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Winfoil Airfoils - Total Number: 277
Name T/C % Camber % Camber Chord % CL Max CD Min
<< First < Prev 21 22 23 24 25 Next > Last >>
NACA 63-209 8.99 1.11 50 0.756 0.006
NACA 63-206 5.99 1.108 50 0.62 0.0052
NACA 631-412 11.98 2.215 50 1.268 0.007
NACA 631-212 11.98 1.108 50 1.071 0.0068
NACA 63-010 9.98 0 0 0.699 0.0065
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
0.2 0.6 0.2 -0.4
0.44 0.8 0.56 -0.7
0.68 0.97 0.82 -0.83
1.17 1.26 1.33 -1.04
2.41 1.77 2.59 -1.39
4.9 2.51 5.1 -1.88
7.39 3.08 7.61 -2.23
9.89 3.54 10.11 -2.51
14.9 4.26 15.1 -2.92
19.91 4.79 20.09 -3.2
24.93 5.17 25.08 -3.38
29.94 5.41 30.06 -3.47
34.96 5.53 35.04 -3.47
39.97 5.52 40.03 -3.38
44.99 5.39 45.01 -3.2
50 5.16 50 -2.95
55.01 4.83 54.99 -2.64
60.02 4.43 59.98 -2.29
65.03 3.96 64.97 -1.9
70.03 3.43 69.97 -1.49
75.03 2.86 74.97 -1.07
80.03 2.27 79.97 -0.68
85.03 1.66 84.97 -0.32
90.02 1.07 89.98 -0.03
95.01 0.51 94.99 0.12
100 0 100 0
V 1.0