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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 21 22 23 24 25 Next > Last >>
NACA 63-209 8.99 34.96 1.11 50 0.756 0.006
NACA 63-206 5.99 34.97 1.108 50 0.62 0.0052
NACA 631-412 11.98 34.88 2.215 50 1.268 0.007
NACA 631-212 11.98 34.94 1.108 50 1.071 0.0068
NACA 63-010 9.98 35 0 0 0.699 0.0065
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