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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 2 3 4 5 6 Next > Last >>
EPPLER 378 4.08 10.36 8.109 35.92 1.686 0.0014
CLARK K 11.38 39.65 3.245 39.65 1.676 0.0066
NACA 4412 12.02 30 3.943 40 1.649 0.0029
CLARK W 11.21 30 3.684 40 1.643 0.0075
ATR 14.52 25.4 2.882 21.4 1.632 0.0092
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