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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 48 49 50 51 52 Next > Last >>
S4180 9.8 26.13 4.49 34.8 1.589 0.0076
S4233 13.63 34.86 3.165 44.08 1.407 0.0071
S7012 8.75 27.74 1.963 38.07 1.024 0.0032
S7055 10.5 31.75 3.604 38.6 1.269 0.006
S8036 15.99 36.85 1.825 36.85 1.538 0.005
Coordinates
XUpper YUpper XLower YLower
0.02 -0.2 0.02 -0.2
0.13 0.64 0.38 -0.81
0.61 1.61 1.31 -1.23
1.47 2.61 2.78 -1.52
2.73 3.6 4.79 -1.67
4.4 4.55 7.35 -1.68
6.48 5.47 10.45 -1.58
8.93 6.32 14.07 -1.42
14.92 7.77 22.62 -0.96
18.38 8.33 27.46 -0.7
22.13 8.75 32.59 -0.43
26.13 9.02 37.94 -0.18
30.35 9.12 43.45 0.06
34.8 9.05 49.04 0.27
39.43 8.83 54.66 0.46
44.2 8.47 60.22 0.6
49.08 8 65.66 0.71
54.02 7.42 70.91 0.78
58.96 6.76 75.9 0.8
63.86 6.04 80.57 0.79
68.66 5.28 84.85 0.74
73.31 4.5 88.69 0.65
77.77 3.72 92.05 0.54
81.97 2.97 94.86 0.41
85.86 2.28 97.09 0.26
89.38 1.66 98.7 0.13
92.48 1.13 99.68 0.04
100 0 100 0
X Y
1 0
0.9248 0.0113
0.8938 0.0166
0.8586 0.0228
0.8197 0.0297
0.7777 0.0372
0.7331 0.045
0.6866 0.0528
0.6386 0.0604
0.5896 0.0676
0.5402 0.0742
0.4908 0.08
0.442 0.0847
0.3943 0.0883
0.348 0.0905
0.3035 0.0912
0.2613 0.0902
0.2213 0.0875
0.1838 0.0833
0.1492 0.0777
0.0893 0.0632
0.0648 0.0547
0.044 0.0455
0.0273 0.036
0.0147 0.0261
0.0061 0.0161
0.0013 0.0064
0.0002 -0.002
0.0002 -0.002
0.0038 -0.0081
0.0131 -0.0123
0.0278 -0.0152
0.0479 -0.0167
0.0735 -0.0168
0.1045 -0.0158
0.1407 -0.0142
0.2262 -0.0096
0.2746 -0.007
0.3259 -0.0043
0.3794 -0.0018
0.4345 0.0006
0.4904 0.0027
0.5466 0.0046
0.6022 0.006
0.6566 0.0071
0.7091 0.0078
0.759 0.008
0.8057 0.0079
0.8485 0.0074
0.8869 0.0065
0.9205 0.0054
0.9486 0.0041
0.9709 0.0026
0.987 0.0013
0.9968 0.0004
1 0
X Y
100 0
92.48 1.13
89.38 1.66
85.86 2.28
81.97 2.97
77.77 3.72
73.31 4.5
68.66 5.28
63.86 6.04
58.96 6.76
54.02 7.42
49.08 8
44.2 8.47
39.43 8.83
34.8 9.05
30.35 9.12
26.13 9.02
22.13 8.75
18.38 8.33
14.92 7.77
8.93 6.32
6.48 5.47
4.4 4.55
2.73 3.6
1.47 2.61
0.61 1.61
0.13 0.64
0.02 -0.2
0.02 -0.2
0.38 -0.81
1.31 -1.23
2.78 -1.52
4.79 -1.67
7.35 -1.68
10.45 -1.58
14.07 -1.42
22.62 -0.96
27.46 -0.7
32.59 -0.43
37.94 -0.18
43.45 0.06
49.04 0.27
54.66 0.46
60.22 0.6
65.66 0.71
70.91 0.78
75.9 0.8
80.57 0.79
84.85 0.74
88.69 0.65
92.05 0.54
94.86 0.41
97.09 0.26
98.7 0.13
99.68 0.04
100 0
V 1.1