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Winfoil Airfoils - Total Number: 277
Name T/C % Camber % Camber Chord % CL Max CD Min
<< First < Prev 14 15 16 17 18 Next > Last >>
NACA M20 8.26 5.939 30 1.436 0.0096
NACA M12 11.9 1.942 30 1.382 0.01
NACA 747A415 14.98 3.048 34.96 1.297 0.0076
NACA 747A315 14.97 2.531 35 1.2 0.0102
NACA 671-215 14.98 1.111 50 0.803 0.0001
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
1.25 1.7 1.25 -0.97
2.5 2.6 2.5 -0.94
5 4.17 5 -0.57
7.5 5.37 7.5 -0.13
10 6.47 10 0.31
15 8.03 15 1.03
20 9.14 20 1.56
30 10.21 30 2.06
40 9.99 40 1.9
50 8.92 50 1.33
60 7.3 60 0.58
70 5.4 70 -0.12
80 3.5 80 -0.55
90 1.78 90 -0.56
95 1.06 95 -0.36
100 0.47 100 0
V 1.0