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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 16 17 18 19 20 Next > Last >>
GOTTINGEN 398 13.75 30 4.409 40 1.815 0.0136
GOTTINGEN 532 12.49 25 4.84 40 0.697 0.006
GOTTINGEN 549 13.83 30 4.688 40 1.706 0.0084
GOTTINGEN 622 8 30 2.38 40 1.015 0.011
HN93-285.935 9.35 30 2.846 40 1.035 0.006
Coordinates
XUpper YUpper XLower YLower
0 3.74 0 3.74
0.5 4.9 0.5 2.8
1 5.7 1 2.3
2.5 7.4 2.5 1.28
5 9.17 5 0.69
7.5 10.37 7.5 0.35
10 11.25 10 0.18
15 12.53 15 0.03
20 13.34 20 0
25 13.6 25 0
30 13.8 30 0.05
40 13.34 40 0.17
50 12.27 50 0.27
60 10.63 60 0.33
70 8.53 70 0.35
80 6.12 80 0.27
90 3.4 90 0.13
100 0.25 100 0
X Y
1 0.0025
0.9 0.034
0.8 0.0612
0.7 0.0853
0.6 0.1063
0.5 0.1227
0.4 0.1334
0.3 0.138
0.25 0.136
0.2 0.1334
0.15 0.1253
0.1 0.1125
0.075 0.1037
0.05 0.0917
0.025 0.074
0.01 0.057
0.005 0.049
0 0.0374
0 0.0374
0.005 0.028
0.01 0.023
0.025 0.0128
0.05 0.0069
0.075 0.0035
0.1 0.0018
0.15 0.0003
0.2 0
0.25 0
0.3 0.0005
0.4 0.0017
0.5 0.0027
0.6 0.0033
0.7 0.0035
0.8 0.0027
0.9 0.0013
1 0
X Y
100 0.25
90 3.4
80 6.12
70 8.53
60 10.63
50 12.27
40 13.34
30 13.8
25 13.6
20 13.34
15 12.53
10 11.25
7.5 10.37
5 9.17
2.5 7.4
1 5.7
0.5 4.9
0 3.74
0 3.74
0.5 2.8
1 2.3
2.5 1.28
5 0.69
7.5 0.35
10 0.18
15 0.03
20 0
25 0
30 0.05
40 0.17
50 0.27
60 0.33
70 0.35
80 0.27
90 0.13
100 0
V 1.1