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 % T/C % Chord Position Camber % Camber Chord % CL Max CD Min
<< First < Prev 41 42 43 44 45 Next > Last >>
EPPLER 205 10.48 29.7 3.007 34.1 1.09 0.0084
EPPLER 197 13.45 34.55 2.931 34.55 1.308 0.0068
EPPLER 193 MOD 11.86 30.97 4.147 39.98 1.429 0.0071
EPPLER 184 8.31 32.12 1.146 36.76 0.7 0.005
EPPLER 182 8.46 32.84 1.741 37.46 0.689 0.0033
Coordinates
XUpper YUpper XLower YLower
0 0 0 0.06
0.33 0.77 0.23 -0.51
1.1 1.59 1.07 -0.99
2.29 2.46 2.42 -1.42
3.91 3.34 4.29 -1.78
5.94 4.21 6.67 -2.05
8.36 5.04 9.53 -2.25
11.16 5.81 12.86 -2.38
14.3 6.51 16.63 -2.44
17.76 7.11 20.78 -2.44
21.51 7.61 25.29 -2.38
25.5 7.97 30.1 -2.29
29.7 8.18 35.15 -2.17
34.1 8.21 40.39 -2.02
38.68 8.08 45.75 -1.86
43.41 7.79 51.17 -1.69
48.27 7.34 56.59 -1.52
53.22 6.78 61.94 -1.35
58.22 6.15 67.15 -1.18
63.2 5.47 72.16 -1.02
68.11 4.78 76.91 -0.88
72.87 4.09 81.34 -0.74
77.41 3.42 85.4 -0.61
81.68 2.79 89.03 -0.5
85.62 2.2 92.2 -0.38
89.18 1.67 94.86 -0.25
92.29 1.2 97.02 -0.13
94.92 0.78 98.64 -0.04
99.65 0.0527 99.65 0
100 0 100 0
X Y
1 0
0.9965 0.000527
0.9492 0.0078
0.9229 0.012
0.8918 0.0167
0.8562 0.022
0.8168 0.0279
0.7741 0.0342
0.7287 0.0409
0.6811 0.0478
0.632 0.0547
0.5822 0.0615
0.5322 0.0678
0.4827 0.0734
0.4341 0.0779
0.3868 0.0808
0.341 0.0821
0.297 0.0818
0.255 0.0797
0.2151 0.0761
0.1776 0.0711
0.143 0.0651
0.1116 0.0581
0.0836 0.0504
0.0594 0.0421
0.0391 0.0334
0.0229 0.0246
0.011 0.0159
0.0033 0.0077
0 0
0 0.0006
0.0023 -0.0051
0.0107 -0.0099
0.0242 -0.0142
0.0429 -0.0178
0.0667 -0.0205
0.0953 -0.0225
0.1286 -0.0238
0.1663 -0.0244
0.2078 -0.0244
0.2529 -0.0238
0.301 -0.0229
0.3515 -0.0217
0.4039 -0.0202
0.4575 -0.0186
0.5117 -0.0169
0.5659 -0.0152
0.6194 -0.0135
0.6715 -0.0118
0.7216 -0.0102
0.7691 -0.0088
0.8134 -0.0074
0.854 -0.0061
0.8903 -0.005
0.922 -0.0038
0.9486 -0.0025
0.9702 -0.0013
0.9864 -0.0004
0.9965 0
1 0
X Y
100 0
99.65 0.0527
94.92 0.78
92.29 1.2
89.18 1.67
85.62 2.2
81.68 2.79
77.41 3.42
72.87 4.09
68.11 4.78
63.2 5.47
58.22 6.15
53.22 6.78
48.27 7.34
43.41 7.79
38.68 8.08
34.1 8.21
29.7 8.18
25.5 7.97
21.51 7.61
17.76 7.11
14.3 6.51
11.16 5.81
8.36 5.04
5.94 4.21
3.91 3.34
2.29 2.46
1.1 1.59
0.33 0.77
0 0
0 0.06
0.23 -0.51
1.07 -0.99
2.42 -1.42
4.29 -1.78
6.67 -2.05
9.53 -2.25
12.86 -2.38
16.63 -2.44
20.78 -2.44
25.29 -2.38
30.1 -2.29
35.15 -2.17
40.39 -2.02
45.75 -1.86
51.17 -1.69
56.59 -1.52
61.94 -1.35
67.15 -1.18
72.16 -1.02
76.91 -0.88
81.34 -0.74
85.4 -0.61
89.03 -0.5
92.2 -0.38
94.86 -0.25
97.02 -0.13
98.64 -0.04
99.65 0
100 0
V 1.1