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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 52 53 54 55 56
WB13535 13.54 25 3.747 50 0.84 0.0241
WB14035 13.92 30 3.58 45 1.58 0.0099
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
1.25 1.875 1.25 -1.2
2.5 3 2.5 -1.8
5 4.65 5 -2.67
7.5 5.9 7.5 -3.275
10 6.915 10 -3.685
12.5 7.7 12.5 -3.93
15 8.325 15 -4.05
17.5 8.825 17.5 -4.085
20 9.2 20 -4.06
22.5 9.47 22.5 -3.995
25 9.66 25 -3.89
27.5 9.8 27.5 -3.75
30 9.9 30 -3.575
35 10 35 -3.185
40 9.975 40 -2.775
45 9.79 45 -2.35
50 9.425 50 -1.925
55 8.875 55 -1.532
60 8.175 60 -1.2
65 7.36 65 -0.94
70 6.465 70 -0.75
75 5.51 75 -0.6
80 4.5 80 -0.5
85 3.425 85 -0.4
90 2.31 90 -0.325
95 1.2 95 -0.25
100 0 100 0
X Y
1 0
0.95 0.012
0.9 0.0231
0.85 0.03425
0.8 0.045
0.75 0.0551
0.7 0.06465
0.65 0.0736
0.6 0.08175
0.55 0.08875
0.5 0.09425
0.45 0.0979
0.4 0.09975
0.35 0.1
0.3 0.099
0.275 0.098
0.25 0.0966
0.225 0.0947
0.2 0.092
0.175 0.08825
0.15 0.08325
0.125 0.077
0.1 0.06915
0.075 0.059
0.05 0.0465
0.025 0.03
0.0125 0.01875
0 0
0 0
0.0125 -0.012
0.025 -0.018
0.05 -0.0267
0.075 -0.03275
0.1 -0.03685
0.125 -0.0393
0.15 -0.0405
0.175 -0.04085
0.2 -0.0406
0.225 -0.03995
0.25 -0.0389
0.275 -0.0375
0.3 -0.03575
0.35 -0.03185
0.4 -0.02775
0.45 -0.0235
0.5 -0.01925
0.55 -0.01532
0.6 -0.012
0.65 -0.0094
0.7 -0.0075
0.75 -0.006
0.8 -0.005
0.85 -0.004
0.9 -0.00325
0.95 -0.0025
1 0
X Y
100 0
95 1.2
90 2.31
85 3.425
80 4.5
75 5.51
70 6.465
65 7.36
60 8.175
55 8.875
50 9.425
45 9.79
40 9.975
35 10
30 9.9
27.5 9.8
25 9.66
22.5 9.47
20 9.2
17.5 8.825
15 8.325
12.5 7.7
10 6.915
7.5 5.9
5 4.65
2.5 3
1.25 1.875
0 0
0 0
1.25 -1.2
2.5 -1.8
5 -2.67
7.5 -3.275
10 -3.685
12.5 -3.93
15 -4.05
17.5 -4.085
20 -4.06
22.5 -3.995
25 -3.89
27.5 -3.75
30 -3.575
35 -3.185
40 -2.775
45 -2.35
50 -1.925
55 -1.532
60 -1.2
65 -0.94
70 -0.75
75 -0.6
80 -0.5
85 -0.4
90 -0.325
95 -0.25
100 0
V 1.1