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Winfoil Airfoils - Total Number: 277
Name T/C % Camber % Camber Chord % CL Max CD Min
<< First < Prev 3 4 5 6 7 Next > Last >>
NACA 63-209 8.99 1.11 50 0.756 0.006
MH23 7.99 1.27 38.95 0.76 0.0042
NACA 0008 7.98 0 0 0.765 0.0064
MH54 8 0.595 40.1 0.776 0.0044
MH33 7.27 1.124 43.91 0.779 0.0042
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
0.2 0.6 0.2 -0.4
0.44 0.8 0.56 -0.7
0.68 0.97 0.82 -0.83
1.17 1.26 1.33 -1.04
2.41 1.77 2.59 -1.39
4.9 2.51 5.1 -1.88
7.39 3.08 7.61 -2.23
9.89 3.54 10.11 -2.51
14.9 4.26 15.1 -2.92
19.91 4.79 20.09 -3.2
24.93 5.17 25.08 -3.38
29.94 5.41 30.06 -3.47
34.96 5.53 35.04 -3.47
39.97 5.52 40.03 -3.38
44.99 5.39 45.01 -3.2
50 5.16 50 -2.95
55.01 4.83 54.99 -2.64
60.02 4.43 59.98 -2.29
65.03 3.96 64.97 -1.9
70.03 3.43 69.97 -1.49
75.03 2.86 74.97 -1.07
80.03 2.27 79.97 -0.68
85.03 1.66 84.97 -0.32
90.02 1.07 89.98 -0.03
95.01 0.51 94.99 0.12
100 0 100 0
X Y
1 0
0.9501 0.0051
0.9002 0.0107
0.8503 0.0166
0.8003 0.0227
0.7503 0.0286
0.7003 0.0343
0.6503 0.0396
0.6002 0.0443
0.5501 0.0483
0.5 0.0516
0.4499 0.0539
0.3997 0.0552
0.3496 0.0553
0.2994 0.0541
0.2493 0.0517
0.1991 0.0479
0.149 0.0426
0.0989 0.0354
0.0739 0.0308
0.049 0.0251
0.0241 0.0177
0.0117 0.0126
0.0068 0.0097
0.0044 0.008
0.002 0.006
0 0
0 0
0.002 -0.004
0.0056 -0.007
0.0082 -0.0083
0.0133 -0.0104
0.0259 -0.0139
0.051 -0.0188
0.0761 -0.0223
0.1011 -0.0251
0.151 -0.0292
0.2009 -0.032
0.2508 -0.0338
0.3006 -0.0347
0.3504 -0.0347
0.4003 -0.0338
0.4501 -0.032
0.5 -0.0295
0.5499 -0.0264
0.5998 -0.0229
0.6497 -0.019
0.6997 -0.0149
0.7497 -0.0107
0.7997 -0.0068
0.8497 -0.0032
0.8998 -0.0003
0.9499 0.0012
1 0
X Y
100 0
95.01 0.51
90.02 1.07
85.03 1.66
80.03 2.27
75.03 2.86
70.03 3.43
65.03 3.96
60.02 4.43
55.01 4.83
50 5.16
44.99 5.39
39.97 5.52
34.96 5.53
29.94 5.41
24.93 5.17
19.91 4.79
14.9 4.26
9.89 3.54
7.39 3.08
4.9 2.51
2.41 1.77
1.17 1.26
0.68 0.97
0.44 0.8
0.2 0.6
0 0
0 0
0.2 -0.4
0.56 -0.7
0.82 -0.83
1.33 -1.04
2.59 -1.39
5.1 -1.88
7.61 -2.23
10.11 -2.51
15.1 -2.92
20.09 -3.2
25.08 -3.38
30.06 -3.47
35.04 -3.47
40.03 -3.38
45.01 -3.2
50 -2.95
54.99 -2.64
59.98 -2.29
64.97 -1.9
69.97 -1.49
74.97 -1.07
79.97 -0.68
84.97 -0.32
89.98 -0.03
94.99 0.12
100 0
V 1.1