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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 32 33 34 35 36 Next > Last >>
NACA 63-206 5.99 34.97 1.108 50 0.62 0.0052
NACA 63-209 8.99 34.96 1.11 50 0.756 0.006
NACA 63-210 9.98 34.95 1.11 50 0.961 0.0061
NACA 632-215 14.97 34.93 1.114 50 0.998 0.0052
NACA 632-415 14.98 34.85 2.213 50 1.268 0.0028
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
0.2 0.4 0.2 -0.3
0.46 0.55 0.54 -0.45
0.7 0.68 0.8 -0.54
1.2 0.88 1.3 -0.66
2.44 1.24 2.56 -0.87
4.93 1.78 5.07 -1.14
7.43 2.19 7.57 -1.34
9.93 2.53 10.07 -1.49
14.93 3.06 15.07 -1.71
19.94 3.45 20.06 -1.86
29.96 3.93 30.04 -1.98
34.97 4.03 35.03 -1.97
39.98 4.04 40.02 -1.9
44.99 3.97 45.01 -1.78
50 3.83 50 -1.62
55.01 3.61 54.99 -1.42
60.02 3.34 59.99 -1.2
65.02 3.01 64.98 -0.95
70.02 2.64 69.98 -0.7
75.02 2.24 74.93 -0.48
80.02 1.8 79.98 -0.21
85.02 1.36 84.98 -0.01
90.01 0.9 89.99 0.13
95.01 0.45 94.99 0.18
100 0 100 0
X Y
1 0
0.9501 0.0045
0.9001 0.009
0.8502 0.0136
0.8002 0.018
0.7502 0.0224
0.7002 0.0264
0.6502 0.0301
0.6002 0.0334
0.5501 0.0361
0.5 0.0383
0.4499 0.0397
0.3998 0.0404
0.3497 0.0403
0.2996 0.0393
0.1994 0.0345
0.1493 0.0306
0.0993 0.0253
0.0743 0.0219
0.0493 0.0178
0.0244 0.0124
0.012 0.0088
0.007 0.0068
0.0046 0.0055
0.002 0.004
0 0
0 0
0.002 -0.003
0.0054 -0.0045
0.008 -0.0054
0.013 -0.0066
0.0256 -0.0087
0.0507 -0.0114
0.0757 -0.0134
0.1007 -0.0149
0.1507 -0.0171
0.2006 -0.0186
0.3004 -0.0198
0.3503 -0.0197
0.4002 -0.019
0.4501 -0.0178
0.5 -0.0162
0.5499 -0.0142
0.5999 -0.012
0.6498 -0.0095
0.6998 -0.007
0.7493 -0.0048
0.7998 -0.0021
0.8498 -0.0001
0.8999 0.0013
0.9499 0.0018
1 0
X Y
100 0
95.01 0.45
90.01 0.9
85.02 1.36
80.02 1.8
75.02 2.24
70.02 2.64
65.02 3.01
60.02 3.34
55.01 3.61
50 3.83
44.99 3.97
39.98 4.04
34.97 4.03
29.96 3.93
19.94 3.45
14.93 3.06
9.93 2.53
7.43 2.19
4.93 1.78
2.44 1.24
1.2 0.88
0.7 0.68
0.46 0.55
0.2 0.4
0 0
0 0
0.2 -0.3
0.54 -0.45
0.8 -0.54
1.3 -0.66
2.56 -0.87
5.07 -1.14
7.57 -1.34
10.07 -1.49
15.07 -1.71
20.06 -1.86
30.04 -1.98
35.03 -1.97
40.02 -1.9
45.01 -1.78
50 -1.62
54.99 -1.42
59.99 -1.2
64.98 -0.95
69.98 -0.7
74.93 -0.48
79.98 -0.21
84.98 -0.01
89.99 0.13
94.99 0.18
100 0
V 1.1