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 2 3 4 5 6 Next > Last >>
EPPLER 1200 16.93 3.48 40.77 1.818 0.0072
P-51D ROOT (BL17.5) 16.45 1.266 68.267 1.482 0.0063
S8036 (16%) 16 1.821 36.848 1.538 0.0054
S8036 15.99 1.825 36.85 1.538 0.005
S8037 15.98 2.431 36.9 1.574 0.005
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
0.13 0.72 0.5 -1.06
1.59 3.1 1.61 -1.77
2.93 4.33 3.27 -2.43
4.67 5.53 5.44 -3.03
6.81 6.68 8.1 -3.56
9.34 7.74 11.22 -4.01
12.24 8.69 14.77 -4.38
15.5 9.52 18.7 -4.68
19.1 10.23 22.97 -4.9
23.01 10.81 27.52 -5.06
27.18 11.28 32.3 -5.13
31.56 11.61 37.24 -5.12
36.11 11.81 42.29 -5.01
40.77 11.86 47.38 -4.8
45.49 11.77 52.48 -4.44
50.21 11.5 57.57 -3.92
54.91 11.05 62.65 -3.26
59.55 10.39 67.71 -2.49
64.14 9.54 72.73 -1.72
68.69 8.51 77.62 -1.01
73.16 7.39 82.28 -0.43
77.51 6.25 86.6 0
81.65 5.14 90.47 0.25
85.53 4.08 93.8 0.35
89.07 3.12 96.49 0.3
92.19 2.27 98.44 0.18
94.84 1.54 99.61 0.05
100 0 100 0
X Y
1 0
0.9484 0.0154
0.9219 0.0227
0.8907 0.0312
0.8553 0.0408
0.8165 0.0514
0.7751 0.0625
0.7316 0.0739
0.6869 0.0851
0.6414 0.0954
0.5955 0.1039
0.5491 0.1105
0.5021 0.115
0.4549 0.1177
0.4077 0.1186
0.3611 0.1181
0.3156 0.1161
0.2718 0.1128
0.2301 0.1081
0.191 0.1023
0.155 0.0952
0.1224 0.0869
0.0934 0.0774
0.0681 0.0668
0.0467 0.0553
0.0293 0.0433
0.0159 0.031
0.0013 0.0072
0 0
0 0
0.005 -0.0106
0.0161 -0.0177
0.0327 -0.0243
0.0544 -0.0303
0.081 -0.0356
0.1122 -0.0401
0.1477 -0.0438
0.187 -0.0468
0.2297 -0.049
0.2752 -0.0506
0.323 -0.0513
0.3724 -0.0512
0.4229 -0.0501
0.4738 -0.048
0.5248 -0.0444
0.5757 -0.0392
0.6265 -0.0326
0.6771 -0.0249
0.7273 -0.0172
0.7762 -0.0101
0.8228 -0.0043
0.866 0
0.9047 0.0025
0.938 0.0035
0.9649 0.003
0.9844 0.0018
0.9961 0.0005
1 0
X Y
100 0
94.84 1.54
92.19 2.27
89.07 3.12
85.53 4.08
81.65 5.14
77.51 6.25
73.16 7.39
68.69 8.51
64.14 9.54
59.55 10.39
54.91 11.05
50.21 11.5
45.49 11.77
40.77 11.86
36.11 11.81
31.56 11.61
27.18 11.28
23.01 10.81
19.1 10.23
15.5 9.52
12.24 8.69
9.34 7.74
6.81 6.68
4.67 5.53
2.93 4.33
1.59 3.1
0.13 0.72
0 0
0 0
0.5 -1.06
1.61 -1.77
3.27 -2.43
5.44 -3.03
8.1 -3.56
11.22 -4.01
14.77 -4.38
18.7 -4.68
22.97 -4.9
27.52 -5.06
32.3 -5.13
37.24 -5.12
42.29 -5.01
47.38 -4.8
52.48 -4.44
57.57 -3.92
62.65 -3.26
67.71 -2.49
72.73 -1.72
77.62 -1.01
82.28 -0.43
86.6 0
90.47 0.25
93.8 0.35
96.49 0.3
98.44 0.18
99.61 0.05
100 0
V 1.1