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Winfoil Airfoils - Total Number: 277
Name T/C % Camber % Camber Chord % CL Max CD Min
<< First < Prev 7 8 9 10 11 Next > Last >>
ARA-D 10% 10.01 3.724 35 1.741 0.0202
ARA-D 13% 13 3.34 30 1.713 0.0247
ARA-D 6% 6.04 4.752 45 1.552 0.0145
ATR 14.52 2.882 21.4 1.632 0.0092
B-29 ROOT 21.92 1.782 39.94 1.699 0.0333
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
0.3 1.37 0.3 -0.73
1 2.52 1 -1.25
2 3.55 2 -1.63
4 4.92 4 -2
7 6.23 7 -2.16
10 7.08 10 -2.1
15 7.95 15 -1.82
20 8.46 20 -1.51
25 8.75 25 -1.25
30 8.89 30 -1.05
35 8.89 35 -0.91
40 8.76 40 -0.81
45 8.52 45 -0.73
50 8.17 50 -0.67
55 7.72 55 -0.63
60 7.2 60 -0.62
65 6.6 65 -0.62
70 5.93 70 -0.64
75 5.21 75 -0.66
80 4.42 80 -0.69
85 3.57 85 -0.71
90 2.66 90 -0.72
95 1.71 95 -0.72
97.5 1.23 97.5 -0.73
100 0.75 100 -0.75
V 1.0