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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 16 17 18 19 20 Next > Last >>
NACA 66-210 10 44.98 1.105 50 0.808 0
NACA 66-209 8.98 44.99 1.109 50 0.722 0.0001
NACA 66-206 6 44.99 1.107 50 0.688 0.0003
NACA 661-212 12 44.98 1.111 50 0.986 0.0011
NACA 65A-410 9.97 41.61 2.125 50 1.032 0.007
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
0.1 0.4 0.1 -0.3
0.2 0.5 0.2 -0.4
0.3 0.7 0.3 -0.55
0.44 0.81 0.56 -0.71
0.68 0.98 0.82 -0.84
1.17 1.25 1.33 -1.03
2.41 1.7 2.59 -1.33
4.9 2.4 5.1 -1.77
7.4 2.96 7.6 -2.11
9.9 3.43 10.1 -2.39
14.9 4.2 15.1 -2.86
19.91 4.8 20.09 -3.2
24.92 5.26 25.08 -3.47
29.94 5.61 30.06 -3.66
34.95 5.86 35.05 -3.8
39.97 6.02 40.03 -3.88
44.98 6.1 45.02 -3.91
50 6.07 50 -3.87
55.02 5.96 54.98 -3.77
60.03 5.74 59.97 -3.59
65.04 5.33 64.96 -3.27
70.05 4.76 69.95 -2.82
75.06 4.07 74.94 -2.28
80.06 3.29 79.94 -1.7
85.05 2.45 84.95 -1.1
90.04 1.57 89.96 -0.54
95.02 0.72 94.98 -0.09
100 0 100 0
X Y
1 0
0.9502 0.0072
0.9004 0.0157
0.8505 0.0245
0.8006 0.0329
0.7506 0.0407
0.7005 0.0476
0.6504 0.0533
0.6003 0.0574
0.5502 0.0596
0.5 0.0607
0.4498 0.061
0.3997 0.0602
0.3495 0.0586
0.2994 0.0561
0.2492 0.0526
0.1991 0.048
0.149 0.042
0.099 0.0343
0.074 0.0296
0.049 0.024
0.0241 0.017
0.0117 0.0125
0.0068 0.0098
0.0044 0.0081
0.003 0.007
0.002 0.005
0.001 0.004
0 0
0 0
0.001 -0.003
0.002 -0.004
0.003 -0.0055
0.0056 -0.0071
0.0082 -0.0084
0.0133 -0.0103
0.0259 -0.0133
0.051 -0.0177
0.076 -0.0211
0.101 -0.0239
0.151 -0.0286
0.2009 -0.032
0.2508 -0.0347
0.3006 -0.0366
0.3505 -0.038
0.4003 -0.0388
0.4502 -0.0391
0.5 -0.0387
0.5498 -0.0377
0.5997 -0.0359
0.6496 -0.0327
0.6995 -0.0282
0.7494 -0.0228
0.7994 -0.017
0.8495 -0.011
0.8996 -0.0054
0.9498 -0.0009
1 0
X Y
100 0
95.02 0.72
90.04 1.57
85.05 2.45
80.06 3.29
75.06 4.07
70.05 4.76
65.04 5.33
60.03 5.74
55.02 5.96
50 6.07
44.98 6.1
39.97 6.02
34.95 5.86
29.94 5.61
24.92 5.26
19.91 4.8
14.9 4.2
9.9 3.43
7.4 2.96
4.9 2.4
2.41 1.7
1.17 1.25
0.68 0.98
0.44 0.81
0.3 0.7
0.2 0.5
0.1 0.4
0 0
0 0
0.1 -0.3
0.2 -0.4
0.3 -0.55
0.56 -0.71
0.82 -0.84
1.33 -1.03
2.59 -1.33
5.1 -1.77
7.6 -2.11
10.1 -2.39
15.1 -2.86
20.09 -3.2
25.08 -3.47
30.06 -3.66
35.05 -3.8
40.03 -3.88
45.02 -3.91
50 -3.87
54.98 -3.77
59.97 -3.59
64.96 -3.27
69.95 -2.82
74.94 -2.28
79.94 -1.7
84.95 -1.1
89.96 -0.54
94.98 -0.09
100 0
V 1.1