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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 11 12 13 14 15 Next > Last >>
RAF 15 6.45 15 2.564 30 1.282 0.0059
RAE(NPL) 5212 11.92 35.49 1.827 69.13 1.408 0.0053
RAE 5214 9.64 30.87 1.433 69.13 1.2 0.0042
RAE 2822 12.09 37.85 1.263 75.71 0.903 0.0066
PRD 2C 8.66 30 3.399 30 1.091 0
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
1.25 1.85 1.25 -0.79
2.5 2.55 2.5 -1.04
5 3.47 5 -1.34
10 4.59 10 -1.47
15 5.2 15 -1.28
20 5.52 20 -0.9
30 5.56 30 -0.35
40 5.31 40 -0.29
50 4.88 50 -0.54
60 4.33 60 -0.85
70 3.66 70 -1.06
80 2.84 80 -0.97
90 1.8 90 -0.79
95 1.19 95 -0.65
100 0 100 0
X Y
1 0
0.95 0.0119
0.9 0.018
0.8 0.0284
0.7 0.0366
0.6 0.0433
0.5 0.0488
0.4 0.0531
0.3 0.0556
0.2 0.0552
0.15 0.052
0.1 0.0459
0.05 0.0347
0.025 0.0255
0.0125 0.0185
0 0
0 0
0.0125 -0.0079
0.025 -0.0104
0.05 -0.0134
0.1 -0.0147
0.15 -0.0128
0.2 -0.009
0.3 -0.0035
0.4 -0.0029
0.5 -0.0054
0.6 -0.0085
0.7 -0.0106
0.8 -0.0097
0.9 -0.0079
0.95 -0.0065
1 0
X Y
100 0
95 1.19
90 1.8
80 2.84
70 3.66
60 4.33
50 4.88
40 5.31
30 5.56
20 5.52
15 5.2
10 4.59
5 3.47
2.5 2.55
1.25 1.85
0 0
0 0
1.25 -0.79
2.5 -1.04
5 -1.34
10 -1.47
15 -1.28
20 -0.9
30 -0.35
40 -0.29
50 -0.54
60 -0.85
70 -1.06
80 -0.97
90 -0.79
95 -0.65
100 0
V 1.1