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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 19 20 21 22 23 Next > Last >>
NACA 651-212 11.98 39.96 1.116 50 0.637 0.0041
NACA 64A-510 9.96 38.24 2.665 50 1.167 0.0045
NACA 64A410 9.96 38.26 2.115 51.68 1.065 0.0009
NACA 64A-312 11.95 38.26 1.554 51.68 1.059 0.009
NACA 64A210 9.97 39.96 1.325 49.99 0.558 0.0004
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
0.1 0.6 0.1 -0.45
0.2 0.8 0.2 -0.6
0.3 0.9 0.3 -0.7
0.4 1 0.4 -0.8
0.42 0.97 0.58 -0.87
0.66 1.18 0.84 -1.04
1.15 1.49 1.35 -1.28
2.39 2.06 2.61 -1.69
4.88 2.92 5.12 -2.29
7.37 3.59 7.63 -2.75
9.87 4.16 10.13 -3.13
14.88 5.07 15.12 -3.73
19.89 5.77 20.11 -4.18
24.91 6.3 25.09 -4.51
29.92 6.69 30.08 -4.74
34.94 6.94 35.06 -4.88
39.96 7.07 40.04 -4.93
44.98 7.04 45.02 -4.85
50 6.86 50 -4.65
55.02 6.51 54.98 -4.32
60.03 6.01 59.97 -3.87
65.04 5.41 64.96 -3.35
70.05 4.72 69.95 -2.77
75.05 3.95 74.95 -2.16
80.05 3.14 79.95 -1.55
85.05 2.3 84.96 -0.96
90.03 1.46 89.97 -0.43
95.02 0.67 94.98 -0.04
100 0 100 0
X Y
1 0
0.9502 0.0067
0.9003 0.0146
0.8505 0.023
0.8005 0.0314
0.7505 0.0395
0.7005 0.0472
0.6504 0.0541
0.6003 0.0601
0.5502 0.0651
0.5 0.0686
0.4498 0.0704
0.3996 0.0707
0.3494 0.0694
0.2992 0.0669
0.2491 0.063
0.1989 0.0577
0.1488 0.0507
0.0987 0.0416
0.0737 0.0359
0.0488 0.0292
0.0239 0.0206
0.0115 0.0149
0.0066 0.0118
0.0042 0.0097
0.004 0.01
0.003 0.009
0.002 0.008
0.001 0.006
0 0
0 0
0.001 -0.0045
0.002 -0.006
0.003 -0.007
0.004 -0.008
0.0058 -0.0087
0.0084 -0.0104
0.0135 -0.0128
0.0261 -0.0169
0.0512 -0.0229
0.0763 -0.0275
0.1013 -0.0313
0.1512 -0.0373
0.2011 -0.0418
0.2509 -0.0451
0.3008 -0.0474
0.3506 -0.0488
0.4004 -0.0493
0.4502 -0.0485
0.5 -0.0465
0.5498 -0.0432
0.5997 -0.0387
0.6496 -0.0335
0.6995 -0.0277
0.7495 -0.0216
0.7995 -0.0155
0.8496 -0.0096
0.8997 -0.0043
0.9498 -0.0004
1 0
X Y
100 0
95.02 0.67
90.03 1.46
85.05 2.3
80.05 3.14
75.05 3.95
70.05 4.72
65.04 5.41
60.03 6.01
55.02 6.51
50 6.86
44.98 7.04
39.96 7.07
34.94 6.94
29.92 6.69
24.91 6.3
19.89 5.77
14.88 5.07
9.87 4.16
7.37 3.59
4.88 2.92
2.39 2.06
1.15 1.49
0.66 1.18
0.42 0.97
0.4 1
0.3 0.9
0.2 0.8
0.1 0.6
0 0
0 0
0.1 -0.45
0.2 -0.6
0.3 -0.7
0.4 -0.8
0.58 -0.87
0.84 -1.04
1.35 -1.28
2.61 -1.69
5.12 -2.29
7.63 -2.75
10.13 -3.13
15.12 -3.73
20.11 -4.18
25.09 -4.51
30.08 -4.74
35.06 -4.88
40.04 -4.93
45.02 -4.85
50 -4.65
54.98 -4.32
59.97 -3.87
64.96 -3.35
69.95 -2.77
74.95 -2.16
79.95 -1.55
84.96 -0.96
89.97 -0.43
94.98 -0.04
100 0
V 1.1