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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
X Y
1 0
0.95 0.009
0.9 0.016
0.85 0.025
0.8 0.032
0.7 0.044
0.6 0.056
0.5 0.062
0.4 0.064
0.3 0.062
0.25 0.061
0.2 0.059
0.15 0.053
0.1 0.043
0.05 0.0336
0.025 0.024
0.0125 0.015
0.005 0.009
0 0
0 0
0.005 -0.005
0.0125 -0.007
0.025 -0.01
0.05 -0.012
0.1 -0.015
0.15 -0.016
0.2 -0.017
0.25 -0.017
0.3 -0.016
0.4 -0.016
0.5 -0.012
0.6 -0.006
0.7 0
0.8 0.004
0.85 0.005
0.9 0.004
0.95 0.003
1 0
X Y
100 0
95 0.9
90 1.6
85 2.5
80 3.2
70 4.4
60 5.6
50 6.2
40 6.4
30 6.2
25 6.1
20 5.9
15 5.3
10 4.3
5 3.36
2.5 2.4
1.25 1.5
0.5 0.9
0 0
0 0
0.5 -0.5
1.25 -0.7
2.5 -1
5 -1.2
10 -1.5
15 -1.6
20 -1.7
25 -1.7
30 -1.6
40 -1.6
50 -1.2
60 -0.6
70 0
80 0.4
85 0.5
90 0.4
95 0.3
100 0
V 1.1