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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 38 39 40 41 42 Next > Last >>
EPPLER 62 (5.62%) 5.66 26.238 5.307 49.334 1.302 0.0058
EPPLER 61 6.15 30 6.517 50 1.149 0.0005
EPPLER 397 13.5 29.45 5.331 52.1 1.47 0.0017
EPPLER 387 9.07 31.08 3.797 40.08 1.199 0.0064
EPPLER 378 4.08 10.36 8.109 35.92 1.686 0.0014
Coordinates
XUpper YUpper XLower YLower
0.024 0.14 0.024 0.14
0.421 0.72 0.115 -0.24
1.238 1.4 0.762 -0.44
2.476 2.14 1.974 -0.53
4.133 2.91 3.744 -0.5
6.202 3.66 6.068 -0.35
8.672 4.4 8.936 -0.09
11.523 5.09 12.328 0.23
14.736 5.73 16.216 0.63
18.28 6.3 20.561 1.06
22.126 6.8 25.315 1.5
26.238 7.22 30.425 1.92
30.578 7.54 35.828 2.31
35.102 7.77 41.449 2.62
39.768 7.9 47.195 2.85
44.527 7.93 52.982 2.99
49.334 7.86 58.733 3.05
54.145 7.66 64.371 3.03
58.925 7.36 69.823 2.92
63.636 6.95 75.016 2.75
68.242 6.46 79.879 2.5
72.697 5.9 84.347 2.19
76.951 5.3 88.357 1.84
80.955 4.66 91.854 1.46
84.665 4.01 94.785 1.05
88.036 3.36 97.092 0.65
91.03 2.71 98.725 0.3
93.61 2.08 99.685 0.07
100 0 100 0
X Y
1 0
0.9361 0.0208
0.9103 0.0271
0.88036 0.0336
0.84665 0.0401
0.80955 0.0466
0.76951 0.053
0.72697 0.059
0.68242 0.0646
0.63636 0.0695
0.58925 0.0736
0.54145 0.0766
0.49334 0.0786
0.44527 0.0793
0.39768 0.079
0.35102 0.0777
0.30578 0.0754
0.26238 0.0722
0.22126 0.068
0.1828 0.063
0.14736 0.0573
0.11523 0.0509
0.08672 0.044
0.06202 0.0366
0.04133 0.0291
0.02476 0.0214
0.01238 0.014
0.00421 0.0072
0.00024 0.0014
0.00024 0.0014
0.00115 -0.0024
0.00762 -0.0044
0.01974 -0.0053
0.03744 -0.005
0.06068 -0.0035
0.08936 -0.0009
0.12328 0.0023
0.16216 0.0063
0.20561 0.0106
0.25315 0.015
0.30425 0.0192
0.35828 0.0231
0.41449 0.0262
0.47195 0.0285
0.52982 0.0299
0.58733 0.0305
0.64371 0.0303
0.69823 0.0292
0.75016 0.0275
0.79879 0.025
0.84347 0.0219
0.88357 0.0184
0.91854 0.0146
0.94785 0.0105
0.97092 0.0065
0.98725 0.003
0.99685 0.0007
1 0
X Y
100 0
93.61 2.08
91.03 2.71
88.036 3.36
84.665 4.01
80.955 4.66
76.951 5.3
72.697 5.9
68.242 6.46
63.636 6.95
58.925 7.36
54.145 7.66
49.334 7.86
44.527 7.93
39.768 7.9
35.102 7.77
30.578 7.54
26.238 7.22
22.126 6.8
18.28 6.3
14.736 5.73
11.523 5.09
8.672 4.4
6.202 3.66
4.133 2.91
2.476 2.14
1.238 1.4
0.421 0.72
0.024 0.14
0.024 0.14
0.115 -0.24
0.762 -0.44
1.974 -0.53
3.744 -0.5
6.068 -0.35
8.936 -0.09
12.328 0.23
16.216 0.63
20.561 1.06
25.315 1.5
30.425 1.92
35.828 2.31
41.449 2.62
47.195 2.85
52.982 2.99
58.733 3.05
64.371 3.03
69.823 2.92
75.016 2.75
79.879 2.5
84.347 2.19
88.357 1.84
91.854 1.46
94.785 1.05
97.092 0.65
98.725 0.3
99.685 0.07
100 0
V 1.1