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Winfoil Airfoils - Total Number: 277
Name T/C % Camber % Camber Chord % CL Max CD Min
<< First < Prev 43 44 45 46 47 Next > Last >>
RAF 27 9.7 0 0 0.854 0.0057
RAF 30 12.56 0.105 0.17 1.065 0.0004
RAF 31 12.69 2.086 50 1.43 0.0056
RAF 32 12.66 5.067 50 1.827 0.0089
RAF 33 12.7 4.663 30.03 1.501 0.0063
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
1.25 1.34 1.25 -1.34
2.5 1.9 2.5 -1.9
5 2.67 5 -2.67
7.5 3.2 7.5 -3.2
10 3.62 10 -3.62
15 4.24 15 -4.24
20 4.6 20 -4.6
30 4.88 30 -4.88
40 4.78 40 -4.78
50 4.37 50 -4.37
60 3.77 60 -3.77
70 2.96 70 -2.96
80 2.08 80 -2.08
90 1.12 90 -1.12
95 0.61 95 -0.61
100 0 100 0
X Y
1 0
0.95 0.0061
0.9 0.0112
0.8 0.0208
0.7 0.0296
0.6 0.0377
0.5 0.0437
0.4 0.0478
0.3 0.0488
0.2 0.046
0.15 0.0424
0.1 0.0362
0.075 0.032
0.05 0.0267
0.025 0.019
0.0125 0.0134
0 0
0 0
0.0125 -0.0134
0.025 -0.019
0.05 -0.0267
0.075 -0.032
0.1 -0.0362
0.15 -0.0424
0.2 -0.046
0.3 -0.0488
0.4 -0.0478
0.5 -0.0437
0.6 -0.0377
0.7 -0.0296
0.8 -0.0208
0.9 -0.0112
0.95 -0.0061
1 0
X Y
100 0
95 0.61
90 1.12
80 2.08
70 2.96
60 3.77
50 4.37
40 4.78
30 4.88
20 4.6
15 4.24
10 3.62
7.5 3.2
5 2.67
2.5 1.9
1.25 1.34
0 0
0 0
1.25 -1.34
2.5 -1.9
5 -2.67
7.5 -3.2
10 -3.62
15 -4.24
20 -4.6
30 -4.88
40 -4.78
50 -4.37
60 -3.77
70 -2.96
80 -2.08
90 -1.12
95 -0.61
100 0
V 1.1