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 38 39 40 41 42 Next > Last >>
NACA 663-418 17.98 2.216 50 1.394 0.0076
NACA 664-221 20.98 1.119 50 1.434 0.008
NACA 671-215 14.98 1.111 50 0.803 0.0001
NACA 747A315 14.97 2.531 35 1.2 0.0102
NACA 747A415 14.98 3.048 34.96 1.297 0.0076
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
0.1 1 0.1 -0.35
0.2 1.2 0.2 -0.6
0.28 1.41 0.72 -1.21
0.51 1.69 0.99 -1.41
0.98 2.15 1.52 -1.72
2.19 3 2.81 -2.26
4.66 4.31 5.34 -3.04
7.14 5.35 7.86 -3.65
9.64 6.23 10.36 -4.16
14.65 7.67 15.35 -4.98
19.68 8.77 20.32 -5.59
24.73 9.63 25.27 -6.05
29.78 10.29 30.23 -6.4
34.83 10.76 35.17 -6.64
39.89 11.06 40.12 -6.78
44.94 11.19 45.06 -6.81
50 11.15 50 -6.74
55.06 10.92 54.94 -6.54
60.11 10.46 59.89 -6.18
65.15 9.64 64.85 -5.52
70.18 8.54 69.82 -4.65
75.19 7.24 74.81 -3.66
80.19 5.79 79.82 -2.61
85.16 4.28 84.84 -1.58
90.12 2.74 89.88 -0.68
95.06 1.28 94.94 -0.01
100 0 100 0
V 1.0