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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 52 53 54 55 56
NACA 664-221 20.98 44.97 1.119 50 1.434 0.008
B-29 ROOT 21.92 29.94 1.782 39.94 1.699 0.0333
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
0.1 1 0.1 -0.5
0.2 1.25 0.2 -0.8
0.37 1.57 0.63 -1.47
0.61 1.87 0.89 -1.73
1.1 2.34 1.41 -2.13
2.32 3.23 2.68 -2.85
4.8 4.58 5.2 -3.95
7.29 5.65 7.71 -4.81
9.79 6.57 10.21 -5.53
14.8 8.04 15.2 -6.69
19.82 9.17 20.19 -7.58
24.84 10.05 25.16 -8.26
29.87 10.71 30.13 -8.77
34.9 11.18 35.1 -9.12
39.93 11.48 40.07 -9.34
44.97 11.6 45.03 -9.4
50 11.54 50 -9.33
55.03 11.28 54.97 -9.09
60.06 10.76 59.94 -8.62
65.09 9.82 64.91 -7.76
70.1 8.58 69.9 -6.64
75.11 7.15 74.89 -5.36
80.11 5.59 79.89 -4
85.09 4 84.91 -2.65
90.07 2.44 89.93 -1.41
95.03 1.03 94.97 -0.4
100 0 100 0
X Y
1 0
0.9503 0.0103
0.9007 0.0244
0.8509 0.04
0.8011 0.0559
0.7511 0.0715
0.701 0.0858
0.6509 0.0982
0.6006 0.1076
0.5503 0.1128
0.5 0.1154
0.4497 0.116
0.3993 0.1148
0.349 0.1118
0.2987 0.1071
0.2484 0.1005
0.1982 0.0917
0.148 0.0804
0.0979 0.0657
0.0729 0.0565
0.048 0.0458
0.0232 0.0323
0.011 0.0234
0.0061 0.0187
0.0037 0.0157
0.002 0.0125
0.001 0.01
0 0
0 0
0.001 -0.005
0.002 -0.008
0.0063 -0.0147
0.0089 -0.0173
0.0141 -0.0213
0.0268 -0.0285
0.052 -0.0395
0.0771 -0.0481
0.1021 -0.0553
0.152 -0.0669
0.2019 -0.0758
0.2516 -0.0826
0.3013 -0.0877
0.351 -0.0912
0.4007 -0.0934
0.4503 -0.094
0.5 -0.0933
0.5497 -0.0909
0.5994 -0.0862
0.6491 -0.0776
0.699 -0.0664
0.7489 -0.0536
0.7989 -0.04
0.8491 -0.0265
0.8993 -0.0141
0.9497 -0.004
1 0
X Y
100 0
95.03 1.03
90.07 2.44
85.09 4
80.11 5.59
75.11 7.15
70.1 8.58
65.09 9.82
60.06 10.76
55.03 11.28
50 11.54
44.97 11.6
39.93 11.48
34.9 11.18
29.87 10.71
24.84 10.05
19.82 9.17
14.8 8.04
9.79 6.57
7.29 5.65
4.8 4.58
2.32 3.23
1.1 2.34
0.61 1.87
0.37 1.57
0.2 1.25
0.1 1
0 0
0 0
0.1 -0.5
0.2 -0.8
0.63 -1.47
0.89 -1.73
1.41 -2.13
2.68 -2.85
5.2 -3.95
7.71 -4.81
10.21 -5.53
15.2 -6.69
20.19 -7.58
25.16 -8.26
30.13 -8.77
35.1 -9.12
40.07 -9.34
45.03 -9.4
50 -9.33
54.97 -9.09
59.94 -8.62
64.91 -7.76
69.9 -6.64
74.89 -5.36
79.89 -4
84.91 -2.65
89.93 -1.41
94.97 -0.4
100 0
V 1.1