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Winfoil Airfoils - Total Number: 277
Name T/C % T/C % Chord Position Camber % Camber Chord % CL Max CD Min
<< First < Prev 4 5 6 7 8 Next > Last >>
S8037 15.98 33.47 2.431 36.9 1.574 0.005
S8036 (16%) 16 36.848 1.821 36.848 1.538 0.0054
S8036 15.99 36.85 1.825 36.85 1.538 0.005
S7055 10.5 31.75 3.604 38.6 1.269 0.006
S7012 8.75 27.74 1.963 38.07 1.024 0.0032
Coordinates
XUpper YUpper XLower YLower
0.02 0.31 0.02 0.31
0.28 1.09 0.03 -0.34
0.76 1.92 0.38 -0.89
1.47 2.78 1.11 -1.42
2.42 3.64 2.16 -1.94
3.61 4.49 3.49 -2.43
5.02 5.32 5.12 -2.89
6.66 6.12 7.02 -3.31
8.52 6.87 9.18 -3.71
10.59 7.57 11.6 -4.06
12.87 8.21 14.25 -4.38
15.34 8.79 17.11 -4.65
18 9.29 20.17 -4.89
20.82 9.72 23.4 -5.09
23.8 10.07 26.79 -5.23
26.91 10.34 30.32 -5.33
30.14 10.53 33.96 -5.37
33.47 10.62 37.69 -5.36
36.9 10.61 41.5 -5.3
40.39 10.51 45.36 -5.17
43.94 10.3 49.26 -4.99
47.54 10 53.17 -4.76
51.18 9.6 57.08 -4.48
54.83 9.11 60.99 -4.15
58.49 8.55 64.85 -3.8
62.14 7.91 68.64 -3.45
65.78 7.21 72.34 -3.08
69.38 6.49 75.91 -2.73
72.91 5.77 79.34 -2.39
76.35 5.05 82.58 -2.06
79.66 4.37 85.61 -1.75
82.81 3.71 88.41 -1.47
85.78 3.1 90.94 -1.22
88.52 2.54 93.19 -0.98
91.02 2.03 95.13 -0.76
93.24 1.58 96.75 -0.55
95.17 1.17 98.06 -0.32
96.78 0.81 99.08 -0.13
98.08 0.47 99.76 -0.02
100 0 100 0
X Y
1 0
0.9808 0.0047
0.9678 0.0081
0.9517 0.0117
0.9324 0.0158
0.9102 0.0203
0.8852 0.0254
0.8578 0.031
0.8281 0.0371
0.7966 0.0437
0.7635 0.0505
0.7291 0.0577
0.6938 0.0649
0.6578 0.0721
0.6214 0.0791
0.5849 0.0855
0.5483 0.0911
0.5118 0.096
0.4754 0.1
0.4394 0.103
0.4039 0.1051
0.369 0.1061
0.3347 0.1062
0.3014 0.1053
0.2691 0.1034
0.238 0.1007
0.2082 0.0972
0.18 0.0929
0.1534 0.0879
0.1287 0.0821
0.1059 0.0757
0.0852 0.0687
0.0666 0.0612
0.0502 0.0532
0.0361 0.0449
0.0242 0.0364
0.0147 0.0278
0.0076 0.0192
0.0028 0.0109
0.0002 0.0031
0.0002 0.0031
0.0003 -0.0034
0.0038 -0.0089
0.0111 -0.0142
0.0216 -0.0194
0.0349 -0.0243
0.0512 -0.0289
0.0702 -0.0331
0.0918 -0.0371
0.116 -0.0406
0.1425 -0.0438
0.1711 -0.0465
0.2017 -0.0489
0.234 -0.0509
0.2679 -0.0523
0.3032 -0.0533
0.3396 -0.0537
0.3769 -0.0536
0.415 -0.053
0.4536 -0.0517
0.4926 -0.0499
0.5317 -0.0476
0.5708 -0.0448
0.6099 -0.0415
0.6485 -0.038
0.6864 -0.0345
0.7234 -0.0308
0.7591 -0.0273
0.7934 -0.0239
0.8258 -0.0206
0.8561 -0.0175
0.8841 -0.0147
0.9094 -0.0122
0.9319 -0.0098
0.9513 -0.0076
0.9675 -0.0055
0.9806 -0.0032
0.9908 -0.0013
0.9976 -0.0002
1 0
X Y
100 0
98.08 0.47
96.78 0.81
95.17 1.17
93.24 1.58
91.02 2.03
88.52 2.54
85.78 3.1
82.81 3.71
79.66 4.37
76.35 5.05
72.91 5.77
69.38 6.49
65.78 7.21
62.14 7.91
58.49 8.55
54.83 9.11
51.18 9.6
47.54 10
43.94 10.3
40.39 10.51
36.9 10.61
33.47 10.62
30.14 10.53
26.91 10.34
23.8 10.07
20.82 9.72
18 9.29
15.34 8.79
12.87 8.21
10.59 7.57
8.52 6.87
6.66 6.12
5.02 5.32
3.61 4.49
2.42 3.64
1.47 2.78
0.76 1.92
0.28 1.09
0.02 0.31
0.02 0.31
0.03 -0.34
0.38 -0.89
1.11 -1.42
2.16 -1.94
3.49 -2.43
5.12 -2.89
7.02 -3.31
9.18 -3.71
11.6 -4.06
14.25 -4.38
17.11 -4.65
20.17 -4.89
23.4 -5.09
26.79 -5.23
30.32 -5.33
33.96 -5.37
37.69 -5.36
41.5 -5.3
45.36 -5.17
49.26 -4.99
53.17 -4.76
57.08 -4.48
60.99 -4.15
64.85 -3.8
68.64 -3.45
72.34 -3.08
75.91 -2.73
79.34 -2.39
82.58 -2.06
85.61 -1.75
88.41 -1.47
90.94 -1.22
93.19 -0.98
95.13 -0.76
96.75 -0.55
98.06 -0.32
99.08 -0.13
99.76 -0.02
100 0
V 1.1