
Winfoil Airfoils - Total Number: 277
Name | T/C % | T/C % Chord Position | Camber % | Camber Chord % | CL Max | CD Min |
---|---|---|---|---|---|---|
<< First < Prev 2 3 4 5 6 Next > Last >> | ||||||
SD7032 | 9.96 | 26.6 | 3.79 | 40.22 | 1.453 | 0.0066 |
SD7003 | 8.5 | 24.36 | 1.584 | 33.41 | 1.124 | 0.0064 |
SD6080 | 9.18 | 30.86 | 3.587 | 39.99 | 1.306 | 0.0051 |
SD6060 | 10.36 | 33.86 | 1.945 | 38.57 | 1.087 | 0.0058 |
SD5060 | 9.45 | 24.93 | 2.343 | 43.51 | 1.217 | 0.006 |
Coordinates
XUpper | YUpper | XLower | YLower |
---|---|---|---|
0.04 | -0.22 | 0.04 | -0.22 |
0.12 | 0.45 | 0.53 | -0.7 |
0.61 | 1.29 | 1.65 | -1.09 |
1.5 | 2.21 | 3.31 | -1.4 |
2.81 | 3.15 | 5.49 | -1.64 |
4.52 | 4.08 | 8.18 | -1.79 |
6.63 | 4.98 | 11.35 | -1.86 |
9.11 | 5.81 | 14.97 | -1.87 |
11.95 | 6.55 | 19.01 | -1.81 |
15.15 | 7.18 | 23.42 | -1.7 |
18.67 | 7.7 | 28.15 | -1.55 |
22.5 | 8.1 | 33.15 | -1.36 |
26.6 | 8.36 | 38.36 | -1.15 |
30.95 | 8.49 | 43.72 | -0.92 |
35.51 | 8.5 | 49.18 | -0.68 |
40.22 | 8.39 | 54.66 | -0.43 |
45.06 | 8.15 | 60.11 | -0.19 |
49.97 | 7.82 | 65.47 | 0.03 |
54.9 | 7.38 | 70.66 | 0.22 |
59.81 | 6.86 | 75.63 | 0.38 |
64.65 | 6.27 | 80.31 | 0.49 |
69.36 | 5.62 | 84.64 | 0.54 |
73.89 | 4.93 | 88.53 | 0.53 |
78.21 | 4.2 | 91.94 | 0.46 |
82.26 | 3.46 | 94.8 | 0.35 |
86.02 | 2.73 | 97.05 | 0.23 |
89.44 | 2.04 | 98.68 | 0.11 |
92.46 | 1.42 | 99.67 | 0.03 |
100 | 0 | 100 | 0 |
X | Y |
---|---|
1 | 0 |
0.9246 | 0.0142 |
0.8944 | 0.0204 |
0.8602 | 0.0273 |
0.8226 | 0.0346 |
0.7821 | 0.042 |
0.7389 | 0.0493 |
0.6936 | 0.0562 |
0.6465 | 0.0627 |
0.5981 | 0.0686 |
0.549 | 0.0738 |
0.4997 | 0.0782 |
0.4506 | 0.0815 |
0.4022 | 0.0839 |
0.3551 | 0.085 |
0.3095 | 0.0849 |
0.266 | 0.0836 |
0.225 | 0.081 |
0.1867 | 0.077 |
0.1515 | 0.0718 |
0.1195 | 0.0655 |
0.0911 | 0.0581 |
0.0663 | 0.0498 |
0.0452 | 0.0408 |
0.0281 | 0.0315 |
0.015 | 0.0221 |
0.0061 | 0.0129 |
0.0012 | 0.0045 |
0.0004 | -0.0022 |
0.0004 | -0.0022 |
0.0053 | -0.007 |
0.0165 | -0.0109 |
0.0331 | -0.014 |
0.0549 | -0.0164 |
0.0818 | -0.0179 |
0.1135 | -0.0186 |
0.1497 | -0.0187 |
0.1901 | -0.0181 |
0.2342 | -0.017 |
0.2815 | -0.0155 |
0.3315 | -0.0136 |
0.3836 | -0.0115 |
0.4372 | -0.0092 |
0.4918 | -0.0068 |
0.5466 | -0.0043 |
0.6011 | -0.0019 |
0.6547 | 0.0003 |
0.7066 | 0.0022 |
0.7563 | 0.0038 |
0.8031 | 0.0049 |
0.8464 | 0.0054 |
0.8853 | 0.0053 |
0.9194 | 0.0046 |
0.948 | 0.0035 |
0.9705 | 0.0023 |
0.9868 | 0.0011 |
0.9967 | 0.0003 |
1 | 0 |
X | Y |
---|---|
100 | 0 |
92.46 | 1.42 |
89.44 | 2.04 |
86.02 | 2.73 |
82.26 | 3.46 |
78.21 | 4.2 |
73.89 | 4.93 |
69.36 | 5.62 |
64.65 | 6.27 |
59.81 | 6.86 |
54.9 | 7.38 |
49.97 | 7.82 |
45.06 | 8.15 |
40.22 | 8.39 |
35.51 | 8.5 |
30.95 | 8.49 |
26.6 | 8.36 |
22.5 | 8.1 |
18.67 | 7.7 |
15.15 | 7.18 |
11.95 | 6.55 |
9.11 | 5.81 |
6.63 | 4.98 |
4.52 | 4.08 |
2.81 | 3.15 |
1.5 | 2.21 |
0.61 | 1.29 |
0.12 | 0.45 |
0.04 | -0.22 |
0.04 | -0.22 |
0.53 | -0.7 |
1.65 | -1.09 |
3.31 | -1.4 |
5.49 | -1.64 |
8.18 | -1.79 |
11.35 | -1.86 |
14.97 | -1.87 |
19.01 | -1.81 |
23.42 | -1.7 |
28.15 | -1.55 |
33.15 | -1.36 |
38.36 | -1.15 |
43.72 | -0.92 |
49.18 | -0.68 |
54.66 | -0.43 |
60.11 | -0.19 |
65.47 | 0.03 |
70.66 | 0.22 |
75.63 | 0.38 |
80.31 | 0.49 |
84.64 | 0.54 |
88.53 | 0.53 |
91.94 | 0.46 |
94.8 | 0.35 |
97.05 | 0.23 |
98.68 | 0.11 |
99.67 | 0.03 |
100 | 0 |
V 1.1