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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
FX63-137 13.67 30.87 5.84 56.53 2.199 0.0076
RAF 19 10.52 15 10.065 40 2.23 0.0084
Coordinates
XUpper YUpper XLower YLower
0 0.24 0 0.24
0.43 1.74 0.43 -0.7
0.96 2.64 0.96 -1.02
1.7 3.55 1.7 -1.28
2.65 4.43 2.65 -1.5
3.81 5.26 3.81 -1.71
5.16 6.05 5.16 -1.88
6.7 6.81 6.7 -2.02
8.43 7.55 8.43 -2.12
10.33 8.27 10.33 -2.2
12.41 8.96 12.41 -2.25
14.65 9.59 14.65 -2.27
17.03 10.17 17.03 -2.27
22.22 11.12 22.22 -2.16
25 11.49 25 -2.04
27.89 11.79 27.89 -1.88
30.87 12 30.87 -1.68
33.93 12.13 33.93 -1.42
37.06 12.18 37.06 -1.12
43.47 12.03 43.47 -0.42
50 11.56 56.53 1.09
56.53 10.8 62.94 1.76
62.94 9.79 69.13 2.29
69.13 8.6 75 2.63
75 7.31 80.44 2.76
80.44 6 85.36 2.66
85.36 4.76 89.67 2.34
89.67 3.62 93.3 1.84
93.3 2.58 96.19 1.23
96.19 1.64 98.3 0.62
100 0 100 0
X Y
1 0
0.9619 0.0164
0.933 0.0258
0.8967 0.0362
0.8536 0.0476
0.8044 0.06
0.75 0.0731
0.6913 0.086
0.6294 0.0979
0.5653 0.108
0.5 0.1156
0.4347 0.1203
0.3706 0.1218
0.3393 0.1213
0.3087 0.12
0.2789 0.1179
0.25 0.1149
0.2222 0.1112
0.1703 0.1017
0.1465 0.0959
0.1241 0.0896
0.1033 0.0827
0.0843 0.0755
0.067 0.0681
0.0516 0.0605
0.0381 0.0526
0.0265 0.0443
0.017 0.0355
0.0096 0.0264
0.0043 0.0174
0 0.0024
0 0.0024
0.0043 -0.007
0.0096 -0.0102
0.017 -0.0128
0.0265 -0.015
0.0381 -0.0171
0.0516 -0.0188
0.067 -0.0202
0.0843 -0.0212
0.1033 -0.022
0.1241 -0.0225
0.1465 -0.0227
0.1703 -0.0227
0.2222 -0.0216
0.25 -0.0204
0.2789 -0.0188
0.3087 -0.0168
0.3393 -0.0142
0.3706 -0.0112
0.4347 -0.0042
0.5653 0.0109
0.6294 0.0176
0.6913 0.0229
0.75 0.0263
0.8044 0.0276
0.8536 0.0266
0.8967 0.0234
0.933 0.0184
0.9619 0.0123
0.983 0.0062
1 0
X Y
100 0
96.19 1.64
93.3 2.58
89.67 3.62
85.36 4.76
80.44 6
75 7.31
69.13 8.6
62.94 9.79
56.53 10.8
50 11.56
43.47 12.03
37.06 12.18
33.93 12.13
30.87 12
27.89 11.79
25 11.49
22.22 11.12
17.03 10.17
14.65 9.59
12.41 8.96
10.33 8.27
8.43 7.55
6.7 6.81
5.16 6.05
3.81 5.26
2.65 4.43
1.7 3.55
0.96 2.64
0.43 1.74
0 0.24
0 0.24
0.43 -0.7
0.96 -1.02
1.7 -1.28
2.65 -1.5
3.81 -1.71
5.16 -1.88
6.7 -2.02
8.43 -2.12
10.33 -2.2
12.41 -2.25
14.65 -2.27
17.03 -2.27
22.22 -2.16
25 -2.04
27.89 -1.88
30.87 -1.68
33.93 -1.42
37.06 -1.12
43.47 -0.42
56.53 1.09
62.94 1.76
69.13 2.29
75 2.63
80.44 2.76
85.36 2.66
89.67 2.34
93.3 1.84
96.19 1.23
98.3 0.62
100 0
V 1.1