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Winfoil Airfoils - Total Number: 277
Name T/C % Camber % Camber Chord % CL Max CD Min
<< First < Prev 27 28 29 30 31 Next > Last >>
NACA 0219 18.99 0 0 1.427 0.013
NACA 1111 10.99 0.996 9.52 0.937 0.0095
NACA 1408 7.99 0.978 40 0.782 0.0067
NACA 1410 9.99 0.971 40 0.913 0.0044
NACA 1412 11.98 0.966 40 1.037 0.007
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
0.1 0.87 0.1 -0.87
0.39 1.72 0.39 -1.72
0.89 2.55 0.89 -2.55
1.57 3.34 1.57 -3.34
2.45 4.1 2.45 -4.1
3.51 4.83 3.51 -4.83
4.76 5.51 4.76 -5.51
6.19 6.15 6.19 -6.15
7.79 6.75 7.79 -6.75
9.56 7.29 9.56 -7.29
11.48 7.78 11.48 -7.78
13.56 8.21 13.56 -8.21
15.78 8.58 15.78 -8.58
18.14 8.89 18.14 -8.89
20.63 9.14 20.63 -9.14
23.23 9.32 23.23 -9.32
25.93 9.44 25.93 -9.44
28.73 9.5 28.73 -9.5
31.62 9.49 31.62 -9.49
34.57 9.43 34.57 -9.43
37.59 9.32 37.59 -9.32
40.66 9.15 40.66 -9.15
43.76 8.93 43.76 -8.93
46.89 8.68 46.89 -8.68
50.03 8.38 50.03 -8.38
53.17 8.05 53.17 -8.05
56.3 7.69 56.3 -7.69
59.4 7.3 59.4 -7.3
62.47 6.9 62.47 -6.9
65.49 6.47 65.49 -6.47
68.44 6.04 68.44 -6.04
71.33 5.6 71.33 -5.6
74.12 5.15 74.12 -5.15
76.83 4.7 76.83 -4.7
79.43 4.25 79.43 -4.25
81.91 3.82 81.91 -3.82
84.26 3.39 84.26 -3.39
86.48 2.97 86.48 -2.97
88.56 2.57 88.56 -2.57
90.48 2.2 90.48 -2.2
92.24 1.84 92.24 -1.84
93.84 1.52 93.84 -1.52
95.26 1.22 95.26 -1.22
96.51 0.96 96.51 -0.96
97.57 0.73 97.57 -0.73
98.44 0.54 98.44 -0.54
99.13 0.39 99.13 -0.39
99.61 0.29 99.61 -0.29
99.91 0.22 99.91 -0.22
100 0.2 100 -0.2
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