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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
X Y
1 0.002
0.9991 0.0022
0.9961 0.0029
0.9913 0.0039
0.9844 0.0054
0.9757 0.0073
0.9651 0.0096
0.9526 0.0122
0.9384 0.0152
0.9224 0.0184
0.9048 0.022
0.8856 0.0257
0.8648 0.0297
0.8426 0.0339
0.8191 0.0382
0.7943 0.0425
0.7683 0.047
0.7412 0.0515
0.7133 0.056
0.6844 0.0604
0.6549 0.0647
0.6247 0.069
0.594 0.073
0.563 0.0769
0.5317 0.0805
0.5003 0.0838
0.4689 0.0868
0.4376 0.0893
0.4066 0.0915
0.3759 0.0932
0.3457 0.0943
0.3162 0.0949
0.2873 0.095
0.2593 0.0944
0.2323 0.0932
0.2063 0.0914
0.1814 0.0889
0.1578 0.0858
0.1356 0.0821
0.1148 0.0778
0.0956 0.0729
0.0779 0.0675
0.0619 0.0615
0.0476 0.0551
0.0351 0.0483
0.0245 0.041
0.0157 0.0334
0.0089 0.0255
0.0039 0.0172
0.001 0.0087
0 0
0 0
0.001 -0.0087
0.0039 -0.0172
0.0089 -0.0255
0.0157 -0.0334
0.0245 -0.041
0.0351 -0.0483
0.0476 -0.0551
0.0619 -0.0615
0.0779 -0.0675
0.0956 -0.0729
0.1148 -0.0778
0.1356 -0.0821
0.1578 -0.0858
0.1814 -0.0889
0.2063 -0.0914
0.2323 -0.0932
0.2593 -0.0944
0.2873 -0.095
0.3162 -0.0949
0.3457 -0.0943
0.3759 -0.0932
0.4066 -0.0915
0.4376 -0.0893
0.4689 -0.0868
0.5003 -0.0838
0.5317 -0.0805
0.563 -0.0769
0.594 -0.073
0.6247 -0.069
0.6549 -0.0647
0.6844 -0.0604
0.7133 -0.056
0.7412 -0.0515
0.7683 -0.047
0.7943 -0.0425
0.8191 -0.0382
0.8426 -0.0339
0.8648 -0.0297
0.8856 -0.0257
0.9048 -0.022
0.9224 -0.0184
0.9384 -0.0152
0.9526 -0.0122
0.9651 -0.0096
0.9757 -0.0073
0.9844 -0.0054
0.9913 -0.0039
0.9961 -0.0029
0.9991 -0.0022
1 -0.002
X Y
100 0.2
99.91 0.22
99.61 0.29
99.13 0.39
98.44 0.54
97.57 0.73
96.51 0.96
95.26 1.22
93.84 1.52
92.24 1.84
90.48 2.2
88.56 2.57
86.48 2.97
84.26 3.39
81.91 3.82
79.43 4.25
76.83 4.7
74.12 5.15
71.33 5.6
68.44 6.04
65.49 6.47
62.47 6.9
59.4 7.3
56.3 7.69
53.17 8.05
50.03 8.38
46.89 8.68
43.76 8.93
40.66 9.15
37.59 9.32
34.57 9.43
31.62 9.49
28.73 9.5
25.93 9.44
23.23 9.32
20.63 9.14
18.14 8.89
15.78 8.58
13.56 8.21
11.48 7.78
9.56 7.29
7.79 6.75
6.19 6.15
4.76 5.51
3.51 4.83
2.45 4.1
1.57 3.34
0.89 2.55
0.39 1.72
0.1 0.87
0 0
0 0
0.1 -0.87
0.39 -1.72
0.89 -2.55
1.57 -3.34
2.45 -4.1
3.51 -4.83
4.76 -5.51
6.19 -6.15
7.79 -6.75
9.56 -7.29
11.48 -7.78
13.56 -8.21
15.78 -8.58
18.14 -8.89
20.63 -9.14
23.23 -9.32
25.93 -9.44
28.73 -9.5
31.62 -9.49
34.57 -9.43
37.59 -9.32
40.66 -9.15
43.76 -8.93
46.89 -8.68
50.03 -8.38
53.17 -8.05
56.3 -7.69
59.4 -7.3
62.47 -6.9
65.49 -6.47
68.44 -6.04
71.33 -5.6
74.12 -5.15
76.83 -4.7
79.43 -4.25
81.91 -3.82
84.26 -3.39
86.48 -2.97
88.56 -2.57
90.48 -2.2
92.24 -1.84
93.84 -1.52
95.26 -1.22
96.51 -0.96
97.57 -0.73
98.44 -0.54
99.13 -0.39
99.61 -0.29
99.91 -0.22
100 -0.2
V 1.1