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Winfoil Airfoils - Total Number: 277
Name T/C % Camber % Camber Chord % CL Max CD Min
1 2 3 4 5 Next > Last >>
WB14035 13.92 3.58 45 1.58 0.0099
WB13535 13.54 3.747 50 0.84 0.0241
USA 50 AIRFOIL 7.01 1.953 40 0.986 0.005
TSAGI 8% AIRFOIL 7.94 1.343 30 0.923 0.0045
TSAGI 12% AIRFOIL 11.88 2.003 30 1.217 0.0058
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
1.25 1.875 1.25 -1.35
2.5 3 2.5 -1.8
5 4.63 5 -2.65
7.5 5.9 7.5 -3.275
10 6.95 10 -3.675
12.5 7.7 12.5 -3.95
15 8.325 15 -4.05
17.5 8.83 17.5 -4.075
20 9.225 20 -4.05
22.5 9.55 22.5 -4.025
25 9.775 25 -3.95
27.5 10.05 27.5 -3.8
30 10.225 30 -3.7
35 10.45 35 -3.475
40 10.45 40 -3.225
45 10.365 45 -2.975
50 10.125 50 -2.75
55 9.725 55 -2.475
60 9.1 60 -2.275
65 8.3 65 -2.05
70 7.1 70 -1.8
75 6.275 75 -1.575
80 5.15 80 -1.3
85 4 85 -1.025
90 2.775 90 -0.8
95 1.475 95 -0.5
100 0.25 100 -0.25
X Y
1 0.0025
0.95 0.01475
0.9 0.02775
0.85 0.04
0.8 0.0515
0.75 0.06275
0.7 0.071
0.65 0.083
0.6 0.091
0.55 0.09725
0.5 0.10125
0.45 0.10365
0.4 0.1045
0.35 0.1045
0.3 0.10225
0.275 0.1005
0.25 0.09775
0.225 0.0955
0.2 0.09225
0.175 0.0883
0.15 0.08325
0.125 0.077
0.1 0.0695
0.075 0.059
0.05 0.0463
0.025 0.03
0.0125 0.01875
0 0
0 0
0.0125 -0.0135
0.025 -0.018
0.05 -0.0265
0.075 -0.03275
0.1 -0.03675
0.125 -0.0395
0.15 -0.0405
0.175 -0.04075
0.2 -0.0405
0.225 -0.04025
0.25 -0.0395
0.275 -0.038
0.3 -0.037
0.35 -0.03475
0.4 -0.03225
0.45 -0.02975
0.5 -0.0275
0.55 -0.02475
0.6 -0.02275
0.65 -0.0205
0.7 -0.018
0.75 -0.01575
0.8 -0.013
0.85 -0.01025
0.9 -0.008
0.95 -0.005
1 -0.0025
X Y
100 0.25
95 1.475
90 2.775
85 4
80 5.15
75 6.275
70 7.1
65 8.3
60 9.1
55 9.725
50 10.125
45 10.365
40 10.45
35 10.45
30 10.225
27.5 10.05
25 9.775
22.5 9.55
20 9.225
17.5 8.83
15 8.325
12.5 7.7
10 6.95
7.5 5.9
5 4.63
2.5 3
1.25 1.875
0 0
0 0
1.25 -1.35
2.5 -1.8
5 -2.65
7.5 -3.275
10 -3.675
12.5 -3.95
15 -4.05
17.5 -4.075
20 -4.05
22.5 -4.025
25 -3.95
27.5 -3.8
30 -3.7
35 -3.475
40 -3.225
45 -2.975
50 -2.75
55 -2.475
60 -2.275
65 -2.05
70 -1.8
75 -1.575
80 -1.3
85 -1.025
90 -0.8
95 -0.5
100 -0.25
V 1.1