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Winfoil Airfoils - Total Number: 277
Name T/C % T/C % Chord Position Camber % Camber Chord % CL Max CD Min
< Prev 1 2 3 4 5 Next > Last >>
J5012 11.99 34.55 0 0 1.039 0.0053
NACA 0008 7.98 30 0 0 0.765 0.0064
NACA 0009 8.97 30 0 0 0.871 0.0065
NACA 0010 9.97 30 0 0 0.877 0.0016
NACA 0012 11.96 30 0 0 1.108 0.0092
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
0.27 0.81 0.27 -0.81
1.09 1.61 1.09 -1.61
2.45 2.38 2.45 -2.38
4.32 3.1 4.32 -3.1
6.7 3.77 6.7 -3.77
9.55 4.36 9.55 -4.36
12.84 4.87 12.84 -4.87
16.54 5.29 16.54 -5.29
20.61 5.62 20.61 -5.62
25 5.85 25 -5.85
29.66 5.98 29.66 -5.98
34.55 6 34.55 -6
39.6 5.93 39.6 -5.93
44.77 5.76 44.77 -5.76
50 5.51 50 -5.51
55.23 5.19 55.23 -5.19
60.4 4.8 60.4 -4.8
65.45 4.36 65.45 -4.36
70.34 3.88 70.34 -3.88
75 3.38 75 -3.38
79.39 2.86 79.39 -2.86
83.46 2.36 83.46 -2.36
87.16 1.87 87.16 -1.87
90.45 1.42 90.45 -1.42
93.3 1.01 93.3 -1.01
95.68 0.66 95.68 -0.66
97.55 0.38 97.55 -0.38
98.91 0.17 98.91 -0.17
99.73 0.04 99.73 -0.04
100 0 100 0
X Y
1 0
0.9973 0.0004
0.9891 0.0017
0.9755 0.0038
0.9568 0.0066
0.933 0.0101
0.9045 0.0142
0.8716 0.0187
0.8346 0.0236
0.7939 0.0286
0.75 0.0338
0.7034 0.0388
0.6545 0.0436
0.604 0.048
0.5523 0.0519
0.5 0.0551
0.4477 0.0576
0.396 0.0593
0.3455 0.06
0.2966 0.0598
0.25 0.0585
0.2061 0.0562
0.1654 0.0529
0.1284 0.0487
0.0955 0.0436
0.067 0.0377
0.0432 0.031
0.0245 0.0238
0.0109 0.0161
0.0027 0.0081
0 0
0 0
0.0027 -0.0081
0.0109 -0.0161
0.0245 -0.0238
0.0432 -0.031
0.067 -0.0377
0.0955 -0.0436
0.1284 -0.0487
0.1654 -0.0529
0.2061 -0.0562
0.25 -0.0585
0.2966 -0.0598
0.3455 -0.06
0.396 -0.0593
0.4477 -0.0576
0.5 -0.0551
0.5523 -0.0519
0.604 -0.048
0.6545 -0.0436
0.7034 -0.0388
0.75 -0.0338
0.7939 -0.0286
0.8346 -0.0236
0.8716 -0.0187
0.9045 -0.0142
0.933 -0.0101
0.9568 -0.0066
0.9755 -0.0038
0.9891 -0.0017
0.9973 -0.0004
1 0
X Y
100 0
99.73 0.04
98.91 0.17
97.55 0.38
95.68 0.66
93.3 1.01
90.45 1.42
87.16 1.87
83.46 2.36
79.39 2.86
75 3.38
70.34 3.88
65.45 4.36
60.4 4.8
55.23 5.19
50 5.51
44.77 5.76
39.6 5.93
34.55 6
29.66 5.98
25 5.85
20.61 5.62
16.54 5.29
12.84 4.87
9.55 4.36
6.7 3.77
4.32 3.1
2.45 2.38
1.09 1.61
0.27 0.81
0 0
0 0
0.27 -0.81
1.09 -1.61
2.45 -2.38
4.32 -3.1
6.7 -3.77
9.55 -4.36
12.84 -4.87
16.54 -5.29
20.61 -5.62
25 -5.85
29.66 -5.98
34.55 -6
39.6 -5.93
44.77 -5.76
50 -5.51
55.23 -5.19
60.4 -4.8
65.45 -4.36
70.34 -3.88
75 -3.38
79.39 -2.86
83.46 -2.36
87.16 -1.87
90.45 -1.42
93.3 -1.01
95.68 -0.66
97.55 -0.38
98.91 -0.17
99.73 -0.04
100 0
V 1.1