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Winfoil Airfoils - Total Number: 277
Name T/C % Camber % Camber Chord % CL Max CD Min
<< First < Prev 44 45 46 47 48 Next > Last >>
RAF 38 12.6 2.531 40 1.523 0.0058
RAF 6 9.97 4.541 29.97 1.996 0.0078
RG 15 8.92 1.761 39.73 1.11 0.0057
RG8 10.78 2.224 60 1.096 0.0069
RITZ 1-30-10 9.94 0.999 30 1.008 0.0093
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
2.5 2.98 2.5 -2.02
5 4.21 5 -2.66
10 5.94 10 -3.38
20 7.91 20 -3.86
30 8.75 30 -3.9
40 8.69 40 -3.66
50 8.06 50 -3.23
60 6.85 60 -2.73
70 5.27 70 -2.13
80 3.54 80 -1.46
90 1.83 90 -0.79
100 0 100 0
V 1.0