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Winfoil Airfoils - Total Number: 277
Name T/C % T/C % Chord Position Camber % Camber Chord % CL Max CD Min
1 2 3 4 5 Next > Last >>
EPPLER 378 4.08 10.36 8.109 35.92 1.686 0.0014
AG08 5.83 14.2151 1.934 26.7002 0.907 0.007
RAF 15 6.45 15 2.564 30 1.282 0.0059
RAF 19 10.52 15 10.065 40 2.23 0.0084
AG09 4.86 15.9674 1.795 33.2344 0.886 0.0096
Coordinates
XUpper YUpper XLower YLower
0.06 -0.2 0.06 0.28
0.43 0.98 0.52 -0.42
1.15 1.79 1.53 -0.42
2.26 2.66 3.03 -0.17
3.73 3.56 5.07 0.37
5.59 4.45 7.73 1.22
7.8 5.32 11.08 2.32
10.36 6.14 15.16 3.6
13.25 6.89 20 4.93
16.44 7.55 25.57 6.14
19.89 8.1 31.81 7.05
23.59 8.52 38.47 7.41
27.5 8.77 45.13 7.23
31.61 8.84 51.59 6.72
35.92 8.72 57.78 6.03
40.4 8.43 63.66 5.25
45.03 7.96 69.19 4.42
49.8 7.36 74.34 3.6
54.67 6.68 79.07 2.82
59.57 5.94 83.36 2.11
64.46 5.17 87.19 1.48
69.25 4.41 90.52 0.95
73.89 3.67 93.36 0.54
78.32 2.96 95.68 0.25
82.48 2.31 97.5 0.1
86.31 1.72 98.86 0.04
99.71 0.0358 99.71 0.01
100 0 100 0
X Y
1 0
0.9971 0.000358
0.8631 0.0172
0.8248 0.0231
0.7832 0.0296
0.7389 0.0367
0.6925 0.0441
0.6446 0.0517
0.5957 0.0594
0.5467 0.0668
0.498 0.0736
0.4503 0.0796
0.404 0.0843
0.3592 0.0872
0.3161 0.0884
0.275 0.0877
0.2359 0.0852
0.1989 0.081
0.1644 0.0755
0.1325 0.0689
0.1036 0.0614
0.078 0.0532
0.0559 0.0445
0.0373 0.0356
0.0226 0.0266
0.0115 0.0179
0.0043 0.0098
0.0006 -0.002
0.0006 0.0028
0.0052 -0.0042
0.0153 -0.0042
0.0303 -0.0017
0.0507 0.0037
0.0773 0.0122
0.1108 0.0232
0.1516 0.036
0.2 0.0493
0.2557 0.0614
0.3181 0.0705
0.3847 0.0741
0.4513 0.0723
0.5159 0.0672
0.5778 0.0603
0.6366 0.0525
0.6919 0.0442
0.7434 0.036
0.7907 0.0282
0.8336 0.0211
0.8719 0.0148
0.9052 0.0095
0.9336 0.0054
0.9568 0.0025
0.975 0.001
0.9886 0.0004
0.9971 0.0001
1 0
X Y
100 0
99.71 0.0358
86.31 1.72
82.48 2.31
78.32 2.96
73.89 3.67
69.25 4.41
64.46 5.17
59.57 5.94
54.67 6.68
49.8 7.36
45.03 7.96
40.4 8.43
35.92 8.72
31.61 8.84
27.5 8.77
23.59 8.52
19.89 8.1
16.44 7.55
13.25 6.89
10.36 6.14
7.8 5.32
5.59 4.45
3.73 3.56
2.26 2.66
1.15 1.79
0.43 0.98
0.06 -0.2
0.06 0.28
0.52 -0.42
1.53 -0.42
3.03 -0.17
5.07 0.37
7.73 1.22
11.08 2.32
15.16 3.6
20 4.93
25.57 6.14
31.81 7.05
38.47 7.41
45.13 7.23
51.59 6.72
57.78 6.03
63.66 5.25
69.19 4.42
74.34 3.6
79.07 2.82
83.36 2.11
87.19 1.48
90.52 0.95
93.36 0.54
95.68 0.25
97.5 0.1
98.86 0.04
99.71 0.01
100 0
V 1.1