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Winfoil Airfoils - Total Number: 277
Name T/C % Camber % Camber Chord % CL Max CD Min
<< First < Prev 26 27 28 29 30 Next > Last >>
NACA 0009 8.97 0 0 0.871 0.0065
NACA 0010 9.97 0 0 0.877 0.0016
NACA 0012 11.96 0 0 1.108 0.0092
NACA 0015 15.01 0 0 1.287 0.0064
NACA 0016 15.91 0 0 1.332 0.0106
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
1.25 1.42 1.25 -1.42
2.5 1.96 2.5 -1.96
5 2.67 5 -2.67
7.5 3.15 7.5 -3.15
10 3.51 10 -3.51
15 4.01 15 -4.01
20 4.3 20 -4.3
25 4.46 25 -4.46
30 4.5 30 -4.5
40 4.35 40 -4.35
50 3.97 50 -3.97
60 3.42 60 -3.42
70 2.75 70 -2.75
80 1.97 80 -1.97
90 1.09 90 -1.09
95 0.61 95 -0.61
100 0.1 100 -0.1
V 1.0