
Winfoil Airfoils - Total Number: 277
Name | T/C % | T/C % Chord Position | Camber % | Camber Chord % | CL Max | CD Min |
---|---|---|---|---|---|---|
<< First < Prev 43 44 45 46 47 Next > Last >> | ||||||
DF102 | 11 | 29.13 | 2.365 | 43.52 | 1.338 | 0.0054 |
DF101 | 11 | 29.13 | 2.055 | 43.51 | 1.216 | 0.006 |
DAE51 | 9.38 | 30.94 | 3.465 | 46.07 | 1.186 | 0.0078 |
CLARK YS | 11.7 | 30 | 2.353 | 30 | 1.274 | 0.0055 |
CLARK YH | 11.9 | 30 | 2.45 | 30 | 1.392 | 0.0095 |
Coordinates
XUpper | YUpper | XLower | YLower |
---|---|---|---|
0 | -0.09 | 0 | -0.09 |
0.12 | 0.55 | 0.49 | -0.77 |
0.66 | 1.43 | 1.52 | -1.35 |
1.65 | 2.45 | 3 | -1.89 |
3.09 | 3.51 | 4.89 | -2.4 |
4.99 | 4.47 | 7.2 | -2.85 |
7.32 | 5.27 | 9.95 | -3.22 |
10.07 | 5.92 | 13.14 | -3.48 |
13.22 | 6.43 | 16.76 | -3.61 |
16.72 | 6.83 | 20.79 | -3.63 |
20.57 | 7.14 | 25.17 | -3.55 |
24.72 | 7.4 | 29.84 | -3.4 |
29.13 | 7.58 | 34.77 | -3.21 |
33.77 | 7.65 | 39.89 | -2.99 |
38.58 | 7.61 | 45.17 | -2.75 |
43.52 | 7.44 | 50.54 | -2.5 |
48.53 | 7.15 | 55.94 | -2.23 |
53.56 | 6.76 | 61.3 | -1.95 |
58.57 | 6.28 | 66.55 | -1.69 |
63.53 | 5.73 | 71.62 | -1.44 |
68.38 | 5.13 | 76.46 | -1.22 |
73.07 | 4.48 | 80.99 | -1 |
77.56 | 3.81 | 85.17 | -0.79 |
81.79 | 3.12 | 88.92 | -0.59 |
85.7 | 2.45 | 92.2 | -0.39 |
89.25 | 1.82 | 94.94 | -0.23 |
92.38 | 1.26 | 97.13 | -0.11 |
95.03 | 0.79 | 98.72 | -0.05 |
97.16 | 0.44 | 99.68 | -0.02 |
100 | -0.01 | 100 | -0.01 |
X | Y |
---|---|
1 | -0.0001 |
0.9716 | 0.0044 |
0.9503 | 0.0079 |
0.9238 | 0.0126 |
0.8925 | 0.0182 |
0.857 | 0.0245 |
0.8179 | 0.0312 |
0.7756 | 0.0381 |
0.7307 | 0.0448 |
0.6838 | 0.0513 |
0.6353 | 0.0573 |
0.5857 | 0.0628 |
0.5356 | 0.0676 |
0.4853 | 0.0715 |
0.4352 | 0.0744 |
0.3858 | 0.0761 |
0.3377 | 0.0765 |
0.2913 | 0.0758 |
0.2472 | 0.074 |
0.2057 | 0.0714 |
0.1672 | 0.0683 |
0.1322 | 0.0643 |
0.1007 | 0.0592 |
0.0732 | 0.0527 |
0.0499 | 0.0447 |
0.0309 | 0.0351 |
0.0165 | 0.0245 |
0.0066 | 0.0143 |
0.0012 | 0.0055 |
0 | -0.0009 |
0 | -0.0009 |
0.0049 | -0.0077 |
0.0152 | -0.0135 |
0.03 | -0.0189 |
0.0489 | -0.024 |
0.072 | -0.0285 |
0.0995 | -0.0322 |
0.1314 | -0.0348 |
0.1676 | -0.0361 |
0.2079 | -0.0363 |
0.2517 | -0.0355 |
0.2984 | -0.034 |
0.3477 | -0.0321 |
0.3989 | -0.0299 |
0.4517 | -0.0275 |
0.5054 | -0.025 |
0.5594 | -0.0223 |
0.613 | -0.0195 |
0.6655 | -0.0169 |
0.7162 | -0.0144 |
0.7646 | -0.0122 |
0.8099 | -0.01 |
0.8517 | -0.0079 |
0.8892 | -0.0059 |
0.922 | -0.0039 |
0.9494 | -0.0023 |
0.9713 | -0.0011 |
0.9872 | -0.0005 |
0.9968 | -0.0002 |
1 | -0.0001 |
X | Y |
---|---|
100 | -0.01 |
97.16 | 0.44 |
95.03 | 0.79 |
92.38 | 1.26 |
89.25 | 1.82 |
85.7 | 2.45 |
81.79 | 3.12 |
77.56 | 3.81 |
73.07 | 4.48 |
68.38 | 5.13 |
63.53 | 5.73 |
58.57 | 6.28 |
53.56 | 6.76 |
48.53 | 7.15 |
43.52 | 7.44 |
38.58 | 7.61 |
33.77 | 7.65 |
29.13 | 7.58 |
24.72 | 7.4 |
20.57 | 7.14 |
16.72 | 6.83 |
13.22 | 6.43 |
10.07 | 5.92 |
7.32 | 5.27 |
4.99 | 4.47 |
3.09 | 3.51 |
1.65 | 2.45 |
0.66 | 1.43 |
0.12 | 0.55 |
0 | -0.09 |
0 | -0.09 |
0.49 | -0.77 |
1.52 | -1.35 |
3 | -1.89 |
4.89 | -2.4 |
7.2 | -2.85 |
9.95 | -3.22 |
13.14 | -3.48 |
16.76 | -3.61 |
20.79 | -3.63 |
25.17 | -3.55 |
29.84 | -3.4 |
34.77 | -3.21 |
39.89 | -2.99 |
45.17 | -2.75 |
50.54 | -2.5 |
55.94 | -2.23 |
61.3 | -1.95 |
66.55 | -1.69 |
71.62 | -1.44 |
76.46 | -1.22 |
80.99 | -1 |
85.17 | -0.79 |
88.92 | -0.59 |
92.2 | -0.39 |
94.94 | -0.23 |
97.13 | -0.11 |
98.72 | -0.05 |
99.68 | -0.02 |
100 | -0.01 |
V 1.1