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Winfoil Airfoils - Total Number: 277
Name T/C % T/C % Chord Position Camber % Camber Chord % CL Max CD Min
<< First < Prev 9 10 11 12 13 Next > Last >>
RAF 6 9.97 29.97 4.541 29.97 1.996 0.0078
RAF 38 12.6 30 2.531 40 1.523 0.0058
RAF 33 12.7 30.03 4.663 30.03 1.501 0.0063
RAF 32 12.66 30 5.067 50 1.827 0.0089
RAF 31 12.69 30 2.086 50 1.43 0.0056
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
2.49 3.59 2.5 -0.5
4.98 5.4 5 -0.49
9.97 7.42 10 -0.47
19.97 9.06 20 -0.43
29.97 9.57 30 -0.4
39.97 9.53 40 -0.36
49.97 9.17 50 -0.33
59.97 8.4 60 -0.29
69.97 7.14 70 -0.25
79.98 5.37 80 -0.22
89.99 3.31 90 -0.18
100 0.15 100 -0.15
X Y
1 0.0015
0.8999 0.0331
0.7998 0.0537
0.6997 0.0714
0.5997 0.084
0.4997 0.0917
0.3997 0.0953
0.2997 0.0957
0.1997 0.0906
0.0997 0.0742
0.0498 0.054
0.0249 0.0359
0 0
0 0
0.025 -0.005
0.05 -0.0049
0.1 -0.0047
0.2 -0.0043
0.3 -0.004
0.4 -0.0036
0.5 -0.0033
0.6 -0.0029
0.7 -0.0025
0.8 -0.0022
0.9 -0.0018
1 -0.0015
X Y
100 0.15
89.99 3.31
79.98 5.37
69.97 7.14
59.97 8.4
49.97 9.17
39.97 9.53
29.97 9.57
19.97 9.06
9.97 7.42
4.98 5.4
2.49 3.59
0 0
0 0
2.5 -0.5
5 -0.49
10 -0.47
20 -0.43
30 -0.4
40 -0.36
50 -0.33
60 -0.29
70 -0.25
80 -0.22
90 -0.18
100 -0.15
V 1.1