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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 31 32 33 34 35 Next > Last >>
MH26 10.98 39.66 1.509 39.66 0.942 0.0046
MH25 9.98 39.57 1.459 39.57 0.851 0.0056
MH24 8.99 39.3 1.301 39.3 0.813 0.0052
MH23 7.99 34.09 1.27 38.95 0.76 0.0042
MH22 7.21 28.86 1.889 33.42 0.739 0.0041
Coordinates
XUpper YUpper XLower YLower
0 0.02 0 0.02
0.02 0.13 0.01 -0.08
0.08 0.3 0.05 -0.16
0.19 0.49 0.13 -0.26
0.77 1.12 0.29 -0.4
1.86 1.86 0.5 -0.54
3.4 2.61 1.69 -1.08
5.39 3.34 3.32 -1.57
7.81 4.03 5.45 -2.01
10.64 4.68 8.08 -2.42
13.88 5.25 11.16 -2.77
17.47 5.76 14.68 -3.09
21.4 6.18 18.59 -3.36
25.63 6.52 22.84 -3.58
30.11 6.77 27.39 -3.76
34.8 6.93 32.18 -3.88
39.66 7.01 37.17 -3.96
44.62 6.99 42.31 -3.98
49.64 6.9 47.53 -3.96
54.67 6.72 52.77 -3.89
59.65 6.47 57.97 -3.78
64.52 6.14 63.08 -3.63
69.24 5.74 68.04 -3.44
73.75 5.28 72.78 -3.2
78 4.75 77.26 -2.91
81.94 4.15 81.42 -2.57
85.56 3.46 85.24 -2.15
88.87 2.69 88.73 -1.69
91.87 1.93 91.84 -1.24
94.52 1.23 94.52 -0.79
96.74 0.65 96.76 -0.41
98.47 0.25 98.5 -0.15
99.6 0.05 99.61 -0.02
100 0 100 0
X Y
1 0
0.996 0.0005
0.9847 0.0025
0.9674 0.0065
0.9452 0.0123
0.9187 0.0193
0.8887 0.0269
0.8556 0.0346
0.8194 0.0415
0.78 0.0475
0.7375 0.0528
0.6924 0.0574
0.6452 0.0614
0.5965 0.0647
0.5467 0.0672
0.4964 0.069
0.4462 0.0699
0.3966 0.0701
0.348 0.0693
0.3011 0.0677
0.2563 0.0652
0.214 0.0618
0.1747 0.0576
0.1388 0.0525
0.1064 0.0468
0.0781 0.0403
0.0539 0.0334
0.034 0.0261
0.0186 0.0186
0.0077 0.0112
0.0019 0.0049
0.0008 0.003
0.0002 0.0013
0 0.0002
0 0.0002
0.0001 -0.0008
0.0005 -0.0016
0.0013 -0.0026
0.0029 -0.004
0.005 -0.0054
0.0169 -0.0108
0.0332 -0.0157
0.0545 -0.0201
0.0808 -0.0242
0.1116 -0.0277
0.1468 -0.0309
0.1859 -0.0336
0.2284 -0.0358
0.2739 -0.0376
0.3218 -0.0388
0.3717 -0.0396
0.4231 -0.0398
0.4753 -0.0396
0.5277 -0.0389
0.5797 -0.0378
0.6308 -0.0363
0.6804 -0.0344
0.7278 -0.032
0.7726 -0.0291
0.8142 -0.0257
0.8524 -0.0215
0.8873 -0.0169
0.9184 -0.0124
0.9452 -0.0079
0.9676 -0.0041
0.985 -0.0015
0.9961 -0.0002
1 0
X Y
100 0
99.6 0.05
98.47 0.25
96.74 0.65
94.52 1.23
91.87 1.93
88.87 2.69
85.56 3.46
81.94 4.15
78 4.75
73.75 5.28
69.24 5.74
64.52 6.14
59.65 6.47
54.67 6.72
49.64 6.9
44.62 6.99
39.66 7.01
34.8 6.93
30.11 6.77
25.63 6.52
21.4 6.18
17.47 5.76
13.88 5.25
10.64 4.68
7.81 4.03
5.39 3.34
3.4 2.61
1.86 1.86
0.77 1.12
0.19 0.49
0.08 0.3
0.02 0.13
0 0.02
0 0.02
0.01 -0.08
0.05 -0.16
0.13 -0.26
0.29 -0.4
0.5 -0.54
1.69 -1.08
3.32 -1.57
5.45 -2.01
8.08 -2.42
11.16 -2.77
14.68 -3.09
18.59 -3.36
22.84 -3.58
27.39 -3.76
32.18 -3.88
37.17 -3.96
42.31 -3.98
47.53 -3.96
52.77 -3.89
57.97 -3.78
63.08 -3.63
68.04 -3.44
72.78 -3.2
77.26 -2.91
81.42 -2.57
85.24 -2.15
88.73 -1.69
91.84 -1.24
94.52 -0.79
96.76 -0.41
98.5 -0.15
99.61 -0.02
100 0
V 1.1