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Winfoil Airfoils - Total Number: 277
Name T/C % Camber % Camber Chord % CL Max CD Min
<< First < Prev 45 46 47 48 49 Next > Last >>
RITZ 2-30-10 9.99 2.01 35 0.904 0.0075
RITZ 3-30-10 9.98 2.983 30 1.221 0.0094
S.I. 53009 9.07 5.007 30 1.178 0.009
S.I. 64009 9.23 6.045 40 1.515 0.0093
S2048 8.62 1.952 55.17 1.102 0.0053
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
0.07 0.55 0.07 -0.29
0.4 0.95 0.4 -0.69
1 1.47 1 -1.13
2 2.08 2 -1.5
4 3.06 4 -2.02
6 3.83 6 -2.32
8 4.5 8 -2.45
10 5 10 -2.65
15 5.95 15 -2.8
20 6.55 20 -2.95
25 6.9 25 -3.02
30 7 30 -3
35 6.94 35 -2.93
40 6.7 40 -2.8
45 6.4 45 -2.64
50 6 50 -2.45
55 5.59 55 -2.29
60 5.15 60 -2.15
65 4.67 65 -1.96
70 4.15 70 -1.75
75 3.58 75 -1.53
80 2.95 80 -1.3
85 2.29 85 -1.06
90 1.6 90 -0.8
95 0.85 95 -0.5
100 0 100 0
X Y
1 0
0.95 0.0085
0.9 0.016
0.85 0.0229
0.8 0.0295
0.75 0.0358
0.7 0.0415
0.65 0.0467
0.6 0.0515
0.55 0.0559
0.5 0.06
0.45 0.064
0.4 0.067
0.35 0.0694
0.3 0.07
0.25 0.069
0.2 0.0655
0.15 0.0595
0.1 0.05
0.08 0.045
0.06 0.0383
0.04 0.0306
0.02 0.0208
0.01 0.0147
0.004 0.0095
0.0007 0.0055
0 0
0 0
0.0007 -0.0029
0.004 -0.0069
0.01 -0.0113
0.02 -0.015
0.04 -0.0202
0.06 -0.0232
0.08 -0.0245
0.1 -0.0265
0.15 -0.028
0.2 -0.0295
0.25 -0.0302
0.3 -0.03
0.35 -0.0293
0.4 -0.028
0.45 -0.0264
0.5 -0.0245
0.55 -0.0229
0.6 -0.0215
0.65 -0.0196
0.7 -0.0175
0.75 -0.0153
0.8 -0.013
0.85 -0.0106
0.9 -0.008
0.95 -0.005
1 0
X Y
100 0
95 0.85
90 1.6
85 2.29
80 2.95
75 3.58
70 4.15
65 4.67
60 5.15
55 5.59
50 6
45 6.4
40 6.7
35 6.94
30 7
25 6.9
20 6.55
15 5.95
10 5
8 4.5
6 3.83
4 3.06
2 2.08
1 1.47
0.4 0.95
0.07 0.55
0 0
0 0
0.07 -0.29
0.4 -0.69
1 -1.13
2 -1.5
4 -2.02
6 -2.32
8 -2.45
10 -2.65
15 -2.8
20 -2.95
25 -3.02
30 -3
35 -2.93
40 -2.8
45 -2.64
50 -2.45
55 -2.29
60 -2.15
65 -1.96
70 -1.75
75 -1.53
80 -1.3
85 -1.06
90 -0.8
95 -0.5
100 0
V 1.1