Airfoil:

mm

Job Status

Please wait while the PDF is generated...

Plot Number:

File:

Search for Airfoil
Winfoil Airfoils - Total Number: 277
Name T/C % Camber % Camber Chord % CL Max CD Min
<< First < Prev 42 43 44 45 46 Next > Last >>
EPPLER 169 14.37 0 0 1.146 0.0079
EPPLER 168 12.42 0 0 1.035 0.0073
EPPLER 1200 16.93 3.48 40.77 1.818 0.0072
ENG.COR 12.42 0 0 1.013 0.0084
DF103 11.16 2.181 44.98 1.166 0.0069
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
0.29 0.81 0.29 -0.81
1.11 1.72 1.11 -1.72
2.38 2.65 2.38 -2.65
4.09 3.56 4.09 -3.56
6.21 4.42 6.21 -4.42
8.72 5.21 8.72 -5.21
11.61 5.89 11.61 -5.89
14.84 6.45 14.84 -6.45
18.41 6.85 18.41 -6.85
22.29 7.11 22.29 -7.11
26.46 7.2 26.46 -7.2
30.88 7.12 30.88 -7.12
35.56 6.88 35.56 -6.88
40.44 6.51 40.44 -6.51
45.5 6.03 45.5 -6.03
50.68 5.47 50.68 -5.47
55.91 4.86 55.91 -4.86
61.15 4.23 61.15 -4.23
66.32 3.59 66.32 -3.59
71.35 2.98 71.35 -2.98
76.17 2.41 76.17 -2.41
80.71 1.9 80.71 -1.9
84.9 1.45 84.9 -1.45
88.67 1.08 88.67 -1.08
91.97 0.77 91.97 -0.77
94.74 0.51 94.74 -0.51
96.95 0.29 96.95 -0.29
98.6 0.11 98.6 -0.11
99.64 0.02 99.64 -0.02
100 0 100 0
V 1.0