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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 8 9 10 11 12 Next > Last >>
RITZ 3-30-10 9.98 30 2.983 30 1.221 0.0094
RITZ 2-30-10 9.99 30 2.01 35 0.904 0.0075
RITZ 1-30-10 9.94 30 0.999 30 1.008 0.0093
RG8 10.78 30 2.224 60 1.096 0.0069
RG 15 8.92 30.25 1.761 39.73 1.11 0.0057
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
0.09 0.49 0.09 -0.28
0.31 0.89 0.31 -0.49
1.25 1.75 1.25 -1
2.5 2.6 2.5 -1.2
5 4 5 -1.4
7.5 5.05 7.5 -1.55
10 5.8 10 -1.7
15 6.9 15 -1.85
20 7.55 20 -1.95
30 8 30 -2
40 7.7 40 -1.9
50 6.9 50 -1.7
60 5.85 60 -1.5
70 4.7 70 -1.2
80 3.3 80 -0.9
90 1.75 90 -0.6
95 0.95 95 -0.35
100 0.1 100 -0.1
X Y
1 0.001
0.95 0.0095
0.9 0.0175
0.8 0.033
0.7 0.047
0.6 0.0585
0.5 0.069
0.4 0.077
0.3 0.08
0.2 0.0755
0.15 0.069
0.1 0.058
0.075 0.0505
0.05 0.04
0.025 0.026
0.0125 0.0175
0.0031 0.0089
0.0009 0.0049
0 0
0 0
0.0009 -0.0028
0.0031 -0.0049
0.0125 -0.01
0.025 -0.012
0.05 -0.014
0.075 -0.0155
0.1 -0.017
0.15 -0.0185
0.2 -0.0195
0.3 -0.02
0.4 -0.019
0.5 -0.017
0.6 -0.015
0.7 -0.012
0.8 -0.009
0.9 -0.006
0.95 -0.0035
1 -0.001
X Y
100 0.1
95 0.95
90 1.75
80 3.3
70 4.7
60 5.85
50 6.9
40 7.7
30 8
20 7.55
15 6.9
10 5.8
7.5 5.05
5 4
2.5 2.6
1.25 1.75
0.31 0.89
0.09 0.49
0 0
0 0
0.09 -0.28
0.31 -0.49
1.25 -1
2.5 -1.2
5 -1.4
7.5 -1.55
10 -1.7
15 -1.85
20 -1.95
30 -2
40 -1.9
50 -1.7
60 -1.5
70 -1.2
80 -0.9
90 -0.6
95 -0.35
100 -0.1
V 1.1