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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 37 38 39 40 41 Next > Last >>
GOTTINGEN 532 12.49 25 4.84 40 0.697 0.006
GOTTINGEN 398 13.75 30 4.409 40 1.815 0.0136
GOTTINGE.COR 13.75 30 4.409 40 1.699 0.016
FX63-137 13.67 30.87 5.84 56.53 2.199 0.0076
FX 60-100 9.97 27.89 3.477 56.53 1.424 0.0062
Coordinates
XUpper YUpper XLower YLower
0 2.45 0 2.45
0.5 4 0.5 1.9
0.98 4.95 0.98 1.42
1 4.9 1 1.6
1.96 6.48 1.96 0.96
2.5 7.05 2.5 0.8
5 8.55 5 0.5
7.5 9.65 7.5 0.3
10 10.5 10 0.15
15 11.6 15 0
20 12.25 20 0
25 12.6 25 0.1
30 12.75 30 0.25
40 12.05 40 0.65
50 10.7 50 1.05
60 9 60 1.35
70 7.1 70 1.5
80 4.9 80 1.35
90 2.6 90 0.45
100 0.1 100 0.1
X Y
1 0.001
0.9 0.026
0.8 0.049
0.7 0.071
0.6 0.09
0.5 0.107
0.4 0.1205
0.3 0.1275
0.25 0.126
0.2 0.1225
0.15 0.116
0.1 0.105
0.075 0.0965
0.05 0.0855
0.025 0.0705
0.0196 0.0648
0.01 0.049
0.0098 0.0495
0.005 0.04
0 0.0245
0 0.0245
0.005 0.019
0.0098 0.0142
0.01 0.016
0.0196 0.0096
0.025 0.008
0.05 0.005
0.075 0.003
0.1 0.0015
0.15 0
0.2 0
0.25 0.001
0.3 0.0025
0.4 0.0065
0.5 0.0105
0.6 0.0135
0.7 0.015
0.8 0.0135
0.9 0.0045
1 0.001
X Y
100 0.1
90 2.6
80 4.9
70 7.1
60 9
50 10.7
40 12.05
30 12.75
25 12.6
20 12.25
15 11.6
10 10.5
7.5 9.65
5 8.55
2.5 7.05
1.96 6.48
1 4.9
0.98 4.95
0.5 4
0 2.45
0 2.45
0.5 1.9
0.98 1.42
1 1.6
1.96 0.96
2.5 0.8
5 0.5
7.5 0.3
10 0.15
15 0
20 0
25 0.1
30 0.25
40 0.65
50 1.05
60 1.35
70 1.5
80 1.35
90 0.45
100 0.1
V 1.1