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Winfoil Airfoils - Total Number: 277
Name T/C % T/C % Chord Position Camber % Camber Chord % CL Max CD Min
<< First < Prev 35 36 37 38 39 Next > Last >>
HQ2.5/9 8.92 40 2.508 60 1.318 0.0076
HQ2.5/8 7.93 40 2.517 50 0.997 0.0097
HQ2.5/10 9.92 40 2.517 50 1.203 0.0103
HN93-S.885 8.83 25 0 0 0.802 0.0056
HN93-S.800 7.98 25 0 0 0.749 0.0049
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
0.5 1 0.5 -0.6
1.25 1.7 1.25 -0.9
2.5 2.6 2.5 -1.2
5 3.5 5 -1.5
10 4.8 10 -1.8
15 5.7 15 -1.9
20 6.3 20 -2.1
25 6.6 25 -2.2
30 6.7 30 -2.1
40 6.9 40 -2.1
50 6.6 50 -1.6
60 6 60 -1
70 4.7 70 -0.3
80 3.4 80 0.2
85 2.6 85 0.4
90 1.7 90 0.3
95 0.9 95 0.3
100 0 100 0
X Y
1 0
0.95 0.009
0.9 0.017
0.85 0.026
0.8 0.034
0.7 0.047
0.6 0.06
0.5 0.066
0.4 0.069
0.3 0.067
0.25 0.066
0.2 0.063
0.15 0.057
0.1 0.048
0.05 0.035
0.025 0.026
0.0125 0.017
0.005 0.01
0 0
0 0
0.005 -0.006
0.0125 -0.009
0.025 -0.012
0.05 -0.015
0.1 -0.018
0.15 -0.019
0.2 -0.021
0.25 -0.022
0.3 -0.021
0.4 -0.021
0.5 -0.016
0.6 -0.01
0.7 -0.003
0.8 0.002
0.85 0.004
0.9 0.003
0.95 0.003
1 0
X Y
100 0
95 0.9
90 1.7
85 2.6
80 3.4
70 4.7
60 6
50 6.6
40 6.9
30 6.7
25 6.6
20 6.3
15 5.7
10 4.8
5 3.5
2.5 2.6
1.25 1.7
0.5 1
0 0
0 0
0.5 -0.6
1.25 -0.9
2.5 -1.2
5 -1.5
10 -1.8
15 -1.9
20 -2.1
25 -2.2
30 -2.1
40 -2.1
50 -1.6
60 -1
70 -0.3
80 0.2
85 0.4
90 0.3
95 0.3
100 0
V 1.1