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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 46 47 48 49 50 Next > Last >>
ARA-D 13% 13 25 3.34 30 1.713 0.0247
ARA-D 10% 10.01 25 3.724 35 1.741 0.0202
AQUILA 9.3% Smoothed 9.38 31.333 4.049 34.667 1.421 0.0046
AQUILA 9.39 31.33 4.045 34.67 1.426 0.0051
AMSOIL 11.62 39 1.93 39 1.412 0.0122
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
0.3 1.66 0.3 -0.88
1 3.05 1 -1.54
2 4.27 2 -2.05
4 5.88 4 -2.63
7 7.4 7 -3.03
10 8.38 10 -3.18
15 9.34 15 -3.17
20 9.83 20 -3.06
25 10.05 25 -2.94
30 10.07 30 -2.85
35 9.93 35 -2.76
40 9.64 40 -2.68
45 9.22 45 -2.58
50 8.7 50 -2.48
55 8.09 55 -2.36
60 7.42 60 -2.24
65 6.68 65 -2.12
70 5.9 70 -1.98
75 5.09 75 -1.83
80 4.26 80 -1.67
85 3.42 85 -1.49
90 2.58 90 -1.29
95 1.74 95 -1.07
97.5 1.32 97.5 -0.97
100 0.9 100 -0.9
X Y
1 0.009
0.975 0.0132
0.95 0.0174
0.9 0.0258
0.85 0.0342
0.8 0.0426
0.75 0.0509
0.7 0.059
0.65 0.0668
0.6 0.0742
0.55 0.0809
0.5 0.087
0.45 0.0922
0.4 0.0964
0.35 0.0993
0.3 0.1007
0.25 0.1005
0.2 0.0983
0.15 0.0934
0.1 0.0838
0.07 0.074
0.04 0.0588
0.02 0.0427
0.01 0.0305
0.003 0.0166
0 0
0 0
0.003 -0.0088
0.01 -0.0154
0.02 -0.0205
0.04 -0.0263
0.07 -0.0303
0.1 -0.0318
0.15 -0.0317
0.2 -0.0306
0.25 -0.0294
0.3 -0.0285
0.35 -0.0276
0.4 -0.0268
0.45 -0.0258
0.5 -0.0248
0.55 -0.0236
0.6 -0.0224
0.65 -0.0212
0.7 -0.0198
0.75 -0.0183
0.8 -0.0167
0.85 -0.0149
0.9 -0.0129
0.95 -0.0107
0.975 -0.0097
1 -0.009
X Y
100 0.9
97.5 1.32
95 1.74
90 2.58
85 3.42
80 4.26
75 5.09
70 5.9
65 6.68
60 7.42
55 8.09
50 8.7
45 9.22
40 9.64
35 9.93
30 10.07
25 10.05
20 9.83
15 9.34
10 8.38
7 7.4
4 5.88
2 4.27
1 3.05
0.3 1.66
0 0
0 0
0.3 -0.88
1 -1.54
2 -2.05
4 -2.63
7 -3.03
10 -3.18
15 -3.17
20 -3.06
25 -2.94
30 -2.85
35 -2.76
40 -2.68
45 -2.58
50 -2.48
55 -2.36
60 -2.24
65 -2.12
70 -1.98
75 -1.83
80 -1.67
85 -1.49
90 -1.29
95 -1.07
97.5 -0.97
100 -0.9
V 1.1