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Winfoil Airfoils - Total Number: 277
Name T/C % T/C % Chord Position Camber % Camber Chord % CL Max CD Min
1 2 3 4 5 Next > Last >>
ENG.COR 12.42 26.739 0 0 1.013 0.0084
EPPLER 168 12.42 26.74 0 0 1.035 0.0073
EPPLER 169 14.37 26.46 0 0 1.146 0.0079
HN93-S.800 7.98 25 0 0 0.749 0.0049
HN93-S.885 8.83 25 0 0 0.802 0.0056
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
0.287 0.733 0.287 -0.733
1.095 1.55 1.095 -1.55
2.363 2.38 2.363 -2.38
4.069 3.187 4.069 -3.187
6.198 3.944 6.198 -3.944
8.73 4.627 8.73 -4.627
11.641 5.211 11.641 -5.211
14.915 5.672 14.915 -5.672
18.536 5.995 18.536 -5.995
22.485 6.177 22.485 -6.177
26.739 6.221 26.739 -6.221
31.262 6.134 31.262 -6.134
36.019 5.924 36.019 -5.924
40.972 5.606 40.972 -5.606
46.075 5.2 46.075 -5.2
51.275 4.728 51.275 -4.728
56.516 4.211 56.516 -4.211
61.736 3.673 61.736 -3.673
66.871 3.135 66.871 -3.135
71.854 2.615 71.854 -2.615
76.616 2.13 76.616 -2.13
81.09 1.691 81.09 -1.691
85.21 1.306 85.21 -1.306
88.914 0.979 88.914 -0.979
92.146 0.706 92.146 -0.706
94.855 0.476 94.855 -0.476
97.018 0.271 97.018 -0.271
98.631 0.108 98.631 -0.108
99.649 0.021 99.649 -0.021
100 0 100 0
X Y
1 0
0.99649 0.00021
0.98631 0.00108
0.97018 0.00271
0.94855 0.00476
0.92146 0.00706
0.88914 0.00979
0.8521 0.01306
0.8109 0.01691
0.76616 0.0213
0.71854 0.02615
0.66871 0.03135
0.61736 0.03673
0.56516 0.04211
0.51275 0.04728
0.46075 0.052
0.40972 0.05606
0.36019 0.05924
0.31262 0.06134
0.26739 0.06221
0.22485 0.06177
0.18536 0.05995
0.14915 0.05672
0.11641 0.05211
0.0873 0.04627
0.06198 0.03944
0.04069 0.03187
0.02363 0.0238
0.01095 0.0155
0.00287 0.00733
0 0
0 0
0.00287 -0.00733
0.01095 -0.0155
0.02363 -0.0238
0.04069 -0.03187
0.06198 -0.03944
0.0873 -0.04627
0.11641 -0.05211
0.14915 -0.05672
0.18536 -0.05995
0.22485 -0.06177
0.26739 -0.06221
0.31262 -0.06134
0.36019 -0.05924
0.40972 -0.05606
0.46075 -0.052
0.51275 -0.04728
0.56516 -0.04211
0.61736 -0.03673
0.66871 -0.03135
0.71854 -0.02615
0.76616 -0.0213
0.8109 -0.01691
0.8521 -0.01306
0.88914 -0.00979
0.92146 -0.00706
0.94855 -0.00476
0.97018 -0.00271
0.98631 -0.00108
0.99649 -0.00021
1 0
X Y
100 0
99.649 0.021
98.631 0.108
97.018 0.271
94.855 0.476
92.146 0.706
88.914 0.979
85.21 1.306
81.09 1.691
76.616 2.13
71.854 2.615
66.871 3.135
61.736 3.673
56.516 4.211
51.275 4.728
46.075 5.2
40.972 5.606
36.019 5.924
31.262 6.134
26.739 6.221
22.485 6.177
18.536 5.995
14.915 5.672
11.641 5.211
8.73 4.627
6.198 3.944
4.069 3.187
2.363 2.38
1.095 1.55
0.287 0.733
0 0
0 0
0.287 -0.733
1.095 -1.55
2.363 -2.38
4.069 -3.187
6.198 -3.944
8.73 -4.627
11.641 -5.211
14.915 -5.672
18.536 -5.995
22.485 -6.177
26.739 -6.221
31.262 -6.134
36.019 -5.924
40.972 -5.606
46.075 -5.2
51.275 -4.728
56.516 -4.211
61.736 -3.673
66.871 -3.135
71.854 -2.615
76.616 -2.13
81.09 -1.691
85.21 -1.306
88.914 -0.979
92.146 -0.706
94.855 -0.476
97.018 -0.271
98.631 -0.108
99.649 -0.021
100 0
V 1.1