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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 45 46 47 48 49 Next > Last >>
RITZ 2-30-10 9.99 30 2.01 35 0.904 0.0075
RITZ 3-30-10 9.98 30 2.983 30 1.221 0.0094
S.I. 53009 9.07 30 5.007 30 1.178 0.009
S.I. 64009 9.23 30 6.045 40 1.515 0.0093
S2048 8.62 35.35 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