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 52 53 54 55 56
EPPLER 378 4.08 8.109 35.92 1.686 0.0014
NACA 4403 3.03 3.971 42.2134 0.896 0.0051
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