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Winfoil Airfoils - Total Number: 277
Name T/C % Camber % Camber Chord % CL Max CD Min
<< First < Prev 9 10 11 12 13 Next > Last >>
CLARK W 11.21 3.684 40 1.643 0.0075
CLARK Y 11.73 3.528 43.47 1.595 0.006
CLARK YH 11.9 2.45 30 1.392 0.0095
CLARK YS 11.7 2.353 30 1.274 0.0055
DAE51 9.38 3.465 46.07 1.186 0.0078
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
1.25 2.19 1.25 -1.61
2.5 3.11 2.5 -2.05
5 4.44 5 -2.57
7.5 5.45 7.5 -2.82
10 6.24 10 -2.93
15 7.49 15 -2.94
20 8.3 20 -2.79
30 9.04 30 -2.17
40 9.05 40 -1.54
50 8.59 50 -1.28
60 7.67 60 -1.23
70 6.32 70 -1.2
80 4.58 80 -0.94
90 2.52 90 -0.54
95 1.35 95 -0.28
100 0.1 100 0
V 1.0