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Winfoil Airfoils - Total Number: 277
Name T/C % Camber % Camber Chord % CL Max CD Min
<< First < Prev 18 19 20 21 22 Next > Last >>
HQ2.5/8 7.93 2.517 50 0.997 0.0097
HQ2.5/9 8.92 2.508 60 1.318 0.0076
HQ2/9 smoothed 8.96 2.006 50 1.191 0.0054
J5012 11.99 0 0 1.039 0.0053
KC-135 BL52.44 15.45 1.015 25 1.382 0.0079
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
0.5 0.9 0.5 -0.5
1.25 1.5 1.25 -0.7
2.5 2.4 2.5 -1
5 3.36 5 -1.2
10 4.3 10 -1.5
15 5.3 15 -1.6
20 5.9 20 -1.7
25 6.1 25 -1.7
30 6.2 30 -1.6
40 6.4 40 -1.6
50 6.2 50 -1.2
60 5.6 60 -0.6
70 4.4 70 0
80 3.2 80 0.4
85 2.5 85 0.5
90 1.6 90 0.4
95 0.9 95 0.3
100 0 100 0
V 1.0