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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 35 36 37 38 39 Next > Last >>
NACA 652-415 14.98 39.9 2.218 50 1.248 0.0026
NACA 653-218 17.97 39.94 1.118 50 1.172 0.0034
NACA 653-418 17.97 39.88 2.221 50 1.41 0.0082
NACA 653-618 17.97 39.826 3.324 50 1.618 0.0085
NACA 654-221 20.98 39.93 1.113 50 0.646 0.0123
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
0.1 0.9 0.1 -0.3
0.2 1 0.2 -0.5
0.3 1.2 0.3 -0.7
0.31 1.21 0.69 -1.01
0.54 1.48 0.96 -1.2
1.02 1.9 1.48 -1.47
4.7 3.86 5.3 -2.6
7.18 4.79 7.82 -3.1
9.68 5.58 10.32 -3.51
14.7 6.84 15.3 -4.15
19.73 7.81 20.27 -4.63
24.76 8.55 25.24 -4.97
29.81 9.09 30.19 -5.21
34.85 9.46 35.15 -5.34
39.9 9.64 40.1 -5.36
44.95 9.62 45.05 -5.24
50 9.37 50 -4.96
55.04 8.91 54.96 -4.53
60.08 8.26 59.92 -3.98
65.11 7.46 64.89 -3.34
70.12 6.54 69.88 -2.65
75.13 5.53 74.87 -1.95
80.13 4.45 79.87 -1.26
85.11 3.32 84.89 -0.63
90.08 2.18 89.92 -0.11
95.04 1.06 94.96 0.21
100 0 100 0
X Y
1 0
0.9504 0.0106
0.9008 0.0218
0.8511 0.0332
0.8013 0.0445
0.7513 0.0553
0.7012 0.0654
0.6511 0.0746
0.6008 0.0826
0.5504 0.0891
0.5 0.0937
0.4495 0.0962
0.399 0.0964
0.3485 0.0946
0.2981 0.0909
0.2476 0.0855
0.1973 0.0781
0.147 0.0684
0.0968 0.0558
0.0718 0.0479
0.047 0.0386
0.0102 0.019
0.0054 0.0148
0.0031 0.0121
0.003 0.012
0.002 0.01
0.001 0.009
0 0
0 0
0.001 -0.003
0.002 -0.005
0.003 -0.007
0.0069 -0.0101
0.0096 -0.012
0.0148 -0.0147
0.053 -0.026
0.0782 -0.031
0.1032 -0.0351
0.153 -0.0415
0.2027 -0.0463
0.2524 -0.0497
0.3019 -0.0521
0.3515 -0.0534
0.401 -0.0536
0.4505 -0.0524
0.5 -0.0496
0.5496 -0.0453
0.5992 -0.0398
0.6489 -0.0334
0.6988 -0.0265
0.7487 -0.0195
0.7987 -0.0126
0.8489 -0.0063
0.8992 -0.0011
0.9496 0.0021
1 0
X Y
100 0
95.04 1.06
90.08 2.18
85.11 3.32
80.13 4.45
75.13 5.53
70.12 6.54
65.11 7.46
60.08 8.26
55.04 8.91
50 9.37
44.95 9.62
39.9 9.64
34.85 9.46
29.81 9.09
24.76 8.55
19.73 7.81
14.7 6.84
9.68 5.58
7.18 4.79
4.7 3.86
1.02 1.9
0.54 1.48
0.31 1.21
0.3 1.2
0.2 1
0.1 0.9
0 0
0 0
0.1 -0.3
0.2 -0.5
0.3 -0.7
0.69 -1.01
0.96 -1.2
1.48 -1.47
5.3 -2.6
7.82 -3.1
10.32 -3.51
15.3 -4.15
20.27 -4.63
25.24 -4.97
30.19 -5.21
35.15 -5.34
40.1 -5.36
45.05 -5.24
50 -4.96
54.96 -4.53
59.92 -3.98
64.89 -3.34
69.88 -2.65
74.87 -1.95
79.87 -1.26
84.89 -0.63
89.92 -0.11
94.96 0.21
100 0
V 1.1