Airfoil:

mm

Job Status

Please wait while the PDF is generated...

Plot Number:

File:

Search for Airfoil
Winfoil Airfoils - Total Number: 277
Name T/C % Camber % Camber Chord % CL Max CD Min
<< First < Prev 13 14 15 16 17 Next > Last >>
EPPLER 231 12.33 2.463 39.36 1.2 0.0061
EPPLER 266 17.3 3.062 39.79 1.483 0.0066
EPPLER 325 12.61 1.812 18.29 0.845 0.0209
EPPLER 336 12.79 2.829 22.94 1.154 0.0198
EPPLER 340 13.69 2.617 22.2 1.184 0.0246
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
0.02 0.15 0.02 -0.14
0.28 0.76 0.09 -0.26
1.01 1.61 0.22 -0.38
2.16 2.51 0.33 -0.47
3.74 3.41 1.29 -0.97
5.75 4.28 2.8 -1.45
8.17 5.11 4.84 -1.89
10.99 5.88 7.38 -2.29
14.18 6.57 10.39 -2.64
17.72 7.17 13.85 -2.94
21.58 7.67 17.7 -3.19
25.71 8.07 21.92 -3.39
30.08 8.37 26.45 -3.54
34.65 8.56 31.24 -3.64
39.36 8.63 36.24 -3.7
44.16 8.58 41.39 -3.71
49.02 8.42 46.62 -3.68
53.86 8.13 51.89 -3.6
58.67 7.7 57.13 -3.48
63.4 7.14 62.28 -3.31
68.01 6.46 67.28 -3.1
72.48 5.65 72.07 -2.85
76.81 4.76 76.59 -2.54
80.97 3.84 80.83 -2.15
84.9 2.95 84.77 -1.69
88.52 2.15 88.39 -1.22
91.77 1.46 91.66 -0.8
94.57 0.9 94.49 -0.45
96.85 0.48 96.8 -0.21
98.55 0.19 98.54 -0.06
99.63 0.04 99.63 -0.01
100 0 100 0
X Y
1 0
0.9963 0.0004
0.9855 0.0019
0.9685 0.0048
0.9457 0.009
0.9177 0.0146
0.8852 0.0215
0.849 0.0295
0.8097 0.0384
0.7681 0.0476
0.7248 0.0565
0.6801 0.0646
0.634 0.0714
0.5867 0.077
0.5386 0.0813
0.4902 0.0842
0.4416 0.0858
0.3936 0.0863
0.3465 0.0856
0.3008 0.0837
0.2571 0.0807
0.2158 0.0767
0.1772 0.0717
0.1418 0.0657
0.1099 0.0588
0.0817 0.0511
0.0575 0.0428
0.0374 0.0341
0.0216 0.0251
0.0101 0.0161
0.0028 0.0076
0.0002 0.0015
0 0
0 0
0.0002 -0.0014
0.0009 -0.0026
0.0022 -0.0038
0.0033 -0.0047
0.0129 -0.0097
0.028 -0.0145
0.0484 -0.0189
0.0738 -0.0229
0.1039 -0.0264
0.1385 -0.0294
0.177 -0.0319
0.2192 -0.0339
0.2645 -0.0354
0.3124 -0.0364
0.3624 -0.037
0.4139 -0.0371
0.4662 -0.0368
0.5189 -0.036
0.5713 -0.0348
0.6228 -0.0331
0.6728 -0.031
0.7207 -0.0285
0.7659 -0.0254
0.8083 -0.0215
0.8477 -0.0169
0.8839 -0.0122
0.9166 -0.008
0.9449 -0.0045
0.968 -0.0021
0.9854 -0.0006
0.9963 -0.0001
1 0
X Y
100 0
99.63 0.04
98.55 0.19
96.85 0.48
94.57 0.9
91.77 1.46
88.52 2.15
84.9 2.95
80.97 3.84
76.81 4.76
72.48 5.65
68.01 6.46
63.4 7.14
58.67 7.7
53.86 8.13
49.02 8.42
44.16 8.58
39.36 8.63
34.65 8.56
30.08 8.37
25.71 8.07
21.58 7.67
17.72 7.17
14.18 6.57
10.99 5.88
8.17 5.11
5.75 4.28
3.74 3.41
2.16 2.51
1.01 1.61
0.28 0.76
0.02 0.15
0 0
0 0
0.02 -0.14
0.09 -0.26
0.22 -0.38
0.33 -0.47
1.29 -0.97
2.8 -1.45
4.84 -1.89
7.38 -2.29
10.39 -2.64
13.85 -2.94
17.7 -3.19
21.92 -3.39
26.45 -3.54
31.24 -3.64
36.24 -3.7
41.39 -3.71
46.62 -3.68
51.89 -3.6
57.13 -3.48
62.28 -3.31
67.28 -3.1
72.07 -2.85
76.59 -2.54
80.83 -2.15
84.77 -1.69
88.39 -1.22
91.66 -0.8
94.49 -0.45
96.8 -0.21
98.54 -0.06
99.63 -0.01
100 0
V 1.1