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Winfoil Airfoils - Total Number: 277
Name T/C % Camber % Camber Chord % CL Max CD Min
<< First < Prev 17 18 19 20 21 Next > Last >>
NACA 65A-312 11.97 1.56 51.68 1.064 0.0012
NACA 65-912 11.96 4.861 50 1.5 0.0046
NACA 654-221 20.98 1.113 50 0.646 0.0123
NACA 653-618 17.97 3.324 50 1.618 0.0085
NACA 653-418 17.97 2.221 50 1.41 0.0082
Coordinates
XUpper YUpper XLower YLower
0.06 0.16 0.06 0.16
0.15 0.37 0.1 -0.14
0.25 0.63 0.23 -0.32
0.36 0.86 0.4 -0.53
0.46 1.02 0.56 -0.72
0.55 1.14 0.69 -0.86
0.66 1.23 0.8 -0.95
0.8 1.34 0.92 -1.02
0.98 1.47 1.07 -1.09
1.23 1.62 1.26 -1.18
1.56 1.8 1.52 -1.28
1.99 2.02 1.87 -1.4
2.54 2.26 2.31 -1.53
3.22 2.52 2.88 -1.67
4 2.79 3.57 -1.82
4.82 3.06 4.35 -1.98
5.65 3.32 5.18 -2.13
6.48 3.56 6.02 -2.27
7.31 3.79 6.85 -2.4
8.16 4.01 7.69 -2.53
9.1 4.23 8.54 -2.65
10.23 4.48 9.48 -2.77
11.6 4.76 10.61 -2.9
13.17 5.06 11.98 -3.05
14.82 5.36 13.53 -3.2
16.49 5.63 15.18 -3.35
18.17 5.88 16.84 -3.49
19.84 6.11 18.5 -3.62
21.51 6.33 20.16 -3.74
23.19 6.52 21.82 -3.84
24.86 6.7 23.48 -3.94
26.54 6.86 25.14 -4.02
28.21 7 26.8 -4.1
29.89 7.13 28.46 -4.16
31.56 7.24 30.11 -4.22
33.24 7.34 31.77 -4.27
34.91 7.42 33.43 -4.31
36.59 7.49 35.09 -4.34
38.26 7.54 36.75 -4.36
39.94 7.58 38.4 -4.37
41.62 7.6 40.06 -4.37
43.29 7.61 41.72 -4.37
44.97 7.6 43.37 -4.35
46.65 7.57 45.03 -4.32
48.32 7.53 46.69 -4.28
50 7.46 48.34 -4.23
51.68 7.39 50 -4.16
53.35 7.29 51.66 -4.09
55.03 7.18 53.32 -4
56.7 7.05 54.97 -3.9
58.38 6.91 56.63 -3.79
60.05 6.75 58.29 -3.67
61.72 6.58 59.95 -3.55
63.4 6.4 61.61 -3.41
65.07 6.21 63.27 -3.27
66.74 6 64.93 -3.13
68.41 5.79 66.59 -2.97
70.08 5.56 68.26 -2.82
71.75 5.32 69.92 -2.65
73.42 5.08 71.58 -2.49
75.09 4.82 73.25 -2.32
76.76 4.56 74.91 -2.15
78.43 4.28 76.58 -1.98
80.09 4 78.24 -1.8
81.76 3.72 79.91 -1.63
83.42 3.42 81.58 -1.46
85.09 3.12 83.25 -1.29
86.75 2.82 84.91 -1.12
88.41 2.51 86.58 -0.96
90.07 2.19 88.26 -0.81
91.73 1.86 89.93 -0.66
93.39 1.52 91.6 -0.52
95.05 1.17 93.28 -0.39
96.67 0.81 94.95 -0.28
98.11 0.47 96.6 -0.19
99.18 0.22 98.07 -0.11
99.75 0.0826 99.16 -0.06
99.76 0.08 99.75 -0.04
99.97 0.03 99.97 -0.03
100 0.03 100 -0.03
V 1.0