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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 37 38 39 40 41 Next > Last >>
NACA 66-209 8.98 44.99 1.109 50 0.722 0.0001
NACA 66-210 10 44.98 1.105 50 0.808 0
NACA 662-215 14.98 44.98 1.109 50 0.915 0.0002
NACA 662-415 14.99 44.95 2.217 50 0.751 0.0001
NACA 663-218 17.97 44.97 1.117 50 1.166 0.0073
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
0.1 0.4 0.1 -0.35
0.2 0.5 0.2 -0.4
0.3 0.65 0.3 -0.5
0.44 0.74 0.56 -0.64
0.69 0.89 0.81 -0.75
1.18 1.14 1.32 -0.92
2.42 1.55 2.58 -1.18
4.91 2.19 5.09 -1.56
7.41 2.71 7.59 -1.86
9.91 3.14 10.09 -2.11
14.91 3.85 15.09 -2.5
19.92 4.4 20.08 -2.8
24.93 4.82 25.07 -3.03
29.94 5.15 30.06 -3.2
34.96 5.38 35.04 -3.32
39.97 5.53 40.03 -3.39
44.99 5.59 45.01 -3.4
50 5.58 50 -3.37
55.01 5.48 54.99 -3.29
60.03 5.28 59.97 -3.13
65.04 4.91 64.96 -2.85
70.05 4.4 69.95 -2.46
75.05 3.77 74.95 -1.98
80.05 3.06 79.95 -1.47
85.04 2.28 84.96 -0.94
90.03 1.48 89.97 -0.44
95.02 0.69 94.98 -0.06
100 0 100 0
X Y
1 0
0.9502 0.0069
0.9003 0.0148
0.8504 0.0228
0.8005 0.0306
0.7505 0.0377
0.7005 0.044
0.6504 0.0491
0.6003 0.0528
0.5501 0.0548
0.5 0.0558
0.4499 0.0559
0.3997 0.0553
0.3496 0.0538
0.2994 0.0515
0.2493 0.0482
0.1992 0.044
0.1491 0.0385
0.0991 0.0314
0.0741 0.0271
0.0491 0.0219
0.0242 0.0155
0.0118 0.0114
0.0069 0.0089
0.0044 0.0074
0.003 0.0065
0.002 0.005
0.001 0.004
0 0
0 0
0.001 -0.0035
0.002 -0.004
0.003 -0.005
0.0056 -0.0064
0.0081 -0.0075
0.0132 -0.0092
0.0258 -0.0118
0.0509 -0.0156
0.0759 -0.0186
0.1009 -0.0211
0.1509 -0.025
0.2008 -0.028
0.2507 -0.0303
0.3006 -0.032
0.3504 -0.0332
0.4003 -0.0339
0.4501 -0.034
0.5 -0.0337
0.5499 -0.0329
0.5997 -0.0313
0.6496 -0.0285
0.6995 -0.0246
0.7495 -0.0198
0.7995 -0.0147
0.8496 -0.0094
0.8997 -0.0044
0.9498 -0.0006
1 0
X Y
100 0
95.02 0.69
90.03 1.48
85.04 2.28
80.05 3.06
75.05 3.77
70.05 4.4
65.04 4.91
60.03 5.28
55.01 5.48
50 5.58
44.99 5.59
39.97 5.53
34.96 5.38
29.94 5.15
24.93 4.82
19.92 4.4
14.91 3.85
9.91 3.14
7.41 2.71
4.91 2.19
2.42 1.55
1.18 1.14
0.69 0.89
0.44 0.74
0.3 0.65
0.2 0.5
0.1 0.4
0 0
0 0
0.1 -0.35
0.2 -0.4
0.3 -0.5
0.56 -0.64
0.81 -0.75
1.32 -0.92
2.58 -1.18
5.09 -1.56
7.59 -1.86
10.09 -2.11
15.09 -2.5
20.08 -2.8
25.07 -3.03
30.06 -3.2
35.04 -3.32
40.03 -3.39
45.01 -3.4
50 -3.37
54.99 -3.29
59.97 -3.13
64.96 -2.85
69.95 -2.46
74.95 -1.98
79.95 -1.47
84.96 -0.94
89.97 -0.44
94.98 -0.06
100 0
V 1.1