59
10 10.66
7.5 9.24
5 7.33
2.5 4.61
1.25 2.7
0 0
0 0
1.25 -0.8
2.5 -1.18
5 -1.07
7.5 -0.55
10 0.26
15 2.09
20 3.82
30 5.88
40 6.54
50 6.3
60 5.36
70 4.22
80 2.68
90 1.04
95 0.17
100 0
V 1.1