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 1 2 3 4 5 Next > Last >>
NACA 653-618 17.97 3.324 50 1.618 0.0085
NACA 23018 17.96 1.835 15 1.275 0.0132
NACA 2418 17.96 1.95 40 1.367 0.0128
NACA 65-218 17.95 1.123 50 1.399 0.0076
EPPLER 266 17.3 3.062 39.79 1.483 0.0066
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
0.172 1.446 0.828 -1.146
0.385 1.776 1.115 -1.356
0.839 2.293 1.661 -1.651
2.026 3.268 2.974 -2.152
4.462 4.776 5.538 -2.88
6.936 5.971 8.064 -3.427
9.431 6.978 10.569 -3.876
14.455 8.602 15.545 -4.564
19.506 9.848 20.494 -5.072
24.574 10.803 25.426 -5.433
29.652 11.504 30.348 -5.672
34.738 11.972 35.262 -5.792
39.826 12.21 40.174 -5.784
44.915 12.186 45.085 -5.616
50 11.877 50 -5.259
55.077 11.293 54.923 -4.723
60.141 10.479 59.859 -4.053
65.189 9.482 64.811 -3.302
70.219 8.338 69.781 -2.506
75.23 7.075 74.77 -1.705
80.22 5.719 79.78 -0.943
85.189 4.306 84.811 -0.268
90.138 2.863 89.862 0.239
95.068 1.433 94.932 0.463
100 0 100 0
X Y
1 0
0.95068 0.01433
0.90138 0.02863
0.85189 0.04306
0.8022 0.05719
0.7523 0.07075
0.70219 0.08338
0.65189 0.09482
0.60141 0.10479
0.55077 0.11293
0.5 0.11877
0.44915 0.12186
0.39826 0.1221
0.34738 0.11972
0.29652 0.11504
0.24574 0.10803
0.19506 0.09848
0.14455 0.08602
0.09431 0.06978
0.06936 0.05971
0.04462 0.04776
0.02026 0.03268
0.00839 0.02293
0.00385 0.01776
0.00172 0.01446
0 0
0 0
0.00828 -0.01146
0.01115 -0.01356
0.01661 -0.01651
0.02974 -0.02152
0.05538 -0.0288
0.08064 -0.03427
0.10569 -0.03876
0.15545 -0.04564
0.20494 -0.05072
0.25426 -0.05433
0.30348 -0.05672
0.35262 -0.05792
0.40174 -0.05784
0.45085 -0.05616
0.5 -0.05259
0.54923 -0.04723
0.59859 -0.04053
0.64811 -0.03302
0.69781 -0.02506
0.7477 -0.01705
0.7978 -0.00943
0.84811 -0.00268
0.89862 0.00239
0.94932 0.00463
1 0
X Y
100 0
95.068 1.433
90.138 2.863
85.189 4.306
80.22 5.719
75.23 7.075
70.219 8.338
65.189 9.482
60.141 10.479
55.077 11.293
50 11.877
44.915 12.186
39.826 12.21
34.738 11.972
29.652 11.504
24.574 10.803
19.506 9.848
14.455 8.602
9.431 6.978
6.936 5.971
4.462 4.776
2.026 3.268
0.839 2.293
0.385 1.776
0.172 1.446
0 0
0 0
0.828 -1.146
1.115 -1.356
1.661 -1.651
2.974 -2.152
5.538 -2.88
8.064 -3.427
10.569 -3.876
15.545 -4.564
20.494 -5.072
25.426 -5.433
30.348 -5.672
35.262 -5.792
40.174 -5.784
45.085 -5.616
50 -5.259
54.923 -4.723
59.859 -4.053
64.811 -3.302
69.781 -2.506
74.77 -1.705
79.78 -0.943
84.811 -0.268
89.862 0.239
94.932 0.463
100 0
V 1.1