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Winfoil Airfoils - Total Number: 277
Name T/C % Camber % Camber Chord % CL Max CD Min
<< First < Prev 25 26 27 28 29 Next > Last >>
MH60 10.07 1.939 32.14 1.089 0.0034
MH61 10.25 1.365 41.57 0.842 0.0042
MH62 9.29 1.409 37.15 0.919 0.0056
MILEY 12.86 5.132 35.03 1.43 0.005
NACA 0008 7.98 0 0 0.765 0.0064
Coordinates
XUpper YUpper XLower YLower
0.06 -0.27 0.06 -0.27
0.09 0.34 0.63 -0.78
0.63 1.1 1.76 -1.31
1.59 1.93 3.39 -1.81
2.97 2.77 5.49 -2.27
4.75 3.58 8.05 -2.66
6.94 4.33 11.04 -2.97
9.52 5 14.44 -3.19
12.49 5.58 18.24 -3.32
15.81 6.05 22.4 -3.37
19.47 6.41 26.88 -3.34
23.43 6.64 31.64 -3.25
27.66 6.75 36.64 -3.1
32.14 6.74 41.81 -2.91
36.81 6.62 47.09 -2.68
41.64 6.38 52.44 -2.44
46.58 6.04 57.77 -2.19
51.57 5.59 63.04 -1.93
56.58 5.06 68.16 -1.68
61.57 4.43 73.08 -1.44
66.5 3.75 77.74 -1.22
71.33 3.04 82.09 -1.01
76.01 2.35 86.05 -0.81
80.47 1.71 89.6 -0.64
84.64 1.15 92.68 -0.49
88.45 0.69 95.26 -0.35
91.83 0.35 97.29 -0.23
94.69 0.13 98.77 -0.12
98.66 -0.02 99.68 -0.03
100 0 100 0
X Y
1 0
0.9866 -0.0002
0.9469 0.0013
0.9183 0.0035
0.8845 0.0069
0.8464 0.0115
0.8047 0.0171
0.7601 0.0235
0.7133 0.0304
0.665 0.0375
0.6157 0.0443
0.5658 0.0506
0.5157 0.0559
0.4658 0.0604
0.4164 0.0638
0.3681 0.0662
0.3214 0.0674
0.2766 0.0675
0.2343 0.0664
0.1947 0.0641
0.1581 0.0605
0.1249 0.0558
0.0952 0.05
0.0694 0.0433
0.0475 0.0358
0.0297 0.0277
0.0159 0.0193
0.0063 0.011
0.0009 0.0034
0.0006 -0.0027
0.0006 -0.0027
0.0063 -0.0078
0.0176 -0.0131
0.0339 -0.0181
0.0549 -0.0227
0.0805 -0.0266
0.1104 -0.0297
0.1444 -0.0319
0.1824 -0.0332
0.224 -0.0337
0.2688 -0.0334
0.3164 -0.0325
0.3664 -0.031
0.4181 -0.0291
0.4709 -0.0268
0.5244 -0.0244
0.5777 -0.0219
0.6304 -0.0193
0.6816 -0.0168
0.7308 -0.0144
0.7774 -0.0122
0.8209 -0.0101
0.8605 -0.0081
0.896 -0.0064
0.9268 -0.0049
0.9526 -0.0035
0.9729 -0.0023
0.9877 -0.0012
0.9968 -0.0003
1 0
X Y
100 0
98.66 -0.02
94.69 0.13
91.83 0.35
88.45 0.69
84.64 1.15
80.47 1.71
76.01 2.35
71.33 3.04
66.5 3.75
61.57 4.43
56.58 5.06
51.57 5.59
46.58 6.04
41.64 6.38
36.81 6.62
32.14 6.74
27.66 6.75
23.43 6.64
19.47 6.41
15.81 6.05
12.49 5.58
9.52 5
6.94 4.33
4.75 3.58
2.97 2.77
1.59 1.93
0.63 1.1
0.09 0.34
0.06 -0.27
0.06 -0.27
0.63 -0.78
1.76 -1.31
3.39 -1.81
5.49 -2.27
8.05 -2.66
11.04 -2.97
14.44 -3.19
18.24 -3.32
22.4 -3.37
26.88 -3.34
31.64 -3.25
36.64 -3.1
41.81 -2.91
47.09 -2.68
52.44 -2.44
57.77 -2.19
63.04 -1.93
68.16 -1.68
73.08 -1.44
77.74 -1.22
82.09 -1.01
86.05 -0.81
89.6 -0.64
92.68 -0.49
95.26 -0.35
97.29 -0.23
98.77 -0.12
99.68 -0.03
100 0
V 1.1