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Winfoil Airfoils - Total Number: 277
Name T/C % Camber % Camber Chord % CL Max CD Min
<< First < Prev 47 48 49 50 51 Next > Last >>
AH21 6.99 1.766 55.23 0.963 0.0044
AH 79-100 B 10.04 6.542 53.27 1.451 0.0072
AG47ct -02f rot. 4.99 1.326 32.0736 0.867 0.0075
AG47c -03f 5.06 1.365 32.0337 0.851 0.0064
AG46ct -02f rot. 6.08 1.704 31.7373 0.982 0.0076
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
0.27 0.63 0.27 -0.4
1.09 1.24 1.09 -0.77
2.45 1.83 2.45 -1.09
4.32 2.38 4.32 -1.36
6.7 2.89 6.7 -1.58
9.55 3.36 9.55 -1.76
12.84 3.78 12.84 -1.9
16.54 4.15 16.54 -1.98
20.61 4.46 20.61 -2.03
25 4.72 25 -2.04
29.66 4.92 29.66 -2.01
34.55 5.05 34.55 -1.94
39.6 5.12 39.6 -1.84
44.77 5.12 44.77 -1.71
50 5.05 50 -1.56
55.23 4.92 55.23 -1.39
60.4 4.71 60.4 -1.21
65.45 4.44 65.45 -1.01
70.34 4.12 70.34 -0.82
75 3.73 75 -0.63
79.39 3.3 79.39 -0.44
83.46 2.83 83.46 -0.28
87.16 2.33 87.16 -0.13
90.45 1.83 90.45 -0.02
93.3 1.35 93.3 0.05
95.68 0.9 95.68 0.08
97.55 0.52 97.55 0.08
98.91 0.23 98.91 0.05
99.73 0.06 99.73 0.01
100 0 100 0
X Y
1 0
0.9973 0.0006
0.9891 0.0023
0.9755 0.0052
0.9568 0.009
0.933 0.0135
0.9045 0.0183
0.8716 0.0233
0.8346 0.0283
0.7939 0.033
0.75 0.0373
0.7034 0.0412
0.6545 0.0444
0.604 0.0471
0.5523 0.0492
0.5 0.0505
0.4477 0.0512
0.396 0.0512
0.3455 0.0505
0.2966 0.0492
0.25 0.0472
0.2061 0.0446
0.1654 0.0415
0.1284 0.0378
0.0955 0.0336
0.067 0.0289
0.0432 0.0238
0.0245 0.0183
0.0109 0.0124
0.0027 0.0063
0 0
0 0
0.0027 -0.004
0.0109 -0.0077
0.0245 -0.0109
0.0432 -0.0136
0.067 -0.0158
0.0955 -0.0176
0.1284 -0.019
0.1654 -0.0198
0.2061 -0.0203
0.25 -0.0204
0.2966 -0.0201
0.3455 -0.0194
0.396 -0.0184
0.4477 -0.0171
0.5 -0.0156
0.5523 -0.0139
0.604 -0.0121
0.6545 -0.0101
0.7034 -0.0082
0.75 -0.0063
0.7939 -0.0044
0.8346 -0.0028
0.8716 -0.0013
0.9045 -0.0002
0.933 0.0005
0.9568 0.0008
0.9755 0.0008
0.9891 0.0005
0.9973 0.0001
1 0
X Y
100 0
99.73 0.06
98.91 0.23
97.55 0.52
95.68 0.9
93.3 1.35
90.45 1.83
87.16 2.33
83.46 2.83
79.39 3.3
75 3.73
70.34 4.12
65.45 4.44
60.4 4.71
55.23 4.92
50 5.05
44.77 5.12
39.6 5.12
34.55 5.05
29.66 4.92
25 4.72
20.61 4.46
16.54 4.15
12.84 3.78
9.55 3.36
6.7 2.89
4.32 2.38
2.45 1.83
1.09 1.24
0.27 0.63
0 0
0 0
0.27 -0.4
1.09 -0.77
2.45 -1.09
4.32 -1.36
6.7 -1.58
9.55 -1.76
12.84 -1.9
16.54 -1.98
20.61 -2.03
25 -2.04
29.66 -2.01
34.55 -1.94
39.6 -1.84
44.77 -1.71
50 -1.56
55.23 -1.39
60.4 -1.21
65.45 -1.01
70.34 -0.82
75 -0.63
79.39 -0.44
83.46 -0.28
87.16 -0.13
90.45 -0.02
93.3 0.05
95.68 0.08
97.55 0.08
98.91 0.05
99.73 0.01
100 0
V 1.1