
Winfoil Airfoils - Total Number: 277
Name | T/C % | T/C % Chord Position | Camber % | Camber Chord % | CL Max | CD Min |
---|---|---|---|---|---|---|
<< First < Prev 1 2 3 4 5 Next > Last >> | ||||||
SD7084 | 9.63 | 29.51 | 2.325 | 38.87 | 1.173 | 0.0051 |
SD7080 | 9.15 | 30.04 | 2.449 | 39.45 | 1.22 | 0.0052 |
SD7062 | 13.97 | 25.5 | 4.167 | 38.78 | 1.77 | 0.0077 |
SD7043 | 9.13 | 26.64 | 3.664 | 45.28 | 1.461 | 0.0058 |
SD7037 | 9.19 | 26.13 | 2.905 | 44.75 | 1.301 | 0.0062 |
Coordinates
XUpper | YUpper | XLower | YLower |
---|---|---|---|
0 | -0.02 | 0 | -0.02 |
0.26 | 0.63 | 0.29 | -0.55 |
0.99 | 1.41 | 1.17 | -1.03 |
2.13 | 2.26 | 2.58 | -1.44 |
3.69 | 3.11 | 4.51 | -1.79 |
5.64 | 3.93 | 6.96 | -2.07 |
7.99 | 4.7 | 9.88 | -2.3 |
10.71 | 5.37 | 13.25 | -2.46 |
13.8 | 5.95 | 17.03 | -2.56 |
17.25 | 6.4 | 21.19 | -2.61 |
21.04 | 6.73 | 25.68 | -2.6 |
25.14 | 6.96 | 30.45 | -2.55 |
29.51 | 7.07 | 35.46 | -2.45 |
34.1 | 7.07 | 40.63 | -2.31 |
38.87 | 6.98 | 45.93 | -2.14 |
43.79 | 6.79 | 51.29 | -1.95 |
48.78 | 6.51 | 56.65 | -1.74 |
53.82 | 6.15 | 61.94 | -1.52 |
58.83 | 5.73 | 67.12 | -1.3 |
63.77 | 5.25 | 72.11 | -1.08 |
68.58 | 4.72 | 76.85 | -0.87 |
73.22 | 4.15 | 81.3 | -0.69 |
77.62 | 3.56 | 85.38 | -0.52 |
81.75 | 2.94 | 89.05 | -0.38 |
85.58 | 2.31 | 92.25 | -0.27 |
89.06 | 1.71 | 94.94 | -0.18 |
92.17 | 1.16 | 97.09 | -0.11 |
94.85 | 0.71 | 98.67 | -0.04 |
97.03 | 0.36 | 99.66 | -0.01 |
100 | 0 | 100 | 0 |
X | Y |
---|---|
1 | 0 |
0.9703 | 0.0036 |
0.9485 | 0.0071 |
0.9217 | 0.0116 |
0.8906 | 0.0171 |
0.8558 | 0.0231 |
0.8175 | 0.0294 |
0.7762 | 0.0356 |
0.7322 | 0.0415 |
0.6858 | 0.0472 |
0.6377 | 0.0525 |
0.5883 | 0.0573 |
0.5382 | 0.0615 |
0.4878 | 0.0651 |
0.4379 | 0.0679 |
0.3887 | 0.0698 |
0.341 | 0.0707 |
0.2951 | 0.0707 |
0.2514 | 0.0696 |
0.2104 | 0.0673 |
0.1725 | 0.064 |
0.138 | 0.0595 |
0.1071 | 0.0537 |
0.0799 | 0.047 |
0.0564 | 0.0393 |
0.0369 | 0.0311 |
0.0213 | 0.0226 |
0.0099 | 0.0141 |
0.0026 | 0.0063 |
0 | -0.0002 |
0 | -0.0002 |
0.0029 | -0.0055 |
0.0117 | -0.0103 |
0.0258 | -0.0144 |
0.0451 | -0.0179 |
0.0696 | -0.0207 |
0.0988 | -0.023 |
0.1325 | -0.0246 |
0.1703 | -0.0256 |
0.2119 | -0.0261 |
0.2568 | -0.026 |
0.3045 | -0.0255 |
0.3546 | -0.0245 |
0.4063 | -0.0231 |
0.4593 | -0.0214 |
0.5129 | -0.0195 |
0.5665 | -0.0174 |
0.6194 | -0.0152 |
0.6712 | -0.013 |
0.7211 | -0.0108 |
0.7685 | -0.0087 |
0.813 | -0.0069 |
0.8538 | -0.0052 |
0.8905 | -0.0038 |
0.9225 | -0.0027 |
0.9494 | -0.0018 |
0.9709 | -0.0011 |
0.9867 | -0.0004 |
0.9966 | -0.0001 |
1 | 0 |
X | Y |
---|---|
100 | 0 |
97.03 | 0.36 |
94.85 | 0.71 |
92.17 | 1.16 |
89.06 | 1.71 |
85.58 | 2.31 |
81.75 | 2.94 |
77.62 | 3.56 |
73.22 | 4.15 |
68.58 | 4.72 |
63.77 | 5.25 |
58.83 | 5.73 |
53.82 | 6.15 |
48.78 | 6.51 |
43.79 | 6.79 |
38.87 | 6.98 |
34.1 | 7.07 |
29.51 | 7.07 |
25.14 | 6.96 |
21.04 | 6.73 |
17.25 | 6.4 |
13.8 | 5.95 |
10.71 | 5.37 |
7.99 | 4.7 |
5.64 | 3.93 |
3.69 | 3.11 |
2.13 | 2.26 |
0.99 | 1.41 |
0.26 | 0.63 |
0 | -0.02 |
0 | -0.02 |
0.29 | -0.55 |
1.17 | -1.03 |
2.58 | -1.44 |
4.51 | -1.79 |
6.96 | -2.07 |
9.88 | -2.3 |
13.25 | -2.46 |
17.03 | -2.56 |
21.19 | -2.61 |
25.68 | -2.6 |
30.45 | -2.55 |
35.46 | -2.45 |
40.63 | -2.31 |
45.93 | -2.14 |
51.29 | -1.95 |
56.65 | -1.74 |
61.94 | -1.52 |
67.12 | -1.3 |
72.11 | -1.08 |
76.85 | -0.87 |
81.3 | -0.69 |
85.38 | -0.52 |
89.05 | -0.38 |
92.25 | -0.27 |
94.94 | -0.18 |
97.09 | -0.11 |
98.67 | -0.04 |
99.66 | -0.01 |
100 | 0 |
V 1.1