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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 26 27 28 29 30 Next > Last >>
NACA 1111 10.99 31.65 0.996 9.52 0.937 0.0095
NACA 0219 18.99 28.73 0 0 1.427 0.013
NACA 0016 15.91 27.3202 0 0 1.332 0.0106
NACA 0015 15.01 28.73 0 0 1.287 0.0064
NACA 0012 11.96 30 0 0 1.108 0.0092
Coordinates
XUpper YUpper XLower YLower
0 0 0 0.52
0.21 1.06 0.2 -0.48
0.62 1.62 0.58 -0.9
1.25 2.2 1.15 -1.28
2.09 2.78 1.89 -1.62
3.15 3.35 2.8 -1.92
4.43 3.9 3.87 -2.19
5.92 4.41 5.09 -2.45
7.62 4.85 6.46 -2.7
9.52 5.22 7.96 -2.95
11.48 5.51 9.59 -3.22
13.57 5.75 11.48 -3.51
15.79 5.97 13.56 -3.76
18.15 6.14 15.78 -3.97
20.64 6.28 18.13 -4.16
23.24 6.38 20.61 -4.31
25.95 6.43 23.21 -4.42
28.76 6.45 25.91 -4.5
31.65 6.44 28.71 -4.54
34.61 6.39 31.59 -4.55
37.63 6.3 34.54 -4.54
40.7 6.18 37.55 -4.49
43.81 6.03 40.62 -4.41
46.94 5.85 43.72 -4.31
50.08 5.65 46.85 -4.19
53.22 5.43 49.98 -4.05
56.35 5.19 53.12 -3.89
59.46 4.93 56.25 -3.72
62.52 4.65 59.35 -3.53
65.54 4.37 62.42 -3.33
68.49 4.07 65.44 -3.13
71.37 3.77 68.39 -2.92
74.17 3.47 71.28 -2.7
76.87 3.17 74.08 -2.49
79.47 2.87 76.78 -2.27
81.95 2.57 79.38 -2.06
84.3 2.28 81.87 -1.85
86.51 2 84.23 -1.64
88.59 1.73 86.45 -1.44
90.51 1.47 88.53 -1.25
92.27 1.23 90.46 -1.07
93.86 1.01 92.22 -0.9
95.28 0.81 93.82 -0.75
96.52 0.63 95.25 -0.6
97.58 0.48 96.5 -0.48
98.45 0.35 97.56 -0.37
99.13 0.25 98.44 -0.28
99.62 0.17 99.12 -0.21
99.9 0.1318 99.61 -0.16
99.91 0.13 99.9 -0.13
100 0.12 100 -0.12
X Y
1 0.0012
0.9991 0.0013
0.999 0.001318
0.9962 0.0017
0.9913 0.0025
0.9845 0.0035
0.9758 0.0048
0.9652 0.0063
0.9528 0.0081
0.9386 0.0101
0.9227 0.0123
0.9051 0.0147
0.8859 0.0173
0.8651 0.02
0.843 0.0228
0.8195 0.0257
0.7947 0.0287
0.7687 0.0317
0.7417 0.0347
0.7137 0.0377
0.6849 0.0407
0.6554 0.0437
0.6252 0.0465
0.5946 0.0493
0.5635 0.0519
0.5322 0.0543
0.5008 0.0565
0.4694 0.0585
0.4381 0.0603
0.407 0.0618
0.3763 0.063
0.3461 0.0639
0.3165 0.0644
0.2876 0.0645
0.2595 0.0643
0.2324 0.0638
0.2064 0.0628
0.1815 0.0614
0.1579 0.0597
0.1357 0.0575
0.1148 0.0551
0.0952 0.0522
0.0762 0.0485
0.0592 0.0441
0.0443 0.039
0.0315 0.0335
0.0209 0.0278
0.0125 0.022
0.0062 0.0162
0.0021 0.0106
0 0
0 0.0052
0.002 -0.0048
0.0058 -0.009
0.0115 -0.0128
0.0189 -0.0162
0.028 -0.0192
0.0387 -0.0219
0.0509 -0.0245
0.0646 -0.027
0.0796 -0.0295
0.0959 -0.0322
0.1148 -0.0351
0.1356 -0.0376
0.1578 -0.0397
0.1813 -0.0416
0.2061 -0.0431
0.2321 -0.0442
0.2591 -0.045
0.2871 -0.0454
0.3159 -0.0455
0.3454 -0.0454
0.3755 -0.0449
0.4062 -0.0441
0.4372 -0.0431
0.4685 -0.0419
0.4998 -0.0405
0.5312 -0.0389
0.5625 -0.0372
0.5935 -0.0353
0.6242 -0.0333
0.6544 -0.0313
0.6839 -0.0292
0.7128 -0.027
0.7408 -0.0249
0.7678 -0.0227
0.7938 -0.0206
0.8187 -0.0185
0.8423 -0.0164
0.8645 -0.0144
0.8853 -0.0125
0.9046 -0.0107
0.9222 -0.009
0.9382 -0.0075
0.9525 -0.006
0.965 -0.0048
0.9756 -0.0037
0.9844 -0.0028
0.9912 -0.0021
0.9961 -0.0016
0.999 -0.0013
1 -0.0012
X Y
100 0.12
99.91 0.13
99.9 0.1318
99.62 0.17
99.13 0.25
98.45 0.35
97.58 0.48
96.52 0.63
95.28 0.81
93.86 1.01
92.27 1.23
90.51 1.47
88.59 1.73
86.51 2
84.3 2.28
81.95 2.57
79.47 2.87
76.87 3.17
74.17 3.47
71.37 3.77
68.49 4.07
65.54 4.37
62.52 4.65
59.46 4.93
56.35 5.19
53.22 5.43
50.08 5.65
46.94 5.85
43.81 6.03
40.7 6.18
37.63 6.3
34.61 6.39
31.65 6.44
28.76 6.45
25.95 6.43
23.24 6.38
20.64 6.28
18.15 6.14
15.79 5.97
13.57 5.75
11.48 5.51
9.52 5.22
7.62 4.85
5.92 4.41
4.43 3.9
3.15 3.35
2.09 2.78
1.25 2.2
0.62 1.62
0.21 1.06
0 0
0 0.52
0.2 -0.48
0.58 -0.9
1.15 -1.28
1.89 -1.62
2.8 -1.92
3.87 -2.19
5.09 -2.45
6.46 -2.7
7.96 -2.95
9.59 -3.22
11.48 -3.51
13.56 -3.76
15.78 -3.97
18.13 -4.16
20.61 -4.31
23.21 -4.42
25.91 -4.5
28.71 -4.54
31.59 -4.55
34.54 -4.54
37.55 -4.49
40.62 -4.41
43.72 -4.31
46.85 -4.19
49.98 -4.05
53.12 -3.89
56.25 -3.72
59.35 -3.53
62.42 -3.33
65.44 -3.13
68.39 -2.92
71.28 -2.7
74.08 -2.49
76.78 -2.27
79.38 -2.06
81.87 -1.85
84.23 -1.64
86.45 -1.44
88.53 -1.25
90.46 -1.07
92.22 -0.9
93.82 -0.75
95.25 -0.6
96.5 -0.48
97.56 -0.37
98.44 -0.28
99.12 -0.21
99.61 -0.16
99.9 -0.13
100 -0.12
V 1.1