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Winfoil Airfoils - Total Number: 277
Name T/C % T/C % Chord Position Camber % Camber Chord % CL Max CD Min
< Prev 1 2 3 4 5 Next > Last >>
SPICA 11.72 30 4.736 35 1.707 0.0071
SD8040 10 29.71 2.59 39.07 1.404 0.0065
SD8020 10.09 27.52 0.084 0.28 0.945 0.006
SD8000 8.85 29.4 1.817 43.88 1.162 0.0057
SD7090 9.98 29.27 1.93 33.89 1.277 0.0058
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
1 2.05 1 -1.28
2 3.04 2 -1.51
4 4.56 4 -1.63
6 5.7 6 -1.59
8 6.63 8 -1.56
10 7.4 10 -1.53
15 8.81 15 -1.45
20 9.69 20 -1.36
25 10.24 25 -1.28
30 10.53 30 -1.19
35 10.58 35 -1.11
40 10.42 40 -1.02
45 10.05 45 -0.94
50 9.49 50 -0.85
55 8.77 55 -0.77
60 7.97 60 -0.68
65 7.11 65 -0.6
70 6.19 70 -0.51
75 5.24 75 -0.43
80 4.26 80 -0.34
85 3.28 85 -0.26
90 2.27 90 -0.17
95 1.2 95 -0.09
100 0 100 0
X Y
1 0
0.95 0.012
0.9 0.0227
0.85 0.0328
0.8 0.0426
0.75 0.0524
0.7 0.0619
0.65 0.0711
0.6 0.0797
0.55 0.0877
0.5 0.0949
0.45 0.1005
0.4 0.1042
0.35 0.1058
0.3 0.1053
0.25 0.1024
0.2 0.0969
0.15 0.0881
0.1 0.074
0.08 0.0663
0.06 0.057
0.04 0.0456
0.02 0.0304
0.01 0.0205
0 0
0 0
0.01 -0.0128
0.02 -0.0151
0.04 -0.0163
0.06 -0.0159
0.08 -0.0156
0.1 -0.0153
0.15 -0.0145
0.2 -0.0136
0.25 -0.0128
0.3 -0.0119
0.35 -0.0111
0.4 -0.0102
0.45 -0.0094
0.5 -0.0085
0.55 -0.0077
0.6 -0.0068
0.65 -0.006
0.7 -0.0051
0.75 -0.0043
0.8 -0.0034
0.85 -0.0026
0.9 -0.0017
0.95 -0.0009
1 0
X Y
100 0
95 1.2
90 2.27
85 3.28
80 4.26
75 5.24
70 6.19
65 7.11
60 7.97
55 8.77
50 9.49
45 10.05
40 10.42
35 10.58
30 10.53
25 10.24
20 9.69
15 8.81
10 7.4
8 6.63
6 5.7
4 4.56
2 3.04
1 2.05
0 0
0 0
1 -1.28
2 -1.51
4 -1.63
6 -1.59
8 -1.56
10 -1.53
15 -1.45
20 -1.36
25 -1.28
30 -1.19
35 -1.11
40 -1.02
45 -0.94
50 -0.85
55 -0.77
60 -0.68
65 -0.6
70 -0.51
75 -0.43
80 -0.34
85 -0.26
90 -0.17
95 -0.09
100 0
V 1.1